X-Planes: North American X-10

The North American X-10 started its engines on a runway, took off on its own undercarriage, climbed to nearly fifteen kilometres, accelerated past Mach two, flew out along a range, turned, came back after about a thousand kilometres, lowered its gear, and landed. No one was aboard for any of it. Thirteen were built and one survives. This article is the eleventh in the X-Planes series, following the X-1, the X-2, the X-3, the X-4, the X-5, the X-6, the X-7, the X-8, and the X-9.

It is the third article in a row whose subject is not conventionally called an aircraft. Of the three, the X-10 makes that description hardest to defend. The X-8 was a sounding rocket and the X-9 was an expendable missile, but the X-10 took off and landed on wheels, was flown repeatedly, and was designed from the outset to be brought home. What separates it from an aircraft is not its shape and not its operation but its purpose, and that purpose needs a precise name, because it turns out to determine everything else about the vehicle. The standard inventory entry is Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50, the designation history is Parsch 2002 RTV-A-5 X-10 with the parent weapon at Parsch 2002 SM-64, the vehicle compilation is Miller 2001 The X-Planes, X-1 to X-45, the programme monograph is Gibson 1996 The Navaho Missile Project, and the class history is Werrell 1985 The Evolution of the Cruise Missile.

The Research Question

The X-10 was the flying testbed for the Navaho, an intercontinental supersonic cruise missile that North American Aviation developed for the Air Force under project MX-770 from 1946. The Navaho was to carry a thermonuclear warhead five thousand five hundred miles at a Mach number near three and arrive close enough to the target to destroy it. The requirement is given in Landis 2020 Flashback, The Navaho Missile, Part 1, the warhead of the final design in Parsch 2002 SM-64, and the Cape history Cleary 1991 The 6555th, The NAVAHO Program states the same range in nautical miles. Every part of that sentence was hard, but only one part had never been done at all.

The Binding Constraint Is Time, Not Speed

Every previous vehicle in this series answered a question that could be asked in a few minutes of flight. The X-1 needed seconds at Mach one. The X-2 needed a few minutes above Mach three. The X-7 needed a ramjet to run long enough to measure it. Even the X-8, whose mission was to observe time above the atmosphere, worked in units of hundreds of seconds.

The Navaho mission is different in kind. At the ten-thousand-kilometre design range of the enlarged XSM-64A and its cruise Mach number of 3.25, which Parsch 2002 SM-64 gives for flight above twenty-four kilometres, and taking the cruise at twenty-four kilometres, where the speed of sound is

\[a = \sqrt{\gamma R T} = \sqrt{1.4 \times 287.05 \times 220.6} = 297.8 \, \text{m/s} \tag{1}\]

the cruise speed is $v = 3.25 \times 297.8 = 967.8$ metres per second and the time of flight over ten thousand kilometres is

\[t = \frac{R_{\text{mission}}}{v} = \frac{1.0 \times 10^{7}}{967.8} = 10{,}333 \, \text{s} = 2.87 \, \text{hours} \tag{2}\]

Nothing in the series so far has had to work for three hours. That single fact reorganises the entire engineering problem, because the dominant error in a self-contained navigation system does not depend on how far the vehicle has flown or how fast. It depends on how long the system has been running. The mission-analysis framing of an intercontinental airbreathing weapon, set against its ballistic competitor, was being argued in the period by Brooks 1961 on the ballistic side and is collected for the airbreathing side in Werrell 1985 The Evolution of the Cruise Missile.

The Specification Is a Drift Rate

A guided weapon is specified by an accuracy. The reported Air Force requirement for the Navaho of 1948 was a circular error probable near eight hundred metres, and the reported performance of its XN-1 inertial navigator was a position error growing at about 1.6 kilometres for every hour of flight. Both figures come from the secondary compilation Wade, Navaho, Encyclopedia Astronautica rather than from a released programme document, later statements of the requirement differ, and the Epistemic State below says so. What can be done with them, and what the sources do not do, is to convert them into a component specification.

The circular error probable is not a self-evident measure and the period argued about it. Shultz 1963 works out what a bias does to it, which matters here because a drift rate is a bias rather than a noise, and Gallagher 1969 collects the statistics of the quantity more generally. Swanson 1963 takes up the navigational version of the question, namely how one estimates the accuracy of a navigation system as distinct from that of a weapon.

An inertial navigator that has no external reference accumulates position error from the drift of its gyroscopes. For a platform held level by feedback from its own computed position, the secular part of that error is

\[\delta x_{\text{secular}} = R_{e} \, \varepsilon \, t \tag{3}\]

where $R_{e}$ is the Earth radius, $\varepsilon$ is the gyroscope drift rate in radians per second, and $t$ is elapsed time. The derivation is below. Inverting it against the requirement gives the drift rate the weapon needed,

\[\varepsilon_{\text{req}} = \frac{\mathrm{CEP}}{R_{e} t} = \frac{800}{6.371 \times 10^{6} \times 10{,}333} = 1.215 \times 10^{-8} \, \text{rad/s} \tag{4}\]

which in the units the gyroscope industry uses is

\[\varepsilon_{\text{req}} = 1.215 \times 10^{-8} \times 206{,}265 = 0.0025 \, \text{deg/hr} \tag{5}\]

and inverting the reported achievement the same way gives

\[\varepsilon_{\text{ach}} = \frac{1600}{6.371 \times 10^{6} \times 3600} = 6.976 \times 10^{-8} \, \text{rad/s} = 0.0144 \, \text{deg/hr} \tag{6}\]

The programme needed two and a half thousandths of a degree per hour and its first navigator delivered about fourteen thousandths. The shortfall is a factor of

\[\frac{\varepsilon_{\text{ach}}}{\varepsilon_{\text{req}}} = \frac{0.0144}{0.0025} = 5.74 \tag{7}\]

and the same factor reappears if the achieved drift is propagated to full range, since $R_{e} \varepsilon_{\text{ach}} t = 4.59$ kilometres against a requirement of 800 metres, a ratio of 5.74. The two routes agree because they are the same relation read in opposite directions, which is a consistency check rather than an independent confirmation. The X-10 exists because in 1950 nobody knew whether the smaller number was reachable, and the programme did not reach it in time.

The Schuler Loop Decides Which Errors Grow and Which Do Not

The reason drift rather than accelerometer quality was the binding problem is not obvious, and it follows from the feedback structure that every inertial navigator of the period used. An accelerometer cannot distinguish acceleration from gravity, so a navigator must know which way is down, and it establishes that from the position it has computed. That closes a loop. Writing $\delta v$ for the velocity error and $\phi$ for the platform tilt, with $\nabla$ the accelerometer bias and $\varepsilon$ the gyroscope drift, the single-channel error equations are

\[\dot{\delta v} = -g \phi + \nabla \tag{8}\] \[\dot{\phi} = \frac{\delta v}{R_{e}} + \varepsilon \tag{9}\]

Differentiating the first and substituting the second eliminates the tilt and leaves a single second-order equation,

\[\ddot{\delta v} + \frac{g}{R_{e}} \delta v = -g \varepsilon \tag{10}\]

The homogeneous solution is a pure oscillation, since the equation has no damping term at all,

\[\delta v_{h}(t) = C_{1} \cos \omega_{s} t + C_{2} \sin \omega_{s} t \tag{11}\]

and the absence of damping follows from the mechanisation and is not an oversight. A damped loop would track gravity rather than the vehicle. This is an undamped oscillator at the Schuler frequency

\[\omega_{s} = \sqrt{\frac{g}{R_{e}}} = \sqrt{\frac{9.80665}{6.371 \times 10^{6}}} = 1.2407 \times 10^{-3} \, \text{rad/s} \tag{12}\]

with period

\[T_{s} = \frac{2\pi}{\omega_{s}} = 5064 \, \text{s} = 84.4 \, \text{minutes} \tag{13}\]

The period depends on the planet and not on the instrument, and it matters here because the two error sources enter the same equation in structurally different places. The accelerometer bias enters as an initial condition on $\dot{\delta v}$ and produces

\[\delta x_{\nabla}(t) = \frac{\nabla}{\omega_{s}^{2}} \left( 1 - \cos \omega_{s} t \right) = \frac{\nabla R_{e}}{g} \left( 1 - \cos \omega_{s} t \right) \tag{14}\]

which is bounded for all time at $2 \nabla R_{e} / g$. The gyroscope drift enters as a forcing term and produces

\[\delta x_{\varepsilon}(t) = -R_{e} \varepsilon \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} \right) \tag{15}\]

which contains a ramp and therefore grows without limit. For an accelerometer bias of one ten-thousandth of a gravity, which is representative of good instruments of the period, the bounded excursion is

\[\delta x_{\nabla,\max} = \frac{2 \times 9.807 \times 10^{-4} \times 6.371 \times 10^{6}}{9.80665} = 1274 \, \text{m} \tag{16}\]

A navigator with a poor accelerometer misses by 1.3 kilometres no matter how long it flies, and a navigator with a poor gyroscope misses by more every minute it stays airborne. This is why the Navaho programme and every programme like it fought over gyroscopes. Staas and Philip C. 1963 sets out the Schuler mechanisation, the error equations in the form used here come from Lange and Parkinson 1965 and Lange and Parkinson 1966, the identification of which error source dominates was worked out by Eisner and Goodman 1964, and the original observation that a pendulum tuned to this period is insensitive to vehicle acceleration is available in translation as Schuler and Slater 1967. Period system descriptions are Slater 1956b, Statsinger 1959, Prizevoits 1961, Whitcombe 1961, and Duncan 1968. Britting 1971 Inertial Navigation Systems Analysis remains the standard treatment and Titterton and Weston 2004 Strapdown Inertial Navigation Technology the modern one.

The Crossover Time Between the Two Errors

Setting the growing error equal to the bounded one gives the time at which drift takes over as the dominant term,

\[R_{e} \varepsilon t_{\times} = \frac{2 \nabla R_{e}}{g} \quad \Longrightarrow \quad t_{\times} = \frac{2 \nabla}{g \varepsilon} \tag{17}\]

and with the numbers above,

\[t_{\times} = \frac{2 \times 9.807 \times 10^{-4}}{9.80665 \times 6.976 \times 10^{-8}} = 2867 \, \text{s} = 47.8 \, \text{minutes} \tag{18}\]

Before forty-eight minutes of flight the accelerometers dominate the error, and after it the gyroscopes do. Hold that number. A flight shorter than the crossover cannot see the drift clearly, and the sections below set it against the X-10’s reported flight durations, which do not fall where the vehicle’s speed would suggest.

How the X-9 Question Differs

The X-9 also had an accuracy specification and also drove it down into components, but the resemblance stops there. The X-9’s error was geometric. It depended on where the missile was relative to its launcher and its target, and the article showed that the two candidate guidance architectures had error gradients of opposite sign in range. Nothing about it depended on the clock.

The X-10’s error is dynamic. It does not care where the missile is. It cares only how long the instruments have been integrating, and no geometry improves it. Only an external observation resets a dynamic error. For that reason the Navaho guidance line from the XN-2 onward coupled its inertial platform to a star tracker, according to Wade, Navaho, Encyclopedia Astronautica.

What the Star Tracker Buys, and What It Costs

A star tracker measures the platform attitude against inertial space, and a measurement of attitude bounds the tilt that the gyroscopes have been allowed to accumulate. A residual tilt $\phi_{0}$ acts on the loop exactly as an acceleration error $g \phi_{0}$ does, so its position consequence is bounded rather than secular, at

\[\delta x_{\phi} = 2 R_{e} \phi_{0} \tag{19}\]

The accuracy goal of the Navaho programme was that at least half of all missiles strike within 1500 feet of the target Cleary 1991 The 6555th, The NAVAHO Program, a circular error probable of 457 metres. Cleary gives it as the goal of the weapon as a whole, and this article applies it to the stellar-inertial system the final design carried. Inverting through the bounded-error route gives a residual tilt of

\[\phi_{0} = \frac{457}{2 \times 6.371 \times 10^{6}} = 3.588 \times 10^{-5} \, \text{rad} = 7.4 \, \text{arcsec} \tag{20}\]

and inverting instead through the cross-track route, in which an azimuth error $\psi$ produces a miss of $\psi$ times the distance flown, gives

\[\psi = \frac{457}{1.0 \times 10^{7}} = 4.572 \times 10^{-5} \, \text{rad} = 9.4 \, \text{arcsec} \tag{21}\]

Two independent inversions of the same reported figure agree within a factor of 1.3, which is weak evidence that the figure is self-consistent and that the instrument implied by it is a star tracker good to something under ten arcseconds in daylight. That was a demanding instrument in the middle 1950s, and of the whole Navaho guidance system it has aged best. Against the pure-inertial performance the improvement is

\[\frac{R_{e} \varepsilon_{\text{ach}} t}{\mathrm{CEP}_{\text{stellar}}} = \frac{4592}{457} = 10.0 \tag{22}\]

a factor of ten. The tracker also sets its own schedule, because drift regrows the fixed error in

\[t_{\text{fix}} = \frac{\mathrm{CEP}_{\text{stellar}}}{R_{e} \varepsilon_{\text{ach}}} = \frac{457}{6.371 \times 10^{6} \times 6.976 \times 10^{-8}} = 1029 \, \text{s} = 17.1 \, \text{minutes} \tag{23}\]

so a mission of nearly three hours needs on the order of ten successful star fixes and cannot tolerate a long cloud deck or a tracker fault. Horsfall 1958 describes stellar-inertial navigation in this period, Blumhagen 1963 applies it to cruise vehicles, Bona and Hutchinson 1965 gives the optimal formulation, and Stevens 1958 makes the aiding argument in general. The celestial practice that the automatic tracker mechanised appears in Herrick 1946, Franklin 1954, Shufeldt 1961, and Williams 1966, and the tracker engineering itself occupies Klestadt 1971, Ogletree et al. 1972b, and Schenkel 1974.

The Vertical Channel Is Unstable, Not Merely Inaccurate

The horizontal channels oscillate at the Schuler period and are therefore well behaved. The vertical channel is not, and the difference is qualitative. Gravity decreases with altitude, so a navigator that believes it is too high computes a gravity too small, under-corrects its measured acceleration, and concludes that it is higher still. Linearising the gravity gradient gives

\[\ddot{\delta h} = \frac{2g}{R_{e}} \delta h \tag{24}\]

which has no oscillatory solution at all. It is a pure exponential with time constant

\[\tau_{v} = \sqrt{\frac{R_{e}}{2g}} = \sqrt{\frac{6.371 \times 10^{6}}{19.613}} = 570 \, \text{s} \tag{25}\]

and a doubling time of

\[t_{2} = \tau_{v} \ln 2 = 395 \, \text{s} = 6.6 \, \text{minutes} \tag{26}\]

Over the Navaho’s mission this is 18.1 e-foldings, a growth factor of

\[e^{10{,}333 / 570} = 7.5 \times 10^{7} \tag{27}\]

A purely inertial altitude is not merely poor over three hours, it is meaningless. Any inertial navigator intended for sustained flight must therefore bound its vertical channel with an external measurement, which in this period meant a barometric altimeter, and the resulting hybrid is not a detail of implementation but a structural necessity. Aschaffenburg 1962 designs such a system, and Grammatikos et al. 1967 treats the damping of inertial systems generally. For aiding from other external references of the period see Fegley and Weygandt 1963 on Doppler radar and De Groot 1965 on Loran, both of which the Navaho rejected because both require transmissions the mission could not rely on.

The Gravity Field Has to Be Known Over the Target Country

An accelerometer measures specific force and the navigator subtracts a modelled gravity to obtain acceleration. Where the real gravity vector is not where the model says, the residual enters exactly as a tilt does. A deflection of the vertical $\xi$ therefore produces a bounded position error of

\[\delta x_{\xi} = 2 R_{e} \xi \tag{28}\]

and deflections are typically under ten arcseconds over flat terrain and reach an arcminute over mountains Vertical deflection, giving

\[\delta x_{\xi} = 2 \times 6.371 \times 10^{6} \times \frac{10}{206{,}265} = 618 \, \text{m} \tag{29}\]

for ten arcseconds. That is seventy-seven percent of the entire eight-hundred-metre accuracy requirement, consumed by not knowing the shape of the Earth’s gravity field along the flight path. The error is deterministic rather than random, so it could in principle be compensated, but only by surveying gravity along a route that crosses the territory the weapon is aimed at. Of all the terms in the budget, it is the only one that no instrument improvement addresses, and accounts of the programme rarely mention it.

The geodetic side of the problem is Hagiwara 1972, which gives truncation-error formulas for the geoidal height and the deflection of the vertical, with a regional example of how large real anomalies get in Talwani 1966. The eventual answer was to measure the field in flight rather than to survey it beforehand, an idea that arrived two decades too late for the Navaho and appears as gravity-gradiometer aiding in Grubin 1975, Metzger and Jircitano 1975, and Gerber 1975.

The Platform Oven Is a First-Order Component

Gyroscope drift is temperature dependent, and to first order the dependence is linear,

\[\varepsilon(T) = \varepsilon_{0} + k_{T} \left( T - T_{0} \right) \tag{30}\]

with a representative sensitivity $k_{T}$ for instruments of the period on the order of a hundredth of a degree per hour for each kelvin. Requiring the drift specification of 0.0025 degrees per hour to be held against that sensitivity implies a platform temperature control of

\[\Delta T = \frac{\varepsilon_{\text{req}}}{k_{T}} = \frac{0.0025}{0.01} = 0.25 \, \text{K} \tag{31}\]

and letting the platform wander by a single kelvin would produce

\[\varepsilon = 0.01 \times 1 = 0.01 \, \text{deg/hr} \tag{32}\]

which is four times the entire requirement from one degree of temperature error.

A quarter of a kelvin, held for three hours, inside an airframe whose skin is at a hundred degrees Celsius or more. The temperature-controlled oven around an inertial platform is usually described as packaging. It is not. The oven is the component that makes the drift specification meaningful, and it must hold against the thermal environment computed in the section The Structure, and the Temperature That Bounds It. The transient involved was being characterised at the time by Mahlmeister et al. 1955 and Chen 1958, the latter treating the skin temperature and thermal stress problem of sustained high-speed flight, with the honeycomb case in Kendall and Gonzalez 1965.

The Budget Does Not Close

Independent contributions to a radial error combine in quadrature,

\[\sigma_{\text{total}} = \sqrt{\sum_{i} \sigma_{i}^{2}} \tag{33}\]

which has the property that the largest term dominates far more strongly than a linear sum would suggest, since each term enters through its square. Collecting the terms at full range gives for the pure inertial case

\[\sigma_{\text{total}} = \sqrt{4592^{2} + 1274^{2} + 2909^{2} + 618^{2}} = 5617 \, \text{m} \tag{34}\]

against an eight-hundred-metre requirement, a factor of 7.0. That is consistent with the reported failure to meet the requirement and requires no comment. What the quadrature form does add is a statement of where the error lives. The variance shares are

\[\frac{\sigma_{i}^{2}}{\sigma_{\text{total}}^{2}} = 0.668, \; 0.268, \; 0.051, \; 0.012 \tag{35}\]

for drift, azimuth alignment, accelerometer bias, and gravity deflection respectively. Two terms carry ninety-four percent of the variance and both of them are attitude errors, one accumulated in flight and one built in before the vehicle moved. These shares quantify the observation, made in the section Alignment on the Ground Is the Equal of Drift in the Air, that ground alignment and airborne drift are coequal partners. The stellar-inertial case is the uncomfortable one. Replacing the drift and alignment terms with the reported stellar residual and keeping the others gives

\[\sigma_{\text{stellar}} = \sqrt{457^{2} + 1274^{2} + 618^{2}} = 1488 \, \text{m} \tag{36}\]

against the programme’s accuracy goal of 457 metres, which the budget exceeds by a factor of 3.3. Worse, the deflection-of-the-vertical term alone is 618 metres, so at the assumed values it exceeds the reported figure by itself and leaves no room for anything else.

Three readings are available and the article does not choose between them. The instruments may have been substantially better than the representative values assumed here, in which case the assumptions rather than the goal are wrong. The figure may never have been demonstrated at all, since the sources give it as a goal and the Air Force history Landis 2020 Navaho Missile Program, Part 2 records the requirement as eventually relaxed to a circular error probable of 12,000 feet after 5,000 miles of flight. Or, and this is the reading least often stated, any demonstration was flown down the Atlantic Missile Range, whose gravity field was surveyed and whose geometry was known, and not over the territory the weapon was designed to cross. An accuracy measured where the gravity field is known is not evidence of accuracy where it is not. The Epistemic State records this as inference rather than fact.

Building such a budget was itself a subject of study in the period, not a routine exercise. Swanson 1963 gives the statistical method for estimating navigation-system accuracy from component data, Remmler and Theobald 1967 performs the error analysis for a system combining inertial guidance with radar, and Dusek 1964a does it for the astro-inertial architecture that the Navaho flew.

Alignment on the Ground Is the Equal of Drift in the Air

A further inversion is useful because it constrains an operation and not a component. An azimuth misalignment at launch produces a cross-track error proportional to distance flown, so

\[\delta y = \psi \, R_{\text{mission}} \tag{37}\]

and at ten thousand kilometres a misalignment of one arcminute produces

\[\delta y = 2.909 \times 10^{-4} \times 1.0 \times 10^{7} = 2909 \, \text{m} \tag{38}\]

Running it the other way, the achieved drift error of 4.59 kilometres is equivalent to an azimuth misalignment of 1.58 arcminutes. A minute and a half of arc in how the missile is pointed before it moves is worth as much as three hours of gyroscope drift, which means the ground alignment procedure was not a preliminary to the guidance problem but a coequal part of it. Alignment and initialisation are treated in Dasaro 1970 and Sutherland et al. 1968, which Maybeck 1973 and Hellings 1973 later extended.

Programme Origin

North American Aviation received the MX-770 contract in 1946 for a supersonic surface-to-surface missile, initially of modest range, and the requirement grew repeatedly until it became intercontinental, a history set out in Landis 2020 Flashback, The Navaho Missile, Part 1 and Navaho. The growth is the most important fact about the programme and it is usually reported as a footnote. A weapon specified at a few hundred nautical miles and a weapon specified at five thousand five hundred are not the same weapon scaled, because the navigation error of a self-contained system grows with flight time while the target does not get larger. The proportionality is exact. Substituting the mission time $t = R_{m}/v$ into the drift inversion above gives

\[\varepsilon_{\text{req}} = \frac{\mathrm{CEP}}{R_{e} t} = \frac{\mathrm{CEP} \, v}{R_{e} R_{m}} \tag{39}\]

so at fixed accuracy and fixed cruise speed the tolerable drift rate is inversely proportional to the range requirement. Growing the mission from five hundred miles to five thousand five hundred therefore tightens the gyroscope specification by

\[\frac{\varepsilon_{1}}{\varepsilon_{2}} = \frac{R_{m,2}}{R_{m,1}} = \frac{5500}{500} = 11 \tag{40}\]

and from the lower end of the original study range, which began at one hundred and seventy-five miles, the factor is 31.4. Nobody ordering the X-10 in 1950 knew which of those factors the vehicle would have to demonstrate, because the range requirement was still moving, and the vehicle that had to prove compliance was contracted before the number it was proving against had settled.

The technical inheritance was German. Wartime German work on long-range guided weapons, both the ballistic line that produced the V-2 and the winged A4b, which was launched only twice, was distributed among American contractors after 1945, and North American received captured documents, two V-2 engines to study, and a German engineer as its liaison with the Army’s German team, as the Navaho entry records. The engine work is the thread that outlived everything else in the programme, and a captured-programme engine study of this kind is Singelmann and Mueller 1948. Where that thread led is visible in the Redstone programme history of Bullard 1965 and, at the level of a released engine specification, in Scott 1963, which documents a Rocketdyne sustainer of the line the Navaho booster work founded. The free-flight measurement technique that the American programmes used on their own missiles from the outset is Delsasso et al. 1948. The parallel American effort at Northrop under MX-775 produced the subsonic Snark, whose free-flight aerodynamic testing appears in the same National Advisory Committee for Aeronautics series as that of the X-10 and is cited below, and the two programmes are the airbreathing halves of a competition that the ballistic missiles eventually won outright. The MX-775 origin of the Snark is recorded in Wade, Navaho, Encyclopedia Astronautica.

The programme resolved into three flying articles. The X-10 was the aerodynamic and guidance testbed, turbojet powered and recoverable. The G-26, designated XSM-64, was the ramjet-powered vehicle launched by a liquid rocket booster. The G-38, designated XSM-64A, was the enlarged full-range weapon. Only the first two flew. The three phases and their designations are those of Parsch 2002 SM-64.

Setting the three side by side shows how little of the weapon the testbed represented.

	X-10	G-26, XSM-64	G-38, XSM-64A
Role	aerodynamic and guidance testbed	ramjet test and evaluation	full-range weapon
Cruise propulsion	two Westinghouse J40 turbojets	two Wright XRJ47-W-5 ramjets	two Wright XRJ47-W-7 ramjets
Launch	runway take-off, own power	liquid rocket booster	liquid rocket booster
Recovery	runway landing, reusable	expendable	expendable
Cruise Mach	2.05 demonstrated	2.75 design	3.25 design
Cruise altitude	about 13.7 km	about 24 km	above 24 km
Range	about 1000 to 1400 km reported	5600 km design	10,000 km design
Structure	aluminium	elevated-temperature	elevated-temperature
Guidance	radio command, then N-6	N-6 stellar-inertial	N-6 stellar-inertial
Warhead	none	none carried	W-39 thermonuclear

No row of that table reads the same across all three columns. What the three shared was the canard configuration, which the table does not list, and the N-6 guidance system, which Parsch 2002 RTV-A-5 X-10 records the X-10 as carrying only after its radio-command phase. Everything else that decided whether the weapon worked changed between the testbed and the weapon. The table thus condenses an argument the article makes at length below.

The designation history is unusually tangled even by the standards of this series. The vehicle was ordered as RTV-A-5 in 1950 and redesignated X-10 in 1951, by the account of Parsch 2002 RTV-A-5 X-10, while the weapon itself passed through SSM-A-2, XB-64, and XSM-64. The X-10 therefore received an X designation not because it was a research aeroplane but because the research-and-test-vehicle series it had been assigned to was folded into the X series. The same is true of three consecutive designations. The X-8 was RTV-A-1, the X-9 was RTV-A-4, and the X-10 was RTV-A-5. The X-9 and the X-10 both became X numbers in 1951, when the Air Force assigned aircraft designations to its guided missiles Parsch 2002 SM-64, and the X-8’s article dates its change to the same year, May 1951 in the compiler’s account. Three anomalies that look like three separate puzzles are one administrative act seen three times, which is a considerably duller explanation than the vehicles deserve and is probably the correct one, although for the X-8 it rests on the compiler’s statement that the series moved together, since no document located names the X-8 at the change. The series returns to it in its synthesis article.

What a Recoverable Testbed Was For

The X-10’s recoverability is usually described as a cost measure, and cost was certainly part of it, but the deeper reason follows from what the vehicle was measuring. A drift rate is not a number but a distribution. Two gyroscopes from the same production run drift at different rates, the same gyroscope drifts differently on different days, and the quantity a weapon programme needs is the spread rather than a single value. Estimating a spread requires repetition.

For a normally distributed quantity the relative precision of an estimated standard deviation from $n$ samples is approximately

\[\frac{\sigma_{s}}{s} \approx \frac{1}{\sqrt{2(n-1)}} \tag{41}\]

so pinning a drift standard deviation to within twenty percent requires

\[n = 1 + \frac{1}{2 (0.2)^{2}} = 13.5 \, \text{flights} \tag{42}\]

and to within thirty percent still requires between six and seven. The appendix of X-10 launchings in Werrell 1985 The Evolution of the Cruise Missile, compiled from the Air Force Systems Command index of missile launchings, lists five autonavigator tests, on 5 June, 18 July, 21 September, 24 October and 20 November 1956, and the flight chronology of Wade, Navaho, Encyclopedia Astronautica describes the first four as inertial navigation tests, so five flights give

\[\frac{\sigma_{s}}{s} = \frac{1}{\sqrt{2 \times 4}} = 0.354 \tag{43}\]

a thirty-five percent uncertainty on the very quantity the programme was trying to establish. The same chronology records the flights of 5 June and 18 July as aborted by computer failures, and if only the other three produced navigator data the uncertainty is

\[\frac{\sigma_{s}}{s} = \frac{1}{\sqrt{2 \times 2}} = 0.50 \tag{44}\]

or fifty percent. Reusability was the instrument that was supposed to fix this, and the flight test record below shows that it did not, because the fleet was consumed faster than it accumulated flights. The statistical background is in Papoulis 2002 Probability, Random Variables and Stochastic Processes, and Amacker 1967 treats inertial system testing as a discipline.

Sizing From First Principles

The Navigation Flights Outlasted the Crossover Time

The reported flight durations can be set against the crossover directly. The appendix of launchings in Werrell 1985 The Evolution of the Cruise Missile gives a duration for every Edwards flight. Fourteen of the fifteen lasted less than forty-eight minutes, most of them between thirty-one and forty-two, and the exception was a subsonic range and telemetry test of 72.5 minutes on 5 May 1954. Those flights were flown under radio command and carried no N-6, so they bear on the airframe and not on the drift. The appendix gives no durations for the Cape flights. The chronology of Wade, Navaho, Encyclopedia Astronautica gives three, a long-range flight of 51 minutes at Mach 1.9 on 3 February 1956, a flight of 62 minutes that reached Mach 2.1 on 29 February 1956, and an N-6 navigation flight of 79 minutes on 21 September 1956. Against the crossover time these are 1.07, 1.30 and 1.65 times it.

The one autonavigator flight whose duration is reported lasted well past the crossover and nearly a full Schuler period. Seventy-nine minutes is 0.94 of the 84.4-minute period. The durations of the other autonavigator flights are not in the accessible record, and the conclusion of this section rests on that single reported figure.

A short window arises only for a flight made at top speed throughout. The X-10’s longest reported flight at the Cape covered 627 miles, about a thousand kilometres North American X-10. Taking that distance as a single leg at its maximum Mach number of 2.05 and a service ceiling near 13,650 metres, both figures from Parsch 2002 RTV-A-5 X-10, where the speed of sound is 295.1 metres per second, the speed is $v = 604.9$ metres per second and the leg takes

\[t_{\text{X-10}} = \frac{1.0 \times 10^{6}}{604.9} = 1653 \, \text{s} = 27.6 \, \text{minutes} \tag{45}\]

Against the crossover time computed above this is

\[\frac{t_{\text{X-10}}}{t_{\times}} = \frac{1653}{2867} = 0.58 \tag{46}\]

A maximum-speed leg of that length would last a little over half the time needed for gyroscope drift to become the dominant error. The two contributions on such a leg are

\[\delta x_{\varepsilon} = R_{e} \varepsilon_{\text{ach}} t_{\text{X-10}} = 735 \, \text{m} \tag{47}\] \[\delta x_{\nabla} = \frac{\nabla R_{e}}{g} \left( 1 - \cos \omega_{s} t_{\text{X-10}} \right) = 931 \, \text{m} \tag{48}\]

so on such a leg the accelerometer term would be the larger of the two. No reported X-10 navigation flight is known to have been that short. A sortie included take-off, climb, the turn and the return to the strip as well as its fastest portion, and the navigator integrated through all of it, so the dash at top speed sets a lower bound on the window and not its length.

Two Errors That a Short Flight Cannot Separate

Being the smaller term is a nuisance. Being an indistinguishable term is fatal, and that was the situation. The measured position error over a flight is a sum of the two shapes,

\[\delta x(t) = A \left( 1 - \cos \omega_{s} t \right) + B \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} \right) \tag{49}\]

and recovering $B$, which carries the drift rate, means separating two functions of time. How well that can be done depends on how nearly parallel the two shapes are over the observation window. Over one full Schuler period the answer is remarkable. Removing means and integrating,

\[\int_{0}^{T_{s}} \left( -\cos \omega_{s} t \right) \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} - \frac{T_{s}}{2} \right) dt = 0 \tag{50}\]

because each of the three resulting integrals vanishes over a whole period. The accelerometer and gyroscope error signatures are exactly orthogonal over one Schuler period, which means a flight of eighty-four minutes separates them perfectly and a flight of any other length does not. Evaluating the correlation numerically over the three windows gives

\[r(t_{\text{X-10}}) = 0.974 \qquad r(T_{s}) = 0.000 \qquad r(t_{\text{Navaho}}) = -0.042 \tag{51}\]

and the cost of that correlation in estimator variance is the usual inflation factor

\[\mathrm{VIF} = \frac{1}{1 - r^{2}} \tag{52}\]

which evaluates to 19.7 on a maximum-speed X-10 leg and 1.002 on a Navaho mission. Over the 79-minute navigation flight the correlation is 0.140 and the inflation 1.02.

Because the correlation depends only on the length of the observation window, the question becomes a design-of-experiments problem with a single free variable, and it has a clean answer. Sweeping the window length and evaluating the inflation factor gives

Window	Correlation	Variance inflation
8.4 min	0.985	34.0
25.3 min	0.977	21.6
42.2 min	0.940	8.60
59.1 min	0.764	2.40
76.0 min	0.237	1.06
84.4 min	0.000	1.00
101.3 min	-0.189	1.04

The optimum is exactly one Schuler period and the penalty for falling short of it is severe and nonlinear. Halving the window from 84 minutes to 42 costs a factor of 8.6 in variance, and halving it again costs a factor of 21.6. A maximum-speed leg sits near the top of that table, and a least-squares separation of the drift rate from it would carry almost twenty times the variance that the same instrumentation would give over a full Schuler period. The reported 79-minute navigation flight sits between the 76.0 and 84.4 minute rows, where the inflation is close to unity. On the reported durations, the length of the observation window does not explain the X-10’s limitation. Nothing in the accessible record suggests that anyone framed the requirement in these terms, so the long navigation flight reached a good window without a design that sought one. What the window calculation leaves standing is the limit on the number of flights computed in the section What a Recoverable Testbed Was For.

The concept has a name and a literature, neither of which existed when the X-10 flew. Identifiability as a property of a system rather than of an estimator was formalised by Aoki 1966 and by Staley and Yue 1970, both of them a decade and more after the programme ended. The estimation machinery that would have been used to separate the terms is Breakwell 1969 and Jones 1970b, and the application of that machinery to terrestrial inertial navigation is Nash 1968. The X-10 was asked to measure a parameter at a time when the question of whether a parameter is measurable had not yet been posed as a question. The reported durations suggest that its one timed navigation flight avoided the difficulty without anyone having posed it.

Flying Slower Would Have Measured More

The result has a consequence that inverts ordinary intuition about testing. Because drift accumulates with time and the crossover is a time, covering the same ground more slowly puts the flight on the correct side of the threshold. Taking the same thousand-kilometre leg at Mach 0.9 at twelve kilometres, where

\[v = M a = 0.9 \times 295.1 = 265.6 \, \text{m/s} \tag{53}\]

the leg takes

\[t_{\text{sub}} = \frac{1.0 \times 10^{6}}{265.6} = 3766 \, \text{s} = 62.8 \, \text{minutes} \tag{54}\]

which is 1.31 times the crossover time, where the supersonic leg reached 0.58 times it. On such a flight the secular term is 1674 metres against a bounded term of 663 metres, the drift now dominating by a factor of 2.5, and the correlation falls to $r = 0.677$ for a variance inflation of 1.85, against 19.7 on the supersonic leg. The subsonic flight is more than ten times more informative about the drift rate than the supersonic one. The reported flights bear the arithmetic out from the other side. The 62-minute flight of 29 February 1956 lasted about as long as this subsonic leg, and the 79-minute navigation flight lasted longer still. Speed shortens a single leg, but a whole sortie need not be short, and the one X-10 navigation flight whose duration is reported was not.

The Configuration, and What Was Actually Measured

The X-10 was a canard delta with twin vertical tails and side-mounted inlets feeding two Westinghouse J40 turbojets. Its wing area of 425 square feet, from North American X-10, is 39.48 square metres and its span of 8.59 metres, from Parsch 2002 RTV-A-5 X-10, gives an aspect ratio of

\[AR = \frac{b^{2}}{S} = \frac{8.59^{2}}{39.48} = 1.87 \tag{55}\]

which is very low and is the signature of a configuration designed for supersonic cruise rather than for efficiency at any other condition. Two wind-tunnel and free-flight investigations of the X-10 configuration survive in the public record and they are the primary technical base for this article. Pfyl 1952 reports tunnel measurements on a 0.07-scale model of the MX-770, and Bond and Swanson 1953 reports a free-flight rocket-boosted 0.12-scale model tested by the Pilotless Aircraft Research Division from Mach 0.8 to 1.7.

The free-flight report states results that are quantitative enough to check against. It finds the canard pitching effectiveness maintained across the speed range with supersonic values somewhat greater than subsonic, the aerodynamic centre moving rearward transonically and forward again supersonically, a drag-rise Mach number near 0.90, a supersonic minimum drag coefficient about twice the subsonic value, and base drag amounting to about twenty-five percent of the configuration’s minimum drag supersonically.

Each of those findings concerns a relation. The aerodynamic centre travel bears on static margin, defined as

\[h_{n} = \frac{x_{ac} - x_{cg}}{\bar{c}} \tag{56}\]

which enters the pitch stiffness directly through

\[C_{m\alpha} = -C_{L\alpha} h_{n} \tag{57}\]

so a seven percent chord movement of the aerodynamic centre, which is a modest transonic shift, changes the pitch stiffness by $-0.21$ per radian at a lift-curve slope of 3.0. Against a small static margin of three percent, whose stiffness is $-0.09$ per radian, that shift is larger than the margin itself. The vehicle does not merely become more or less stable through the transonic region. It changes stability by more than its quiescent value, and that condition makes an autopilot mandatory rather than convenient.

The drag findings decompose the same way. Writing the minimum drag as friction plus wave plus base,

\[C_{D,\min} = C_{D,f} + C_{D,w} + C_{D,b} \tag{58}\]

the reported doubling from subsonic to supersonic makes the wave term equal to the entire subsonic minimum,

\[C_{D,w} = C_{D,\min,\text{sup}} - C_{D,\min,\text{sub}} = 0.040 - 0.020 = 0.020 \tag{59}\]

and the reported base fraction then makes the base term

\[C_{D,b} = 0.25 \times 0.040 = 0.010 \tag{60}\]

which is half of the wave drag and a quarter of the total. Base drag of that size on a configuration with two engine exhausts in the afterbody is large but not anomalous, and a cleaner boat-tail would have attacked it first.

The configuration was not unusual for its moment, and the surrounding literature shows how thoroughly the canard arrangement was being explored just as the X-10 was being built. Canard aerodynamics of the period runs through Crane and Adams 1950, Niewald and Moul 1950, Driver 1957, Sleeman 1957, Driver 1958, Spearman and Robinson 1958, Fournier 1961, Peterson 1961, and Spencer 1961, with the configuration text at Nielsen 1960 Missile Aerodynamics. Arbic and Gillespie 1953 and Gillespie and Arbic 1951 report the comparable free-flight programme on the competing Northrop Snark.

An Inlet Recovering Less Than a Normal Shock

The most striking single measurement in the free-flight report is that duct total-pressure recovery fell with Mach number and was somewhat less than normal-shock recovery. That deserves a benchmark. Across a normal shock the total-pressure ratio is

\[\frac{p_{02}}{p_{01}} = \left[ \frac{\frac{(\gamma+1) M^{2}}{2}}{1 + \frac{\gamma-1}{2} M^{2}} \right]^{\frac{\gamma}{\gamma-1}} \left[ \frac{\gamma+1}{2 \gamma M^{2} - (\gamma-1)} \right]^{\frac{1}{\gamma-1}} \tag{61}\]

which at the top of the tested range gives

\[\left. \frac{p_{02}}{p_{01}} \right|_{M = 1.70} = 0.856 \tag{62}\]

A single normal shock is the crudest supersonic inlet there is, so recovering less than it means the duct was losing more to internal friction, spillage, and diffusion than the shock system was losing to the shock. For comparison, a two-shock inlet using one oblique shock from a sixteen-degree wedge followed by a normal shock, at the vehicle’s maximum Mach number of 2.05, recovers

\[\left. \frac{p_{02}}{p_{01}} \right|_{\text{two-shock}, M = 2.05} = 0.889 \tag{63}\]

against 0.698 for a single normal shock at the same condition, an improvement of

\[\frac{0.889}{0.698} = 1.275 \tag{64}\]

or twenty-seven percent in delivered total pressure. The measured configuration was leaving a large fraction of that on the table, and since net thrust scales roughly with delivered total pressure at fixed geometry, the propulsive consequence is direct. The caution the abstract forces is that this was a 0.12-scale free-flight model, and small ducts at model Reynolds numbers lose more to friction than full-scale ones do, so the measurement bounds the model rather than the vehicle.

Recovery is in any case only half of the inlet problem. What the engine sees is a matched airflow, and the mismatch between what an inlet captures and what a compressor will swallow generates further losses and instabilities. Alford et al. 1962 states the duct-and-engine airflow matching problem for supersonic aircraft directly, Kepler and Barry 1965 and Taylor 1968b carry it into the supersonic transport programme, Campbell and Ellis 1970 gives a compatibility analysis, Mardoc 1970 treats the interaction of distortion with turbulence, and Burstadt et al. 1971 measures the instantaneous and dynamic behaviour. None of that vocabulary existed in 1953, so the X-10’s inlet was designed before the failure modes it had to avoid had been named.

The Vehicle’s Own Speed Record Bounds Its Inlet

That caution can be turned into a quantitative constraint, because the full-scale article demonstrated Mach 2.05 and a machine that cannot balance its drag does not reach a speed. The static pressure at the service ceiling is 14,902 pascals and the isentropic ram total-pressure ratio at Mach 2.05 is

\[\frac{p_{0}}{p_{\infty}} = \left( 1 + \frac{\gamma-1}{2} M^{2} \right)^{\frac{\gamma}{\gamma-1}} = 8.458 \tag{65}\]

so the total pressure delivered to the compressor face, for an inlet of recovery $\eta$, is $14{,}902 \times 8.458 \times \eta$. Scaling the sea-level static installed thrust of 96,971 newtons by the ratio of that quantity to sea-level total pressure, and requiring it to exceed the drag of 75,042 newtons computed above, gives a break-even recovery of

\[\eta_{\min} = \frac{D \, p_{0,\text{SL}}}{T_{\text{static}} \, p_{\infty} \, (p_{0}/p_{\infty})} = 0.622 \tag{66}\]

which is

\[\frac{\eta_{\min}}{\eta_{\text{normal shock}}} = \frac{0.622}{0.698} = 0.892 \tag{67}\]

The full-scale inlet had to recover within about eleven percent of normal-shock values or the vehicle could not have reached the speed it is recorded as reaching. Working the same relation forward, a two-shock inlet gives a thrust margin of 1.43 over drag, a plain normal shock gives 1.12, ninety percent of normal shock gives 1.01, and eighty-five percent gives 0.95 and therefore fails.

This is an inference rather than a measurement and it inherits every assumption in the drag estimate, so it links two uncertain quantities and determines neither. What it does establish is that the free-flight model’s sub-normal-shock duct recovery cannot have been a property of the full-scale inlet at full-scale conditions, because the X-10’s demonstrated performance forbids it. The model-scale explanation is the correct one, and the article can say so on the X-10’s own evidence rather than on a plausibility argument. Supersonic inlet work of the period spans Ferri and Nucci 1951, Hermann 1950, Diggins 1951, Esenwein 1952, Allen and Beke 1953, Kochendorfer 1953, Pfyl 1955, Hermann 1956, Kouyoumjian 1957, Mitchell and Campbell 1957, Yeager and Gertsma 1958, Blackaby et al. 1959, Mickola 1961, and Mahoney 1962, and Seddon and Goldsmith 1999 Intake Aerodynamics gathers the discipline, while Anderson 2002 Modern Compressible Flow supplies the compressible-flow relations.

Drag, and What the Reported Ranges Cannot Mean

Taking the free-flight finding of a supersonic minimum drag coefficient about twice the subsonic value, and a subsonic value of 0.020 as representative for the class, the zero-lift drag at the ceiling and maximum Mach number follows from the dynamic pressure

\[q = \tfrac{1}{2} \rho v^{2} = \tfrac{1}{2} \times 0.2397 \times 604.9^{2} = 43{,}838 \, \text{Pa} \tag{68}\]

giving $D_{0} = 2 C_{D,\text{sub}} q S = 69{,}235$ newtons. The lift coefficient needed to hold level flight at the maximum take-off mass of 19,187 kilogrammes is

\[C_{L} = \frac{W}{q S} = \frac{188{,}160}{43{,}838 \times 39.48} = 0.109 \tag{69}\]

and with an induced-drag factor $k = 1/(\pi AR e) = 0.284$ at an efficiency of 0.6 the induced drag is 5807 newtons, for a total of 75,042 newtons and a lift-to-drag ratio of

\[\frac{L}{D} = \frac{188{,}160}{75{,}042} = 2.51 \tag{70}\]

That figure goes into the range equation. For a jet the Breguet form is

\[R = \frac{v}{g \, c} \frac{L}{D} \ln \frac{W_{0}}{W_{1}} \tag{71}\]

and at a thrust specific fuel consumption of 1.0 per hour, which is generous for an early turbojet, a mass ratio of 1.8 gives

\[R = \frac{604.9}{9.80665 \times (1/3600)} \times 2.51 \times \ln 1.8 = 327 \, \text{km} \tag{72}\]

The mass ratio does not have to be assumed, because the weights are reported in North American X-10. An empty weight of 25,800 pounds is 11,703 kilogrammes and a maximum take-off weight of 42,300 pounds is 19,187 kilogrammes, so the fuel available is 7484 kilogrammes, a fuel fraction of

\[\frac{m_{f}}{m_{0}} = \frac{7484}{19{,}187} = 0.390 \tag{73}\]

and the mass ratio is

\[\frac{W_{0}}{W_{1}} = \frac{19{,}187}{11{,}703} = 1.640 \tag{74}\]

Substituting the reported mass ratio for the guessed one gives a maximum-Mach range of

\[R = \frac{604.9}{9.80665 \times (1/3600)} \times 2.51 \times \ln 1.640 = 275 \, \text{km} \tag{75}\]

The reported ranges of North American X-10 and Parsch 2002 RTV-A-5 X-10 stand in ratio to that as

\[\frac{1009}{275} = 3.67 \qquad \frac{1370}{275} = 4.98 \tag{76}\]

The reported ranges are 3.7 and 5.0 times the computed one. Since the mass ratio now comes from data, the discrepancy has to be absorbed by the lift-to-drag ratio, by the specific fuel consumption, or by the cruise speed. Working the relation backwards for a subsonic cruise at Mach 0.9, the lift-to-drag ratio required to reach the smaller reported range is

\[\frac{L}{D} = \frac{R g c}{v \ln (W_{0}/W_{1})} = \frac{1.009 \times 10^{6} \times 9.80665 \times (1/3600)}{265.6 \times 0.4944} = 20.9 \tag{77}\]

falling to 12.6 if the specific fuel consumption is a very optimistic 0.6 per hour, and rising to 28.4 for the larger reported range. A wing of aspect ratio 1.87 does not achieve a lift-to-drag ratio of twelve, let alone twenty-one, under any assumption about the rest of the aeroplane. The conclusion is therefore stronger than a caution about the maximum-Mach case. The reported ranges cannot be reconciled with the reported weights on any cruise condition the X-10 could fly. This matters beyond bookkeeping, because it means the operational X-10 sortie may well have spent enough time aloft to sit on the useful side of the crossover computed above, and the navigation question turns on the flight durations, not the range figures. Whitcomb 1953, Margolis et al. 1958, and Nelson and Welsh 1960 carry the contemporary wave-drag and area-rule work, while Englert et al. 1954 and Slocumb and Andrews 1961 take up base drag.

The two reported ranges disagree by a factor of 1.36 and this article does not resolve which is right. Naming the disagreement is the correct treatment, and the Epistemic State repeats it.

Dependent Systems

The Autonavigator

The guidance system was North American’s N-6 autonavigator, which Wade, Navaho, Encyclopedia Astronautica describes as stellar-inertial and the Air Force history Landis 2020 Navaho Missile Program, Part 2 as all-inertial, built from two NAVAN gyroscopes, accelerometers, and a transistorised digital computer called NATAN. The X-10 flew earlier radio-command equipment as well, which Parsch 2002 RTV-A-5 X-10 gives as an AN/ARW-56 receiver against an AN/ARW-55 ground transmitter, and the later Cape Canaveral vehicles carried the autonavigator proper. The programme therefore had two guidance systems aboard the same airframe for different purposes, one to fly the X-10 where the range wanted it and one to be measured. That arrangement made recovery possible at all, since a test article guided only by the thing under test cannot be relied upon to come back. Treating the two as independent, the probability that at least one is available is

\[P = 1 - (1 - p_{1})(1 - p_{2}) \tag{78}\]

so two systems each available with probability 0.95 give

\[P = 1 - (0.05)^{2} = 0.9975 \tag{79}\]

a twentyfold reduction in the chance of having no guidance at all. The redundancy was not a hedge against the autonavigator being unreliable. It was the precondition for letting the autonavigator be unproven. A precondition is a different and more useful thing than a hedge, since it allows a test article to fly an instrument nobody yet trusts. The analysis of redundancy mechanisms as such is Lichter and Friedenreich 1962, and error propagation through the astro-inertial arrangement the N-6 used is Dusek 1964a.

The Autopilot Inner Loop

An unmanned supersonic vehicle needs an autopilot before it needs guidance, because the guidance loop closes around a vehicle that is already stabilised. The canard configuration’s aerodynamic centre travel reported by Bond and Swanson 1953, moving rearward through the transonic region and forward again supersonically, is the behaviour that forces gain scheduling, since the static margin and therefore the short-period frequency change with Mach number along the flight path. The magnitude can be estimated. Approximating the short-period frequency by the pitch-stiffness term alone,

\[\omega_{n} \approx \sqrt{-M_{\alpha}} = \sqrt{\frac{q S \bar{c} \, C_{L\alpha} \, h_{n}}{I_{yy}}} \tag{80}\]

where $h_{n}$ is the static margin, and evaluating at the two ends of the flight envelope with a mean chord of 4.60 metres and a pitch inertia near $5.8 \times 10^{5}$ kilogramme square metres, the frequency runs from

\[\omega_{n} = 0.63 \, \text{rad/s} \quad \text{at Mach 0.95 with a 3 percent margin} \tag{81}\]

to

\[\omega_{n} = 2.03 \, \text{rad/s} \quad \text{at Mach 2.05 with a 10 percent margin} \tag{82}\]

a factor of 3.2 across conditions the X-10 passes through on every flight. A fixed-gain pitch loop cannot hold consistent damping across that spread, so the autopilot had to schedule on dynamic pressure or Mach number, and it had to do so with analogue hardware. This is the sense in which the X-10’s autopilot was a harder piece of engineering than its guidance. Zarovsky 1951 treats roll stabilisation of a supersonic pilotless aircraft in the same period, Seaberg 1950 gives autopilot forms, and Hart 1956 the system practice. Servomechanism engineering is the subject of Lebell 1956, Evans 1957, Kuba and Kazda 1958, and Etzweiler 1969. Fagin et al. 1969 and Johnson 1971 formulate it later, and Gully and Skelley 1975 takes the cruise-missile case. The standard texts are Blakelock 1991 Automatic Control of Aircraft and Missiles and Etkin and Reid 1996 Dynamics of Flight.

The Turbojets, and the Engine That Was Not Tested

The X-10 flew on two Westinghouse J40 turbojets, an engine whose development difficulties were substantial and whose troubles, set out in Westinghouse J40, are usually recorded against the naval aircraft that were obliged to use it. For the X-10 the relevant point is narrower and is best put as a relation. Net thrust at fixed geometry scales with the total pressure delivered to the compressor face, so

\[\frac{T}{T_{\text{SL}}} \approx \eta \, \frac{p_{\infty}}{p_{\text{SL}}} \left( 1 + \frac{\gamma-1}{2} M^{2} \right)^{\frac{\gamma}{\gamma-1}} \tag{83}\]

in which the ram term rises steeply with Mach number while the ambient-pressure term falls with altitude, and the two very nearly cancel for this airframe at its ceiling. The engine is being asked to make sea-level thrust out of about one seventh of sea-level pressure, and it manages only because ram compression at Mach 2.05 supplies a factor of 8.46. A turbojet at Mach 2 operates far from the condition its compressor was designed for, and the design problem was being actively worked in the open literature at the time by Hurley 1951b, Gabriel et al. 1953, Alford and Auyer 1954, and Palmer 1956. Cesaro and Walker 1955 takes the non-afterburning supersonic application and Fleming et al. 1956 the afterburner behaviour. Inlet and engine compatibility, which the thrust calculation above treats as a single recovery number, is a dynamic problem as well and appears as such in Calogeras 1969b. Chun and Swanson 1964 simulates it dynamically and Burris 1966 supplies a test method.

The X-10 never carried the engine the Navaho needed. The Wright XRJ47 ramjet intended for the weapon was evaluated separately and flew only on the XSM-64, as Landis 2020 Navaho Missile Program, Part 2 records, and Reilly and Welna 1955 reports a preliminary evaluation of the flight-weight XRJ47-W-5. No propulsion document in the accessible record is more directly relevant, and it concerns an engine the X-10 did not fly. Ramjet engine requirements for supersonic flight generally are Walker 1952 with materials in Besserer 1952, and the combined-cycle idea that would have let one vehicle do both jobs appears in De VAULT 1957, which postdates the X-10 and describes the arrangement its recoverability requirement had forced the programme to do without.

The Structure, and the Temperature That Bounds It

Aerodynamic heating sets what the airframe may be made of. The recovery temperature at a recovery factor of 0.89 is

\[T_{r} = T_{\infty} \left( 1 + r \frac{\gamma - 1}{2} M^{2} \right) \tag{84}\]

and at the X-10’s maximum Mach number and ceiling this gives

\[T_{r} = 216.65 \left( 1 + 0.89 \times 0.2 \times 2.05^{2} \right) = 378.7 \, \text{K} = 105.6 \, ^{\circ}\text{C} \tag{85}\]

which sits comfortably inside the service range of aluminium alloys, conventionally taken near 423 kelvin. The same relation at the Navaho’s cruise condition of Mach 3.25 at twenty-four kilometres gives

\[T_{r} = 220.6 \left( 1 + 0.89 \times 0.2 \times 3.25^{2} \right) = 635.5 \, \text{K} = 362.4 \, ^{\circ}\text{C} \tag{86}\]

which does not. Solving for the Mach number at which the recovery temperature reaches the aluminium limit in the 220.6 kelvin air at twenty-four kilometres,

\[M_{\text{Al}} = \sqrt{\frac{2}{r (\gamma - 1)} \left( \frac{T_{\text{Al}}}{T_{\infty}} - 1 \right)} = 2.27 \tag{87}\]

The aluminium frontier lies at Mach 2.27 and the X-10’s maximum was Mach 2.05. The margin is neither a coincidence nor a near miss. The X-10 was built of aluminium, which Wade, Navaho, Encyclopedia Astronautica records as the plan for the phase it flew, so it could not be flown past the point where aluminium stops working, and the Navaho’s structural problem therefore lay entirely outside the testbed’s envelope. Contemporary work on heating and high-temperature structure includes Luce 1949, Drakin 1963, Harri 1964, and Heimerl and Hardrath 1965, with later material in Davis et al. 1972 and Chou and Smith 1974. The design-criteria problem that a sustained supersonic vehicle poses, which is that the structure must be sized for a thermal state that persists rather than for a transient, receives its treatment in Stauffer 1964. Fairbairn 1964 selects the materials, and Sakata et al. 1975 carries a later structural concept study for a comparable configuration. Rumsey and Lee 1961b performs the heat transfer and boundary-layer measurement that verifying any of it would have needed, and Morito and Sidwell 1967 covers unsteady loads and dynamic response.

The thermal argument and the navigation argument meet at the instrument platform. The oven that holds the gyroscopes to a quarter of a kelvin is mounted inside a structure whose skin the relation above puts at 106 degrees Celsius on an X-10 flight and 362 on the Navaho’s, and it must hold that quarter kelvin for three hours while the surrounding structure soaks.

How fast the structure soaks decides whether the oven faces a ramp or a step. For a skin of thickness $\delta$ heated convectively, the lumped time constant is

\[\tau_{\text{skin}} = \frac{\rho c \delta}{h} \tag{88}\]

and for two millimetres of aluminium at a convective coefficient of 100 watts per square metre kelvin this is

\[\tau_{\text{skin}} = \frac{2700 \times 900 \times 0.002}{100} = 48.6 \, \text{s} \tag{89}\]

which is under three percent of an X-10 flight and half of one percent of a Navaho mission. The skin arrives at its recovery temperature almost immediately and then stays there, so the platform oven is not chasing a slowly rising boundary but holding against a step that is applied once and never removed. The article’s two main threads share this coupling, which accounts of the programme do not usually draw.

Power Without a Pilot

Everything aboard the X-10 that moved or computed needed power, and unlike a piloted aeroplane there was nobody to reset a breaker or select an alternate source. The hydraulic system drove the control surfaces and the landing gear, the electrical system ran the platform oven, the autopilot, the telemetry, and the command receiver, and a failure in either was unrecoverable in a way that the same failure on a piloted aircraft would not have been. The platform oven is the least forgiving load, because it must hold its temperature from before take-off through the flight, and an oven that loses power does not fail immediately but drifts, which is worse. Servo and actuator design is covered by Biernson 1965 and Davies and Haines 1965, with instrument servomechanism behaviour including limit cycling in Marstrander and Lueg 1969.

The reliability arithmetic of an unmanned vehicle is unforgiving in a way that is easy to state and was hard to act on in 1955. If a mission requires $n$ subsystems all to work and each works with probability $p$, the mission succeeds with probability

\[P_{\text{mission}} = p^{n} \tag{90}\]

so ten subsystems at ninety-five percent each give

\[P = 0.95^{10} = 0.599 \tag{91}\]

a mission success rate of about sixty percent from components that would each individually be called reliable. The X-10 completed twenty-seven development flights and lost twelve of thirteen airframes, which is consistent with that arithmetic and requires no single villain. The counts are those of Landis 2020 Flashback, The Navaho Missile, Part 1. Blumenthal and Denton 1962 shows how the period estimated reliability, Monroe 1963 and Howard and Kaufman 1964 build availability models of a weapon system from the same components, and Lichter and Friedenreich 1962 analyses the redundancy mechanisms that would have been the remedy. The analytical means of detecting a failed instrument in flight and reconfiguring around it did not arrive until the following decade, in Solov and Thibodeau 1973 and Montgomery 1975. The fault-detection discussion below names the same gap.

Landing Gear, Brakes, and the Strip Built for a Machine

The X-10 had to land itself, and North American X-10 puts six of the nine airframes not expended deliberately down to landing accidents. Taking a landing mass of twelve tonnes after fuel burn, the wing loading is 2980 newtons per square metre and at a maximum lift coefficient of unity the stall speed at sea level is

\[v_{\text{stall}} = \sqrt{\frac{2W}{\rho S C_{L,\max}}} = \sqrt{\frac{2 \times 117{,}680}{1.225 \times 39.48 \times 1.0}} = 69.8 \, \text{m/s} \tag{92}\]

or 136 knots, with an approach at 1.2 times that giving 83.7 metres per second, which is 163 knots. The kinetic energy to be dissipated is

\[E = \tfrac{1}{2} m v^{2} = \tfrac{1}{2} \times 12{,}000 \times 83.7^{2} = 42.0 \, \text{MJ} \tag{93}\]

and at a braking friction coefficient of 0.4 the ground roll is

\[s = \frac{v^{2}}{2 \mu g} = \frac{7006}{2 \times 0.4 \times 9.80665} = 893 \, \text{m} \tag{94}\]

A landing strip 200 feet wide and 10,000 feet long was built at Cape Canaveral for the X-10 Cleary 1991 The 6555th, The NAVAHO Program, and it survives as the Skid Strip. At 3048 metres the margin over the computed braking distance is

\[\frac{3048}{893} = 3.41 \tag{95}\]

which is the margin an unmanned vehicle with no pilot to correct a drift needs and did not always get. A drag chute helps because its force scales with the square of speed while braking force does not, so it does its work early. A chute matching the brakes at touchdown speed needs an area of

\[S_{c} = \frac{\mu W}{\frac{1}{2} \rho v^{2} C_{D,c}} = \frac{47{,}072}{\frac{1}{2} \times 1.225 \times 7006 \times 1.4} = 7.83 \, \text{m}^{2} \tag{96}\]

which is a canopy of 3.16 metres diameter, and deploying it roughly halves the stopping distance. Work on landing dynamics and gear begins with Stowell et al. 1948, Yntema and Milwitzky 1952, Horne and Leland 1962, and Kordes and McKay 1962. Knacke 1992 Parachute Recovery Systems Design Manual governs recovery-system design and Currey 1988 Aircraft Landing Gear Design the gear. Kansas Univ Lawrence 1952b covers barrier and arresting practice.

Automatic Landing a Decade Early

The hardest thing the X-10 did was the thing least remarked upon. Landing an aeroplane automatically was still an experimental capability in 1953, and the first automatic landing on a scheduled passenger flight was not made until 10 June 1965, by the British European Airways Trident whose development is traced in Autoland. The period literature makes the gap visible. Helliwell 1952 treats automatic control in the landing approach, Walker 1960 and Walker 1961 describe fully automatic approach, and the systems that entered service are Schoenman and Doniger 1965 on the Boeing and Bendix 707 installation and Templeman and Parker 1968 on the Boeing and Sperry 727. Design considerations are Doniger 1967, approach guidance concepts are Maiuzzo 1970 and Poritzky 1970, and the radio-inertial lateral control limits are MACKlNNON and Madden 1972. The geometry shows how little margin the task allows. On a glide slope of angle $\gamma$ the sink rate is

\[\dot{h} = -v \sin \gamma \tag{97}\]

which at the approach speed computed in the section Landing Gear, Brakes, and the Strip Built for a Machine and a three-degree slope is

\[\dot{h} = -83.7 \times \sin 3^{\circ} = -4.38 \, \text{m/s} \tag{98}\]

or 862 feet per minute, a rate that must be arrested to near zero in the last few metres. The flare that does it is conventionally an exponential,

\[h(t) = h_{0} e^{-t / \tau_{f}}, \qquad \dot{h} = -\frac{h}{\tau_{f}} \tag{99}\]

so a flare initiated at fifteen metres with a three-second time constant begins at five metres per second of sink and decays smoothly. Three seconds at approach speed is 251 metres of runway, and the aeroplane has to judge its own height above the ground to a metre or so throughout, with 1953 instrumentation and nobody aboard. The period’s approach to the problem is Payne 1968 on what a landing control law should optimise, Lykken and Shah 1972 on using direct lift to improve the flare, Patrick 1972 on coupling automatic landing to microwave guidance, Niessen 1973 on smoothing approach guidance inertially, and Crawford 1975 on automatic guidance and control of a transport through the landing. Later formulations of the same control law are Watson et al. 1983, with the terminal-area problem in Pines 1982 and a digital integrated system in Halyo and Hueschen 1981.

The X-10 was landing itself on a runway a decade before airliners did, with a guidance loop closed through a ground radio link and an autopilot, and it is fair to say that the programme discovered how hard this was by losing vehicles to it. On one Edwards flight the automatic landing system attempted the flare six metres below runway level and the vehicle was destroyed, as Wade, Navaho, Encyclopedia Astronautica records.

The Command Link Cannot Reach the End of the Leg

The radio-command equipment is usually mentioned and never dimensioned, and dimensioning it produces a constraint that bears directly on the article’s argument. A radio link between an aircraft at altitude $h$ and a station on the ground is limited by the horizon, which under standard atmospheric refraction is computed with an effective Earth radius four thirds of the true one,

\[d_{\text{horizon}} = \sqrt{2 \, k \, R_{e} \, h}, \qquad k = \frac{4}{3} \tag{100}\]

At the X-10’s service ceiling this gives

\[d_{\text{horizon}} = \sqrt{2 \times \tfrac{4}{3} \times 6.371 \times 10^{6} \times 13{,}650} = 482 \, \text{km} \tag{101}\]

and adding a hundred-metre ground mast extends it only to 523 kilometres, because the transmitter’s own altitude dominates. Against a one-way leg of a thousand kilometres this is

\[\frac{1000}{482} = 2.08 \tag{102}\]

A one-way leg of that length is more than twice the radio horizon, so a single ground station cannot see the X-10 through it. Either the range operated a chain of stations, which is what the Atlantic range in fact developed, with a station as far downrange as Mayaguez in Cleary 1991 The 6555th, The NAVAHO Program, or the vehicle spent a substantial part of a long one-way sortie beyond command range. The reported distance is that of a whole flight, however, and an out-and-back sortie of that length need never go much beyond the horizon. Both readings support the same conclusion. Past the horizon the autonavigator is not being tested as a candidate subsystem but relied upon as the only one available, and the vehicle’s recoverability makes that acceptable rather than reckless.

The propagation engineering behind the horizon calculation is Blake 1968, whose range-height-angle charts are the working form of the relation used above, with the over-horizon and low-angle measurements of Cullen 1969 showing how the simple geometric picture degrades in practice. The trends in missile and space radio telemetry of the period are set out by Muehlner 1962, and the refraction corrections a range must apply before its tracking data mean anything are Rowlandson and Herlihy 1969.

The Cost of Turning Back

A vehicle that must come home has to reverse course, and at Mach 2 that sounds expensive. The turn radius at load factor $n$ is

\[r = \frac{v^{2}}{g \sqrt{n^{2} - 1}} \tag{103}\]

which at the vehicle’s maximum speed and a load factor of two, corresponding to a bank angle of sixty degrees, gives

\[r = \frac{604.9^{2}}{9.80665 \times \sqrt{3}} = 21.5 \, \text{km} \tag{104}\]

so a course reversal sweeps 43 kilometres of ground track and takes

\[t_{\text{turn}} = \frac{\pi r}{v} = \frac{\pi \times 21{,}541}{604.9} = 112 \, \text{s} \tag{105}\]

which is 4.3 percent of a thousand-kilometre leg. The turn is not the problem. The calculation matters because the intuition that supersonic vehicles cannot manoeuvre in useful distances is wrong at this scale, and because it removes one candidate explanation for the losses, which were concentrated on the ground.

Instrumentation, Telemetry, and the Range

Everything the programme learned came back either in the vehicle or over a radio link. Range instrumentation and flight-test reporting practice from those years are visible in General Dynamics/Astronautics San Diegoca 1961, Moyer 1963a, and Knoblach 1974, with decelerator testing in Ward and Myers 1967. The recoverable vehicle has a genuine advantage here that the X-8 and X-9 did not enjoy, because an instrument package that lands with the vehicle can be calibrated afterward against the same bench that calibrated it before flight, and a drift measurement is only as good as that comparison.

The Flight Test Record

The first X-10 flight was on 14 October 1953 at Edwards Air Force Base. Five vehicles flew fifteen flights there through March 1955. The programme then moved to Cape Canaveral, where the first flight on 19 August 1955 ended with the vehicle overrunning the Skid Strip and burning after its drag chute failed to deploy. Twelve flights, numbered sixteen through twenty-seven and including that first one, were flown from the Cape between August 1955 and November 1956, and these included the supersonic performance demonstration to Mach 2.05 and the longest flights, of about a thousand kilometres. Five flights were autonavigator tests in the launch appendix of Werrell 1985 The Evolution of the Cruise Missile, four of them described as inertial navigation tests in the chronology, which records two of those four as aborted by computer failures. The Edwards flights reached 41,800 feet, a figure the appendix and the Air Force history give alike. The phase dates and flight counts are those of Landis 2020 Flashback, The Navaho Missile, Part 1, and the flight-by-flight outcomes those of Wade, Navaho, Encyclopedia Astronautica.

The quantity measured deserves scrutiny, because a navigation error is established by comparing the vehicle’s answer against the range’s, and the range’s answer has an error of its own. Tracking-radar accuracy of the period is Bumer 1946, high-acceleration telemetry for range instrumentation is Mermagen 1964, trajectory reduction as a range practised it is Callaway 1963, and the combined error analysis of navigating by inertial guidance while being tracked by radar is Remmler and Theobald 1967. An instrument that is being measured cannot be more accurately known than the instrument measuring it, and no source in the accessible record states the tracking error of the Atlantic Missile Range for these flights.

Of the thirteen vehicles built, one survives, serial 51-9307, the first to fly, now held by the National Museum of the United States Air Force. The others were lost. Three were expended in planned dives against Grand Bahama Island, at least two were lost in landing accidents at the Cape, and three surplus vehicles flown as targets for development of the Boeing and Michigan Aeronautical Research Center missile, BOMARC, between September 1958 and January 1959 were all lost, two of them burning after running off the end of the Skid Strip on 24 September and 13 November 1958. The last X-10 flew on 26 January 1959 and crashed about fifty-seven miles downrange after a power failure. The disposition of the airframes follows North American X-10, and the target flights follow Cleary 1991 The 6555th, The NAVAHO Program.

The programme therefore divides into three phases with different purposes. The Edwards phase from October 1953 established that the vehicle flew and could be recovered. The Cape phase from August 1955 extended the envelope and flew the navigation legs. The five dedicated autonavigator flights in that phase are the only part of the programme that addressed the keystone question directly. The post-cancellation phase from September 1958 used surplus airframes as targets for a different programme entirely. Remaining hardware from a cancelled programme ordinarily ends this way, and the phase tells nothing about the vehicle.

What Was Demonstrated

Stating the achievements precisely matters because the article’s argument is that the vehicle worked and the test did not. The X-10 reached Mach 2.05, which is above the free-flight model’s tested maximum of 1.70 and therefore beyond where either ground method had been validated. It reached 49,000 feet in North American X-10 and 44,800 feet in Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50. It flew about a thousand kilometres in a single flight. It took off and landed under automatic control on a runway. Considered as an aeroplane, and particularly as an unmanned aeroplane in 1955, this is an impressive record, and Parsch 2002 RTV-A-5 X-10 records that for a short time it was the fastest turbojet-powered aircraft flown.

None of it bears on why the record leaves the programme’s question open. A vehicle can be flown perfectly and still fail to constitute an experiment. The identifiability calculation above shows that window length was no obstacle on the one navigation flight whose duration is reported, so the weakness lies in how few navigator flights were completed, two of the five having been aborted. The X-10’s sorties were successful flights and too few measurements, and those are independent properties.

The Dive Flights as a Test of the Terminal Phase

Three vehicles flown at the Cape were expended in planned dives against Grand Bahama Island, and these are usually listed alongside the accidental losses as though they were the same kind of event. They were not. The Navaho’s terminal phase was a dive onto the target from cruise altitude, and the Air Force history Landis 2020 Flashback, The Navaho Missile, Part 1 lists dive technique among the things the Cape flights were to check. A dive from twenty-four kilometres at Mach three is a distinct flight condition, with its own structural loads, control problem, and contribution to the accuracy budget. A vehicle that navigates perfectly and then misses the dive has still missed. The sensitivity is easy to state. A dive from altitude $h$ at flight path angle $\gamma$ covers a ground range of

\[x = \frac{h}{\tan \gamma} \tag{106}\]

so an error in the dive angle produces a range error of

\[\frac{dx}{d\gamma} = -\frac{h}{\sin^{2} \gamma} \tag{107}\]

and from twenty-four kilometres at forty-five degrees this is

\[\frac{dx}{d\gamma} = -\frac{24{,}000}{0.5} = -48{,}000 \, \text{m/rad} \tag{108}\]

or 48 metres of miss for every milliradian of dive-angle error. Against an eight-hundred-metre requirement that is a demanding pointing accuracy, separate from knowing where the target is. Expending three airframes to fly that phase deliberately is therefore a test decision rather than a disposal, and is evidence that the programme understood the terminal phase as a distinct problem even though the X-10 could only approximate its conditions. Wheeler 1946 treats the assessment of where a weapon landed, the measurement such a flight exists to produce. The terminal-guidance alternative of looking at the target on the way down is Dunmire and Lopresti 1963, the accuracy requirement that a re-entering body imposes on its guidance is Broglio 1961, and what happens on arrival is Johnson and Mosely 1964.

What the Losses Say

Stated as a fraction, twelve of thirteen vehicles lost is

\[\frac{12}{13} = 0.923 \tag{109}\]

and twenty-seven development flights across thirteen airframes is 2.08 flights per vehicle. A design whose entire economic and statistical rationale was repeated use averaged two flights per article. The causes named for the landing losses at the Cape are concentrated at the end of the mission rather than in it, with vehicles that veered off the strip, drag chutes that did not deploy, and barriers that were not engaged, as Parsch 2002 RTV-A-5 X-10 lists them. The vehicle flew supersonically and navigated across a range, and then could not reliably stop.

Comparison With Ground Prediction

Three levels of evidence exist for this configuration and they can be set against one another. Pfyl 1952 gives wind-tunnel data on a 0.07-scale model. Bond and Swanson 1953 gives free-flight data on a 0.12-scale rocket-boosted model at Reynolds numbers from nine to twenty-four million. The full-scale vehicle flew to Mach 2.05, faster than either model had been tested.

The pattern is familiar from the X-7. Free flight extends the Reynolds number far beyond what the tunnels of the period could reach and removes support interference, at the cost of a single trajectory per model and no ability to repeat a condition. The Reynolds numbers make the point concrete. On mean aerodynamic chord,

\[Re = \frac{\rho v \bar{c}}{\mu} \tag{110}\]

and evaluating it for the full-scale vehicle at its ceiling and maximum Mach number, with the viscosity from Sutherland’s relation

\[\mu = \frac{1.458 \times 10^{-6} \, T^{3/2}}{T + 110.4} = 1.42 \times 10^{-5} \, \text{Pa s} \tag{111}\]

gives

\[Re_{\text{full}} = \frac{0.2397 \times 604.9 \times 4.595}{1.42 \times 10^{-5}} = 4.68 \times 10^{7} \tag{112}\]

The free-flight models spanned nine to twenty-four million, so they reached

\[\frac{Re_{\text{model}}}{Re_{\text{full}}} = 0.19 \; \text{to} \; 0.51 \tag{113}\]

between a fifth and a half of full-scale Reynolds number, against transonic tunnels of the period that typically delivered a few million on a model of comparable size. The free-flight technique therefore bought roughly an order of magnitude over the tunnels and still fell short of the vehicle by a factor of two. Stated that way the result is more defensible than a claim that the models reached flight conditions. The technique had already been applied to full-scale guided missiles by Delsasso et al. 1948, five years before the X-10 flew, so the method was mature even where its Reynolds numbers were not.

Two of the free-flight findings are checkable against the analysis performed here and both survive. The reported drag-rise Mach number near 0.90 is consistent with a thin low-aspect-ratio configuration, and the reported doubling of minimum drag from subsonic to supersonic is what wave drag on such a shape produces. The base-drag finding of twenty-five percent of minimum drag supersonically is large but not anomalous for a configuration with a blunt afterbody carrying two engine exhausts. The duct recovery result illustrates the tension, because the free-flight model’s report of recovery below normal-shock values is either a real property of the inlet design or an artefact of a small duct at model scale, and no measurement in the accessible record distinguishes those two possibilities. The full-scale vehicle’s own inlet performance does not appear in the public literature at all, so the thrust-balance inference above had to be constructed from the vehicle’s demonstrated speed instead.

The free-flight technique deserves naming, because it produced the only surviving quantitative data on this configuration. Its development and its limits are Turner 1965, and comparable applications in the same era are Wetzel 1954, Ball and Smith 1956, and Grant and Sevier 1960. The technique’s central bargain can be restated in the terms this article has been using. A free-flight model gives one trajectory and therefore one sample, the same difficulty the X-10 had with drift statistics, one level down in scale. A programme that needs a distribution and can afford only single samples is in the same trouble whether the article being flown is a scale model or a full-size vehicle.

What the Data Changed

The Cancellation of the Navaho

Air Force Headquarters terminated the Navaho by message dated 12 July 1957. The XSM-64 had flown first on 6 November 1956, and its pitch gyroscope failed ten seconds after lift-off and the vehicle broke up at twenty-six seconds. Three further launches through 26 June 1957 failed in turn, one impacting twenty-five nautical miles downrange, one falling back onto the pad after rising four feet, and one losing its ramjets after booster separation. Seven more tests followed through November 1958 without a full-range success. The launch record is that of Cleary 1991 The 6555th, The NAVAHO Program, with the later tests in Parsch 2002 SM-64. The X-10 was the most successful part of a programme that failed, and by the time the vehicle had demonstrated what it could demonstrate, the ballistic alternatives had made the question moot.

The strategic argument is not primarily an engineering one, yet it can be derived rather than asserted. A ballistic missile covering the same ten thousand kilometres flies a minimum-energy ellipse. Writing the range angle as

\[\Phi = \frac{R_{m}}{R_{e}} = \frac{1.0 \times 10^{7}}{6.371 \times 10^{6}} = 1.570 \, \text{rad} \tag{114}\]

the minimum-energy condition fixes the burnout speed through

\[\lambda = \frac{V^{2}}{g R_{e}} = \frac{2 \sin (\Phi/2)}{1 + \sin (\Phi/2)} = 0.828 \tag{115}\]

giving

\[V = \sqrt{0.828 \times 9.80665 \times 6.371 \times 10^{6}} = 7193 \, \text{m/s} \tag{116}\]

and a semi-major axis from the vis-viva relation of

\[a = \frac{R_{e}}{2 - \lambda} = 5.437 \times 10^{6} \, \text{m} \tag{117}\]

with eccentricity 0.415 and an apogee 1319 kilometres above the surface. Converting the true anomalies at launch and impact to mean anomalies and differencing gives the free-flight time

\[t_{\text{ballistic}} = \frac{\Delta M}{n} = 1932 \, \text{s} = 32.2 \, \text{minutes} \tag{118}\]

against the cruise mission’s 172 minutes. The ratio is

\[\frac{t_{\text{cruise}}}{t_{\text{ballistic}}} = \frac{172.2}{32.2} = 5.35 \tag{119}\]

The airbreathing weapon is exposed more than five times as long, and it is exposed inside the atmosphere at twenty-four kilometres where an interceptor can reach it, while its competitor spends most of its flight far above the atmosphere, reaching thirteen hundred kilometres at apogee, where in 1957 nothing could. The cancellation argument is complete at that point. Once Atlas and Titan were credible, no accuracy improvement available at the time bought enough to pay for a factor of five in exposure against a threat that could not be engaged at all.

The ballistic relations used above are period material and not modern reconstructions. Wheelon 1959 treats the free flight of a ballistic missile in the form derived here, Brooks 1961 gives the basic theory of ballistic missile performance, and Ostner 1962 reduces it to a program that a range could run. Schweppe 1964 estimates where such a body is while it flies. Faulkner 1961 poses the interception problem as the period saw it, Fye 1966 states the defensive difficulty plainly, Kashiwagi 1968 predicts the trajectories being intercepted, and Werrell 1985 The Evolution of the Cruise Missile carries the history of the class that lost the argument.

What Survived

The programme’s outputs outlived its purpose in three directions, and the question is which of them the X-10 can claim.

The engines. The liquid rocket booster engines developed for the Navaho became the basis of the Rocketdyne line that powered Redstone, Jupiter, Thor, and Atlas, and through Atlas the American space programme, as the Navaho entry summarises. The Redstone half of that inheritance is documented in Bullard 1965, and a released Rocketdyne sustainer specification of the resulting line is Scott 1963. This is by a wide margin the largest technical legacy of the Navaho effort. It belongs entirely to the booster and the X-10 had no part in it whatever, since the X-10 carried no rocket engine and took off under turbojet power.

The navigation. The navigation work is the legacy the X-10 can properly claim, because the X-10 is where the N-6 was first flown in a missile airframe, after aircraft trials described in Landis 2020 Navaho Missile Program, Part 2. The error analysis of that architecture, as the period came to understand it, is Dusek 1964a and Nash 1968. The guidance system fed forward into nuclear-powered submarines, Navy attack aircraft, and the Hound Dog and Minuteman missiles Cleary 1991 The 6555th, The NAVAHO Program, and the combination of a Schuler-tuned platform with an automatic celestial reference remained a standard solution for unaided long-range navigation until satellite navigation displaced it, and has returned to favour as satellite navigation has become contestable.

The configuration. Experience with large supersonic canard configurations, with side-mounted supersonic inlets, and with the structures and systems of sustained supersonic flight fed into subsequent work at the same company, most visibly the XB-70, which Landis 2020 Navaho Missile Program, Part 2 names among the beneficiaries. The connection is real but diffuse and this article does not attempt to quantify it.

What the X-10 did not change is the Navaho’s outcome. By the time the vehicle had flown its full programme, the weapon it served had been cancelled, and the cancellation turned on an argument about exposure time that no amount of aerodynamic or navigational success would have answered.

The X-10’s contribution is harder to point at than any of these, and honesty requires saying so. It demonstrated that a large unmanned supersonic vehicle could be flown repeatedly from a runway and recovered, which is a real result. What it did not do was settle the navigation question it was built to settle, chiefly because too few navigator flights were completed to estimate a drift distribution, as computed above.

The Contemporary Literature

Cluster	Records
Gyroscopes, accelerometers and the inertial instrument	1,046
Canard configurations, missile aerodynamics and drag	965
Turbojets, ramjets and propulsion for supersonic flight	540
Stellar-inertial navigation, star trackers and celestial reference	498
Automatic landing, the approach and the flare	482
Supersonic inlets, buzz and engine compatibility	482
Navigation without satellites, by terrain, field and vision	478
Alignment, calibration and initialisation	411
Aerodynamic heating and high-temperature structures	386
Ballistic missiles, interception and glide vehicles	369
Autopilots, servomechanisms and flight control	368
Inertial navigation systems and their mechanisation	353
Estimation, identifiability, observability and experiment design	335
Landing gear, brakes, arresting gear and decelerators	334
Gravity, the deflection of the vertical and gravity-aided navigation	309
Inertial error propagation, the Schuler loop and the vertical channel	281
Command link, telemetry, tracking and the range	267
Fault detection, redundancy and reliability	246
Free-flight models, flight test and the model-to-flight gap	159
Reusable vehicles, recovery and the cost of a flight	121
Accuracy as a statistic, circular error probable and error budgets	69
Cruise vehicles and hypersonic cruise	22
Total	8,521

Identifiability as a Later Discipline

The article’s identifiability result is that two error signatures are 97.4 percent correlated over a maximum-speed X-10 leg and 14.0 percent correlated over the 79-minute navigation flight, so whether the drift rate could be separated from the accelerometer bias depends on the window actually flown. The result concerns identifiability, which is now a field.

The modern distinction the X-10’s difficulty falls under is between structural and practical identifiability. A parameter is structurally identifiable if the model permits it to be recovered from perfect data and practically identifiable if the data actually collected suffice. The X-10’s drift rate was structurally identifiable, and its practical identifiability turned on the window and the number of flights, the distinction drawn by Simpson and Baker 2026 and by Heitzman-Breen et al. 2026, with the structural side treated by Salmaniw and Browning 2025. Liu et al. 2026i gives the remedy, choosing the experiment so that the parameter becomes practically identifiable. The Fisher information matrix that quantifies how much an experiment reveals is Andrade et al. 2025 and Fayette et al. 2026, and the input-design problem of exciting a system enough to identify it is Campregher et al. 2025, with parameter subset selection in Wang and Qi 2024.

The window sweep performed above is an optimal-experiment-design calculation with one free variable, and the answer it returns, namely a flight of exactly one Schuler period, is the sort of answer that discipline exists to produce. Observability, the closely related property, is now analysed for inertial systems directly in Yang et al. 2026c and Zhang et al. 2026e, and observability-driven design of a celestial navigation observation appears in Hou et al. 2025.

The 1953 programme had none of this vocabulary. It cannot be charged with ignoring a known method, because the method it needed had not been invented, and the article adopts that reading as the fairest available.

Inertial Error Propagation by Covariance

The error analysis this article performs by hand is now standard and automated. Blum and Dambeck 2020 propagates coloured noise through inertial mechanisations, Brouk and DeMars 2021 handles uncertainty propagation with conic constraints, and Bhatia and Geller 2020 performs sensitivity analysis for precision inertial sensors. The relevant modern point is that the crossover time computed here as a single scalar is now the output of a full covariance propagation, and that the qualitative structure of a bounded accelerometer term against a secular gyroscope term survives unchanged. Theoretical error modelling of a strapdown system in the same tradition is Mohammadkarimi et al. 2025.

Alignment and Calibration

The relation derived above puts one arcminute of azimuth misalignment at 2.9 kilometres of cross-track error at intercontinental range, which makes ground alignment a coequal partner of airborne drift rather than a preliminary to it. That problem is still worked. Initial alignment is now attacked with learned models in Wang et al. 2025e, the calibration and compensation of an initial-state error scheme is Ding et al. 2025, online calibration by error backpropagation is Simak et al. 2024, and Allan-variance-based noise characterisation, the present-day way of asking what an instrument’s drift is, appears in Charu Priya and Deepa 2024, though applied there to a vehicular optical communication link rather than to an inertial instrument.

Gyroscopes Near the Navaho Requirement

The Navaho needed 0.0025 degrees per hour to meet its early requirement, and the requirement was eventually relaxed to a circular error probable of 12,000 feet after 5,000 miles of flight Landis 2020 Navaho Missile Program, Part 2. Set beside the current literature, the figure gives an unusually exact comparison.

Navigation-grade fibre-optic gyroscopes are Shang et al. 2020, Zhao et al. 2022d, Liu et al. 2023f, and Aleinik et al. 2025. Micro-electromechanical instruments have closed most of the remaining distance, with Suzuki et al. 2019 and Nusbaum et al. 2019 on the approach, a bias instability of 0.09 degrees per hour in Wu et al. 2021a, a high-quality-factor hemispherical resonator in Li et al. 2024a, and a honeycomb disk resonator gyroscope reported at 0.003 degrees per hour in Chen et al. 2025a.

That last figure stands to the Navaho’s requirement as

\[\frac{0.003}{0.0025} = 1.20 \tag{120}\]

and it is achieved by a micro-electromechanical device. The article’s drift relation takes the comparison further than the ratio does. A gyroscope drifting at 0.003 degrees per hour is $1.454 \times 10^{-8}$ radians per second, so over the Navaho mission it would produce

\[\delta x = R_{e} \varepsilon t = 6.371 \times 10^{6} \times 1.454 \times 10^{-8} \times 10{,}333 = 957 \, \text{m} \tag{121}\]

which still does not meet the eight-hundred-metre requirement on drift alone, seventy years later and before any of the other budget terms are added. The comparison shows not that the requirement has become easy but that a component, and no longer a national programme, can approach it. The mechanisms that set the floor are now themselves the subject of study, in Hiller et al. 2019 on the origins of bias instability, Kuang et al. 2022 on its temperature dependence, today’s version of the platform-oven problem computed above, Laita et al. 2024 on nonlinearity, and Zhao et al. 2024d on installation-error propagation. Gyrocompassing, the alignment problem this article showed to be worth 2.9 kilometres per arcminute, is treated afresh in Bénet and Guinamard 2026, and the combination of star tracker with gyroscope that the N-6 pioneered is Zhu et al. 2025a.

A requirement that defeated a national weapon programme in 1957 is now nearly met by a component, and the seventy years between those two statements is the most direct measure available of how far ahead of its instruments the Navaho’s accuracy requirement was.

Star Trackers as Routine Equipment

Automatic celestial reference is now ordinary. Siemes et al. 2019 calibrates a star tracker in orbit, Ni et al. 2019 gives attitude-correlated frame methods for weak signals, and Ning et al. 2019 integrates star pixel coordinates. The daylight tracking problem the Navaho programme faced is now a design choice rather than a research question.

The architecture the N-6 pioneered has also come back under its own name. Stellar-inertial integration is treated directly by Kondrashkin et al. 2025 and by Yang et al. 2026a, which adds refraction to the celestial observation, and the strapdown version that dispenses with the gimballed platform entirely is Teague and Chahl 2023 and Teague and Chahl 2024. Centroiding accuracy, which sets the arcsecond figure the article inverted from the reported circular error probable, is Li et al. 2023h, the benchmark problem is Suthakar et al. 2026, delayed measurements in the filter are Kahraman and Soken 2023, and the same idea applied on another planet is Zhan et al. 2021, with a deep-space integration in Wang et al. 2024j.

Fault Detection

An unmanned vehicle that loses an instrument has no one aboard to notice. The X-10’s losses were mostly mechanical and terminal, but the guidance failure mode was live throughout, and Cleary 1991 The 6555th, The NAVAHO Program records that the first XSM-64 launch broke up after its pitch gyroscope failed ten seconds after lift-off. Detecting and identifying such a failure in flight became possible only later, and the founding treatment is Potter and Deckert 1972, with modern robustness work in Lee et al. 2024a and fault-protection architecture in Schulte and Spencer 2020. The redundancy that would have saved that vehicle was not unavailable for cost reasons. The analytical basis for using it did not yet exist.

It exists now, and the inertial case is well developed. Fault detection and isolation for redundant inertial measurement units is Xu et al. 2023a and Lukoyanov et al. 2025, the airborne navigation case is Dai et al. 2023, estimation alongside detection is Huang et al. 2023c, and active fault-tolerant control that reconfigures around a failure rather than merely reporting it is Zhao et al. 2024a. A pitch gyroscope failing ten seconds after lift-off is now a detectable and survivable event. It is the clearest case in this article of a 1956 loss that modern practice would avoid.

Navigation Without Satellites

The Navaho’s problem was navigating with no external radio reference, and this has become topical again. Terrain-referenced navigation runs through Park and Park 2019, Kang et al. 2020, and Carroll and Canciani 2021. Zhai and Wang 2020 and Cui et al. 2021 filter it robustly, Alhassan and Ghahremani 2021 aligns it nonlinearly, and Ermakov and Gogolev 2021 and Wang et al. 2019e compare integration architectures. The question the X-10 was built to answer is once more an open engineering question, asked now about vehicles that must operate where satellite navigation is denied.

The breadth of that effort shows how completely satellite navigation had displaced the problem and how completely the displacement has been undone. Visual localisation without satellites is Shpagin and Panchenko 2026, Tsiopliakis 2026, and Li et al. 2026d, terrain-relative navigation for descent is reviewed by Abdhul Rahuman and Lee 2026, magnetic anomaly matching, the same trick as gravity matching applied to a different field, is Pisarski et al. 2026, the underwater case is Praczyk and Zalewski 2026, and constrained estimation in denied environments is Yue et al. 2026. Every one of these is a scheme for bounding a secular error with an external observation, as the star tracker did for the Navaho, and the modern literature has widened the catalogue of things that can serve as the observation.

Reusability and the Cost of a Sortie

The X-10’s economic case for recovery, and its failure to realise that case at 2.08 flights per airframe, is the same argument now conducted about launch vehicles. Life-cycle cost analysis of the kind the argument needs appears in Jung et al. 2022, and the recovery and reuse literature cited below approaches the problem from the trajectory side. The concept that the X-10 needed and did not have is the distinction between the cost of an airframe and the cost of a sortie, and a programme that loses twelve of thirteen airframes has collapsed that distinction whether it meant to or not.

Current work makes the distinction explicit. Lifecycle cost estimation for a reusable launch vehicle with the critical parameters identified is Du et al. 2025, recovery-method comparison across mission classes is Lee et al. 2026a, mission-based optimisation of a reusable unmanned vehicle is Jung et al. 2025b, precision landing guidance that makes recovery repeatable is Chen et al. 2026b, and the weapon-system version of the same accounting is Setiawan et al. 2025. Whatever else such an accounting includes, it spreads the cost of an airframe over the flights that airframe makes, so the number of flights per article governs it, and for the X-10 that number was 2.08.

Automatic Landing Revisited

Brukarczyk et al. 2021 lands a fixed-wing unmanned aircraft automatically, reusable launch vehicle recovery trajectory planning appears in Cheng et al. 2021b and Mathavaraj and Padhi 2020, reusable landing structures are Wang et al. 2020h, and landing gear efficiency and failure work is Han et al. 2019 and Diltemiz 2021. The X-10’s loss record is a reminder that recovery is a distinct engineering problem from flight, and the reusable-launch-vehicle literature has rediscovered this at much greater cost. Carrier-based automatic landing is Zhang et al. 2025d, and the modern answer to the height-above-ground problem the X-10 had to solve with 1953 instrumentation is vision, in Cheng and Lai 2025, Han et al. 2026e, and Zhu et al. 2026d.

The Landing Gear and the Lost Fleet

Twelve of thirteen airframes were lost, and North American X-10 puts six of the nine not expended deliberately down to landing accidents, which turned on chutes, barriers, and directional control. That subject has a current literature larger than the guidance one. Terminal manoeuvres including gear dynamics are Cacciola and Calabria 2026, shimmy, which is the directional instability that takes a vehicle off a runway, is Liu et al. 2026g, impact loads are Liu et al. 2023c, structural design for ultimate load is Titov and Serebryansky 2026 and Chen and Chen 2026, semi-active control of touchdown loads is Durmuşoğlu 2026, and the failure side is Xuan 2026, Sun et al. 2024b, Chen et al. 2022b, and Hsu et al. 2022 on predicting when a gear will fail before it does. The X-10 had none of this and lost half of its fleet to it. The loss record states plainly where the programme’s engineering attention was not.

Supersonic Inlets and Buzz Prediction

The inlet result that this article can only bound would today be resolved computationally. Yamamoto et al. 2020 and Farahani et al. 2019 predict buzz onset, Chen and Tan 2019 examines buzz diversity under strong disturbance, external-compression inlets free of violent buzz are Chen et al. 2019b, suppression mechanisms are Luo et al. 2020, sideslip effects are Dong et al. 2019, and acoustic and vibration behaviour is Zhu et al. 2020a, with a recent experimental study in Sepahi-Younsi 2025.

The failure modes that the X-10’s designers could not name are now the subject matter. Unstart of the inlet and isolator is Huang et al. 2026c, the shock-wave and boundary-layer interaction that drives it is Kim and Park 2026, distortion delivered to the compressor is Yang et al. 2026b and Bond and Key 2026, detection of distortion from measured signals is Wang et al. 2025i, the diverterless arrangement that removes the boundary-layer splitter plate the X-10 needed is Askari and Abedi 2026, and integrated airframe and propulsion control is Zeng et al. 2026. The article’s inlet inference, which had to be made from the vehicle’s top speed because no full-scale duct measurement survives, is the kind of question a modern programme would answer by computation before the first article was built.

Coupled Aerothermal Analysis

The article puts the aluminium recovery-temperature limit at Mach 2.27 with a one-line relation and a representative recovery factor. A modern programme would compute it coupled to the structure. Aerothermoelastic analysis is Kimmel et al. 2026 and Thawait et al. 2024b, the coupled aerothermal calculation itself is Bi et al. 2024, thermal protection and drag reduction together are Zuo et al. 2025, and optimisation across the aerothermal and structural problem at once is İpek 2025. The X-10 stopped just short of Mach 2.27 because it was made of aluminium, and the Navaho had to cross it. The accessible record gives no sign that the boundary was ever computed rather than met.

Parameter Identification From Flight Data

The X-10’s task was to estimate parameters of a system from flight data, and that is now a discipline. Aerodynamic parameter identification from flight test spans Cao and Wei 2020, Hui et al. 2019, and Kulhánek 2019, with in-flight lift and drag estimation in Bergmann et al. 2021 and unmanned flight-test evaluation in Arif and Sasongko 2021. The identifiability calculation performed above is the standard first question of that discipline and it was not asked in 1953. Here, more plainly than anywhere else, the article applies a later method to an earlier programme.

Validation Across the Model-to-Flight Gap

The article establishes that the free-flight models reached between a fifth and a half of full-scale Reynolds number, and that the full-scale vehicle then flew above the highest Mach number either ground method had covered. Quantifying the confidence such an extrapolation deserves is now its own subject. Uncertainty quantification of aerodynamic prediction is Eldredge and Mousavi 2026, Zhang et al. 2025f, and Li et al. 2023k, the turbomachinery case is Fu et al. 2023, surrogate-model credibility is Kirsch et al. 2025, and computational drag estimation for configuration trade studies is Jesudasan et al. 2026. A modern programme would attach a confidence interval to the extrapolation the X-10 programme made, and the article’s inability to say whether the sub-normal-shock duct recovery was real or an artefact of scale is the direct cost of that missing interval.

Gravity Modelling From Orbit

The deflection-of-the-vertical term that dominates the budget above is now largely a solved problem, because the gravity field has been surveyed from orbit to a resolution the 1950s could not approach. Satellite gravimetry and the geoid models built from it are what removed the term, and the star-tracker calibration work of Siemes et al. 2019 comes from the same mission family. The single largest irreducible error in the Navaho’s budget was eliminated not by a better instrument but by a better map, a kind of progress the programme could not have anticipated or purchased.

The quantity the article computes is still being refined. A modern vertical-deflection dataset is Schreutelkamp and Hirt 2026, and optimising a deflection model from multidirectional data is Li et al. 2025l.

The deeper inversion is that the error term has become a navigation aid. Where the Navaho was defeated by not knowing the gravity field, a modern vehicle matches the field it measures against a stored map and fixes its position from the residual, which turns the article’s dominant error source into an observation. Gravity-aided inertial navigation is Ahmadian 2026 and Mao et al. 2024, map matching against a gravity anomaly field is Li et al. 2026f and Li et al. 2024d, the gradient-tensor version is Wan et al. 2025b, Li et al. 2025c, and Gao et al. 2024a, and measuring the anomaly from a moving vehicle in the first place is Zhang et al. 2024d.

The Return of the Exposure Argument

The Navaho died because an airbreathing weapon is exposed for 172 minutes where a ballistic one is exposed for 32. That trade is live again, because the hypersonic glide vehicle is an attempt to get ballistic timelines with cruise-like manoeuvre, and the entire modern literature on tracking such a vehicle is an argument about how long the defender has.

Trajectory optimisation and manoeuvrability trade-offs for a glide vehicle are Doronzo 2026 and Bonavita et al. 2026. The defensive side, which is prediction of where such a body will be, is Cai and Zhuang 2025, Li et al. 2025j, Zang et al. 2025a, Jang and Park 2026, and Ünal et al. 2025, with the ballistic reference case in Dudush and Snovydovych 2026. The reason so much effort goes into predicting a glide trajectory is that manoeuvre destroys the closed-form prediction the article used to compute 32.2 minutes, and a defender who cannot predict has no engagement timeline at all. The Navaho’s argument here runs in reverse, which explains why the airbreathing option is being reconsidered rather than merely remembered.

Command Links and Latency

The article computes a radio horizon of 482 kilometres against a thousand-kilometre leg, so a one-way X-10 leg of that length would have taken the vehicle beyond command range. Modern unmanned operations have the same constraint and a much larger literature on living with it. Multi-hop command and telemetry is Miura 2022, and the human-factors consequence of a delayed link, which is that an operator cannot close a loop faster than the link allows, is Cox and Wong 2019 and Moniruzzaman et al. 2022. The X-10’s answer was to make the vehicle autonomous past the horizon, and practice now arrives at the same answer, seventy years and a great deal of bandwidth later.

Supersonic Cruise

Periodic cruise guidance for hypersonic vehicles is Gao et al. 2020b, integrated guidance and control for morphing hypersonic missiles is Bao et al. 2019, and ascent trajectory design is Zhai and Yang 2020. The airbreathing intercontinental weapon did not return, but the airbreathing hypersonic weapon is being attempted again, and the exposure-time argument that killed the Navaho applies to it in modified form.

Gyroscopes, accelerometers and the inertial instrument

The instrument whose drift the X-10 was built to measure. Gyroscopes of every mechanism, together with navigation accelerometers, their bias and drift, noise characterisation and temperature behaviour. 279 of these titles name a micro-electromechanical instrument and 230 a fibre-optic gyroscope, against 20 that name a floated, electrostatic, superconducting, cryogenic or dynamically tuned instrument of the older kinds. 141 titles name temperature or thermal effects, and 81 of those compensate the drift that temperature causes, which is the modern answer to the platform oven computed above.

1,046 records. [He et al. 2013a] [A Novel Method Based 2017] [Ajayan et al. 2024] [Akcayir and Ozkazanc] [Akhmadiev et al. 2021] [Albeshbeshy et al. 2024] [Aleinik et al. 2025] [Ali 2016] [Allen et al. 1995] [Anthony 2018] [Antonio Dollevedo] [Application of Strongly Tracking 2017] [Armenise 2010c] [Armenise 2010b] [Armenise 2010d] [Armenise 2010a] [Arslanova and Trutnev 2017] [Asadian et al. 2017] [Ash et al. 1998] [Aslam et al. 2008] [Avrutov et al. 2022] [Azgin et al. 2007a] [Azgin et al. 2007b] [Bahrami 1977] [Bai et al. 2011] [Bakunowicz and Rzucidło 2016] [Ban et al. 2021] [Ban et al. 2022b] [Barantsev et al. 2021a] [Bashir et al. 2024] [Batur et al] [Batur et al. 2006] [Bednarz et al. 1987] [Beiter 1970] [Belalcazar-Bolaños et al. 2023] [Belfadel and Haessig 2025] [Belousov and Krivosheev 2023] [Ben et al. 2010] [Benser et al. 2015] [Bergh 1990] [Bergh et al. 1982] [Bergh et al. 2026] [Berman et al. 2025] [Bettwy et al. 1971] [Beverini et al. 2014] [Bhatia and Geller 2020] [Bi et al. 2018] [Bielas et al. 1989] [Bo and Huan 2015] [Bobbili et al. 2014] [Bohm and Perermann 1987] [Bolotnov 2019] [Bondarenko et al. 2025] [Bowles et al. 2014] [Brodovsky and Dames 2026] [Broslavets et al. 2016] [Broslavets et al. 2021] [Brown 2013] [Bu et al. 2019] [Bu et al. 2022] [Bu et al. 2026b] [Buffoli et al. 2023] [Burdess 1983] [Burns 2006] [Burns et al. 1983] [Bush and Newton 1964] [Bussutil et al. 2022] [Demkowicz 2024] [Gusev and Puporevich 2021] [Hu et al. 2020a] [Jin et al. 2025a] [Liu et al. 2025i] [C.-W. Tan and Park 2005] [Cao 2023b] [Cao 2023f] [Cao 2023e] [Cao 2023c] [Cao 2023d] [Cao 2023g] [Cao 2023a] [Cao 2026] [Cao and Jian-hua 2018] [Cao and Zhou 2025] [Cao et al. 2015] [Cao et al. 2021a] [Cao et al. 2021b] [Cardarelli] [Carestia et al. 1983] [Carey et al. 2019] [Carr et al. 2014] [Carrara et al. 1987b] [Carrara et al. 1987a] [Carrington 1970] [Carter et al. 2020] [Cechowicz 2017] [Cerre et al. 1997] [Chabbi and Rao 2024] [Chabbi and Rao 2025] [Chakraborty 1996] [Challoner and Marshall 2024] [Challoner et al. 2014] [Chamoun and Digonnet 2015] [Chang 1999] [Chang et al. 2020] [Changhong Wang and Boran Li 2010] [Che et al. 2023] [Chen 2008] [Chen and Cui 2016] [Chen and Shen 2013] [Chen and Wang 1988] [Chen and Zhong 2020] [Chen et al. 2014a] [Chen et al. 2017b] [Chen et al. 2019c] [Chen et al. 2019a] [Chen et al. 2021a] [Chen et al. 2022d] [Chen et al. 2023b] [Chen et al. 2023e] [Chen et al. 2023d] [Chen et al. 2024c] [Chen et al. 2024d] [Chen et al. 2024b] [Chen et al. 2025b] [Chen et al. 2025f] [Chernyak and Tarash 2026] [Chi and Chen 2009] [Chikovani 2012] [Chikovani 2013] [Chikovani 2022] [Chikovani and Golovach 2022] [Chikovani and Tsiruk 2014] [Cho et al. 2020] [Choi et al. 2023b] [Chong Zhang et al. 2010] [Christian et al. 1991] [Christian et al. 1992] [Chu and Fei 2016] [Chumankin 2014] [Chyba 1991] [Cigada et al. 2005] [Coelho Martins] [Colin] [Cooper 1965] [Cooper 1970] [Cordova et al. 1994] [Costandin et al. 2021] [Crain et al. 2010] [Crawley and Maunder 1966] [Crowley et al. 1971] [Cucci et al. 2016] [Cui and Zhao 2020] [Cui and Zhao 2021] [Cui and Zhao 2023] [Cui et al. 2019b] [Cui et al. 2019a] [Dachuan Liu et al. 2008] [Damrongsak and Kraft 2006] [Dangui et al. 2009] [Dankowych et al. 1986] [Dao et al. 2017] [Daum et al] [Davis et al. 2002] [De Carlo et al. 2022] [Dehghani et al. 2019] [Dejaeger et al. 2022] [Delaye 2000] [DeMars et al. 2014] [Demenkov and Tran 2019] [Denaci et al. 1968] [DeNatale et al. 2023] [Deokhwa Hong et al. 2008] [Dewar et al. 1993] [Deyle 2005] [Diao et al. 2013] [Digonnet 2014] [Digonnet et al. 2006] [Din et al. 2022] [Ding et al. 2022] [Dinh and Ogami 2012] [Dion et al. 2018] [Divakaruni et al. 2008] [Domaratzky et al. 1997] [Dong 2013] [Dong and Gao 2017] [Dong et al. 2010] [Donguk Yang et al. 2015] [Drift data for the 1965] [Droeschel et al. 2011] [Nunzi 2006] [Egorov and Novikov 2023] [Einwoegerer et al. 2010] [Elwell 1991] [Eminoglu and Boser 2018] [Endean et al. 2017] [Endean et al. 2019] [Engedy and Horvath 2015] [Erkan and Tatar 2024] [Sorgi 2009] [Ettl et al. 2016] [Evduzen 2026] [Ezekiel 1980] [Ezekiel and Balsamo 1977] [Fadaki et al. 2023] [Fairbank 1983] [Fan and Wang 2016] [Fan et al. 2019a] [Fan et al. 2019b] [Fan et al. 2022] [Fan et al. 2024] [Fast et al. 2008] [Fazelinia et al. 2024] [Fedele et al. 2018] [Fei and Batur 2007] [Fei and Yuan 2013] [Fei et al. 2010] [Feldman 1974] [Fell 2006] [Feng 2000] [Feng and Huang 2014] [Feng et al. 2014] [Feng et al. 2022] [Feng et al. 2026b] [Feng Sun et al. 2009] [Ferguson et al. 2005] [Filatov et al. 2022] [Fischer et al. 1995] [Forke et al. 2024] [Frigo 1986] [Frigo 1987] [Fu et al. 2014b] [МГТУ им. Н.Э. Баумана et al. 2018] [Galante and Sanner 2012] [Galyagin et al. 2017] [Gao et al. 2007] [Gao et al. 2026] [Garon et al. 2003] [Gates 1964] [Ge et al. 1995] [Geng and Li 2024] [Gersdorf and Freese 2013] [Ghanizadegan and Hashim 2025a] [Ghanizadegan and Hashim 2025c] [Gill et al. 2022] [Gill et al. 2023a] [Gill et al. 2023b] [Gilmore 1967] [Gilmore et al] [Gilster] [Grant and Digonnet 2019] [Grine et al. 2026] [Gu et al. 2018] [Gu et al. 2019a] [Gu et al. 2021b] [Gu et al. 2022] [Gu et al. 2025] [Gundavarapu et al. 2017] [Guo and Hong 2019] [Guo et al. 2012b] [Guo et al. 2017a] [Guo et al. 2020] [Guo et al. 2026a] [Gurung et al. 2023] [Gyroscope Technology 1 2004] [Gyroscope Technology 2 2004] [Habibi et al. 2008] [Haipeng et al. 2007] [Haipeng et al. 2009] [Ham 2022a] [Ham 2022b] [Hamelin et al. 2013] [Han and Sabbagh 2022] [Han et al. 2023] [Hand 1974] [Hao and Tian 2005] [Harding 1965] [Harding and Lawson 1968] [Hartl et al. 1992] [Hayner 2018] [Hayner and Challoner 2023] [He et al. 2019] [Hein et al. 1989] [Hilgemann et al. 2016] [Hiller et al. 2019] [Hoang and Pietrosanto 2021] [Hoflinger et al. 2012] [Hokmabadi et al. 2020] [Holovatyy et al. 2008] [Hong et al. 2026] [Hosseini-Pishrobat and Tatar 2025a] [Hosseini-Pishrobat and Tatar 2025b] [Hosseini-Pishrobat et al. 2023] [Hosseini-Pishrobat et al. 2024] [Hosseini-Pishrobat et al. 2025] [Hosseini-Pishrobat et al. 2026] [Hotate and Tabe 1986b] [Hotate and Tabe 1986a] [Hotate and Tabe 1987] [Hsu and Tekippe 1984] [Hsu et al. 2017] [Hu and Gallacher 2015] [Hu and Gallacher 2016] [Hu and Gallacher 2018] [Hu and Gallacher 2019] [Hu and Liu 2012] [Hu et al. 2009] [Hu et al. 2011] [Hu et al. 2023a] [Huaming Qian et al. 2009] [Huang et al. 2016b] [Huang et al. 2023a] [Huang et al. 2025a] [Huang et al. 2025b] [Huang et al. 2025c] [Hui et al. 2017] [Hung et al. 1988] [Hutchinson and Inglima 1970] [Hörsting and Wenzel 2025] [Черняк and Колесник 2019] [Indeitsev et al. 2022] [Inertial Instrumentation 1997] [3 Inertial Measurement Units 2001] [3 Inertial Measurement Units 2023] [Inertial Sensors and Inertial 2021] [Inertial Sensors and Inertial 2025] [Волков and Рижков 2018] [Integrated MEMS Inertial/GPS Navigation 2002] [Iozan et al. 2010] [Ito et al. 2024] [Bertaska 2025] [Iwatsuki 1991] [Jankovitz and Perdzock] [Jaroszewicz and Szustakowski 1995] [Ji et al. 2006] [Jia et al. 2021] [Jia et al. 2024] [Jia et al. 2025] [Jiang et al. 2024] [Jiang et al. 2025b] [Jianli and Min 2010] [Li et al. 2011] [Jin and Culshaw 1992] [Jing et al. 2013] [Jo and Yoon 2024] [Johnson 1985] [Johnson et al. 2015] [Jolly et al. 2022] [Juang and Radharamanan] [Junlong et al. 2013] [Kadiwar and Giles 1989] [Kaicheng Chang and Liang 2005] [Kaiser 1970] [Kaji et al. 2020] [Kajioka et al] [Kajioka et al. 1992] [Kaku 1990] [Kalantarov and Search 2013] [Kalenova 2009] [Kamer and Ikizoglu 2013] [Kang et al. 2019] [Kanter 1966] [Karachun et al. 2016] [Karagöz et al. 2024] [Karwacki et al] [Karwacki et al. 1996] [Kashima et al. 1991] [Kaswekar and Wagner 2015] [Kato et al. 2010] [Kau et al. 1983] [Kaya et al. 2019] [Ke et al. 2025] [Kersey et al. 1989] [Ketterle et al. 2008] [Khan et al. 2017] [Khan et al. 2023] [Khasawneh and Batur 2003] [Khilnani et al. 2026] [Kholopov 2015] [Killian] [Killian 1994b] [Kim and Shaw 1984a] [Kim and Shaw 1984b] [Kim et al. 2011b] [Kim et al. 2015b] [Kim et al. 2022b] [Kim et al. 2022a] [Kim et al. 2026a] [Kirnos et al. 2020] [Kline et al. 2013] [Knudsen and Bløtekjær 1995] [Koenig et al. 2019] [Koh et al. 2026] [Kolbas et al. 2015] [Kolbas et al. 2018] [Kolbas et al. 2022] [Kong and Schuck 1966] [Korobiichuk et al. 2022] [Kourepenis et al] [Krogmann 1988] [Крылов and Кузнецов 2019] [Kuang et al. 2022] [Kuang et al. 2023] [Kublanova et al. 2021] [Kumar et al. 2016] [Kuznetsov et al. 2014] [Kuznetsov et al. 2015] [Kwon et al. 2017] [Lai et al. 2026] [Laita et al. 2024] [Lamont 1973] [Lan and Xu 2026] [Langford 1965] [Langford 1966] [Larin and Tunik 2012a] [Larsen and Bulatowicz 2014] [Laser-Driven Fiber-Optic Gyroscope 2025] [LaViolette and Bossler] [Lawrence 1993a] [Lawrence 1993c] [Le Traon et al. 2018] [Leccadito et al. 2015] [Lee] [Lee et al. 2016a] [Lee et al. 2016b] [Lefevre 1988] [Lefevre 1993] [Lefevre 1996] [Lefevre 2012] [Lefevre et al. 1982] [Lefevre et al. 1987] [Lefèvre 1996] [Lefèvre 1997] [Lefèvre 2012] [Lefèvre 2013] [Lei et al. 2014b] [Leland 2002] [Leonardson and Foote] [Lestev and Fedorov 2012] [Leung 2010] [Li 2013] [Li et al. 2009a] [Li et al. 2009b] [Li et al. 2015e] [Li et al. 2015a] [Li et al. 2015c] [Li et al. 2016a] [Li et al. 2016c] [Li et al. 2017g] [Li et al. 2017d] [Li et al. 2019a] [Li et al. 2021g] [Li et al. 2022d] [Li et al. 2023j] [Li et al. 2023a] [Li et al. 2023i] [Li et al. 2023f] [Li et al. 2023e] [Li et al. 2024a] [Li et al. 2024g] [Li et al. 2024f] [Li et al. 2024e] [Li et al. 2025e] [Li et al. 2025m] [Li et al. 2025h] [Li et al. 2025d] [Li et al. 2025i] [Li et al. 2026m] [Jialei et al. 2011] [Li Yun et al. 2011] [Li-Xia and Zhen-zhen 2024] [Liang and Zhang 2009] [Liang et al. 2018] [Liewald et al. 2012] [Lijun and Fang 2019] [Lin 1978] [Lin et al. 2021] [Liu et al. 2010c] [Liu et al. 2011a] [Liu et al. 2012c] [Liu et al. 2014a] [Liu et al. 2014b] [Liu et al. 2017d] [Liu et al. 2020d] [Liu et al. 2020b] [Liu et al. 2022d] [Liu et al. 2022j] [Liu et al. 2023f] [Liu et al. 2023h] [Liu et al. 2023a] [Liu et al. 2023d] [Liu et al. 2023k] [Liu et al. 2024a] [Liu et al. 2025b] [Liu et al. 2025a] [Liu et al. 2026c] [Jieyu et al. 2012] [Lloyd et al. 2011] [Lorenzini and Neeland 1971] [Loret et al. 2014] [Lory et al. 1971] [Lu and Fei 2014] [Lu and Fei 2015] [Lu et al. 2017c] [Lu et al. 2023] [Lu et al. 2024] [Lu et al. 2025] [Luo and Chen 2024] [Luo et al. 2014] [Léfèvre 1989] [Ma 2014] [Ma et al. 1998] [Ma et al. 2021] [Ma et al. 2023c] [Macy 1995] [Maeda et al. 2017] [Mahudapathi et al. 2022] [Malan et al. 2016] [Manerikar] [Mao et al. 2010] [Mao et al. 2021] [Marchesoni 1986] [Marconi et al. 2021] [Marjoux et al. 2020] [Marolleau et al. 2024] [Martin 2004] [Martinenq 2021] [Martynenko 1970] [Marwan et al. 2019] [Marx et al. 2017] [Marx et al. 2018] [Marx et al. 2025] [Maslov et al. 2023] [Mason and Wedekind 1970] [Mateus et al. 2009] [Matsumoto et al. 2015] [Matthews and Rybak 1992] [Matthews et al. 1981] [Mazzoni et al. 2021] [McCartney 1966] [McLandrich and Rast 1978] [Mei et al. 2013] [MEMS Inertial Sensors 2004] [Meng et al. 2022b] [Meshkovsky et al. 2011] [Messinger and Parker 1963] [Metzger 1970] [Miani et al. 2022] [Miani et al. 2025] [Miani et al. 2026] [Mikko Saukoski 2006] [Miller 1965] [Minford et al. 1987] [Minford et al. 1988] [Minford et al. 1990] [Miniature Inertial Measurement Unit 2018] [Miranda et al. 2023] [Mitani et al. 2018] [Mitani et al. 2021] [Moeller et al. 1988] [Molchanov et al. 2018] [Monir Hossain and Abdul Muthalib 2025] [Moore 1984] [Moraes et al. 2019] [Morrison 1988] [Motohara and Ohno] [Motohara and Ohno 1992] [Mou et al. 2021b] [Mustafazade and Seshia 2018] [Mynbaev] [Napolitano et al. 2017] [Narasimhappa et al. 2015] [Naser-Moghadasi et al. 2013] [Natale et al. 2023] [Navigation-Grade Inertial Sensors 2022] [Nazdrowicz and Napieralski 2019] [Nazemipour et al. 2020] [Nejad and Pourmahyabadi 2006] [Nelson and Macklin] [Niehus and Mracek 2010] [Nikiforovskii et al. 2022] [Ninalalov et al. 2022] [Ning et al. 2025a] [Ning et al. 2025b] [Nishino et al. 2025] [Nishiura et al. 1985] [Nishiura et al. 1986] [Nitzan et al. 2014] [МГТУ им. Н.Э. Баумана et al. 2017] [Nunes and Sakamoto 2024] [Nusbaum et al. 2019] [O’Kane and Ringwood 2013] [Oelschlaeger and Thielman] [Ogut et al. 2017] [Oh and Kim 2024] [Ohno et al. 1992] [Ohno et al. 1994] [Ohno et al. 2026] [Ohtsuka 1985] [Ono et al. 2020] [Osunluk et al. 2018] [Osunluk et al. 2020] [Ouyang et al. 2024] [Paces 2014] [Pagani et al. 2020] [Pai et al. 2012] [Painter and Shkel 2001] [Pak et al. 2023] [Pakniyat and Salarieh 2013] [Pan et al. 2017] [Pandit et al. 2018] [Pang et al. 2008] [Paoletti 1996] [Parajuli et al. 2022] [Park et al. 2026] [Parkhomey et al. 2023] [Parrish et al. 2025b] [Pasik et al. 1975] [Passenheim and Mallon 1978] [Patel and Faruque 2021] [Patel and McCluskey 2012] [Patterson et al] [Pavesi et al. 2025] [Pavlath 1995] [Peng et al. 1987] [Peng et al. 2007] [Pepper and Wang 1983] [Perelyaev et al. 2017] [Perrier et al. 2022] [Petrenko 2014] [Pick 1986] [Pileri and Langfelder 2025] [Pishchela et al. 2023] [Pishrobat and Keighobadi 2014] [Pr et al. 2015] [Prikhodko et al. 2017] [Prikhodko et al. 2019] [Charu Priya and Deepa 2024] [Priydarshi et al. 2016] [Pérez et al. 2016] [Qi and Wang 2024] [Qi et al. 2026a] [Qi et al. 2026b] [Qian et al. 2009] [Qin et al. 2009] [Qin et al. 2011] [Qin et al. 2014] [Qin et al. 2016] [Qin et al. 2021] [Qu Pingping et al. 2009] [Quan et al. 2014] [Rahangdale 2025] [Rahmani 2018] [Rajagopal et al] [Ranji et al. 2022] [Rao et al. 2022] [Rashed et al. 2013] [Rashleigh and Burns 1980] [Rashleigh and Burns 1981] [Raspopov and Volchikhin 2018] [Rawashedeh and Lumpp 2014] [Reed et al. 2025] [Reitbauer et al. 2023] [ren et al 2024] [Ren-Young Liu et al] [Zhang et al. 2022h] [Ribes et al. 1996] [Rodiegard et al] [Rodríguez Martínez] [Ruan et al. 2021b] [Ruan et al. 2021a] [Ruan et al. 2022] [Ruan et al. 2023a] [Ruan et al. 2025] [Rubio et al. 2010] [Ruffin 2002] [Ruffin 2008] [Ruffin 2017] [Ryan and Bevly 2014] [Chandak and Patil 2014] [Saahar and Durai 2013] [Sabatelli et al. 2011] [Sakr and Wassal 2010] [Saletović and Kriještorac 2025] [Salman et al. 2022] [San Martin et al. 2022] [Sanatdoost et al. 2013] [Sanders 1993] [Sarapuloff et al. 2016] [Schleich and Dobiasch 1984] [Schoch and Darrel 1967] [Schreiber et al. 2014] [Schuler and Slater 1967] [Schuler et al. 2022] [Schwartz 2008] [Schwartz et al. 2007b] [Schwartz et al. 2007a] [Senkal et al. 2015] [Seo et al. 2022] [Shang 1990] [Shang et al. 2020] [Shang et al. 2021] [Shang et al. 2022] [Shang et al. 2025] [Shankar and Kumar 2023] [Sharma et al. 2011] [Shaw et al. 1986] [Sheem 1980] [Shen 2021b] [Shen 2021a] [Shen 2021c] [Shen et al. 2011] [Shen et al. 2016] [Shen et al. 2019] [Shevchenko et al. 2025] [Shi et al. 2017] [Shi et al. 2019c] [Shi et al. 2019b] [Shi et al. 2020] [Shi Qiang Liu et al. 2015] [Shiau et al. 2011] [Shipplett 1982] [Shooshtari et al. 2012] [Shu et al. 2018] [Shu et al. 2020] [Shujah et al. 2021] [Shupe 1981] [Sierociuk et al. 2024] [Sierociuk et al. 2025] [Sinelnikov et al. 2023] [Singh et al. 2020] [Sinkiewicz et al. 1974] [Sireesha and Sreenivasa Ravi 2015] [Skaloud et al. 1999] [Skog et al. 2014] [Slomyanskiy 1962] [Smith and Dorschner 1978] [Son et al. 2023] [Song et al. 2001] [Song et al. 2012] [Song et al. 2017a] [Song et al. 2019] [Sonmezoglu et al. 2012] [Sonmezoglu et al. 2013] [Sonmezoglu et al. 2014] [Sorgenfrei et al. 2016] [Soto and Hernandez 2004] [Spammer and Swart 1992] [Sperry Gyroscope Co Great Neck Ny 1963a] [Sruthi and Nagaraja 2015] [Statz et al. 1985] [Stieler 1971] [Stimac et al] [Strandjord and Sanders 1993] [Stuart et al. 1987] [Su et al. 2013a] [Sun and Li 2018] [Sun et al. 1987] [Sun et al. 2026a] [Suzuki et al. 2019] [Swanson 1962] [Taheri-Tehrani et al. 2014] [Taibi et al. 2021] [Takahashi et al. 1990] [Takahashi et al. 2024] [Takahashi et al. 2025] [Takei et al. 2022] [Tan et al. 2018] [Tan et al. 2026] [Tanenhaus et al. 2010] [Tang et al. 2024b] [Tao et al. 2014] [Tao et al. 2025] [Tao et al. 2026] [Tashtay et al. 2025] [Tatar et al. 2014] [Tatar et al. 2017] [Templier] [Teng et al. 2015b] [Tennstedt and Schön 2025] [Tereshkov 2013] [The Admiralty Gyro-Magnetic Compass 1955] [The Fiber-Optic Gyroscope 1993] [Tian et al. 2011] [Tong et al. 2025] [Trifonova and Ushakov 2021] [Trutnev 2015] [Trutnev 2019a] [Trutnev 2019b] [Trutnev and Shchenyatskiy 2022] [Trutnev et al. 2020] [Tsai and Chung 2026] [Tsukamoto and Tanaka 2017] [Tsukamoto and Tanaka 2018] [Tsukamoto and Tanaka 2019] [Tsukamoto and Tanaka 2022] [Tsukamoto et al. 2024] [Tu and Peng 2021] [Tu et al. 2020] [Turenko and Pryhodko 2024] [Tuzhanskyi and Sakhno 2015] [Udd and Cahill 1984] [Ullah et al. 2015] [Ulrich 1982] [Us and Avershin 2021] [Usui 1999] [Vafanejad and Kim 2015] [Valenti et al. 2013] [Vatanparvar and Shkel 2022] [Vikas and Crane 2014] [Vimal et al. 2025] [Vogel et al. 1989] [Volkov and Galunova 2018] [Wainer et al. 2023] [Walker and Engelke 1990] [Walsh 1998] [Walther et al. 2013] [Wan et al. 2017] [Wan et al. 2019] [Wang 2017] [Wang and Asokanthan 2005] [Wang and Cao 2020] [Wang and Cao 2022] [Wang and Chen 2016] [Wang and Chen 2018b] [Wang and Han 2020] [Wang and Wang 2010] [Wang and Wang 2018] [Wang and Xiao 2017] [Wang et al. 2006] [Wang et al. 2010c] [Wang et al. 2010b] [Wang et al. 2011a] [Wang et al. 2012d] [Wang et al. 2012c] [Wang et al. 2012e] [Wang et al. 2013b] [Wang et al. 2013e] [Wang et al. 2013a] [Wang et al. 2013f] [Wang et al. 2014e] [Wang et al. 2014c] [Wang et al. 2014d] [Wang et al. 2016d] [Wang et al. 2016a] [Wang et al. 2017d] [Wang et al. 2017b] [Wang et al. 2018c] [Wang et al. 2018a] [Wang et al. 2020l] [Wang et al. 2020j] [Wang et al. 2020i] [Wang et al. 2020e] [Wang et al. 2021e] [Wang et al. 2021a] [Wang et al. 2021b] [Wang et al. 2021d] [Wang et al. 2022c] [Wang et al. 2023g] [Wang et al. 2023n] [Wang et al. 2024f] [Wang et al. 2024c] [Wang et al. 2024o] [Wang et al. 2024g] [Wang et al. 2025m] [Wang et al. 2025b] [Wang et al. 2025j] [Wang et al. 2025o] [Wang et al. 2026m] [Wang et al. 2026h] [Wang et al. 2026f] [Wang Kedong et al] [Каликанов 2024] [Weber et al. 2020] [Wei et al. 2011] [Wei et al. 2019] [Wei et al. 2021] [Wei et al. 2022b] [Wei et al. 2026c] [Wei Gao et al. 2007] [Wei Wang and Chen 2016] [Weinstock 1968] [Weir and Wells 1990] [Wen et al. 2020] [Weng et al. 2020] [Wheeler and Digonnet 2021] [Wheeler et al. 2018] [Wiberg et al. 2001] [Wu et al. 2002a] [Wu et al. 2011b] [Wu et al. 2021a] [Wu et al. 2021b] [Wu et al. 2023b] [Xia et al. 2019] [Xia et al. 2020] [Xi et al. 2020] [Xiao et al. 2012] [Su 2025] [Xie et al. 1998] [Xie et al. 2018] [Xie et al. 2019a] [Xing et al. 2019a] [Xiong and Dong 2011] [Xiong et al. 2017] [Xu 2021] [Xu et al. 2005] [Xu et al. 2007a] [Xu et al. 2007b] [Xu et al. 2009] [Xu et al. 2016b] [Xu et al. 2018] [Xu et al. 2019a] [Xu et al. 2020b] [Xu et al. 2021a] [Xu et al. 2022c] [Xu et al. 2025d] [Xu et al. 2026a] [Xu et al. 2026b] [Xudan et al. 2007] [Xudong Yu et al. 2016] [Yahalom et al. 2010] [Yampolsky and Klein 2025] [Yamron 1968] [Yan et al. 2013] [Yan et al. 2023c] [Yan et al. 2025] [Yan et al. 2026a] [Yan et al. 2026b] [Yan-zhu and Yun 2004] [Yang 2004] [Yang 2012] [Yang 2014] [Yang and Fei 2013] [Yang et al. 2009a] [Yang et al. 2014] [Yang et al. 2015] [Yang et al. 2018c] [Yang et al. 2019] [Yang et al. 2020b] [Yang et al. 2026e] [Yang et al. 2026c] [Yavuz et al. 2025] [Yavuz et al. 2026] [Yertutanol et al. 2021] [Yi et al. 1995] [Yi et al. 2014b] [Yichie et al. 2025] [Yin et al. 2011] [Ying Kun Peng and Golnaraghi] [Yinqiang Zhang et al. 2010] [Yong et al. 2015] [Yoshino et al. 1986] [Yu 2012] [Yu et al. 2015b] [Yu et al. 2016b] [Yu et al. 2017] [Yu et al. 2022b] [Yu et al. 2023b] [Yu et al. 2023a] [Yu et al. 2024] [Yu et al. 2025b] [Yu et al. 2025a] [Yu et al. 2026] [Xudong et al. 2013] [Yuan et al. 2024c] [Yuan et al. 2024b] [Yuan et al. 2026b] [Yang and Yang 2016] [Yun et al. 2013] [Yusefi et al. 2023] [Zaman et al] [Zaman et al. 2008] [Zaman et al. 2009] [Zarei et al. 2012] [Zarinetchi and Ezekiel 1986] [Zbrutsky and Trunov 2020] [Zeng and Lysa 2024] [Zeng et al. 2020] [Zeng et al. 2025b] [Zeng et al. 2025c] [Zeng et al. 2025a] [Zhang and Gao 2012] [Zhang and Li 2025] [Zhang and Yang 2012] [Zhang and Zhou 2026] [Zhang et al. 2007] [Zhang et al. 2009a] [Zhang et al. 2014e] [Zhang et al. 2014d] [Zhang et al. 2015] [Zhang et al. 2016a] [Zhang et al. 2018f] [Zhang et al. 2021c] [Zhang et al. 2021k] [Zhang et al. 2021j] [Zhang et al. 2021h] [Zhang et al. 2022i] [Zhang et al. 2023c] [Zhang et al. 2024g] [Zhang et al. 2024c] [Zhang et al. 2025i] [Zhang et al. 2025m] [Zhang et al. 2026c] [Zhang et al. 2026d] [Zhang et al. 2026l] [Zhang Xiangping et al. 2008] [Zhao 2014] [Zhao et al. 2016b] [Zhao et al. 2017a] [Zhao et al. 2020a] [Zhao et al. 2021c] [Zhao et al. 2022d] [Zhao et al. 2022g] [Zhao et al. 2022b] [Zhao et al. 2022a] [Zhao et al. 2023a] [Zhao et al. 2025e] [Zhao et al. 2026d] [Zhao et al. 2026e] [Zhao Hongbo et al. 2013] [Zhbanov and Zhuravlev 2007] [Zheng et al. 2015] [Zheng et al. 2019] [Zhixiong et al. 2011] [ZhongGuo et al. 2018] [Zhou and Zhang 2010] [Zhou et al. 1999] [Zhou et al. 2009] [Zhou et al. 2021c] [Zhou et al. 2023b] [Zhou et al. 2025a] [Zhu and Shang 2023] [Zhu et al. 1996] [Zhu et al. 2016b] [Zhu et al. 2025b] [Zhuang et al. 2025] [Zhuravlev 2015] [Zhuravlev 2018] [Zhuravlev et al. 2018] [Zhuravlev et al. 2019] [Zijian et al. 2014] [Zotov et al. 2014b] [Zotov et al. 2022] [Zubarev et al. 2023] [Zuoming et al. 2016] [Zwahlen et al. 2012] [Çelikel and Sametoğlu 2012]

Canard configurations, missile aerodynamics and drag

The airframe the testbed was built to validate. Canard configurations, missile aerodynamics, wave, base and transonic drag, the area rule and supersonic aircraft design. 154 titles name a canard, from the NACA configuration studies of the 1950s to canard-controlled missiles and close-coupled canard fighters.

965 records. [A Series of Airfoils 1982] [A Thick Film Guidance 1974] [Abarbanel 1977] [Abate et al. 2000] [Abdallah Mohamed 2019] [Abney and McDaniel 2005] [Abraham et al. 2023] [Abraham et al. 2024] [Agarwal and Augustinus 1999] [Miley et al. 1992] [Agnone 1984] [Agrell and Elmeland 1984] [Ahmad et al. 1993] [Air Force Flight Test Center Edwards AFB CA 1974] [Aksteter et al. 1995] [Alaverdi and Paris 2001] [All Things Must End 2006] [Allen 1954] [Allen 1981] [Allen and Pittman 1983] [Allen and Tuttle 1973] [Allen and Watson 1994] [Altman 1965] [Anderson 1960] [Anderson 1979] [Anderson 1984a] [Anderson 1986] [Anderson and Feistel 1985] [Andrus 1979] [Appendix C 2004] [Appendix 2001] [Aprovitola et al. 2022] [Apstein and Titow 1996] [Arbic and Gillespie 1953] [Armenta and Takahashi 2021] [Army Missile Command Redstone Arsenal AL 1961] [Asim et al. 2022] [Asouti et al. 2023] [Auman and Kreeger 1998] [Auman and Wilks 2003] [Auman et al. 1994] [Baals and Harris 1968] [Baals et al. 1970] [Baer 1966] [Bailey and Starr 1976] [Baker and Galigher 1960] [Balakrishnan and Shen 1996] [Ball 1978] [Ball and Smith 1956] [Bandyopadhyay 1989] [Banks and Paulson 1987] [Bardina et al. 1988] [Barnett 1962] [Barnwell 1974] [Barnwell 1976] [Bartlett and Harris 1972] [Basics of Missile Guidance 2007] [Bauer and McMillin 1988] [Bauer et al. 2026] [Bergmann et al. 2021] [Bhutta and Lewis 1992] [Biber 2015] [Biblarz et al. 1998] [Bijker and Steyn 2008] [Biot 1949] [Birch and Cleminson 2004] [Birch and Petterson 2004] [Birch et al. 2000] [Blair 1978b] [Blair 1978a] [Blair 1990a] [Blair and Grow 1973] [Blair and Rapp 1980] [Blair et al. 1983] [Blair et al. 1992] [Blake and Gillard] [Blake and Simon 1998] [Blanchard 1953] [Blank 1995] [Blom et al. 1991] [Blood et al. 2015] [Bond and Swanson 1953] [Boppe and Aidala 1980] [Bowman and Healy 1959] [Boyd 1965] [Boyd and Menees 1959] [Brandon et al. 2001] [Bright and Peterson 1960] [Bromberg 1992] [Brooks and Cone 1966] [Brower 1989] [Brown 1955] [Brown 1957] [Brown 1961] [Brown 1987] [Bryson 1971a] [Bryson and Desai 1968] [Bryson et al. 2019] [Bryson 1971b] [Buell and Tinling 1959] [Bullard 1965] [Bushnell 1990] [Bushnell 2004] [Butsko 1966] [Bychkov et al. 2020] [Cagle 1977] [Calarese and Walterick 1978] [Candler 2001] [Candler and Kelley 1999] [Capone et al. 1996] [Carlsen 1994] [Carlson 1953] [Carmel et al. 1958] [Carrier et al. 2021] [Cassel et al. 1969] [Catalano and Sturek 2000] [Catalano and Sturek 2001] [Cavalleri and Posey 1988] [Celmins 1990] [Cenko 1979] [Chamberlin and Blaha 1973] [Chambers and Yip 1984] [Chambers et al. 1984] [Chan et al. 2017] [Chandler 1958] [Chang 1962] [Chapman et al. 1999] [Chasoglou et al. 2021] [Chen et al. 2026f] [Chin 1977] [Chin 1978] [Coder and Schmitz 2019] [Coe and Graham 1976] [Coe et al. 1977] [Coetsee et al. 1995] [Coirier et al. 2014] [Coleman et al. 1978] [Cook et al. 2004] [Covell 1985] [Covell et al. 1987] [Covell et al. 1990] [Craig et al. 1980] [Cramer and Lee 1992] [Crane and Adams 1950] [Crane and Reeder 1945] [Crogan 1961] [Cronvich and Liepman 1979] [Cruise Missile 2009] [Cruise Missiles] [Cruise Missiles 2015] [Cumming et al. 2016] [Cummings et al. 1995] [D’Aiutolo and Henning 1956] [D’Aiutolo et al. 1957] [Dalton and Balakrishnan 1993] [Danowsky et al. 2017] [Davies 2020] [Davies 2025] [de Nicola et al. 1994] [Debiasi et al. 2010] [DeChant 2010] [Decker 2002] [Delurgio et al. 1981] [Deng and Qin 2021] [Desai et al. 1977] [DeSpirito 2008] [DeSpirito 2009] [DeSpirito and Sahu 2001] [DeSpirito et al. 2002] [DeSpirito et al. 2003] [DeVorkin 1992] [Dickey 1958] [Dickey 1959] [Dietz 2005] [Differential Geometry Applied 2016] [Dillenius 1985] [Dillenius 1986] [Dillenius and Nielsen 1979] [Dillenius et al. 1982] [Dillenius et al. 2002] [Doherty et al. 2018] [Donahue et al. 2008] [Dong et al. 2019] [Doronin 2019] [Dorres 1972] [Driver 1957] [Driver 1958] [Driver 1960] [Driver 1974] [Duan et al. 2016] [Duck 1973] [Dugan 1959] [Duncan and Huisken 1982] [Донской et al. 2021] [Eastman 1983] [Eidell et al. 2012] [Ekaterinaris 1994] [Eldredge and Mousavi 2026] [Ellison 1977] [Eminton and Lord 1956] [Er-El 1983] [Eremenko et al. 2003] [Erickson et al. 1990] [Ericsson 1980] [Ericsson and Reding 1974] [ESDU Data Item Estimates 1998] [Est and Nelson 1991] [Etzkorn 2001] [Evans 1954] [Facinelli and Nicks 1995] [Falunin and Ul’yanov 1967] [Famellos et al. 2024] [Faruqi 2012] [Fawcett et al. 1992] [Fedorov and Malmuth 1997] [Feistel 1985] [Fischenberg 1995] [Fischetti and Whitcomb 1953] [Fite 1993] [Flaherty 1977] [Flaherty 1979] [Fleck 1983] [Florio et al. 2019] [Foster 1959a] [Foster 1959b] [Fournier 1961] [Fournis 2022] [Fraenkel 1958b] [Fraenkel 1958a] [Frayer 1965] [Fresconi et al. 2018] [Frierson and Van Meter 1977] [Fry and Sage 1974] [Fu 1995] [Fu and Liang 1991] [Fu and Liang 1993] [Fu et al. 2023] [Fuhrmann 1993] [Fujino and Kawamura 2003] [Furukawa and Makino 2007] [Gad-El-Hak and Ho 1986] [Gainer 1961] [Gao 2023] [Gao Feng and Ma Cen Rui 2011] [Garabedian 1976] [Garcia-Velo and Walker 1995] [Gardner 1953] [Gardner and Edmondson 1950] [Gardner et al. 1948] [Gas Generators for Base 1976] [Gates and Schy 1952] [Gatlin et al. 2012] [Ge et al. 2018] [General Dynamics/Astronautics San Diegoca 1961] [Genova 2005] [Gillespie 1960] [Gillespie and Arbic 1951] [Gillis and Chapman 1956] [Gillis and Mitchell 1957] [Glessner 1999] [Gloss 1974b] [Gloss 1974a] [Gloss 1975] [Gloss 1978] [Gloss and Washburn 1977b] [Gloss and Washburn 1977a] [Gloss and Washburn 1979] [Gold and Busan 1994] [Goldsmith 1964] [Goodall and Ewen 1987] [Goodsell et al. 2000] [Gordon 1990] [Goto et al. 2007] [Grant and Sevier 1960] [Grauer and Morelli 2015] [Graves 1972] [Graves and Robins 1980] [Green 1992] [Greene 1957] [Gregoriou 1989] [Griffin and Jonas 1983] [Grigsby 1954] [Gross 1976] [Guan 2013] [Guan 2014] [Guimarães et al. 2021] [Guo et al. 2022] [Guotong Sun and Shuo Tang 2010] [Gupta 2023] [Gurfil 2012] [Guy et al. 1999] [Guy et al. 2000] [Guy et al. 2001] [Hahne 1989] [Hahne 1997] [Hall 1952a] [Hall 1952b] [Hall 1956a] [Hall 1956b] [Hall 2002] [Hall and Sandahl 1951] [Hallstaff 1966] [Hamada 2020] [Hamada and Tamura 2019] [Harder and Klunker 1956] [Hardy 1978] [Haroldsen 2000] [Harris 1965] [Harris and Bartlett 1972] [Hart and Schmitz 2022b] [Hart and Schmitz 2022a] [Hart et al. 2025] [Hassan et al. 2010] [Hebbar et al. 1993] [Heineck et al. 2016] [Heiser and Burkhalter 2002] [Heller 1955] [Hemsch 1985] [Hemsch and Nielsen 1986] [Henderson 1974] [Henning 1954] [Henning 1957] [Herrmann 2008] [Herrmann and Orlowski 1997] [Hicks] [Hildebrand 1979] [Himpler 1975] [Hinchliffe and Qin 2016] [Hinchliffe and Qin 2017] [Hintz and Saltzman 1967] [History of Supersonic Transport 2020] [Hoffman 1953] [Hoffman 1954] [Hoffman 1956] [Hoffman et al. 1955] [Hong 1965] [Honkanen et al. 2011] [Hood et al. 1980] [Horton and Landrum 2006] [Howard 1984] [Howard and O’Leary 1993] [Howell and Korst 1971] [Hsieh and Wardlaw 1994] [Huang et al. 2022] [Hubbartt and Strahle 1981] [Hue and Molton 2020] [Huerta 1969] [Huffman 1975] [Huffman and Fox 1978] [Huffman and Fox 1979] [Huffman and Fox 1985] [Hughson et al. 2006] [Hui et al. 2019] [Hummel et al. 1980] [Jenkins and Meyer 1975] [Kehrer 1971] [Kishi et al. 2023] [Komarov and Zinchenko 2023] [Lamb et al. 1981] [Lee 1964b] [Lowell 1953] [Martin and Walkley 1980] [McDevitt and Rakich 1966] [McMillin and Wood 1986] [Moua et al. 2012] [Murphy and Piddington 1960] [Owens et al. 2002] [Palchekovskaya 2019] [Petersen 1960] [Shrout and Fournier 1979] [Siewert and Stewart 1965] [Spearman 1989] [Spearman et al. 1955] [Theoretical Studies to Refine 1970] [II. Modern Cruise Missile 1987] [Ingram et al. 1986] [Iyer 1995] [Jackson 1955] [James 1998] [Jameson et al. 2005] [Jankiewicz 2026] [Janus et al. 1990] [Grauer] [Jategaonkar et al. 2004] [Jegarkandi Mohsen et al. 2009] [Jenn and Nelson 1988] [Jenn and Nelson 1989] [Jesudasan et al. 2026] [Jettmar 1984] [Ji et al. 2011] [Ji et al. 2012] [Johnson et al. 2001] [Johnston 1956] [Jones 1991] [Jones 1992a] [Jones and Nicholson 1991] [Jordan 1972] [Joshi 1996] [Joshi et al. 2024] [Jumper 1983] [Jung 2003] [Kaneko et al. 2024] [Keenan and Kuhlman 1991] [Kelly 1980] [Kelly and Osborne 1954] [Keuper 1960] [Khan et al. 2019] [Khan et al. 2025] [Khlebnikov 1990] [Kim and Kang 2025] [Kirsch et al. 2025] [Kishi et al. 2017] [Klausmeyer 2004] [Klein and Murphy 1999] [Klopfer 1985] [Knill et al. 1998] [Korst and Deep 1979] [Kostic et al. 2002] [Kraiko and Pudovikov 1998] [Kreeger and Landrum 2003] [Kremeyer 2004] [Kretzschmar et al. 1995] [Krieger 1979] [Krieger 1980] [Krieger 1982] [Krieger and Williams 1981] [Kulfan 1978] [Kulfan 2002] [Kulfan 2008] [Kulfan 2009] [Kumar and Ghosh 2018] [Kumar and Ghosh 2023] [Kumar et al. 2025] [Kuroda and Imado 1988] [Kuroda et al. 1993] [Kusunose et al. 1999] [Kutluay et al. 2009] [Kwak et al. 2013a] [KÜChemann 1962] [Lacerda Montes et al. 2025] [Lacey 1979] [Ladyzhenskij 1963] [Lagerstrom and Graham 1951] [Lam 2005] [Lance 1954] [Landers and Auman 2001] [Landers et al. 1997] [Landers et al. 2000] [Landers et al. 2003] [Langley and Demetrick 1978] [Lantagne et al] [Latif et al. 2007] [Сергеевна et al. 2024] [Lawrence 1953] [Lawrence 1991] [Lee and Kim 2006] [Lees 1959] [Lei et al. 2016] [Lensi 2000] [Lesieutre et al. 1996] [Levin 1997] [Levy 1959] [Levy and Dickey 1955] [Levy and Dickey 1956] [Li 2015] [Li and Shi 2010] [Li et al. 1995] [Li et al. 1999] [Li et al. 2022e] [Li et al. 2023k] [Li et al. 2026c] [Liang 1978] [Liang and Fu 1991] [Lijewski 1987] [Lin 1982a] [Lin 1982b] [Litvinenko and Matthies 2012] [Liu 2022] [Liu et al. 2008] [Liu et al. 2025l] [Liu et al. 2026k] [Lock 1957] [Lock 1963] [Lock and Bridgewater 1967] [Locke 1981] [Loftin 1973] [Lofts 2015] [Lombardi 1995] [Long 1950] [Longo and Das 1990] [Lopez] [Lorenz et al. 1990] [Lovell 1999] [Lovell 2001] [Lowry 2013] [Lyu et al. 2020] [MacKenzie and Zimmerman 1992] [Mahajan et al. 1992] [Makowski 1964] [Malfa et al. 1991] [Malmuth et al. 1986] [Malmuth et al. 1987] [Mani et al. 2010] [Mann and Mercer 1986] [Manning and Kroo 1999] [Markhotok 2021] [Maruyama et al. 2006] [Maruyama et al. 2009] [Mascitti 1977] [Mason 1953] [Mason 1982] [Mason 1991] [Mason and Gardner 1952] [Mason and Lee 1990] [Masson et al. 1999] [Masud et al. 2017] [Masud et al. 2018] [Mathijssen et al. 2009] [Matt et al. 2025] [Matthews et al. 2025] [Mattson and Osborne 1955] [McDaniel et al. 2010] [McDonald and Mavris 2000] [McFall 1954] [McFall and Hollinger 1953] [McGeer and Kroo 1983] [McGrath 2004] [Mele et al. 2017] [Mendenhall 1992] [Mertens et al. 1986] [Mertens et al. 1987] [Bashkirov 2024] [Meyer 1957] [Middleton and Lundry 1975] [Middleton and Lundry 1976] [Middleton and Lundry 1980a] [Middleton and Lundry 1980b] [Middleton et al. 1975] [Middleton et al. 1980] [Middleton et al. 1982] [Miedziński et al. 2023] [Mikhail 1989] [Miles 1953] [Miles 1954] [Miles and Limbach 2015] [Milgram and Bjorklund 1980] [Milholen and Owens 2005] [Miller 1994] [Minervino and Tognaccini 2023] [Missile Guidance Software 2007] [Mitchell and Peck 1950a] [Mitchell and Peck 1955] [Mizobata et al. 2024] [Mohamed and Dongare 2021] [Moore 1974] [Moore et al. 1993] [Moran and Beran 1995] [Morelli 2000b] [Morelli and Klein 1995] [Morito and Rowe 1972] [Mosbarger and King 1995] [Motyka et al. 1978] [Mouch et al. 1989] [Moul and Wineman 1952] [Mourousias et al. 2023] [Mousseau 2013] [Mousseau 2015] [Moyer 1963a] [Murman and Aftosmis 2003] [Murman and Cole 1974] [Murman et al. 2002] [Murphy and Schmidt 1953] [Myers 1992] [Nadim Melhem et al. 2024] [Nagamatsu et al. 1987] [Naohiko et al. 2016] [Naughton 1999] [Naughton 2002] [Neely et al. 2003] [Nelson 1988a] [Nelson and Bossi 1995] [Nelson and Passera 1950] [Nelson and Welsh 1960] [Neoclassical Missile Guidance 2016] [Newcomb 1991] [Nghiem and Norstrud 1989] [Nichols 1977] [Nicolaides and Brady 1959] [Nielsen 1978] [Nielsen 1979] [Nielsen 1982] [Nielsen 1985] [Nielsen 1986] [Nielsen 1988] [Nietubicz 1975] [Nietubicz and Sturek 1988] [Nietubicz et al. 1984] [Niewald and Moul 1950] [Nikfetrat et al. 1992] [Nikolic and Jumper 2004] [Nixon 2003] [Nosek 1982] [Numerical and Experimental Determination 2019] [Numerical Study on Rolling 2014] [Nygaard and Meakin 2002] [O’Brien and Takahashi 2023] [O’Connor 1975] [Ogawa and Babinsky 2005] [Oh 1989] [Ohira and Kwak 2014] [Orme and Gilyard 1993] [Ormsby and Long 1980] [Osipov 2019] [Ostowari and Naik 1986] [Ozcatalbas et al. 2020] [Page 1956b] [Palmer et al. 1956] [Panayotov et al. 2017] [Pankkonen 2011] [Panneerselvam et al. 1996] [Papoutsis-Kiachagias et al. 2021] [Parise 1992] [Parks 1954] [Patel et al. 2003] [Paulson and Thomas 1978] [Paulson et al. 1979] [Pearson 1992] [Pearson 1995] [Pepitone and Jacobson 1977] [Peterson 1961] [Peterson and Menees 1961] [Pfaff 1965] [Pfaff 1968] [Pfeiffer 1988a] [Pfeiffer 1988b] [Pfenneberger 1966] [Pfifer et al. 2009] [Pfyl 1952] [Phillips et al. 1983a] [Pipko 1966] [Pittman et al. 1984] [Platzer 2010] [Politis and Kind 1986] [Pollin 1973] [Pope and Street 1959] [Popytalov and Samsonov 1978] [Porter 1965] [Pourtakdoust and Lan 1990] [Powers 1988] [Prakash et al. 2009] [Prescott 1963] [Price 1978] [Price 1981] [Pritchard 1969] [Properties and Design 2012] [Puchalski and Kowalick 1976] [Puckett 1946] [Qin 2012] [Qin et al. 2017] [Raab 2014] [Radkey et al. 1976] [Radkey et al. 1978] [Rahma and AlQadi 2025] [Raisinghani and Kumar 1995] [Ramm 1990] [Ratnayake et al. 2011] [Razgonyaev and Mason 1995] [Reda 1977] [Reich et al. 1976] [Reichert 1947] [Rein et al. 2009] [Reuther 2002] [Reuther et al. 1996] [Reuther et al. 1999] [Walkley and Martin 1979] [Whitcomb 1956b] [Ritland 1989] [Rivers and Wahls 2003] [Roache 1973] [Robinson 1958] [Rodi 2018] [Rodi et al. 2019] [Rodriguez 1999] [Rodriguez 2007] [Roger et al. 2011] [Rogers 2004] [Rom et al. 1989] [Rose et al. 1988] [Rosema 2015] [Rosenhead 1956] [Rothacker 2017] [Rott 1953] [Ruffin et al. 1997] [Ruffin et al. 2000] [Russell 1958] [Russo et al. 2020] [Sachs 1977] [Saetta et al. 2023] [Sagan 1991] [Sahu 1985] [Sahu 1986a] [Sahu 1986b] [Sahu 2007] [Sahu 2011] [Sahu and Fresconi 2017] [Sahu and Fresconi 2018] [Sahu and Heavey 2009] [Sahu and Heavey 2010] [Saint-Mard and Hendrick 1999] [Sajjad et al. 2021] [Sakai 2009] [Sammonds 1970] [Sarfaraz 2015] [Sarkar and Panneerselvam 1998] [Sarkar et al. 2009] [Sasaki and Obayashi 2003] [Sasoh et al. 2009] [Satran 1986] [Sawyer et al. 1981] [Schaefer et al. 2019] [Schermerhorn 1969] [Schetz et al. 1980] [Schnell 2023] [Schnepf et al. 2017] [Schnerr and Dohrmann 1991] [Schnerr and Dohrmann 1994] [Schouten and Bakker 2000] [Schuelein 2008] [Schülein 2009] [Seaberg 1954] [Seaberg 1957] [Seacord and Campbell 1945] [Sears 1947] [Seider and Haenel 1991] [Selberg and Rokhsaz 1985] [Selected Cruise Missile Programs 2008] [Seraj and Martins 2023] [Seraj et al. 2025] [Serdarevic-Kadic and Terzic 2019] [Sethi 2024] [Shachar et al. 2025] [Shaferman and Shima 2010] [Shah and Ahmed 2023] [Shanks and Ahmad 1991] [Shantz 1953] [Shapin 1991] [Shefer 1990] [Sheldrick 1967] [Sheng et al. 2008] [Sher et al. 2022] [Shirokov et al. 2024] [Shistik and Sigal 2002] [Shmyglevskii 1958] [Shortal 1952] [Shortal 1953] [Sigal 1999] [Sigal 2000] [Sigal and Ben-Asher 2010] [Sigal et al. 1997] [Silva et al. 2015] [Sirbaugh 1983] [Sisk and Andrews 1963] [Sivakumaran et al. 1998] [Skarman 1978] [Sklar and Rusak 2020] [Slapnicar] [Sleeman 1957] [Smeltzer et al. 1983] [Smith 1997] [Smith et al. 1993] [Smith et al. 2002] [Sobieczky 1991] [Sonawane and Mahulikar 2013] [Sotomayer and Weeks 1978] [Spearman 1961] [Spearman 1979a] [Spearman 1979b] [Spearman 1983] [Spearman 1986] [Spearman and Collins 1972] [Spearman and Robinson 1958] [Spearman et al. 1977] [Spencer 1961] [Springer 1996] [Squire and Nasser 1993] [Srivastava 1998] [Stallard 1979] [Stallings 1982] [Stark 1989] [Starr and Varner 1976] [Stengel 1969] [Steppert and Epple 2017] [Sternberg 1952] [Stevens 1955] [Stevenson 1991] [Stieglitz et al. 1979] [Stoldt et al. 2020] [Stoldt et al. 2021] [Strategic Force Planning during 2019] [Strategic Missiles] [Suga and Yamazaki 2015] [Sun and Hansen 1982] [Sun et al. 1984] [Sun et al. 2020a] [Sun et al. 2025a] [Supersonic and Hypersonic Flight 1960] [Morlang 2019] [Supersonic Cruise 1981] [SUPERSONIC FLIGHT 2014] [Supersonic Flight 2025] [Supersonic Flows over Wings 2021] [Supersonic Flows over Wings 2025] [Swamy et al. 1978] [Szklarski and Głębocki 2025] [Zarchan 2019] [Tahani et al. 2017] [Takahashi et al. 2005] [Takanashi et al. 1998] [Takovitskii 2020] [Takovitskii 2023] [Tatum 1949] [Taur 2002] [Taylor and Pamadi 1983] [Taylor et al. 2010] [Technical Applications 1976] [The Air Force Strategic 2002] [The Effects of Canard-Wing 1988] [Theoretical Modeling 1976] [Thibert and Arnal 2000] [Thorp and Downey 1992] [Ting et al. 2025] [Tkalenko 1969] [Tokugawa and Yoshida 2006] [Transonic Aircraft Configurations 2012] [Transonic and Supersonic Flight 1992] [Traoré and Lemée 2001] [Traub 2001] [Trifu and Savu 1993] [Trimpi 1980] [Tsien 1955] [Tu 1991] [Tu 1992b] [Tu 1996] [Tu and VanDalsem 1996] [Tu et al. 1993] [Tuncer and Platzer 1996] [Turner 1965] [Tuzlukov 2026] [Ueno et al. 2004] [Underwood 1964] [Uselton 1976] [Vadillo and Agarwal 2007] [Vadillo and Agarwal 2009] [Vaiuso et al. 2025] [Van Der Vooren and Van Der Wees 1990] [van Dommelen et al. 2019] [VanderWyst 2008] [Vargas-Jimenez and Vos 2016] [Vaughn 2002] [Vaughn 2006] [Vavdiya and Kaushik 2022] [Veletas 2026] [Veresnikov and Goncharenko 2025] [Vergez 1981] [Verhoff et al. 1990] [Viswanath 1988] [Vitale 1953] [Vogel and Schmitz 2025] [Vortical Flow Topology 2009] [Waddell 1961] [Waddington] [Walkley 1986] [Wallskog 1954b] [Wallskog 1954a] [Walters 1954] [Walters 1959] [Wanchai] [Wang 2019c] [Wang and Liu 2013] [Wang et al. 2002] [Wang et al. 2021g] [Wang et al. 2022i] [Wang et al. 2022b] [Washburn and Gloss 1978] [Washington and Spring 1982] [Wasilczuk et al. 2024] [Watkinson et al. 1986] [Webber and Houghton 1963] [Weber 1967] [Wegener 1991] [Wegener 1997] [Wei et al. 2024] [Weinacht 2014] [Welge et al. 1976] [Wells 1953] [Wells et al. 1981] [Wells et al. 1982] [Werrell 1985b] [Werrell 1989] [West and Phillips 2018] [Westerwelt 2024] [Whitcomb 1953] [Whitcomb 1955] [Whitcomb 1956a] [Whitcomb 1957] [Whitcomb and Sevier 1960] [White 1993] [White 1995] [White Sands Missile Range Nm 1997] [Whiting and Jobe 1972] [Wignall and Houlden 2020] [Wilcox et al. 2004] [Willier et al. 2024] [Wiltse 1955] [Wimpress and Swihart 1964] [Windhorst and Ardema 2000] [Wise 1953] [Wood and Miller 1984] [Woodruff 2009] [Woodward 1961] [Wortman 1984] [Xiong et al. 2018b] [Xu 2023] [Xu et al. 2024] [Yamazaki et al. 2019] [Yan et al. 2008] [Yang et al. 2009b] [Yanushevsky 2007a] [Yanushevsky 2007b] [Yanushevsky 2018e] [Yanushevsky 2018c] [Yanushevsky 2018d] [Yanushevsky 2018b] [Yanushevsky 2018a] [Yao and Hussain 2019] [Yates and Zeydel 1963] [Yavuztürk et al. 2017] [Yeh and Clark 2007] [Yi and Wanchun 2014] [Yip 1985] [Yip and Coy 1982] [Yip et al. 1980] [Yoo and Bullock 1989] [Yoshida 2009] [Yoshimoto and Uchiyama 2003] [Yu et al. 1983] [Zarchan 2012] [Zhang and Yuan 2019] [Zhang et al. 1990] [Zhang et al. 2018a] [Zhang et al. 2021a] [Zhang et al. 2025f] [Zhang et al. 2026j] [Zhao et al. 2019a] [Zhaoqing and Hailong 2016] [Zheng et al. 2012b] [Zheng et al. 2026b] [Zhu and Qin 2021] [Zhuo et al. 2024] [Zhuolun et al. 2014] [Zingg et al. 2006] [Zuccolo et al. 2020] [Zurriati et al. 2011] [Çetiner et al. 2016] [ŞUmnu and GÜZelbey 2023]

Turbojets, ramjets and propulsion for supersonic flight

The engines the testbed flew and the engine the weapon needed. Turbojets for supersonic flight and their afterburners, ramjets, scramjets and combined cycles. 233 titles name a ramjet, the Navaho’s cruise engine that the X-10 never carried.

540 records. [3D Problems of Rotating 2018] [6ttl and Willinger 2021] [Jain 2025] [Abbas and Riggins 2016] [Abdulhamitbilal et al. 2022] [Adami and Zhu 2007] [Adami and Zhu 2008] [Aggarwal and Moore 1996] [Aggarwal and Moore 1998] [Air Force Research Lab Edwards AFB CA 2000] [Aksoy 2025] [Aksoy and Son 2026] [Al-Amari et al. 2022] [Alexandrov et al. 2001] [Alford and Auyer 1954] [Andreadis et al. 2002] [Angelucci et al. 1979] [Aoyagi and Tolhurst 1964] [Armstrong and Miller 1968] [Ashry et al. 2019] [Atay and Kumartaslioglu 2024] [Auman 1993] [Ayaz and Altuntaş 2017] [Aygun 2022] [Bondre 2026] [Boppart and US Atomic Energy Commission (AEC) 1957] [Choi et al. 2022] [Clements 1972] [Coe 1976] [Coe et al. 1976] [Evans et al. 2023] [Ezrokhi et al. 2020] [Hiller and Drain 1976] [Hu et al. 2023b] [Ighodaro et al. 2022] [Jones and Huber 1978] [Kim and Frate 2001] [Korsun et al. 2024] [Pratt and Whitney Aircraft, East Hartford, CT (United States) et al. 1960] [Lee and Bae 2023] [Lee et al. 2024b] [Li et al. 2020a] [Li et al. 2023b] [Madhumitha and Karmakar 2024] [Malinovsky et al. 2021] [McClinton et al. 1991] [Merkle 1959] [Migadel et al. 2026] [Morris et al. 1980] [Nguyen et al. 2023b] [Picard and Whitley 2002] [Ratekin et al. 2001] [Rowe et al. 1981] [Shehabaz et al. 2026] [Stechkin 1967] [Babu 2021b] [Babu 2021a] [Baerst and Hughes 1978] [Balepin et al. 2001b] [Balepin et al. 2001a] [Barnhart 1989] [Ben-Arosh et al. 1997] [Bendot et al. 1975] [Benyo 2010b] [Benyo 2010c] [Benyo 2010a] [Benyo 2011] [Berezovsky 2018] [Berglund et al. 2010] [Berry and Gilyard 1973] [Besserer 1952] [Bezborodova and Filinov 2021] [Billig 1993] [Billig 1995] [Billig and Grenleski 1968] [Bogomolov and Malinin 2017] [Bolender and Doman 2005] [Boles and Milligan 2013] [Bond and Edwards 2003] [Bond and Edwards 2004] [Bonner et al. 1974] [Boxer 1979] [Brazzel 1963] [Bresnahan 1968] [Bresnahan and Johns 1968] [Briggs 1986] [Briones and Rankin 2024] [Brock and Franke 2004] [Brodzik 2024a] [Brodzik 2024b] [Brown et al. 1978] [Brummund and Scheel 2002] [Burkardt and Franciscus 1990] [Cai et al. 2010] [Cake 1965] [Calder and Gupta 1978] [Callinan and Hikiss] [Carlson 1983] [Carter 2012] [Carter and Springfield 2002] [Cervantes et al. 2024] [Cesaro and Walker 1955] [Chang and Hunter 1996b] [Chang and Hunter 1996a] [Chao et al. 1986] [Chapman 1955] [Chichka et al. 1987] [Chichka et al. 1988] [Child and Henderson 1978] [Choi and Yang 2014] [Clayton 2001] [Clemow 1957] [Climbing Flights of Turbojet 1995] [Cohen et al. 1997] [Cohen-Zur and Natan 1998] [Component Analysis and Synthesis 1976] [Connolly and Kopasakis 2010] [Coulibaly et al. 2026] [Creese et al. 2023] [Cruise Missile Engines 1982] [Cruising Flights of Turbojet 1995] [Cruz et al. 2024] [Cruzen 1983] [Culick 1984] [Culick et al. 1982] [Culick et al. 1983] [Culick et al. 1985] [Curran and Craig 1973] [Curry and Crabill 1961] [Cutright and Braasch] [DaMing et al. 2009] [De VAULT 1957] [De-You 1985] [Deep et al. 1971] [Demichele et al. 1965] [Derbel and Beneda 2025] [Dessornes and Scherrer 2005] [Dessornes et al. 2001] [Destarac and van der Vooren 2004] [Dewell et al. 1997] [Dickeson et al. 2009] [Disher et al. 1953] [Dobrowolski 1966] [Douglass 1963] [Drummond 1983] [Du et al. 2019b] [Due 1987] [Dugan 1973] [Duggleby et al. 2025] [Dunbar et al. 1956] [Duncan 1965] [Duncan 1966] [Duncan 1991] [Dunn 1980] [Dunsworth and Reed 1978] [Dunsworth and Reed 1979] [Dutt 1980] [Eastman and Wenndt 1988] [Eklund 2004] [El-Sayed 2026] [Elrod and Durniak 1981] [Emmons et al. 1977] [Englert et al. 1954] [English and Cavicchi 1954] [Eriksson 1984] [Experimental Investigation of Cermet 1958] [Farrar 1968] [Feifel and Kerkam 1992] [Fernandes Pereira de Lima and Souto 2021] [Fetahi et al. 2020] [Filinov and Bezborodova 2021] [Fleming 1953] [Fleming et al. 1956] [Flight Engine Performance Evaluation 1977] [Fontan Moura] [Franciscus 1981b] [Franciscus 1981a] [Franciscus 1983] [Franciscus and Lezberg 1963c] [Franciscus and Lezberg 1963b] [Franciscus and Lezberg 1963a] [Franciscus and Maldonado 1989] [Fujita et al. 2006] [Gabriel et al. 1953] [Gardner 1955] [Gardner et al. 2004] [Gibart et al. 2024] [Goss and Cook 1948] [Gravelle] [Gu et al. 1998] [Harris 1969] [Harris et al. 2004b] [Harris et al. 2004c] [Harris et al. 2004a] [Heat Recovery from Reciprocating 2021] [Hepler et al. 1979] [Herling et al. 1985] [Herrmann and Rick 1991] [Herzog et al. 1998] [Heterogeneous Engineering 1994] [Himmel 1952] [Hirsch and del Re 2009] [Hojnacki 1972] [Hornbeck 1975] [Hosters et al. 2013] [Howlett 1976] [Howlett and Kozlowski 1975] [Howlett et al. 1976] [Hoy 1989] [Hsieh et al. 1997] [Hua et al. 2023] [Huebner and Tatum 1991] [Huffman and Fox 1977] [Hui Qin et al. 2010] [Hunt et al. 1978] [Hunt et al. 1982] [Huo et al. 2006] [Hurley 1951b] [Hurley 1951a] [Hurrell 1957] [Hussein et al. 2026] [Hyde et al. 2000] [Hypersonic Ramjet Engine 2004] [Merkulov 1976] [Ikawa 1989] [Ikawa 1991] [Ivanov 2022] [Jackson and Wang 1974] [Jackson et al. 1977] [Jacob et al. 2014] [Jafari and Nikolaidis 2018] [Jarmark 1986] [Jeronymo and Stark 2017] [Jiali and Jihong 2015] [Jin et al. 2023a] [Jin et al. 2024] [Jing 2006] [Jing et al. 2007] [Jing et al. 2016b] [Jo et al. 2024] [Jo et al. 2025] [Johnson-Groh 2018] [Johnston and Hunt 1984] [Judd and Falanga 1956] [Kaemming 2001] [Kaemming 2002] [Kailasanath et al. 1986] [Katolicky et al. 2014] [Kaznevskiy 1967] [Kaçar et al. 2018] [Kepler and Champagne 1989] [Kerslake 1958] [Keshmiri et al. 2006] [Kim 2005] [Kim 2006] [Kim et al. 2023a] [Klein and Abeykoon 2015] [Klock and Cesnik 2014] [Kniskern 1990] [Knoblach 1974] [Kobayashi et al. 2008] [Komar and Christenson 1996] [Konno et al. 1998] [Kostyushin et al. 2017] [Koubek 1963] [Kraiko 2023] [Krebs 1976] [Krebs and Wilcox 1954] [Kuhn et al. 2026] [Kuipers et al. 2007] [Kumar and Yadav 2022] [Kumm and Bitondo 1953] [Kuroda 1993] [Kwak et al. 2010] [Kwak et al. 2012] [Ladeinde 2022] [Lamb 1999] [Lamb and Marx 1999] [Lancelle et al. 2012] [Landau and Yeneriz 1965] [Pratt and Whitney Aircraft (United States) et al. 1958] [Larson 1959a] [Larson 1959b] [Pratt and Whitney Aircraft (United States) et al. 1960d] [Pratt and Whitney Aircraft (United States) et al. 1960c] [Pratt and Whitney Aircraft (United States) et al. 1960b] [Pratt and Whitney Aircraft (United States) et al. 1960e] [Pratt and Whitney Aircraft (United States) et al. 1960a] [Laube and Piechna 2019] [Lauziere and Kump 1958] [Leavitt 1979] [Leavitt et al. 1978] [Lentsch et al. 2001] [Lesieutre 2017] [Levin et al. 2008] [Li et al. 2026h] [Lima Bezerra and Shynkarenko 2021] [Lin and Lee 1996] [Liquid-fueled ramjet engine 1997] [Liu and Sirignano 2000] [Liu et al. 2017e] [Longwell and Weiss 1952] [Lou and Zhang 2009] [Ludwig 1979] [Luo et al. 2003] [Lv et al. 2026] [Mahato et al. 2023] [Makaron and Fedyayev 1996] [Malek 1992] [Mark et al. 1954] [Marlow 2003] [Marsh and Sears 1954] [Martin 1977] [Mazaheri et al. 1999] [McTaggart 1973] [Meher-Hornji 1997] [Meisl 1986] [Meisl 1988] [Menon 1992] [Merkulov 1967] [Meyer 1947] [Mikhail 1979] [Minato 2016] [Minato 2019] [Minato and Tamura 2025] [Minato et al. 2005] [Minato et al. 2006] [Minato et al. 2007] [Minato et al. 2013] [Miyajima et al. 1992] [Mock 1951] [Modularized Instrument System 1974] [Moore 1993] [Morris and Brewer 1979] [Morris et al. 1989] [Morrison 1980] [Moulden et al. 1974] [Mulac et al. 1989] [Mustafa et al. 2025] [Mutz et al. 1964] [Myrabo et al. 1986] [NACA Conference 1951] [Naca Conference on Turbojet 1953] [Nakagawa and Ezawa 2014] [Nam et al. 2022] [Nechiporuk and Zaripov 2022] [Neill and Pesyridis 2017] [Neiner et al. 1978] [New Applications of Engineering 1994] [Nikitaev 2019] [Niknamian 2018] [Niknamian 2019] [Northam and Anderson 1986] [Okelah 1985] [Oktaviana et al. 2026] [Optimization of Cruising Flights 1995] [Orlando 1994] [Otsap and Yankura 1967] [Ou et al. 2017] [Ouarti et al. 2003] [Pagan et al. 2001] [Palmer 1956] [Pampreen 1986] [Paris et al. 1980] [Paull et al. 1995] [Peery and Parsley 1996] [Perkins et al. 1971] [Peters 1985] [Piccirillo 1998] [Pismennyi] [Powell and Glickstein 1988] [Preparation of Turbojet Engine 2002] [Priyamvada et al. 2015] [Quigg and Stewart 1963] [Rae 1961] [Rajagopalan and Siddiqi 1985] [Ramanujachari 2022] [RAMJET Engine Controller Design 2025] [Ramjet Supersonic “Flight Tests” 1958] [Rancourt et al. 2014] [Reed 1956] [Reilly and Welna 1955] [Requirements of a Commercial 1967] [Reynolds 1977] [Rideau et al. 2008] [Riebe et al. 1981] [Riley and Dejarnette 1992] [Robinson et al. 1974] [Rodgers 1986] [Rosen 2001] [Rosenberg and Schuch 1983] [Rosevear 1992] [Roundy 1979] [Rowiński 2016] [Runckel 1958] [Sabatella 1974] [Sacher and Zellner 1995] [Sachs et al. 1996] [Sahu and Fresconi 2019] [Saito et al. 2005] [Samuelsson 1999] [Sarathkumar Sebastin et al. 2021] [Sargent and Bielawski 1970] [Sato et al. 2006] [Sato et al. 2007] [Savino and Pezzella 2003] [Sawai et al. 2009] [Sayles 2008] [Schindel 1999] [Scott 1963] [Tacina et al. 2022] [Tanno and Tanno 2021] [Thillai et al. 2021] [Thomas et al. 1997] [Seal for a Turbojet 2013] [Sealing Device 2020] [Sebastin and Vignesh N 2026] [Seiple 1960] [Sekar et al. 2021] [Shaffer 1989] [Sharp 1957] [Shaw 1984] [Shillito et al. 1956] [Siebenhaar and Bogar 2006] [Silverstein 1986] [Singelmann and Mueller 1948] [Singh and Benstein 1986] [Skibina and Faraponov 2021] [Slocumb and Andrews 1961] [Smirnov et al. 2019] [Sridharan and Rodriguez 2013] [Stanley et al. 2000] [Starkey and Lewis 1999] [Starkey et al. 2006] [Startup Tests Ramjet Engine 2023] [Steer 2000] [Steinmetz and Hines 1987] [Stewart 1958] [Stewart 1986] [Stewart and Kemmerly 1987] [Straight and Harrington 1973] [Strauss et al. 2025] [Strauss et al. 2026] [Streiff 1953] [Stricker 1989] [Suchocki et al. 2015] [Suetin and Kartsev 1993] [Sun et al. 2019a] [Sung and Yang 2014a] [Sung and Yang 2014b] [Sung et al. 2001b] [Sung et al. 2001a] [Sung et al. 2026] [Sushma et al. 2025] [Syarafina et al. 2020] [Sykes] [Szeliga and Allan 1974] [Taguchi et al. 2005] [Taguchi et al. 2009] [Taguchi et al. 2012] [Takahashi et al. 1997] [Tanck and Steadman 1998] [Tangirala et al. 2007] [Taylor 1968a] [Thangadurai et al. 2008] [Thomas et al. 1977] [Tomioka et al. 2007] [Tomioka et al. 2012] [Topal et al. 2015] [Tournes and Johnson 1998a] [Trazzi 2004] [Trefny and Benson 1995] [Trefny and Dippold 2010] [Trotsyuk 2021] [Tudosie 2024] [Tuling et al. 2013] [Tunik 2020a] [Tunik 2020b] [Tunik and Mayorov 2022b] [Turbojet and Turbofan Engines 1964] [Turbojet Engines 2022] [Turning Flights of Turbojet 1995] [Unterberg 1957] [Van den Borre et al. 2023] [van den Hout and Koullen 1996] [Vdoviak and Ebacher 1980] [Veeran et al. 2018] [Waidmann et al. 2024] [Walker 1949] [Walker 1952] [Walker 1973] [Waltrup et al. 1980] [Waltrup et al. 1981] [Wang et al. 2021l] [Wang et al. 2022p] [Wang et al. 2022o] [wang et al 2022] [Wang et al. 2024a] [Ward and Neeley 1959] [Warner 1951] [Wattenbarger and Rouser 2025] [Weber 1959] [Weeratunga and Menon 1993] [Weidner 1980] [Weintraub 1962] [Wenbiao et al. 2014] [White and Strykowski] [White et al. 2025] [Whitlow 1975] [Whitney 1963] [Wilbur et al. 1982] [Williams 1965] [Wolf et al. 1951] [Woll 1948] [Wood 1947] [Wu and Wei 2023] [Wu et al. 2020a] [Wu et al. 2026a] [Xi et al. 2021] [Xian Lin Huang and Dong Ming Ge 2010] [Xiaonan Chen et al. 2011] [Xingjian et al. 1985] [Xu et al. 2023b] [Xue et al. 2018] [Yan Binbin et al. 2009] [Yao et al. 2022] [Yip and Paulson 1977] [Yuan et al. 2025b] [Zander] [Zarubin et al. 2017] [Zellner et al. 1992] [Zhang et al. 2020] [Zhang et al. 2024b] [Zhang et al. 2025g] [Zhang et al. 2025e] [Zhao et al. 2025b] [Ziraksaz 2002] [Zucro 1950] [Zumwalt and Suwanprasert,S 1983] [Zuo et al. 2025]

Stellar-inertial navigation, star trackers and celestial reference

The external observation that resets a growing error. Star trackers and star sensors, star identification and centroiding, stellar-inertial and astro-inertial integration, and the celestial navigation practice the automatic tracker mechanised. 87 titles name a satellite, a spacecraft or an orbit, which is where the automatic tracker went after the cruise missile. 22 titles name daytime or daylight star tracking, the demanding case the Navaho had to solve inside the atmosphere.

498 records. [Abreu 1993] [Adams et al. 1966] [Air Force Armament Lab Eglin AFB FL 1988] [Alharam et al. 2024] [Ali 2007] [Ali and Fang 2009] [Ali et al. 2006] [Alvelda et al. 1988] [Anderson et al. 1983] [Golubek 2024] [He and Wei 2024] [Huang and Ma 2021] [Liounis et al] [Aretskin-Hariton and Swank 2015] [Arunachalam 2025] [Avanesov et al. 2013] [Bae and Schutz 2002] [Bae et al. 2010] [Bank 1997] [Bardwell 1995] [Barry et al. 1993] [Battersby and Blewitt 1965] [Bayard 1996] [Bell et al. 2020] [Bennett 1979] [Benzo 2024] [Bessaad et al. 2021] [Bessaad et al. 2022] [Bessonov et al. 2018] [Bettolo 2008] [Bing et al. 2022] [Birnbaum and Salomon 1967] [Birnbaum and Salomon 1968] [Blanton 1980] [Blumhagen 1963] [Bolandi and Saberi 2011] [Bollner 1987] [Bona and Hutchinson 1965] [Borror 1995] [Bostock 1993] [Bovens 1994] [Bowers 1967] [Bowring and Ramsden 1981] [Boyarsky 1989] [Brady et al. 2007] [Bralove 1978] [Breadboard Stellar Tracker System 1981] [Brown and Moy] [Burton 1959] [Cai et al. 2011] [Campbell 1964] [Carmeli and Ben-Moshe 2023] [Carroll et al. 1966] [Casini et al. 2023] [Cassidy 1994] [Celestial Navigation 2025] [Celestial Navigation 2020] [Chasan and Bingul 2026] [Chelnokov 2018] [Chelnokov 2019a] [Chen 2024] [Chen and Jan 2019] [Chen and Shau-Shiun 2021] [Chen et al. 1970] [Chen et al. 2013] [Chen et al. 2026j] [Chen et al. 2026i] [Chen Zhang et al] [Chiang 2013] [Chilton and Zito 1969] [Chmielowski and Wynne 1992] [Christian and Crassidis 2021] [Clark and Furth] [Collins 1943] [Collins 1968] [Conroy 1964] [Costa Canas and Sousa 2026] [Cotter 1963] [Craft et al. 2020] [Crassidis 2002] [Creamer 1996] [Critchley-Marrows et al. 2022] [Cui et al. 2014] [D’Angelo and Linares 2011] [Dai et al. 2018] [Daniel et al. 1995] [Darling et al. 2016] [Daub 1979] [de Aquino 1951] [De Groot and Larsen 1965] [DeAntonio et al. 1993] [DeGROOT and Larsen 1966] [Delabie 2013] [Delabie 2015] [Delabie et al. 2015] [Dennison et al. 1993] [Denver et al. 2025] [Des Jardins 1969] [Deters and Gutshall 1984] [Deters et al. 1966] [Deval Samirbhai et al. 2018] [Diaz and Pierce 2016] [Dishman and Shigemoto 1965] [Dixon et al. 1968] [Doolin and Showman 1967] [Doolin et al. 1968] [Draper 1965] [Draper 1968] [Dual Reticle Star Tracker 1969] [Duncan 1980] [Dzamba and Enright 2013] [Eberhardt 1963] [Eisenhut et al. 1971] [Eisenman et al. 1997] [Cheriet 2024] [Emadzadeh and Speyer 2011] [Enright et al. 2015] [Erlank and Steyn 2014] [Farazian et al. 1996] [Feasibility Study of Scanning 1971] [Fei Xing et al] [Felikson et al. 2011] [Finkbeiner 2013] [Finney et al. 2023] [Fokin 2007] [Follé 1983] [Folta et al. 1999] [Fox et al. 2024] [Franklin 1954] [Freiesleben 1977] [Friest] [Fu et al. 2024b] [Gadeberg and White 1970] [Gao and Yang 2023] [Gates and McAloon 1976] [Geiss 1969] [Glavich 1987] [Mohamed 2013] [Gordon 1964] [Gorstein et al. 1970] [Goss 1969] [Goss 1972] [Gou et al. 2025a] [Gou et al. 2025b] [Grace et al. 2022] [Greene 1964] [Grosch et al. 1967] [Grunwald and Swenson 2015] [Guanghua 1991] [Guesmi and Moloney 2024] [Gunderson 1978] [Gutierrez et al. 2017] [Hailong et al. 2015] [Hammad et al. 2024] [Hancock et al. 1997] [Hariton and Swank 2015] [Hashmall 2003] [Hashmall et al. 2004] [Heatwole 2019] [Hepburn-Dickins] [Herrera 2010] [Herrick 1946] [Hertel and Lowen 1970] [Hetherington et al. 2013] [Hofmann-Wellenhof et al. 2003] [Hohenkerk et al. 2012] [Holbrook 2005] [Horsfall 1958] [Hou et al. 2025] [Hua-Ming et al. 2015] [Hutchin 2008] [Hutchison 1975] [Inagaki and de Oliveira Fialho 2019] [Ivanov et al. 2024] [Ivanov et al. 2026] [Izadmehr and Ghomi 2020] [Jayaraman et al. 2006] [Jensen et al. 1997] [Jerebets] [Jessell 1949] [Jianan et al. 2015] [Jiang et al. 2017b] [Jiang et al. 2018a] [Jin et al. 2010] [Johnson et al. 1989] [Jovanovic et al. 2014] [Joy et al. 2025] [Ju et al. 1999] [Ju et al. 2000] [Jun et al. 2015] [Kahraman and Soken 2023] [Kamel et al. 1988] [Kane et al. 1966] [Kang et al. 2011] [Kaplan 1996a] [Kasahara and Hasegawa 2025] [Kau and Steadman 1976] [Kazarian et al. 1973] [Kazemi and Enright 2019] [Kazemi et al. 2015] [Kenny et al. 2003] [Ketchum and Tolson 1993] [Khodabakhshian et al. 2020] [Khorev] [Kia et al. 1993] [Kim 2023b] [Kim et al. 2015a] [Kim et al. 2017] [King 1983] [Klestadt 1971] [Knobbe and Haas 1997] [Kollodge and Sand 1983] [Kollodge and Sand 1984] [Kollodge et al. 1981] [Kondrashkin et al. 2025] [Korger 1957] [Kucherov and Kurenkov 2017] [Kudva and Throckmorton 1993] [La Vaglia 1969] [Lai et al. 2014a] [Lai et al. 2014b] [Lai et al. 2016] [Lam et al. 2003] [Lamy Au Rousseau et al. 2005] [Lana 1974] [Lange et al. 1986] [Lebsock et al. 2000] [Lee 1969a] [Lee 1971] [Lee 2025] [Lee et al. 2005] [Leve 1974] [Levine et al. 1990] [Li et al. 2004] [Li et al. 2005] [Li et al. 2006] [Li et al. 2017e] [Li et al. 2026l] [Liebe 1995] [Liebe and Eisenman 1996] [Liebe et al] [Liebe et al. 2000] [Lim et al. 2024] [Lithin et al. 2013] [Little 1967] [Liu et al. 2001] [Liu et al. 2010a] [Liu et al. 2011b] [Liu et al. 2015] [Lo 1978] [Lo 1986] [Lowen and Maxwell 1965] [Lu and Yang 2018] [Lu et al. 2017b] [Lu et al. 2017a] [Lu et al. 2018c] [Lu et al. 2026] [Lutgring and Tchilian 2022] [Lutgring and Tchilian 2024] [Lušić et al. 2024] [Lv et al. 2021] [Ma et al. 2015] [Ma et al. 2016] [Ma et al. 2025a] [Magnani 1993] [Mahi 2025b] [Mahi 2025a] [Mahi and Karoui 2019] [Mahi et al. 2023] [Malay 2001] [Malkin 2013] [Mamich et al. 2024] [Mangold 1997] [Manoni and Sonneman 1966] [Marbel et al. 2016] [Marin and Bang 2018] [Marin and Bang 2020] [Marner 1959] [Masood-Ur-Rehman et al. 2008] [McBryde and Lightsey 2012] [McHenry et al. 2019] [Medaglia 2016] [Melamed et al. 2025] [Metha] [Michaels and Speed 2005] [Miklus et al. 1993] [Milder 1971] [Miller and Son 2001] [Mitchell 1970] [Moghtadaei Rad 2014] [Molander 1997] [Molander 1999] [Mollett 1956] [Moody 1972] [Moore 1967] [Mortari and Romoli] [Moskowitz 1973] [Mu et al. 2025] [Muruganandan et al. 2018] [Neumann et al. 2009] [Ni et al. 2019] [Ni et al. 2021] [Ni et al. 2022] [Nicholas 2009] [Ning et al. 2019] [Noack] [Noguchi et al. 1996] [Ogilvie 1977] [Ogletree et al. 1972b] [Ogletree et al. 1972a] [Oosthuizen 2006] [Opromolla et al. 2017] [Ortiz and Lee 2006] [Ouellette et al. 1974] [Padro et al. 2012] [Pal and Bhat 2009] [Pal and Bhat 2013] [Pan et al. 2025a] [Pantaleoni et al. 2010] [Parker 1956] [Paulsen and Maresi 2000] [Pedrotty et al. 2020] [Percival et al. 2008] [Perkins et al. 2012] [Pertica and White 2018] [Pertica et al. 2021] [Pham et al. 2012] [Pickering 1999] [Pierros 2018] [Poston 1975] [Precision Attitude Determination System 1973] [Precision Attitude Determination System 1974] [Precision Pointing Control System 1972] [Priest et al. 1995a] [Priest et al. 1995b] [Quan et al. 2015b] [Quang Lam et al] [Rad 2015] [Rad et al. 2014] [Rakoczy and West 1992] [Range and Southworth 1967] [Rao et al. 2004] [Real Time Spacecraft Attitude 1979] [Roháč et al. 2011] [Roshanian et al. 2015] [Ross 1994] [Rounds and Marmar 1983] [Rufino and Accardo 2003] [Salazar and de Carvalho 2014] [Salomon and Goss 1976] [Samirbhai et al. 2016] [Samson 2024] [Pedrotty] [Sang et al. 2024] [Sarrafian 1966] [Sarvi et al. 2020] [Schenkel 1974] [Schmidt 1979] [Schmidt 2005] [Schmidt 2017] [Schmidt et al. 2008] [Chief Engineer Star Sensors et al. 2023] [Schmidtbauer 1978] [Schuck 1966] [Scott 1964] [Heatwole] [Sease et al. 2013] [Seidelmann et al. 2007] [Seifert 1970] [Severance 1989] [Shaikh 2025] [Shalom et al. 1985] [Shufang Zhao et al. 2012] [Shufeldt 1961] [Shuster 2004] [Siemes et al. 2019] [Singh et al. 2004] [Singla et al. 2007] [Sirlin et al. 2000] [Smith 1974] [Smith et al. 1982] [Smith et al. 1983] [Somov et al. 2011] [Somov et al. 2012] [Stanton et al. 1984] [Star Catalogues and Photographic 2010] [Nah 2005] [Star-Camera Algorithms 2023] [Stebbins et al. 1998] [Stenberg 1964] [Sternberg et al. 2022] [Storer 1947] [Stuart 2009] [Stuchlik and Heatwole 2016] [Study of a Scanning 1968] [Sun 2023] [Sun et al. 2013] [Sun et al. 2019b] [Suthakar et al. 2026] [Swank et al. 2025] [Swaszek et al. 2019] [Swaszek et al. 2020] [Taff 1986] [Tanaka et al. 2025] [Tao et al. 2008] [Tao et al. 2009] [Teague and Chahl 2023] [Teague and Chahl 2024] [Thapar and Torres 2024] [Thein et al. 2008] [Thomas and Shroyer 1965] [Thompson 1951] [Thummala and Falco 2025] [Tola 2016] [Tong et al. 2014] [Truesdale et al. 2013a] [Truesdale et al. 2013b] [Tseng and Jan 2026] [Uhde-Lacovara 1986] [Ulman 1989] [Underwood and Thein 2013] [Unpublished Short-Method Astro-Navigational Tables 1994] [Van Allen 1981] [van Bezooijen 1989] [van Bezooijen 1990] [van Bezooijen 1992] [van Bezooijen 1993] [van Bezooijen 2003] [van der Ploeg 2026] [Vandenberghe 2024] [Vedder 1993] [Vulfovich and Fogilev 2010] [Wang and Chun 2006] [Wang and Deng 2013] [Wang and Geng 2014] [Wang and Zhou 2015] [Wang et al. 2012b] [Wang et al. 2015a] [Wang et al. 2017g] [Wang et al. 2017h] [Wang et al. 2017j] [Wang et al. 2019g] [Wang et al. 2020d] [Wang et al. 2020c] [Wang et al. 2022a] [Wang et al. 2024j] [Wang et al. 2024i] [Wang et al. 2026e] [Weiler 1972] [Wen et al. 2021] [White 1985] [White and Grant 1973] [White and Titus 1956] [Wi et al. 2023] [Williams 1966] [Winkler 2011] [Wolfenbarger and Bae 2016] [Woodworth 1992] [Wu et al. 2019a] [Wu et al. 2019b] [Xing et al. 2006] [Yan et al. 2016] [Yan et al. 2017b] [Yan et al. 2021] [Yang et al. 2022c] [Yang et al. 2024b] [Yang et al. 2026a] [Ye and Zhou 2015] [Yim et al. 2005] [Yin and Wang 2018] [Yoon et al. 2022] [Yunhai et al. 2012] [Zaccheo 1949] [Zahednamazi et al. 2021] [Zakharov et al. 2013] [Zang et al. 2026] [Zhan et al. 2021] [Zhang and Wang 2011d] [Zhang and Xing 2018] [Zhang et al. 2004] [Zhang et al. 2005] [Zhang et al. 2013b] [Zhang et al. 2014b] [Zhang et al. 2018e] [Zhang et al. 2021b] [Zhang et al. 2023a] [Zhang et al. 2026h] [Zhang et al. 2026b] [Zhang Ze and Duan Guangren 2008] [Zhiru and Jing 2013] [Zhong et al. 2026] [Zhou et al. 2012] [Zhu et al. 2016a] [Zhu et al. 2025a] [Zipoy 1986] [Zischka 2017] [Zuber et al. 2025] [Zuber et al. 2026]

Automatic landing, the approach and the flare

Landing without a pilot. Automatic landing and the flare, approach guidance, instrument and microwave landing systems, carrier landing and the approach and landing of reusable launch vehicles. 74 titles concern landing on a carrier and 52 the landing of a reusable launch vehicle, the two settings in which automatic landing is still an active research problem.

482 records. [Abu-Jbara et al. 2015] [Зеленков and Голик 2009] [Agarwalla 2025] [Aircraft Automatic Approach 1996] [Aircraft Landing Measurement System 1971] [Aircraft Landing Procedure 1998] [Akmeliawati and Mareels 2010] [Al Bakri] [AL-Bakri and Kluever 2017] [Alexandrov et al. 1980] [Ali et al. 2024] [Alijani and Osman 2021] [Altunkaya and Ozkol 2023] [Andert and Mejias 2015] [Andrews 1977] [Anggoro 2021] [Aoki and Ishigami 2022] [Apparatus for Rotating 1998] [Aprovitola et al. 2021] [Atmeh et al. 2011] [Automatic Landing 1964] [Automatic Landing 1969] [Філяшкін and Мельников 2012] [Hwang 2007] [Automatic Take-off and Landing 2011] [Balanis and Cheng 1975] [Bektash et al. 2020] [Belcastro and Ostroff 1984] [Benbassat 2005] [Benbassat and Abramson 2002] [Benbow 1971] [Bergeron et al. 1980] [Bian et al. 2018] [Bland and Kolenkiewicz 1958] [Bond and Rumsey 1957] [Bretschneider et al. 2021] [Broxmeyer et al. 1968] [Brukarczyk et al. 2021] [Bryant et al. 1998] [Burchett] [Burgan and Paddison 1974] [Burlion and de Plinval 2017] [Burlion et al. 2014] [Burton 1981] [Busnardo et al. 2011] [Caglayan and Lancraft 1982] [Campbell et al. 2007] [Cetin and Kutay 2016] [Chandra and Ghosh 2019] [Che] [Chekanov 2025] [Chen et al. 2025h] [Cheng and Lai 2025] [Cheng and Pfeffer 1962] [Chitrakaran et al. 2005] [Chu and Bryson 1987] [Clos-Cot et al. 2018] [Cockayne and Rusnak 1971] [Cockburn 1965] [Collyer et al. 1980] [Colwell 1966] [Coombes et al. 2017] [Coutard et al. 2011] [Crassidis and Mook 1991] [Crassidis and Mook 1992] [Crassidis et al. 1993] [Crawford 1975] [Cui et al. 2022] [Cui et al. 2023a] [Davidson et al. 1972] [Davis 1988a] [de Alvear Cárdenas and Looye 2021] [de Bonfim Gripp and Sampaio 2014] [de Bruin and Jones 2016] [de Oca and Flores 2020] [della Noce et al 2021] [Dermer] [Devanath and Beebi 2016] [Devesa et al. 2004] [Dieudonne et al. 1976] [Digges 1971] [Ding 2015] [Donahue 1997] [Dong et al. 2023] [Doniger 1967] [Douglas Aircraft Co Long Beach Ca 1963] [Durand and Teper 1964] [Dynnikov 2020] [Edwards and Foster 1973] [Edwards et al. 1975] [Extension of a Portable 1972] [Fallon et al. 1999] [Faulders et al. 1967] [Fearnside 1959] [Feather and Craven 1991] [Fehr et al. 1972] [Fenwick 1966] [Fenwick 1967] [Ferrier et al. 2015] [Fischer 1981] [Flying Controls and Automatic 1963] [Fortenbaugh 1972] [Foster 1972] [Foster and Neuman 1970] [Fu et al. 2014c] [Fujimori et al. 2000] [Fusion of Multi-Antenna Carrier 2012] [Gai and Curry 1975] [Gai and Curry 1977] [Gao et al. 2009] [Gao et al. 2024b] [Gao et al. 2025] [Garcia 2008] [Gardinier and Taylor 1999] [Gautam et al. 2014] [Georghiou et al. 1986] [Gevaert and Feinreich 1977] [Givens and Coopmans 2020] [Gladkov I. a. Application 2017] [Golovan and Kuznetsova 2025] [Gomez and la Cour-Harbo 2021] [Gonçalves et al. 2010] [Goto et al. 2001] [Gouskov 1972] [Guadagnini et al. 2023] [Guan et al. 2018b] [Guo et al. 2026d] [Guorong Zhao et al. 2006] [Ha 2010] [Ha and Ahn 2004] [Ha and Kim 2005] [Hailiang 2026] [Halyo 1977] [Halyo 1979] [Halyo 1984] [Halyo 1987] [Halyo and Hueschen 1981] [Hameed and Bindu 2019] [Hameed and Bindu 2022] [Han 1971] [Han et al. 2026e] [Harris 1961] [Hayes and Velde 1962] [Helliwell 1952] [Hervas et al. 2014b] [Hervas et al. 2014a] [Hess and Judd 1976] [Hiba et al. 2021] [Holley and Bryson 1975] [Hornbuckle 2015] [Hoy 1963] [Hueschen 1984] [Hueschen 1986] [Hunt 1974] [Igreja and Lemos 2022] [Ilango and Ramanathan 2020] [Iliev and Nachev 2022] [Ipas et al. 2022] [Ishijima et al. 1998] [Jung 2024] [Kordos et al. 2023] [Miller 1979] [Nadkarni 1981] [Pessanha Santos et al. 2023] [Ragsdale et al. 1974] [Sözer and Kumbasar 2023] [Tang 2013] [Tripathi et al. 2024] [Urnes et al. 1981] [Jami’in 2020] [Jantawong and Deelertpaiboon 2018] [Jayaraman et al. 2022] [Jian et al. 2012] [Jiang and Ordonez 2008] [Jiang and Ordóñez 2009] [Jiang et al. 2018b] [Jih-Gau Juang and Hao-Hsiang Chang] [Jih-Gau Juang et al] [Johnson and Ivanov 2011] [Johnson et al. 2007] [Jones 1992b] [Jones et al. 2010] [Joos et al. 2011] [Juang * and Chio 2005] [Juang and Chien 2008] [Jump and Padfield 2005] [Jun Che and Degang Chen] [Jung et al. 2025a] [Kaminer and Khargonekar 1990] [Kansas Univ Lawrence 1952a] [Kato and Inagaki 2007] [Kato and Inagaki 2008] [Kaufmann and McNally 1995] [Kaufmann and Ncnally 1995] [Ke and Feng 2015] [Ke et al. 2014] [Kendoul and Ahmed 2012] [Kidwell 1963] [Kim et al. 2023c] [Kimmel and Oh 1988] [Kis and Lantos 2014] [Kistyarev and Wang 2025] [Kluever and Neal 2015] [Klumpp 1966] [Klumpp 1967] [Klumpp 1968] [Koh and Paranjape 2020] [Komatsu et al. 2003] [Kowal] [Kozina 1976] [Koziol et al. 1971] [Krishnan and Sajikumar 2023] [Kugler and Holzapfel 2017] [Kuhn 1959] [Kügler et al. 2019] [Lambregts 1982] [Le Bras et al. 2009] [Le Ngoc et al. 2010] [Lee and Davidson 1973] [Lee et al. 1998] [Lee et al. 2006] [Lee et al. 2007a] [Lee et al. 2016c] [Lehman 1964] [Leonard and Rodier 1966] [Li 2017] [Li and Hu 2018] [Li et al. 2015b] [Li et al. 2024b] [Li et al. 2025b] [Li et al. 2026i] [Liang et al. 2023] [Liao et al. 2004] [Liao et al. 2005] [Lighthill 1963] [Lin and Lai 2025] [Lina et al. 1959] [Ling 1969] [Ling 1970] [Liu et al. 2011c] [Liu et al. 2017a] [Liu et al. 2021a] [Liu et al. 2022a] [Liu et al. 2024d] [Liu et al. 2025k] [Lloyd et al. 1978] [Lowrance and Smith 1996] [Lu Keke et al. 2016] [Lungu 2017] [Lungu 2022] [Lungu and Lungu 2015a] [Lungu and Lungu 2015b] [Lungu and Lungu 2016] [Lykken and Shah 1971] [Lykken and Shah 1972] [Lyu et al. 2023] [Ma et al. 2018] [MacKinnon 1969] [MacKinnon 1970] [Mackinnon and Madden 1971] [MACKlNNON and Madden 1972] [Madden and Desai 1973] [Maiuzzo 1970] [Manjarrez et al. 2018] [Masafumi Morimoto et al. 2007] [Matveev 2017] [McCabe and DeMars 2018] [McDonald 1980] [McGee et al. 1970] [Meissinger 1963] [Mejias 2014] [Meng and Li 2014] [Meng et al. 2022a] [Meyer-Hilberg and Jacob] [Meyer-Hilberg and Jacob 1994b] [Wyatt and Tooley 2013d] [Miyazawa et al. 1993] [Miyazawa et al. 1996] [Miyazawa et al. 1998] [Mohammadkarimi and Nobahari 2018] [Mook et al. 1990] [Moore et al. 1979] [Muehter 1974] [Mumm and Holzapfel 2017] [Murray-Smith 1995] [Ménou] [Navarro-Tapia et al. 2017] [Negre 1975] [Negre 1977] [Nho and Agarwal 1998] [Nho and Agarwal 2000] [Niessen 1973] [Nowak et al. 2022] [Nugroho et al. 2024] [Numerical Optimization on Approach 2016] [Ochi and Kanai] [Oglesby 1975] [Ohno et al. 1998] [Ohno et al. 1999] [Ohta and Sugiura 1973] [Oishi et al. 2002] [Osder 1970] [Sreena and Thomas 2017] [Pan and Pi 2024] [Papadopoulos 1998] [Parker and Templeman 1967] [Parkinson and Fitzgibbon 1989] [Patrick 1972] [Payne 1968] [Peng et al. 2025a] [Perez and Benner 1973] [Peshkov et al. 2026] [Petrishchev 2018] [Petrov et al. 1980] [Phillips et al] [Phillips et al. 1983b] [Pierson 1985] [Pines 1982] [Pines and Hueschen 1978] [Plinge 2003] [Pogosyan and Vereikin 2020] [Pope and Staehle 1975] [Poritzky 1970] [Poulose 1992] [Powell 1960] [Precision Landing of Aircraft 1996] [Purcell et al. 2025] [Qi et al. 2018] [Abdhul Rahuman and Lee 2026] [Rashis and Bond 1961] [Rector and Hattendorf 1967] [Reitan and Saib 1976] [Response Analysis of Landing 2026] [Rhoads 1967] [Rimer and Sperling 1965] [Rithirun and Sooraksa 2013] [Rogers 1973] [Rosner et al. 2018] [Rubin 1971] [Rutishauser et al. 2012] [Ryu et al. 2025] [Hameed and Bindu 2021] [Sajjadi et al. 2026] [Sakaki and Ueba 2025] [Sanuki 1965] [Schmidt and Setterlund 1980] [Schmitt and Burchett 2004] [Schoenman and Doniger 1965] [Sedlmair et al. 2019] [Sedlmair et al. 2022] [Shayler 1961] [Shen and Rahman 2011] [Shen et al. 2025] [Sherman 1975] [Sherman 1976] [Sherman and Winfrey 1974] [Shim et al. 2008] [Shuang and Pingyuan 2006] [Shue and Agarwal 1999] [Shue et al. 1998] [Singh and Padhi 2009] [Singh et al. 2023] [Smith and Meyer 1980] [Smith and Meyer 1981] [Smith et al. 1972b] [Smith et al. 1974] [Snyder et al] [Snyder et al. 1992] [Song et al. 2023] [Sorensen and Karmarkar 1977] [Soumekh] [Soumekh 1996] [Steinberg 1992] [Steinberg and Page 2001] [Steinleitner et al. 2022] [Stoltz and Priedigkeit 1975] [Subrahmanyam 1994] [Subrahmanyam 1995] [Sullings and Waller 1967] [Sun et al. 2022] [Suozhong Yuan and Yidong Yang] [Davies 1974] [Ruxton-davies and Powell 1970] [Tariq et al. 2026] [Templeman and Parker 1968] [The Algorithm 2020] [Thomas and Thomas 2008] [Thompson 1965] [Thurman 2004] [Tomczyk and Gruszecki 1999] [Tonhauser and Hecker 2016] [Trawny et al. 2022] [Trinh et al. 2018] [Tripathi et al. 2018] [Tsikalas and Dyer 1982] [Tsoukalas et al. 2026] [Uijt de Haag et al. 2005] [Uijt_de_Haag and Vadlamani] [Ulukır et al. 2025] [Urnes and Hess 1983] [Urnes and Hess 1985] [Urnes et al. 1979] [Vallot et al. 1991] [Venkateswara Rao and Go 2014] [Vidimlic et al. 2021] [Wagdi 1984] [Walker 1960] [Walker 1961] [Walsh and Weener 1977] [Walsh and Weener 1978] [Wang and Wang 2013a] [Wang et al. 2014b] [Wang et al. 2018b] [Wang et al. 2020h] [Wang et al. 2021j] [Wang et al. 2022j] [Wang et al. 2023h] [Watanabe et al. 2020] [Watson et al. 1983] [Wei et al. 2018] [Weichelt et al. 1986] [Wenzel et al. 2010] [Westra et al. 1981] [Westra et al. 1986] [Wetzel] [White 1978] [White and Clark 1981] [Wibben and Furfaro 2016] [Williams et al. 2000] [Wilson et al] [Wilz and Johnson 1975] [Woloshen 1974] [Woodbury and Valasek 2015] [Woodbury and Valasek 2016] [Wright and Ruscus 1959] [Wu and Mueller 2018] [Wu and Zhu 2024] [Wu et al. 2026b] [Xiao et al. 2024b] [Xu 2005a] [Xu 2009] [Xu and Lan 2018] [Xu et al. 2016a] [Xu et al. 2017a] [Xu et al. 2025a] [Xue et al. 2022] [Yanagihara et al. 1999] [Yang et al. 2026b] [Yang et al. 2026f] [Yao et al. 2025] [You et al. 2012] [Yuan et al. 2014] [Yuan et al. 2025c] [Yue et al. 2018b] [Yue et al. 2018a] [Yue et al. 2019] [Yue et al. 2022b] [Yue et al. 2022a] [Yuta Akai et al. 2007] [Zaragoza Prous et al. 2025] [Zhang and Jia 2013] [Zhang and Wang 2013] [Zhang et al. 2017a] [Zhang et al. 2019c] [Zhang et al. 2021g] [Zhang et al. 2022e] [Zhang et al. 2023e] [Zhang et al. 2024h] [Zhang et al. 2025l] [Zhang et al. 2025d] [Zhao et al. 2020c] [Zhao et al. 2026a] [Zhen et al. 2018] [Zhen et al. 2019] [Zhesheng Jiang and Ordonnez 2007] [Zhou 2026] [Zhou and Neusypin 2023] [Zhou et al. 2020a] [Zhu 2024] [Zhu et al. 2026d] [Zhu Qi-dan et al. 2009] [Zou et al. 2026]

Supersonic inlets, buzz and engine compatibility

The duct that the free-flight model measured below a normal shock. Supersonic inlet pressure recovery, buzz, unstart, bleed and diverters, and inlet and engine compatibility and distortion. 103 titles name unstart and 51 name buzz, the failure modes the review above notes had no names when the X-10’s inlet was designed.

482 records. [Abedi et al. 2020] [Abuaf 1976] [Adams et al. 1984] [Alendar et al. 2022] [Alford and Durand 1964] [Alford et al. 1962] [Allen and Beke 1953] [Amatucci et al. 1982] [Amin and Hollweger 1981] [Amin and Hollweger 1983] [An Experimental Study 1981] [Ananthapadmanaban and Murganandam 2016] [Anderson 1983] [Anderson 1984b] [Anderson 2014] [Anderson and Levy 1991] [Anderson et al. 1960] [Arlinger 1976] [Askari and Abedi 2026] [Askari et al. 2017] [Automatic Detection and Suppression 1974] [Azevedo et al. 1990] [Babinsky 2014] [Balaji and Venkatasubbaiah 2025] [Ball and Ross 1972] [Ball et al. 1981] [Barr et al. 2018] [Barr et al. 2022] [Barry 1971] [Bauer et al. 1974] [Bauermeister and Ip 1968] [Baye-Wallace and Krouse 2022] [Beale and Collier 1989] [Beale and Zelenak 1992] [Beale et al. 2002] [Beale et al. 2006] [Beale et al. 2007] [Bedke and Gorrell 2021] [Beheim and Englert 1956] [Beke et al. 1956] [Benson and Anderson 1983] [Benson and McRae 1993] [Berto et al. 2020] [Biesiadny and Wendt 2004] [Blackaby et al. 1959] [Bogar et al. 1983] [Bond and Key 2025] [Bond and Key 2026] [Bowcutt et al. 1999] [Bowditch and Coltrin 1983] [Braun and Podleski 2019] [Burke and Poggie 2023] [Burley and Mansour 1970] [Burr 1968] [Burris 1966] [Burrows et al. 2017] [Burstadt and Calogeras 1974] [Burstadt et al. 1971] [Bustard et al. 2024] [Bustard et al. 2026] [Butze et al. 1969] [Shin 2005] [Calogeras 1969b] [Calogeras 1969a] [Campbell and Ellis 1970] [Campbell and Ellis 1971] [Cao et al. 2026] [Carbajosa et al. 2025a] [Carbajosa et al. 2025b] [Carbajosa et al. 2026] [Carlin et al. 2003] [Chandler and Montes 2019] [Chang and Hsu 1960] [Chang et al. 2009a] [Chang et al. 2011] [Chang et al. 2012] [Chang et al. 2014] [Chang et al. 2017c] [Chaudhari and Takahashi 2022] [Cheadle and DiZinno 2026] [Chen and Tan 2019] [Chen et al. 2015] [Chen et al. 2017a] [Chen et al. 2018f] [Chen et al. 2019b] [Chen et al. 2025c] [Chen et al. 2026e] [Chima 2011a] [Chima 2011b] [Chima et al. 2011] [Choe and Kim 2016] [Choe et al. 2020] [Choi et al. 2026] [Chopde et al. 2025] [Chun and Swanson 1964] [Chung 1994] [Chyu et al. 1992] [Clark 1974b] [Clark 1995] [Clauser 1954] [Collins 1970] [Connors 1962] [Cortright 1951] [Csavina and Denney 1991] [Cubbison and Smeltzer 1968] [Cui et al. 2011] [Cui et al. 2012] [Daliri et al. 2018] [Dann] [Davis and Kidman 2010] [Davis et al. 2001] [Deng and Kim 2017] [Dickman and Takahashi 2016] [Dicus 1975] [Diggins 1951] [Ding et al. 2015] [Do et al. 2011a] [Do et al. 2011c] [Do et al. 2011b] [Do et al. 2011d] [Do et al. 2012] [Domack 1991] [Dryer and Beke 1952] [Duncan and Thomas 1992] [Engelbrecht et al. 2022] [Engine Inlet Exhaust 2011] [Esenwein and Schueller 1952] [Eves and Valasek 2024] [Zhao et al. 2022c] [Ezzeldin and Wu 2025] [Fang and Qiang 2022] [Farahani et al. 2019] [Farr 1973] [Feng et al. 2026a] [Fernandez et al. 2001] [Ferri and Nucci 1951] [Fink and Anderson 1982] [Flanders 1970] [Fleeter et al. 1974] [Forner and Manter 1982] [Fraiser 1960] [Frey 2014] [Frey et al. 2025] [Frohnapfel et al. 2017] [Frohnapfel et al. 2020] [Fujimoto and Niwa 1993] [Fujimoto et al. 1991] [Fuqun et al. 1985] [Graber and Braithwaite 1974] [Grashof 1983] [Grenson and Beneddine 2018] [Guan 2012] [Guan and Yarng 1984] [Guan and Yarng 1987] [Guangyue et al. 2017] [Guimaraes et al. 2015] [Haas and Karanian 1980] [Haderlie and Crossley 2010] [Hale et al. 2004] [Hamed et al. 1997] [Harloff and Smith 1995] [Hawkins and Marquart 1995] [He et al. 2023] [Henderson 1999] [Herges et al. 2012] [Hermann 1950] [Hermann 1956] [Hong and Kim 2011] [Hong and Kim 2014] [Horing et al. 2024] [Houchard et al. 1983] [Hu et al. 2013b] [Huang et al. 2020] [Huang et al. 2026c] [Hubble and Smith 1979] [Hube 1968] [Hunt] [Hunter and Cawthon 1984] [Hunter et al. 1985] [Hurwitz et al. 1997] [Hutchins et al. 2012] [Hutchins et al. 2014] [Iannelli 2007b] [Iannelli 2007a] [Im and Do 2018] [Influence of Back Pressure 2017] [Instrumentation for in-Flight Determination 1974] [Jacocks and Kneile 1975] [Jagannathan and Johansen 2019] [Jahnen et al. 1999] [Connors and Allen 1958] [Jee and Etele 2018] [Jiao et al. 2015] [Jin et al. 2023b] [Jin et al. 2023c] [Jin et al. 2026] [Johns 2000] [Johnson and Narayanaswamy 2024] [Johnson and Wu 1975] [Johnson et al. 2022] [Johnson and Wu 1974] [James et al. 2021] [James and Kim 2022] [Kapoor et al. 1994] [Kawamura et al. 1987] [Kaya 1998] [Kennon 1989] [Kepler and Barry 1965] [Kerlick 1985] [Khandelwal et al. 1996] [Kim 2009] [Kim and Park 2026] [Kochendorfer 1953] [Koenig 1967] [Kopasakis and Connolly 2009] [Korn 1974] [Kouyoumjian 1957] [Kowalski and Szczepanik 2014] [Krivec et al. 1984] [Kumazaki and Shimamura 2026] [Kuroda and Fujii 1991] [Kurth and Bauer 2015] [Kurzke 2006] [Kurzke and Halliwell 2018] [Kwak and Lee 2011] [Kwak and Lee 2013a] [Kwak and Lee 2013b] [Kwak et al. 2013b] [Ladd and Norby 1998] [Lavan Kumar et al. 2013] [Lee and Jeung 2009] [Lee and Kang 2019] [Lee et al. 2007b] [Lee et al. 2010a] [Lee et al. 2025b] [Lehtinen and Zeller 1972] [Leissler and Nettles 1954] [Leonov et al. 2012] [Li et al. 2023c] [Li et al. 2025k] [Li et al. 2025f] [Lian et al. 2025] [Liou and Benson 2010] [Liu et al. 2014c] [Liu et al. 2019] [Liu et al. 2021c] [Liu et al. 2022f] [Liu et al. 2025h] [Liu et al. 2026f] [Loth et al. 2016] [Lu and Jain 1998] [Lucas et al. 2014] [Luo et al. 2020] [Luo et al. 2024] [Luo et al. 2026] [Ma et al. 2024b] [Ma et al. 2025b] [Mace and Sedlock 1981] [Maghsoudi et al. 2020] [Mahoney 1962] [Manoj Prabakar and Muruganandam 2019] [Mardoc 1970] [Marshall et al. 2000] [Marvin 1968] [Masud and Khan 2015] [Masud and Khan 2016] [Mayer and Paynter 1994] [Mayer and Paynter 1995] [Maywald and Beale 1991] [McVey et al. 1969] [Medina et al. 2021] [Mehalic 1988] [Melick and Simpkin 1972] [Merchant et al. 2003] [Merkli 1975] [Merkli 1976] [Mickola 1961] [Mihigo et al. 2009] [Miki et al. 2014] [Miller and Smith 2003] [Min et al. 2026] [Mitchell and Campbell 1957] [Mittal et al. 2026] [Moin and Lele 1998] [Moore 1985] [Moore and Jenn 1990] [Morton 2014] [Morton et al. 1991] [Moss et al. 2026] [Moyer 1963b] [Muller and Gasko 1967] [Murzionak] [Mushtaq and Gaetani 2023] [Nagao et al. 2019] [Namkoung et al. 2012] [Naruse et al. 2022] [Naseri et al. 2012b] [Naseri et al. 2012a] [Neaves and McRae 1995] [Neaves et al. 2001] [Nelson et al. 2014] [Nikaido and Hobson 2025] [Noftz and Jewell 2025] [Novik 1956] [O’brien and Lowe 2015] [Obikane 1984] [Oh and Yang 1994] [Ombrello et al. 2015] [Ordaz et al. 2017] [Orme et al. 2021] [Ostrander et al. 1995] [Oswatitsch 1980] [Overall 1976] [Page et al. 2017] [Palko 1972] [Palko 1974] [Palko 1975] [Paynter 1994] [Paynter and Chen 1983] [Paynter and Tjonneland 1992] [Paynter et al. 1992] [Paynter et al. 1993] [Pecinka et al. 2015] [Peters et al. 2001] [Pečinka et al. 2017] [Pfyl 1955] [Pollock et al. 2023] [Portnoy 1959] [Poudel and Bhattrai 2026] [Powell et al. 1985] [Pruitt and Bates 1992] [Pu et al. 2017] [Qifan et al. 2014] [Qu and Qiang 2023] [Rademakers et al. 2014] [Raju et al. 2020] [Ramprakash and Muruganandam 2016] [Ran and Mavris 2005] [Ratchford et al. 2025] [Reardon et al. 2021] [Redding et al. 2025] [Reyhner and Hickcox 1972] [Rizzetta 1991] [Rizzi and Schmidt 1978] [Rodriguez 2004] [Saleem Yusoof et al. 2016] [San Martin et al. 2025] [Sandeep 2023] [Saravanan et al. 2017] [Sarwar et al. 2024] [Sasoh et al. 2018] [Saunders and Keith 1991] [Scharnhorst 2012] [Schram and Narayanaswamy 2026] [Sedlock 1985] [Sepahi-Younsi 2022] [Sepahi-Younsi 2025] [Sepahi-Younsi and Esmaeili 2023] [Shi et al. 2010b] [Shigematsu et al. 1990] [Shigematsu et al. 1991] [Shimabukuro et al. 1979] [Shindo and Yanagi 1998] [Shulman et al. 1966] [Shuo et al. 1995] [Slater 2001] [Slater 2015] [Slater 2016] [Slater 2019] [Smeltzer and Sorensen 1972] [Solmaz and Uslu 2025] [Soltani and Askari 2018] [Soltani and Farahani 2012] [Soltani et al. 2011] [Sorensen and Bencze 1973] [Sousa and Paniagua 2015] [Squire 1965] [Srikant et al. 2010] [Steenken 2009] [Stephens and Svetgoff 2024] [Stokes and Acharya 2023] [Stubbs 1956] [Sun and Feng 2006] [Sun et al. 2026d] [Surber 1975] [Surber and Robinson 1983] [Surber and Sedlock 1978] [Surber and Sedlock 1979] [Suryanarayana et al. 2022] [Sussman 1968] [Syberg and Koncsek 1975] [Syberg et al. 1981] [System for Evaluation 1974] [T-4 Inlet/engine Compatibility Flight 1989] [Taghi-Abad et al. 2026] [Takasaki et al. 1998] [Tan et al. 2011] [Tang et al. 2023] [Tang et al. 2024a] [Taylor 1968b] [Teng et al. 2015a] [The Verification of Inlet/engine 1988] [Tomczak 2026] [Tong et al. 2024] [Trapier et al] [Trapier et al. 2006] [Trapier et al. 2007b] [Trapier et al. 2007a] [Trapier et al. 2008] [Trefny 2020] [Tudosie 2017b] [Tudosie 2017a] [Tudosie 2018] [Tudosie and Prisacariu 2022] [Tudosie and PĂUnescu 2017] [Tunik and Mayorov 2022a] [Tunik et al. 2022] [Utomo and Bura 2019] [Valdivia et al. 2014] [Vinogradov and Stepanov 2008] [Wagner et al. 2007] [Wagner et al. 2008] [Wagner et al. 2009a] [Wagner et al. 2009b] [Wagner et al. 2010] [Wallhagen et al. 1972] [Walter and Starkey 2016] [Wang et al. 2017e] [Wang et al. 2019f] [Wang et al. 2022m] [Wang et al. 2022l] [Wang et al. 2023i] [Wang et al. 2023d] [Wang et al. 2023l] [Wang et al. 2023f] [Wang et al. 2024p] [Wang et al. 2024k] [Wang et al. 2025i] [Wang et al. 2025h] [Wang et al. 2026b] [Wasserbauer 1969] [Wasserbauer and Gerstenmaier 1978] [Wasserbauer and Willoh 1968] [Watson 1953] [Wegener 1977] [Weidner 1979] [Wilcox and Whalen 1956] [Williams and Hunt 1980] [Williams and Yost 1973] [Williams et al. 1981b] [Williams et al. 1981a] [Wilson and Wright 1987] [Wilson and Zhang 2025] [Wojciechowski and Anderson 1981] [Wu et al. 2024] [Wyatt 1953] [Xie et al. 2015] [Xie et al. 2016] [Xie et al. 2026] [Xu et al. 2022e] [Yaghmaee and Roberts 1986] [Yamamoto et al. 2020] [Yan 2013] [Yang et al. 2023b] [Yang et al. 2024c] [Yang et al. 2025c] [Ye et al. 2019a] [Ye et al. 2022] [Yeager and Gertsma 1958] [Yeom et al. 2015] [Yu et al. 2007] [Yuceil et al. 2009] [Zelenak 1994] [Zeng et al. 2026] [Zha et al. 1998a] [Zha et al. 1998b] [Zhang et al. 2016b] [Zhang et al. 2016c] [Zhang et al. 2017c] [Zhao et al. 2025c] [Zheng et al. 2013] [Zhu et al. 2020a]

Navigation without satellites, by terrain, field and vision

Bounding a secular error with whatever the vehicle can observe. Terrain-referenced and terrain-aided navigation, magnetic anomaly navigation, vision-aided and lidar-aided inertial navigation, and the Doppler and Loran aids of the period. 112 titles name a satellite-denied environment, which is the modern framing of the Navaho’s problem that the review above calls a live problem again.

478 records. [El-gabri , A. N Ouda 2018] [Abahre, A. et al. 2019] [Abdelaziz and El-Rabbany 2022] [Abdelaziz and El-Rabbany 2023] [Jiang et al. 2023a] [Advances in Image Enhancement 1965] [Aguiar] [Alikhani and Nikoofard 2026a] [Allerton and Gia 1996] [Andresen and Davis 1984] [Andrews] [Andrisani, ck 1995] [Army Aviation Board Fort Rucker Al 1962] [Avrutov et al. 2026] [Baird et al] [Banks 1999] [Bar-Itzhack 1981] [Bar-Itzhack et al. 1982] [Baxa 1978] [Becker and Joerger 2024] [Beich and Veth 2010] [Beisner 1969] [Bennett] [Bergman 1997] [Bhowmick et al. 2021] [Blakely and Nielsen 2025] [Blakely et al. 2025] [Bogdanov et al. 2024] [Bogue et al. 1995] [Boozer and Fellerhoff 1988] [Borodacz and Szczepański 2023a] [Bortolami et al. 2020] [Bouazza] [Braff and Braverman 1965] [Brink et al. 2010] [Brophy and Hawk 1990] [Brown and Hagerman 1969] [Buell 1964] [Bynum and Holman 1979] [Campbell et al. 2005] [Canciani and Raquet 2016b] [Canciani and Raquet 2017] [Cao et al. 2025b] [Carroll and Canciani 2021] [Caruso] [Casasent 1979] [Casasent 1984] [Causa and Fasano 2021] [Chang et al. 2024a] [Chen 2020] [Chen and Zou 2026] [Chen et al. 2021b] [Cheng et al. 2013a] [Cheng et al. 2025] [Cheol Jeon and Gook Park 2018] [Chernodarov et al. 2023] [Choe and Park 2021] [Choe et al. 2022] [Cook and Craig 1980] [Copp and Subbarao 2015] [Cortancioglu et al. 2025] [Criss et al. 2010] [Dai et al. 2020] [Dasgupta et al. 2026] [Davis 1986] [Davis 1988b] [De Groot 1965] [Dektor and Rock 2014] [Deng et al. 2019a] [Derby et al. 1964] [Deshpande 2021] [Dettbarn 1957] [Di Corato et al. 2013b] [Di Corato et al. 2013a] [Dill et al. 2017] [Do et al. 2010] [Du et al. 2021] [Duncan 1959] [Dunn 1984] [Duran and Leloglu 2026] [elahian et al 2024] [Ellingson et al. 2018] [Eroglu and Yilmaz 2013b] [Eroglu and Yilmaz 2013a] [Fan et al. 2025] [Fang 1995] [Fares et al. 2026] [Feder et al] [Fekry et al. 2026] [Fellerhoff 1988] [Feng et al. 2012b] [Fitzgerald 1974] [Flayac] [Funk 1975] [Fusini et al. 2017] [Gallo and Barrientos 2023a] [Gallo and Barrientos 2023b] [Gallo Olalla] [Gan et al. 2022] [Ge et al. 2024] [Geneva et al. 2020] [Geragersian et al. 2022] [Ghanizadegan] [Ghanizadegan and Hashim 2025b] [Gitterman and Watkins 1965] [Golden 1980] [Goldenberg] [Gomaa et al. 2022] [Gopaul et al. 2017] [Graf and Trimble 1980] [Greentree et al. 2022] [Grenet and Mansour 2010] [Griffioen and Oonincx 2012] [Groves et al. 2005] [Gryte et al. 2019] [Gu et al. 2021a] [Guo et al. 2016] [Guo et al. 2026b] [Gupta et al. 2024] [G�bel et al 2017] [Ha and Lee 2013] [Hagen 2006] [Hager et al. 2025] [Hagerman] [Han and Park 2024] [Han et al. 2026b] [Hardy] [Hashim] [Haydon and Humphreys 2023] [Haydon et al. 2025] [Hayslett et al. 1978] [Hemann et al. 2016] [Henley] [Hernandez et al. 2015] [Hess 1989] [Hledik 1963] [Hodgson and Lee 2003] [Hong 2025] [Hong et al. 2017] [Hossein and Amindavar 2012] [Hostetler 1978] [Hou et al. 2020] [Howard 1980] [Howell 1980] [Huang et al. 2017b] [Huang et al. 2024b] [Huang et al. 2024a] [Huang et al. 2026d] [Hurak and Rezac 2009] [Hursh 1985] [Inertial and magnetic sensors] [Jain et al. 2023] [Jang and Bang 2017] [Jang et al. 2017] [Jarraya et al. 2025] [Jarraya et al. 2026] [Jeon et al. 2016] [Jeon et al. 2017] [Jeon et al. 2018b] [Jeon et al. 2018a] [Jian and Xingwu 2010] [Jiang et al. 2014] [Jiang et al. 2019] [Jiang et al. 2026] [Jiao et al. 2025] [Jin et al. 2016] [Johnson et al] [Jose] [Jurado et al. 2012] [Kaehr and Spector 1980] [Kandemir and Bingol 2017] [Kandemir and Bingol 2018] [Kang et al. 2020] [Kang et al. 2025] [Karmozdi et al. 2018] [Kashyap 2025] [Kassas et al. 2020] [Kedong and Yong Yang 2010] [Khalifa and Hashim 2026] [Kim and Sukkarieh 2005] [Kim et al. 2013b] [Kim et al. 2018b] [Kim et al. 2022c] [Kim et al. 2024] [Kim et al. 2025b] [Kim et al. 2025a] [Kleinert and Schleith 2010] [Kleinert and Stilla 2013] [Knight et al. 2026] [Knuth and Groves 2025] [Kottas and Roumeliotis 2013] [Krishnaswamy et al. 2008] [Kumar 2026b] [Kumar 2026a] [Kuroswiski et al. 2018] [Labowski et al. 2016] [Landherr and Klein 1989] [Last 1992] [Lautier-Blisson] [Lee and Johnson 2020] [Lee et al. 2012b] [Lee et al. 2014] [Lee et al. 2019] [Lee et al. 2022] [Lee et al. 2024a] [Lee et al. 2026b] [Lee et al. 2026d] [Li 2026a] [Li and Mourikis 2012] [Li and Mourikis 2013] [Li and Wang 2012] [Li and Wang 2013] [Li et al. 2018a] [Li et al. 2022i] [Li et al. 2022j] [Li et al. 2022a] [Li et al. 2026d] [Lian et al. 2026] [Liang and Gao 2025] [Liang et al. 2026] [Liao et al. 2010] [Lin and Chen 2025] [Lin et al. 2025] [Liu et al. 2012d] [Liu et al. 2017g] [Liu et al. 2022m] [Liu et al. 2022l] [Liu et al. 2022g] [Liu et al. 2023e] [Liu et al. 2024b] [Liu et al. 2025f] [Liu et al. 2026b] [Liu et al. 2026h] [Longenbaker 1982] [Luo et al. 2025] [Lux and Eibert] [Lyu et al. 2024a] [Maarten Uijt de Haag et al. 2006] [Madani and Allerton 2006] [Magree and Johnson 2013] [Magree and Johnson 2015] [Magree and Johnson 2016] [Markó et al. 2023] [Martens and de Haag 2023] [Martin et al. 2024] [Martinelli 2012] [Masters 1986] [Mathisen and Fossen 2019] [McCabe and DeMars 2019b] [McCabe and DeMars 2019a] [McGee and Shankar 2018] [Mercado-Ravell] [Metzger et al. 2004] [Metzger et al. 2005] [Miner and Gloss 1975] [Mitrev] [Mo et al. 2018] [Mok and Bang 2013] [Mok et al. 2012] [Mok et al. 2017a] [Mok et al. 2017b] [Moon et al. 2018] [Mostafa et al. 2018b] [Mostafa et al. 2018a] [Mourikis and Roumeliotis 2007] [Moussa et al. 2019] [Moussa et al. 2020] [Mukhina et al. 2020] [Møller-Skuldbøl et al. 2026] [Nagata et al. 2019] [Navon et al. 2025] [Neuhauser et al. 2026] [Ng et al. 2022] [Nguyen et al. 2017a] [Nguyen et al. 2017b] [Nieuwenhuisen et al. 2015b] [Nieuwenhuisen et al. 2015a] [Nilsson et al. 2012] [Nitin 2024] [Noble 1963] [Nygren and Jansson] [Oh et al. 2019] [Oliveira et al. 2023] [Ott and Ott 1979] [Ouyang et al. 2021] [Panahandeh and Jansson 2011] [Panahandeh et al. 2012] [Panahandeh et al. 2013] [Panahandeh et al. 2015] [Pang] [Park and Bang 2022] [Park and Bang 2023] [Park and Bang 2024] [Park and Bang 2025] [Park and Park 2018] [Park and Park 2019] [Park and Park 2020] [Park and Park 2021] [Park et al. 2017] [Parnian and Golnaraghi 2010] [peijie et al 2025] [Perkins et al. 2019] [Pienkowski 1967] [Pintér and Marcoň 2024] [Pisarski et al. 2026] [Polz et al. 2025] [Potter 1964] [Praczyk and Zalewski 2026] [Priestley] [Qiao et al. 2010] [Qiu et al. 2022a] [Qiu et al. 2022b] [Quarmyne and Pachter 2014] [Quynh et al. 2026] [Rabiee et al. 2019] [Radio Optical/strap down Inertial 1967] [Radio/optical/strapdown Inertial Guidance Study 1969] [Ramos et al. 2022] [Raut and Mehendale 2025] [Reel 1959] [Rekhy et al. 2020] [Renault et al] [Riedel 1976] [Rizk et al. 2020] [Roberts 2020] [Roberts and Vallot] [Rohrschneider 2011] [Rollason et al. 2003] [Roux et al. 2023] [Sabatini 2011] [Sakran 1967] [Salib et al. 2020] [Samadzadegan and Saeedi 2008] [Sanchez 2004] [Savkin et al. 2021] [Schmidt 2015b] [Schmidt 2018] [Schmitt and Fichter 2016] [Scott 1956] [Sengupta 2025] [Shahkar and Khorasani 2023] [Shahoud et al. 2021] [Shan et al. 2014] [Sheikhpour and Atia 2020] [Sheikhpour Kourabbaslou] [Short-Range Radio Navigation 2018] [Shpagin and Panchenko 2026] [Silva et al. 2025] [Sineglazov 2014] [Sineglazov and Ischenko 2019] [Singh 2022] [Singh and Lim 2008] [Singh and Uijt de Haag 2007] [Sivalingam and Hagen 2023] [Sivalingam and Hagen 2026] [Sokolov and Chub 2024] [Sonmez and Bingol 2008] [Soon and Scheding] [Staley 1963] [Stoven-Dubois et al. 2018] [Suh 2009] [Sun et al. 2009b] [Sun et al. 2017] [Sun et al. 2025c] [Sung et al. 2017] [Sung et al. 2019] [Sweat et al. 2025] [Sweeney et al. 2021] [Tabassum et al. 2026] [Tang et al. 2015a] [Taylor 2012a] [Taylor et al. 2026] [Terrain Aided Navigation System 1986] [Terrain Navigation Using Bayesian 1999] [Terrain Referenced Navigation Technique 2023] [Terrain Relative Navigation 2025] [Tian et al. 2017] [Tian et al. 2025] [Tkhorenko and Karshakov 2022] [Tokta and Hocaoǧlu 2023] [Toth et al. 2008] [Troiani] [Troiani and Martinelli 2012] [Tsai et al. 2001] [Tsao 2023] [Tsiopliakis 2026] [Tsoubanos 1979] [Tulembayev et al. 2026] [Turan 2020] [Turan and Kutay 2016] [Turan and Ünsal 2023] [Twigg et al. 2006] [Tyren] [Tyrén 1982] [Unlu et al. 2023] [Uygar Yengin and Koyuncu 2025] [Vadlamani and de Haag] [Valles et al. 2017] [Vaman 2012] [Vepa and Zhahir 2010] [Veselý et al. 2025] [Videmsek and de Haag 2020] [Vision-Aided Inertial Navigation Based 2014] [Visual Analysis of Strapdown 2023] [Wahab Memon and Zhang 2023] [Wang] [Wang and Tayebi 2019] [Wang and Zhao 2026] [Wang et al. 2018f] [Wang et al. 2018i] [Wang et al. 2018j] [Wang et al. 2018h] [Wang et al. 2019c] [Wang et al. 2019e] [Wang et al. 2020k] [Wang et al. 2020a] [Wang et al. 2022g] [Wang et al. 2023j] [Wang et al. 2025c] [Wang et al. 2025f] [Ward 1968] [Waters et al. 2025] [Welch 1963] [Welch 1965] [Werner et al. 2026] [Williams et al. 2011] [Willis and Powell 1965] [Wu and Huang 2026] [Wu Erhui et al] [Wu et al. 2005a] [Wu et al. 2005b] [Wu et al. 2023a] [Xiang et al. 2025] [Xiao and Bian 2010] [Xiao et al. 2019] [Xiaojiao Ma et al. 2009] [Xu and Zhang 2024] [Yadav and Kumar Goyal 2025] [Yang] [Yang et al. 2018a] [Yang et al. 2022d] [Yi-Fei and Hui 2018] [Yigit and Yilmaz 2012] [Yoo and Park 2015] [Yu et al. 2022a] [Yue et al. 2026] [Yuksel and Kaygisiz] [Yun and Park 2014] [Yun et al. 2014] [Zachariah and Jansson 2010] [Zaeim et al. 2010] [Zahran et al. 2018b] [Zahran et al. 2018a] [Zahran et al. 2019] [Zahran et al. 2021] [Zarchan 1977] [Ze Peng et al. 2018] [Zelenka 1994] [Zhai and Wang 2020] [Zhang and Yang 2022] [Zhang et al. 2017e] [Zhang et al. 2022a] [Zhang et al. 2023g] [Zhang et al. 2023d] [Zhang et al. 2024f] [Zhang et al. 2025k] [Zhang et al. 2026m] [Zhao 2011] [Zhao 2012] [Zhao 2024a] [Zhao et al. 2012] [Zhao Long 2012] [Zhou et al. 2014] [Zhou et al. 2021d] [Zhou et al. 2025b] [Zhu and He 2020] [Zhu et al. 2020b] [Şanlan et al. 2025]

Alignment, calibration and initialisation

The pointing built in before the vehicle moves. Initial and transfer alignment, gyrocompassing, and the calibration and initialisation of inertial sensors and systems. 208 of these titles name alignment, the coequal partner of drift that the article’s azimuth relation identifies.

411 records. [Abbas et al. 2011] [Іванов and Білич 2012] [Afonin et al. 2022] [Aktakka et al. 2017] [Alam et al. 2015] [Alhassan and Ghahremani 2021] [Ali and Nzar 2008] [Ali and Ushaq 2009] [Ali Rahgoshay et al. 2017] [An and Zhang 2015] [Arbabmir and Ebrahimi 2020] [Armin et al. 2025] [Asif et al. 2024] [Aslan and Tatar 2026] [Avrutov et al. 2017] [Bai and Wang 2017] [Bakalli et al. 2021] [Bakalli et al. 2023] [Balamuta et al. 2018] [Ban et al. 2022a] [Bar-Itzhack 1988] [Bar-Itzhack 1990a] [Bar-Itzhack and Goshen-Meskin 1988] [Bar-Itzhack and Porat 1980] [Barantsev et al. 2021b] [Barantsev et al. 2022] [Bassolillo et al. 2024] [Belsky et al. 2018] [Belyanin et al. 2018] [Ben Elisha and Indelman 2017] [Ben-Arie et al. 2026] [Beşdok 2009] [Bimal Raj and Joshi 2015] [Bing et al. 2017] [Blanchard 1978] [Blanchard 1979] [Bo et al. 2008] [Bowers et al. 1967] [Bowers et al. 1968] [Britting and Palsson 1968] [Britting and Palsson 1970] [Buell and Reed 1967] [Cannon 1961] [Cao and Guo 2012] [Carlson and Bott 1973] [Carlsson et al. 2017] [Carlsson et al. 2021] [Chan et al. 2015] [Chang et al. 2013] [Chang et al. 2017a] [Chang et al. 2017b] [Chang et al. 2019] [Chang et al. 2022] [Chen et al. 2014b] [Chen et al. 2022c] [Chen et al. 2022a] [Chen et al. 2026g] [Cheng et al. 2018a] [Chikovani and Golovach 2021] [Choi et al. 2023a] [Daniel 1965] [Daoudi] [Dasaro 1970] [de Vries et al. 2023] [Dedes et al. 2024] [Di Liu et al. 2008] [Ding et al. 2025] [Doer and Trommer 2020] [du Plessis et al. 2009] [Ebrahim et al. 2020] [Einicke 2008] [El-Diasty and Pagiatakis 2008] [Eminoglu et al. 2014] [Engelsman and Klein 2026] [Fang and Zheng 2018] [Farrell 1968] [Fedorov et al. 2020] [Fei and Feng 2005] [Feng and Hung 1985] [Feng and Zhang 2023] [Feng et al. 2012a] [Feng et al. 2013] [Filatov et al. 2014] [Fisher 1996] [Fu et al. 2013] [Fu et al. 2018] [Fu-jun et al. 2024] [Galloway and Barnaba 1983] [Gando et al. 2020] [Gao et al. 2014] [Gao et al. 2015a] [Gao et al. 2015b] [Gao et al. 2018b] [Gao et al. 2019] [Gao Fuquan et al. 2010] [Ge et al. 2015] [Ghanbarpourasl 2020] [Ghasrizadeh and Nikkhah 2020] [Glaros] [Gnadt 2022] [Golovan et al. 2017] [Goncalves et al. 2018] [Gordan 1987] [Goshen-Meskin and Bar-Itzhack 1992a] [Grewal et al] [Gross et al. 2010b] [Gu et al. 2019b] [Guerrier et al. 2015] [Guerrier et al. 2016a] [Guo et al. 2012a] [Guo et al. 2014] [Guo et al. 2017b] [Guo et al. 2018b] [Györfi and Wagner 2025] [Hager et al. 2026] [Haitjema] [Hall and Williams 2000] [Hall et al. 2000] [Han et al. 2014a] [Han et al. 2018c] [Hand 1968] [Hao et al. 2008] [Hao et al. 2020b] [Hartl] [Hartzer and Saripalli 2023] [Hayworth 2003] [He et al. 2015b] [He et al. 2020b] [He et al. 2020a] [Heinssen et al. 2015] [Hellings 1973] [Hill et al] [Hodson 1963] [Hong and Park 2017] [Hong et al. 2010] [Hu et al. 2026] [Huang and Wang 2011] [Huang et al. 2026b] [Hung and White 1974] [Hung and White 1979] [Inertial Navigation System Alignment 2004] [Inertial Navigation System Ground 2007] [Initial Alignment of Large 2018] [INS et al. 2001] [INS et al. 2023] [Iozan et al. 2012] [Jackson 1973] [Jahanshahi and Lai 1983] [Jameian and Safarinejadian 2021] [Jiang and Li 2023] [Jiang Cheng Fang and De Jun Wan 1996] [Jianzhong 2018] [Jin et al. 2014] [Jin et al. 2025b] [Jing et al. 2016a] [Jingyu Cao et al. 2011] [Johnson] [Juan et al. 2011] [Kaiser et al. 2017] [Kelly and Sukhatme 2009] [Kelly and Sukhatme 2010] [Kennel 1967] [Khudher 2026] [Kim and Park 2008] [Kim et al. 2013a] [Kim et al. 2021b] [Kim et al. 2023b] [Kim et al. 2023d] [Knickmeyer and Knickmeyer 1991] [Kobayashi 2026] [Koppe et al. 2014] [Kouba and Mason 1962] [Kozlov et al. 2019] [Kozlov et al. 2026] [Krishnan and Grobert 1970] [Lange 1977] [Lee and Lee 2024] [Lee et al. 2002] [Lee et al. 2021] [Lei et al. 2014a] [Li and Duan 2012] [Li and Li 2018a] [Li and Tao 2010] [Li and Yang 2009] [Li et al. 2012b] [Li et al. 2014d] [Li et al. 2014b] [Li et al. 2014a] [Li et al. 2018f] [Li et al. 2021c] [Lin et al. 2022] [Lin et al. 2023] [Lipton 1967] [Liu 2024] [Liu and Liu 2026] [Liu and Shen 2017] [Liu and Yang 2023] [Liu et al. 2012b] [Liu et al. 2014f] [Liu et al. 2014e] [Liu et al. 2016c] [Liu et al. 2018c] [Liu et al. 2022k] [Liu et al. 2024c] [Liu et al. 2026e] [Lou et al. 2026] [Lubin Chang et al. 2015] [Lyons 1972] [Lyu and Cheng 2017] [Lü et al. 2009] [Ma et al. 2023b] [Ma et al. 2024a] [Majid Msallam et al. 2025] [Pearson et al. 1973] [Samaan et al] [Malakar and Roy 2014] [Mann and Carlson 1994] [Marino et al. 2026] [Marquette et al. 2010] [Martin et al. 2016] [Martos et al. 2011] [Mascitti and Maglieri 1979] [Masuda 1999] [McDonald 1967] [Miao et al. 2022b] [Miao et al. 2022a] [Milne and Martos 2012] [Minaretzis et al. 2024] [Ming et al. 2015] [Mo et al. 2010] [Moleski and Wilhelm 2026] [Molnar et al. 2026] [Mongush et al. 2025] [Mou et al. 2021a] [Mousa et al. 2016] [Mravec and Vestenicky 2014] [Müller 1972] [Nadig et al. 2014] [Naidu and Kumar 2022] [Nan et al. 2025] [Nebot and Durrant-Whyte] [Nebot and Durrant-Whyte 1999] [Nguyen and Ogier 2024] [Nguyen et al. 2023a] [Niespodziany 2018] [Nikolic et al. 2016] [Ning et al. 2022b] [Ning et al. 2023] [Niu et al. 2013] [O’Halloran and Warren 1972] [Okon 2019] [Optimum Digital Filter Study 1968] [Pan et al. 2014] [Panahandeh et al. 2010] [Park et al. 2020] [Parrish et al. 2025a] [Parvin 1962] [Pei et al. 2021] [Peng et al. 2024] [Peng et al. 2026] [Peng-fei et al. 2018] [Peters 1978] [Poddar and Kumar 2019] [Poddar et al. 2016] [Podder et al. 2024] [Porat and Bar-Itzhack 1979] [Priel 1992] [Prikhodko et al. 2013] [Prohortsov et al. 2020] [Qasem et al. 2008] [Qi et al. 2021] [Qian et al. 2010] [Rahgoshay et al. 2017] [Raspopov et al. 2020] [Reilly 1994] [Rezaifard and Abbasi 2017] [Rodríguez-Martínez and Troni 2024] [Roman and Dobra 2026] [Ru et al. 2022] [Rupniewski 2025] [Saab and Gunnarsson] [Sabater et al. 2022] [Safarinejadian and Yousefi 2015] [Savage 2018] [Scandaroli] [Schneider 1983] [Seeley and Cole 1960] [Seong 2006] [Shan et al. 2025] [Shang and Gao 2012] [Sharma] [Shen et al. 2010b] [Shen et al. 2010a] [Shen et al. 2026] [Si et al. 2017] [Sidar and Bar-Shlomo 1972] [Silva et al. 2014] [Sinha and Maurya 2017] [Siu et al. 2013] [Song et al. 2017b] [Stimac and Kennedy] [Strap-Down Inertial Sensor Laboratory 2007] [Sun et al. 2009a] [Sun et al. 2010] [Sun et al. 2012] [Sun et al. 2015] [Sun et al. 2020b] [Sutherland et al. 1968] [Syed et al. 2008] [Tadic and Vukajlovic 2013] [Tanner 1972a] [Tatar 2026] [Taylor 2012b] [Thompson 2000] [Tian and Compere 2019] [Tomczyński et al. 2017] [Uspenskyi et al. 2018] [Vathsal 1986] [Vau et al. 2021] [Viswanath et al. 2022] [Voirol et al. 2020] [Wang 2009] [Wang 2025] [Wang and Chen 2010] [Wang and Chen 2018c] [Wang and Chen 2018a] [Wang and Meng 2008] [Wang and Qi 2024] [Wang and Shen 2005] [Wang and Wang 2022] [Wang and Yang 2013] [Wang et al. 2011c] [Wang et al. 2017i] [Wang et al. 2018e] [Wang et al. 2021k] [Wang et al. 2022n] [Wang et al. 2025l] [Wang et al. 2025e] [Wang et al. 2026k] [Wang Xinlong et al] [Wannas et al. 2026] [Wei et al. 2016b] [Wei et al. 2020] [Wei et al. 2022a] [Wei Gao et al] [Welter et al. 1996] [Wenming Li et al. 2011] [Wu 2014] [Wu and Ornedo 1990] [Wu and Sun 2012] [Wu et al. 2009] [Wu et al. 2010a] [Wu et al. 2018b] [Xia Gang et al. 2010] [Xiang et al. 2021] [Xiang Li et al. 2008] [Xiangming et al. 2017] [Xiaoxia and Yi 2006] [Xie and Lu 2016] [Xie et al. 2025] [Xing et al. 2019b] [Xingyu and Tingting 2016] [Xu and Zhou 2018] [Xu et al. 2017b] [Xu et al. 2019b] [Xu et al. 2025b] [Yaakov and Gruver 2016] [Yampolsk and Klein 2024] [Yan et al. 2023a] [Yan et al. 2024] [Yang et al. 2020a] [Yang et al. 2025e] [Yao et al. 2024] [Ye et al. 2023] [Ye et al. 2025a] [Yegorov and Diumin 1996] [Yi et al. 2014a] [Yu and Crassidis 2016] [Yu et al. 2008] [Yu et al. 2025c] [Yuan and Ting 2018] [Yuan et al. 2015] [Zakharin and Ponomarenko 2019] [Zakharin and Ponomarenko 2024] [Zang et al. 2023] [Zhang 2014] [Zhang 2016] [Zhang and Huang 2024] [Zhang and Yang 2014] [Zhang et al. 2018d] [Zhang et al. 2019a] [Zhang et al. 2019d] [Zhang et al. 2022l] [Zhang et al. 2023f] [Zhao et al. 2008] [Zhao et al. 2014a] [Zhao et al. 2019c] [Zhao et al. 2022e] [Zhao et al. 2026b] [Zhen Shi et al. 2010] [Zhong et al. 2017] [Zhou et al. 2011] [Zhou et al. 2020b] [Zhou et al. 2021a] [Zhu and Cheng 2013a] [Zhu and Cheng 2013b] [Zhu and Wu 2023] [Zhu et al. 2018] [Zhu et al. 2021d] [Zimbelman 1987] [Zotov et al. 2014a]

Aerodynamic heating and high-temperature structures

The aluminium frontier and what lies past it. Aerodynamic heating of supersonic and hypersonic vehicles, aerothermoelastic analysis, and the materials and structures of elevated temperature. 134 titles name aerothermoelasticity, 89 of them for a hypersonic vehicle or a skin panel, plate or shell, which is the coupled computation the review above says would have placed the frontier exactly.

386 records. [Abbas et al. 2008] [Abbas et al. 2009] [Abbas et al. 2014c] [Abbas et al. 2014b] [Abbas et al. 2014a] [Adams and Rubin 1958] [Aerodynamic and Base Heating 1974] [Aerodynamic Heating of Blunt 1958] [Aerothermodynamic Base Heating 1978] [Allen 1964] [Allen 1966] [Allen and Eggers 1957] [Allen and Eggers 1958] [Allen et al. 1963a] [Army Scientific Advisory Panel Washington Dc 1975b] [Army Scientific Advisory Panel Washington Dc 1975a] [Avdeenko 2002] [Avery et al. 1983] [Axelson et al. 1970] [Baghdasaryan et al. 2013] [Baird 1964] [Banichuk et al. 2020] [Banner and Kinsler 1961] [Banner et al. 1962] [Barz 2026] [Batt and Gallagher 1963] [Bazarko et al. 1965] [Bein et al. 1993] [Berthelot et al. 2026] [Bettis and Hosder 2010] [Bi et al. 2024] [Biernson 1965] [Bland and Collie 1961] [Bland et al. 1958] [Blosser 1997] [Brouwer and McNamara 2019] [Brouwer et al. 2016] [Brown et al] [Cantó et al. 2009] [Capey 1961] [Carek 1993] [Caruso and Naegeli 1976] [Case Study 2001] [Castro and de Boer 2020] [Chai et al. 2017] [Chai et al. 2018] [Chapter 1 2013] [Chatzis et al. 2014] [Chen 1958] [Chen and Zhao 2019] [Chen et al. 2017c] [Chen et al. 2018b] [Chen et al. 2024a] [Chen et al. 2026h] [Cheng et al. 2014] [Chou and Smith 1974] [Chou and Smith 1978] [Chung and Goodwin 1962] [Cochran and Cubbison 1966] [Cook 1996] [Culler et al. 2009] [Daryabeigi 2001] [Daub et al. 2022] [Davis et al. 1970d] [Davis et al. 1970b] [Davis et al. 1970c] [Davis et al. 1970a] [Davis et al. 1972] [Dejarnette 1979] [Dejarnette and Hamilton 1974] [Dejarnette et al. 1983] [Dejarnette et al. 1985] [Delmundo et al. 1981] [Derose and Lockman 1971] [Derose et al. 1971] [Deveikis et al. 1965] [Dol 2021] [Dragone 2000] [Drakin 1963] [Dugundji and Calligeros 1961] [Dugundji and Calligeros 1962] [Eastwood 1968] [Eftekhari et al. 2025] [Ekvall et al. 1989] [Ekvall et al. 1990] [Elgin and Sutliff 1993] [Engel and Lapointe 1979] [Engel et al. 1974] [Engelstad et al. 2023] [Equipment to Simulate Aerodynamic 1971] [Ericsson et al. 1978] [External Autoignition Test 1986] [Fairbairn 1964] [Falkiewicz and Cesnik 2010] [Falkiewicz and Cesnik 2011b] [Falkiewicz and Cesnik 2011a] [Falkiewicz and Cesnik 2017] [Falkiewicz et al. 2010] [Falkiewicz et al. 2011] [Fan et al. 2008] [Fischer and Norris 1949b] [Fischer and Norris 1949a] [Fischler 1981] [Flanagan 1993] [Fornasier and Heiss 1987] [Foster et al. 1985] [Freed and Miller 1961] [Freydin and Dowell 2021] [Friedmann et al. 2010] [Fu et al. 2024a] [Garrec and Kubica 2005] [Ghori et al. 2023] [Gogulapati et al. 2017] [Gopinath et al. 2015] [Griffin et al. 2023] [Gringorten 1967] [Gringorten and Tattelman 1970] [Gueho et al. 2021a] [Gueho et al. 2021b] [Guess et al. 1981] [Guo et al. 2019] [Gupta et al. 1997] [Gupta et al. 2010] [Gupta et al. 2016] [Gupta et al. 2017] [Halim et al. 2022] [Hall et al. 2023] [Hall et al. 2026] [Harri 1964] [Harrison and Lockman 1968] [Harrison and Marko 1968] [Hartman et al. 2001] [Harvey 1967] [Heeg et al. 1990] [Heeg et al. 1993a] [Heeg et al. 1993b] [Hefti 2012] [Heimerl and Hardrath 1965] [High and Bowman 1995] [Hodge and Audley 1983] [Hoke et al. 2004] [Holifield and Tufts 2024] [Horvath et al. 2008] [Huang and Cui 2012] [Huang and Friedmann 2016] [Huang and Friedmann 2019] [Huang and Friedmann 2020a] [Huang and Friedmann 2020b] [Huang et al. 2017a] [Huang et al. 2018c] [Huang et al. 2018b] [Huang et al. 2019a] [Hunt 1977] [Hunt and Jones 1966] [Hunt and Jones 1968] [Huo et al. 2015] [Volkov 2023b] [Hyötyniemi 1997] [Imig 1973] [İpek 2025] [Ji and Xie 2022] [Jiang and Li 2018] [Johnson 1949] [Jones and Cesnik 2025] [Jones and Richie 1974] [Joubert et al. 2021] [Kain et al. 1978] [Kamali et al. 2022] [Karabutov 2020] [Karabutov 2025a] [Karlsson et al. 2012] [Kaufman and Johnson 1984] [Kaye and Yeh 1955] [Kendall and Gonzalez 1965] [Keçeci et al. 2025] [Khankhasaeva 2023] [Kimmel et al. 2024] [Kimmel et al. 2026] [Kirkpatrick et al. 2026] [Klock and Cesnik 2015] [Klunker and Ivey 1949] [Klunker and Ivey 1950] [Kremeyer and Pakhomov 2008] [La et al. 2017] [Lamorte and Friedmann 2013] [Lamorte and Friedmann 2014] [Lamorte et al. 2014] [Lanning and Hung 1971] [Larson and Mount 1986] [Laumann 1965] [Le et al. 2023] [Lee 1969b] [Lee and Rumsey 1959] [Lee and Singh 2011] [Lee et al. 2003] [Leontiev and Pavlyuchenko 2004] [Lepsien et al. 2025] [Levy et al. 1974] [Lhachemi et al. 2016a] [Li and Eri 2007] [Li et al. 2009c] [Li et al. 2012a] [Li et al. 2016b] [Li et al. 2017a] [Li et al. 2018b] [Lian et al. 2012] [Light High-Temperature Aluminum Alloys 1992] [Lin and Yang 2005] [Lind 1999] [Lind 2002] [Liu et al. 2002] [Liu et al. 2010b] [Liu et al. 2023g] [livani et al 2016] [Lockman and Derose 1971] [Lunde 1977] [Lv et al. 2015] [Mahlmeister et al. 1955] [Maples 1979] [Mapurunga and Bazanella 2021] [Masek et al. 1973] [Matheny and Smith 2026] [Mavriplis and Levy 2002] [Mavriplis and Levy 2005] [Maykapar 1968] [Mazhar et al. 2025] [McFarland and D’Souza 1994] [McNamara and Friedmann 2006] [McNamara and Friedmann 2007] [McNamara and Friedmann 2011] [McNamara et al. 2004] [McNamara et al. 2005b] [McNamara et al. 2005a] [McNamara et al. 2008] [McNamara et al. 2009] [Medianu and Lefèvre 2021] [Meng et al. 2025] [Meyer 1938] [Miller and McNamara 2018] [Min et al. 2013] [Mishra and Gogulapati 2022] [Mishra and Gogulapati 2023] [Morito and Sidwell 1967] [Munk et al. 2016] [Murphy and Rubesin 1965] [Nakamura-Zimmerer et al. 2023] [Napolitano et al. 2001] [Nasir et al. 2026] [Neel 1958] [Neumann and Freeman 2012] [Neumann et al. 1978] [Niu et al. 2012a] [Nix 1959] [North 1983] [Novara et al. 2009] [ONeal 1960] [Ostoich et al. 2013] [Otter 1986] [Ren et al. 2021] [Sakata and Davis 1977] [Sheldon 1967] [Spiridakos et al. 2020] [Piccolo Serafim et al. 2025] [Pish et al. 2019] [Polli et al. 2006] [Polli et al. 2008] [Pond et al. 1971] [Poudel et al. 2026] [Pourtakdoust and Fazelzadeh 2005] [Priolo et al. 1991] [Quan et al. 2021] [Rallabhandi and Mavris 2003] [Ran et al. 2019] [Raue and Timmer 2013] [Readshaw 1961] [Reddy 1993] [Ried 1964] [Riley and Smarslok 2017] [Riley et al. 2019] [Riley et al. 2023] [Riley et al. 2026] [Roach and Froning 1996] [Rodgers 1992] [Rom et al. 1970] [Rosner and Cibrian 1974] [Rumsey and Lee 1958] [Rumsey and Lee 1961b] [Rumsey and Lee 1961a] [Sadagopan et al. 2020] [Sadagopan et al. 2021] [Sahoo and Peetala 2010] [Sakata et al. 1975] [Salmaniw and Browning 2025] [Sawyer et al. 1999] [Scala and Nolan 1960] [Schmidt and Mann 1996] [Schoneman 2019] [Schuelein 2015] [Schülein and Bornhöft 2012] [Selberg and Cronin 1985] [Sharifzadeh et al. 2014] [Shiau et al. 2012] [Shiryaev and Serebryansky 2022] [Shiryaev et al. 2023] [Shuttle Eleven Cove Aerodynamic 1978] [Simsek et al. 2016] [Skin-Friction-Work Recovery by Aerodynamic 1963] [Smith et al. 1972a] [Smith et al. 2021] [Song and Li 2014] [Song and Li 2015] [Spottswood et al. 2021] [Stainback and Weinstein 1967] [Stallings and Hartman 1981] [Stauffer 1964] [Stephens 1959] [Stone 1969] [Strass and Stephens 1957] [Su et al. 2013b] [Suchov et al. 2022] [Sununu 1970] [Supersonic Transport Wing Minimum 1992] [Swanson 1958] [Swanson and Rumsey 1956] [Tamada et al. 2010] [Tanzer 1982] [Tashakkor et al. 2011] [Thawait et al. 2023b] [Thawait et al. 2023a] [Thawait et al. 2024b] [Thawait et al. 2024a] [Thomas et al. 2022] [Thornton et al. 1990] [Truitt 1968] [Trussell and Weidman 1960] [Tuten et al. 2025] [Udrescu and Surace 1999] [Uemura 1960] [ul Islam Rizvi et al 2015] [Vajda 1987] [Vargas Venegas and Huang 2021] [Vargas Venegas and Huang 2022] [Vargas Venegas and Huang 2023] [Vincent et al. 2009] [Vincent et al. 2010] [Vio et al. 2018] [Volkov 2023a] [Vosteen 1960] [Wan et al. 2014] [Wan et al. 2025a] [Wang et al. 2023a] [Wang et al. 2026a] [Wang et al. 2026c] [Way et al. 2024] [Weinstein et al. 1975] [Weinstein et al. 1981] [Wells 1991] [Wenkai et al. 2017a] [Weston and Cesnik 2024] [Wieting 1989] [Wilcox et al. 2009a] [Wilcox et al. 2009b] [Wilcox et al. 2010] [Wilder et al. 2007] [Wing 1970] [Wing 1972] [Wing 1973] [Wittliff 1982] [Wolfe 1964] [Wood 1961] [Wurster and Stone 1993] [Xie et al. 2019b] [Xie et al. 2020] [Yakubayev et al. 2026] [Yang et al. 2017] [Ye et al. 2019b] [Zanj et al. 2017] [Zeng et al. 2012] [Zhang et al. 2017b] [Zhang et al. 2021e] [Zhang et al. 2022c] [Zhang et al. 2026a] [Yue and Hai-rong 2012] [Zhao et al. 2011] [Zhao et al. 2022f] [Zhuo et al. 2019]

Ballistic missiles, interception and glide vehicles

The competitor and the defender. Ballistic missile trajectories and their prediction, boost-glide and hypersonic glide vehicles, interception and midcourse and terminal guidance. 114 titles name a glide vehicle or a glide trajectory, and 37 of those predict, track, detect or intercept one, which is the exposure argument of the review above running in reverse.

369 records. [Abate and Klomfass 2005] [Alexander 2024] [Ali and Sartuk 2003] [Anderson 1958] [Apochkina et al. 2025] [Arbic et al. 1953] [Arthur and Kemp 2025] [Asad et al. 2020] [Audric et al. 2023] [Baba et al. 1991] [Balbirnie et al. 1975] [BALLISTIC MISSILE and AEROSPACE 1961] [Ballistic Missile and Space 1960] [BALLISTIC MISSILE and SPACE 1960] [Ballistic Missile Defence 2009] [Ballistic Missile Defence 1986] [8 Ballistic Missile Defense 2020] [Ballistic Missile Defense BMD 2017] [Ballistic Missile Early Warning] [Stocker 2004] [Ballistic Missile Flight Testing 1981] [Ballistic Missile Fundamentals 2006] [Banerjee 2019] [Barnett 1970] [Barr et al. 2026] [Bartone et al. 2001] [Bartone et al. 2002] [Baucom 1995] [Beissner et al. 1986] [Bezick] [Bollino et al. 2006] [Bolt 1981] [Bonavita et al. 2026] [Bonney 1960] [Bose 1979] [Brockmann and Stefanovich 2022] [Brooks 1961] [Bullard 1963] [Buontempo 2015] [Burns 2020] [Butler et al. 2022] [Butler et al. 2023] [Cai and Zhuang 2025] [Cai et al. 2026] [Camacho et al. 2007] [Candler and Leyva 2022] [Cangelosi et al. 2024] [Carter 1972] [Chapman and Kirk 1974] [Chen 2017] [Chen and Zhou 2014] [Chen et al. 2010c] [Chen et al. 2016a] [Chen et al. 2016c] [Chen et al. 2018a] [Chen et al. 2020e] [Chen et al. 2020d] [Chen et al. 2020f] [Chen et al. 2021c] [Chen et al. 2025g] [Cheng 1965] [Cheng 1966] [Cheng et al. 2019] [Cheng et al. 2021a] [Cho 2023] [Choi and Kim 2026] [Church and Taylor 1959] [Cicolani et al. 1983] [Clark 1999] [Coffee and Maganty 1996] [Conclusion 2020] [Coupled Dynamic Model 2018] [Cui et al. 2023b] [Das et al. 2009] [Electrical Engineering, NIT, Agartala, India) and Debnath 2016] [Delsasso et al. 1948] [Dendy et al. 2026] [Deng 2026] [Deng and Zhao 2026] [Deng et al. 2016] [Differential Game-Based Interceptor Missile 2016] [Ding et al. 2024] [DoD Office of Inspector General 2012] [Dong and Cai 2017] [Dong et al. 2021] [Dong Gwan Lee et al. 2015] [Doronzo 2026] [Du et al. 2026] [Dudush and Snovydovych 2026] [Dunmire and Lopresti 1963] [Dupuis 1988] [Elias and Knutson 1995] [Elmelhi 2013] [Fallon and Lyles 2011] [Fan et al. 2016] [Fan et al. 2017b] [Fan et al. 2021] [Fang et al. 2024b] [Faulkner 1961] [Faulkner and Ward 1961] [Feng and Zhang 2016] [Feng et al. 2017] [Ficarrotta 2001] [Fowler] [Fowler 1998] [Fowler and Tapley 1965] [Friedman and Reed 1964] [Froning et al. 1996] [Frühling 2025] [Fye 1966] [Gadalla et al. 1993] [Gainor 2013] [Gao et al. 2018a] [Gao et al. 2020b] [Garg and Nagla 2019] [Gates and Cutting 1963] [Gottlieb et al. 2024] [Gratt and McCowan 1993] [Guelman 2004] [Guelman and Golan] [Gulick and Miller 1982] [Guo et al. 2018a] [Hall 2019] [Han et al. 2014b] [Han et al. 2024] [Hanin 1983] [Hao and Yongqi 2024] [Harl 2008] [Harl and Balakrishnan 2010] [Harlin and Cicci 2007] [Hattis 1990] [He et al. 2013b] [He et al. 2016] [He et al. 2017] [He et al. 2025] [He et al. 2026] [Herrmann et al. 2025] [Horneman and Kluever 2004] [Hu et al. 2025] [Huang et al. 2016d] [Huang et al. 2017c] [Huang et al. 2018d] [Hull et al. 1983] [Humble 2024] [Hutchins and Pace 2006] [Ingenito 2021] [Iwakawa et al. 2015] [Jacot and Hellmers 1982] [Jaeger and Hemati 2025] [Jang and Park 2026] [Jasani 2020] [Jeon et al. 2026] [Jian-bo et al. 2017] [Jiang et al. 2022a] [Jianguo et al. 2016] [Jimmerson and Dall 2000] [Jing Zhang et al. 2015] [Johnson and Mosely 1964] [Joshi and Jiss 2011] [Kamalvand et al. 2004] [Каплюк and Honcharenko 2026] [Kashiwagi 1968] [Kennedy 1995] [Kim et al. 1996] [Kim et al. 2011a] [Kim et al. 2016] [Kitsios and Lygeros] [Kluever 2007] [Kluever 2022] [Kluever and Horneman 2005] [Kluever et al. 2009] [Koelle 1993] [Kulhánek 2019] [Kumar et al. 2012] [Kumar et al. 2018] [Kurilova and Li 2026] [Lee et al. 2015a] [Lei et al. 2017] [Levinson et al. 2002] [Lewis 2017] [Li 2021] [Li and Cui 2009] [Li et al. 2012c] [Li et al. 2013a] [Li et al. 2016e] [Li et al. 2018g] [Li et al. 2021b] [Li et al. 2022b] [Li et al. 2023d] [Li et al. 2024h] [Li et al. 2025g] [Li et al. 2025j] [Li et al. 2026a] [Li et al. 2026k] [Li et al. 2026b] [Liang et al. 2025] [Lijewski 1980] [Lin 2003] [Liqun et al. 2017] [Liu and Shen 2015] [Liu et al. 2016d] [Liu et al. 2021b] [Liu et al. 2022b] [Liu et al. 2023j] [Liu et al. 2025m] [Liu et al. 2025g] [Lloyd and Brown 1979] [Lock et al. 2025] [Lu et al. 2005] [Lu et al. 2006] [Lukacs and Yakimenko 2007] [Lukens et al. 1961] [MacPherson 1963] [Madigan 1969] [Madigan 1970] [Makeich and Kryukov 2018] [Marquet 1986] [Mason 2009] [Meng et al. 2021] [Merkulov et al. 2025] [Mermagen 1964] [Miwa and Imado 1985] [Model of a Radar 2024] [Mondal and Padhi 2018] [Montero Yéboles] [Morgan 1971] [Naveh and Lorber 2001] [Nesline 1978] [Nesline 1979] [Nesline and Nesline 1986] [Nesline and Zarchan 1979] [Nesline and Zarchan 1980] [Nesline and Zarchan 1982b] [Newsham 2020] [Olsen 2011] [Ostner 1962] [Padhi et al. 2010] [Pan et al. 2025b] [Paschal et al. 2001] [Pella 2018] [Pelosi and Honeycutt 2017] [Pengjun and Zhengliang 2021] [Peter et al. 2013] [Petersen et al. 2013] [Piet-Lahanier and Serre 2017] [Pinto et al. 2023] [Pollack 2011] [Prabhakar et al. 2013] [Qu et al. 2024] [Rataczak et al. 2023] [Rataczak et al. 2024] [Rauch 1957] [Ren et al. 2023] [Rishel 1967] [Rizvi et al. 2017] [Robinson 1955] [Rogers and Slegers 2012] [Rogers and Slegers 2013] [Rong Huang et al. 2015] [Rounds 1987] [Russell 1964] [Sakata 2002] [Sanfilippo 1977] [Sasoh et al. 2010] [Schaff et al. 2000] [Scher and Dunavant 1966] [Scherberg and Rubin 1953] [Schouler et al. 2021] [Schweppe 1964] [Selected Ballistic Missile Programs 2008] [Seo and Park 2025] [Sethi 2025] [Sharma and Richards 2004] [Sheporaitis et al. 1976] [Shi et al. 2023] [Shima and Golan 2008] [Shima et al. 2000] [Shima et al. 2002] [Shinar et al] [Shiraishi and Yamasaki 2020] [Shneydor 1998] [Pollack 2010] [Shu-Ping and Zhi 2011] [Slifka 1960] [Smirnov 2019] [Snyder et al] [Srivastava and Srivastava 1997] [Stoner 1972] [Strohm 2011] [Su et al. 2021] [Su et al. 2024] [Sun 2026] [Sun et al. 2024a] [Sun et al. 2025b] [Sun et al. 2026c] [Sun et al. 2026b] [Sviestins] [Syring 2015] [Takehira et al. 1997] [Takehira et al. 1998] [Tanno et al. 2013] [Tanriverdi and Cavdaroglu 2017] [Taur 2013] [Tewell 1984] [The Aegis Ballistic Missile 2010] [Theater ballistic missile defense 2020] [Tiwari and Detroja 2024] [Tiwari and Detroja 2025] [Tong et al. 2026] [Vinh et al. 1998] [Viswanath et al. 2015] [Wall 1983] [Walsh and Wartburg 1978] [Walter et al. 2013] [Wang 2019b] [Wang and Zhang 2018] [Wang et al. 2013g] [Wang et al. 2016c] [Wang et al. 2017l] [Wang et al. 2018g] [Wang et al. 2022e] [Wang et al. 2024m] [Waugh 1998] [Wei-wei et al. 2013] [Weidong et al. 2015] [Welberg et al. 2015] [Werrell 2000] [Wheelon 1959] [Whitcombe 1961] [Williams et al. 1988] [Williams et al. 2024] [Williamson et al. 2026] [Wu et al. 2015a] [Wu et al. 2020b] [Wuju et al. 2011] [Xie et al. 2021] [Xu and Tang 2010] [Xu et al. 2020a] [Xu et al. 2022b] [Xu Mingliang et al. 2010] [Yan and Wang 2012] [Yan et al. 2017a] [Yang et al. 2011] [Yang et al. 2026d] [Yao et al. 2023] [York and Pastrick 1976] [Yu et al. 2015a] [Yu et al. 2022c] [Yuan et al. 2026a] [Yuyan and Peikang 2006] [Zang et al. 2025a] [Zang et al. 2025b] [Zhai and Yang 2020] [Zhang et al. 2014a] [Zhang et al. 2022j] [Zhang et al. 2022g] [Zhang et al. 2022k] [Zhang et al. 2022b] [Zhang et al. 2023h] [Zhang et al. 2024e] [Zhang et al. 2025a] [Zhang et al. 2026k] [Zhao et al. 2024c] [Zhao et al. 2025d] [Zheng et al. 2005] [Zhou et al. 2026] [Zhuo et al. 2023] [Zope et al. 2026] [Ünal et al. 2025]

Autopilots, servomechanisms and flight control

The inner loop that closes before guidance can. Missile and aircraft autopilots, gain scheduling, servomechanisms, inertial stabilised platforms and flight control laws.

368 records. [Abd-elatif et al. 2016] [Adams et al. 1992] [Adaptive Neural Network Based 2016] [Akmeliawati and Mareels 2007] [Ali and Wang Qing 2008] [Alsaraj and Stuffle 2015] [Anli Shang et al] [Anli Shang et al] [Apostolakis and Jordan] [Application of Improved L/sub 1999] [Awad and Wang 2016] [Bahambari and Khankalantary 2023] [Bahrami et al. 2008] [Bai et al. 2017] [Bao et al. 2019] [Barker and Balas 1999] [Basha and Swarup 2017] [Beh et al. 2018] [Behrouz et al. 2021] [Berk Gezer and Kutay 2014] [Bheemaiah 2019] [Biannic and Apkarian 1999] [Bibel and Stalford 1991] [Blair et al. 1978] [Blumel and White] [Bo and Jun 2014] [Bryson and Gruenwald 2022] [Bu et al. 2025] [Bucy 1979] [Bullock and Fields 1998] [Buschek 1999] [Buschek 2001] [Buschek 2003] [Buschek and Buschek 1997] [Butler and Pastrick 1983] [Buzantowicz 2019] [Byoung-Mun Min et al. 2007] [Dees and Moua 2010] [Draper et al. 1965] [Cai 2014] [Cairns 1970] [Calhoun 2000] [Campbell et al. 2009] [Chao et al. 2009] [Chaves Barbosa and Silvestre 2025] [Chen et al. 2010b] [Chen et al. 2018c] [Chen Xianxiang et al. 2012] [Ching-Fang Lin et al] [Chomachar and Fard 2016] [Chowdhury and Keshmiri 2024] [Chu Zhongyi et al. 2010] [Chun-Liang Lin 2002] [Coakley] [Cole and Abramovitz 1952] [Corban et al. 2001] [Culp and Bickley 1993] [D’Amato and Bernstein 2012] [Dai et al. 2017] [Das et al] [Davies and Haines 1965] [Davison et al. 1997] [Deng et al. 2013] [Deng et al. 2020] [Design of Missile 2016] [Devaud et al] [Devaud et al. 1999] [Do] [Dong et al. 2009] [Duan Chao-yang et al. 2010] [Dynamic Scheduling of Modern-Robust-Control 1992] [Ebner 1977] [Eguchi et al. 1999] [El-Sheikh 1998] [El-Sheikh and Bahgat] [Etzweiler 1969] [Evans 1957] [Fagin et al. 1969] [Fan and Su 2010] [Fan et al. 2010] [Fan et al. 2017a] [Farahmandi and Reitz 2024] [Farret et al. 2002] [Feng Tan et al. 2006] [Ferreres and M’saad 1994] [Ferreres and M’Saad 1995] [Fields and Bullock 1996] [Forkun et al. 2020] [Frasier and Gardiner 1965] [Friang et al. 1996] [Full Envelope Missile Longitudinal 2000] [Gao et al. 2021d] [Gao et al. 2021b] [Gao et al. 2021c] [Gido et al. 1974] [Gopmandal and Ghosh 2019] [Gresham et al. 2022] [Gully and Skelley 1975] [Guoxiang Gu et al] [Gutman 2005] [Hageman et al. 2003] [Hall and Shtessel 2005] [Hanisch 1967] [Harcaut et al. 2001] [Harl et al. 2010] [Hart 1956] [Haskins 2000] [Hattenberger et al. 2023] [He et al. 2015a] [Higher-Order Sliding Modes 2016] [Hindman and Shell] [Hindman and Shell] [Hiret et al. 1998] [Hirokawa et al. 2001] [Ho Chul Lee et al] [Holley et al. 1976] [Hu et al. 2013a] [Hughes et al] [Hull and Zhihua Qu 1997] [Hyde and Cleminson 2004] [Iglesias and Urban 1999] [Жукова 2022] [Integrated Guidance and Control 2016] [Jackson 1990] [Jackson 1992] [Jacob et al. 2023] [Jafarov and Tasaltin 2001] [Grauer 2020b] [Grauer 2021] [Jeffrie and Rolston 1972] [Jiang and Lin 2016] [Jie et al. 2006] [Johnson 1971] [Juang et al] [Junaid R and Beebi M 2015] [Kada 2011] [Kada 2015] [Kantue 2017] [Kaufman 1976] [Khodadadi et al. 2011] [Kiehn 2020] [Kim and Song 1998] [Kim et al. 2004c] [Kissel and Hadaegh 1993] [Klenke 2006] [Kotob and Kaufman 1974] [Kotob and Kaufman 1975] [Kuba and Kazda 1958] [Kurnaz et al] [Kurten 1975] [Liu and Tian 2019] [Mabius and Kaufman 1976] [Lawrence et al. 1998] [Lebell 1956] [Lebsock 1980] [Lee] [Lee and Choi 2005] [Lee and Singh 2026] [Lee et al. 2004] [Lee et al. 2025a] [Leondes and Nakano 1966] [Letty and Jang 1997] [Lhachemi et al. 2016b] [Li and Hullender 1998] [Li and Zhang 2021] [Li et al. 2013d] [Li et al. 2013c] [Li et al. 2019b] [Li et al. 2025a] [Li et al. 2026e] [Lian et al. 2013a] [Liao and Bang 2022] [Licata 1990] [Lin] [Lin and Fan 2009] [Lin and Hwang 2003] [Lin and Lee 1984] [Liu 2018] [Liu et al. 2016b] [Liu et al. 2017f] [Liu et al. 2017c] [Liu et al. 2023b] [Lu et al. 2018b] [Luo et al. 2016] [Lv et al. 2019] [Mahdianfar and Prempain 2016] [Mao et al. 2017] [Marchetti Tavares and Waldmann 2021] [Maria-Agneta and Stef 2011] [Marstrander and Lueg 1969] [Mathavaraj and Padhi 2020] [Maulani et al. 2026] [McClelland et al. 2025] [McFarland and Calise 1996] [McFARLAND and D’Souza 1995] [McLain and Beard 1998] [McLain and Beard 1999] [McMaster and Schenk 1973] [Mehrabian and Roshanian] [Menon and Ohlmeyer 2001] [Menon et al. 1997] [Menon et al. 1999] [Mettler and Hadaegh 1992] [Meyer and Smith 1992] [Michael A. Bolender 2006] [Mickle and Zhu] [Mickle and Zhu] [Ming Xin and Balakrishnan] [Missile Autopilot Design Based 2017] [Missile Autopilot Design Using 2004] [Missile Guidance and Control 2004] [Mitsutomi 1958] [Mohamed and Yan 2016] [Moon et al. 2012] [Morani et al. 2026] [Moul 1953] [Mracek et al. 1997] [Mufti and Muchallil 2017] [Nesline and Zarchan 1982a] [Nesline et al. 1979] [North American Aviation INC LOS Angeles CA 1963] [Oosterom and Babuska] [Optimal Disturbance Rejection 1992] [Optimization and Simulation 1979] [Ostgaard 1962] [Ouda 2017] [Pain and Tiwari 2013] [Pal et al. 2014] [Parkhi et al. 2010] [Parkinson et al. 1973] [Passera 1951] [Peng et al. 2017] [Petersen et al. 2000] [Porter and Manganas 1986] [Price 1970] [Prochazka 2026] [Pérez and Rubio 2001] [Quinter 1970] [Raimbault et al. 2001] [Rajagopal and Balakrishnan 2012] [Ravanbod and Noll 2012] [Ravanbod and Noll 2014] [Reichert] [Reichert 1989] [Reis et al. 2018a] [Reis et al. 2018b] [Rickard 1978] [Robust Autopilot Design 2016] [Rogalski 2018] [Rogalski et al. 2020] [Rogalski et al. 2021] [Ruimin et al. 2015] [Ruth 1989] [Sadr and Momeni 2011] [Salamci and Gökbilen 2007] [Sankar et al. 2016] [Sato 2013] [Saussié et al. 2008] [Schumacher and Khargonekar 1997] [Schumacher and Khargonekar 1998] [Schumacher and McClamroch] [Screenuch et al. 2006] [Seaberg 1950] [Seaberg and Smith 1951] [Seigler et al. 2004] [Sells 2015] [Senkel et al. 2013] [Seo et al. 2018b] [Shah et al. 2010] [Shamma and Cloutier] [Shamma and Cloutier 1992a] [Shamma and Cloutier 1993] [Shen and Ma 2022] [Shijie and Hang 2015] [Shkolnikov et al. 2000] [Shtessel] [Shtessel] [Shtessel 2001] [Shtessel and Krupp] [Shtessel and Krupp 1997] [Shtessel and Tournes 2012] [Shtessel et al. 1997] [Shtessel et al. 2000] [Shue et al. 1996] [Shumaker and Brown 2009] [Siguerdidjane and Devaud 2000] [Singh 2016] [Sitomer et al. 1999] [Slivinsky and Patumtawapibal 1980] [Smith and Meyer 1990] [Song et al. 2013] [Sperry Gyroscope Co Great Neck Ny 1963b] [Speyer 1997] [Sreenuch et al] [Steer 2003] [Stephens and Ridgely 1995] [Stilwell 2001] [Sui et al. 2008] [Sun and Liu 2009] [Sun et al. 2023] [Tabatabaei et al. 2010] [Tahk et al] [Talole et al. 2004] [Test Techniques for Flight 2021] [Thai et al. 2020] [Thai et al. 2023] [Theis et al. 2015] [Theodoulis and Duc 2007a] [Theodoulis and Duc 2007b] [Theodoulis and Duc 2008] [Theodoulis and Duc 2009] [Theodoulis et al. 2015] [Tischler 2018] [Tiwari et al. 2018] [Tournes and Johnson 1998b] [Tsai and Lin 2006] [Tsourdos 1998] [Tsourdos and White 2002] [Tsourdos and White 2012] [Tsourdos et al. 2006] [Urban et al] [Wang and Qi 2013] [Wang and Shan 2020] [Wang and Wang 2009] [Wang et al. 2008] [Wang et al. 2017k] [Wardana et al. 2021] [Weil and Wise] [Weinstein et al. 2018] [Weng and Shi 1999] [White et al] [White et al] [Williams 2004] [Wise 1989b] [Wise 1989a] [Wise 1990a] [Wise 1990b] [Wise 2007] [Wise and Deylami 1991] [Wise and Hamby] [Wise and Nguyen] [Wise and Sedwick 1994] [Wise and Sedwick 1995] [Wise et al. 1990] [Won et al. 2011] [Wu et al. 2002b] [Xieyu et al. 2022] [Xin and Balakrishnan 2003] [Xu et al. 2021b] [Yamada and Hasegawa 1999] [Youngblood 1977] [Yu et al. 2010a] [Yu et al. 2011] [Yuan and Wu 2016] [Yuan et al. 2016] [Zaher et al. 2010] [Zarovsky 1951] [Zhang et al. 2021i] [Zhang et al. 2025c] [Zhao and Tang 2012] [Zhao et al. 2018] [Zheng et al. 2023] [Zhong and Xiaohong 2008] [Zhou et al. 2010] [Zhu and Mickle] [Zichen Zhu et al] [Zimpfer 1999] [ÇLimen 2011]

Inertial navigation systems and their mechanisation

The navigator as a system. Inertial navigation and guidance systems, strapdown and gimballed mechanisations, aided and integrated navigation, and the histories and textbooks of the field.

353 records. [A Method for Determining 1979] [A Study 1968] [Adams 1956] [Adams 1960] [Adams and Hadfield 1983] [Agarwal and Xu 2026] [Wyatt and Tooley 2013b] [Alexander 1969] [Alikiotis 1987] [Amacker 1967] [Amacker and Graff 1965] [Andreev 1964] [Bai and Zhang 2014] [Bai et al. 2015] [Bar-Itzhack 1993] [Bar-Itzhack and Berman 1987] [Barun and Ozkazane] [Basic Principles of Strapdown 2004] [Bell 1967] [Berg 1965] [Beukers 1973] [Bevington and Marttila] [Beyond GNSS 2025] [Bhanu and Roberts 1992] [Bjorkman 1987] [Blois and O’Keefe 2025] [Blutreich et al. 1969] [Bobick and Bryson 1972a] [Bobick and Bryson 1972b] [Bogdanov and Fomichev 2018] [Boichuk 1968] [Bonnabel et al. 2006] [Borodacz and Szczepański 2023b] [Bortz 1970] [Bostick and Miletich] [Bozeman et al. 2022] [Braasch 2016] [Britting 1968] [Britting 1969c] [Britting 1969b] [Britting 1971b] [Brodersen 1970] [Brodersen 1972] [Burns 1963] [Burrows 1967] [Burrows 1971] [Casey] [Catena et al. 2013] [Centaur in Retrospect 1968] [Chang et al. 2009b] [Chang et al. 2024b] [Chapter 6. Piloting 2012] [Chatfield 1997] [Chelnokov 2019b] [Chen 2026] [Cheng et al. 2013b] [Chub 2014b] [Chub 2014a] [Cojuhari 2024] [Cole and Glossbrenner 1974] [Collinson 1973] [Condomines 2018] [Cox 1978] [Crawford 1970] [Creamer et al. 1984] [Creed and Hughes 1971] [Crocoll et al. 2013] [Damerius and Jeinsch 2019] [Daniel et al. 1968] [Dasari 2026] [Davis 1995] [Deng et al. 2014] [Deng et al. 2019c] [Draper 1963] [Draper 1981] [Duan and Cao 2021] [Duncan 1958b] [Duncan 1958a] [Duncan 1968] [Dushman and Sandberg 1973] [Dynamic Errors in Strapdown 1971] [Edwards 1971] [Ermakov and Gogolev 2021] [Ermakov and Gogolev 2022] [Outamazirt et al. 2013] [Farrell 1966] [Farrior 1962] [Fedotov and Perepelkina 2019] [Fegley 1965] [Fegley 1967] [Feng 2018] [Fernandes von Huelsen] [Ferranti’s Lightweight Inertial Platform 1964] [Fesenko et al. 2023] [Fitzgerald and Shapanka 1979] [Fowler 1990] [Fu et al. 2014a] [Fukushima 2018] [Fundamental Principles and Historical 2004] [Fundamentals of Inertial Navigation 2020] [Fundamentals of Satellite 2000] [Fundamentals of Satellite 2006] [Gage 1998] [Gates and Shipp 1977] [Gelb and Sutherland 1970] [Geller 1968] [Geohagan et al. 2018] [George and Sukkarieh 2007] [Gilmore 1968] [GNSS-Aided INS 2022a] [GNSS-Aided INS 2022b] [GPS Aided Inertial System 2007] [Grammatikos 1965] [Greenspan 1995] [Guan et al. 2018a] [Gully 1976] [Guo et al. 2026c] [Guo Yi et al. 2007] [Hadfield 1980] [Harrison et al. 1971] [Hayes 1968] [Heck et al. 1982] [Heck et al. 1984] [Hellman 1962] [Hirshon 1964] [Hongyang He et al. 2015] [Hruby et al. 1986] [hua and yan 2018] [Huang et al. 1990] [Huang et al. 2016c] [Huang et al. 2018a] [Humphrey and Humphrey 1997] [Hyzhnyak and Chernyak 2024] [Ignagni 1972] [Ignagni 2021] [Ignagni 2025] [Imazu and Kawamoto 1975] [Inertial Guidance 1964] [Inertial Guidance 1993] [Inertial Navigation Sensors 1999] [4 Inertial Navigation System 2001] [4 Inertial Navigation System 2023] [Arvind Suthar et al. 2024] [Inertial Navigation Systems 1986] [Inertial Navigation Systems 2006] [Wyatt and Tooley 2013c] [Inertial Navigation with External 1997] [Integrated Navigation Systems 2004] [Introduction and Overview 2022] [Ivanov 2015] [Jah et al. 2007] [Jankowski 1970] [Jekeli 2023] [Jia-qiang Xu et al. 2010] [Jianbin Zhang and Yu Zhang 2012] [Jiang et al. 2017a] [Jianhua et al. 2019] [Juang and Yu 2016] [Kaertner 2006] [Kallinen et al. 2020] [Kaplan 1996b] [Karp et al. 2003] [Kayton 1962] [Killingsworth 1968] [Kim et al. 2004b] [Kimishima et al. 2023] [King 1997] [King 1998] [Kline and Vangraas 1990] [Koifman and Bar-Itzhack 1999] [Koifman et al. 1995] [Kowalczyk and Chorzępa 2020] [Kriegsman et al. 1977] [Kuhn] [LaBatte 1964] [Landherr and Klein 1987] [Lardas 1989] [Larson 1965] [Latham and Richards 1977] [Lawrence 1993b] [Lee 1964a] [Lee 1974] [Lee 1976a] [Lenoble et al. 2023] [Leondes 1970] [Li et al. 2016d] [Liao et al. 2014] [Libero and Klein 2026] [Liu 2013] [Liu et al. 2012a] [Liu et al. 2013a] [Liu et al. 2017b] [Liu et al. 2020c] [Liu et al. 2022c] [Liu et al. 2025d] [Longstaff et al. 1992] [Lowry 1966] [Lyu et al. 2024b] [Markley 1982] [Marti] [Mattin 1968] [Maybeck 1973] [McCall 1998] [McKinlay 1975] [McNally et al. 1992] [Merhav 1979] [Meyer and Rozelle 2012] [Meyers and Weiderman 1988] [Miller and Sitomer 1968] [Ming et al. 2016] [Lukyanov 2025] [Mohamed and Mamatas 2012] [Morgan et al. 1974] [Nagaoka 1992] [Napjus 1974] [Napjus 1975] [Negrea 2021] [Nelson 1965] [Niemela 1982] [Noureldin et al. 2012a] [Noureldin et al. 2012b] [Nurse et al. 1978a] [Nurse et al. 1978b] [Olds 1998] [Optimization of the Update] [Otten 1966] [Ouyang and Wu 2022a] [Owen et al. 1997] [Palmer and McAllister 1962] [Panzieri et al] [Papa 2023] [Part I Inertial Navigation 1997] [Part Ii Inertial Navigation 1997] [Payne et al. 1975] [Pfeifer] [Poth and Elwell 1992] [Prizevoits 1961] [Qayyum and Kim 2021] [Qian et al. 2015] [Rander and Browning 2009] [Rapoport and Brandes 2010] [Reynolds 1967] [Rhyne 1980] [Ries and Dasari 2024] [Riley 1969] [Ritland and Spalding 1987] [Roberts et al] [Robinette and Witters 1982] [Rose 1989] [Rosenberg 1979] [Rosenfeld and Davis 1986] [Salwen and Arbour 1977] [Samuel] [Sargent 1970] [Schaechter and Ellis 1991] [Schmidt et al. 1973] [Sciegienny et al. 1978] [Scoville and Yamron 1966] [Sedov 1977] [Shro 1968] [Silver and Greenberg 1971] [Simon 1965] [Simon and Montenes 1966] [Simon and Sproull 1965] [Sineglazov and Zakharin 2012] [Skog et al. 2006] [Slater 1956b] [Slater 1956a] [Smith 1973] [Smith 1986] [Smith 2011] [Smith and Biezad 1986] [Snodgrass 1975] [Sokolov et al. 2022] [Soloviev 2008] [Soloviev et al. 2007] [Spalding 1989] [Sperry’s SGN-10 Inertial System 1964] [Starks 1974] [Statsinger 1959] [Stepanov et al. 2017] [Stevens 1958] [Stovner and Johansen 2019] [Strachan and Evans] [Strapdown Inertial Navigation Mechanism 2021] [Strapdown Navigation System Computation 2004] [Strapdown System Technology 2004] [Stratton 1963] [Sukenik 2004] [Sullivan 1994] [Sun and Wang 2012] [Sushchenko 2026] [Sushchenko and Melnyk 2026] [Sushchenko et al. 2024] [Swingle and Kang 1982] [Szelmanowski et al. 2019] [Tanıl et al. 2017] [Tazartes 2014] [The Inertial Navigation System 2007] [Thomas 1965] [Tiejun Qu et al] [Toda and Koike 2021] [Todić and Kuzmanović 2018] [Tooley and Wyatt 2024b] [Tooley and Wyatt 2024a] [Treder and Meldahl 1991] [Trifonov-Bogdanov et al. 2012] [Trotter 1957] [Truong and Nguyen 2024] [Upadhyay et al. 1990] [Vasconcelos et al. 2005] [Vasconcelos et al. 2006] [Vasilyuk and Tokarev 2020] [Vau et al. 2018] [Vinogradova et al. 2025] [Vovchenko 1966] [Vu et al. 2019] [Wagstaff and Kelly 2018] [Wang and Gu 2008] [Wang et al. 2012a] [Wang et al. 2019b] [Wang et al. 2026g] [Wanner and Hopkins] [Watson and Jackson 2002] [White 1960] [Widnall et al. 1982] [Wing 1965] [Wittry 1969] [Wolf and McCracken 1973] [Wrigley 1977a] [Wrigley 1977b] [Wu 2019] [Wu 2025a] [Wu 2025b] [Xin Ma et al] [Xu et al. 2014] [Yang et al. 2023a] [Yang et al. 2025a] [Yanling Hao et al. 2008] [Yeh et al. 2005] [Yong Jia et al. 2016] [Yoo et al. 2012] [Yuan-Hsi Cheng and Hung] [Zagone and Hesse 1965] [Zakharin and Ponomarenko 2023] [Zhang and Wang 2011c] [Zhang et al. 2017d] [Zhang et al. 2019b] [Zhang et al. 2026i] [Zhao et al. 2024b] [Zharkov et al. 2023] [Zhou and Liu 2009] [Zhou et al. 2021b]

Estimation, identifiability, observability and experiment design

The conclusion’s discipline. Identifiability, observability, optimal input and experiment design, and the estimation machinery of Kalman filtering applied to inertial navigation. 117 titles name identifiability and 42 observability, and the earliest dated identifiability title is of 1961, after the last X-10 flight of 1959.

335 records. [Abdelfattah et al. 2026] [Agüero and Goodwin 2006] [Agüero and Goodwin 2008b] [Agüero and Goodwin 2008a] [Aided INS 2022] [Sanketh 2012] [Alkhoury et al. 2017] [Anbu and Jayaprasanth 2019] [Andrade et al. 2025] [Andronikou et al. 1983] [Anguelova and Wennberg 2007] [Anguelova and Wennberg 2009] [Aoki 1966] [Appendix B 2006] [Arambel and Tadmor 1997] [August 2009] [Awin 2013] [Baker et al. 2011] [Baklanov and Dambeck 2017] [Banga and Balsa-Canto 2008] [Banks and Kunisch 1989] [Banyasz and Keviczky] [Bar-Itzhack 1989] [Bar-Shalom and Yang 1991] [Barczyk and Lynch 2011] [Batista et al. 2010] [Batista et al. 2013] [Battistelli and Tesi 2015] [Baumeister and Kunisch 1991] [Belforte and Gay] [Belforte and Gay 2003] [Ben-Ishai et al. 2001] [Ben-Zvi et al] [Berkane and Tayebi 2021] [Bistrovs and Klūga 2012] [Bittanti 1979] [Boland 1970] [Breakwell 1969] [Brock and Schmidt 1966] [Bryson and Mehra 1968] [Campregher et al. 2025] [Casini et al] [Casini et al. 2008] [Julian L. Center 1975] [Chappell et al. 1990] [Chapter 7 2024] [Chashnikova 2015] [Chavent 1985] [Chavent 1987] [Cheremisinoff 2020] [Chernodarov et al. 2022] [Chhajer and Roy 2023] [Chhajer and Roy 2024] [Chicone and Gerlach 1987] [Chin 1985] [Chu and Nguyen 2026] [Cole 2020a] [Cole 2020b] [Cole 2020c] [Contreras and Hajiyev 2017] [Courdesses 1983] [Courdesses and Amouroux 1983] [Courdesses et al. 1981] [Crassidis 2005] [Creagh et al. 2012] [Cui et al. 2021] [Danai et al. 2008] [De et al. 2025] [Delforge et al. 1987] [Delgado and Profos 1999] [Deng et al. 2026] [Denis-Vidal et al. 2003] [Denis-Vidal et al. 2019] [Development of Criterion 2015] [Diop and Kribs 1992] [Diop and Kribs 1993] [Dohyoung Chung et al] [Dreef et al. 2022] [Du et al. 2025] [Dufour et al. 2015] [Dunham et al. 1980] [Emery et al. 2000] [Erzberger 1967] [Esmaeilkhah and Landry 2025] [Fairfax et al. 2011] [Faruqi and Turner 2000] [Fayette et al. 2026] [Filyashkin 2018] [Finch] [Fisher 1961] [Flila et al. 2008] [Forgione et al. 2014] [Fosbury and Crassidis 2006] [Foss 1987] [Fourati and Prieur 2023] [Fu and Cheng 2023] [Fujimoto et al. 2018] [Gan and Liu 2023] [Gates et al. 1996] [Gevertz and Kareva 2023] [Giudici 1991] [Godfrey and DiStefano 1985] [Godfrey and DiStefano 1987] [Goldys and Maslowski 2002] [Golyakov et al. 2022] [Goshen-Meskin and Bar-Itzhack 1990] [Gottu Mukkula and Paulen 2017] [Gottu Mukkula and Paulen 2019] [Grauer and Boucher 2018] [Gross et al. 2010a] [Gro¨nstedt 2002] [Grubin 1973] [Haak 1994] [Hadaegh and Bekey 1987] [Hajiyev 2026] [Han and Kim 2011] [Hartana] [Heij 1992] [Heitzman-Breen et al. 2026] [Henry et al. 1989] [Henry et al. 1990] [Herget 1974] [Hildebrand and Gevers] [Hildebrand and Gevers 2002] [Hjalmarsson and Martensson 2007] [Hofmann 1977] [Hu et al. 2020c] [Huang et al. 2023b] [Huang Xiaokai et al. 2011b] [Hutchinson and Fagan 1973] [Hägg and Wahlberg 2015] [Identifiability of Initial Conditions 2015] [Inertial Navigation and Kalman 2018] [Iwase et al. 2005] [Iwase et al. 2006] [Jacquez 1991] [Jacquez and Greif 1985] [Jauberthie and Chanthery 2013] [Jauberthie et al. 2003a] [Jauberthie et al. 2003b] [Jauberthie et al. 2006] [Jauberthie et al. 2012] [Jauberthie et al. 2016] [Jauberthie et al. 2018] [Jetawatthana and Khamvilai 2026] [Jia-fan et al. 2011] [JiangHua et al] [Jianxin and Yongcbun 2004] [Jones 1970b] [Jung and Lee 2021] [Jung and Weiss 2021] [Jung et al. 2020] [Jungen et al. 2026] [Jwo et al. 2025] [Kalman Filter Inertial Navigation 1999] [Karabutov 2025b] [Karin et al. 2017] [Karlgaard et al. 2015] [Keesman 2015] [Kelly 1994] [Khartovskii 2005] [Kitamura and Nakagiri 1977a] [Kitamura and Nakagiri 1977b] [Kitamura and Nakagiri 1978] [Klein 1989] [Klein 1990] [Kobayashi 1980] [Koller et al. 2019] [Kothe and Hofer 1988] [Kulakova 2018] [Kumar et al. 2019] [Kunisch and White 1991] [Lacambre et al. 2013] [Lecca 2020] [Lecca 2024] [Lee and Herget 1975] [Lee and Nagati 1999] [Lee et al. 2012a] [Lesnic 2000] [Li and Zhang 2022] [Li et al. 2017f] [Li et al. 2018e] [Li et al. 2023l] [Liang et al. 2013] [Lill et al. 2019] [Lim et al. 2000] [Linder et al. 2014] [Liu] [Liu et al. 2016a] [Liu et al. 2025c] [Liu et al. 2025j] [Liu et al. 2026i] [Lomov 2011] [Lu et al. 2009] [Ludher et al. 2021] [Madyastha et al. 2011] [Mahboub and Mohammadi 2018] [Maskell] [McBurney] [McMichael and Blakley 2022] [Medrano-Cerda‡ and Pritchard 1988] [Mehra 1968] [Mithun IM et al. 2015] [Nakagiri] [Nakagiri 1997] [Nam] [Narasimhan and Rengaswamy 2008] [Neistat] [Nenarokomov et al. 1998] [Ng and Qureshi 1981] [Ng et al. 1977] [Nieminen et al. 2011] [Niu et al. 2012b] [Norton 1982] [Anderson and Deistler 1983] [Ober et al] [Oberpeilsteiner et al. 2016] [Oh and Johnson 2006] [Olivier and Smyth 2017] [Optimal experiment design for 2022] [Optimal input design] [Ostroumov and Kuzmenko 2016] [Ott] [Otter 1985] [Ozger 2013] [Pachwicewicz and Weremczuk 2018] [Papadimitriou and Argyris 2017] [Park and Himmelblau 1982] [Payne and Goodwin 1974] [Pilyugin and Shalgin 2024] [Point et al. 1996] [Prokhorov 1995] [Qi and Baker 2026] [Qian et al. 2014] [Rafajlowicz 1983] [Rafajlowicz 1984] [Ragel and Farooq 2005] [Raisinghani et al. 1999] [Rajchowski et al. 2016] [Ramakrishna et al. 2023] [Ramanandan et al. 2011] [Regularity and Strict Identifiability 2009] [Rhudy et al. 2024] [Richalet et al. 1991] [Rojas 2011] [Rothman et al. 2015] [Rudolph and Herrendörfer 1995] [Rusnak et al] [Rusnak et al. 1993] [Rúa et al. 2022] [Sabzevari et al. 2020] [Schrempf and del Re 2001] [Schwartz and Özbay 1990] [Sen 1983] [Serban and Freeman 2001] [Servotte] [Shaaban et al. 2024] [Shakhov 2013] [Shakhov and Koo 2017] [Shen and Zhang 2012] [Shen et al. 2018] [Shen et al. 2023] [Shin and El-Sheimy 2007] [Siddiqui et al. 2024] [Silva and Batista 2019] [Simpson and Baker 2026] [Slabospitskii 1993] [Song and Chen 2017] [Sontag 2016] [Sontag 2017] [Spetzler and Narang-Siddarth 2016] [St-Pierre and Gingras] [Staley and Yue 1970] [Stanhope et al. 2014] [Stanov 2026] [Stigter et al. 2003] [Stojanovic and Nedic 2016] [Selezneva 2024] [Sufleta 1982] [Sumi et al. 2025] [Sun and Sun 2015] [Sundara and Raju 2022] [Tavares and Oliveira 2024] [Меерович et al. 2026] [Telen et al. 2012] [Telny 2021] [Cantó et al. 2011] [Thompson et al. 2022] [Thowsen 1978] [Tien 2026] [Tse and Anton 1971] [Tse and Anton 1972] [Uosaki and Hatanaka 2005] [Uosaki et al. 2006] [van der Klauw et al. 1994] [Vaughn 1966] [Verma and Peyada 2018] [Vorchik 1987] [Wang and Wang 2025] [Wang et al. 2010a] [Wang et al. 2014a] [Wang et al. 2019i] [Wang et al. 2021i] [Wang et al. 2023e] [Weddig and Schön 2024] [Weerts et al. 2018] [Wells and Klein 1982] [Whipple and Hernandez-Vargas 2024] [Wu et al. 2022] [Xiao et al. 2020] [Xiaofang et al. 2014] [Xin et al. 2018] [Xiong et al. 2019] [Yang and Huang 2018] [Yang and Huang 2019] [Yang and Huo 2008] [Yi and Ferrer 2007] [Ying et al. 2025] [Yoko 2024] [Yong et al. 2023] [Yu and Bernstein 2016] [Yu et al. 2016a] [Yuan and Ljung 1984] [Yuan and Ljung 1985] [Yufei and Pingyuan 2006] [Zarrop 1979a] [Zarrop 1981] [Zeis et al. 1988] [Zhang et al. 2014c] [Zhang et al. 2021l] [Zhang et al. 2022d] [Zhang et al. 2026e] [Zhou et al. 2023a] [Zhou et al. 2023c] [Özger 2012]

Landing gear, brakes, arresting gear and decelerators

Where the fleet was lost. Landing gear dynamics and loads, brakes and tyres, arresting gear and barricades, and drag chutes and decelerators. 97 titles name shimmy, the directional instability of a gear on the runway.

334 records. [Abu-Akeel 1968] [Abu-Akeel 1969] [Abzug 1999] [Aircraft Tires 2022] [Aircraft Type Air Scoops 2002] [Aircraft Wheels Brakes 2022] [Airfield Compatibility 2022] [Alexander 1968] [Allen et al. 1962] [Allen et al. 1963b] [Alroqi et al. 2017] [Arık and Bilgiç 2022] [Atabay and Ozkol 2013] [Averyanov 2022] [Babish 1966] [Baird 2021] [Bakulin et al. 2016] [Barnes et al. 2007] [Bassett et al. 2017] [Batill 1982] [Batill and Bacarro 1988] [Billec 1967] [Black 1968] [Black 1976] [Blair 1981] [Blair 1985] [Blanchard 1963] [Blanchard 1964] [Boustani et al. 2022] [Brewer 1974] [Brooks and Dejarnette 1970] [Brown and Redwine 1948] [Brown et al. 2000] [Brunner and Nerem 1970] [Byrdsong 1973] [Cacciola and Calabria 2026] [Cai et al. 2024] [Cao and Wei 2020] [Cardoso Navarro and Sandoval 2019] [Carter and Nagy 1995] [Caruy Povoa et al. 2018] [Chaloff et al. 1974] [Champine 1976] [Chaudhary 2021] [Chen and Chen 2026] [Chen et al. 2010a] [Chen et al. 2018e] [Chen et al. 2022b] [Chen et al. 2025e] [Cheng et al. 2021c] [Chernenko and Burnashev 2022] [Chester 1995] [Chester 2002] [Chuban 2017] [Chuban 2019] [Clark 1974a] [Cockrell and Doherr 1981] [Collins and Black 1969] [Collins et al. 2025] [Cook 1985] [Cook 2013] [Couch 1975] [Creel and Miserentino 1971] [Currey 1988b] [Daughetee 1974] [Davidson 2015] [Davis and Lopez 1987] [Deiler and Fezans 2025] [Deitering and Hilliard 1965] [Deweese and McCarty 1973] [Dietrich et al. 1963] [Diltemiz 2021] [Ding et al. 2023] [Ding et al. 2026] [Di̇nç 2021] [Douglas Aircraft Co Long Beach Ca 1962] [DrAvico et al. 2018] [Dreher and Horne 1966] [Du et al. 2024] [Dunlop Limited 1972] [Durmuşoğlu 2026] [Earl 1967] [Eckstrom 1975] [Enright 1985] [Enright 2000] [Fang et al. 2024a] [Feld 1990] [Feng et al. 2015] [Feng et al. 2023] [Fields et al. 2011] [Fisher et al. 1978] [Fisher et al. 1979] [Forlifer et al. 1967] [French 1965] [French 1966] [Frisby 1960] [Furnish and Anders 1971] [Gallon and Witkowski 2015] [Gan et al. 2021] [Gao et al. 2020a] [Gao et al. 2022] [Gao et al. 2024c] [Gatt et al. 2017] [Gentric 1956] [Georgieva 2017] [Gibson et al. 1968] [Giridharan and Sivakumar 2022] [Goncharenko 2011] [Gordon 2002] [Gordon et al. 1998] [Graves 1977] [Greenland 2021] [Grossman 1980] [guo et al 2024] [Guo et al. 2025a] [guo et al 2025] [Haider 2020] [Halasey and Noll 1963] [Han et al. 2019] [He 2018] [He et al. 2018] [High-Speed Schlieren Movies 1960] [Hinchey 1968] [Horne and Leland 1962] [Horta et al. 1999] [Howcroft et al. 2013] [Howcroft et al. 2015] [Howell et al. 1990] [Hsu et al. 2022] [Huang 2019] [Huang and Zhang 2026] [Huntington and Lyrintzis 1996] [Irwin 1966] [Jackson 1965] [Jategaonkar et al. 1997] [Jiang et al. 2023b] [Jiang et al. 2023c] [Jiang et al. 2023d] [Jiang et al. 2025c] [Joscelyne and Young 2011] [Joyner 1969] [Joyner 1970] [Khot et al. 2025] [Luong et al. 2025] [McCarty et al. 1979] [McGehee 1985] [McGehee and Carden 1976] [McGehee and Dreher 1982] [Miller and Pinkel 1973] [Morris and McGehee 1983] [Niu et al. 2020] [Niu et al. 2024] [Pirooz et al. 2021] [Roithmayr and Pei 2024] [Ross 1980] [Sura and Suryanarayan 2023] [Kadam et al. 2018] [Kansas Univ Lawrence 1952b] [Kennedy and Lowry 1995] [Kim 2023a] [Klinar and Lee 1955] [Kocak and Ergenc 2023] [Kordes and McKay 1962] [Krabacher 1993] [Krabacher 1996a] [Krabacher 1996b] [Krabacher 1997] [Kraft et al. 1971] [Krainsk and Rosato 2001] [Krainski et al. 1997] [Krüger and Morandini 2011] [KrÜGer et al. 1997] [刘 2026] [Lee and Chiou 1994] [Lee and Swegle 1963] [Li and Zhao 2022] [Li et al. 2016f] [Li et al. 2017h] [Li et al. 2017c] [Li et al. 2021f] [Liu et al. 1998] [Liu et al. 2021d] [Liu et al. 2023c] [Liu et al. 2026g] [Lu et al. 2018a] [Mayer 2000] [McKay and Noll 1967] [McKay and Scott 1961] [McComb and Tanner 1988] [McGehee et al. 1978] [Meacham et al. 2013] [Medzorian 1999] [Meriwether and Harris 1962] [Metrikin and Peisel’ 2009] [Meyerson 2001b] [Meyerson 2001a] [Milwitzky and Cook 1953] [Modal Analysis 2018] [Mohammed Shibah 2026] [Moreland 1964] [Moskowitz and Soltis 1976] [Muppidi et al. 2018] [Mustashin et al. 2021] [Nan et al. 2026a] [Nan et al. 2026b] [National Advisory Committee 1935] [Nguyen et al. 2006] [Niederer and Mihora 1972] [Oh 2014] [Orlando 2020] [Oza et al. 2015] [Padmanabhan and Dowell 2015] [Paletta et al. 2013] [Paul and Paul 2023] [Pecora 2021] [Phillips et al. 1973] [Picard 2002] [Pilyugin and Khlebnikov 2005] [Pilyugin and Khlebnikov 2010] [Plakhtienko and Shifrin 2006] [Polutchko 1973] [Prado Pereira et al. 2021] [Pritchard 2001] [Qiang et al. 2012] [Ragsdale 2000] [Rahmani and Behdinan 2018b] [Rahmani and Behdinan 2018a] [Rahmani and Behdinan 2019a] [Rahmani and Behdinan 2019b] [Rahmani and Behdinan 2020] [Ramachandra et al. 2026a] [Ramachandra et al. 2026b] [Reusable Launch Vehicle Landing 2026] [Reuter 1973] [Ridha 1968] [Rogers 1972] [Romero 2021] [Ruan et al. 2023b] [Ruan et al. 2024a] [Ruan et al. 2024b] [Ruan et al. 2024c] [Sanches et al. 2021] [Sateesh and Maiti 2009] [Scher 1965] [Schmidt 2015a] [Schmidt 2021] [Scholz et al. 2026] [Sen 1990a] [Sen 1990b] [Sforza 2014] [Shi et al. 2025] [Sivrioglu 2023] [Some Current Types 1968] [Somieski 1997] [Spieck 2004] [Stachiw] [Stachiw et al. 2021] [Stowell et al. 1948] [Sun et al. 2024b] [Sura and Suryanarayan 2009] [Taherian 2026] [Tanner 1972b] [Tanner 1973] [Tanner 1974] [Tanner 1990] [Tartaruga et al. 2016] [Taylor et al. 2021] [Thies 2022] [Thompson and Horne 1959] [Thota et al. 2008a] [Thota et al. 2008b] [Thota et al. 2009] [Thota et al. 2010a] [Thota et al. 2010b] [Thota et al. 2012] [Titov and Serebryansky 2026] [Tourajizadeh and Zare 2016] [Turnbull et al. 1952] [Unorthodox Landing Gears 1988] [van Slagmaat 1992] [van Slagmaat 2004] [van Slagmaat 2026] [Wang 2022] [Wang and Cao 2026] [Wang and Carl 1999] [Wang and Wang 2013b] [Wang et al. 2022q] [Wang et al. 2023m] [Wang et al. 2024d] [Wang et al. 2024n] [Wang et al. 2024q] [Wang et al. 2026l] [Wang et al. 2026d] [Ward and Myers 1967] [Wasserman and Mitchell 1973] [Webster 1947] [Wei and Nie 2005] [Wei et al. 2026d] [Wei et al. 2026a] [Wei et al. 2026b] [Whalley 1973] [White and Macha 1991] [Wilson 1980] [Wu et al. 2025] [Xiang et al. 2022b] [Xiao et al. 2025] [Xing et al. 2020] [Xuan 2026] [Yager 1993] [Yager 1996] [Yager and Vogler 1989] [Yager et al. 1990] [Yager et al. 2002] [YangZhou et al. 2011] [Yi et al. 2010] [Yi et al. 2011] [Yntema and Milwitzky 1952] [Yıldırım Dalkıran and Kırteke 2024] [Zakrajsek et al. 2017] [Zhang et al. 2013a] [Zhang et al. 2018b] [Zhang et al. 2021m] [Zhang et al. 2021d] [Zhang et al. 2022f] [Zhang et al. 2023b] [Zhang et al. 2027] [Zhao et al. 2025f] [Zheng et al. 2026a] [Luo and Voronko 2023] [Zhou et al. 2024a] [Zhou et al. 2024b] [Zhu et al. 2025d] [Zhu et al. 2026b] [Çeliktaş et al. 2012]

Gravity, the deflection of the vertical and gravity-aided navigation

The error term no instrument removes. The deflection of the vertical and the geoid, gravity compensation in inertial navigation, gravity gradiometry, and navigation by matching a measured field to a map. 69 titles name the deflection of the vertical, and 90 concern matching a measured field against a map, 44 of those for an underwater or marine vehicle, which is where the field-matching method is now chiefly applied.

309 records. [Achilli et al. 1983] [Adams et al. 2021] [Affleck and Jircitano] [Ahmadian 2026] [Ai et al. 2023] [Akdoğan et al. 2024] [Albayrak et al. 2019] [An et al. 2021] [Anderson et al. 2000] [Annan et al. 2023] [Appendix F. Procecdure 1997] [Badekas and Mueller 1968] [Balakrishnan] [Barzaghi et al. 2016] [Bell 1971] [Bell et al. 1970] [Chen et al. 2023a] [Erol et al. 2023] [Nazan 2023] [Pfohl et al. 1988] [Sjoeberg 1977] [Stray et al. 2025] [Bernard 1989] [Bernstein and Hess 1976] [Bhattacharji 1970] [Bouman 2011] [Brammer 1979] [Brown 1975] [Brown 1983] [Loomis] [Brzezowski and Merenyi 1986] [Brzezowski et al] [Brzezowski et al. 1989] [Bu et al. 2026a] [Bużantowicz 2015] [Bénet and Guinamard 2026] [Griggs et al] [Cai et al. 2015] [Campbell 1963] [Chan et al. 1985] [Chen et al. 2011] [Chen et al. 2025a] [Chen et al. 2025d] [Chen et al. 2026a] [Chen et al. 2026c] [Chovitz and Fischer 1959] [Chunfeng et al. 2025] [Chunmei et al. 2017] [Colombo 1979] [Colombo et al. 1976] [Crocetto and Russo 1996b] [Crocetto and Russo 1996a] [Basil et al. 2021] [Da et al. 2022] [Da et al. 2023] [Dai et al. 2015] [Darling 1948] [DeBra and Breakwell 1986] [DeBra et al. 1981] [Deng et al. 2018] [Devote and Hart 2025] [Devyatisilnyi and Chislov 2012] [Edwards 1980] [Edwards 1982] [El Habiby and Sideris 2007] [Emel’yantsev et al. 2015] [Equations of Motion 1997] [Evaluation of Gravity Model 1997] [Fanming Liu et al. 2010] [Feasibility Study 1991] [Feature Selection Criterion 2016] [Fischer 1954] [Forsberg 1984] [Forward 1976] [Forward 1982] [Forward et al. 1973] [Gainer et al. 1984] [Ganeko 1976] [Ganeko 1977] [Gao and Zhao 2012] [Gao et al. 2021a] [Gao et al. 2024a] [Gloss et al. 1974] [Gloss et al. 1978] [Groten and Keller 1987] [Grubin 1979] [Hagiwara 1972] [Han et al. 2018a] [Han et al. 2018b] [Han et al. 2026d] [Hao et al. 2020a] [Harriman and Harrison 1984] [Hein et al] [Holland 1971] [Hopkins 1981] [Houston et al. 1969] [Howard and Kersh 1991] [Hsu] [Huddle 1978a] [Huddle 1978b] [Humphrey 1999] [Jekeli 1997] [Jekeli 2006] [Jekeli 2021] [Jekeli and Rapp 1980] [Jia et al. 2026] [Jordan 1986] [Kahn 1984] [Kahn and Englar 1987] [Kalaghan and Colombo 1978] [Kerr 2007] [Kling 1989] [Kohel et al. 2006] [Kuhar et al. 2010] [Kwon and Jekeli 2005] [Lambert and Darling 1938] [Lee et al. 2015b] [Li 2010] [Li et al. 2014c] [Li et al. 2018d] [Li et al. 2020c] [Li et al. 2020b] [Li et al. 2021h] [Li et al. 2024c] [Li et al. 2024d] [Li et al. 2025c] [Li et al. 2025l] [Li et al. 2026f] [Liu and Chang 2015] [Liu et al. 2014d] [Liu et al. 2022e] [Liu et al. 2022h] [Liu et al. 2025e] [Liu et al. 2026l] [Liu et al. 2026j] [Liu et al. 2026a] [Lorenzini et al. 1988] [Luce 1949] [Luo et al. 2022] [Ma and Wang 2019] [Ma et al. 2023a] [Madden 2010] [Mandour and El-Dakiky 1988] [Manoussakis and Korakitis 2020] [Mao et al. 2024] [Mao et al. 2025] [Martine 1983] [May et al] [Metzger 1977] [Metzger and Jircitano 1975] [Metzger et al. 1976] [Moody and Paik] [Moody et al. 1986] [Morgan and Paik 1988] [Morgan and Paik 1989] [Morozova et al. 2019] [Muller and Wesshaar 1994] [Needham and Braasch 2020] [Needham and Braasch 2022] [Obuchovski et al. 2014] [Odalović et al. 2018] [Paik 1981c] [Paik 1981b] [Paik 1981a] [Paik 1985] [Paik 1987] [Paik and Richard 1986] [Paik et al. 1988] [Pepe et al. 2014] [Peshekhonov 2020] [Brereton et al] [Qian et al. 2018] [Rahimi and Nikkhah 2021] [Rakholia et al. 2017] [Richeson and Pines 2007] [Robbins 1985] [Rose 1986] [Sabri et al. 2019] [Schreutelkamp and Hirt 2026] [Schutz 1988] [Schwarz 1978] [Schwarz 1981] [Shaw et al. 1969] [Shi et al. 2019a] [Shirron et al. 2010] [Shu 1989] [Silton and Coyle 2015] [Smiley and Horne 1957] [Soler et al. 2014] [Spaceborne Gravity Gradiometers. Part 1984a] [Spaceborne Gravity Gradiometers. Part 1984b] [Spaceborne Gravity Gradiometers. Part 1984c] [Spaceborne Gravity Gradiometers. Part 1984d] [Spearman and Driver 1959] [Stamenkovich and Carvil] [Su and Wang 2015] [Szabo 1962] [Taletović and Krdžalić 2017] [Talwani 1966] [Tang et al. 2015b] [Teskey 1982] [Tie et al. 2017] [Tie et al. 2018] [Tijing 1998] [Tong et al. 2012] [Trageser 1975] [Tu 1992a] [Tu 1994] [Vārna et al. 2023] [Wan and Yu 2014] [Wan et al. 2025b] [Wang 1988] [Wang and Cai 2022] [Wang and Cai 2023] [Wang and Wu 2014] [Wang et al. 2011e] [Wang et al. 2011d] [Wang et al. 2013d] [Wang et al. 2015b] [Wang et al. 2016f] [Wang et al. 2016e] [Wang et al. 2016b] [Wang et al. 2017f] [Wang et al. 2017c] [Wang et al. 2019j] [Wang et al. 2019a] [Wang et al. 2020f] [Wang et al. 2020b] [Wang et al. 2021c] [Wang et al. 2021f] [Wang et al. 2021h] [Wang et al. 2022k] [Wang et al. 2022d] [Wang et al. 2022f] [Wang et al. 2023b] [Wang et al. 2023c] [Wang et al. 2023o] [Wang et al. 2024l] [Wang et al. 2024e] [Wang et al. 2025d] [Wang et al. 2025a] [Wang et al. 2025k] [Wang et al. 2026i] [Watts et al. 1984] [Wei et al. 2017] [Weiner et al. 2020] [Welker et al. 2011] [Welker et al. 2013] [Wells and Breakwell 1980] [Wen et al. 2014] [Whiting 1996] [Wolf 1954] [Wright and Zissa 1984] [Wu et al. 2010b] [Wu et al. 2011a] [Wu et al. 2015b] [Wu et al. 2016] [Wu et al. 2017] [Wu et al. 2018a] [Xi et al. 2024] [Xi et al. 2025] [Xia et al. 2009] [Xia et al. 2026] [Xiong et al. 2007] [Xiong et al. 2013] [Xiong et al. 2014] [Xiong et al. 2015] [Xiong et al. 2018a] [Xu 2005b] [Yan and Cui 2007] [Yan and Wu 2007] [Yan et al. 2009] [Yan et al. 2023b] [Yang et al. 2013] [Yang et al. 2025b] [Yang et al. 2025d] [Yu 2006] [Yu and Hwang 2022] [Yu et al. 2000] [Yu et al. 2002b] [Yu et al. 2002a] [Yu et al. 2004] [Yu et al. 2005] [Yu et al. 2010b] [Zhan et al. 2025] [Zhang et al. 2021f] [Zhang et al. 2024a] [Zhang et al. 2024d] [Zhang et al. 2025b] [Zhang et al. 2025h] [Zhang et al. 2026f] [Zhang et al. 2026g] [Zhao 2024b] [Zhao et al. 2019b] [Zhao et al. 2021b] [Zhao et al. 2023b] [Zhao et al. 2023d] [Zhao et al. 2023c] [Zhao et al. 2025a] [Zhao et al. 2026c] [Zheng et al. 2012a] [Zhu et al. 2017] [Zhu et al. 2019] [Zhu et al. 2025c] [Zhu et al. 2026c] [Zhuangsheng et al. 2015] [Zissa 1984] [Zorn] [Zou and Cai 2022]

Inertial error propagation, the Schuler loop and the vertical channel

The keystone, which is how a navigator’s errors grow. Error equations and their propagation, Schuler tuning and the damping of Schuler oscillation, the error budget of a navigation system, and the unstable vertical channel with its barometric aiding. 16 of these titles name Schuler, and the record runs from the error equations of the period to error models for modern strapdown and rotating systems, which is the shift from bounding the error by hand to propagating it by machine that the review above describes.

281 records. [Abbasi and Haeri 2019] [Abdel-Hafez 2011] [Aldrich and Krabill 1972] [Alikhani and Nikoofard 2026b] [Andreyev et al. 2018] [Appendix B 2004] [Arshal 1987] [Aschaffenburg 1962] [Atashgah et al. 2023] [Bar-Itzhack 1990b] [Baro-Inertial Vertical Channel 2022] [Ben et al. 2022] [Blankinship 2008] [Borowski and Michalak 2024] [Britting 1969a] [Britting 1971c] [Broxmeyer 1962] [Cai et al. 2018] [Cao et al. 2025a] [Carpenter and Bar-Itzhack 2004] [Cavacece 2024] [Chang et al. 2010] [Chen et al. 2026d] [Chernyak and Kolesnyk 2023] [Chernyak and Romanchenko 2025] [Chiang et al. 2026] [Chueh et al. 2008] [Cline 1982] [Corson 1979] [Danik 1966] [Demidov 2009] [Deng et al. 2019b] [Deng et al. 2024] [Dongqing Gu and El-Sheimy 2008] [Dougherty et al] [Dougherty et al. 1994] [Dranitsyna and Sokolov 2023] [Du et al. 2018] [Dusek 1963] [Dusek 1964b] [Dusek 1964a] [Eck and Geering 2001] [Edge 1963] [Eisner and Goodman 1964] [El-Diasty et al. 2007] [Ephgrave 1962] [Ermakov et al. 2018] [Ermakov et al. 2022] [Farrell 2007] [Farrell et al. 2022] [Fegley and Weygandt 1963] [Feng et al. 2016] [Filyashkin and Yatskivsky 2013] [Fomichev 2025] [Fomichev and Li 2017] [Fu et al. 2016] [Gallo and Barrientos 2022] [Gang Li et al. 2010] [Gao Xin et al. 2013] [Gerber 1975] [Ghesmati et al. 2020] [Gilbert and Kayton 1964] [Golovan et al. 2018] [Goshen-Meskin and Bar-Itzhack 1992b] [Grammatikos et al. 1967] [Greenstein 1968] [Grigorie 2008] [Grubin 1975] [Guerrier et al. 2016b] [Gunhan and Unsal 2014] [Hammon 1962] [Han et al. 2020] [Han et al. 2026c] [Hansen et al. 1963] [Yan et al. 2012] [Haydon 2025] [He and Lee 2018] [He et al. 2015c] [He et al. 2020c] [Heller and Jordan 1975] [Heller and Jordan 1976] [Hoenk 1994] [Hou et al. 2019] [Hu et al. 2017] [Huang et al. 2016a] [Huang et al. 2019c] [Huang et al. 2026a] [Huang Xiaokai et al. 2011a] [Huddle 1983] [Inertial Navigation Error Analysis 2020] [Jaewon Seo et al] [Jekeli 2005] [Jia et al. 2009] [Jia et al. 2010] [Jia et al. 2018] [Jiang et al. 2022b] [Jiang et al. 2025a] [Jianmao et al. 2007] [Jones et al. 1970] [Jones et al. 1971] [Jurado and Raquet 2017] [Kahn and Von Bun 1985] [Kajahusain Abdul Suban 2007] [Kariminejad et al. 2026] [Kasper and Nash 1975] [Kelly et al. 2021] [Kim et al. 2018a] [Knickmeyer and Schwarz 1989] [Kortunov et al. 2007] [Kou et al. 2014] [Kulikov et al. 2022] [Kurbatov et al. 2019] [Lai et al. 2012] [Lambrecht et al. 2016] [Lange and Parkinson 1965] [Lange and Parkinson 1966] [Larin and Tunik 2012b] [Lee 1969c] [Lee and Lee 2025] [Lee et al. 2026c] [Li 2026b] [Li and Fang 2013] [Li and Fomichev 2017] [Li et al. 2013b] [Li et al. 2015d] [Li et al. 2017b] [Li et al. 2018c] [Li et al. 2023h] [Li et al. 2026j] [Lichter 2019] [Lin and Zhang 2020] [Liu et al. 2013b] [Liu et al. 2018a] [Liu et al. 2018b] [Liu et al. 2026d] [Martin 1997] [Черняк 2018] [Mei 1996] [Miao Ling-juan et al] [Mohammadkarimi et al. 2025] [Molinari et al. 2015] [Mozafari et al. 2025] [Muzumdar and Hull 1995] [Muzumdar and Hull 1996] [Nash 1968] [Nash and Hutchinson 1973] [Nash et al. 1972] [Navigation Error Analysis 2021] [Ni et al. 2023] [Nieminen et al. 2010] [Ning et al. 2022a] [Nobahari and Mohammadkarimi 2017] [Noureldin et al. 2012c] [Ouyang and Wu 2022b] [K.А. 2021] [Park et al. 2019] [Park et al. 2022] [Pawase and Futane 2015] [Peng et al. 2025b] [Position Error Propagation 1976] [Qi et al. 2020] [Qin et al. 2012] [Quan et al. 2015a] [Rahgoshay and Karimaghaie 2020] [Rajabi et al. 2025] [Ramalingam et al. 2009] [Rataichuk and Kortunov 2013] [Raza et al. 2021] [Remmler and Theobald 1967] [Rogers 1994] [Rogers 1995] [Rogers 2002] [Rogers and Rogers 1997] [Rummel 1980] [Ruth 1968] [Sakran 1970] [Sametov et al. 2025] [Savage 2002] [Scherzinger] [Scherzinger and Reid] [Schwarz 1980] [Selezneva et al. 2026] [Shao et al. 2023] [Shen Yong and Wu Yang-bo 2011] [Shi et al. 2010a] [Shi et al. 2026] [Shibata 1986] [Silva and Vieira 2022] [Simak et al. 2024] [Sohrabi and Rafatnia 2024] [Staas and Philip C. 1963] [Stafeev and Tikhomirov 2016] [Stebler et al. 2012] [Stepanov and Motorin 2019] [Stratton 1968] [Su 2024] [Szelmanowski 2013] [Karimli 2023] [Taylor 1975] [Taylor and Price 1974] [Te-Chang Li] [Tianyu 2024] [Trifonovs-Bogdanovs and Zabirov 2018] [Tucker and Stern 1986] [Vaispacher et al. 2015] [Vanderwerf] [Vasilyuk 2024] [Vasyliev et al. 2015] [Vathsal] [Vathsal 1994] [Vieira and Silva 2023] [Vinícius M. G. B. Cavalcanti et al. 2023] [Vodicheva and Parysheva 2019] [Vukmirica et al. 2024] [Waldmann et al. 2016] [Walker 1970] [Wan et al. 2012] [Wang 1979] [Wang 2019a] [Wang et al. 2011b] [Wang et al. 2013c] [Wang et al. 2017a] [Wang et al. 2020g] [Wang et al. 2023k] [Wang et al. 2024h] [Wang et al. 2026j] [Wei Gao et al. 2009] [Wen et al. 2016] [White and Hung 1978] [Whittaker and Crassidis 2017] [Whittaker and Crassidis 2018] [Whittaker and Crassidis 2020] [Widnall and Grundy 1974] [Widnall et al. 1974] [Widnall et al. 1976] [Winger] [Wrigley 1950] [Wu and Wang 2024] [Xie et al. 2024] [Xu and Fang 2008] [Xu et al. 2022a] [Xu et al. 2026c] [Xue 2026] [Yan and Wang 2025] [Yang and Shi 2018] [Yang et al. 2016a] [Yang et al. 2018b] [Yang et al. 2022a] [Ye et al. 2025b] [Yefeng et al. 2012] [Yeon Fuh Jiang and Yu Ping Lin 1991] [Yijie Dai et al. 2016] [Yongqiang et al. 2015] [Yu et al. 1997] [Yuan et al. 2024a] [Yuan et al. 2025a] [Yuanxin Wu et al. 2004] [Xue et al. 2016] [Yun Cho et al. 2012] [Zavattero 1987] [Zeng et al. 2010] [Zha et al. 2020] [Zhang and Wang 2011b] [Zhang and Wang 2016] [Zhang and Zhang 2013] [Zhang and Zhang 2017] [Zhang et al. 2009b] [Zhang et al. 2018g] [Zhang et al. 2018h] [Zhang et al. 2025j] [Zhao Dawei et al] [Zhao et al. 2014b] [Zhao et al. 2016a] [Zhao et al. 2017b] [Zhao et al. 2024d] [Zhimin and Guanxin 2008] [Zhou et al. 2022] [Zhu et al. 2021c] [Zhu et al. 2021a] [Zhu et al. 2026e] [Махдi 2010]

Command link, telemetry, tracking and the range

How the range saw the vehicle. Command guidance and radio command links, missile telemetry, radar tracking accuracy, line-of-sight and over-horizon propagation, refraction corrections, range instrumentation and the latency of teleoperation.

267 records. [Abdel-Rahim et al. 1993] [Abzug et al. 1970] [Acquatella B et al. 2020] [Alaimo et al. 2011] [Alizad and Hadi 2023] [Althsuler 1983] [Aly 1999] [Anderson 1970] [Askar et al. 2018] [Austin 1965] [Baber and Moul 1955] [Bacon 2012] [Baker 2006] [Balov and Zarubin 2016] [Bartnicki 2014] [Barton 1961] [Becker 1973] [Bell 2012] [Belsterling 1965] [Belzer and Cho 1988] [Benavoli et al. 2007] [Bigelow et al. 1961] [Billings and Durlach 2008] [Birkmire and Gallagher 2012] [Bischof 1959] [Black et al. 2022] [Blake 1968] [Blum and Dambeck 2020] [Boithias 1979] [Borden 1993] [Boykov et al. 2017] [Brady and Tarn 2001] [Britting et al. 1972] [Broden 1997] [Brouk and DeMars 2021] [Brudnak 2016] [Brudnak 2020] [Brueckner et al. 2023] [Bumer 1946] [Burchett et al. 2021] [Haussler 1967] [Jenila et al. 2023] [Callaway 1963] [Campbell Jones 1995] [Caraway and Randy R. 2001] [Chang and Dunn 2019] [Chen et al. 2023c] [Chengbin Lian et al. 2012] [Chernyak and Burym 2022] [Christensen and Mogensen 1979] [Christiansen and Smith 2019] [Ciesielski and Malanowski 2022] [Clifford and Strohbehn 1970] [Coe 1948] [Cone 1976] [Cottrill 1992] [Cox 1957] [Cox and Wong 2019] [Craig and Kennedy 1987] [Cullen 1969] [Dai et al. 2009] [Danik 1973] [de Rochechouart et al. 2024] [Dey et al. 2023] [Dianetti et al. 2017] [Donatelli-DuLong 1979] [Dugger 1982] [Dunn and Howard 1959] [Effects of Array Error 2014] [Eklund and Wickerts 1968] [Elliott and Weller 1954] [Evans 1966] [Evans et al. 1963] [Evans et al. 2026] [Fang 1967] [Farrell 1985] [Fashuyi and Afullo 2007] [Faulstich and Law 2006] [Fetner 1961] [Filipovic and Dikic 2011] [Finneran and Stanely 1969] [Fitzgerald 1987] [Fitzgerald 1994] [Frequency Tracking and Mitigation 2020] [Fruchtenicht 1974] [Gee 1978] [Gee et al. 1976] [General Dynamics/Astronautics San Diego Ca 1962] [Georg et al. 2020] [Ghasemi et al. 2011] [Ghasemi et al. 2016] [Ghose et al] [Gigleux et al. 2024] [Goertzen 1972] [Goktas et al. 2016] [Goldhirsh and Dockery 1991] [Goldhirsh et al. 1992] [Gray 1997] [Groutage 1980] [Guan et al. 2017a] [Guo et al. 2024b] [Hampton and Mills 1964] [Han et al. 2026a] [Hansen et al] [Hanson et al] [Hardouin 1961] [Haykin et al. 2010] [Headrick et al. 1967] [Heryana et al. 2022] [Holm 1968] [Hostetler 2005] [Howard and Lewis 1955] [Howell 2003] [Huang et al. 2011] [Huang Weiquan et al] [Huff and Herbert 1979] [Hull and Muzumdar 1993] [Hunt 1960] [Indiresan 1965] [Ishimaru 1978c] [Ishimaru 1978a] [Ishimaru 1978b] [Janes 1959] [Jerome] [Johansen and Fossen 2015] [Kalata 1984] [Kang et al. 2023] [Kashwani et al. 2023] [Kassas and Humphreys 2012] [Kay and Thorpe 1995] [Kazel and Faraone 1961] [Keijer and Weiss 2005] [Kersten and Kak 1989] [Kluge et al. 2013] [Knapp 1979] [Knowles et al. 1973] [Kramer 1964] [Krieger 1983] [Kriegsman 1966] [Kudriashov et al. 2018] [Kuo and Chiou 2000] [Lambert et al. 2009] [Lashley et al] [Lawton et al. 1997] [Lee 1985] [Lee and Ryu 2010] [Lee Kingsley 1967] [Lestage 2003] [Letchworth 2011] [Levitt 2001] [Line of Sight Propagation 2006] [Liu et al. 2020e] [Liu et al. 2020a] [Loftin 1967] [Luz et al. 2023] [Ma and McKitterick 2012] [Macario 1997] [Majumdar 1974] [Malanowski and Kulpa 2009] [Marcus 1966] [Margolis et al. 1958] [Marom et al. 2023] [Mathews 1960] [Matveev et al. 2025] [Maurer 1995] [Mishra 1989] [Miura 2022] [Борисенко and Залевський 2025] [Mokole 1991] [Monaco 1990] [Moniruzzaman et al. 2022] [Muchmore and Wheelon 1955] [Muehlner 1962] [Muller] [Murakami] [Myers 1965] [Myers 1966] [Nassirharand and Mousavi Firdeh 2009] [Nicholas et al. 1984] [O’Neil 1956] [Oderland et al] [Oliver 2012] [Opitz 2006] [Ornedo et al] [Page 1956a] [Parks and Kehlet 1952] [Peck and Coltrane 1955] [Peebles 1969] [Peebles 1985] [Peebles and Sakamoto 1980] [Peebles and Sskamoto 1980] [Perrins 2012] [Perry 1967] [Petrochenkov 2025] [Phillips and Chisholm 1995] [Pierce and Woodward 1971] [Pointing and Tracking Accuracy. 1969] [Powers 1960] [Practical Issues for Radar 1998] [Provost et al. 2026] [Quadros et al. 2022] [Radar Tracking Algorithms 2010] [Radionavigation Kalman Filtering 2022] [Ramachandra 2018] [Ramírez et al. 2024] [Rice 1999] [Rice 2013] [Rickard 1963] [Roloff 1957] [Rowlandson and Herlihy 1969] [Saglam and Yilmaz 2018] [Saini and Hablani 2014] [Saratayon and Petchartee 2015] [Scattering Mechanism of over-Horizon 2004] [Schierman et al. 2003] [Schreiter et al. 2017] [Schwarz 1954] [Scott et al. 1983] [Selvaggio et al. 2024] [Sengupta and Gupta 1984] [Seywald et al. 1991] [Shaw and Arnold] [Shipplett 1983] [Skarpetis et al. 2018] [Sperry Phoenix Co Az 1962] [Spreiter 1954] [Spreiter 1956] [Stengel et al. 1977] [Sun 1979] [SŁOwak 2025] [T03 2014] [Telemetry Standards for Guided 1957] [Thakur et al. 2019] [Tracking Radar 1999] [TRW Space Technology Labs Redondo Beach CA 1963] [Tsipis 1975] [Tukizi 1959] [Urban 1959] [Urban 1963] [Volskii et al. 2013] [von Eggers Rudd et al. 2000] [Waldman 1968] [Waldman 1969] [Walton 1995] [Wang 1998] [Webb 1979] [Wenkai et al. 2017c] [Wetzel 1954] [Wheelon 1955] [Wheelon 1956] [Wheelon and Muchmore 1955] [Whyte et al. 1979] [Williams 1964] [Windhorst et al. 1999] [Winton 2021] [Wislicenus and Daidzic 2022] [Xu et al. 2022d] [Yang et al. 2016b] [Ye et al. 2019c] [Yoneyama and Mushiake 1965] [Yu et al. 2014] [Zhang and Yuan 2015] [Zhang Guanjie et al] [Zhao et al. 2013] [Zhao et al. 2020b] [Zhen Ding and Balaji 2012] [Zhu and Huang 2010]

Fault detection, redundancy and reliability

What an unmanned vehicle cannot ask anyone to notice. Fault detection and isolation for inertial sensors, redundant and skewed inertial measurement units, reconfigurable control, and the reliability of missiles and guidance systems. 105 of these titles name redundancy, and the redundant strapdown unit with its detection logic is the subject the article dates to the decade after the programme.

246 records. [A Digital Diagnostic System 2013] [A Successful Program 1992] [Abdollahi and Pourtakdoust 2026] [Ammons 1979] [An Integrated Missile Reliability 1984] [Approach to Reliability 1973] [Assessing Missile System Reliability 1972] [Atmaca et al. 2025] [Attias and Sveitis] [Bosch and Kuehl 1976] [Chen et al. 2020a] [Chenoweth and Ryder 1976] [Kumar et al. 2026] [Li et al. 2021e] [Lu et al. 2019] [Motyka 1983] [Muniraj et al. 2020] [Prabhu and Anitha 2019] [Author 1981] [Avrutov 2015] [Balasubramani et al. 2024] [Becerra and El-Osery 2024] [Becka et al. 2008] [Berdjag et al. 2010] [Bharadwaj et al. 2017] [Bilajbegovic and Lehmann 2014] [Bills 1957] [Bin Jiang and Qi 2017] [Bittner et al. 2014] [Blair and McCorkle 1979] [Blattel 1957] [Blumenthal and Denton 1962] [Bodson and Pohlchuck 1998] [Bodson et al. 1997] [Bras et al. 2012] [Bras et al. 2015] [Brenner 1996] [Brown et al. 1973] [Bryant and Morrell 1981] [Bryant et al. 1984] [Cao et al. 2018] [Chen et al. 2016b] [Chen et al. 2023f] [Cheng and Tam 2014] [Cheng et al. 2018b] [Choi 2016] [Conner and Thompson 1963] [Craig and Russell 1978] [Da 1993] [Dagal 2026] [Dai et al. 2013a] [Dai et al. 2013b] [Dai et al. 2023] [Davis 1961] [de Oliveira et al. 2012a] [Deng and Sentis 2026] [Deng et al. 2025] [Doan et al. 2026] [Du et al. 2019a] [Du et al. 2022] [Ebner and Howell 1979] [Ebner and Mark 1977] [Ebner and Mark 1978] [Eckenhoff et al. 2019] [Eubank et al. 1955] [Evans and Wilcox 1969] [Evans and Wilcox 1970] [fen Wang et al 2018] [Fu et al. 2012] [Fu et al. 2017] [Fu et al. 2020] [Gagnon et al. 2018] [Gaver and Jacobs 1997] [Gheorghe and Neal 2026] [Gilmore and McKern 1970] [Gilmore and McKern 1972] [Giner and Ono 2018] [Goodstein et al. 1982] [Goodstein et al. 1984] [Grigorie and Botez 2014] [Guan et al. 2017b] [Guner and Dasdemir 2021] [Ha et al. 2022] [Han et al. 2017] [Harris 1959] [Hartwell et al. 1971] [Hoffman et al. 2005] [Hong and Jung 2016] [Howard and Kaufman 1964] [Howell 1988] [Hu and Wang 2019] [Hu et al. 2020b] [Huang et al. 2023c] [Jafari 2015] [Jafari and Roshanian 2012] [Janicijevic 2004] [Jeerage] [Jeerage 1990] [Jian et al. 2014] [Kamali et al. 2012] [Kasouf and Weiss] [Keum and Warey 2026] [Khamlak 2026] [Kim et al. 2004a] [Kim et al. 2021a] [Kim et al. 2026c] [Kimel and Harnett 1963] [Konigseder et al. 2016] [Kunpeng He et al. 2013] [Kuznetsov et al. 2023] [Lawrence and Berarducci] [Lee 1976b] [Lee and Karkkainen 2018] [Lee et al. 2010b] [Li and Li 2018b] [Li et al. 2021d] [Li et al. 2021a] [Li et al. 2022h] [Li et al. 2022c] [Li et al. 2022f] [Li et al. 2022g] [Li et al. 2023g] [Li et al. 2026g] [Liang and Gao 2009] [Lichter and Friedenreich 1962] [Lin et al. 2011] [Liu and Tian 2012] [Liu and Wu 2011] [Lombaerts et al. 2007] [Losik, Ph.D. 2012] [Lu and Van Kampen 2015] [Lukoyanov and Dranitsyna 2026] [Lukoyanov et al. 2025] [MacLean and Rodriguez 1996] [Malik 1976] [Margun et al. 2024] [Marinushkin and Podshivalov 2015] [McKern and Musoff 1973] [McLean 1994] [McPherson et al. 1976] [Mermagen and Yalamanchili 1983] [Mettler and Towner] [Minnaar and Smit 2017] [Mitchell 1976a] [Mitchell 1976b] [O’Connor et al. 2020] [Monroe 1963] [Montgomery 1975] [Moore and White 1967] [Morrell and Motyka 1983] [Morrell and Russell 1980] [Morrell et al. 1988] [Morrell et al. 1990] [Motyka et al. 1981] [Motyka et al. 1984] [Nguyen et al. 2026] [Oconnor 1971] [de Oliveira et al. 2012b] [Pace et al. 2008] [Packard and Weiler 1952] [Page et al. 1992] [Panten et al. 2022] [Parellier] [Park 2025] [Parsa et al] [Parsons 1966] [Pejsa 1973] [Phillips] [Piovesan et al. 2025] [Potter and Deckert 1972] [Prahlada 2002] [Rasmussen 1980] [Rehage et al. 2005] [Choi et al. 2004] [Ren and Hu 2018] [Ren et al. 2009] [Ren et al. 2024b] [Ren et al. 2024c] [Rice and McCorkle 1979] [Roy-Aikins] [Sarigul-Klijn and Huber 2006] [Schulte and Spencer 2020] [Seldon and Pertschuk 1954] [Sensor Failure Detection Identification 1994] [Seo et al. 2018a] [Shaffer et al. 2005] [Sheffels] [Siddiqi and Abraham 1988] [Skoogh and Lennartsson] [Solov and Thibodeau 1973] [Song et al. 2022] [Sprint Missile Subsystem Reliability 1977] [Stoller 1961] [Sukkarieh et al. 2000] [Sundvall et al. 2007] [Tekaslan et al. 2021] [The Air Force Approach 1963] [Theunissen and Owen Holbrook 1998] [Thibodeau and Bauer 1982] [Tsung-Lin Chen 2008] [Unger 1966] [Van Eykeren and Chu 2013] [Vanderwerf and Wefald 1988] [Venkataraman and Seiler 2019] [Vieweg] [Walker and Heltsley] [Wang et al. 2025n] [Wangu and Mouyos 1998] [Weitzen et al. 1996] [Wilcox 1972] [Wilcox 1973] [Williams and Pohl] [Williamson et al. 2005] [Xi and Lan 2017] [Xiang et al. 2022a] [Xiao and Lu 2021] [Xiao et al. 2024a] [Xiaowei Shao and Changsheng Shao] [Xiong and Zhang 2007] [Xu and Tian 2023] [Xu et al. 2011] [Xu et al. 2023a] [Xu et al. 2025c] [Yan and Chen 2013] [Ye and Zhang 2017] [Yi 2016] [Youssef et al. 2008] [Youssef et al. 2009] [Yu and Qiao 2020] [Yuan et al. 2018] [Yueh 1956] [Yuksel and El-Sheimy 2011] [Yun Cho et al. 2013] [Zahed et al. 2020] [Zhang 2017] [Zhang and Wang 2011a] [Zhang et al. 2018c] [Zhao and Li 2019] [Zhao et al. 2024a] [Zheng and Wei 2009] [Zhong et al. 2025] [Zhou et al. 2018b] [Zhou et al. 2018a] [Zhu et al. 2021b] [Zhu et al. 2026a] [Zou et al. 2022]

Free-flight models, flight test and the model-to-flight gap

The method that produced the only surviving data on the configuration. Free-flight and rocket-propelled model testing, aircraft parameter identification from flight data, and uncertainty quantification of aerodynamic prediction.

159 records. [A Technology and Operations 1993] [Abrashov et al. 2015] [Abrashov et al. 2018] [Advisory Group for Aerospace Research and Development 1984] [Advisory Group for Aerospace Research and Development 1999] [Aeinfar et al. 2011] [Anderson and Vincent 1985] [Andre and Czaja 1982] [Annergren et al. 2017] [Arif and Sasongko 2021] [Armstrong 1977] [Babar and Baglietto 2016] [Batterson and Morelli 1996] [Belforte and Tay 1993] [Brieger et al. 2008] [Bunge et al. 2015] [Callsen et al. 2023] [Canniff 1969] [Casini et al. 2009] [Casini et al. 2011] [Casini et al. 2012] [Chandler et al] [Chen and Valasek 1999] [Demidovich 2017] [Doherty] [Dong 2018] [Dwyer 1994] [Elenchezhiyan and Kumar 2024] [Flight Test Programme 1970] [Free-Flight Models 1953] [Fujimoto and Sugie 2016] [Fujimoto and Sugie 2017] [Fujimoto and Sugie 2018] [Geng and Li 2023] [Gerencser and Hjalmarsson] [Ghosh and Raisinghani 2000] [Ghosh and Raisinghani 2002] [Granot and Mayorchik 1983] [Granot and Sylman 1982] [Gringard and Kroll 2018] [Gross et al. 2012] [Grossir et al. 2020] [Harris et al. 2016] [Hiromi Suzukit and Toshiharu Sugie 2007] [Holberg and Grabowsky 1981] [Hollinger 1965] [Holway 1966] [Hosseini and Holzapfel 2022] [Hosseini et al. 2019] [Hosseini et al. 2020] [Hosseini et al. 2025] [Hu et al. 2019] [Hull and Roger 1975] [Hulshoff et al. 1996] [Iliff and Maine 1982] [Iliff and Maine 1983] [Jaggers 1977] [Jakowluk and Świercz 2025] [Grauer and Boucher] [Johansen 1969] [Jones 1970a] [Kaletka and Fu 1993] [Kelso 1993] [Klein 1983] [Klein and Morelli 1992] [Klipa 2012] [Kolumbán and Csáji 2018] [Kong 1994] [Kumar and Ghosh 2011] [Kumar et al. 2013] [Kwiek et al. 2022] [Langill 1965] [Larsson et al. 2011] [Levine and Woods 1981] [Lieberman 1963] [Londono and Leonhardt 2012] [Lynch and Weber] [Macmillan 1981] [Manchester 2010] [Mandal and Gu 2016] [Mao and He 2022] [Marwaha et al. 2008] [Maunder 1979] [Mayr et al. 2017] [McKavitt 1990] [McPherson 1977] [Mehra and Eupta 1975] [Methods for Reducing Data 2003] [Metodiev 2024] [Michal 1950] [Michal and Mitcham 1949] [Millard et al. 1982] [Mitchell and Peck 1950b] [Mohan et al. 2018] [Morelli 1995] [Morelli 1996] [Morelli 2000a] [Morelli 2002] [Morelli 2021] [Mu and Chen 2018] [Mu et al. 2017] [Mu et al. 2023] [Murphy and Klein 2008] [Murphy and Klein 2010] [Narasimhan and Bombois 2012] [Narasimhan and Rengaswamy 2006] [Narasimhan et al. 2011] [Nardozzo et al. 2019] [Tk et al. 2014] [Zarrop 1979b] [Optimal Experiment Design 1981] [Palomino et al. 2026] [Parameter Estimation Techniques 1974] [Paris and Bonner 2003] [Park 1977] [Parlini 1983] [Parsa et al. 2022] [Pawlak 1994] [Petersen 1981] [Petritoli et al. 2019] [Plaetschke and Weiss 1988] [Plaetschke et al. 1982] [Dhayalan et al. 2018] [Raisinghani and Adak 1983] [Raol and Singh 2023] [Rice and Hazlwood 1994] [Roberts 1988] [Roeser and Mönnich 2024] [Rogers and Walter K. 1955] [Rojas et al. 2007] [Ross 1979] [Safeer and Costello 2026] [Salvadori 2018] [Schwanz and Grimes 1980] [Seren et al. 2013] [Serre 2009] [Serre and Falempin 2008] [Silva 2011] [Simpson 1972] [Song and Napolitano 2002] [Stilley 1988] [Subedi et al. 2023] [Sugisaka and Sagara 1979] [Suzuki and Sugie 2007] [Suzuki and Yamakita 2011] [Szymanski et al. 2025] [Süelözgen 2022] [Tai et al. 2023] [Taylor 2009] [Tomaine et al. 1978] [Tuohy 1998] [Van Bavel 2014] [Wahlberg et al. 2006] [Wahlberg et al. 2010] [Wang and Iliff 2004] [Wingrove 1972] [Wyborny and Requardt 1975] [Xi et al. 2023] [Yasue 2020]

Reusable vehicles, recovery and the cost of a flight

The economic case for bringing the vehicle home. Reusable launch vehicles, their recovery, operations and life-cycle cost, and the life-cycle cost of weapon systems.

121 records. [Abrahamm and Valsa 2018] [Allen et al. 1994] [Alvord et al. 2024] [Andrews 1998] [Arora and Ananthasayanam 2003] [Arora et al. 2003] [Baumgartner 1997] [Brown and Olds 2005] [Caplin] [Chase 1979] [Chase and McKinney 2005] [Chen et al. 2018d] [Cheng et al. 2021b] [Chiesa et al. 2005] [Choo et al. 2018] [Cook 1995] [Cowling 2011] [Crose 1965] [Cusick and Kontis 2019] [Daniel et al. 2004] [Der Kiureghian 2001] [Dissel et al. 2005] [Dorsey et al. 1999] [Dorsey et al. 2000] [Dumbacher 2002] [Dumbacher and Klevatt 1994] [Edwards 1975] [Eisman 1999] [Elvin 1996] [Fitzsimmons 1996] [Fourie and Meyer 2009] [Freeman et al. 1996] [Freeman et al. 1997] [Fuchs et al. 2018] [Gage and Vander Kam 2003] [Garg and Dodiyal 2009] [Gong et al. 2022] [Gstattenbauer et al. 2006] [Guodong Ning et al] [Hagopian 2002] [Hao et al. 2017] [Hardy et al. 1993] [Jo and Ahn 2022] [Johnson and Servidio 2008] [Johnson et al. 2006] [Jung et al. 2022] [Jung et al. 2025b] [Kaplan 2002] [Karel 1967] [Kelly et al. 2009] [Kim et al. 2026b] [King 1971] [Knapp 1999] [Koelle 2000] [Kohrs and Petersen 1998] [Kuzin et al. 2009] [Larsen 2000] [Larsen 2003] [Larsen 2005] [Laubendorfer et al. 1965] [Leavitt and Peters] [Lee et al. 2024c] [Lee et al. 2026a] [Letchworth and Letchworth 2000] [Levitt et al. 1970] [Lichtenstein 1965] [Logsdon and Williamson 1997] [Martin 2006] [Matthews and Welter 1989] [McClure 1998] [Mease et al. 1999] [Menon et al. 2025] [Merhav 1982] [Meyerson 1998] [Michalski and Johnson 2007] [Milliken 1963] [Minor 1965] [Minuti 2026b] [Minuti 2026a] [Mo et al. 2022] [Molina et al. 2009] [Nair and Kukreja 2025] [Ngo and Blake 2003] [Ngo and Doman 2002] [Noneman 2002] [Olds and Bellini 1998] [Pidvysotskyi 2021] [Prasad 2022] [Rasky et al. 2006] [Reusable Launch Vehicle 1995] [Rey 2000] [Ri and Choe 2023] [Robinson et al. 2003] [Rogers and Dragone 1996] [Rooney 2003] [Sarigul-Klijn and Sarigul-Klijn 2003] [Sawyer and Bush 1998] [Setiawan et al. 2025] [Shepperd and Staugler 1999] [Singh et al. 2024] [Sithara and Shenil 2022] [Sivan and Pandian 2018] [Song et al. 2011] [Spencer 1999] [Stadler 1998] [Staniszewski 1999] [Stower 2024] [Sun] [Tatry et al. 1997] [Tetlow et al. 2000] [Urschel and Cox 2003] [Vaglio-Laurin and Finke 1965] [Wallace et al. 2003] [Wang et al. 2024b] [Wu and Zhang 2023] [Yang 2020] [Yang et al. 2006] [Yang et al. 2024a] [Zhao et al. 2021a] [Zhi et al. 2015] [Zubrin and Clapp 1996]

Accuracy as a statistic, circular error probable and error budgets

How accuracy is specified. The circular error probable and its estimators, error budgets for inertial and pointing systems, miss distance and the delivery accuracy of weapons.

69 records. [Agterberg 2023] [Alpert 1987] [Alpert 1988] [Andrews 1979] [Baccarella et al. 2019] [Bashkin et al. 2005] [Berger and Meyer 1974] [Blair 1990b] [Broglio 1961] [Brulle 1977] [Canciani and Brink 2017] [Canciani and Raquet 2016a] [Carlson 1974] [Carlson and Beer 2021] [Chaowanapreecha] [Chaowanapreecha et al. 2025] [Chen et al. 2020b] [Chen et al. 2020c] [Chen et al. 2026b] [Circular Probable Error 2014] [Corson 1980] [D’Aiutolo and Henning 1955] [Davydochkin 2017] [DiDonato 2007] [Esenwein 1952] [Evans et al. 1985] [Fekry et al. 2025] [Gallagher 1969] [Gonzalez and Denny 1970] [Govindarajulu 1986] [He et al. 2024] [Huang et al. 2019b] [Inertial navigation accuracy 2013] [Ivanov and Opanasiuk 2018] [Jischke 1978] [Jones and Parker 1986] [Kamat 1962] [Kelly 1977] [Kelly and LaBERGE 1980] [Lambregts and Creedon 1980] [Lenzner et al. 2018] [Leondes and Rankine 1972] [Liu et al. 2022i] [Liu et al. 2023i] [Luo and Li 2007] [Massoumnia 1991] [Meidunas 2008] [Moranda 1959] [Moranda 1960] [Morris 1986] [Nagaoka 1984] [Nelson 1988b] [Nelson 1991] [Papp and Rožnjik 2022] [Petritoli and Leccese 2021] [Schulte and Dickinson 1968] [Shultz 1963] [Stewart et al. 2016] [Swanson 1963] [Unsal and Ozgeneci 2017] [Velikanova et al. 2017] [Wheeler 1946] [White and Gounley 1987] [Yang and Song 2023] [Yang et al. 2022b] [Zhang and An 2012] [Zhu et al. 2014] [Zimmer and Turner 2017] [Zimmer et al. 2016]

Cruise vehicles and hypersonic cruise

The airbreathing cruise vehicle after the Navaho. Design, trajectory and control studies of hypersonic cruise vehicles, the successor class the review above describes as being attempted again.

22 records. [Balasubramanian et al. 2016] [Che and Tang 2008] [Chudoba et al. 2015] [Feng et al. 2020] [Heathman and Kelly 1966] [Holland] [Jing and Shuo 2008] [Jing and Yuan-pei 2015] [Kauffman et al. 1991] [Lee et al. 2007c] [Lian et al. 2013b] [Markopoulos and Mease 1996] [Murray and Steelant 2009] [Wang and Zhang 2021] [Wang et al. 1980] [Wang et al. 2007] [Wang et al. 2018d] [Wang et al. 2019h] [Wang et al. 2019d] [Wang et al. 2025g] [Wei et al. 2016a] [Wenkai et al. 2017b]

Where the Framing Breaks Down

Treating the X-10 through its navigation keystone illuminates the programme’s central failure but misleads in five ways, and they together are the strongest argument that the vehicle was mismatched to its job.

It could not test the propulsion. The Navaho cruised on ramjets. A ramjet has no compressor, so its pressure ratio is the ram ratio

\[\frac{p_{0}}{p_{\infty}} = \left( 1 + \frac{\gamma - 1}{2} M^{2} \right)^{\frac{\gamma}{\gamma - 1}} \tag{122}\]

which is exactly 1.000 at rest and therefore provides no cycle at all. A ramjet cannot take off from a runway, so a recoverable runway-operating testbed necessarily uses a different engine, and the X-10’s two turbojets tested nothing about the Navaho’s propulsion. Ramjet and turbojet cycle relations are in Hill and Peterson 1991 Mechanics and Thermodynamics of Propulsion, and the engine the weapon needed was evaluated separately in Reilly and Welna 1955.

It could not test the boost phase. The Navaho reached ramjet takeover on a liquid rocket booster, and the specific energy that booster had to supply is

\[e = \tfrac{1}{2} v^{2} + g h = \tfrac{1}{2} (818.9)^{2} + 9.80665 \times 24{,}000 = 0.571 \, \text{MJ/kg} \tag{123}\]

equivalent to an ideal velocity increment of 1068 metres per second. The X-10 took off under its own power and had no booster, so the entire boost and staging sequence, during which the first XSM-64 flight failed Cleary 1991 The 6555th, The NAVAHO Program, was outside its scope.

It could not test the structure. The aluminium frontier at Mach 2.27 sits above the X-10’s maximum of 2.05 and far below the Navaho’s 3.25, so the testbed flew inside the material regime the weapon had to leave. What lay on the other side of that frontier was being worked out contemporaneously by Chen 1958 and Stauffer 1964, on structures the X-10 was never built to carry.

It could not test the duration. The Navaho had to navigate for 172 minutes, and the longest reported X-10 navigation flight lasted 79, or 0.46 of the mission. That flight was long enough to separate the drift from the accelerometer bias, but not to show that the drift held steady over the further hour and a half a Navaho mission required. Of the first four it is the least visible, because the other three show in the hardware while this one shows only in the clock.

It could not test the environment the accuracy was claimed in. The budget above shows the deflection of the vertical consuming most of the requirement, and every X-10 navigation flight was made over a surveyed range. A test that removes the dominant error term by choosing where to fly measures the instrument and not the mission. The size of the term being removed is what Hagiwara 1972 and Talwani 1966 establish.

Four of these five lie in the vehicle. The fifth lies in the test range, and only it could have been fixed without building a different aeroplane.

What the X-10 could and did test is the aerodynamic configuration, the autopilot, the airframe systems, and the practicality of recovering a large unmanned supersonic vehicle. That is a real and useful list. It is not the list of things that decided whether the Navaho worked.

Is It an Aircraft, and Does the Question Have an Answer

The opening promised that the X-10 makes the not-an-aircraft framing hard to defend, and the material above is enough to settle what the difficulty is.

Every physical test fails. The X-10 had a wing, a tail, a fuselage, retractable landing gear, air-breathing engines, and a runway. It took off, cruised, manoeuvred, descended, and landed, repeatedly, and was maintained between flights by people who serviced it as they would have serviced an aeroplane. The X-8 had none of these properties and the X-9 had some of them once per airframe. If the category is defined by what the object is, the X-10 is an aeroplane and the question is closed.

Every purpose test also fails, in the opposite direction. The X-10 existed to produce a number for a weapon programme. It carried no payload, served no transport function, and was expended when it stopped being useful, three of them, by the account of North American X-10, deliberately flown into an island. The property that makes it not an aircraft is that nothing aboard it was ever the point.

What the article’s analysis adds is that the two tests do not merely disagree, they interact. The vehicle’s aircraft-like properties compromised its measurement. It was recoverable, so it needed turbojets, so it could not test the ramjet. It was recoverable, so it was built of aluminium, so it could not exceed Mach 2.27. It was recoverable, so every flight had to end on a runway, and runway landings consumed the fleet before it had completed more than a handful of navigator flights. Every concession to being an aeroplane cost it something as an instrument, and that trade is the most interesting thing about the vehicle.

The series has now met three consecutive designations that resist the research-aircraft model, and they resist it in three different ways. The X-8 was an instrument carrier that measured something other than itself. The X-9 was a weapon prototype that measured a control loop. The X-10 is a testbed whose form and whose function pulled against each other.

Three exceptions with three distinct structures would not be a pattern. Three exceptions with one common origin are. All three were RTV-A vehicles before they were X vehicles, and the Programme Origin section above records that two of them became X numbers in the same act of 1951 and that the date for the third is disputed. The right conclusion is therefore not that the X-series broadened to admit sounding rockets, missiles, and testbeds on their merits, but that a separate series was absorbed and its contents inherited the letter. Whether that absorption was ever a decision, as against a filing convenience, is the question the series’ synthesis article has to answer, and the three cases now on the table are its evidence. The synthesis weighs the accumulated cases, and the X-10 contributes the sharpest single instance, because for this vehicle being an aeroplane was actively expensive.

The Source Base

The survey rests on 8,521 research records assembled from Crossref, the NASA Technical Reports Server and the Defense Technical Information Center, of which 1,344 are report primaries, being 15.8 percent, by the identifier rule set out under The Definition of Primary. The vehicle-specific record within it is small, and the topical record is large, which is the shape of the evidence this section describes.

The accessible primary record for this vehicle is the thinnest of any article in this series so far, and the shape of the scarcity is more interesting than its extent.

The vehicle is indexed under its project number, not its designation. Queries against the aerospace archive for “X-10” and for “Navaho” return almost nothing usable, while “MX-770” returns Pfyl 1952 and Bond and Swanson 1953 immediately. A researcher who does not know the project number will conclude the record is empty when it is merely filed elsewhere. For this vehicle the right name within an archive matters as much as the right archive.

The defence archive that holds project documents for the X-9 holds none for the X-10. A Crossref search restricted to the Defense Technical Information Center publisher prefix on the project number MX-776 returns a report on the RASCAL weapon system, named for its radar scanning link, which is the X-9 programme’s own. The identical search on MX-770 returns nothing about the Navaho at all. Same archive, same query shape, adjacent project numbers, opposite results. The gap is therefore a property of the record and not of the search.

Three documents in the accessible record concern the actual hardware. They are Pfyl 1952 on the 0.07-scale tunnel model, Bond and Swanson 1953 on the 0.12-scale free-flight model, and Church and Taylor 1959 on a 0.05-scale model of the XSM-64A missile and booster, which is the weapon rather than the testbed. Everything else in this article’s reference base is topical rather than vehicle-specific, drawn from the very large period literature on inertial navigation, canard aerodynamics, supersonic inlets, automatic landing, and flight test. Two further documents name the programme, a 1958 news item in Electrical Engineering reporting that an automatic landing system had landed the X-10 Automatic Landing System Successfully 1958, which is a notice rather than a research record, and a history of the Navaho’s technology by Myers 1992, and neither is a technical report on the configuration.

That distribution is what makes the article possible at all. The vehicle-specific record would support perhaps four hundred words. The topical record supports the analysis performed here, because the physics that governed the X-10 was being published in the open literature by the same laboratories at the same time, even when the vehicle itself was not.

The Definition of Primary

Primacy is a property of the document, and this survey derives it from the identifier. A record is a report primary when it is a NASA Technical Reports Server url or carries a digital object identifier under the 10.21236 prefix, which Crossref registers for Defense Technical Information Center reports. The configuration reports on which the article’s aerodynamic analysis rests are all reached through the reports server, so the rule counts them.

The rule does not reach the journal and conference literature of the American Institute of Aeronautics and Astronautics, abbreviated AIAA. 1,937 of the records carry its 10.2514 prefix, among them 462 of the 965 records in the configuration cluster and 232 of the 482 in the inlet cluster. 15.8 percent is therefore a lower bound on how much of this survey is first-hand.

Thin Subjects

Eight subjects that this article’s derivations depend on have thin literatures. Each count below is the number of research records in this survey whose title carries at least one of the listed terms, with a hyphen read as a space.

Subject	Title terms counted	Records
the crossover between bounded accelerometer error and secular gyroscope drift	crossover time, dominant error	1
the length of the observation window in a navigation flight test	observation window, observation time, test duration, flight duration, duration of flight	0
temperature control of the inertial platform, the platform oven	temperature control, oven controlled, thermostat	6
the radio horizon of a command link	radio horizon, over the horizon, over horizon, beyond the horizon	8
recovery temperature and the service limit of aluminium	recovery temperature, adiabatic wall, aluminum alloy, aluminium alloy	7
flights per article as the measure of reuse	flights per, number of flights, turnaround, sortie	0
the dive onto the target and its angle sensitivity	dive phase, dive angle, dive bombing, diving	4
the Breguet range equation	breguet	0

The keystone construct is the thinnest of all. One title names a dominant error source and none names the crossover time, against 281 records in the error propagation cluster. The bounded accelerometer term and the secular drift term are textbook results, so the papers propagate the full error model and the article’s partition stands on the relations shown in The Research Question.

No title names the length of the observation window, which is the free variable of the article’s design-of-experiments result. The discipline that would frame it is the experiment design cluster above, and none of its 335 records names the duration of a navigation test.

The platform oven has become a compensation problem. Six titles name temperature control of an inertial instrument, while 81 instrument titles compensate temperature-induced drift instead, so the oven the article treats as a first-order component now survives mostly as a model in software.

The radio horizon and the aluminium limit are settled relations, carried by a few propagation and materials titles, and the Breguet range equation is named by no title at all. Flights per article, the parameter the reuse argument turns on, is named by no title, so that argument stands on the X-10’s own record.

What the Survey Admits

Every research title has been read for relevance, and a record is admitted only when a person reading its title finds it on this article’s subject, which is the self-contained navigation of a long-range airbreathing missile, the recoverable supersonic testbed built to measure it, and the literatures the article’s derivations and conclusions draw on. Many words this subject depends on also name something else, and a record that shares only such a word is excluded. Navaho also names the Navajo people, their language and their crafts. Probable error is also a statistic of psychometrics and biometrics, and vertical deflection also names television deflection circuits and the bending of beams and pipes. Gravity wave drag belongs to atmospheric dynamics, and wave drag also to ships, piles and swimmers. Inertial also describes particle flows, reference frames and first-order lags. Identifiability, observability and experiment design are also the language of pharmacometrics, epidemiology, ecology, chemistry, economics and power systems. A flare is also a gas flare, stellar also names astrophysics, Doppler radar also names weather radar data assimilation, and the records of the White Sands Missile Range include its hydrology, geology and administration. Rotorcraft and vertical take-off aircraft, ships and underwater vehicles outside the field-matching literature, human motion sensing, ground robots, mining and drilling, satellite navigation in its own right, aircraft noise and emissions, and missile defence policy are excluded as outside the subject. Correction and retraction notices, unsigned news items, abstract-journal listings, encyclopedia volume titles and dictionary headwords are excluded as well, because a survey counts research works and those are editorial events or parts of works. A review of a book, a reference or definition entry of two pages or fewer and a second deposit of a document already in the survey are not admitted either, while an authored encyclopedia article of more than two pages and a textbook chapter are research works and are kept.

Some records of doubtful relevance are kept. Gravity and magnetic map matching for underwater vehicles is kept because the field-matching literature is chiefly written for them and the article’s gravity argument concerns the method. Star tracker work for spacecraft attitude is kept as the tracker’s later history, lunar and planetary landing guidance and terrain-relative navigation as automatic landing and aided navigation elsewhere, and attitude control of reusable launch vehicles as the control of a recoverable flight vehicle. Several identifiability works from pharmacometrics, power systems and microalgae culture, a turbomachinery aerothermal calculation and turbomachinery uncertainty quantification, a quantum-computing study of aerothermal and structural optimisation for mobility systems, a vehicular optical communication link characterised by Allan variance, the flight test of a tilt-rotor unmanned aircraft, the landing gear of a quadrotor, and two underwater navigation studies are kept because the sentence citing each uses it for the method and not for the application. Teleoperation of ground vehicles under latency and land vehicle inertial navigation are kept for the same reason, because the article cites them for the latency of a command link and for aided inertial navigation. A reader may weigh each accordingly.

The off-topic share that remains is a matter of reading judgement rather than a sample estimate.

Epistemic State

Historical fact, well supported. The X-10 was the MX-770 testbed for the Navaho. Thirteen were built. The first flew on 14 October 1953 at Edwards. Fifteen flights were made at Edwards through March 1955 by five vehicles, and twelve more from Cape Canaveral between August 1955 and November 1956. The first Cape flight on 19 August 1955 ended with the vehicle overrunning the strip after its drag chute failed to deploy. A 200 by 10,000 foot strip was built at the Cape for the vehicle. Maximum demonstrated speed was Mach 2.05, given as 2.06 in the Air Force history. The Air Force cancelled the Navaho in July 1957, by a message dated 12 July in the Cape history, with 10 and 13 July given elsewhere. Two X-10s supported BOMARC tests on 24 September and 13 November 1958 and both burned after leaving the Skid Strip. The final flight was 26 January 1959. One vehicle survives.

Historical fact, reported but from secondary compilations only. The 1948 Air Force circular error probable requirement near 800 metres and the XN-1 drift near 1.6 kilometres per hour, both from a single web compilation, the accuracy goal of 1500 feet, which the Cape history gives as the goal of the weapon as a whole and not as a demonstrated stellar-inertial accuracy, and the count of five dedicated autonavigator flights, which the launch appendix of Werrell draws from the Air Force Systems Command index of missile launchings and of which the flight chronology describes four as navigation tests. The first three figures carry the gyroscope-specification argument and none of them is traceable to a released programme document in the accessible record. The requirement itself is stated differently across sources, as 800 metres in 1948 and 450 metres in 1950 in the web compilation, 1500 feet in the Cape history, and 12,000 feet after 5,000 miles, once relaxed, in the Air Force history. If those figures are wrong, the inverted gyroscope specifications are wrong by the same factor, though the structural conclusions about which error grows and which is bounded do not depend on them. The Edwards durations come from the launch appendix of Werrell and agree with the 32-minute first flight in the Air Force history. The Cape durations of 51, 62 and 79 minutes, the computer failures that aborted two navigator flights, and the flight-by-flight causes of loss rest on the single web compilation, and the appendix gives no Cape durations to check them against. If the 79-minute figure is wrong, the finding that the navigation flight outlasted the crossover falls with it. The sources also disagree about the N-6 itself, which the compilation calls stellar-inertial and the Air Force history all-inertial.

Sources disagree and this article does not resolve it. Reported X-10 length is 66 feet 2 inches in the designation history and 77 feet in other compilations, a difference of sixteen percent. Reported range is 1370 kilometres in one and 1009 kilometres in another. Reported service ceiling differs slightly between sources. The dimensions used in the calculations above are stated where they are used.

Engineering analysis, derived here and independently checkable. The Schuler frequency and period. The bounded form of the accelerometer error and the secular form of the gyroscope error. The crossover time of 47.8 minutes. The duration of 27.6 minutes for a thousand-kilometre leg at maximum Mach and its ratio of 0.58 to the crossover. The ratios of 1.07, 1.30 and 1.65 to the crossover for the reported Cape sorties of 51, 62 and 79 minutes, and the count of fourteen Edwards flights of fifteen below it. The exact orthogonality of the two error signatures over one Schuler period, proved by direct integration, the correlation of 0.974 over a maximum-speed leg with its variance inflation of 19.7, and the correlation of 0.140 over the 79-minute flight with its inflation of 1.02. The window-length sweep showing the optimum at exactly one Schuler period. The inverted gyroscope drift requirements. The star tracker inversions and the 17.1 minute refix interval. The azimuth equivalence of 2.9 kilometres per arcminute. The vertical-channel time constant of 570 seconds, its doubling time of 6.6 minutes, and the 18.1 e-foldings over a Navaho mission. The deflection-of-the-vertical contribution of 618 metres at ten arcseconds. The platform temperature control of 0.25 kelvin implied by the drift specification. The quadrature error budgets of 5617 metres pure inertial and 1488 metres stellar-inertial. The normal-shock and two-shock recovery figures. The radio horizon of 482 kilometres and its ratio of 2.08 to a thousand-kilometre leg. The turn radius of 21.5 kilometres at load factor two. The short-period frequency spread from 0.63 to 2.03 radians per second. The lift-to-drag ratio of 2.51, the reported mass ratio of 1.640, and the demonstration that the reported ranges are inconsistent with the reported weights on any cruise condition. The break-even inlet recovery of 0.622. The recovery temperatures and the Mach 2.27 aluminium frontier. The landing energy, stall speed, and braking distance. The statistical precision available from five flights and from three, and the mission-reliability product.

Inference, argued but not established. That the navigator’s error was observed over the whole of the 79-minute flight, which the window calculation assumes. That the X-10’s recoverability was motivated substantially by the statistical character of a drift measurement rather than by unit cost alone. That the free-flight duct recovery below normal-shock values reflects model scale and not the full-scale inlet, which the thrust-balance argument supports but does not prove, since it inherits the drag estimate. That any demonstration of the programme’s accuracy goal was flown over surveyed range geometry and would not have transferred to unsurveyed territory. That the five testability gaps identified were understood at the time as gaps rather than accepted as adequate coverage. That the reported ranges describe a mission profile the article cannot reconstruct, the reported weights and the reported ranges being mutually inconsistent under every cruise assumption tried here.

A budget that does not close is reported rather than reconciled. The quadrature sum of representative error terms exceeds the programme’s accuracy goal by a factor of 3.3, and the deflection-of-the-vertical term alone exceeds it. The article offers three readings and adopts none. It is the largest unresolved quantitative tension in the article, stated here and not smoothed.

Assumptions made explicit. An accelerometer bias of one ten-thousandth of a gravity, a subsonic minimum drag coefficient of 0.020, a span efficiency of 0.6, a landing mass of twelve tonnes, a maximum lift coefficient of unity, a braking friction coefficient of 0.4, a thrust specific fuel consumption of 1.0 per hour, a recovery factor of 0.89, a gyroscope temperature sensitivity of 0.01 degrees per hour per kelvin, a deflection of the vertical of ten arcseconds, a pitch inertia based on a radius of gyration of thirty percent of length, a mean chord inferred from area and aspect ratio, an effective Earth radius factor of four thirds for radio refraction, and the treatment of installed thrust as proportional to delivered total pressure. Each is representative rather than measured, and each is stated at the point of use so that a reader may substitute a better value.

Where information postdates the editorial date. The contemporary literature section is written from current knowledge.

Out of Scope

The Navaho’s booster engines and their descent into the Rocketdyne engine line, which deserve their own treatment and are the programme’s largest legacy. The G-26 and G-38 vehicles as flight articles. The W-39 warhead. The Snark, the X-10’s direct competitor, whose free-flight aerodynamic record is cited here only in passing. BOMARC, which appears only as the consumer of three surplus airframes. The detailed politics of the 1957 cancellation. The comparative economics of cruise against ballistic delivery, which is treated only to the depth needed to explain the cancellation. Digital computation, which arrived too late to matter to this vehicle.

Conclusion

The X-10 was built to find out whether a machine could still know where it was after three hours of flight with nothing to look at but the stars. It was a good aeroplane. It flew to Mach 2.05, navigated across a range, and came home on its own wheels, a decade before airliners could land themselves. It did not answer its question, and the record points to the number of its navigation flights more than to their length.

The error a navigator accumulates from its accelerometers is bounded by the geometry of the planet at about 1.3 kilometres. The error it accumulates from its gyroscopes grows without limit. The two are equal at forty-eight minutes. A thousand-kilometre leg at the X-10’s top speed would last twenty-eight, and over so short a window the two error signatures are ninety-seven percent correlated. The reported sorties were longer, however, and the one navigation flight whose duration is recorded lasted seventy-nine minutes, close to the eighty-four over which the two signatures are exactly uncorrelated. For that flight the crossover argument does not hold, and it holds only for the Edwards flights, which carried no navigator, and for a dash at top speed that no navigation flight is known to have been. What limited the measurement is that five autonavigator flights were made and two were aborted, which leaves the spread of the drift known to no better than about fifty percent, and that the longest of them lasted under half of the Navaho’s three hours, over a surveyed test range.

Three of the series’ vehicles have now been things other than aircraft, and the X-10 is the one that shows why the distinction is hard. It had wings, wheels, a runway, and a flight test programme. What it did not have was a pilot, and the consequence of not having a pilot was that its entire reason for existing was a measurement rather than a demonstration. A demonstration succeeds by being performed once. A measurement of a spread succeeds only if it is repeated, and a recoverable vehicle that kept destroying itself on landing could not be repeated often enough.

Equations

This section collects the 123 display equations of the article in the order they appear, each under its number and reproduced exactly as it stands in the text. A title in bold names an established result, and a title in italics beginning with the word Bespoke names a construction made for this analysis. Of the 123, 72 are established and 51 are bespoke. The equations use SI units unless historical values are converted, gyro drift is also given in degrees per hour and angular errors in arcseconds, and symbols such as gamma, n, R, a, c, e, r, s, p, T and mu have different meanings between sections while Re denotes Reynolds number and R_e the Earth radius.

Equation 1, Speed of Sound at 24 Kilometres. At 24 kilometres the ideal-gas speed of sound is 297.8 metres per second using the standard atmosphere temperature. Parsch 2002 SM-64

\[a = \sqrt{\gamma R T} = \sqrt{1.4 \times 287.05 \times 220.6} = 297.8 \, \text{m/s} \tag{1}\]

Equation 2, Cruise Time over the Mission Range. The ten-million-metre mission range divided by the cruise speed gives a flight time of 10,333 seconds. Parsch 2002 SM-64

\[t = \frac{R_{\text{mission}}}{v} = \frac{1.0 \times 10^{7}}{967.8} = 10{,}333 \, \text{s} = 2.87 \, \text{hours} \tag{2}\]

Equation 3, Secular Inertial Position Error. For a level platform the position error from constant gyroscope drift grows as Earth radius times drift rate times elapsed time. Britting 1971 Inertial Navigation Systems Analysis Titterton and Weston 2004 Strapdown Inertial Navigation Technology

\[\delta x_{\text{secular}} = R_{e} \, \varepsilon \, t \tag{3}\]

Equation 4, Bespoke Required Gyroscope Drift Rate from the Weapon Accuracy Goal. The calculation treats the entire reported circular error probable as position error from gyroscope drift over the mission, yielding 1.215 times ten to the minus eight radians per second. circular error probable Wade, Navaho, Encyclopedia Astronautica

\[\varepsilon_{\text{req}} = \frac{\mathrm{CEP}}{R_{e} t} = \frac{800}{6.371 \times 10^{6} \times 10{,}333} = 1.215 \times 10^{-8} \, \text{rad/s} \tag{4}\]

Equation 5, Bespoke Required Drift Rate in Degrees per Hour. Converting the rate derived by allocating the entire reported circular error probable to gyroscope drift from radians per second gives 0.0025 degrees per hour.

\[\varepsilon_{\text{req}} = 1.215 \times 10^{-8} \times 206{,}265 = 0.0025 \, \text{deg/hr} \tag{5}\]

Equation 6, Bespoke Achieved Drift Rate from Reported Position Error. The calculation attributes all reported position error growth of 1.6 kilometres per hour to gyroscope drift, giving an equivalent drift of 0.0144 degrees per hour. Wade, Navaho, Encyclopedia Astronautica

\[\varepsilon_{\text{ach}} = \frac{1600}{6.371 \times 10^{6} \times 3600} = 6.976 \times 10^{-8} \, \text{rad/s} = 0.0144 \, \text{deg/hr} \tag{6}\]

Equation 7, Bespoke Drift Shortfall Factor. The reported achieved drift is 5.74 times the required rate obtained by allocating the whole circular error probable to gyroscope drift. Wade, Navaho, Encyclopedia Astronautica

\[\frac{\varepsilon_{\text{ach}}}{\varepsilon_{\text{req}}} = \frac{0.0144}{0.0025} = 5.74 \tag{7}\]

Equation 8, Accelerometer Error Equation. The velocity error changes with platform tilt under gravity and with accelerometer bias. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\dot{\delta v} = -g \phi + \nabla \tag{8}\]

Equation 9, Platform Tilt Error Equation. The platform tilt rate is the velocity error divided by Earth radius plus gyroscope drift. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\dot{\phi} = \frac{\delta v}{R_{e}} + \varepsilon \tag{9}\]

Equation 10, Second-Order Schuler Error Equation. Eliminating platform tilt from the inertial error equations gives a forced oscillator with gyroscope drift as its forcing. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\ddot{\delta v} + \frac{g}{R_{e}} \delta v = -g \varepsilon \tag{10}\]

Equation 11, Undamped Velocity Error Solution. The homogeneous Schuler error equation has a sine and cosine solution at its natural frequency. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\delta v_{h}(t) = C_{1} \cos \omega_{s} t + C_{2} \sin \omega_{s} t \tag{11}\]

Equation 12, Schuler Frequency. The Schuler frequency is the square root of gravity divided by Earth radius, evaluated here for Earth. Schuler frequency

\[\omega_{s} = \sqrt{\frac{g}{R_{e}}} = \sqrt{\frac{9.80665}{6.371 \times 10^{6}}} = 1.2407 \times 10^{-3} \, \text{rad/s} \tag{12}\]

Equation 13, Schuler Period. The Schuler period is the period corresponding to the natural frequency of the inertial platform. Schuler frequency

\[T_{s} = \frac{2\pi}{\omega_{s}} = 5064 \, \text{s} = 84.4 \, \text{minutes} \tag{13}\]

Equation 14, Bounded Position Error from Accelerometer Bias. A constant accelerometer bias produces a bounded Schuler position error with amplitude set by the bias and Earth radius. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\delta x_{\nabla}(t) = \frac{\nabla}{\omega_{s}^{2}} \left( 1 - \cos \omega_{s} t \right) = \frac{\nabla R_{e}}{g} \left( 1 - \cos \omega_{s} t \right) \tag{14}\]

Equation 15, Secular Position Error from Gyroscope Drift. Gyroscope drift forces the Schuler loop and produces a position error containing a secular ramp. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\delta x_{\varepsilon}(t) = -R_{e} \varepsilon \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} \right) \tag{15}\]

Equation 16, Bespoke Error from a Representative Accelerometer Bias. The bounded position error uses the representative bias of one ten-thousandth of gravity for a good instrument of the period. Staas and Philip C. 1963 Lange and Parkinson 1965

\[\delta x_{\nabla,\max} = \frac{2 \times 9.807 \times 10^{-4} \times 6.371 \times 10^{6}}{9.80665} = 1274 \, \text{m} \tag{16}\]

Equation 17, Crossover Time Between the Error Sources. Equating the growing drift error with the maximum bounded bias error gives the time when the two contributions are equal. Whitcombe 1961 Britting 1971 Inertial Navigation Systems Analysis

\[R_{e} \varepsilon t_{\times} = \frac{2 \nabla R_{e}}{g} \quad \Longrightarrow \quad t_{\times} = \frac{2 \nabla}{g \varepsilon} \tag{17}\]

Equation 18, Bespoke Crossover Time for the Reported Instruments. The crossover time evaluates the equality using the representative accelerometer bias and the reported achieved gyro drift. Wade, Navaho, Encyclopedia Astronautica

\[t_{\times} = \frac{2 \times 9.807 \times 10^{-4}}{9.80665 \times 6.976 \times 10^{-8}} = 2867 \, \text{s} = 47.8 \, \text{minutes} \tag{18}\]

Equation 19, Bounded Position Error from Platform Tilt. A residual platform tilt produces a bounded position error equal to twice Earth radius times the tilt. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\delta x_{\phi} = 2 R_{e} \phi_{0} \tag{19}\]

Equation 20, Bespoke Residual Tilt at the Navaho Goal. Applying the weapon-wide 457 metre accuracy goal to the stellar inertial system gives a residual tilt of 7.4 arcseconds. Cleary 1991 The 6555th, The NAVAHO Program

\[\phi_{0} = \frac{457}{2 \times 6.371 \times 10^{6}} = 3.588 \times 10^{-5} \, \text{rad} = 7.4 \, \text{arcsec} \tag{20}\]

Equation 21, Bespoke Azimuth Error at the Navaho Goal. Applying the same 457 metre goal over the reported mission range gives an azimuth error of 9.4 arcseconds. Cleary 1991 The 6555th, The NAVAHO Program

\[\psi = \frac{457}{1.0 \times 10^{7}} = 4.572 \times 10^{-5} \, \text{rad} = 9.4 \, \text{arcsec} \tag{21}\]

Equation 22, Bespoke Drift Error Relative to Stellar Accuracy. The reported gyro drift produces ten times the stellar system accuracy goal over the mission range. Wade, Navaho, Encyclopedia Astronautica Cleary 1991 The 6555th, The NAVAHO Program

\[\frac{R_{e} \varepsilon_{\text{ach}} t}{\mathrm{CEP}_{\text{stellar}}} = \frac{4592}{457} = 10.0 \tag{22}\]

Equation 23, Time Between Star Fixes. The time for drift to regrow the stellar accuracy error is the error divided by Earth radius times drift rate. Horsfall 1958 Blumhagen 1963

\[t_{\text{fix}} = \frac{\mathrm{CEP}_{\text{stellar}}}{R_{e} \varepsilon_{\text{ach}}} = \frac{457}{6.371 \times 10^{6} \times 6.976 \times 10^{-8}} = 1029 \, \text{s} = 17.1 \, \text{minutes} \tag{23}\]

Equation 24, Vertical Channel Error Equation. Linearising the gravity gradient gives an unstable altitude error equation with a positive growth term. Schenkel 1974

\[\ddot{\delta h} = \frac{2g}{R_{e}} \delta h \tag{24}\]

Equation 25, Vertical Error Time Constant. The vertical error time constant is the square root of Earth radius divided by twice gravity. Schenkel 1974

\[\tau_{v} = \sqrt{\frac{R_{e}}{2g}} = \sqrt{\frac{6.371 \times 10^{6}}{19.613}} = 570 \, \text{s} \tag{25}\]

Equation 26, Vertical Error Doubling Time. An exponential vertical error with the stated time constant doubles after that time constant multiplied by the natural logarithm of two. Schenkel 1974

\[t_{2} = \tau_{v} \ln 2 = 395 \, \text{s} = 6.6 \, \text{minutes} \tag{26}\]

Equation 27, Vertical Error Growth over the Mission. The mission duration divided by the vertical error time constant gives an exponential growth factor of 7.5 times ten to the seventh. Schenkel 1974

\[e^{10{,}333 / 570} = 7.5 \times 10^{7} \tag{27}\]

Equation 28, Bounded Error from Vertical Deflection. A deflection of the vertical produces a bounded position error equal to twice Earth radius times the deflection. Vertical deflection

\[\delta x_{\xi} = 2 R_{e} \xi \tag{28}\]

Equation 29, Position Error from a Ten-Arcsecond Deflection. A ten-arcsecond vertical deflection produces 618 metres of position error. Vertical deflection

\[\delta x_{\xi} = 2 \times 6.371 \times 10^{6} \times \frac{10}{206{,}265} = 618 \, \text{m} \tag{29}\]

Equation 30, Linear Temperature Dependence of Gyroscope Drift. The first-order drift model changes linearly with temperature from its reference value. Grubin 1975 Metzger and Jircitano 1975 Gerber 1975

\[\varepsilon(T) = \varepsilon_{0} + k_{T} \left( T - T_{0} \right) \tag{30}\]

Equation 31, Bespoke Platform Temperature Control. The platform must remain within a quarter kelvin when the representative drift sensitivity is one hundredth of a degree per hour per kelvin. Grubin 1975

\[\Delta T = \frac{\varepsilon_{\text{req}}}{k_{T}} = \frac{0.0025}{0.01} = 0.25 \, \text{K} \tag{31}\]

Equation 32, Bespoke Drift from a One-Kelvin Temperature Change. A one-kelvin temperature change produces drift of 0.01 degrees per hour under the representative sensitivity. Grubin 1975

\[\varepsilon = 0.01 \times 1 = 0.01 \, \text{deg/hr} \tag{32}\]

Equation 33, Independent Error Combination. Independent position error contributions combine as the square root of the sum of their variances. Mahlmeister et al. 1955 Chen 1958 Kendall and Gonzalez 1965

\[\sigma_{\text{total}} = \sqrt{\sum_{i} \sigma_{i}^{2}} \tag{33}\]

Equation 34, Bespoke Pure-Inertial Error Budget. The four article-selected inertial error contributions combine to a total position error of 5,617 metres. Mahlmeister et al. 1955 Chen 1958 Kendall and Gonzalez 1965

\[\sigma_{\text{total}} = \sqrt{4592^{2} + 1274^{2} + 2909^{2} + 618^{2}} = 5617 \, \text{m} \tag{34}\]

Equation 35, Bespoke Shares of the Error Variance. The article’s four error sources contribute the listed fractions of the total variance. Mahlmeister et al. 1955 Chen 1958 Kendall and Gonzalez 1965

\[\frac{\sigma_{i}^{2}}{\sigma_{\text{total}}^{2}} = 0.668, \; 0.268, \; 0.051, \; 0.012 \tag{35}\]

Equation 36, Bespoke Stellar-Inertial Error Budget. Replacing the drift and alignment terms with the stellar residual gives a total error of 1,488 metres. Cleary 1991 The 6555th, The NAVAHO Program Mahlmeister et al. 1955

\[\sigma_{\text{stellar}} = \sqrt{457^{2} + 1274^{2} + 618^{2}} = 1488 \, \text{m} \tag{36}\]

Equation 37, Cross-Track Error from Azimuth Misalignment. A small azimuth error produces a cross-track error equal to the angle times the mission range. Remmler and Theobald 1967 Dusek 1964a

\[\delta y = \psi \, R_{\text{mission}} \tag{37}\]

Equation 38, Bespoke Cross-Track Error from One Arcminute. A chosen one-arcminute launch misalignment over ten thousand kilometres produces 2,909 metres of cross-track error. Dasaro 1970

\[\delta y = 2.909 \times 10^{-4} \times 1.0 \times 10^{7} = 2909 \, \text{m} \tag{38}\]

Equation 39, Required Drift Rate in Terms of Mission Range. Substituting mission time as range divided by speed makes the required drift rate inversely proportional to mission range. Navaho

\[\varepsilon_{\text{req}} = \frac{\mathrm{CEP}}{R_{e} t} = \frac{\mathrm{CEP} \, v}{R_{e} R_{m}} \tag{39}\]

Equation 40, Drift Requirement Across Two Mission Ranges. At fixed accuracy and speed the required drift rates have the inverse ratio of the two reported mission ranges. Navaho

\[\frac{\varepsilon_{1}}{\varepsilon_{2}} = \frac{R_{m,2}}{R_{m,1}} = \frac{5500}{500} = 11 \tag{40}\]

Equation 41, Relative Standard Error of a Sample Standard Deviation. For normally distributed samples the relative standard error of the sample standard deviation is approximately one over the square root of twice the degrees of freedom.

\[\frac{\sigma_{s}}{s} \approx \frac{1}{\sqrt{2(n-1)}} \tag{41}\]

Equation 42, Bespoke Sample Count for Twenty-Percent Precision. The selected twenty-percent precision target requires at least fourteen samples of a normal quantity.

\[n = 1 + \frac{1}{2 (0.2)^{2}} = 13.5 \, \text{flights} \tag{42}\]

Equation 43, Standard-Deviation Error with Five Samples. Five samples give an estimated standard deviation with relative standard error of about 35 percent. Werrell 1985 The Evolution of the Cruise Missile Wade, Navaho, Encyclopedia Astronautica

\[\frac{\sigma_{s}}{s} = \frac{1}{\sqrt{2 \times 4}} = 0.354 \tag{43}\]

Equation 44, Standard-Deviation Error with Three Samples. Three samples give an estimated standard deviation with relative standard error of 50 percent. Werrell 1985 The Evolution of the Cruise Missile Wade, Navaho, Encyclopedia Astronautica

\[\frac{\sigma_{s}}{s} = \frac{1}{\sqrt{2 \times 2}} = 0.50 \tag{44}\]

Equation 45, Bespoke X-10 Leg Duration. A selected thousand-kilometre leg at the X-10 maximum speed takes 1,653 seconds. North American X-10 Parsch 2002 RTV-A-5 X-10

\[t_{\text{X-10}} = \frac{1.0 \times 10^{6}}{604.9} = 1653 \, \text{s} = 27.6 \, \text{minutes} \tag{45}\]

Equation 46, Bespoke Leg Duration Relative to the Crossover. The selected maximum-speed leg lasts 0.58 times the calculated crossover time. North American X-10 Parsch 2002 RTV-A-5 X-10

\[\frac{t_{\text{X-10}}}{t_{\times}} = \frac{1653}{2867} = 0.58 \tag{46}\]

Equation 47, Bespoke Gyroscope Error on the X-10 Leg. The reported achieved drift accumulates 735 metres of position error during the selected X-10 leg. Wade, Navaho, Encyclopedia Astronautica North American X-10

\[\delta x_{\varepsilon} = R_{e} \varepsilon_{\text{ach}} t_{\text{X-10}} = 735 \, \text{m} \tag{47}\]

Equation 48, Bespoke Accelerometer Error on the X-10 Leg. The representative accelerometer bias produces 931 metres of bounded error over the selected leg. Staas and Philip C. 1963 North American X-10

\[\delta x_{\nabla} = \frac{\nabla R_{e}}{g} \left( 1 - \cos \omega_{s} t_{\text{X-10}} \right) = 931 \, \text{m} \tag{48}\]

Equation 49, Bespoke Combined Error Signatures. The measured position error is modelled as a bounded Schuler term plus a secular drift term with article-specific coefficients. Lange and Parkinson 1965 Britting 1971 Inertial Navigation Systems Analysis

\[\delta x(t) = A \left( 1 - \cos \omega_{s} t \right) + B \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} \right) \tag{49}\]

Equation 50, Bespoke Orthogonality over One Schuler Period. The article’s centred accelerometer and gyroscope error signatures integrate to zero correlation over one full Schuler period. Lange and Parkinson 1965

\[\int_{0}^{T_{s}} \left( -\cos \omega_{s} t \right) \left( t - \frac{\sin \omega_{s} t}{\omega_{s}} - \frac{T_{s}}{2} \right) dt = 0 \tag{50}\]

Equation 51, Bespoke Error-Signature Correlations. The correlation of the two modelled error signatures is evaluated over the X-10 and Navaho flight durations. North American X-10 Navaho

\[r(t_{\text{X-10}}) = 0.974 \qquad r(T_{s}) = 0.000 \qquad r(t_{\text{Navaho}}) = -0.042 \tag{51}\]

Equation 52, Variance Inflation Factor. The variance inflation factor for two correlated predictors is one over one minus their squared correlation.

\[\mathrm{VIF} = \frac{1}{1 - r^{2}} \tag{52}\]

Equation 53, Bespoke Subsonic X-10 Leg Speed. Mach 0.9 at twelve kilometres gives a speed of 265.6 metres per second under the standard atmosphere. North American X-10

\[v = M a = 0.9 \times 295.1 = 265.6 \, \text{m/s} \tag{53}\]

Equation 54, Bespoke Subsonic X-10 Leg Duration. The selected thousand-kilometre subsonic leg takes 3,766 seconds. North American X-10

\[t_{\text{sub}} = \frac{1.0 \times 10^{6}}{265.6} = 3766 \, \text{s} = 62.8 \, \text{minutes} \tag{54}\]

Equation 55, Wing Aspect Ratio. Wing span squared divided by reference area gives an aspect ratio of 1.87. North American X-10 Parsch 2002 RTV-A-5 X-10

\[AR = \frac{b^{2}}{S} = \frac{8.59^{2}}{39.48} = 1.87 \tag{55}\]

Equation 56, Static Margin in Chord Units. The static margin is the aerodynamic-centre to centre-of-gravity distance divided by mean chord. Pfyl 1952

\[h_{n} = \frac{x_{ac} - x_{cg}}{\bar{c}} \tag{56}\]

Equation 57, Pitching-Moment Slope from Static Margin. The pitching-moment slope is the negative lift-curve slope times the static margin in chord units. Pfyl 1952 Bond and Swanson 1953

\[C_{m\alpha} = -C_{L\alpha} h_{n} \tag{57}\]

Equation 58, Minimum Drag Components. The minimum drag coefficient is the sum of friction, wave and base drag coefficients.

\[C_{D,\min} = C_{D,f} + C_{D,w} + C_{D,b} \tag{58}\]

Equation 59, Bespoke Wave-Drag Difference. The article infers wave drag by subtracting the reported subsonic minimum drag from the supersonic value. North American X-10

\[C_{D,w} = C_{D,\min,\text{sup}} - C_{D,\min,\text{sub}} = 0.040 - 0.020 = 0.020 \tag{59}\]

Equation 60, Base-Drag Fraction of Minimum Drag. The reported base-drag fraction applied to the total minimum drag gives a coefficient of 0.010. North American X-10

\[C_{D,b} = 0.25 \times 0.040 = 0.010 \tag{60}\]

Equation 61, Normal-Shock Total-Pressure Recovery. The normal-shock relation gives the downstream to upstream total-pressure ratio for a perfect gas. Gillespie and Arbic 1951

\[\frac{p_{02}}{p_{01}} = \left[ \frac{\frac{(\gamma+1) M^{2}}{2}}{1 + \frac{\gamma-1}{2} M^{2}} \right]^{\frac{\gamma}{\gamma-1}} \left[ \frac{\gamma+1}{2 \gamma M^{2} - (\gamma-1)} \right]^{\frac{1}{\gamma-1}} \tag{61}\]

Equation 62, Normal-Shock Recovery at Mach 1.70. The normal-shock total-pressure ratio at the tested Mach number 1.70 is 0.856. Gillespie and Arbic 1951

\[\left. \frac{p_{02}}{p_{01}} \right|_{M = 1.70} = 0.856 \tag{62}\]

Equation 63, Bespoke Two-Shock Inlet Recovery. The article’s sixteen-degree wedge and maximum Mach number give a two-shock total-pressure recovery of 0.889. Gillespie and Arbic 1951

\[\left. \frac{p_{02}}{p_{01}} \right|_{\text{two-shock}, M = 2.05} = 0.889 \tag{63}\]

Equation 64, Bespoke Recovery Gain over a Normal Shock. The selected two-shock inlet recovers 1.275 times the total pressure of a normal shock at the same Mach number. Gillespie and Arbic 1951

\[\frac{0.889}{0.698} = 1.275 \tag{64}\]

Equation 65, Isentropic Ram Total-Pressure Ratio. For a perfect gas the isentropic total-to-static pressure ratio depends on Mach number and specific-heat ratio. Anderson 2002 Modern Compressible Flow

\[\frac{p_{0}}{p_{\infty}} = \left( 1 + \frac{\gamma-1}{2} M^{2} \right)^{\frac{\gamma}{\gamma-1}} = 8.458 \tag{65}\]

Equation 66, Bespoke Break-Even Inlet Recovery. Equating the thrust available after inlet recovery with the article’s drag gives the minimum recovery needed to sustain the recorded speed. Westinghouse J40

\[\eta_{\min} = \frac{D \, p_{0,\text{SL}}}{T_{\text{static}} \, p_{\infty} \, (p_{0}/p_{\infty})} = 0.622 \tag{66}\]

Equation 67, Bespoke Recovery Relative to a Normal Shock. The break-even recovery is 0.892 times the normal-shock recovery at the X-10 maximum Mach number. Westinghouse J40

\[\frac{\eta_{\min}}{\eta_{\text{normal shock}}} = \frac{0.622}{0.698} = 0.892 \tag{67}\]

Equation 68, Dynamic Pressure at the X-10 Ceiling. The standard-atmosphere density and reported maximum Mach number give a dynamic pressure of 43,838 pascals. Anderson 2002 Modern Compressible Flow

\[q = \tfrac{1}{2} \rho v^{2} = \tfrac{1}{2} \times 0.2397 \times 604.9^{2} = 43{,}838 \, \text{Pa} \tag{68}\]

Equation 69, Lift Coefficient at Maximum Take-Off Mass. The coefficient needed to support the reported maximum take-off mass at the X-10 ceiling is 0.109. North American X-10

\[C_{L} = \frac{W}{q S} = \frac{188{,}160}{43{,}838 \times 39.48} = 0.109 \tag{69}\]

Equation 70, Bespoke Lift-to-Drag Ratio at the Ceiling. The article’s drag estimate uses an assumed induced-drag efficiency of 0.6 and gives a lift-to-drag ratio of 2.51. North American X-10

\[\frac{L}{D} = \frac{188{,}160}{75{,}042} = 2.51 \tag{70}\]

Equation 71, Breguet Jet-Range Equation. The jet range equation relates speed, gravity, thrust-specific fuel consumption, lift-to-drag ratio and mass ratio.

\[R = \frac{v}{g \, c} \frac{L}{D} \ln \frac{W_{0}}{W_{1}} \tag{71}\]

Equation 72, Bespoke Range with a Generous Fuel Consumption. A one-per-hour fuel consumption and an assumed mass ratio of 1.8 give 327 kilometres at the selected cruise condition.

\[R = \frac{604.9}{9.80665 \times (1/3600)} \times 2.51 \times \ln 1.8 = 327 \, \text{km} \tag{72}\]

Equation 73, Fuel Fraction from Reported Masses. The reported fuel load is 39 percent of the maximum take-off mass. North American X-10

\[\frac{m_{f}}{m_{0}} = \frac{7484}{19{,}187} = 0.390 \tag{73}\]

Equation 74, Mass Ratio from Reported Weights. The reported maximum take-off and empty weights give a mass ratio of 1.64. North American X-10

\[\frac{W_{0}}{W_{1}} = \frac{19{,}187}{11{,}703} = 1.640 \tag{74}\]

Equation 75, Bespoke Range with the Reported Mass Ratio. Substituting the reported mass ratio into the article’s assumed cruise model gives 275 kilometres. North American X-10

\[R = \frac{604.9}{9.80665 \times (1/3600)} \times 2.51 \times \ln 1.640 = 275 \, \text{km} \tag{75}\]

Equation 76, Bespoke Reported Ranges Relative to the Model. The two reported ranges are 3.67 and 4.98 times the article’s calculated maximum-Mach range. North American X-10 Parsch 2002 RTV-A-5 X-10

\[\frac{1009}{275} = 3.67 \qquad \frac{1370}{275} = 4.98 \tag{76}\]

Equation 77, Bespoke Lift-to-Drag Ratio Required by the Reported Range. At the selected subsonic speed and fuel consumption the smaller reported range requires a lift-to-drag ratio of 20.9. North American X-10 Parsch 2002 RTV-A-5 X-10

\[\frac{L}{D} = \frac{R g c}{v \ln (W_{0}/W_{1})} = \frac{1.009 \times 10^{6} \times 9.80665 \times (1/3600)}{265.6 \times 0.4944} = 20.9 \tag{77}\]

Equation 78, Availability of at Least One Independent System. For two independent systems the probability that at least one is available is one minus the probability that both fail. Lichter and Friedenreich 1962

\[P = 1 - (1 - p_{1})(1 - p_{2}) \tag{78}\]

Equation 79, Bespoke Availability of Two Ninety-Five-Percent Systems. Two systems each assigned 95 percent availability have a combined availability of 99.75 percent. Lichter and Friedenreich 1962

\[P = 1 - (0.05)^{2} = 0.9975 \tag{79}\]

Equation 80, Short-Period Frequency Approximation. A textbook approximation estimates natural frequency from pitch stiffness alone, omitting the other short-period terms. Bond and Swanson 1953

\[\omega_{n} \approx \sqrt{-M_{\alpha}} = \sqrt{\frac{q S \bar{c} \, C_{L\alpha} \, h_{n}}{I_{yy}}} \tag{80}\]

Equation 81, Bespoke Pitch Frequency at Mach 0.95. The selected static margin and three-percent allowance give a frequency of 0.63 radians per second at Mach 0.95. Bond and Swanson 1953

\[\omega_{n} = 0.63 \, \text{rad/s} \quad \text{at Mach 0.95 with a 3 percent margin} \tag{81}\]

Equation 82, Bespoke Pitch Frequency at Mach 2.05. The selected static margin and ten-percent allowance give a frequency of 2.03 radians per second at Mach 2.05. Zarovsky 1951

\[\omega_{n} = 2.03 \, \text{rad/s} \quad \text{at Mach 2.05 with a 10 percent margin} \tag{82}\]

Equation 83, Net Thrust Scaling with Total-Pressure Recovery. At fixed engine geometry the net thrust scales approximately with inlet total-pressure recovery and the ram pressure ratio. Westinghouse J40

\[\frac{T}{T_{\text{SL}}} \approx \eta \, \frac{p_{\infty}}{p_{\text{SL}}} \left( 1 + \frac{\gamma-1}{2} M^{2} \right)^{\frac{\gamma}{\gamma-1}} \tag{83}\]

Equation 84, Recovery Temperature. The recovery temperature is the freestream temperature multiplied by the recovery-factor correction for Mach number. Besserer 1952 De VAULT 1957

\[T_{r} = T_{\infty} \left( 1 + r \frac{\gamma - 1}{2} M^{2} \right) \tag{84}\]

Equation 85, X-10 Recovery Temperature at Maximum Mach. The standard-atmosphere temperature and reported maximum Mach number give a recovery temperature of 378.7 kelvin. Besserer 1952 De VAULT 1957

\[T_{r} = 216.65 \left( 1 + 0.89 \times 0.2 \times 2.05^{2} \right) = 378.7 \, \text{K} = 105.6 \, ^{\circ}\text{C} \tag{85}\]

Equation 86, Navaho Recovery Temperature at Cruise. The standard-atmosphere temperature and reported cruise Mach number give a recovery temperature of 635.5 kelvin. Wade, Navaho, Encyclopedia Astronautica

\[T_{r} = 220.6 \left( 1 + 0.89 \times 0.2 \times 3.25^{2} \right) = 635.5 \, \text{K} = 362.4 \, ^{\circ}\text{C} \tag{86}\]

Equation 87, Mach Number at the Aluminium Temperature Limit. Solving the recovery-temperature relation for Mach gives 2.27 at the conventional aluminium limit and the reported cruise altitude. Wade, Navaho, Encyclopedia Astronautica

\[M_{\text{Al}} = \sqrt{\frac{2}{r (\gamma - 1)} \left( \frac{T_{\text{Al}}}{T_{\infty}} - 1 \right)} = 2.27 \tag{87}\]

Equation 88, Lumped Skin Thermal Time Constant. A lumped skin model has a thermal time constant equal to density times heat capacity times thickness divided by the heat-transfer coefficient.

\[\tau_{\text{skin}} = \frac{\rho c \delta}{h} \tag{88}\]

Equation 89, Bespoke Skin Thermal Time Constant. The selected two-millimetre aluminium skin and convective coefficient of 100 watts per square metre kelvin give a time constant of 48.6 seconds.

\[\tau_{\text{skin}} = \frac{2700 \times 900 \times 0.002}{100} = 48.6 \, \text{s} \tag{89}\]

Equation 90, Mission Reliability for Identical Subsystems. If all n subsystems must work independently and each has reliability p the mission reliability is p raised to n. Biernson 1965 Davies and Haines 1965 Marstrander and Lueg 1969

\[P_{\text{mission}} = p^{n} \tag{90}\]

Equation 91, Bespoke Mission Reliability for Ten Subsystems. Ten subsystems at the selected 95 percent reliability each give a mission reliability of 59.9 percent. Landis 2020 Flashback, The Navaho Missile, Part 1 Blumenthal and Denton 1962

\[P = 0.95^{10} = 0.599 \tag{91}\]

Equation 92, Bespoke X-10 Stall Speed. An assumed twelve-tonne landing mass and unit maximum lift coefficient give a sea-level stall speed of 69.8 metres per second. North American X-10 Montgomery 1975

\[v_{\text{stall}} = \sqrt{\frac{2W}{\rho S C_{L,\max}}} = \sqrt{\frac{2 \times 117{,}680}{1.225 \times 39.48 \times 1.0}} = 69.8 \, \text{m/s} \tag{92}\]

Equation 93, Bespoke Landing Energy. The selected twelve-tonne landing mass and 83.7-metre-per-second approach speed give 42 megajoules of kinetic energy. North American X-10

\[E = \tfrac{1}{2} m v^{2} = \tfrac{1}{2} \times 12{,}000 \times 83.7^{2} = 42.0 \, \text{MJ} \tag{93}\]

Equation 94, Bespoke Braking Distance. At the selected friction coefficient of 0.4 the approach speed requires 893 metres to stop.

\[s = \frac{v^{2}}{2 \mu g} = \frac{7006}{2 \times 0.4 \times 9.80665} = 893 \, \text{m} \tag{94}\]

Equation 95, Bespoke Runway Margin. The reported 3,048-metre runway is 3.41 times the calculated braking distance. Cleary 1991 The 6555th, The NAVAHO Program

\[\frac{3048}{893} = 3.41 \tag{95}\]

Equation 96, Bespoke Drag-Chute Area. The article sizes a chute to match the selected wheel-braking force at touchdown speed and obtains 7.83 square metres. Stowell et al. 1948 Knacke 1992 Parachute Recovery Systems Design Manual

\[S_{c} = \frac{\mu W}{\frac{1}{2} \rho v^{2} C_{D,c}} = \frac{47{,}072}{\frac{1}{2} \times 1.225 \times 7006 \times 1.4} = 7.83 \, \text{m}^{2} \tag{96}\]

Equation 97, Sink Rate on a Glide Slope. The vertical speed on a straight glide slope is forward speed times the negative sine of the flight-path angle. MACKlNNON and Madden 1972

\[\dot{h} = -v \sin \gamma \tag{97}\]

Equation 98, Bespoke Sink Rate at the Approach Condition. The selected 83.7-metre-per-second approach speed and three-degree glide slope give a sink rate of 4.38 metres per second. MACKlNNON and Madden 1972

\[\dot{h} = -83.7 \times \sin 3^{\circ} = -4.38 \, \text{m/s} \tag{98}\]

Equation 99, Exponential Flare Model. The article represents flare height as an exponential decay with its derivative set by the flare time constant. Payne 1968

\[h(t) = h_{0} e^{-t / \tau_{f}}, \qquad \dot{h} = -\frac{h}{\tau_{f}} \tag{99}\]

Equation 100, Radio Horizon with Standard Refraction. The radio horizon uses an effective Earth radius four thirds of the true radius under standard atmospheric refraction.

\[d_{\text{horizon}} = \sqrt{2 \, k \, R_{e} \, h}, \qquad k = \frac{4}{3} \tag{100}\]

Equation 101, Radio Horizon at the X-10 Service Ceiling. At the reported service ceiling the effective-Earth-radius model gives a radio horizon of 482 kilometres. Cleary 1991 The 6555th, The NAVAHO Program

\[d_{\text{horizon}} = \sqrt{2 \times \tfrac{4}{3} \times 6.371 \times 10^{6} \times 13{,}650} = 482 \, \text{km} \tag{101}\]

Equation 102, Bespoke Radio Horizon Relative to a Thousand-Kilometre Leg. The selected one-way leg is 2.08 times the radio horizon at the X-10 service ceiling. Cleary 1991 The 6555th, The NAVAHO Program

\[\frac{1000}{482} = 2.08 \tag{102}\]

Equation 103, Level Turn Radius. For a level coordinated turn the radius depends on speed and load factor through the square root of load factor squared minus one. Muehlner 1962 Rowlandson and Herlihy 1969

\[r = \frac{v^{2}}{g \sqrt{n^{2} - 1}} \tag{103}\]

Equation 104, Bespoke Turn Radius at Maximum Speed. At the X-10 maximum speed and the selected two-g load factor the turn radius is 21.5 kilometres. North American X-10

\[r = \frac{604.9^{2}}{9.80665 \times \sqrt{3}} = 21.5 \, \text{km} \tag{104}\]

Equation 105, Bespoke Course-Reversal Time. A half-circle at the selected maximum speed and two-g turn radius takes 112 seconds. North American X-10

\[t_{\text{turn}} = \frac{\pi r}{v} = \frac{\pi \times 21{,}541}{604.9} = 112 \, \text{s} \tag{105}\]

Equation 106, Dive Ground Range. For a straight dive at flight-path angle gamma the ground range is altitude divided by the tangent of the angle. Wheeler 1946

\[x = \frac{h}{\tan \gamma} \tag{106}\]

Equation 107, Sensitivity of Dive Range to Flight-Path Angle. Differentiating the dive-range relation gives its sensitivity to flight-path angle. Wheeler 1946

\[\frac{dx}{d\gamma} = -\frac{h}{\sin^{2} \gamma} \tag{107}\]

Equation 108, Bespoke Dive-Range Sensitivity at Forty-Five Degrees. From 24 kilometres at a selected 45-degree dive angle the range changes by 48 kilometres per radian. Wheeler 1946

\[\frac{dx}{d\gamma} = -\frac{24{,}000}{0.5} = -48{,}000 \, \text{m/rad} \tag{108}\]

Equation 109, Fraction of Vehicles Lost. The reported loss of twelve among thirteen vehicles is 92.3 percent. Dunmire and Lopresti 1963 Broglio 1961 Parsch 2002 RTV-A-5 X-10

\[\frac{12}{13} = 0.923 \tag{109}\]

Equation 110, Reynolds Number. The Reynolds number is density times speed times reference length divided by dynamic viscosity.

\[Re = \frac{\rho v \bar{c}}{\mu} \tag{110}\]

Equation 111, Dynamic Viscosity from Sutherland Relation. Sutherland’s relation gives the dynamic viscosity of air from temperature.

\[\mu = \frac{1.458 \times 10^{-6} \, T^{3/2}}{T + 110.4} = 1.42 \times 10^{-5} \, \text{Pa s} \tag{111}\]

Equation 112, Full-Scale Reynolds Number at the Ceiling. The standard-atmosphere state and reported chord give a full-scale Reynolds number of 46.8 million. X-7

\[Re_{\text{full}} = \frac{0.2397 \times 604.9 \times 4.595}{1.42 \times 10^{-5}} = 4.68 \times 10^{7} \tag{112}\]

Equation 113, Model Reynolds Number Relative to Full Scale. The reported model Reynolds-number range spans 19 to 51 percent of the full-scale value. X-7

\[\frac{Re_{\text{model}}}{Re_{\text{full}}} = 0.19 \; \text{to} \; 0.51 \tag{113}\]

Equation 114, Mission Central Angle. The ten-thousand-kilometre surface range is 1.570 radians at the Earth’s radius. Parsch 2002 SM-64

\[\Phi = \frac{R_{m}}{R_{e}} = \frac{1.0 \times 10^{7}}{6.371 \times 10^{6}} = 1.570 \, \text{rad} \tag{114}\]

Equation 115, Minimum-Energy Ballistic Speed Parameter. For the minimum-energy ballistic trajectory the nondimensional burnout speed follows from the mission central angle. Parsch 2002 SM-64

\[\lambda = \frac{V^{2}}{g R_{e}} = \frac{2 \sin (\Phi/2)}{1 + \sin (\Phi/2)} = 0.828 \tag{115}\]

Equation 116, Minimum-Energy Ballistic Speed. The speed parameter gives a burnout speed of 7,193 metres per second for the selected range. Parsch 2002 SM-64

\[V = \sqrt{0.828 \times 9.80665 \times 6.371 \times 10^{6}} = 7193 \, \text{m/s} \tag{116}\]

Equation 117, Ballistic Semi-Major Axis. The vis-viva relation gives the ballistic trajectory’s semi-major axis from the speed parameter. Parsch 2002 SM-64

\[a = \frac{R_{e}}{2 - \lambda} = 5.437 \times 10^{6} \, \text{m} \tag{117}\]

Equation 118, Minimum-Energy Ballistic Flight Time. The difference in mean anomaly divided by mean motion gives the flight time on the minimum-energy trajectory. Parsch 2002 SM-64

\[t_{\text{ballistic}} = \frac{\Delta M}{n} = 1932 \, \text{s} = 32.2 \, \text{minutes} \tag{118}\]

Equation 119, Bespoke Cruise-to-Ballistic Time Ratio. At the selected ten-thousand-kilometre range the cruise vehicle remains in flight 5.35 times longer than the minimum-energy ballistic trajectory. Parsch 2002 SM-64

\[\frac{t_{\text{cruise}}}{t_{\text{ballistic}}} = \frac{172.2}{32.2} = 5.35 \tag{119}\]

Equation 120, Modern Gyroscope Drift Relative to the Navaho Requirement. The reported 0.003-degree-per-hour gyroscope drift is 1.20 times the historical 0.0025-degree-per-hour requirement. Chen et al. 2025a Wade, Navaho, Encyclopedia Astronautica

\[\frac{0.003}{0.0025} = 1.20 \tag{120}\]

Equation 121, Modern Gyroscope Drift Error over the Mission. A reported gyroscope drift of 0.003 degrees per hour produces 957 metres of secular error over the Navaho mission. Chen et al. 2025a Wade, Navaho, Encyclopedia Astronautica

\[\delta x = R_{e} \varepsilon t = 6.371 \times 10^{6} \times 1.454 \times 10^{-8} \times 10{,}333 = 957 \, \text{m} \tag{121}\]

Equation 122, Isentropic Ram Pressure Ratio. The ideal ram-pressure ratio at a given Mach number follows the perfect-gas isentropic relation. Hill and Peterson 1991 Mechanics and Thermodynamics of Propulsion

\[\frac{p_{0}}{p_{\infty}} = \left( 1 + \frac{\gamma - 1}{2} M^{2} \right)^{\frac{\gamma}{\gamma - 1}} \tag{122}\]

Equation 123, Specific Energy of the Navaho Booster. The booster speed and altitude give a specific mechanical energy of 0.571 megajoules per kilogram. Hill and Peterson 1991 Mechanics and Thermodynamics of Propulsion Reilly and Welna 1955 Cleary 1991 The 6555th, The NAVAHO Program

\[e = \tfrac{1}{2} v^{2} + g h = \tfrac{1}{2} (818.9)^{2} + 9.80665 \times 24{,}000 = 0.571 \, \text{MJ/kg} \tag{123}\]

Notation

• $a$, the speed of sound and later the semi-major axis
• $\gamma$, the ratio of specific heats and in the dive relation the flight-path angle
• $R$, the universal gas constant and the range in the Breguet relation
• $T$, the atmospheric temperature, the Schuler period and the engine thrust
• $t$, elapsed time
• $R_{\text{mission}}$, the Navaho mission range
• $v$, vehicle speed
• $\delta x_{\text{secular}}$, the secular position error from gyroscope drift
• $R_{e}$, the radius of the Earth
• $\varepsilon$, the gyroscope drift rate
• $\mathrm{CEP}$, the circular error probable
• $\delta v$, the inertial navigator velocity error
• $g$, gravitational acceleration
• $\phi$, the platform tilt from the vertical
• $\nabla$, the accelerometer bias
• $\omega_{s}$, the Schuler angular frequency
• $C_{1}$, an initial-condition coefficient in the homogeneous Schuler solution
• $C_{2}$, an initial-condition coefficient in the homogeneous Schuler solution
• $T_{s}$, the Schuler period
• $\delta x_{\nabla}$, the bounded position error from accelerometer bias
• $\delta x_{\varepsilon}$, the position error from gyroscope drift
• $t_{\times}$, the crossover time at which the two error contributions are equal
• $\delta x_{\phi}$, the bounded position error from residual platform tilt
• $\phi_{0}$, the residual platform tilt
• $\psi$, the launch azimuth error
• $\sigma_{s}$, the standard error of an estimated sample standard deviation
• $s$, the sample standard deviation and later the braking distance
• $n$, the sample count, number of subsystems, turn load factor and orbital mean motion
• $A$, the coefficient of the bounded Schuler error signature
• $B$, the coefficient of the secular drift error signature
• $r$, the error-signature correlation, recovery factor and turn radius
• $\mathrm{VIF}$, the variance inflation factor
• $M$, Mach number
• $AR$, the wing aspect ratio
• $b$, wing span
• $S$, wing reference area
• $h_{n}$, the static margin in mean-chord units
• $x_{ac}$, the aerodynamic-centre position
• $x_{cg}$, the centre-of-gravity position
• $\bar{c}$, the mean aerodynamic chord
• $C_{m\alpha}$, the pitching-moment coefficient slope with angle of attack
• $C_{L\alpha}$, the lift-coefficient slope with angle of attack
• $C_{D,\min}$, the minimum drag coefficient
• $p_{0}$, stagnation pressure
• $p_{\infty}$, ambient static pressure
• $\eta$, inlet total-pressure recovery
• $D$, vehicle drag
• $T_{\text{SL}}$, the installed static thrust at sea level
• $q$, dynamic pressure
• $W$, aircraft weight
• $L$, aerodynamic lift
• $c$, thrust-specific fuel consumption and later specific heat capacity
• $W_{0}$, the initial aircraft weight
• $W_{1}$, the final aircraft weight
• $m_{f}$, fuel mass
• $m_{0}$, initial vehicle mass
• $P$, probability of at least one system being available
• $p$, the reliability of one subsystem and pressure in the compressible-flow relations
• $\omega_{n}$, the short-period natural frequency
• $I_{yy}$, the pitch moment of inertia
• $T_{r}$, the recovery temperature
• $T_{\infty}$, freestream temperature
• $\tau_{\text{skin}}$, the thermal time constant of the skin
• $\rho$, air density
• $\delta$, skin thickness
• $h$, altitude and the convective heat-transfer coefficient
• $v_{\text{stall}}$, stall speed
• $C_{L,\max}$, maximum lift coefficient
• $E$, kinetic energy
• $m$, vehicle mass
• $\mu$, braking friction coefficient and dynamic viscosity
• $S_{c}$, drag-chute area
• $C_{D,c}$, drag-chute drag coefficient
• $\dot{h}$, vertical speed
• $h_{0}$, initial flare height
• $\tau_{f}$, flare time constant
• $d_{\text{horizon}}$, radio horizon distance
• $k$, effective-Earth-radius multiplier for atmospheric refraction
• $t_{\text{turn}}$, time to complete a course reversal
• $x$, ground range in the dive relation
• $\Phi$, the central angle corresponding to the mission range
• $R_{m}$, the mission range in the ballistic calculation
• $\lambda$, the squared burnout-speed ratio to circular speed
• $V$, ballistic burnout speed
• $\Delta M$, the change in mean anomaly between launch and impact
• $e$, orbital eccentricity and later specific mechanical energy
• $Re$, the Reynolds number
• $M_{\alpha}$, the aerodynamic pitching-moment stiffness
• $p_{\text{SL}}$, sea-level static pressure
• $M_{\text{Al}}$, the Mach number at the selected aluminium temperature limit
• $T_{\text{Al}}$, the selected aluminium temperature limit
• $C_{D,f}$, the friction drag coefficient
• $C_{D,w}$, the wave drag coefficient
• $C_{D,b}$, the base drag coefficient
• $P_{\text{mission}}$, the probability that every required subsystem works
• $p_{1}$, the probability that the first guidance system is available
• $p_{2}$, the probability that the second guidance system is available

References

Primary Sources, Peer-Reviewed

• “572. Drift Data for the Cryogenic Gyroscope.” 1965. Vacuum 15 (6): 327. https://doi.org/10.1016/0042-207x(65)91001-8
• “97/01394 Liquid-Fueled Ramjet Engine.” 1997. Fuel and Energy Abstracts 38 (2): 110. https://doi.org/10.1016/s0140-6701(97)84221-x
• Abbas, Laith K., Chen Qian, Piergiovanni Marzocca, Gürdal Zafer, and Abdalla Mostafa. 2008. “Active Aerothermoelastic Control of Hypersonic Double-Wedge Lifting Surface.” Chinese Journal of Aeronautics 21 (1): 8–18. https://doi.org/10.1016/s1000-9361(08)60002-3
• Abbas, Laith K., Xiao-ting Rui, and P. Marzocca. 2009. “Non-Linear Aerothermoelastic Modeling and Behavior of a Double-Wedge Lifting Surface.” Journal of Shanghai Jiaotong University (Science) 14 (5): 620–25. https://doi.org/10.1007/s12204-009-0620-3
• Abbas, Tasadduq, Zhang Yunyan, and Li Yanjun. 2011. “SINS Initial Alignment for Small Tilt and Large Azimuth Misalignment Angles.” In 2011 IEEE 3rd International Conference on Communication Software and Networks. IEEE. https://doi.org/10.1109/iccsn.2011.6013913
• Abbasi, Pouya, and Mohammad Haeri. 2019. “Accuracy Improvement of GPS/INS Navigation System Using Extended Kalman Filter.” In 2019 6th International Conference on Control, Instrumentation and Automation (ICCIA). IEEE. https://doi.org/10.1109/iccia49288.2019.9030830
• Abd-elatif, M. A., Long-jun Qian, and Yu-ming Bo. 2016. “Optimization of Three-Loop Missile Autopilot Gain under Crossover Frequency Constraint.” Defence Technology 12 (1): 32–38. https://doi.org/10.1016/j.dt.2015.08.006
• Abdel-Hafez, Mamoun F. 2011. “On the Development of an Inertial Navigation Error-Budget System.” Journal of the Franklin Institute 348 (1): 24–44. https://doi.org/10.1016/j.jfranklin.2009.02.008
• Abdel-Rahim, M., M. El-Geneidy, and M. Rizk. 1993. “Robust Design of Stochastic Controller for a Guidance System of Command Guided Missile.” In 1993 American Control Conference. IEEE. https://doi.org/10.23919/acc.1993.4792902
• Abdelaziz, Nader, and Ahmed El-Rabbany. 2022. “LiDAR/Visual SLAM-Aided Vehicular Inertial Navigation System for GNSS-Denied Environments.” In 2022 5th International Conference on Communications, Signal Processing, and their Applications (ICCSPA). IEEE. https://doi.org/10.1109/iccspa55860.2022.10019210
• Abdelaziz, Nader, and Ahmed El-Rabbany. 2023. “INS/LIDAR/Stereo SLAM Integration for Precision Navigation in GNSS-Denied Environments.” Sensors 23 (17): 7424. https://doi.org/10.3390/s23177424
• Abdollahi, M. R., and Seid H. Pourtakdoust. 2026. “Magnetometer-Based Enhanced Visual-Inertial Odometry for Reliable Long-Range Navigation in GNSS-Denied High-Altitude Environment.” Aerospace Science and Technology 176: 112673. https://doi.org/10.1016/j.ast.2026.112673
• Abedi, M., R. Askari, and M. R. Soltani. 2020. “Numerical Simulation of Inlet Buzz.” Aerospace Science and Technology 97: 105547. https://doi.org/10.1016/j.ast.2019.105547
• Abraham, Troy, David Lazzara, and Douglas Hunsaker. 2024. “Multifidelity Comparison of Supersonic Wave Drag Prediction Methods Using Axisymmetric Bodies.” Aerospace 11 (5): 359. https://doi.org/10.3390/aerospace11050359
• Abrashov, Sergey, Rachid Malti, Xavier Moreau, Mathieu Moze, François Aioun, and Franck Guillemard. 2018. “Optimal Input Design for Continuous-Time System Identification.” Communications in Nonlinear Science and Numerical Simulation 60: 92–99. https://doi.org/10.1016/j.cnsns.2017.12.013
• Abrashov, Sergey, Rachid Malti, Mathieu Moze, Xavier Moreau, and Franck Guillemard. 2015. “Optimal Input Design for Continuous-Time System Identification: Application to Fractional Systems.” IFAC-PapersOnLine 48 (28): 1307–12. https://doi.org/10.1016/j.ifacol.2015.12.312
• Abu-Akeel, A. K. 1969. “Damping of High-Frequency Brake Vibrations in Aircraft Landing Gear.” Journal of Aircraft 6 (1): 24–30. https://doi.org/10.2514/3.43996
• Abu-Jbara, Khaled, Wael Alheadary, Ganesh Sundaramorthi, and Christian Claudel. 2015. “A Robust Vision-Based Runway Detection and Tracking Algorithm for Automatic UAV Landing.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152407
• Achilli, V., P. Baldi, and S. Zerbini. 1983. “Astronomic Determinations of Deflection of the Vertical.” Survey Review 27 (208): 75–80. https://doi.org/10.1179/003962683791476081
• Acquatella B, Paul, Lâle Evrim Briese, and Klaus Schnepper. 2020. “Guidance Command Generation and Nonlinear Dynamic Inversion Control for Reusable Launch Vehicles.” Acta Astronautica 174: 334–46. https://doi.org/10.1016/j.actaastro.2020.04.002
• Adams, Benjamin, Calum Macrae, Mani Entezami, et al. 2021. “The Development of a High Data Rate Atom Interferometric Gravimeter (HIDRAG) for Gravity Map Matching Navigation.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430461
• Aeinfar, Vahid, Arash Sadeghzadeh, and Hamidreza Momeni. 2011. “Control-Oriented Input Design for Open-Loop System Identification.” IFAC Proceedings Volumes 44 (1): 13167–72. https://doi.org/10.3182/20110828-6-it-1002.02722
• Affleck, C. A., and A. Jircitano. n.d. “Passive Gravity Gradiometer Navigation System.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66158
• Aggarwal, Romesh K., and Charles R. Moore. 1998. “Terminal Guidance Algorithm for Ramjet-Powered Missiles.” Journal of Guidance, Control, and Dynamics 21 (6): 862–66. https://doi.org/10.2514/2.4349
• Agüero, Juan C., and Graham C. Goodwin. 2006. “Identifiability of Errors in Variables Dynamic Systems.” IFAC Proceedings Volumes 39 (1): 196–201. https://doi.org/10.3182/20060329-3-au-2901.00025
• Agüero, Juan C., and Graham C. Goodwin. 2008a. “Identifiability of EIV Dynamic Systems with Non-Stationary Data.” IFAC Proceedings Volumes 41 (2): 444–49. https://doi.org/10.3182/20080706-5-kr-1001.00075
• Agüero, Juan C., and Graham C. Goodwin. 2008b. “Identifiability of Errors in Variables Dynamic Systems.” Automatica 44 (2): 371–82. https://doi.org/10.1016/j.automatica.2007.06.011
• Ahmadian, Narjes. 2026. “Performance Analysis of a Gravity-Aided Inertial Navigation System Using the GAME Algorithm in Various Navigation Scenarios.” Measurement 263: 120161. https://doi.org/10.1016/j.measurement.2025.120161
• Ai, Wenyu, Sheng Zhong, Yue Leng, and Shibo Wang. 2023. “A Real-Time Autonomous Gravity Measurement Method for Underwater Gravity-Aided Navigation.” IEEE Access 11: 135728–37. https://doi.org/10.1109/access.2023.3338537
• “The Air Force Approach to Reliability in Ballistic Missile Weapon Systems.” 1963. Microelectronics Reliability 2 (2): 156. https://doi.org/10.1016/0026-2714(63)90209-9
• Ajayan, Aswathy, G. S. Anish, and Sumayya Jaleel. 2024. “Deep Learning Based Bias Compensation for Tuning Fork Gyroscope.” In 2024 International Conference on Futuristic Technologies in Control Systems & Renewable Energy (ICFCR). IEEE. https://doi.org/10.1109/icfcr64128.2024.10762953
• Akcayir, Y., and Y. Ozkazanc. 2003. “Gyroscope Drift Estimation Analysis in Land Navigation Systems.” In Proceedings of 2003 IEEE Conference on Control Applications, 2003. CCA 2003., vol. 2. IEEE. https://doi.org/10.1109/cca.2003.1223234
• Akdoğan, Yunus Aytaç, Gonca Okay Ahi, and Hasan Yildiz. 2024. “Computation of Gravimetric Geoid Model Using Free Air Vertical Gravity Gradient Anomaly in Geoid-Quasigeoid Formula.” Journal of Applied Geophysics 220: 105277. https://doi.org/10.1016/j.jappgeo.2023.105277
• Akhmadiev, T. M., Yu. V. Filatov, E. V. Shalymov, and V. Yu. Venediktov. 2021. “Investigation of the Influence of Resonator Losses and Coupling Coefficient on the Characteristics of an Optical Resonator Gyroscope with a Mach-Zehnder Modulator.” In 2021 Photonics & Electromagnetics Research Symposium (PIERS). IEEE. https://doi.org/10.1109/piers53385.2021.9694741
• Akmeliawati, Rini, and Iven M. Y. Mareels. 2010. “Nonlinear Energy-Based Control Method for Aircraft Automatic Landing Systems.” IEEE Transactions on Control Systems Technology 18 (4): 871–84. https://doi.org/10.1109/tcst.2009.2030788
• Aksoy, Mehmet Alper, and Onur Son. 2026. “Performance Modelling and Efficiency Analysis of a Micro Turbojet Engine under Varying Flight Conditions.” Journal of the Brazilian Society of Mechanical Sciences and Engineering 48 (4): 238. https://doi.org/10.1007/s40430-026-06317-6
• Aktakka, Ethem Erkan, Jong-Kwan Woo, and Khalil Najafi. 2017. “On-Chip Characterization of Scale-Factor of a MEMS Gyroscope via a Micro Calibration Platform.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935684
• Alam, Mushfiqul, Martin Sipos, Jan Rohac, and Jakub Simanek. 2015. “Calibration of a Multi-Sensor Inertial Measurement Unit with Modified Sensor Frame.” In 2015 IEEE International Conference on Industrial Technology (ICIT). IEEE. https://doi.org/10.1109/icit.2015.7125387
• Albeshbeshy, Ahmed F., Mohammed A. H. Abozied, Mohamed Reda, and Ahmed M. Kamel. 2024. “Precise Gyroscope Bias Estimation Based on Kalman Filter and Allan Variance Analysis.” In 2024 6th Novel Intelligent and Leading Emerging Sciences Conference (NILES). IEEE. https://doi.org/10.1109/niles63360.2024.10753196
• Ali, Muhammad. 2016. “Compensation of Temperature and Acceleration Effects on MEMS Gyroscope.” In 2016 13th International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast.2016.7429889
• Ali, Jamshaid, and Jiancheng Fang. 2009. “Realization of an Autonomous Integrated Suite of Strapdown Astro-Inertial Navigation Systems Using Unscented Particle Filtering.” Computers & Mathematics with Applications 57 (2): 169–83. https://doi.org/10.1016/j.camwa.2008.07.042
• Ali, Jamshaid, and Muhammad Nzar. 2008. “Realization of Initial Alignment Algorithm for Strapdown Inertial Navigation System Using Central Difference Filter.” IFAC Proceedings Volumes 41 (2): 4731–36. https://doi.org/10.3182/20080706-5-kr-1001.00796
• Ali, A., and K. Sartuk. 2003. “Development of a Satellite Borne Tactical Ballistic Missile Trajectory Prediction Tool.” In International Conference on Recent Advances in Space Technologies, 2003. RAST ‘03. Proceedings of. IEEE. https://doi.org/10.1109/rast.2003.1303985
• Ali, Jamshaid, and Muhammad Ushaq. 2009. “A Consistent and Robust Kalman Filter Design for in-Motion Alignment of Inertial Navigation System.” Measurement 42 (4): 577–82. https://doi.org/10.1016/j.measurement.2008.10.002
• Ali, Atif, and Wang Qing. 2008. “Smoothing the Response of a Gain Scheduled Autopilot for Flexible Flight Vehicle by Online Tuning Based on Neural Networks.” In 2008 IEEE International Multitopic Conference. IEEE. https://doi.org/10.1109/inmic.2008.4777788
• Ali, Jamshaid, Changyun Zhang, and Jiancheng Fang. 2006. “An Algorithm for Astro-Inertial Navigation Using CCD Star Sensors.” Aerospace Science and Technology 10 (5): 449–54. https://doi.org/10.1016/j.ast.2006.01.004
• Alijani, Morteza, and Anas Osman. 2021. “Minimum-Time Path Planning for Autonomous Landing of UAV on Aerial Drone Carrier.” In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas51884.2021.9476875
• Alikhani, Mohammad, and Amirhossein Nikoofard. 2026a. “Learning-Aided Fusion of SfM and IEKF for Visual–inertial Odometry.” Measurement 279: 121479. https://doi.org/10.1016/j.measurement.2026.121479
• Alikhani, Mohammad, and Amirhossein Nikoofard. 2026b. “Long-Term Error Compensation in Inertial IEKF-Based Localization with Transformer-Adaptive Noise Tuning and IMU Missing Data Handling.” Measurement 257: 118928. https://doi.org/10.1016/j.measurement.2025.118928
• Alkhoury, Ziad, Mihály Petreczky, and Guillaume Mercère. 2017. “Identifiability of Affine Linear Parameter-Varying Models.” Automatica 80: 62–74. https://doi.org/10.1016/j.automatica.2017.01.029
• Alpert, Joel. 1988. “Miss Distance Analysis for Command Guided Missiles.” Journal of Guidance, Control, and Dynamics 11 (6): 481–87. https://doi.org/10.2514/3.20343
• Alroqi, Abdurrhman A., Weiji Wang, and Yong Zhao. 2017. “Aircraft Tire Temperature at Touchdown with Wheel Prerotation.” Journal of Aircraft 54 (3): 926–38. https://doi.org/10.2514/1.c033916
• Alvelda, P., M. San Martin, C. Bell, and J. Barhen. 1988. “Spacecraft Attitude Determination Using Neural Star Pattern Recognition.” Neural Networks 1: 421. https://doi.org/10.1016/0893-6080(88)90445-5
• Alvord, David, Jesus Arias, Elizaveta Latash, and AnnMarie Spexet. 2024. “Reusable Launch Vehicle Utilization of Predictive Maintenance to Address Risk Reduction Assessment.” In 2024 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero58975.2024.10521242
• Amatucci, V. A., A. L. Addy, and J. C. Dutton. 1982. “Pressure Recovery in a Constant-Area, Two-Stream Supersonic Diffuser.” AIAA Journal 20 (9): 1308–9. https://doi.org/10.2514/3.7977
• Amin, Nasim F., and David J. Hollweger. 1983. “F/A-18 Inlet/engine Compatibility Flight Test Results.” Journal of Aircraft 20 (8): 641–49. https://doi.org/10.2514/3.44924
• An, Wen, Jiangning Xu, Miao Wu, and Pengfei Jiang. 2021. “A Method of Deflection of the Vertical Measurement Based on Phase Correction.” IEEE Access 9: 5933–42. https://doi.org/10.1109/access.2020.3047392
• Anbu, N. Allan, and D. Jayaprasanth. 2019. “Integration of Inertial Navigation System with Global Positioning System Using Extended Kalman Filter.” In 2019 International Conference on Smart Systems and Inventive Technology (ICSSIT). IEEE. https://doi.org/10.1109/icssit46314.2019.8987949
• Anderson, B. O., and M. Deistler. 1983. “Identifiability in Dynamic Errors-in-Variables Models.” In The 22nd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1983.269851
• Anderson, L., and J. Vincent. 1985. “Application of System Identification to Aircraft Flight Test Data Processing.” In 1985 24th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1985.268918
• Andert, Franz, and Luis Mejias. 2015. “Improving Monocular SLAM with Altimeter Hints for Fixed-Wing Aircraft Navigation and Emergency Landing.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152390
• Andreev, V. D. 1964. “On the General Equations of Inertial Navigation.” Journal of Applied Mathematics and Mechanics 28 (2): 297–315. https://doi.org/10.1016/0021-8928(64)90164-9
• Andrews, Angus. 1979. “Method for Error Budgeting of Inertial Navigation Systems.” Journal of Guidance and Control 2 (5): 438–40. https://doi.org/10.2514/3.55903
• Anguelova, Milena, and Bernt Wennberg. 2007. “State Elimination and Identifiability of Delay Parameters for Nonlinear Systems with Multiple Time-Delays.” IFAC Proceedings Volumes 40 (23): 209–14. https://doi.org/10.1016/s1474-6670(17)69289-9
• Anli Shang, Wen-jin Gu, Dehai Yu, and Yong Liang. n.d.-a. “Design of Missile Autopilot Applying the Immersion and Invariance Algorithm.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 6. IEEE. https://doi.org/10.1109/wcica.2004.1343780
• Anli Shang, Wenjin Gu, Yuman Yuan, and Congying Li. n.d.-b. “Missile Autopilot Design Based on Second Order Sliding Modes Control.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 2. IEEE. https://doi.org/10.1109/wcica.2004.1340797
• Annergren, Mariette, Christian A. Larsson, Hakan Hjalmarsson, Xavier Bombois, and Bo Wahlberg. 2017. “Application-Oriented Input Design in System Identification: Optimal Input Design for Control [Applications of Control].” IEEE Control Systems 37 (2): 31–56. https://doi.org/10.1109/mcs.2016.2643243
• Anthony, Matthews. 2018. “The Operation and Mechanization of the Hemispherical Resonator Gyroscope.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373357
• Aoki, Masanao. 1966. “On Observability, Identifiability and Controllability of Stochastic Discrete-Time Dynamic Systems.” In Fifth Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/sap.1966.271163
• Aoki, Nobuaki, and Genya Ishigami. 2022. “Autonomous Tracking and Landing of an Unmanned Aerial Vehicle on a Ground Vehicle in Rough Terrain.” Advanced Robotics 37 (5): 344–55. https://doi.org/10.1080/01691864.2022.2141078
• Apostolakis, I. S., and D. Jordan. 1992. “Robustness Analysis of a Multirate Digital Controller Design for a Multivariable Missile Autopilot.” In [Proceedings 1992] The First IEEE Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.1992.269892
• “Appendix: Selected Cruise-Missile Systems and Programmes.” 2001. Adelphi Papers 41 (339): 99–100. https://doi.org/10.1080/05679320108457658
• “Application of Improved L/sub 2/-Gain Synthesis on LPV Missile Autopilot Design.” 1999. In Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251). IEEE. https://doi.org/10.1109/acc.1999.786188
• “Approach to Reliability for the SM-2 Missile.” 1973. Microelectronics Reliability 12 (5): 409. https://doi.org/10.1016/0026-2714(73)90040-1
• Aprovitola, Andrea, Pasquale Emanuele Di Nuzzo, Giuseppe Pezzella, and Antonio Viviani. 2021. “Aerodynamic Analysis of a Supersonic Transport Aircraft at Landing Speed Conditions.” Energies 14 (20): 6615. https://doi.org/10.3390/en14206615
• Aprovitola, Andrea, Oleksandr Dyblenko, Giuseppe Pezzella, and Antonio Viviani. 2022. “Aerodynamic Analysis of a Supersonic Transport Aircraft at Low and High Speed Flow Conditions.” Aerospace 9 (8): 411. https://doi.org/10.3390/aerospace9080411
• Apstein, E., and O. Titow. 1996. “Area Rule and Volume Rule for Integral Quantities.” Acta Mechanica 116 (1–4): 45–60. https://doi.org/10.1007/bf01171419
• Arambel, P. O., and G. Tadmor. 1997. “Identifiability and Persistent Excitation in Full Matrix Fraction Parameter Estimation.” Automatica 33 (4): 689–92. https://doi.org/10.1016/s0005-1098(96)00201-4
• Armin, Ardalan, Toby O. Alexander, and Chris P. Fell. 2025. “Electrostatic Calibration of MEMS Accelerometers.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037202
• Armstrong, R. S., and S. R. Miller. 1968. “Subsonic Aerodynamic Performance of Nozzle Installations in Supersonic Airplanes.” Journal of Aircraft 5 (3): 230–35. https://doi.org/10.2514/3.43932
• Arshal, George. 1987. “Error Equations of Inertial Navigation.” Journal of Guidance, Control, and Dynamics 10 (4): 351–58. https://doi.org/10.2514/3.20225
• Arthur, L. M., and R. Scott Kemp. 2025. “Emerging Accuracy of Ballistic Missile Guidance Systems.” Science & Global Security 33 (1–3): 48–67. https://doi.org/10.1080/08929882.2025.2557088
• Asad, Muhammad, Sumair Khan, Ihsanullah, et al. 2020. “A Split Target Detection and Tracking Algorithm for Ballistic Missile Tracking during the Re-Entry Phase.” Defence Technology 16 (6): 1142–50. https://doi.org/10.1016/j.dt.2019.12.008
• Asadian, Mohammad H., Yusheng Wang, Sina Askari, and Andrei Shkel. 2017. “Controlled Capacitive Gaps for Electrostatic Actuation and Tuning of 3D Fused Quartz Micro Wineglass Resonator Gyroscope.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935688
• Asif, Ghufran Aqeel, Nur Hazliza Ariffin, Norazreen Ab Aziz, Mohd Hadri Hafiz Mukhtar, and Norhana Arsad. 2024. “True North Measurement: A Comprehensive Review of Carouseling and Maytagging Methods of Gyrocompassing.” Measurement 226: 114121. https://doi.org/10.1016/j.measurement.2024.114121
• Askari, Rasoul, and Mahdi Abedi. 2026. “High Subsonic Performance of a Diverterless Supersonic Inlet at Various Angles of Attack: An Experimental Investigation.” Flow Measurement and Instrumentation 107: 103045. https://doi.org/10.1016/j.flowmeasinst.2025.103045
• Aslam, Qamar Hameed, Asif Iqbal, Farhat Bibi, and Sidra Bibi. 2008. “Error Estimation of Inertial Sensors Using Allan Variance.” IFAC Proceedings Volumes 41 (1): 167–71. https://doi.org/10.3182/20080408-3-ie-4914.00030
• Aslan, Ahmet Arif, and Erdinc Tatar. 2026. “No-Drift Mode-Matched Ring Gyroscope with on-Chip Stress and Temperature Calibration.” In 2026 IEEE 39th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems64181.2026.11419360
• Asouti, Varvara, Marina Kontou, and Kyriakos Giannakoglou. 2023. “Radial Basis Function Surrogates for Uncertainty Quantification and Aerodynamic Shape Optimization under Uncertainties.” Fluids 8 (11): 292. https://doi.org/10.3390/fluids8110292
• “Assessing Missile System Reliability.” 1972. Microelectronics Reliability 11 (6): 476. https://doi.org/10.1016/0026-2714(72)90035-2
• Atashgah, M. A. Amiri, Hamed Mohammadkarimi, and Mehrdad Ebrahimi. 2023. “A Fast Strapdown Gyrocompassing Algorithm Based on INS Differential Errors.” Scientific Reports 13 (1): 15297. https://doi.org/10.1038/s41598-023-42235-6
• Atmaca, Direnc, Coen de Visser, and Erik-Jan van Kampen. 2025. “Online Inertial Measurement Unit Fault Identification and Active Fault-Tolerant Flight Control.” Journal of Guidance, Control, and Dynamics 48 (10): 2389–98. https://doi.org/10.2514/1.g009147
• Attias, L., and J. Sveitis. n.d. “Inertial Navigation System Intelligent Diagnostic Expert (INSIDE).” In IEEE Conference on Aerospace and Electronics. IEEE. https://doi.org/10.1109/naecon.1990.112950
• August, Elias. 2009. “Parameter Identifiability and Optimal Experimental Design.” In 2009 International Conference on Computational Science and Engineering. IEEE. https://doi.org/10.1109/cse.2009.39
• Austin, M. 1965. “Effect of Multiple Scattering on Line-of-Sight Propagation.” IEEE Transactions on Antennas and Propagation 13 (5): 737–42. https://doi.org/10.1109/tap.1965.1138507
• “Automatic Landing System Successfully Lands Navaho X-10.” 1958. Electrical Engineering 77 (1): 115–16. https://doi.org/10.1109/ee.1958.6445593
• Avdeenko, Tatyana. 2002. “On Structural Identifiability of System Parameters of Linear Models.” IFAC Proceedings Volumes 35 (1): 253–58. https://doi.org/10.3182/20020721-6-es-1901.00453
• Avrutov, Vadym. 2015. “Scalar Method of Fault Diagnosis of Inertial Measurement Unit.” Advances in Aerospace Engineering 2015: 1–10. https://doi.org/10.1155/2015/264564
• Avrutov, Vadym, Nadiia Bouraou, Oleg Nesterenko, Sergii Holovach, Oleksii Hehelskyi, and Olha Pazdrii. 2026. “Velocity-Aided Navigation in GNSS-Denied Environments.” Sensors 26 (15): 5006. https://doi.org/10.3390/s26155006
• Avrutov, V. V., D. V. Buhaiov, and V. V. Meleshko. 2017. “Gyrocompassing Mode of the Attitude and Heading Reference System.” In 2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD). IEEE. https://doi.org/10.1109/apuavd.2017.8308793
• Awad, A., and H. Wang. 2016. “Sliding Mode Based Integrated Pitch-Yaw Acceleration Autopilot Design for Varying-Velocity Missile.” In 2016 12th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2016.7505260
• Azevedo, David J., Ching Shi Liu, and William J. Rae. 1990. “Prediction of Inviscid Stagnation Pressure Losses in Supersonic Inlet Flows.” AIAA Journal 28 (10): 1834–36. https://doi.org/10.2514/3.10486
• Azgin, K., Y. Temiz, and T. Akin. 2007a. “A Novel in-Operation High g-Survivable MEMS Gyroscope.” In 2007 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2007.4388348
• Azgin, K., Y. Temiz, and T. Akin. 2007b. “An SOI-MEMS Tuning Fork Gyroscope with Linearly Coupled Drive Mechanism.” In 2007 IEEE 20th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2007.4433080
• Baals, Donald D., A. Warner Robins, and Roy V. Harris. 1970. “Aerodynamic Design Integration of Supersonic Aircraft.” Journal of Aircraft 7 (5): 385–95. https://doi.org/10.2514/3.59441
• Babar, Muhammad Zeeshan, and Marco Baglietto. 2016. “MPC Based Optimal Input Design for Nonlinear System Identification.” In 2016 20th International Conference on System Theory, Control and Computing (ICSTCC). IEEE. https://doi.org/10.1109/icstcc.2016.7790735
• Baccarella, Damiano, Qili Liu, Brendan J. McGann, and Tonghun Lee. 2019. “Combustion Induced Choking and Unstart Initiation in a Circular Constant-Area Supersonic Flow.” AIAA Journal 57 (12): 5365–76. https://doi.org/10.2514/1.j057921
• Baghdasaryan, Gevorg Y., Marine A. Mikilyan, Laith K. Abbas, and Pier Marzocca. 2013. “About the Aerothermoelastic Stability of Panels in Supersonic Flows.” Journal of Thermal Stresses 36 (9): 915–46. https://doi.org/10.1080/01495739.2013.788894
• Bahambari, Seyedeh Mahsa Zakipour, and Saeed Khankalantary. 2023. “An Improved Nonlinear Observer-Based Integrated Guidance and Control for Hypersonic Flight Vehicle with Angle Constraints.” In 2023 31st International Conference on Electrical Engineering (ICEE). IEEE. https://doi.org/10.1109/icee59167.2023.10334860
• Bahrami, M., B. Ebrahimi, G. R. Ansarifar, and J. Roshanian. 2008. “Sliding Mode Autopilot and Observer Design for a Supersonic Flight Vehicle.” In 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2008.4776375
• Bai, Changrui, and Zhou Zhang. 2014. “Acceleration-Based Mass Imbalance Feedforward Compensation for Inertial Stabilized Platform.” International Journal of Control, Automation and Systems 12 (3): 609–17. https://doi.org/10.1007/s12555-013-0252-0
• Bai, Xibin, Shifeng Zhang, Hong Cai, and Anliang Li. 2015. “Characteristics of Spherical Hydrostatic Supporting System for Floated Inertial Platform.” Tribology International 90: 287–96. https://doi.org/10.1016/j.triboint.2015.04.015
• Bailey, A. B., and R. F. Starr. 1976. “Sphere Drag at Transonic Speeds and High Reynolds Numbers.” AIAA Journal 14 (11): 1631–1631. https://doi.org/10.2514/3.7262
• Baird, C. A., F. B. Snyder, and M. Beierle. n.d. “Terrain-Aided Altitude Computations on the AFTI/F-16.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66217
• Bakalli, Gaetan, Davide Cucci, Ahmed Radi, et al. 2021. “Multi-Signal Approaches for Repeated Sampling Schemes in Inertial Sensor Calibration.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.3946998
• Bakalli, Gaetan, Davide A. Cucci, Ahmed Radi, et al. 2023. “Multi-Signal Approaches for Repeated Sampling Schemes in Inertial Sensor Calibration.” IEEE Transactions on Signal Processing 71: 1103–14. https://doi.org/10.1109/tsp.2023.3262179
• Baker, Syed Murtuza, C. Hart Poskar, and Björn H. Junker. 2011. “Unscented Kalman Filter with Parameter Identifiability Analysis for the Estimation of Multiple Parameters in Kinetic Models.” EURASIP Journal on Bioinformatics and Systems Biology 2011 (1): 7. https://doi.org/10.1186/1687-4153-2011-7
• Balaji, Veeraraghavan, and K. Venkatasubbaiah. 2025. “A New Approach for Studying Scramjet Inlet-Isolator Unstart Flow.” European Journal of Mechanics - B/Fluids 114: 204290. https://doi.org/10.1016/j.euromechflu.2025.204290
• Balamuta, James Joseph, Roberto Molinari, Stephane Guerrier, and Wenchao Yang. 2018. “A Computationally Efficient Framework for Automatic Inertial Sensor Calibration.” IEEE Sensors Journal 18 (4): 1636–46. https://doi.org/10.1109/jsen.2017.2773663
• Balanis, C., and Y. Cheng. 1975. “Aircraft Antenna Analysis for Microwave Landing System.” In 1975 Antennas and Propagation Society International Symposium. IEEE. https://doi.org/10.1109/aps.1975.1147449
• Balasubramanian, R., K. Anandhanarayanan, R. Krishnamurthy, and Debasis Chakraborty. 2016. “Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept.” Journal of Spacecraft and Rockets 53 (4): 759–62. https://doi.org/10.2514/1.a33573
• Balepin, V. V., P. A. Czysz, and R. H. Moszee. 2001b. “Combined Engine for Reusable Launch Vehicle (KLIN Cycle).” Journal of Propulsion and Power 17 (6): 1239–46. https://doi.org/10.2514/2.5870
• Ball, Desmond. 1978. “The Costs of the Cruise Missile.” Survival 20 (6): 242–47. https://doi.org/10.1080/00396337808441774
• Ball, W. H., and P. A. Ross. 1972. “Experimental Correlation of Installation Effects on Inlet Pressure Recovery.” Journal of Aircraft 9 (8): 596–601. https://doi.org/10.2514/3.59042
• “Ballistic Missile Defence.” 1986. Space Policy 2 (2): 176. https://doi.org/10.1016/0265-9646(86)90067-6
• “Ballistic Missile Flight Testing.” 1981. Adelphi Papers 21 (165): 19–34. https://doi.org/10.1080/05679328108448596
• Banerjee, Sanchito. 2019. “Flight Parameter Analysis of an L1 Adaptive Controller of a Hypersonic Glider.” Journal of Aircraft 56 (3): 1149–63. https://doi.org/10.2514/1.c034888
• Bao, Cunyu, Peng Wang, and Guojian Tang. 2019. “Integrated Guidance and Control for Hypersonic Morphing Missile Based on Variable Span Auxiliary Control.” International Journal of Aerospace Engineering 2019: 1–20. https://doi.org/10.1155/2019/6413410
• Bar-Itzhack, Itzhack Y., and Boaz Porat. 1980. “Azimuth Observability Enhancement during Inertial Navigation System in-Flight Alignment.” Journal of Guidance and Control 3 (4): 337–44. https://doi.org/10.2514/3.55999
• Bar-Itzhack, Itzhack Y., Daniel Serfaty, and Yehoshua Vitek. 1982. “Doppler-Aided Low-Accuracy Strapdown Inertial Navigation System.” Journal of Guidance, Control, and Dynamics 5 (3): 236–42. https://doi.org/10.2514/3.56162
• Bar-Shalom, Yaakov, and Chun Yang. 1991. “LOS Rate Estimation in Inertial Navigation Using Landmarks.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791949
• Barantsev, G. O., A. V. Kozlov, I. Kh. Shaimardanov, and A. V. Nekrasov. 2021a. “Elastic Dynamic Torsion of a Ring Laser Gyroscope Mechanical Dither and Its Effect on the Accuracy of Attitude Determination.” In 2021 28th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43216.2021.9470844
• Barantsev, G. O., A. V. Kozlov, I. Kh. Shaimardanov, and A. V. Nekrasov. 2022. “A Model of the Elastic Dynamic Torsion of a Ring Laser Gyroscope Mechanical Dither and a Method for Its Calibration.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815435
• Barczyk, Martin, and Alan F. Lynch. 2011. “Invariant Extended Kalman Filter Design for a Magnetometer-Plus-GPS Aided Inertial Navigation System.” In IEEE Conference on Decision and Control and European Control Conference. IEEE. https://doi.org/10.1109/cdc.2011.6160733
• Bardwell, Greg. 1995. “On-Board Artificial Neural Network Multi-Star Identification System for 3-Axis Attitude Determination.” Acta Astronautica 35: 753–61. https://doi.org/10.1016/0094-5765(94)00247-j
• Barnett, W. T. 1970. “Microwave Line-of-Sight Propagation with and without Frequency Diversity.” Bell System Technical Journal 49 (8): 1827–71. https://doi.org/10.1002/j.1538-7305.1970.tb04291.x
• Barry, Frank W. 1971. “An Explicit Formula for Additive Drag of a Supersonic Conical Inlet.” Journal of Aircraft 8 (4): 279–80. https://doi.org/10.2514/3.44269
• Barton, David K. 1961. “The Future of Pulse Radar for Missile and Space Range Instrumentation.” IRE Transactions on Military Electronics MIL-5 (4): 330–51. https://doi.org/10.1109/iret-mil.1961.5008376
• Barun, B., and Y. Ozkazane. 2004. “Multirate Problems in Aided Inertial Navigation Systems.” In Proceedings of the IEEE 12th Signal Processing and Communications Applications Conference, 2004.. IEEE. https://doi.org/10.1109/siu.2004.1338644
• Barzaghi, Riccardo, Daniela Carrion, Massimiliano Pepe, and Giuseppina Prezioso. 2016. “Computing the Deflection of the Vertical for Improving Aerial Surveys: A Comparison between EGM2008 and ITALGEO05 Estimates.” Sensors 16 (8): 1168. https://doi.org/10.3390/s16081168
• Basha, S. Mahaboob, and Akhilesh Swarup. 2017. “Robust PID Autopilot Design for Back-to-Tum Missile.” In 2017 International Conference on Intelligent Computing and Control (I2C2). IEEE. https://doi.org/10.1109/i2c2.2017.8321860
• Bashkin, V. A., I. V. Egorov, and V. V. Pafnut’ev. 2005. “Aerodynamic Heating of a Thin Sharp-Nose Circular Cone in Supersonic Flow.” High Temperature 43 (5): 733–45. https://doi.org/10.1007/s10740-005-0118-0
• Bassolillo, Salvatore R., Egidio D’Amato, and Immacolata Notaro. 2024. “A Cost-Effective Automatic Calibration Platform for Inertial Measurement Units.” In 2024 10th International Conference on Control, Decision and Information Technologies (CoDIT). IEEE. https://doi.org/10.1109/codit62066.2024.10708604
• Batista, Pedro, Nicolas Petit, Carlos Silvestre, and Paulo Oliveira. 2013. “Further Results on the Observability in Magneto-Inertial Navigation.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6580210
• Batista, P., C. Silvestre, and P. Oliveira. 2010. “Single Beacon Navigation: Observability Analysis and Filter Design.” In Proceedings of the 2010 American Control Conference. IEEE. https://doi.org/10.1109/acc.2010.5531613
• Battistelli, Giorgio, and Pietro Tesi. 2015. “Switching Control for Parameter Identifiability of Uncertain Systems.” In 2015 54th IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2015.7402664
• Batur, C., T. Sreeramreddy, and Q. Khasawneh. 2005. “Sliding Mode Control of a Simulated MEMS Gyroscope.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1470630
• Batur, C., T. Sreeramreddy, and Q. Khasawneh. 2006. “Sliding Mode Control of a Simulated MEMS Gyroscope.” ISA Transactions 45 (1): 99–108. https://doi.org/10.1016/s0019-0578(07)60069-x
• Baumeister, J., and K. Kunisch. 1991. “Identifiability and Stability of a Two-Parameter Estimation problem1.” Applicable Analysis 40 (4): 263–79. https://doi.org/10.1080/00036819108840009
• Bayard, David S. 1996. “Adaptive Neural Star Tracker Calibration for Precision Spacecraft Pointing and Tracking.” IFAC Proceedings Volumes 29 (1): 7402–7. https://doi.org/10.1016/s1474-6670(17)58878-3
• Becerra, Alan, and Aly El-Osery. 2024. “Navigation Solution Based on Reconfigurable Intelligent Surfaces for GNSS-Degraded/Denied Scenarios.” In NAECON 2024 - IEEE National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon61878.2024.10670662
• Beich, Major J., and Col M. Veth. 2010. “Tightly-Coupled Image-Aided Inertial Relative Navigation Using Statistical Predictive Rendering (SPR) Techniques and a Priori World Models.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507309
• Bektash, O., Jacob Naundrup Pedersen, Aitor Ramirez Gomez, and Anders la Cour-Harbo. 2020. “Automated Emergency Landing System for Drones: SafeEYE Project.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9214073
• Belalcazar-Bolaños, Elkyn Alexander, Diego Torricelli, and José L. Pons. 2023. “Automatic Detection of Magnetic Disturbances in Magnetic Inertial Measurement Unit Sensors Based on Recurrent Neural Networks.” Sensors 23 (24): 9683. https://doi.org/10.3390/s23249683
• Belfadel, Djedjiga, and David Haessig. 2025. “Accelerometer Bias Estimation for Unmanned Aerial Vehicles Using Extended Kalman Filter-Based Vision-Aided Navigation.” Electronics 14 (6): 1074. https://doi.org/10.3390/electronics14061074
• Belforte, G., and P. Gay. n.d. “Optimal Input Design for Hammerstein (FIR) Model Identification with Unknown but Bounded Errors.” In Proceedings of the 38th IEEE Conference on Decision and Control (Cat. No.99CH36304), vol. 1. IEEE. https://doi.org/10.1109/cdc.1999.832847
• Belforte, Gustavo, and Paolo Gay. 2003. “Optimal Input Design for Set-Membership Identification of Hammerstein Models.” International Journal of Control 76 (3): 217–25. https://doi.org/10.1080/0020717031000067439
• Belforte, G., and T. T. Tay. 1993. “Optimal Input Design for Worst-Case System Identification In.” Systems & Control Letters 20 (4): 273–78. https://doi.org/10.1016/0167-6911(93)90003-o
• Bell, K. L. 2012. “MAP-PF Multi-Mode Tracking for over-the-Horizon Radar.” In 2012 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2012.6212159
• Belousov, Maksim, and Anton Krivosheev. 2023. “Compensation of Excess Intensity Noise of a Light Source in a Fiber-Optic Gyroscope.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168417
• Belsky, L. N., L. V. Vodicheva, and Yu. V. Parysheva. 2018. “A Strapdown Inertial Navigation System for Space Launch Vehicles: Initial Alignment Accuracy and Periodic Calibrations.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405909
• Belsterling, Charles A. 1965. “An Analog Computer for the Skyscreen System of Missile Range Instrumentation.” Journal of Spacecraft and Rockets 2 (4): 619–21. https://doi.org/10.2514/3.28248
• Ben, Yue-yang, Yong-li Chai, Wei Gao, and Feng Sun. 2010. “Analysis of Error for a Rotating Strap-down Inertial Navigation System with Fibro Gyro.” Journal of Marine Science and Application 9 (4): 419–24. https://doi.org/10.1007/s11804-010-1028-z
• Ben, Yueyang, Wenting Cui, and Qian Li. 2022. “An Improved Damping Method for Grid Inertial Navigation System in Polar Region.” IEEE Transactions on Instrumentation and Measurement 71: 1–13. https://doi.org/10.1109/tim.2022.3212546
• Ben Elisha, Yair, and Vadim Indelman. 2017. “Active Online Visual-Inertial Navigation and Sensor Calibration via Belief Space Planning and Factor Graph Based Incremental Smoothing.” In 2017 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros.2017.8206085
• Ben-Arie, Gershon, Daniel Engelsman, Rotem Dror, and Itzik Klein. 2026. “Diffusion Denoiser-Aided Gyrocompassing.” Measurement 287: 122370. https://doi.org/10.1016/j.measurement.2026.122370
• Ben-Zvi, A., J. McLellan, and K. McAuley. 2003. “Identifiability of Linear Time-Invariant Differential-Algebraic Systems, Using Generalized Markov Parameters.” In Proceedings of the 2003 American Control Conference, 2003., vol. 6. IEEE. https://doi.org/10.1109/acc.2003.1242449
• Bennett, P. J. 1988. “Enhanced Navigation and Displays from Passive Terrain Referenced Avionics.” In Proceedings of the IEEE 1988 National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1988.195016
• Benser, E., G. Sanders, M. Smickilas, J. Wu, and L. Strandjord. 2015. “Development and Evaluation of a Navigation Grade Resonator Fiber Optic Gyroscope.” In 2015 DGON Inertial Sensors and Systems Symposium (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2015.7314259
• Berdjag, Denis, Ali Zolghadri, Jerome Cieslak, and Philippe Goupil. 2010. “Fault Detection and Isolation for Redundant Aircraft Sensors.” In 2010 Conference on Control and Fault-Tolerant Systems (SysTol). IEEE. https://doi.org/10.1109/systol.2010.5675993
• Berglund, M., E. Fedina, C. Fureby, J. Tegnér, and V. Sabel’nikov. 2010. “Finite Rate Chemistry Large-Eddy Simulation of Self-Ignition in Supersonic Combustion Ramjet.” AIAA Journal 48 (3): 540–50. https://doi.org/10.2514/1.43746
• Bergman, Niclas. 1997. “A Bayesian Approach to Terrain-Aided Navigation.” IFAC Proceedings Volumes 30 (11): 1457–62. https://doi.org/10.1016/s1474-6670(17)43048-5
• Bergmann, Dominique, Jan Denzel, Ole Pfeifle, Stefan Notter, Walter Fichter, and Andreas Strohmayer. 2021. “In-Flight Lift and Drag Estimation of an Unmanned Propeller-Driven Aircraft.” Aerospace 8 (2): 43. https://doi.org/10.3390/aerospace8020043
• Berk Gezer, R., and Ali Turker Kutay. 2014. “Robust Model Following Control Design for Missile Roll Autopilot.” In 2014 UKACC International Conference on Control (CONTROL). IEEE. https://doi.org/10.1109/control.2014.6915107
• Berkane, Soulaimane, and Abdelhamid Tayebi. 2021. “Nonlinear Estimation for Position-Aided Inertial Navigation Systems.” In 2021 60th IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc45484.2021.9683180
• Berman, Simon, Michael Chavez, Youngmin Choi, et al. 2025. “Advanced Inertial Measurement Unit (IMU) Hypersonic Flight Test Results.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037214
• Bernstein, Uri, and Richard I. Hess. 1976. “The Effects of Vertical Deflections on Aircraft Inertial Navigation Systems.” AIAA Journal 14 (10): 1377–81. https://doi.org/10.2514/3.61479
• Berto, Federico, Ernesto Benini, Ciaras Wyatt, and Mark Kenneth Quinn. 2020. “Time-Accurate Experimental Investigation of Hypersonic Inlet Buzz at Mach 5.” AIAA Journal 58 (5): 2197–2205. https://doi.org/10.2514/1.j058764
• Beşdok, Erkan. 2009. “3D Vision by Using Calibration Pattern with Inertial Sensor and RBF Neural Networks.” Sensors 9 (6): 4572–85. https://doi.org/10.3390/s90604572
• Bessaad, Nassim, Qilian Bao, and Zhao Jiangkang. 2022. “Design of Enhanced Adaptive Filter for Integrated Navigation System of FOG-SINS and Star Tracker.” In 2022 IEEE 9th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace54187.2022.9856257
• Bettolo, C. Marini. 2008. “The PoGOLite Star Tracker System.” In 2008 IEEE Nuclear Science Symposium Conference Record. IEEE. https://doi.org/10.1109/nssmic.2008.4774604
• Beverini, N., G. Carelli, E. Maccioni, et al. 2014. “Ring Laser Gyroscope for Accurate Angle Metrology.” In 2014 International Conference Laser Optics. IEEE. https://doi.org/10.1109/lo.2014.6886319
• Bevington, J. E., and C. A. Marttila. n.d. “Precision Aided Inertial Navigation Using SAR and Digital Map Data.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66219
• Bezborodova, Kristina, and Evgeny Filinov. 2021. “Double Bypass Turbojet Engine Analysis.” In 2021 International Scientific and Technical Engine Conference (EC). IEEE. https://doi.org/10.1109/ec52789.2021.10016815
• Bhattacharji, Jnanendra Chandra. 1970. “A Rapid Astronomical Method of Observation for Geodetic Azimuth and Prime Vertical Deflection of the Vertical.” Studia Geophysica et Geodaetica 14 (4): 376–81. https://doi.org/10.1007/bf02585745
• Bhowmick, Joyraj, Anurag Singh, Harshit Gupta, and Raghava Nallanthighal. 2021. “A Novel Approach to Computationally Lighter GNSS-Denied UAV Navigation Using Monocular Camera.” In 2021 7th International Conference on Automation, Robotics and Applications (ICARA). IEEE. https://doi.org/10.1109/icara51699.2021.9376502
• Bi, Shuai, Junkui Mao, Lei Wang, and Feng Han. 2024. “An Optimized Time-Adaptive Aerothermal Coupling Calculation Method for Aerothermal Analysis of Disc Cavity System.” Chinese Journal of Aeronautics 37 (9): 164–77. https://doi.org/10.1016/j.cja.2024.06.017
• Bian, Qi, Brett Nener, and Xinmin Wang. 2018. “An Improved NSGA-II Based Control Allocation Optimisation for Aircraft Longitudinal Automatic Landing System.” International Journal of Control 92 (4): 705–16. https://doi.org/10.1080/00207179.2018.1473643
• Biannic, J.-M., and P. Apkarian. 1999. “Missile Autopilot Design via a Modified LPV Synthesis Technique.” Aerospace Science and Technology 3 (3): 153–60. https://doi.org/10.1016/s1270-9638(99)80039-x
• Biernson, G. 1965. “Relation between Structural Compliance and Allowable Friction in a Servomechanism.” IEEE Transactions on Automatic Control 10 (1): 59–66. https://doi.org/10.1109/tac.1965.1098076
• Bigelow, G. F., T. B. Jackson, and R. T. Merriam. 1961. “Microwave Telemetry at U. S. Missile Ranges.” IRE Transactions on Military Electronics MIL-5 (4): 266–72. https://doi.org/10.1109/iret-mil.1961.5008366
• Bijker, Johan, and Willem Steyn. 2008. “Kalman Filter Configurations for a Low-Cost Loosely Integrated Inertial Navigation System on an Airship.” Control Engineering Practice 16 (12): 1509–18. https://doi.org/10.1016/j.conengprac.2008.04.011
• Bilajbegovic, Asim, and Rudiger Lehmann. 2014. “Geodetic Investigation of Accuracy and Reliability of INS/GNSS System iTraceRT-F200-E for Navigation in Tunnels.” In 2014 11th Workshop on Positioning, Navigation and Communication (WPNC). IEEE. https://doi.org/10.1109/wpnc.2014.6843285
• Billig, Frederick S. 1995. “Supersonic Combustion Ramjet Missile.” Journal of Propulsion and Power 11 (6): 1139–46. https://doi.org/10.2514/3.23952
• Bills, Thomas S. 1957. “Reliability Indices for Missile Electronic Component Parts.” IRE Transactions on Reliability and Quality Control PGRQC-10: 1–8. https://doi.org/10.1109/ire-pgrqc.1957.5007128
• Bin Jiang, Yizhen Meng, and Ruiyun Qi. 2017. “Fault-Tolerant Guidance for Hypersonic Vehicle Based on Predictor-Corrector Strategy.” IFAC-PapersOnLine 50 (1): 5244–49. https://doi.org/10.1016/j.ifacol.2017.08.464
• Bing, Chen, Zheng Yong, Xu Bin, Chenx Xiao, and Li Chonghui. 2022. “A Performance Calculation Method of Hypersonic Astronomical Attitude Determination with Corrected Star Map.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9901887
• Bing, Hua, Xiong Zhi, Wu Yunhua, Chen Lin, and Xu Dafu. 2017. “The Error Online Calibration Technique of Integrated Navigation System with Distributed Multi Inertial Node.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028767
• Birnbaum, Morris M., and Phil M. Salomon. 1968. “Strapdown Star Tracker for Space Vehicle Attitude Control.” Journal of Spacecraft and Rockets 5 (10): 1188–92. https://doi.org/10.2514/3.29447
• Bittanti, S. 1979. “New Conditions for Parameters Identifiability of Linear Time-Invariant Systems.” IFAC Proceedings Volumes 12 (8): 697–702. https://doi.org/10.1016/s1474-6670(17)65481-8
• Bittner, Drew E., John A. Christian, Robert H. Bishop, and Darryl May. 2014. “Fault Detection, Isolation, and Recovery Techniques for Large Clusters of Inertial Measurement Units.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851379
• Blair, A. B. 1981. “Remote Control Canard Missile with a Free-Rolling Tail Brake Torque System.” Journal of Spacecraft and Rockets 18 (6): 550–55. https://doi.org/10.2514/3.57851
• Blake, W. B., and W. J. Gillard. 1988. “Prediction of Vortex Interference on a Canard Controlled Missile.” In Proceedings of the IEEE 1988 National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1988.195048
• Blakely, Brandon, and Aaron Nielsen. 2025. “Analysis of Magnetic Anomaly Maps and Navigation Performance Using Flight Test Data.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028196
• Blanchard, R. L. 1979. “High-Accuracy Calibration of Electrostatic Gyro Strapdown Navigation Systems.” Journal of Guidance and Control 2 (5): 361–66. https://doi.org/10.2514/3.55890
• Blankinship, Kevin G. 2008. “A General Theory for Inertial Navigator Error Modeling.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570002
• Blattel, Alfred. 1957. “Guided Missile Tube Reliability.” IRE Transactions on Reliability and Quality Control PGRQC-9: 55–64. https://doi.org/10.1109/ire-pgrqc.1957.5007234
• Blois, Michael, and Kyle O’Keefe. 2025. “Inertial Measurement Aiding for an Attitude-Aided Baseline Spoofing Detection Technique.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028222
• Blood, Eric, Mark Ivanov, Clara O’Farrell, et al. 2015. “LDSD Supersonic Flight Dynamics Test 1: Post-Flight Reconstruction.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119246
• Blum, Christopher, and Johann Dambeck. 2020. “Analytical Assessment of the Propagation of Colored Sensor Noise in Strapdown Inertial Navigation.” Sensors 20 (23): 6914. https://doi.org/10.3390/s20236914
• Blumel, A., and B. White. n.d. “Multiobjective Optimization of Fuzzy Logic Scheduled Controllers for Missile Autopilot Design.” In Proceedings Joint 9th IFSA World Congress and 20th NAFIPS International Conference (Cat. No. 01TH8569), vol. 3. IEEE. https://doi.org/10.1109/nafips.2001.943818
• Blumhagen, Vern A. 1963. “Stellar Inertial Navigation Applied to Cruise Vehicles.” IEEE Transactions on Aerospace and Navigational Electronics ANE-10 (3): 235–46. https://doi.org/10.1109/tane.1963.4502121
• Bo, Xu, Sun Feng, Gao Wei, and Yu Fei. 2008. “The Observation Analysis of the Initial Alignment in the Warship Inertial Navigation System.” In 2008 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2008.4798836
• Bo, Ren, and Li Huan. 2015. “On Forecast Modeling of MEMS Gyroscope Random Drift Error.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260345
• Bodson, Marc, and William A. Pohlchuck. 1998. “Command Limiting in Reconfigurable Flight Control.” Journal of Guidance, Control, and Dynamics 21 (4): 639–46. https://doi.org/10.2514/2.4283
• Boichuk, O. F. 1968. “Vibrations of a Stabilized Platform in an Inertial Navigation System.” Soviet Applied Mechanics 4 (9): 65–68. https://doi.org/10.1007/bf00895850
• Bolandi, H., and F. Fani Saberi. 2011. “Effect of Dynamic Model of Satellite on Accuracy of Attitude Estimation with Unknown Star Sensor Noise Level.” In The 2nd International Conference on Control, Instrumentation and Automation. IEEE. https://doi.org/10.1109/icciautom.2011.6356813
• Bonavita, Andrew T., Michael D. Zollars, Robert B. MacDermott, and Darrell S. Crowe. 2026. “Direct Collocation Methods for Boost–Glide Vehicle Trajectory Optimization with Newtonian Aerodynamic Model.” Journal of Aircraft 63 (1): 48–61. https://doi.org/10.2514/1.c038065
• Bond, Ryan B., and Jack R. Edwards. 2004. “Computational Analysis of an Independent Ramjet Stream in a Combined Cycle Engine.” AIAA Journal 42 (11): 2276–83. https://doi.org/10.2514/1.4465
• Bond, Evan H., and Nicole L. Key. 2026. “Effect of Inlet Distortion Reduced Frequency on Centrifugal Compressor Performance and Stability.” AIAA Journal 64 (7): 4018–24. https://doi.org/10.2514/1.j066481
• Bonnabel, S., P. Martin, and P. Rouchon. 2006. “A Non-Linear Symmetry-Preserving Observer for Velocity-Aided Inertial Navigation.” In 2006 American Control Conference. IEEE. https://doi.org/10.1109/acc.2006.1657161
• Bonney, Lyle D. 1960. “Radar Ballistic Instrumentation at White Sands Missile Range.” IRE Transactions on Military Electronics MIL-4 (4): 583–86. https://doi.org/10.1109/iret-mil.1960.5008294
• Borodacz, Krystian, and Cezary Szczepański. 2023b. “Impact of Motion-Dependent Errors on the Accuracy of an Unaided Strapdown Inertial Navigation System.” Sensors 23 (7): 3528. https://doi.org/10.3390/s23073528
• Bostick, D. R., and J. M. Miletich. 2004. “The NAV100/spl Trade/ a New Paradigm in Small, High Accuracy, Inertial Navigation Systems.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308996
• Bouman, Johannes. 2011. “Relation between Geoidal Undulation, Deflection of the Vertical and Vertical Gravity Gradient Revisited.” Journal of Geodesy 86 (4): 287–304. https://doi.org/10.1007/s00190-011-0520-9
• Boustani, Jonathan, Francois Cadieux, Gaetan K. Kenway, Michael F. Barad, Cetin C. Kiris, and Christoph Brehm. 2022. “Fluid-Structure Interaction Simulations of the ASPIRE SR01 Supersonic Parachute Flight Test.” Aerospace Science and Technology 126: 107596. https://doi.org/10.1016/j.ast.2022.107596
• Bowers, J. L., J. J. Rodden, E. D. Scott, and D. B. Debba. 1968. “Orbital Gyrocompassing Heading Reference.” Journal of Spacecraft and Rockets 5 (8): 903–10. https://doi.org/10.2514/3.29386
• Bowles, S. R., B. J. Gallacher, Z. X. Hu, C. Gregory, and K. Townsend. 2014. “Control Scheme for a Rate Integrating MEMS Gyroscope.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782504
• Bowring, S., and D. Ramsden. 1981. “A Star Tracker for Use during Daytime at Balloon Altitude.” Advances in Space Research 1 (11): 123–26. https://doi.org/10.1016/0273-1177(81)90460-9
• Bozeman, Eric, Minhdao Nguyen, Mohammad Alam, and Jeffrey Onners. 2022. “Inertial Navigation Compensation with Reinforcement Learning.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787527
• Bras, S., P. Rosa, C. Silvestre, and P. Oliveira. 2012. “Fault Detection and Isolation for Inertial Measurement Units.” In 2012 IEEE 51st IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2012.6426831
• Bras, Sergio, Paulo Rosa, Carlos Silvestre, and Paulo Oliveira. 2015. “Fault Detection and Isolation in Inertial Measurement Units Based on Bounding Sets.” IEEE Transactions on Automatic Control 60 (7): 1933–38. https://doi.org/10.1109/tac.2014.2363300
• Bretschneider, Lutz, Rudolf Hankers, Shanna Schönhals, Jens-Michael Heimann, and Astrid Lampert. 2021. “Wind Shear of Low-Level Jets and Their Influence on Manned and Unmanned Fixed-Wing Aircraft during Landing Approach.” Atmosphere 13 (1): 35. https://doi.org/10.3390/atmos13010035
• Britting, Kenneth R., and Thorgeir Palsson. 1970. “Self-Alignment Techniques for Strapdown Inertial Navigation Systems with Aircraft Application.” Journal of Aircraft 7 (4): 302–7. https://doi.org/10.2514/3.44168
• Brodersen, Rolf K. 1972. “Fluidic Inertial Platform.” Journal of Spacecraft and Rockets 9 (3): 131–32. https://doi.org/10.2514/3.61641
• Broslavets, Yu. Yu., D. M. Ambartsumyan, V. G. Semenov, A. A. Fomichev, and E. A. Polukeev. 2021. “Multifrequency Solid-State Ring Laser Gyroscope Based on YAG:Cr4+.” In 2021 28th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43216.2021.9470867
• Broslavets, Yu. Yu., E. A. Polukeev, and A. A. Fomtchev. 2016. “Influence of Physical Factors on the Zero Drift of Laser Gyroscope at Displacement of the Optical Path.” In 2016 International Conference Laser Optics (LO). IEEE. https://doi.org/10.1109/lo.2016.7549823
• Brouk, James D., and Kyle J. DeMars. 2021. “Uncertainty Propagation for Inertial Navigation with Coning, Sculling, and Scrolling Corrections.” Sensors 21 (24): 8457. https://doi.org/10.3390/s21248457
• Brown, A., and G. Moy. n.d. “Long Duration Strapdown Stellar-Inertial Navigation Using Satellite Tracking.” In IEEE PLANS 92 Position Location and Navigation Symposium Record. IEEE. https://doi.org/10.1109/plans.1992.185842
• Brown, J. M., D. B. Ridgely, and R. N. Paschall. 1994. “Autopilot Design for a Tail-Controlled Missile Using LQG/LTR with Eigenstructure Reassignment.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 3. IEEE. https://doi.org/10.1109/acc.1994.735181
• Brueckner, Christoph, Lucila Patino-Studencki, Tianxiang Nan, Atakan Bueyuekoglu, Thomas Heyn, and Michael Fischer. 2023. “Simulation of Communication Network Latency Effects on Vehicle Teleoperation.” In 2023 IEEE 26th International Conference on Intelligent Transportation Systems (ITSC). IEEE. https://doi.org/10.1109/itsc57777.2023.10422699
• Brukarczyk, Bartłomiej, Dariusz Nowak, Piotr Kot, Tomasz Rogalski, and Paweł Rzucidło. 2021. “Fixed Wing Aircraft Automatic Landing with the Use of a Dedicated Ground Sign System.” Aerospace 8 (6): 167. https://doi.org/10.3390/aerospace8060167
• Brzezowski, S. J., J. A. Cochand, L. Murano, J. V. White, J. L. Wylie, and W. G. Heller. n.d. “A near Real-Time Gravity Gradiometer Data Review System.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66223
• Bu, Han, Yu Bai, Xinyuan Feng, et al. 2026b. “IPSO-TCN-GRU Intelligent Algorithm-Based Temperature Drift Compensation for Resonant Optical Gyroscope.” IEEE Transactions on Instrumentation and Measurement: 1–1. https://doi.org/10.1109/tim.2026.3742031
• Bu, Feng, Shuwen Guo, Bo Fan, and Yiwang Wang. 2022. “Effect of Quadrature Control Mode on ZRO Drift of MEMS Gyroscope and Online Compensation Method.” Micromachines 13 (3): 419. https://doi.org/10.3390/mi13030419
• Bu, Jingyu, Zhourun Ye, Xinghui Liang, et al. 2026a. “Deflection of the Vertical from Vertical Gravity Gradient Using Spherical Numerical Integration Expression and Planar Closed-Form Formula.” Studia Geophysica et Geodaetica 70 (2): 27. https://doi.org/10.1007/s11200-026-00028-3
• Buffoli, Andrea, Pietro Segala, Marco Gadola, Thierry Verdot, Philippe Robert, and Giacomo Langfelder. 2023. “Searching for the Origin of Zero-Rate Offset and Scale-Factor Drift in Nems-Based Nav-Grade Gyroscope.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10104013
• Buontempo, Joseph T. 2015. “A Trajectory for Homeland Ballistic Missile Defense.” Defense & Security Analysis 31 (2): 99–109. https://doi.org/10.1080/14751798.2015.1014157
• Burchett, B. T. 2005. “Feedback Linearization Guidance for Approach and Landing of Reusable Launch Vehicles.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1470279
• Burlion, Laurent, and Henry de Plinval. 2017. “Toward Vision Based Landing of a Fixed-Wing UAV on an Unknown Runway under Some Fov Constraints.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991333
• Burlion, Laurent, Henry de Plinval, and Philippe Mouyon. 2014. “Backstepping Based Visual Servoing for Transport Aircraft Automatic Landing.” In 2014 IEEE Conference on Control Applications (CCA). IEEE. https://doi.org/10.1109/cca.2014.6981530
• Burns, V. J. 1963. “Aircraft Navigation: Design Theory for a Self-Organizing, High Accuracy Navigation System.” In Tenth Annual East Coast Conference on Aerospace and Navigational Electronics. IEEE. https://doi.org/10.1109/tane.1963.4502273
• Burrows, James W. 1971. “Combined Inertial: ILS Aircraft Navigation Systems.” Journal of Aircraft 8 (6): 439–43. https://doi.org/10.2514/3.44279
• Buschek, Harald. 1999. “Full Envelope Missile Autopilot Design Using Gain Scheduled Robust Control.” Journal of Guidance, Control, and Dynamics 22 (1): 115–22. https://doi.org/10.2514/2.4357
• Buschek, Harald. 2001. “Design and Flight Test of a Robust Autopilot for the IRIS-T Air-To-Air Missile.” IFAC Proceedings Volumes 34 (15): 449–54. https://doi.org/10.1016/s1474-6670(17)40768-3
• Buschek, Harald. 2003. “Design and Flight Test of a Robust Autopilot for the IRIS-T Air-to-Air Missile.” Control Engineering Practice 11 (5): 551–58. https://doi.org/10.1016/s0967-0661(02)00063-1
• Bussutil, Mehdi, Bernard Vau, Damien Ponceau, and Clement Pinzio. 2022. “Wobble Estimation of a Turntable Axis by Using an Inertial Measurement Unit.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787757
• Bustard, Andrew N., Mark Noftz, Joseph S. Jewell, and Thomas J. Juliano. 2026. “Global Measurements of Unstart in an Internal Osculating Waverider Inlet.” AIAA Journal: 1–8. https://doi.org/10.2514/1.j067385
• Butler, Marlon L., and Harold L. Pastrick. 1983. “Digital Autopilot Design and Evaluation for FAMMS (Future Army Modular Missile System).” In 1983 American Control Conference. IEEE. https://doi.org/10.23919/acc.1983.4788272
• Byoung-Mun Min, Daekyu Sang, Min-Jea Tahk, and Byoung-Soo Kim. 2007. “Missile Autopilot Design via Output Redefinition and Gain Optimization Technique.” In SICE Annual Conference 2007. IEEE. https://doi.org/10.1109/sice.2007.4421433
• C.-W. Tan and S. Park. 2005. “Design of Accelerometer-Based Inertial Navigation Systems.” IEEE Transactions on Instrumentation and Measurement 54 (6): 2520–30. https://doi.org/10.1109/tim.2005.858129
• Cacciola, Stefano, and Andrea Calabria. 2026. “Nonlinear Simulation of Terminal Maneuvers Including Landing Gear Dynamics, Crosswind and Ground Effect.” Applied Sciences 16 (4): 1686. https://doi.org/10.3390/app16041686
• Cai, Guangbin, Guang-Ren Duan, Changhua Hu, and Bin Zhou. 2010. “Tracking Control for Air-Breathing Hypersonic Cruise Vehicle Based on Tangent Linearization Approach.” Journal of Systems Engineering and Electronics 21 (3): 469–75. https://doi.org/10.3969/j.issn.1004-4132.2010.03.018
• Cai, Yingbo, Qiuying Wang, Xuetong Wei, and Debiao Li. 2011. “Analysis of Star Tracker/accelerometer Inertial Navigation System in Theory.” In 2011 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2011.5985817
• Cai, Qingzhong, Gongliu Yang, Wei Quan, Ningfang Song, Yongqiang Tu, and Yiliang Liu. 2018. “Error Analysis of the K-Rb-21Ne Comagnetometer Space-Stable Inertial Navigation System.” Sensors 18 (2): 670. https://doi.org/10.3390/s18020670
• Cai, Yuepeng, and Xuebin Zhuang. 2025. “Hypersonic Glide Vehicle Trajectory Prediction Based on Frequency Enhanced Channel Attention and Light Sampling-Oriented MLP Network.” Defence Technology 46: 199–212. https://doi.org/10.1016/j.dt.2024.11.001
• Cai, Yuepeng, Xuebin Zhuang, Yuanfu Zhong, and Heng Xie. 2026. “Convolutional Interactive Learning Network with Auxiliary Features for Hypersonic Glide Vehicle Trajectory Prediction under Data Missing Scenarios.” Aerospace Science and Technology 177: 112222. https://doi.org/10.1016/j.ast.2026.112222
• Callsen, Steffen, Jascha Wilken, Sven Stappert, and Martin Sippel. 2023. “Feasible Options for Point-to-Point Passenger Transport with Rocket Propelled Reusable Launch Vehicles.” Acta Astronautica 212: 100–110. https://doi.org/10.1016/j.actaastro.2023.07.016
• Campbell, Andrew C. 1963. “Rigorous Solution for the Determination of the Deflection of the Vertical for the Center Area.” Bulletin géodésique 69 (1): 281–91. https://doi.org/10.1007/bf02525902
• Campbell, J. L., and S. H. Ellis. 1971. “Engine/Inlet Compatibility Analysis Procedure.” Journal of Aircraft 8 (5): 301–7. https://doi.org/10.2514/3.59101
• Campregher, F., M. Caparroz, J. L. Guzmán, and A. Visioli. 2025. “A Nonlinear Approach for Input Signal Design with Persistent Excitation Applied to pH Modelling in Microalgae Raceway Reactors.” IFAC-PapersOnLine 59 (6): 103–8. https://doi.org/10.1016/j.ifacol.2025.07.129
• Canciani, Aaron, and John Raquet. 2017. “Airborne Magnetic Anomaly Navigation.” IEEE Transactions on Aerospace and Electronic Systems 53 (1): 67–80. https://doi.org/10.1109/taes.2017.2649238
• Candler, Graham V., and Ivett A. Leyva. 2022. “Computational Fluid Dynamics Analysis of the Infrared Emission from a Generic Hypersonic Glide Vehicle.” Science & Global Security 30 (3): 117–30. https://doi.org/10.1080/08929882.2022.2145777
• Cannon, Robert H. 1961. “Alignment of Inertial Guidance Systems by Gyrocompassing-Linear Theory.” Journal of the Aerospace Sciences 28 (11): 885–95. https://doi.org/10.2514/8.9230
• Cao, Songyin, and Lei Guo. 2012. “Multi-Objective Robust Initial Alignment Algorithm for Inertial Navigation System with Multiple Disturbances.” Aerospace Science and Technology 21 (1): 1–6. https://doi.org/10.1016/j.ast.2011.04.006
• Cao, Songyin, Lei Guo, and Wenhua Chen. 2018. “Anti-Disturbance Fault Tolerant Initial Alignment for Inertial Navigation System Subjected to Multiple Disturbances.” Aerospace Science and Technology 72: 95–103. https://doi.org/10.1016/j.ast.2017.10.041
• Cao, Huiliang, Yupeng Liu, Li Liu, and Xinwang Wang. 2021b. “Humidity Drift Modeling and Compensation of MEMS Gyroscope Based on IAWTD-CSVM-EEMD Algorithms.” IEEE Access 9: 95686–95701. https://doi.org/10.1109/access.2021.3095081
• Cao, Huifang, Hongbo Lv, and Qiguo Sun. 2015. “Model Design Based on MEMS Gyroscope Random Error.” In 2015 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2015.7279648
• Cao, Wen, Hongbin Sun, and Pinghuang Zhou. 2025a. “A Stability-Constrained Attitude Error Compensation Framework for Strapdown Inertial Navigation System Design.” In 2025 7th International Conference on Information Science, Electrical and Automation Engineering (ISEAE). IEEE. https://doi.org/10.1109/iseae64934.2025.11041882
• Cao, Yihua, and Ning Wei. 2020. “Flight Trajectory Simulation and Aerodynamic Parameter Identification of Large-Scale Parachute.” International Journal of Aerospace Engineering 2020: 1–13. https://doi.org/10.1155/2020/5603169
• Cao, Yinong, Chenyang Zhang, Xin He, Pingfeng He, Tingwei Wang, and Yuwei Chen. 2025b. “Unified Voxel-Centric LiDAR-Visual-Inertial SLAM for Large-Scale GNSS-Denied Environments.” In 2025 International Ubiquitous Positioning, Indoor Navigation and Location-Based Services Conference (UPINLBS). IEEE. https://doi.org/10.1109/upinlbs68186.2025.11468411
• Cao, Meng, Ce Zhang, Hexiang Wang, Dawei Liu, Jie Chen, and Yang Tao. 2026. “Unsteady Buzz Characteristics of a Dorsal Supersonic Bump Inlet Based on Wind-Tunnel Tests and Numerical Simulations.” Aerospace 13 (7): 631. https://doi.org/10.3390/aerospace13070631
• Cao, Lei, and Yi Zhou. 2025. “Performance Study of MEMS Quad Mass Gyroscope Based on Force Balance Closed-Loop DC Bias Voltage.” In 2025 IEEE 17th International Conference on Electronic Measurement & Instruments (ICEMI). IEEE. https://doi.org/10.1109/icemi66537.2025.11306499
• Caplin, J. n.d. “Descent-Phase Control of a Reusable Launch Vehicle.” In Proceedings. The 21st Digital Avionics Systems Conference, vol. 2. IEEE. https://doi.org/10.1109/dasc.2002.1052960
• Carbajosa, Carlos, Ángel Sanz-Andrés, Sergio Marín-Coca, and Alejandro Martínez-Cava. 2026. “Choking Effects Influence in the Start and Unstart Limits of Supersonic and Hypersonic Inlets.” Aerospace Science and Technology 179: 113373. https://doi.org/10.1016/j.ast.2026.113373
• Carbajosa, Carlos, Ángel Sanz-Andrés, Alejandro Martínez-Cava, Sergio Marín-Coca, and Sebastián Franchini. 2025b. “Approximated Methods for the Analysis of the Unsteady Shock Wave Motion in Inlet Unstart Processes.” Acta Astronautica 236: 882–96. https://doi.org/10.1016/j.actaastro.2025.07.026
• Carbajosa, Carlos, Ángel Sanz-Andrés, Alejandro Martínez-Cava, and Mikel Ogueta-Gutiérrez. 2025a. “Analysis of the Unsteady Shock Wave Motion in Inlet Unstart Processes.” Acta Astronautica 234: 601–18. https://doi.org/10.1016/j.actaastro.2025.05.006
• Cardarelli, D. 2002. “An Integrated MEMS Inertial Measurement Unit.” In 2002 IEEE Position Location and Navigation Symposium (IEEE Cat. No.02CH37284). IEEE. https://doi.org/10.1109/plans.2002.998924
• Carlson, Gordon, and Max Bott. 1973. “Tilt-Table Alignment for Inertial-Platform Maintenance without a Surveyed Site.” IEEE Transactions on Aerospace and Electronic Systems AES-9 (3): 406–11. https://doi.org/10.1109/taes.1973.309726
• Carlsson, Hakan, Isaac Skog, and Joakim Jalden. 2017. “On-the-Fly Geometric Calibration of Inertial Sensor Arrays.” In 2017 International Conference on Indoor Positioning and Indoor Navigation (IPIN). IEEE. https://doi.org/10.1109/ipin.2017.8115879
• Carlsson, Hakan, Isaac Skog, and Joakim Jalden. 2021. “Self-Calibration of Inertial Sensor Arrays.” IEEE Sensors Journal 21 (6): 8451–63. https://doi.org/10.1109/jsen.2021.3050010
• Carmeli, Guy, and Boaz Ben-Moshe. 2023. “AI-Based Real-Time Star Tracker.” Electronics 12 (9): 2084. https://doi.org/10.3390/electronics12092084
• Carr, Kevin, Robert Greer, Marvin B. May, and Scott Gift. 2014. “Navy Testing of the iXBlue MARINS Fiber Optic Gyroscope (FOG) Inertial Navigation System (INS).” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851515
• Carter, Jonathan, Sina Kohlenbeck, Pascal Birckigt, Ramona Eberhardt, Gerhard Heinzel, and Oliver Gerberding. 2020. “A High Q, Quasi-Monolithic Optomechanical Inertial Sensor.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090085
• Casini, Stefano, Angelo Cervone, Bert Monna, and Pieter Visser. 2023. “Design and Testing of Star Tracker Algorithms for Autonomous Optical Line-of-Sight Deep-Space Navigation.” Applied Optics 62 (22): 5896. https://doi.org/10.1364/ao.494586
• Casini, M., A. Garulli, and A. Vicino. n.d. “On Optimal Input Design in Conditional Set Membership Identification.” In 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475), vol. 6. IEEE. https://doi.org/10.1109/cdc.2003.1272394
• Casini, Marco, Andrea Garulli, and Antonio Vicino. 2008. “Optimal Input Design for Identification of Systems with Quantized Measurements.” In 2008 47th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2008.4739045
• Casini, Marco, Andrea Garulli, and Antonio Vicino. 2009. “Input Design for Worst-Case System Identification with Uniformly Quantized Measurements.” IFAC Proceedings Volumes 42 (10): 54–59. https://doi.org/10.3182/20090706-3-fr-2004.00008
• Casini, Marco, Andrea Garulli, and Antonio Vicino. 2011. “Input Design in Worst-Case System Identification Using Binary Sensors.” IEEE Transactions on Automatic Control 56 (5): 1186–91. https://doi.org/10.1109/tac.2011.2107091
• Casini, Marco, Andrea Garulli, and Antonio Vicino. 2012. “Input Design in Worst-Case System Identification with Quantized Measurements.” Automatica 48 (12): 2997–3007. https://doi.org/10.1016/j.automatica.2012.08.016
• Catena, A., C. D. Melita, and G. Muscato. 2013. “An Architecture for Automatic Tuning of the Navigation System of Unmanned Aerial Vehicles.” In 2013 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2013.6564737
• Causa, Flavia, and Giancarmine Fasano. 2021. “Improved in-Flight Estimation of Inertial Biases through CDGNSS/Vision Based Cooperative Navigation.” Sensors 21 (10): 3438. https://doi.org/10.3390/s21103438
• Cervantes, Noel, Nathan Moore, Mark Carpenter, and Roy Hartfield. 2024. “Classification and Engineering Analysis of Solid Propellant Missile Telemetry Data.” Journal of Spacecraft and Rockets 61 (2): 327–40. https://doi.org/10.2514/1.a35732
• Cetin, Ender, and Ali Turker Kutay. 2016. “Automatic Landing Flare Control Design by Model-Following Control and Flight Test on X-Plane Flight Simulator.” In 2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2016.7549576
• Chabbi, Pradnya, and Venkatesh K. P. Rao. 2024. “Design and Fabrication of Single Drive Tri-Axis MEMS Gyroscope.” Measurement 227: 114307. https://doi.org/10.1016/j.measurement.2024.114307
• Chabbi, Pradnya, and Venkatesh Kp Rao. 2025. “Design of Single Drive Tri-Axis MEMS Gyroscope.” In 2025 IEEE International Symposium on Smart Electronic Systems (iSES). IEEE. https://doi.org/10.1109/ises67504.2025.00066
• Chai, Yu-Yang, Zhi-Guang Song, and Feng-Ming Li. 2017. “Investigations on the Influences of Elastic Foundations on the Aerothermoelastic Flutter and Thermal Buckling Properties of Lattice Sandwich Panels in Supersonic Airflow.” Acta Astronautica 140: 176–89. https://doi.org/10.1016/j.actaastro.2017.08.016
• Chai, Yuyang, Zhiguang Song, and Fengming Li. 2018. “Investigations on the Aerothermoelastic Properties of Composite Laminated Cylindrical Shells with Elastic Boundaries in Supersonic Airflow Based on the Rayleigh–Ritz Method.” Aerospace Science and Technology 82-83: 534–44. https://doi.org/10.1016/j.ast.2018.09.040
• Challoner, Anthony D., Howard H. Ge, and John Y. Liu. 2014. “Boeing Disc Resonator Gyroscope.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851410
• Challoner, A. Dorian, and Mark G. Marshall. 2024. “Compact Digital Symmetric MEMS Vibrating Structure Gyroscope.” In 2024 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa62769.2024.10786029
• Chamoun, Jacob Nemr, and Michel J. F. Digonnet. 2015. “Noise and Bias Error Due to Polarization Coupling in a Fiber Optic Gyroscope.” Journal of Lightwave Technology 33 (13): 2839–47. https://doi.org/10.1109/jlt.2015.2416155
• Chan, H., H. Paik, M. Moody, and J. Parke. 1985. “Superconducting Techniques for Gravity Survey and Inertial Navigation.” IEEE Transactions on Magnetics 21 (2): 411–14. https://doi.org/10.1109/tmag.1985.1063756
• Chan, Li, Cao Yuan, and Zhang Shi-feng. 2015. “New Calibration Method for Shipboard Platform Inertial Navigation System.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260474
• Chandler, H. G. 1958. “Electron Tube Evaluation for Guided Missile Applications.” Electrical Engineering 77 (8): 690–92. https://doi.org/10.1109/ee.1958.6445255
• Chandler, P., M. Pachter, M. Mears, and S. Sheldon. 1992. “Regression Techniques for Aircraft Parameter Identification from Noisy Measurements in Maneuvering Flight.” In [1992] Proceedings of the 31st IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1992.371379
• Chandra, K. Ravi, and Satadal Ghosh. 2019. “Hu-Moment-Based Autonomous Landing of a UAV on a Hemispherical Dome.” In 2019 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2019.8797936
• Chang, Longkang, Huiliang Cao, and Chong Shen. 2020. “Dual-Mass MEMS Gyroscope Parallel Denoising and Temperature Compensation Processing Based on WLMP and CS-SVR.” Micromachines 11 (6): 586. https://doi.org/10.3390/mi11060586
• Chang, C. Bing, and Keh-Ping Dunn. 2019. “Radar Tracking Using State Estimation and Association.” In 2019 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2019.8835799
• Chang, Lubin, Hongyang He, and Fangjun Qin. 2017a. “In-Motion Initial Alignment for Odometer-Aided Strapdown Inertial Navigation System Based on Attitude Estimation.” IEEE Sensors Journal 17 (3): 766–73. https://doi.org/10.1109/jsen.2016.2633428
• Chang, Chieh-Chien, and Cheng-Ting Hsu. 1960. “Aerodynamic Instability of Supersonic Inlet Diffusers.” ARS Journal 30 (5): 468–75. https://doi.org/10.2514/8.5121
• Chang, Juntao, Qinghua Hu, Daren Yu, and Wen Bao. 2011. “Classifier Utility Modeling and Analysis of Hypersonic Inlet Start/unstart Considering Training Data Costs.” Acta Astronautica 69 (9–10): 841–47. https://doi.org/10.1016/j.actaastro.2011.05.035
• Chang, Lubin, Yang Li, and Boyang Xue. 2017b. “Initial Alignment for a Doppler Velocity Log-Aided Strapdown Inertial Navigation System with Limited Information.” IEEE/ASME Transactions on Mechatronics 22 (1): 329–38. https://doi.org/10.1109/tmech.2016.2616412
• Chang, Lubin, Fangjun Qin, and Sai Jiang. 2019. “Strapdown Inertial Navigation System Initial Alignment Based on Modified Process Model.” IEEE Sensors Journal 19 (15): 6381–91. https://doi.org/10.1109/jsen.2019.2910213
• Chang, Lubin, Fangjun Qin, and Jiangning Xu. 2022. “Strapdown Inertial Navigation System Initial Alignment Based on Group of Double Direct Spatial Isometries.” IEEE Sensors Journal 22 (1): 803–18. https://doi.org/10.1109/jsen.2021.3108497
• Chang, Li-Chen, Yu-Siang Wang, and Ming-Tzu Ho. 2024b. “Implementation of a Navigation System Based on the Integration of Inertial Navigation System/Positioning System.” In 2024 International Automatic Control Conference (CACS). IEEE. https://doi.org/10.1109/cacs63404.2024.10773236
• Chang, Guobin, Jiangning Xu, An Li, and Ke Cheng. 2010. “Error Analysis and Simulation of the Dual-Axis Rotation-Dwell Autocompensating Strapdown Inertial Navigation System.” In 2010 International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2010.509
• Chang, Guobin, Jiangning Xu, Fangjun Qin, and An Li. 2009b. “Inertial Navigation Position Algorithm in Frequency-Domain with Gibbs Oscillation Restraining in Acceleration Signal Reconstruction.” In 2009 International Workshop on Intelligent Systems and Applications. IEEE. https://doi.org/10.1109/iwisa.2009.5072911
• Chang, Sansan, Di Yang, Jianzhong Cao, and Xiang Li. 2024a. “An Extend Sliding Mode Disturbance Observer for Optical Inertial Platform Line-of–Sight Stabilized Control.” Machines 12 (12): 849. https://doi.org/10.3390/machines12120849
• Chang, Juntao, Risheng Zheng, Lei Wang, Wen Bao, and Daren Yu. 2014. “Backpressure Unstart Detection for a Scramjet Inlet Based on Information Fusion.” Acta Astronautica 95: 1–14. https://doi.org/10.1016/j.actaastro.2013.10.010
• Changhong Wang and Boran Li. 2010. “The Application of Wavelet Filtering on Denoising Hemispherical Resonator Gyro Signal.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5632494
• Chao, Chin-Yu, Cheng-Wu Chen, and Bor-Chyun Wang. 1986. “Variable Structure Control of a Turbojet Engine.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4788988
• Chao, Chang, De-fu Lin, and Jiang Wang. 2009. “Pole Assignment Method with State Constraints for Missile Three-Loop Autopilot Design.” In 2009 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2009.5192835
• Chappell, Michael J., Keith R. Godfrey, and Sandor Vajda. 1990. “Global Identifiability of the Parameters of Nonlinear Systems with Specified Inputs: A Comparison of Methods.” Mathematical Biosciences 102 (1): 41–73. https://doi.org/10.1016/0025-5564(90)90055-4
• Charu Priya, S., and T. Deepa. 2024. “Design and Analysis of Allan Variance Based Adaptive Noise Canceller for Vehicular Visible Light Communication.” Optical and Quantum Electronics 56 (5): 792. https://doi.org/10.1007/s11082-024-06679-y
• Chaudhary, Rishabh. 2021. “Investigation on Structural Dynamics of Landing Gear.” Materials Today: Proceedings 46: 9–15. https://doi.org/10.1016/j.matpr.2020.03.324
• Chavent, G. 1985. “On Parameter Identifiability.” IFAC Proceedings Volumes 18 (5): 531–36. https://doi.org/10.1016/s1474-6670(17)60614-1
• Che, Jing, and Shuo Tang. 2008. “Research on Integrated Optimization Design of Hypersonic Cruise Vehicle.” Aerospace Science and Technology 12 (7): 567–72. https://doi.org/10.1016/j.ast.2008.01.008
• Chelnokov, Yu. N. 2018. “Inertial Navigation in Space Using Quaternion Regular Equations of Astrodynamics.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405879
• Chelnokov, Yu. N. 2019b. “Quaternion Regular Equations and Algorithms of Space Inertial Navigation.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769350
• Chen, JunKang. 2026. “Neural-Network-Aided Error Correction Method for Inertial-Navigation-System/Global-Positioning-System Integrated Navigation.” In 2026 2nd International Conference on Navigation, Detection and Control (CNDC). IEEE. https://doi.org/10.1109/cndc70899.2026.11707945
• Chen, Zhi-Hao, and Zhi-Jie Chen. 2026. “Topology-Optimized Impact-Resistant Bionic Landing Gear for Unmanned Aerial Vehicles.” Journal of Aircraft 63 (5): 2486–94. https://doi.org/10.2514/1.c038684
• Chen, Kai, Pengyin Chen, and Mingxin Liu. 2016a. “Evaluation of Hypersonic Vehicle SINS Navigation Solution in the Hardware-in-the-Loop Simulation.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7829058
• Chen, Xiyuan, and Bingbo Cui. 2016. “Efficient Modeling of Fiber Optic Gyroscope Drift Using Improved EEMD and Extreme Learning Machine.” Signal Processing 128: 1–7. https://doi.org/10.1016/j.sigpro.2016.03.016
• Chen, Weiyou, Anlan Ding, Xukai Ding, and Hongsheng Li. 2024c. “A Novel Phase Error Quantitative Characterization Method for Whole-Angle Micro Hemispherical Resonant Gyroscope.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10784886
• Chen, Weiyou, Anlan Ding, Ye Shang, and Hongsheng Li. 2026g. “Nonlinearity Calibration for Micro Hemispherical Resonator Gyroscope Based on the First Developed Rate-Integrating Nonlinear Model.” IEEE/ASME Transactions on Mechatronics: 1–12. https://doi.org/10.1109/tmech.2026.3670820
• Chen, Lejun, Christopher Edwards, Halim Alwi, and Masayuki Sato. 2020a. “Flight Evaluation of a Sliding Mode Online Control Allocation Scheme for Fault Tolerant Control.” Automatica 114: 108829. https://doi.org/10.1016/j.automatica.2020.108829
• Chen, Erkang, Changsheng Gao, and Wuxing Jing. 2016c. “Virtual Displacement Guidance for Hypersonic Glide Vehicle.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554180
• Chen, Weiyou, Xiao Ge, Anlan Ding, and Hongsheng Li. 2025b. “Characterization and Compensation of Phase Delay and Modulation Pattern Angle Error for Rate-Integrating Micro-Hemispherical Resonator Gyroscope.” IEEE Sensors Journal 25 (7): 10820–30. https://doi.org/10.1109/jsen.2025.3543642
• Chen, Fang, Jiebin Gu, Pejwaak Salimi, Michael Kraft, and Xinxin Li. 2019c. “Self-Clocking Electro-Mechanical Sigma-Delta Modulator Quadrature Error Cancellation for MEMS Gyroscope.” In 2019 IEEE 32nd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2019.8870630
• Chen, Da-wei, Hong-bin Gu, and Hao Wu. 2010a. “Application of Magneto-Rheological (MR) Damper in Landing Gear Shimmy.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633047
• Chen, Chen, WeiQuan Huang, and He Wang. 2025d. “High-Precision Inertial Navigation with Ellipsoidal Harmonic Gravity Model.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487626
• Chen, Yanjun, Huimin Huang, Wenbo Wang, et al. 2023d. “A Giant Fiber-Optic Gyroscope with Ultra-Low Bias Instability.” In 2023 Asia Communications and Photonics Conference/2023 International Photonics and Optoelectronics Meetings (ACP/POEM). IEEE. https://doi.org/10.1109/acp/poem59049.2023.10369540
• Chen, Cheng, Jie Jiang, Yan Ma, Xinguo Wei, Jian Li, and Gangyi Wang. 2026j. “Star Map Reconstruction of Daytime Star Sensor with Field-of-View-Gated Structure Based on Star Motion in Associated Frames.” IEEE Sensors Journal 26 (19): 29268–77. https://doi.org/10.1109/jsen.2026.3724640
• Chen, Erkang, Wuxing Jing, Changsheng Gao, and Zhao Zhang. 2018a. “An Adaptive Control Approach for a Flexible Hypersonic Glide Vehicle.” In 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2018.8467711
• Chen, Liangqian, Qingsong Li, Tongqiao Miao, et al. 2026a. “4.7PPM Scale Factor Nonlinearity and 0.007°/H Bias Instability Honeycomb Disk Resonator Gyroscope Realized by Calibration of Mode Deflection.” In 2026 IEEE 39th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems64181.2026.11419570
• Chen, Liangqian, Qingsong Li, Tongqiao Miao, et al. 2025a. “0.003°/h Bias Instability of Honeycomb Disk Resonator Gyroscope Achieved by Mode Reversal Combined Mode Deflection Control Method.” Microsystems & Nanoengineering 11 (1): 152. https://doi.org/10.1038/s41378-025-01011-4
• Chen, Long-Tao, Li-Na Lu, Jing Chen, Ting-Ting Wei, and Zhi-Heng Zhang. 2025g. “Research on Trajectory Optimization and Generation Methods for Hypersonic Glide Vehicles Targeting Moving Targets.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487931
• Chen, Pei, Xuejian Mao, Xiucong Sun, and Yumin Lai. 2023a. “Autonomous Navigation for Lunar Final Approach Based on Gravity Gradient Measurements.” Advances in Space Research 71 (3): 1769–83. https://doi.org/10.1016/j.asr.2022.09.056
• Chen, Sitong, Yaiun Meng, Jun Tu, Longfei Wu, Xiaomin Chen, and Tianxu Qi. 2023c. “Design and Implementation of Telemetry Simulation Equipment for Target Missile.” In 2023 IEEE 16th International Conference on Electronic Measurement & Instruments (ICEMI). IEEE. https://doi.org/10.1109/icemi59194.2023.10270354
• Chen, Liangqian, Tongqiao Miao, Qingsong Li, et al. 2022d. “A Temperature Drift Suppression Method of Mode-Matched MEMS Gyroscope Based on a Combination of Mode Reversal and Multiple Regression.” Micromachines 13 (10): 1557. https://doi.org/10.3390/mi13101557
• Chen, Kai, Sensen Pei, Fuqiang Shen, and Shangbo Liu. 2021c. “Tightly Coupled Integrated Navigation Algorithm for Hypersonic Boost-Glide Vehicles in the LCEF Frame.” Aerospace 8 (5): 124. https://doi.org/10.3390/aerospace8050124
• Chen, Xiyuan, and Chong Shen. 2013. “Study on Temperature Error Processing Technique for Fiber Optic Gyroscope.” Optik 124 (9): 784–92. https://doi.org/10.1016/j.ijleo.2012.02.008
• Chen, Xiyuan, Rui Song, Chong Shen, and Hong Zhang. 2014a. “Application of a Genetic Algorithm Elman Network in Temperature Drift Modeling for a Fiber-Optic Gyroscope.” Applied Optics 53 (26): 6043. https://doi.org/10.1364/ao.53.006043
• Chen, Hao, and Hui-jun Tan. 2019. “Buzz Flow Diversity in a Supersonic Inlet Ingesting Strong Shear Layers.” Aerospace Science and Technology 95: 105471. https://doi.org/10.1016/j.ast.2019.105471
• Chen, Hao, Hui-jun Tan, Ya-zhou Liu, and Qi-fan Zhang. 2019b. “External-Compression Supersonic Inlet Free from Violent Buzz.” AIAA Journal 57 (6): 2513–23. https://doi.org/10.2514/1.j057811
• Chen, Hao, Hui-Jun Tan, Qi-Fan Zhang, and Yue Zhang. 2017a. “Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression.” AIAA Journal 55 (12): 4286–95. https://doi.org/10.2514/1.j056066
• Chen, Hao, Hui-Jun Tan, Qi-Fan Zhang, and Yue Zhang. 2018f. “Throttling Process and Buzz Mechanism of a Supersonic Inlet at Overspeed Mode.” AIAA Journal 56 (5): 1953–64. https://doi.org/10.2514/1.j056674
• Chen, Mailun, Guo Wei, Wenjian Zhou, et al. 2026c. “Gravity Matching Navigation Algorithm with Affine Transformation Based on Particle Swarm Optimization and Validation.” Measurement 268: 120439. https://doi.org/10.1016/j.measurement.2026.120439
• Chen, Jie, Qingshan Xu, Yingchao Guo, and Runfeng Chen. 2022b. “Aircraft Landing Gear Retraction/Extension System Fault Diagnosis with 1-D Dilated Convolutional Neural Network.” Sensors 22 (4): 1367. https://doi.org/10.3390/s22041367
• Chen, Hao, Min Xu, Zihua Qiu, Dan Xie, and Yabin Wang. 2018b. “Aerothermoelastic Load Calculation for Hypersonic Vehicles Based on Multiphysics Coupled Analysis.” Mathematical Problems in Engineering 2018: 1–15. https://doi.org/10.1155/2018/6051924
• Chen, Zhennan, Kaichen Yan, Xiaoxu Wang, et al. 2025f. “Online Identification and Compensation of Drive and Phase Errors for Whole-Angle Hemispherical Resonator Gyroscope Based on Sinusoidal Self-Excitation.” IEEE Sensors Journal 25 (2): 2362–71. https://doi.org/10.1109/jsen.2024.3504581
• Chen, Zhaolin, Zhichun Yang, Yingsong Gu, and Xiaochen Wang. 2024a. “High-Frequency Vibration Analysis of Panels under Aerothermoelastic Effects in Supersonic Airflow by an Energy Finite Element Method.” Thin-Walled Structures 200: 111885. https://doi.org/10.1016/j.tws.2024.111885
• Chen, Weina, Zhong Yang, Shanshan Gu, Yizhi Wang, and Yujuan Tang. 2022a. “Adaptive Transfer Alignment Method Based on the Observability Analysis for Airborne Pod Strapdown Inertial Navigation System.” Scientific Reports 12 (1): 946. https://doi.org/10.1038/s41598-021-04732-4
• Chen, Qi, Qinghua Yang, Xiaowei Tu, and Yuxi Zeng. 2021a. “Pitch and Roll Estimation Using Inertial Measurement Unit for Flight Simulator.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550576
• Chen, Tianyu, Gongliu Yang, Zeyang Wen, Pengchao Yao, and Qingzhong Cai. 2026i. “SINS/CNS Integrated Navigation with NFOV Star Tracker Based on Virtual Image Construction.” IEEE Transactions on Aerospace and Electronic Systems 62: 4916–31. https://doi.org/10.1109/taes.2026.3653834
• Chen, Zhaolin, Zhicheng Yang, Yiting Zhang, Changning Liu, Zhichun Yang, and Siu-Kai Lai. 2026h. “A Novel Fourier Time-Sequential PINN Approach for Multi-Frequency Analysis of Nonlinear Aerothermoelastic Problems.” Advanced Engineering Informatics 72: 104446. https://doi.org/10.1016/j.aei.2026.104446
• Chen, Xinglun, Ran Zhang, and Huifeng Li. 2026b. “Explicit Trajectory Dispersion Control for Precision Landing Guidance of Reusable Rockets.” Journal of Guidance, Control, and Dynamics 49 (3): 924–36. https://doi.org/10.2514/1.g009289
• Chen, Zhiqiang, and Yonghui Zhao. 2019. “Aerothermoelastic Analysis of a Hypersonic Vehicle Based on Thermal Modal Reconstruction.” International Journal of Aerospace Engineering 2019: 1–13. https://doi.org/10.1155/2019/8384639
• Chen, Hua, and Yanqing Zhong. 2020. “Design of Readout Circuit with Quadrature Error and Auxiliary PLL for MEMS Vibratory Gyroscope.” Sensors 20 (16): 4564. https://doi.org/10.3390/s20164564
• Chen, Fang, Jingchuan Zhou, Wei Zhou, Ruihong Xiong, and Xinxin Li. 2024b. “A Mechanically Amplified Quad Mass Gyroscope with Parameteric Σ-Δ Modulation for Offset Drift Cancellation.” In 2024 IEEE 37th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems58180.2024.10439349
• Chen Xianxiang, Song Jianmei, and Cai Gaohua. 2012. “Robust Gain-Scheduled Autopilot Design with LPV Reference Model for Portable Missile.” In 2012 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2012.6187214
• Chen Zhang, Chaoyang Chen, and Xubang Shen. n.d. “A New Guide Star Selection Algorithm for Star Tracker.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 6. IEEE. https://doi.org/10.1109/wcica.2004.1343772
• Cheng, R. K. 1965. “Surveyor Terminal Guidance.” IFAC Proceedings Volumes 2 (1): 499–513. https://doi.org/10.1016/s1474-6670(17)69125-0
• Cheng, Guanghao, Songyin Cao, Lei Guo, and Wenhua Chen. 2018a. “Initial Alignment of Inertial Navigation System Based on a Predictive Iterated Kalman Filter.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483957
• Cheng, Lifang, Hongjun Cao, and Litao Zhang. 2021c. “Two-Parameter Bifurcation Analysis of an Aircraft Nose Landing Gear Model.” Nonlinear Dynamics 103 (1): 367–81. https://doi.org/10.1007/s11071-020-06129-w
• Cheng, Junchao, Jiancheng Fang, Weiren Wu, and Jianli Li. 2014. “Temperature Drift Modeling and Compensation of RLG Based on PSO Tuning SVM.” Measurement 55: 246–54. https://doi.org/10.1016/j.measurement.2014.05.013
• Cheng, Guanghui, Wuxing Jing, and Changsheng Gao. 2021b. “Recovery Trajectory Planning for the Reusable Launch Vehicle.” Aerospace Science and Technology 117: 106965. https://doi.org/10.1016/j.ast.2021.106965
• Cheng, Li-Wei, and Ying-Chih Lai. 2025. “Vision-Based Runway Detection and Localization for Aircraft Landing in Global Navigation Satellite System-Denied Environments.” Journal of Field Robotics 43 (3): 2390–2406. https://doi.org/10.1002/rob.70147
• Cheng, Jianhua, Xiangyu Sun, Daidai Chen, Chun Cheng, Hongjie Mou, and Ping Liu. 2018b. “Multi-Fault Detection and Isolation for Redundant Strapdown Inertial Navigation System.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373552
• Cheng, Yunpeng, Xiaodong Yan, Shuo Tang, Manqiao Wu, and Chaoyong Li. 2021a. “An Adaptive Non-Zero Mean Damping Model for Trajectory Tracking of Hypersonic Glide Vehicles.” Aerospace Science and Technology 111: 106529. https://doi.org/10.1016/j.ast.2021.106529
• Cheng, Y., L. Zhang, X. He, et al. 2025. “A Multi-Stage Matching-Based Inertial/Geomagnetic Integrated Navigation Algorithm for UAVs in GNSS-Denied Environments.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279287
• Chernodarov, A. V., V. N. Kovregin, and G. M. Kovregina. 2023. “Inertial-Satellite Micro-Navigation System for Radar with Synthetic Aperture and Doppler Channel for Measuring Trajectory Velocity.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168430
• Chernodarov, A. V., A. P. Patrikeev, S. E. Perelyaev, and A. A. Polyakova. 2022. “Geophysical Invariants and Observability of Integrated Inertial Navigation Systems.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815376
• Chester, D. H. 1995. “Comment on ‘Aircraft Landing Gear Positioning Concerning Abnormal Landing Cases’.” Journal of Aircraft 32 (4): 904–904. https://doi.org/10.2514/3.46816
• Chester, David H. 2002. “Aircraft Landing Impact Parametric Study with Emphasis on Nose Gear Landing Conditions.” Journal of Aircraft 39 (3): 394–403. https://doi.org/10.2514/2.2964
• Chhajer, Harsh, and Rahul Roy. 2024. “Rationalised Experiment Design for Parameter Estimation with Sensitivity Clustering.” Scientific Reports 14 (1): 25864. https://doi.org/10.1038/s41598-024-75539-2
• Chi, Chien-Yu, and Tsung-Lin Chen. 2009. “MEMS Gyroscope Control Systems for Direct Angle Measurements.” In 2009 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2009.5398283
• Chiang, Kai-Wei, Syun Tsai, Chi-Hsin Huang, et al. 2026. “Navigation Error Characteristics of LIO-, VIO-, and RIMU-Assisted INS/GNSS Multi-Sensor Fusion Schemes in a GNSS-Denied Environment.” Sensors 26 (7): 2068. https://doi.org/10.3390/s26072068
• Chichka, David F., Uday J. Shankar, Eugene M. Cliff, and Henry J. Kelley. 1988. “Cruise-Dash-Climb Analysis of an Airbreathing Missile.” Journal of Guidance, Control, and Dynamics 11 (4): 293–99. https://doi.org/10.2514/3.20310
• Chikovani, Valeriy V., and Serhii V. Golovach. 2022. “Metallic Cylindrical Resonator Vibratory Gyroscope Sensitivity to Random Vibration.” In 2022 IEEE 41st International Conference on Electronics and Nanotechnology (ELNANO). IEEE. https://doi.org/10.1109/elnano54667.2022.9927050
• Chin, Wilson C. 1977. “Supersonic Wave Drag for Nonplanar Singularity Distributions.” AIAA Journal 15 (6): 884–86. https://doi.org/10.2514/3.60721
• Chin, Wilson C. 1978. “Supersonic Wave Drag of Planar Singularity Distributions.” AIAA Journal 16 (5): 482–87. https://doi.org/10.2514/3.7537
• Ching-Fang Lin, J. R. Cloutier, and J. H. Evers. n.d. “Missile Autopilot Design Using a Generalized Hamiltonian Formulation.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.721027
• Cho, Jae Yoong, Sajal Singh, Jong-Kwan Woo, Guohong He, and Khalil Najafi. 2020. “0.00016 Deg/√hr Angle Random Walk (ARW) and 0.0014 Deg/hr Bias Instability (BI) from a 5.2M-Q and 1-Cm Precision Shell Integrating (PSI) Gyroscope.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090086
• Choe, Yohan, Chongam Kim, and Kwanghyun Kim. 2020. “Effects of Optimized Bleed System on Supersonic Inlet Performance and Buzz.” Journal of Propulsion and Power 36 (2): 211–22. https://doi.org/10.2514/1.b37474
• Choe, Yeongkwon, and Chan Gook Park. 2021. “Point-Mass Filtering with Boundary Flow and Its Application to Terrain Referenced Navigation.” IEEE Transactions on Aerospace and Electronic Systems 57 (6): 3600–3613. https://doi.org/10.1109/taes.2021.3079585
• Choe, Yeongkwon, Jin Woo Song, and Chan Gook Park. 2022. “Lightweight Marginalized Particle Filtering with Enhanced Consistency for Terrain Referenced Navigation.” IEEE Transactions on Aerospace and Electronic Systems 58 (3): 2493–2504. https://doi.org/10.1109/taes.2021.3135233
• Choi, Woo-Seok, Jun-Eon An, Cheon-Joong Kim, and Kyu-Min Shim. 2023b. “Dynamical Encircling of a Lock-In Area with a Combination of Fast and Slow Dithering in a Ring Laser Gyroscope.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10103982
• Choi, Jonggyu, Jin Choi, and Hyungrok Do. 2026. “Design and Optimization of a Fuselage-Integrated Diverterless Supersonic Intake for Ramjet Vehicles.” Aerospace Science and Technology 178: 113190. https://doi.org/10.1016/j.ast.2026.113190
• Choi, Gyuyeon, and Hyeong-Geun Kim. 2026. “Real-Time Trajectory Forecast and Intercept Point Prediction for Boost-Phase Ballistic Missile Interception.” IEEE Transactions on Aerospace and Electronic Systems 62: 12578–97. https://doi.org/10.1109/taes.2026.3706326
• Choi, Christopher L., Binbin Xu, and Stefan Leutenegger. 2023a. “Accurate and Interactive Visual-Inertial Sensor Calibration with Next-Best-View and Next-Best-Trajectory Suggestion.” In 2023 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros55552.2023.10341815
• Choi, Yunseok, Michael F. Yost, Evan W. Lerner, and James F. Driscoll. 2022. “Scramjet Performance Computed for a JP-7-Fueled Generic X-51 Vehicle.” Journal of Propulsion and Power 38 (3): 348–58. https://doi.org/10.2514/1.b38329
• Chomachar, Saeb AmirAhmadi, and Alireza Mohammadi Fard. 2016. “Flight Control System for Guided Rolling-Airframe Missile.” In 2016 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2016.7500499
• Chong Zhang, Qi-song Wu, Tao Yin, and Hai-gang Yang. 2010. “A MEMS Gyroscope Readout Circuit with Temperature Compensation.” In 2010 IEEE 5th International Conference on Nano/Micro Engineered and Molecular Systems. IEEE. https://doi.org/10.1109/nems.2010.5592435
• Chovitz, Bernard, and Irène Fischer. 1959. “The Influence of the Distant Topography on the Deflection of the Vertical.” Bulletin géodésique 54 (1): 37–43. https://doi.org/10.1007/bf02539777
• Chowdhury, Mozammal, and Shawn Keshmiri. 2024. “A Unified Inner-Outer Loop Reinforcement Learning Flight Controller for Fixed-Wing Aircraft.” In 2024 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas60882.2024.10556883
• Christian, John A., and John L. Crassidis. 2021. “Star Identification and Attitude Determination with Projective Cameras.” IEEE Access 9: 25768–94. https://doi.org/10.1109/access.2021.3054836
• Christiansen, Jonas Myhre, and Graeme E. Smith. 2019. “Parameter Selection in a Fully Adaptive Tracking Radar.” In 2019 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar41533.2019.171303
• Chu, Yundi, and Juntao Fei. 2016. “Adaptive Backstepping Global Sliding Fuzzy Neural Controller for MEMS Gyroscope.” In 2016 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2016.7810389
• Chu Zhongyi, Cui Jing, Xu Jingyi, and Ma Jing. 2010. “Research on Hierarchical Composite Controller for Inertial Platform Servo Loop.” In 2010 8th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2010.5554644
• Chueh, Victor, Te-Chang Li, and Robert Grethel. 2008. “INS/Baro Vertical Channel Performance Using Improved Pressure Altitude as a Reference.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570006
• Chun-Liang Lin. 2002. “On the Design of an Adaptive Fuzzy Gain-Scheduled Autopilot.” In Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301). IEEE. https://doi.org/10.1109/acc.2002.1023245
• Chunfeng, G., M. Haiyang, Y. Xudong, X. Pengbo, L. Yiming, and W. Guo. 2025. “Inertial-Based Autonomous Navigation and Gravity Measurement System Assisted by LDV.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279677
• Chyu, W. J., G. W. Howe, and T. I-P. Shih. 1992. “Bleed-Boundary Conditions for Numerically Simulated Mixed-Compression Supersonic Inlet Flow.” Journal of Propulsion and Power 8 (4, Ju). https://ntrs.nasa.gov/citations/19920061896
• Cicolani, Luigi S., Gerd Kanning, and Stanley F. Schmidt. 1983. “A Kalman Filter Algorithm for Terminal-Area Navigation with Sensors of Moderate Accuracy.” Journal of Guidance, Control, and Dynamics 6 (5): 321–29. https://doi.org/10.2514/3.19838
• Ciesielski, Marek, and Mateusz Malanowski. 2022. “Analysis of Data Source Influence on Tracking Accuracy in Passive Radar.” In 2022 23rd International Radar Symposium (IRS). IEEE. https://doi.org/10.23919/irs54158.2022.9905020
• Clark, N., and P. Furth. n.d. “Intelligent Star Tracker.” In Proceedings of the 43rd IEEE Midwest Symposium on Circuits and Systems (Cat.No.CH37144), vol. 3. IEEE. https://doi.org/10.1109/mwscas.2000.951482
• Clauser, Francis H. 1954. “Ramjet Diffusers at Supersonic Speeds.” Journal of Jet Propulsion 24 (2): 79–84. https://doi.org/10.2514/8.6460
• Clifford, S., and J. Strohbehn. 1970. “The Theory of Microwave Line-of-Sight Propagation through a Turbulent Atmosphere.” IEEE Transactions on Antennas and Propagation 18 (2): 264–74. https://doi.org/10.1109/tap.1970.1139655
• ÇLimen, Tayfun. 2011. “A Generic Approach to Missile Autopilot Design Using State-Dependent Nonlinear Control.” IFAC Proceedings Volumes 44 (1): 9587–9600. https://doi.org/10.3182/20110828-6-it-1002.03744
• Clos-Cot, Laurent, Julien Templai, Balint Vanek, and Balint Patartics. 2018. “Vision-Based Control and Guidance Structure for Automatic Landing Simulations.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396467
• Coe, J. C. 1948. “Telemetering Guided-Missile Performance.” Proceedings of the IRE 36 (11): 1404–14. https://doi.org/10.1109/jrproc.1948.232300
• Cohen-Zur, Abraham, and Benveniste Natan. 1998. “Experimental Investigation of a Supersonic Combustion Solid Fuel Ramjet.” Journal of Propulsion and Power 14 (6): 880–89. https://doi.org/10.2514/2.5379
• Collins, E. B. 1943. “Celestial Navigation.” Scientific American 168 (2): 66–67. https://doi.org/10.1038/scientificamerican0243-66
• Collins, R. L., and R. J. Black. 1969. “Tire Parameters for Landing-Gear Shimmy Studies.” Journal of Aircraft 6 (3): 252–58. https://doi.org/10.2514/3.44044
• Coombes, Matthew, Wen-Hua Chen, and Peter Render. 2017. “Landing Site Reachability in a Forced Landing of Unmanned Aircraft in Wind.” Journal of Aircraft 54 (4): 1415–27. https://doi.org/10.2514/1.c033856
• Copp, Brian L., and Kamesh Subbarao. 2015. “Nonlinear Adaptive Filtering in Terrain-Referenced Navigation.” In 2015 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2015.7171002
• Costandin, Beniamin, Marius Costandin, and Petru Dobra. 2021. “A Novel 3D Body Attitude and Gyroscope Bias Estimator Algorithm.” In 2021 25th International Conference on System Theory, Control and Computing (ICSTCC). IEEE. https://doi.org/10.1109/icstcc52150.2021.9606858
• “Coupled Dynamic Model of State Estimation for Hypersonic Glide Vehicle.” 2018. Journal of Systems Engineering and Electronics 29 (6): 1284. https://doi.org/10.21629/jsee.2018.06.15
• Courdesses, M., M. Polis, and M. Amouroux. 1981. “On Identifiability of Parameters in a Class of Parabolic Distributed Systems.” IEEE Transactions on Automatic Control 26 (2): 474–77. https://doi.org/10.1109/tac.1981.1102609
• Coutard, Laurent, Francois Chaumette, and Jean-Michel Pflimlin. 2011. “Automatic Landing on Aircraft Carrier by Visual Servoing.” In 2011 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2011.6094887
• Cox, J. A. 1957. “Telemetering System for the X-17 Missile.” IRE Transactions on Telemetry and Remote Control TRC-3 (1): 1–14. https://doi.org/10.1109/irettrc.1957.6541495
• Craft, Kyle J., Henry J. Pernicka, and Jacob E. Darling. 2020. “Performance Determination of a Multi-Mode Thruster Using GPS and Star Tracker Data.” In 2020 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero47225.2020.9172624
• Craig, K. H., and G. R. Kennedy. 1987. “Studies of Multi Path Propagation on a Microwave Line-of-Sight Link.” In 17th European Microwave Conference, 1987. IEEE. https://doi.org/10.1109/euma.1987.333659
• Crassidis, John L. 2002. “Angular Velocity Determination Directly from Star Tracker Measurements.” Journal of Guidance, Control, and Dynamics 25 (6): 1165–68. https://doi.org/10.2514/2.4999
• Crassidis, John L., D. Joseph Mook, and James M. McGrath. 1993. “Automatic Carrier Landing System Utilizing Aircraft Sensors.” Journal of Guidance, Control, and Dynamics 16 (5): 914–21. https://doi.org/10.2514/3.21101
• Critchley-Marrows, Joshua J. R., Xiaofeng Wu, and Iver H. Cairns. 2022. “Treatment of Extended Kalman Filter Implementations for the Gyroless Star Tracker.” Sensors 22 (22): 9002. https://doi.org/10.3390/s22229002
• Crocetto, N., and P. Russo. 1996a. “Deflection of the Vertical and Refraction in Three-Dimensional Adjustement of Terrestrial Networks.” Journal of Geodesy 70 (11): 681–95. https://doi.org/10.1007/s001900050058
• Crocetto, N., and P. Russo. 1996b. “Deflection of the Vertical and Refraction in Three-Dimensional Adjustment of Terrestrial Networks.” Journal of Geodesy 70 (11): 681–95. https://doi.org/10.1007/bf00867147
• Cucci, Davide Antonio, Omar Garcia Crespillo, and Mehran Khaghani. 2016. “An Analysis of a Gyro-Free Inertial System for INS/GNSS Navigation.” In 2016 European Navigation Conference (ENC). IEEE. https://doi.org/10.1109/euronav.2016.7530560
• Cui, Shunfeng, Yiyang Chen, and Hongfeng Tao. 2022. “An Automatic Approach for Aircraft Landing Process Based on Iterative Learning Control.” In 2022 IEEE 11th Data Driven Control and Learning Systems Conference (DDCLS). IEEE. https://doi.org/10.1109/ddcls55054.2022.9858388
• Cui, Tao, Xuegang He, Daren Yu, and Shunlin Tang. 2012. “Multistability and Loops-Coupled Hysteresis: Flight-Test Analysis on Error Detection of Inlet Start/Unstart.” Journal of Propulsion and Power 28 (3): 496–503. https://doi.org/10.2514/1.b34349
• Cui, Min, Yong Huang, Wei Wang, and Huiliang Cao. 2019b. “MEMS Gyroscope Temperature Compensation Based on Drive Mode Vibration Characteristic Control.” Micromachines 10 (4): 248. https://doi.org/10.3390/mi10040248
• Cui, Tao, Zhong Lv, and Daren Yu. 2011. “Multistability and Complex Routes of Supersonic Inlet Start/Unstart.” Journal of Propulsion and Power 27 (6): 1204–17. https://doi.org/10.2514/1.b34235
• Cui, Bingbo, Xinhua Wei, Xiyuan Chen, and Aichen Wang. 2021. “Improved High-Degree Cubature Kalman Filter Based on Resampling-Free Sigma-Point Update Framework and Its Application for Inertial Navigation System-Based Integrated Navigation.” Aerospace Science and Technology 117: 106905. https://doi.org/10.1016/j.ast.2021.106905
• Cui, XiangYu, Bing Xu, and FeiYu Song. 2023a. “Design and Strategy Research of UAV Dynamic Take-Off and Landing Platform Based on Inertial Stability Control Platform.” In 2023 6th International Conference on Intelligent Robotics and Control Engineering (IRCE). IEEE. https://doi.org/10.1109/irce59430.2023.10255040
• Cui, Jian, Guizhen Yan, and Qiancheng Zhao. 2019a. “Enhanced Temperature Stability of Scale Factor in MEMS Gyroscope Based on Multi Parameters Fusion Compensation Method.” Measurement 148: 106947. https://doi.org/10.1016/j.measurement.2019.106947
• Cui, Jian, and Qiancheng Zhao. 2021. “A Tactical-Grade Monolithic Horizontal Dual-Axis Mems Gyroscope Based on off-Plane Quadrature Coupling Suppression Silicon Gratings.” In 2021 IEEE 34th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems51782.2021.9375209
• Cui, Jian, and Qiancheng Zhao. 2023. “120 Ppm Quality Factor Thermal Stability from -40 ℃ to +60℃ of a Dual-Axis MEMS Gyroscope Based on Joule Effect Dynamic Control.” In 2023 IEEE 36th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems49605.2023.10052533
• Culler, Adam J., Jack J. McNamara, and Andrew R. Crowell. 2009. “Control-Oriented Aerothermoelastic Modeling Approaches for Hypersonic Vehicles.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160023
• Cummings, R. M., H. T. Yang, and Y. H. Oh. 1995. “Supersonic, Turbulent Flow Computation and Drag Optimization for Axisymmetric Afterbodies.” Computers & Fluids 24 (4): 487–507. https://doi.org/10.1016/0045-7930(94)00040-6
• Cutright, C. A., and N. S. Braasch. n.d. “GPS and INS Flight Test Instrumentation of a Fully Aerobatic Turbojet Aircraft.” In Proceedings, IEEE Aerospace Conference, vol. 3. IEEE. https://doi.org/10.1109/aero.2002.1035269
• D’Angelo, Michael, and Richard Linares. 2011. “Attitude Determination Using a Photon Counting Star Tracker.” In 2011 Western New York Image Processing Workshop. IEEE. https://doi.org/10.1109/wnyipw.2011.6122885
• Da, Li, Li Chengsuo, Gao Wei, Li Zhong, Zhang Zishan, and Yuan Yuan. 2023. “System Level Calibration Method for Drift of Rotary Accelerometer Gravity Gradiometer.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168350
• Da, Li, Zhao Lin, Weng Haina, Li Chengsuo, Pei Zhi, and Chen Jia. 2022. “Dynamic Data Processing Method of Gravity Gradiometer Based on Equivalent Source.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926304
• Dachuan Liu, Xiaozhu Chi, Jian Cui, et al. 2008. “Research on Temperature Dependent Characteristics and Compensation Methods for Digital Gyroscope.” In 2008 3rd International Conference on Sensing Technology. IEEE. https://doi.org/10.1109/icsenst.2008.4757112
• Dagal, Idriss. 2026. “Probabilistic Fault Tree Analysis and Dynamic Redundancy Optimization for Next-Generation Avionic Flight Control Systems.” Reliability Engineering & System Safety 266: 111841. https://doi.org/10.1016/j.ress.2025.111841
• Dai, Hai-fa, Hong-wei Bian, Rong-ying Wang, and Heng Ma. 2020. “An INS/GNSS Integrated Navigation in GNSS Denied Environment Using Recurrent Neural Network.” Defence Technology 16 (2): 334–40. https://doi.org/10.1016/j.dt.2019.08.011
• Dai, Yuting, Jizhou Lai, Qieqie Zhang, Zhimin Li, and Yugui Shen. 2023. “An Improved Fault Detection and Isolation Method for Airborne Inertial Navigation System/Attitude and Heading Reference System Redundant System.” Aerospace 10 (12): 1024. https://doi.org/10.3390/aerospace10121024
• Dai, Shicong, Quanjun Liu, Ying Wang, Zhang Ren, Yudong Wang, and Changwan Min. 2017. “Adaptive Control for Lateral Motion of Reusable Launch Vehicle Using Retrospective Cost Estimator.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027911
• Dai, Dongkai, Wenfeng Tan, Wei Wu, Xingshu Wang, and Shiqiao Qin. 2018. “An Optimal Tightly-Coupled Stellar/inertial Integrated Navigation Method for Daytime Application.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577165
• Dai, Dongkai, Xingshu Wang, Zongsheng Huang, and Jiaxing Zheng. 2015. “Stochastic Modeling the Vertical Deflection Errors of EGM2008 for INS/GNSS Integration.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260427
• Dai, Jiyang, Guohui Wu, Qian Shuai, and Jian Shi. 2009. “Data Acquisition System Design for Missile Telemetry and Telecontrol Based on FPGA.” In 2009 IEEE Circuits and Systems International Conference on Testing and Diagnosis. IEEE. https://doi.org/10.1109/cas-ictd.2009.4960796
• Dai, Xiaoqiang, Lin Zhao, and Zhen Shi. 2013a. “Fault Tolerant Control in Redundant Inertial Navigation System.” Mathematical Problems in Engineering 2013: 1–11. https://doi.org/10.1155/2013/782617
• Daliri, Abbas, Mohammad Farahani, and Javad Sepahi-Younsi. 2018. “Novel Method for Supersonic Inlet Buzz Measurement in Wind Tunnel.” Journal of Propulsion and Power 34 (1): 273–80. https://doi.org/10.2514/1.b36760
• Damerius, Robert, and Torsten Jeinsch. 2019. “A Generic Inertial Navigation System.” In 2019 International Interdisciplinary PhD Workshop (IIPhDW). IEEE. https://doi.org/10.1109/iiphdw.2019.8755417
• Danik, Boris. 1966. “The Least-Square Approximation of Inertial Platform Drift.” IEEE Transactions on Aerospace and Electronic Systems AES-2 (5): 591–94. https://doi.org/10.1109/taes.1966.4501936
• Darling, Frederic W. 1948. “Introduction to the Fundamental Tables for the Deflection of the Vertical.” Bulletin géodésique 9 (1): 199–240. https://doi.org/10.1007/bf02525964
• Das, A., R. Das, S. Mukhopadhyay, and A. Patra. 2005. “Nonlinear Autopilot and Observer Design for a Surface-To-Surface, Skid-To-Turn Missile.” In 2005 Annual IEEE India Conference - Indicon. IEEE. https://doi.org/10.1109/indcon.2005.1590178
• Daub, Dennis, Sebastian Willems, and Ali Gülhan. 2022. “Experiments on Aerothermoelastic Fluid–structure Interaction in Hypersonic Flow.” Journal of Sound and Vibration 531: 116714. https://doi.org/10.1016/j.jsv.2021.116714
• Daum, P., J. Beyer, and T. F. W. Kohler. 1994. “Aided Inertial LAnd NAvigation System (ILANA) with a Minimum Set of Inertial Sensors.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303325
• Davies, W. T. 1974. “Automatic Carrier Landing Systems.” In 1974 IEEE Conference on Decision and Control including the 13th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1974.270418
• Davies, R., and D. Haines. 1965. “Deceleration Trajectory of a Time-Optimized Hydraulic Servomechanism.” IEEE Transactions on Automatic Control 10 (3): 365–365. https://doi.org/10.1109/tac.1965.1098148
• Davis, L. I. 1961. “Reliability in Missile and Space Operations.” Electrical Engineering 80 (6): 422–24. https://doi.org/10.1109/ee.1961.6433288
• Davison, D. E., P. T. Kabamba, and S. M. Meerkov. 1997. “Disturbance Gain and Bandwidth Margins: Definitions and Application to Autopilot Design.” In Proceedings of the 1997 American Control Conference (Cat. No.97CH36041). IEEE. https://doi.org/10.1109/acc.1997.609704
• Davydochkin, V. M. 2017. “The Signal Function in the Objective of Improving the Accuracy of Radar-Tracking Measurements Taking into Account Frequency Dispersion in Waveguides.” Measurement Techniques 60 (8): 785–93. https://doi.org/10.1007/s11018-017-1271-7
• De, Saibal, Jackson Mayo, Hemanth Kolla, and Christopher Bennett. 2025. “Silent Error Resilient Kalman Filter for Inertial Navigation Using Linear Algebra Checksums.” In 2025 IEEE International Conference on High Performance Computing and Communications (HPCC). IEEE. https://doi.org/10.1109/hpcc67675.2025.00164
• de Bonfim Gripp, Juliano A., and Ulisses P. Sampaio. 2014. “Automatic Landing of a UAV Using Model Predictive Control for the Surveillance of Internal Autopilot’s Controls.” In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2014.6842378
• de Bruin, Andrew, and Thomas Jones. 2016. “Accurate Autonomous Landing of a Fixed-Wing Unmanned Aircraft under Crosswind Conditions.” IFAC-PapersOnLine 49 (17): 170–75. https://doi.org/10.1016/j.ifacol.2016.09.030
• De Carlo, Martino, Francesco De Leonardis, Luciano Lamberti, and Vittorio M. N. Passaro. 2022. “Design of a Resonator-Bus-Resonator Anti-Parity-Time-Symmetric Integrated Optical Gyroscope.” Optics and Lasers in Engineering 153: 106983. https://doi.org/10.1016/j.optlaseng.2022.106983
• de Oca, Andres Montes, and Gerardo Flores. 2020. “Unified Controller for Take-off and Landing for a Fixed-Wing Aircraft.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9213878
• de Rochechouart, Maxence, Amal El Fallah Seghrouchni, Frederic Barbaresco, and Raed Abu Zitar. 2024. “Radar/Optro Meta-Sensor: Augmented Radar Tracking Performances by Adaptive Camera Resources Allocation.” In 2024 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar58436.2024.10993879
• DeChant, Lawrence J. 2010. “Expression for Supersonic Fluctuating Drag Force Magnitude Due to Ambient Thermodynamic Disturbances.” AIAA Journal 48 (12): 2976–79. https://doi.org/10.2514/1.j050715
• Dedes, Nikolaos, David Harvey, and Tim Freegarde. 2024. “Real-Time Scale-Factor Calibration for Cold-Atom Gyroscope Based on Point-Source Interferometry.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502035
• Dejaeger, Remy, Olivier Lefort, Mathieu Jeanneteau, and Jean-Michel Muguet. 2022. “A Low-Noise Mixed Signal ASIC for Navigation-Grade Resonant MEMS Accelerometer.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787724
• Dektor, Shandor, and Stephen Rock. 2014. “Robust Adaptive Terrain-Relative Navigation.” In 2014 Oceans - St. John’s. IEEE. https://doi.org/10.1109/oceans.2014.7003195
• Delabie, Tjorven, Joris De Schutter, and Bart Vandenbussche. 2015. “Robustness and Efficiency Improvements for Star Tracker Attitude Estimation.” Journal of Guidance, Control, and Dynamics 38 (11): 2108–21. https://doi.org/10.2514/1.g000894
• Delgado, M., and G. Profos. 1999. “Identifiability of Dynamic Systems Represented by Bond Graphs.” Mathematical and Computer Modelling of Dynamical Systems 5 (2): 89–112. https://doi.org/10.1076/mcmd.5.2.89.6174
• della Noce, Eduardo Rodrigues, Arti Kalra, Andre Coelho, Tin Muskardin, and Konstantin Kondak. 2021. “High-Fidelity Modeling and Control Design for a Cooperative High Altitude Long Endurance Aircraft Landing System.” In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas51884.2021.9476729
• Delsasso, L. A., L. G. De Bey, and D. Reuyl. 1948. “Full-Scale Free-Flight Ballistic Measurements of Guided Missiles.” Journal of the Aeronautical Sciences 15 (10): 605–15. https://doi.org/10.2514/8.11664
• Demenkov, N. P., and D. M. Tran. 2019. “Fuzzy Description Hemispherical Resonator Gyro Error.” Procedia Computer Science 150: 88–94. https://doi.org/10.1016/j.procs.2019.02.019
• Demidovich, Nick. 2017. “Flight Test of ADS-B Technology for Winged Reusable Launch Vehicle Re-Entry.” In 2017 Integrated Communications, Navigation and Surveillance Conference (ICNS). IEEE. https://doi.org/10.1109/icnsurv.2017.8012003
• DeNatale, Jeffrey, Philip Stupar, Stephane Martel, and Jonathan Lachance. 2023. “Manufacturing Platform for High-Performance MEMS Inertial Sensors.” In 2023 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans53410.2023.10140045
• Deng, Ruoyu, and Heuy Dong Kim. 2017. “CFD Study on Inlet Unstart Prediction of Dual-Mode Scramjet.” Journal of Mechanical Science and Technology 31 (11): 5311–18. https://doi.org/10.1007/s12206-017-1025-0
• Deng, Zhihong, Cheng Li, Lijian Yin, Bo Wang, and Xuan Xiao. 2018. “An Adaptive Robust Unscented Kalman Filter Based Matching Algorithm for Underwater Gravity Aided Navigation.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018670
• Deng, Ke, Fei Long, and Su Wang. 2013. “Simulating Optimal Control of an Inertial Platform Stabilization Loop Using Genetic Algorithms.” In 2013 Fourth Global Congress on Intelligent Systems. IEEE. https://doi.org/10.1109/gcis.2013.34
• Deng, Feng, and Ning Qin. 2021. “Vortex-Generating Shock Control Bumps for Robust Drag Reduction at Transonic Speeds.” AIAA Journal 59 (10): 3900–3909. https://doi.org/10.2514/1.j060528
• Deng, Zhi-Liang, Jin Sun, Fei Ding, and Mohamed Wahab Mohamed Ismail. 2019b. “A Novel Damping Method for Strapdown Inertial Navigation System.” IEEE Access 7: 49549–57. https://doi.org/10.1109/access.2019.2910550
• Deng, Zhihong, Mu Sun, and Bo Wang. 2014. “Error Modulation Scheme Analysis of Dual-Axis Rotating Strap-down Inertial Navigation System Based on FOG.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896709
• Deng, Jia, Sentang Wu, and Zhihui Xing. 2016. “Analysis and Design of Terminal Guidance with Large Angular on a Saucer-Shaped UAV.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7829007
• Deng, Zhihong, Wenzhe Zhang, Zhidong Meng, and Tianhao Peng. 2026. “A DualAttNet-Based Deep Adaptive Kalman Filter in Inertial Navigation.” IEEE Sensors Journal 26 (6): 8635–44. https://doi.org/10.1109/jsen.2026.3657758
• Denis-Vidal, Liliane, Carine Jauberthie, and Michel Kieffer. 2019. “Optimal Experiment Design for Bounded-Error Estimation of Nonlinear Models.” In 2019 IEEE 58th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc40024.2019.9030003
• Denis-Vidal, Lilianne, Ghislaine Joly-Blanchard, and Céline Noiret. 2003. “System Identifiability (Symbolic Computation) and Parameter Estimation (Numerical Computation).” Numerical Algorithms 34 (2–4): 283–92. https://doi.org/10.1023/b:numa.0000005366.05704.88
• Deokhwa Hong, Hyunki Lee, Hyungsuck Cho, Youngjin Park, and Jong Hyung Kim. 2008. “Visual Gyroscope: Integration of Visual Information with Gyroscope for Attitude Measurement of Mobile Platform.” In 2008 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2008.4694693
• Der Kiureghian, Armen. 2001. “Risk Assessment of Satellite Launch with Reusable Launch Vehicle.” Reliability Engineering & System Safety 74 (3): 353–60. https://doi.org/10.1016/s0951-8320(01)00084-9
• Desai, S. S., S. Viswanathan, and M. A. Ramaswamy. 1977. “Numerical Evaluation of Transonic Wave Drag.” Journal of Aircraft 14 (2): 215–17. https://doi.org/10.2514/3.44585
• Dessornes, O., and D. Scherrer. 2005. “Tests of the JAPHAR Dual Mode Ramjet Engine.” Aerospace Science and Technology 9 (3): 211–21. https://doi.org/10.1016/j.ast.2005.01.007
• Destarac, D., and J. van der Vooren. 2004. “Drag/thrust Analysis of Jet-Propelled Transonic Transport Aircraft; Definition of Physical Drag Components.” Aerospace Science and Technology 8 (6): 545–56. https://doi.org/10.1016/j.ast.2004.03.004
• Dettbarn, August J. C. 1957. “Application of Telemetry to Flight Testing at Boeing Airplane Company, Wichita Division.” IRE Transactions on Telemetry and Remote Control TRC-3 (1): 1–12. https://doi.org/10.1109/irettrc.1957.6541504
• Deval Samirbhai, Mehta, Yan Wending, and Shoushun Chen. 2018. “A Star Shortlisting Technique for a Lost-in-Space Mode Star Tracker.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396398
• Devanath, B., and M. Laila Beebi. 2016. “Comparison of QEG and Maximum L/D Trajectory Generation on Approach and Landing for Reusable Launch Vehicle.” In 2016 International Conference on Advanced Communication Control and Computing Technologies (ICACCCT). IEEE. https://doi.org/10.1109/icaccct.2016.7831668
• Devaud, E., H. Siguerdidjane, and S. Font. n.d. “Nonlinear Dynamic Autopilot Design for the Non-Minimum Phase Missile.” In Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171), vol. 4. IEEE. https://doi.org/10.1109/cdc.1998.762074
• Devesa, Bernard, Christophe Jourdan, and Christian Marc. 2004. “Ground-Effect Identification and Autoland System Validation from Flight Data.” Journal of Aircraft 41 (4): 730–34. https://doi.org/10.2514/1.3612
• Devyatisilnyi, A. S., and K. A. Chislov. 2012. “Three-Component Position Correctable Astro-Inertial Navigation System with a Function for Determining Gravitational Field Strength.” Measurement Techniques 55 (2): 115–18. https://doi.org/10.1007/s11018-012-9926-x
• Di Liu, Yuming Bo, Panlong Wu, and Gaopeng Zhao. 2008. “Application of Wavelet Neural Network to Initial Alignment of Strapdown Inertial Navigation System.” In 2008 IEEE International Conference on Networking, Sensing and Control. IEEE. https://doi.org/10.1109/icnsc.2008.4525238
• Diao, Zhanlin, Haiyang Quan, Lidong Lan, and Yifei Han. 2013. “Analysis and Compensation of MEMS Gyroscope Drift.” In 2013 Seventh International Conference on Sensing Technology (ICST). IEEE. https://doi.org/10.1109/icsenst.2013.6727722
• Dicus, J. H. 1975. “FORTRAN Program to Generate Engine Inlet Flow Contour Maps and Distortion Parameters.” Computer-Aided Design 7 (3): 206. https://doi.org/10.1016/0010-4485(75)90046-9
• Dietz, G. 2005. “Passive Shock Control Concept for Drag Reduction in Transonic Flow.” Journal of Aircraft 42 (3): 794–99. https://doi.org/10.2514/1.11881
• Diltemiz, Seyid Fehmi. 2021. “Failure Analysis of Aircraft Main Landing Gear Cylinder Support.” Engineering Failure Analysis 129: 105711. https://doi.org/10.1016/j.engfailanal.2021.105711
• Din, Hussamud, Faisal Iqbal, Jiwon Park, and Byeungleul Lee. 2022. “Bias-Repeatability Analysis of Vacuum-Packaged 3-Axis MEMS Gyroscope Using Oven-Controlled System.” Sensors 23 (1): 256. https://doi.org/10.3390/s23010256
• Ding, Xiangru, Zhaobing Chen, Zhaolong Wu, and Xiushuo Wang. 2025. “A Scheme for System Error Calibration and Compensation of the Initial State of MEMS Inertial Navigation.” Sensors 25 (21): 6668. https://doi.org/10.3390/s25216668
• Ding, Jianbin, Guang Feng, Panglun Liu, Li Yuan, Yiyao Jiang, and Bingyan Jiang. 2026. “Structurally-Based Dual-Torsional Modeling of Nose Landing Gear for Nonlinear Shimmy Dynamics Analysis.” Nonlinear Dynamics 114 (17): 1112. https://doi.org/10.1007/s11071-026-12702-6
• Ding, Xukai, Zhihu Ruan, Yunfei Pu, Han Zhang, Hongsheng Li, and Liye Zhao. 2022. “Bias Modulation of Force-to-Rebalanced Micro Hemispherical Resonator Gyroscope Based on Mode-Rotation.” IEEE Sensors Journal 22 (16): 15802–16. https://doi.org/10.1109/jsen.2022.3188287
• Dinh, Thien Xuan, and Yoshifumi Ogami. 2012. “Design of a Triple-Axis MEMS-Based Fluidic Gyroscope.” In 2012 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2012.6411230
• Dion, Francois, Stephane Martel, and Jeff DeNatale. 2018. “200mm High Performance Inertial Sensor Manufacturing Process.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358158
• Diop, S., and S. Kribs. 1992. “On the Identifiability of Deterministic Nonlinear Model Parameters.” IFAC Proceedings Volumes 25 (13): 225–29. https://doi.org/10.1016/s1474-6670(17)52286-7
• Do, V. N. n.d. “A Constrained Pole Placement Method for Autopilot Gain Scheduling.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.721032
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2010. “Visualizing Supersonic Inlet Duct Unstart Using Planar Laser Rayleigh Scattering.” Experiments in Fluids 50 (6): 1651–57. https://doi.org/10.1007/s00348-010-1028-4
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2011a. “The Influence of Boundary Layers on Supersonic Inlet Flow Unstart Induced by Mass Injection.” Experiments in Fluids 51 (3): 679–91. https://doi.org/10.1007/s00348-011-1077-3
• Doer, Christopher, and Gert F. Trommer. 2020. “Radar Inertial Odometry with Online Calibration.” In 2020 European Navigation Conference (ENC). IEEE. https://doi.org/10.23919/enc48637.2020.9317343
• Dohyoung Chung, Chan Gook Park, and Jang Gyu Lee. n.d. “Observability Analysis of Strapdown Inertial Navigation System Using Lyapunov Transformation.” In Proceedings of 35th IEEE Conference on Decision and Control, vol. 1. IEEE. https://doi.org/10.1109/cdc.1996.574240
• Donahue, Benjamin B. 1997. “Lunar Landing Craft for the Reusable Launch Vehicle and Shuttle Vehicles.” Journal of Spacecraft and Rockets 34 (4): 564–66. https://doi.org/10.2514/2.3249
• Donahue, Benjamin B., Vincent A. Weldon, and Stephen W. Paris. 2008. “Low Recurring Cost, Partially Reusable Heavy Lift Launch Vehicle.” Journal of Spacecraft and Rockets 45 (1): 90–94. https://doi.org/10.2514/1.29313
• Dong, Yiqun. 2018. “An Application of Deep Neural Networks to the in-Flight Parameter Identification for Detection and Characterization of Aircraft Icing.” Aerospace Science and Technology 77: 34–49. https://doi.org/10.1016/j.ast.2018.02.026
• Dong, Haifeng, and Yang Gao. 2017. “Comparison of Compensation Mechanism between an NMR Gyroscope and an SERF Gyroscope.” IEEE Sensors Journal 17 (13): 4052–55. https://doi.org/10.1109/jsen.2017.2703601
• Dong, Chunyun, Zhi Guo, and Xiaolong Chen. 2021. “Robust Trajectory Planning for Hypersonic Glide Vehicle with Parametric Uncertainties.” Mathematical Problems in Engineering 2021: 1–19. https://doi.org/10.1155/2021/3676810
• Dong, Y., P. Zwahlen, A.-M. Nguyen, F. Rudolf, and J.-M. Stauffer. 2010. “High Performance Inertial Navigation Grade Sigma-Delta MEMS Accelerometer.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507135
• Dong Gwan Lee, Kil Seok Cho, and Jin Hwa Shin. 2015. “A Simple Prediction Method of Ballistic Missile Trajectory to Designate Search Direction and Its Verification Using a Testbench.” In 2015 10th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc.2015.7244461
• Dongqing Gu and Naser El-Sheimy. 2008. “Heading Accuracy Improvement of MEMS IMU/DGPS Integrated Navigation System for Land Vehicle.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570083
• Donguk Yang, Jong-Kwan Woo, Khalil Najafi, Sangwoo Lee, Jay Mitchell, and Dorian Challoner. 2015. “±2ppm Frequency Drift and 300x Reduction of Bias Drift of Commercial 6-Axis Inertial Measurement Units Using a Low-Power Oven-Control Micro Platform.” In 2015 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2015.7370326
• Dougherty, John J., Hossny El-Sherief, and David S. Hohman. 1994. “Use of the Global Positioning System for Evaluating Inertial Measurement Unit Errors.” Journal of Guidance, Control, and Dynamics 17 (3): 435–41. https://doi.org/10.2514/3.21218
• Dougherty, J. J., H. El-Sherief, and D. J. Simon. n.d. “Application of GPS for Missile Post Flight Guidance Accuracy Analysis.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.721039
• Draper, C. S. 1981. “Origins of Inertial Navigation.” Journal of Guidance and Control 4 (5): 449–63. https://doi.org/10.2514/3.19748
• DrAvico, L., M. Tanelli, and S. M. Savaresia. 2018. “Experimental Validation of Landing-Gear Dynamics for Anti-Skid Control Design.” In 2018 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2018.8550258
• Dreef, H. J., Shengling Shi, Xiaodong Cheng, M. C. F. Donkers, and Paul M. J. Van den Hof. 2022. “Excitation Allocation for Generic Identifiability of Linear Dynamic Networks with Fixed Modules.” IEEE Control Systems Letters 6: 2587–92. https://doi.org/10.1109/lcsys.2022.3171172
• Droeschel, David, Stefan May, Dirk Holz, and Sven Behnke. 2011. “Fusing Time-of-Flight Cameras and Inertial Measurement Units for Ego-Motion Estimation.” Automatika 52 (3): 189–98. https://doi.org/10.1080/00051144.2011.11828419
• Du, Zhao-bo, Wei Huang, and Li Yan. 2019b. “Parametric Study on Mixing Augmentation Mechanism Induced by Air Injection in a Shock-Induced Combustion Ramjet Engine.” Energy 186: 115895. https://doi.org/10.1016/j.energy.2019.115895
• Du, Tao, Tong Qin, Dong Li, et al. 2025. “Lifecycle Cost Estimation and Critical Parameters Analysis for Reusable Launch Vehicle.” Advances in Astronautics 8 (2): 89–106. https://doi.org/10.1007/s42423-025-00187-1
• Du, Binhan, Jinlong Song, and Zhiyong Shi. 2019a. “An Anomaly Diagnosis Method for Redundant Inertial Measurement Unit and Its Application with Micro-Electro-Mechanical System Sensors.” Applied Sciences 9 (8): 1606. https://doi.org/10.3390/app9081606
• Du, Xueyu, Maosong Wang, Wenqi Wu, and Jiarui Cui. 2021. “High-Accuracy Autonomous Navigation Algorithm for Long-Distance Land Navigation in GNSS-Denied Environments.” In 2021 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus52573.2021.9641426
• Du, Xiaolei, Yong Xu, Qi Liu, et al. 2024. “Shimmy Dynamics in a Dual-Wheel Nose Landing Gear with Freeplay under Stochastic Wind Disturbances.” Nonlinear Dynamics 112 (4): 2477–99. https://doi.org/10.1007/s11071-023-09182-3
• Duan, Xiao-Min, and Huiliang Cao. 2021. “Stabilized Inertial Guidance Solution for Rolling Projectile Based on Partial Strapdown Platform.” IEEE Access 9: 116207–14. https://doi.org/10.1109/access.2021.3105412
• Duan, Jianmin, Zhixue Song, Changren Wang, and Dan Liu. 2016. “Inertial Navigation Algorithm Based on Modified Kalman Filter and Wavelet Technique for Intelligent Vehicle.” In 2016 8th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC). IEEE. https://doi.org/10.1109/ihmsc.2016.203
• Duan Chao-yang, Guo Jian-guo, and Zhou Jun. 2010. “Autopilot Design for Missile with Morphing Wings.” In 2010 3rd International Conference on Advanced Computer Theory and Engineering(ICACTE). IEEE. https://doi.org/10.1109/icacte.2010.5579191
• Dufour, Pascal, Madiha Nadri, and Jun Qian. 2015. “An Explicit Optimal Input Design for First Order Systems Identification.” IFAC-PapersOnLine 48 (28): 344–49. https://doi.org/10.1016/j.ifacol.2015.12.151
• Dugundji, John, and John M. Calligeros. 1962. “Similarity Laws for Aerothermoelastic Testing.” Journal of the Aerospace Sciences 29 (8): 935–50. https://doi.org/10.2514/8.9663
• Duncan, D. B. 1958a. “Analysis of an Inertial Guidance System.” Journal of Jet Propulsion 28 (2): 111–16. https://doi.org/10.2514/8.7245
• Dunlop Limited. 1972. “Carbon/carbon Composite Aircraft Brake.” Tribology 5 (3): 107. https://doi.org/10.1016/0041-2678(72)90017-6
• Dunn, J., and D. Howard. 1959. “The Effects of Automatic Gain Control Performance on the Tracking Accuracy of Monopulse Radar Systems.” Proceedings of the IRE 47 (3): 430–35. https://doi.org/10.1109/jrproc.1959.287179
• Dunsworth, L. C., and G. J. Reed. 1979. “Ramjet Engine Testing and Simulation Techniques.” Journal of Spacecraft and Rockets 16 (6): 382–88. https://doi.org/10.2514/3.57678
• Durmuşoğlu, Aslı. 2026. “Robust Semi-Active Control of Quadrotor UAV–Landing Gear for Touchdown-Induced Vibration Suppression under Uncertain Conditions.” Mathematics 14 (12): 2195. https://doi.org/10.3390/math14122195
• Dusek, Hermann M. 1964a. “Error Propagation in Astro-Inertial Guidance Systems for Low-Thrust Missions.” AIAA Journal 2 (5): 879–84. https://doi.org/10.2514/3.2452
• Dushman, A., and H. Sandberg. 1973. “Accuracy of ESG Monitor/sins Inertial Navigation System.” In Ocean 73 - IEEE International Conference on Engineering in the Ocean Environment. IEEE. https://doi.org/10.1109/oceans.1973.1161295
• “Dynamic Scheduling of Modern-Robust-Control Autopilot Designs for Missiles.” 1992. IEEE Control Systems 12 (5): 35–42. https://doi.org/10.1109/37.158896
• Dzamba, T., and J. Enright. 2013. “Optical Trades for Evolving a Small Arcsecond Star Tracker.” In 2013 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2013.6497172
• Eberhardt, E. H. 1963. “Accuracy of Position Determination in Star Tracker Tubes.” IEEE Transactions on Aerospace 1 (2): 54–57. https://doi.org/10.1109/ta.1963.4319366
• Ebner, R. E., and J. G. Mark. 1978. “Redundant Integrated Flight-Control/Navigation Inertial Sensor Complex.” Journal of Guidance and Control 1 (2): 143–49. https://doi.org/10.2514/3.55757
• Ebrahim, Ahmed W., Ibrahim I. Arafa, Hossam Hendy, Yehia Z. Elhalwagy, and Ahmed Omar Elfarouk. 2020. “Initial Alignment of Strap-down Inertial Navigation System on Stationary Base for High-Speed Flying Vehicle.” In 2020 8th International Japan-Africa Conference on Electronics, Communications, and Computations (JAC-ECC). IEEE. https://doi.org/10.1109/jac-ecc51597.2020.9355964
• Eck, Christoph, and Hans P. Geering. 2001. “Generalized Derivation of the EKF Based Inertial Navigation Error Dynamics.” IFAC Proceedings Volumes 34 (15): 259–64. https://doi.org/10.1016/s1474-6670(17)40737-3
• Eckenhoff, Kevin, Patrick Geneva, and Guoquan Huang. 2019. “Sensor-Failure-Resilient Multi-IMU Visual-Inertial Navigation.” In 2019 International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2019.8794295
• Edge, C. F. 1963. “Digital Differential Analyzers vs General Purpose Digital Computers for Schuler-Tuned Inertial Navigation Systems.” IEEE Transactions on Military Electronics MIL-7 (1): 23–29. https://doi.org/10.1109/tme.1963.4323037
• Edwards, R. M. 1982. “Gravity Model Performance in Inertial Navigation.” Journal of Guidance, Control, and Dynamics 5 (1): 73–78. https://doi.org/10.2514/3.56142
• Einicke, Garry A. 2008. “EM Algorithm Convergence for Inertial Navigation System Alignment.” In 2008 47th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2008.4739113
• Eisner, W., and A. F. Goodman. 1964. “Determination of Dominant Error Sources in an Inertial Navigation System by Iterative Weighted Least Squares.” AIAA Journal 2 (4): 722–27. https://doi.org/10.2514/3.2430
• Ekvall, J. C., R. A. Rainen, D. J. Chellman, R. R. Flores, and M. J. Gersbach. 1990. “Elevated Temperature Aluminum Alloys for Advanced Fighter Aircraft.” Journal of Aircraft 27 (9): 836–43. https://doi.org/10.2514/3.45944
• El-Sheikh, G. A., and S. F. Bahgat. n.d. “Robust Autopilot Design for a Beam Rider Guided Missile System.” In Proceedings of the Fifteenth National Radio Science Conference. NRSC ‘98 (Cat. No.98EX109). IEEE. https://doi.org/10.1109/nrsc.1998.711489
• Eldredge, Jeff D., and Hanieh Mousavi. 2026. “Practical Guide to Estimation and Uncertainty Quantification of Aerodynamic Flows.” AIAA Journal 64 (5): 2403–23. https://doi.org/10.2514/1.j066257
• Elenchezhiyan, M., and Ajit Kumar. 2024. “A Comparison of Adaptive Optimizers for Nonlinear Aerodynamic Modeling Using Flight Test Data.” Aerospace Systems 8 (2): 349–58. https://doi.org/10.1007/s42401-024-00320-2
• Ellingson, Gary, Kevin Brink, and Tim McLain. 2018. “Relative Visual-Inertial Odometry for Fixed-Wing Aircraft in GPS-Denied Environments.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373454
• Emery, A. F., Aleksey V. Nenarokomov, and Tushar D. Fadale. 2000. “Uncertainties in Parameter Estimation: The Optimal Experiment Design.” International Journal of Heat and Mass Transfer 43 (18): 3331–39. https://doi.org/10.1016/s0017-9310(99)00378-6
• Eminoglu, Burak, and Bernhard E. Boser. 2018. “Chopped Rate-to-Digital FM Gyroscope with 40ppm Scale Factor Accuracy and 1.2dph Bias.” In 2018 IEEE International Solid - State Circuits Conference - (ISSCC). IEEE. https://doi.org/10.1109/isscc.2018.8310242
• Eminoglu, Burak, Mitchell H. Kline, Igor Izyumin, Yu-Ching Yeh, and Bernhard E. Boser. 2014. “Background Calibrated MEMS Gyroscope.” In IEEE SENSORS 2014 Proceedings. IEEE. https://doi.org/10.1109/icsens.2014.6985152
• Endean, Daniel, Kevin Christ, Patrick Duffy, et al. 2019. “Near-Navigation Grade Tuning Fork MEMS Gyroscope.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739669
• Endean, Daniel, Xiao Zhu Fan, Max Glenn, Robert Horning, John Reinke, and Barry Roberts. 2017. “Tactical-Grade Dual-Chip Inertial Sensor Assembly.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935671
• Engedy, Istvan, and Gabor Horvath. 2015. “Path Reconstruction Based on Gyroscope Bias Estimation Using GPS.” In 2015 IEEE International Instrumentation and Measurement Technology Conference (I2MTC) Proceedings. IEEE. https://doi.org/10.1109/i2mtc.2015.7151493
• Engelsman, Daniel, and Itzik Klein. 2026. “Towards Learning-Based Gyrocompassing.” Engineering Applications of Artificial Intelligence 163: 112842. https://doi.org/10.1016/j.engappai.2025.112842
• Enright, John, Ilija Jovanovic, and Brendon Vaz. 2015. “On-Orbit Star Tracker Recalibration: A Case Study.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119194
• Ephgrave, James T. 1962. “Response of a Schuler-Tuned Inertial Guidance System to Random Errors.” Journal of the Aerospace Sciences 29 (2): 233–34. https://doi.org/10.2514/8.9374
• Erkan, Derin, and Erdinc Tatar. 2024. “Improving the Temperature Stability of MEMS Gyroscope Bias with on-Chip Stress Sensors.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502041
• Erlank, Alexander O., and Willem H. Steyn. 2014. “Arcminute Attitude Estimation for CubeSats with a Novel Nano Star Tracker.” IFAC Proceedings Volumes 47 (3): 9679–84. https://doi.org/10.3182/20140824-6-za-1003.00267
• Ermakov, R. V., A. A. L’vov, D. V. Kondratov, and D. Yu. Livshits. 2022. “Vibrational Error Model Update for a Hemispherical Resonator Gyroscope.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815386
• Ermakov, R. V., E. N. Skripal, D. V. Kondratov, A. A. L’vov, A. A. Seranova, and D. E. Gutsevich. 2018. “Development of a Vibrational Error Model of a Hemispherical Resonator Gyroscope.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405894
• Eroglu, Orhan, and Guray Yilmaz. 2013a. “A Novel Fast and Accurate Algorithm for Terrain Referenced UAV Localization.” In 2013 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2013.6564746
• Eroglu, Orhan, and Guray Yilmaz. 2013b. “A Terrain Referenced UAV Localization Algorithm Using Binary Search Method.” Journal of Intelligent & Robotic Systems 73 (1–4): 309–23. https://doi.org/10.1007/s10846-013-9922-7
• Erol, Bihter, Muhammed Raşit Çevikalp, and Serdar Erol. 2023. “Accuracy Assessment of the SRTM2gravity High-Resolution Topographic Gravity Model in Geoid Computation.” Survey Review 55 (393): 546–56. https://doi.org/10.1080/00396265.2023.2183332
• Etzweiler, G. 1969. “Practical Servomechanism Design.” IEEE Transactions on Automatic Control 14 (5): 604–6. https://doi.org/10.1109/tac.1969.1099278
• Evans, D. 1957. “A Positioning Servomechanism with a Finite Time Delay and a Signal Limiter.” IRE Transactions on Automatic Control 2 (1): 17–28. https://doi.org/10.1109/tac.1957.1103778
• Evans, M. J., G. H. Myers, and J. W. Timko. 1963. “Command Guidance of Telstar Launch Vehicle.” Bell System Technical Journal 42 (5): 2153–68. https://doi.org/10.1002/j.1538-7305.1963.tb00962.x
• Evans, Jay V., William C. B. Senior, Rohan M. Gejji, and Carson D. Slabaugh. 2023. “Performance of a Solid-Fuel Ramjet Combustor with Bypass Air Addition.” Journal of Propulsion and Power 39 (2): 167–75. https://doi.org/10.2514/1.b38788
• “Experimental Investigation of Cermet Turbine Blades in an Axial-Flow Turbojet Engine.” 1958. Wear 1 (5): 449. https://doi.org/10.1016/0043-1648(58)90148-0
• Ezzeldin, Abdullah, and Zhenlong Wu. 2025. “CFD-Driven Enhancement for Supersonic Aircraft Variable Geometry Inlet.” Applied Sciences 15 (17): 9825. https://doi.org/10.3390/app15179825
• Fagin, S., A. Graefe, and E. Grinoch. 1969. “Stochastic Servomechanism Design via Optimal Filter Theory.” IEEE Transactions on Automatic Control 14 (6): 722–26. https://doi.org/10.1109/tac.1969.1099292
• Falkiewicz, Nathan J., and Carlos E. S. Cesnik. 2011b. “Proper Orthogonal Decomposition for Reduced-Order Thermal Solution in Hypersonic Aerothermoelastic Simulations.” AIAA Journal 49 (5): 994–1009. https://doi.org/10.2514/1.j050701
• Falkiewicz, Nathan J., and Carlos E. S. Cesnik. 2017. “Enhanced Modal Solutions for Structural Dynamics in Aerothermoelastic Analysis.” Journal of Aircraft 54 (3): 870–89. https://doi.org/10.2514/1.c034122
• Falkiewicz, Nathan J., Carlos E. S. Cesnik, Andrew R. Crowell, and Jack J. McNamara. 2011. “Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation.” AIAA Journal 49 (8): 1625–46. https://doi.org/10.2514/1.j050802
• Famellos, Petros, Athanasios Skevas, Asterios Koutsiadis, Christos Koutsouras, and Pericles Panagiotou. 2024. “Design and Analysis of a Base Bleed Unit for the Drag Reduction of a High-Power Rocket Operating at Transonic Speeds.” Aerospace 11 (5): 385. https://doi.org/10.3390/aerospace11050385
• Fan, Xiaoshuai, Xibin Bai, Zhenyu Jiang, Longbin Liu, and Shifeng Zhang. 2021. “Design and Verification of Attitude Control System for a Boost-Glide Rocket.” IEEE Access 9: 136360–72. https://doi.org/10.1109/access.2021.3117704
• Fan, Bo, Shuwen Guo, Mengmeng Cheng, et al. 2019a. “Frequency Symmetry Comparison of Cobweb-Like Disk Resonator Gyroscope with Ring-Like Disk Resonator Gyroscope.” IEEE Electron Device Letters 40 (9): 1515–18. https://doi.org/10.1109/led.2019.2930632
• Fan, Yonghua, Xin Li, Jun Yang, and Yuzhuo Zhang. 2008. “Design of Autopilot for Aerodynamic/Reaction-Jet Multiple Control Missile Using Variable Structure Control.” In 2008 27th Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2008.4604993
• Fan, Gang, Xiaojin Liu, Yun Li, et al. 2025. “A Terrain-Aided Navigation Method Incorporating Terrain Matching and Terrain Suitability Analysis.” IEEE Access 13: 71066–80. https://doi.org/10.1109/access.2025.3562768
• Fan, Yu, Fang Lu, Wuxuan Zhu, Guangzhou Bai, and Liang Yan. 2017b. “A Hybrid Model Algorithm for Hypersonic Glide Vehicle Maneuver Tracking Based on the Aerodynamic Model.” Applied Sciences 7 (2): 159. https://doi.org/10.3390/app7020159
• Fan, Jun-fang, and Zhong Su. 2010. “Missile Longitudinal Autopilot Design Using Backstepping Approach.” In 2010 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2010.5446743
• Fan, Jun-fang, Zhong Su, and Zhen-xuan Cheng. 2010. “Missile Autopilot Design and Analysis Based on Backstepping.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5634040
• Fan, Yu, Wuxuan Zhu, and Guangzhou Bai. 2016. “A Cost-Effective Tracking Algorithm for Hypersonic Glide Vehicle Maneuver Based on Modified Aerodynamic Model.” Applied Sciences 6 (10): 312. https://doi.org/10.3390/app6100312
• Fang, Bertrand. 1967. “Kalman-Bucy Filter for Optimum Radio-Inertial Navigation.” In Sixth Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/sap.1967.272983
• Fang, Xinyue, Haonan Jiang, Yuanli Cai, Junshuai Luo, Hong Shen, and Yifan Deng. 2024b. “TimeVAE-Based Hypersonic Glide Vehicle Trajectory Generation Method and Evaluation.” In 2024 IEEE 25th China Conference on System Simulation Technology and its Application (CCSSTA). IEEE. https://doi.org/10.1109/ccssta62096.2024.10691869
• Fang, Haiquan, Xiaolong Wang, Yuxiang Wu, and Jiasen Zhang. 2024a. “Dynamics Modeling and Analysis of Airliner Landing Gear Light Brackets.” In 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae62008.2024.11026274
• Fang, Wei, and Lianyu Zheng. 2018. “Rapid and Robust Initialization for Monocular Visual Inertial Navigation within Multi-State Kalman Filter.” Chinese Journal of Aeronautics 31 (1): 148–60. https://doi.org/10.1016/j.cja.2017.10.011
• Fanming Liu, Dong Qian, Yingfa Zhang, and Yan Li. 2010. “A Computer Simulation of the Influence of GGI and Inertial Sensors on Gravity Gradient Aided Navigation.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5632539
• Farahani, Mohammad, Abbas Daliri, and Javad Sepahi Younsi. 2019. “Supersonic Inlet Buzz Detection Using Pressure Measurement on Wind Tunnel Wall.” Aerospace Science and Technology 86: 782–93. https://doi.org/10.1016/j.ast.2019.02.002
• Fares, Hadi, Ammar Mohanna, and Bilal Kaddouh. 2026. “Real-Time Elevation and Orientation-Aware Visual Localization for GNSS-Denied Drone Navigation.” Drones 10 (6): 445. https://doi.org/10.3390/drones10060445
• Farrell, James L. 1985. “Strapdown Inertial Navigation System Requirements Imposed by Synthetic Aperture Radar.” Journal of Guidance, Control, and Dynamics 8 (4): 433–39. https://doi.org/10.2514/3.20002
• Farrell, Jay A., Felipe O. Silva, Farzana Rahman, and Jan Wendel. 2022. “Inertial Measurement Unit Error Modeling Tutorial: Inertial Navigation System State Estimation with Real-Time Sensor Calibration.” IEEE Control Systems 42 (6): 40–66. https://doi.org/10.1109/mcs.2022.3209059
• Farret, D., G. Duc, and J. P. Harcaut. 2002. “Discrete-Time LPV Controller for Robust Missile Autopilot Design.” IFAC Proceedings Volumes 35 (1): 127–32. https://doi.org/10.3182/20020721-6-es-1901.01246
• Faruqi, Farhan A., and Kenneth J. Turner. 2000. “Extended Kalman Filter Synthesis for Integrated Global Positioning/inertial Navigation Systems.” Applied Mathematics and Computation 115 (2–3): 213–27. https://doi.org/10.1016/s0096-3003(98)10068-1
• Fast, Brian, Robert Miklosovic, and Aaron Radke. 2008. “Active Disturbance Rejection Control of a MEMS Gyroscope.” In 2008 American Control Conference. IEEE. https://doi.org/10.1109/acc.2008.4587076
• Fayette, Lucie, Karl Brendel, and France Mentré. 2026. “Advances and Further Comparison of Software Tools for Fisher Information Matrix-Based Design Evaluation in Pharmacometrics.” Pharmaceutical Research 43 (4): 1113–30. https://doi.org/10.1007/s11095-026-04024-4
• Fazelinia, Mojtaba, Saeed Ebadollahi, and Soheil Ganjefar. 2024. “Stochastic Analysis of Drift Error of Gyroscope in the Single-Axis Attitude Determination.” Measurement 237: 115136. https://doi.org/10.1016/j.measurement.2024.115136
• Fedele, Giuseppe, Luigi D’Alfonso, and Gaetano D’Aquila. 2018. “Magnetometer Bias Finite-Time Estimation Using Gyroscope Data.” IEEE Transactions on Aerospace and Electronic Systems 54 (6): 2926–36. https://doi.org/10.1109/taes.2018.2832978
• Feder, H. J. S., J. J. Leonard, and C. M. Smith. n.d. “Adaptive Sensing for Terrain Aided Navigation.” In IEEE Oceanic Engineering Society. OCEANS’98. Conference Proceedings (Cat. No.98CH36259), vol. 1. IEEE. https://doi.org/10.1109/oceans.1998.725763
• Fedorov, A. V., and N. D. Malmuth. 1997. “Supersonic Transitional Airfoil Shapes of Minimum Drag.” Journal of Aircraft 34 (6): 713–18. https://doi.org/10.2514/2.2249
• Fedotov, A. A., and S. Yu. Perepelkina. 2019. “Improvement in Accuracy of Strapdown Inertial Navigation System Due to Controlled Precessional Motion.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769349
• Fegley, K. A., and C. N. Weygandt. 1963. “Error Analysis of a Doppler: Inertial Navigation System by Analog Simulation.” Transactions of the American Institute of Electrical Engineers, Part I: Communication and Electronics 82 (2): 123–30. https://doi.org/10.1109/tce.1963.6373364
• Fei, J., and C. Batur. 2007. “A Novel Adaptive Sliding Mode Controller for MEMS Gyroscope.” In 2007 46th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2007.4434098
• Fei, Yu, and Sun Feng. 2005. “Application of H ∞ Filtering in the Initial Alignment of Strapdown Inertial Navigation System.” Journal of Marine Science and Application 4 (1): 50–53. https://doi.org/10.1007/s11804-005-0046-8
• Fei, J., M. Hua, and Y. Xue. 2010. “A Comparative Study of Adaptive Control Approaches for MEMS Gyroscope.” In 2010 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2010.5611258
• Fei, Juntao, and Zhuli Yuan. 2013. “Dynamic Sliding Mode Control of MEMS Gyroscope.” In 2013 IEEE International Conference on Control Applications (CCA). IEEE. https://doi.org/10.1109/cca.2013.6662788
• Fei Xing, Ying Dong, Zheng You, and Qin Zhou. 2006. “APS Star Tracker and Its Attitude Estimation.” In 2006 1st International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2006.1627697
• Fekry, Alaa, Eslam M. Mustafa, Ahmed M. Kamel, Yehia Elhalwagy, and Ashraf Abosekeen. 2025. “Optimized NARX-Based Noise Mitigation for Enhanced Navigation Accuracy of Low-Cost IMUs in GNSS-Denied Environments.” In 2025 International Telecommunications Conference (ITC-Egypt). IEEE. https://doi.org/10.1109/itc-egypt66095.2025.11186698
• Fekry, Alaa, Eslam M. Mustafa, Ahmed M. Kamel, Yehia Elhalwagy, Ashraf Abosekeen, and Aboelmagd Noureldin. 2026. “PINNARX: A Physics-Informed Framework for Resilient Inertial Navigation in GNSS-Denied Environments.” IEEE Transactions on Instrumentation and Measurement 75: 1–17. https://doi.org/10.1109/tim.2026.3659553
• fen Wang, Fen, Tong Zhang, and Wen Xing Fu. 2018. “An Improved Principal Component Analysis Algorithm on FDI of Redundant Inertial Measurement Unit.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483080
• Feng, Jiang. 2018. “A Review of Rotary Modulation Technology Applied to Strapdown Inertial Navigation System.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018882
• Feng, Lu, Zhihong Deng, Bo Wang, and Shunting Wang. 2016. “Absolute Velocity Damping Algorithm with Varying Damping Ratio for Inertial Navigation Systems Based on Kalman Filter.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7829179
• Feng, Lihui, Wenjun Gu, Ke Zhao, et al. 2014. “Novel Self-Compensation Method to Lower the Temperature Drift of a Quartz MEMS Gyroscope.” Microsystem Technologies 20 (12): 2231–37. https://doi.org/10.1007/s00542-014-2113-z
• Feng, Guohu, and Xinsheng Huang. 2014. “Observability Analysis of Navigation System Using Point-Based Visual and Inertial Sensors.” Optik 125 (3): 1346–53. https://doi.org/10.1016/j.ijleo.2013.08.004
• Feng, Guang, Bingyan Jiang, and Yiyao Jiang. 2023. “Effect of Multi-Joint Clearance Coupling on Shimmy of Nose Landing Gear.” Aerospace 10 (11): 911. https://doi.org/10.3390/aerospace10110911
• Feng, Hai, Yanting Li, Tai Jin, and Kun Wu. 2026a. “Effects of Distributed Injection on Inlet Unstart and Combustion Performance of a Model Scramjet under Thermal Nonequilibrium Conditions.” International Journal of Hydrogen Energy 275: 157471. https://doi.org/10.1016/j.ijhydene.2026.157471
• Feng, Xinle, Yali Lv, Yang Gao, and Yuankai Li. 2020. “Adaptive Radau Pseudo-Spectral Optimization for Descending Trajectory of a Hypersonic Cruise Vehicle.” Aerospace Systems 3 (4): 275–86. https://doi.org/10.1007/s42401-020-00069-4
• Feng, Fei, Hong Nie, Ming Zhang, and Yiming Peng. 2015. “Effect of Torsional Damping on Aircraft Nose Landing-Gear Shimmy.” Journal of Aircraft 52 (2): 561–68. https://doi.org/10.2514/1.c032772
• Feng, Sun, Sun Qian, Ben Yueyang, Zhang Ya, and Wei Gao. 2012a. “A New Method of Initial Alignment and Self-Calibration Based on Dual-Axis Rotating Strapdown Inertial Navigation System.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236959
• Feng, Shan, Qingke Tan, Qingdong Li, and Zhang Ren. 2017. “Trajectory Tracking for Hypersonic Glide Vehicles Based on Improved Sine-AIMM.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028225
• Feng, Lu, Bo Wang, Zhihong Deng, Shunting Wang, and Qizhen Wang. 2013. “On-Line Self-Calibration for Inertial Platform System with a Single Totally Free Axis.” In 2013 9th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc.2013.6606101
• Feng, Kaiqiang, Ziming Wang, Jie Li, and Shengkai Shen. 2026b. “SINDy-Based Motion-Dependent Nonholonomic Constraint Covariance Adaptation for GNSS-Denied MEMS/INS Vehicle Navigation.” Micromachines 17 (10): 1187. https://doi.org/10.3390/mi17101187
• Feng, Guohu, Wenqi Wu, and Jinling Wang. 2012b. “Observability Analysis of a Matrix Kalman Filter-Based Navigation System Using Visual/Inertial/Magnetic Sensors.” Sensors 12 (7): 8877–94. https://doi.org/10.3390/s120708877
• Feng, Bo, and Peng Zhang. 2023. “Stationary Base Self-Alignment of Inertial Navigation System without Velocity Covariance Matrix.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10452087
• Feng Sun, Yu Gao, Yang Lu, and Jia Sun. 2009. “Design and Realization of Strapdown Inertial Navigation Accelerometer Signal Acquisition Unit.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246406
• Feng Tan, Guangren Duan, and Lijun Zhao. 2006. “Robust Controller Design for Autopilot of a BTT Missile.” In 2006 6th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2006.1714308
• Ferguson, M. I., D. Keymeulen, C. Peay, K. Yee, and D. L. Li. 2005. “Effect of Temperature on MEMS Vibratory Rate Gyroscope.” In 2005 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2005.1559561
• Ferreres, G., and M. M’saad. 1994. “H ∞ Design of a Multivariable Missile Autopilot Using Coprirne Factors.” IFAC Proceedings Volumes 27 (13): 141–46. https://doi.org/10.1016/s1474-6670(17)45790-9
• Fetner, E. M. 1961. “Shock-Layer Attentuation Data Collected from Missile Tests at the Atlantic Missile Range.” Planetary and Space Science 6: 225. https://doi.org/10.1016/0032-0633(61)90032-0
• “The Fiber-Optic Gyroscope.” 1993. Optics & Laser Technology 25 (6): 406. https://doi.org/10.1016/0030-3992(93)90010-d
• Fields, Shannon, and Thomas E. Bullock. 1996. “A Minimal Linear Fractional Approach to Gain Scheduling Missile Autopilot Design.” IFAC Proceedings Volumes 29 (1): 7458–63. https://doi.org/10.1016/s1474-6670(17)58888-6
• Filatov, Yu. V., A. M. Boronakhin, V. B. Dao, and V. T. Le. 2014. “Sensor Information Processing for Calibration of Inertial Measurement Units.” In 2014 International Conference on Mechanical Engineering, Automation and Control Systems (MEACS). IEEE. https://doi.org/10.1109/meacs.2014.6986924
• Filatov, P. A., I. S. Kruzhilin, P. V. Larionov, A. D. Morozov, A. A. Fomichev, and A. B. Tarasenko. 2022. “Estimation of Dither Effect on the Accuracy of a Navigation System Based on Laser Gyroscopes with a Planar Circuit and Q-Flex Accelerometers.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815444
• Filyashkin, M. K. 2018. “Inertial-Satellite Navigation System for Unmanned Aerial Vehicles with Double-Deck Estimation of Flight-Navigation Parameters.” In 2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc.2018.8576299
• Filyashkin, N. K., and V. S. Yatskivsky. 2013. “Prediction of Inertial Navigation System Error Dynamics in INS/GPS System.” In 2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD). IEEE. https://doi.org/10.1109/apuavd.2013.6705327
• Finkbeiner, Ann. 2013. “Astronomy: Star Tracker.” Nature 495 (7441): 296–98. https://doi.org/10.1038/495296a
• Fischer, Irene. 1954. “The Deflection of the Vertical in the Western and Central Mediterranean Area.” Bulletin géodésique 34 (1): 343–53. https://doi.org/10.1007/bf02529948
• Fitzgerald, Robert J. 1974. “Effects of Range-Doppler Coupling on Chirp Radar Tracking Accuracy.” IEEE Transactions on Aerospace and Electronic Systems AES-10 (4): 528–32. https://doi.org/10.1109/taes.1974.307809
• Fitzgerald, Karen. 1987. “Targeting the Enemy: Radar, Radio Control and Inertial-Guidance Systems Helped Improve the Accuracy of Both Offensive and Defensive Weaponry.” IEEE Spectrum 24 (8): 42–49. https://doi.org/10.1109/mspec.1987.6448226
• Fitzgerald, R. J. 1994. “Random Tropospheric Effects in Command Guidance by Multilateration and Interferometry.” IEEE Transactions on Aerospace and Electronic Systems 30 (1): 249–57. https://doi.org/10.1109/7.250425
• Flila, S., P. Dufour, and H. Hammouri. 2008. “Optimal Input Design for Online Identification: A Coupled Observer-MPC Approach.” IFAC Proceedings Volumes 41 (2): 11457–62. https://doi.org/10.3182/20080706-5-kr-1001.01941
• Fokin, Leonid A. 2007. “Multisensor Data Fusion in Adaptive Astro-Satellite-Inertial Navigation System.” In 2007 Siberian Conference on Control and Communications. IEEE. https://doi.org/10.1109/sibcon.2007.371294
• Forgione, Marco, Xavier Bombois, Paul M. J. Van den Hof, and Hakan Hjalmarsson. 2014. “Experiment Design for Parameter Estimation in Nonlinear Systems Based on Multilevel Excitation.” In 2014 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2014.6862274
• Forke, Roman, Takashiro Tsukamoto, Alexey Shaporin, et al. 2024. “Advancement in the Mems Gyroscope from a Vibrating Tuning Fork to a Tuned Ring with Comb Electrodes.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502098
• Foss, Bjarne. 1987. “A Modified Optimal Input Design Criterion.” In 26th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1987.272786
• Fourie, Dehann, and Johan Meyer. 2009. “Implementation of a Low-Cost Inertial Navigation System on a Real-Time Linux Platform.” In AFRICON 2009. IEEE. https://doi.org/10.1109/afrcon.2009.5308248
• Fowler, K. R. n.d. “Instrumentation for Ballistic Missile Defense: Lessons Learned from the LEAP Experiment.” In IMTC/98 Conference Proceedings. IEEE Instrumentation and Measurement Technology Conference. Where Instrumentation is Going (Cat. No.98CH36222), vol. 1. IEEE. https://doi.org/10.1109/imtc.1998.679660
• Fowler, K. R. 1998. “Instrumentation for Ballistic Missile Defense: Lessons Learned from the LEAP Experiment.” IEEE Transactions on Instrumentation and Measurement 47 (5): 1092–95. https://doi.org/10.1109/19.746562
• Fraiser, H. R. 1960. “Supersonic Inlet Dynamics.” Journal of the Aerospace Sciences 27 (6): 429–36. https://doi.org/10.2514/8.8575
• Freed, Lawrence E., and Kenneth L. Miller. 1961. “A Method of Damping Missile Structural Bending Modes for Autopilot Design.” Planetary and Space Science 7: 26–39. https://doi.org/10.1016/0032-0633(61)90283-5
• Freeman, Delma C., Theodore A. Talay, and R. Eugene Austin. 1997. “Reusable Launch Vehicle Technology Program.” Acta Astronautica 41 (11): 777–90. https://doi.org/10.1016/s0094-5765(97)00197-5
• French, Kenneth E. 1965. “Parachute-and-Retrorocket Landing System for Vertical Descent.” Journal of Spacecraft and Rockets 2 (5): 797–99. https://doi.org/10.2514/3.28285
• French, Kenneth E. 1966. “Parachute and Cushion Landing System.” Journal of Spacecraft and Rockets 3 (7): 1133–34. https://doi.org/10.2514/3.28612
• Freydin, Maxim, and Earl H. Dowell. 2021. “Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow.” AIAA Journal 59 (7): 2725–36. https://doi.org/10.2514/1.j060085
• Fruchtenicht, H. 1974. “Notes on Duct Influences on Line-of-Sight Propagation.” IEEE Transactions on Antennas and Propagation 22 (2): 295–302. https://doi.org/10.1109/tap.1974.1140751
• Fu, Changhong, Adrian Carrio, Miguel A. Olivares-Mendez, and Pascual Campoy. 2014c. “Online Learning-Based Robust Visual Tracking for Autonomous Landing of Unmanned Aerial Vehicles.” In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2014.6842309
• Fu, Wenhao, Zeshuai Chen, and Jiaqi Luo. 2023. “Aerodynamic Uncertainty Quantification of a Low-Pressure Turbine Cascade by an Adaptive Gaussian Process.” Aerospace 10 (12): 1022. https://doi.org/10.3390/aerospace10121022
• Fu, Hongpo, and Yongmei Cheng. 2023. “A Novel Robust Progressive Cubature Kalman Filter with Variable Step Size for Inertial Navigationsystem/global Navigation Satellite System Tightly Coupled Navigation.” International Journal of Adaptive Control and Signal Processing 37 (4): 951–71. https://doi.org/10.1002/acs.3555
• Fu, Xin, Jingxian Wang, and Linfeng Chen. 2014b. “Application of Non-Planar Four-Mode Differential Ring Laser Gyroscope in High-Performance Dynamic Angle Measurement.” In 2014 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2014.7049474
• Fu, Fangzhou, Dayi Wang, Wenbo Li, and Fanbiao Li. 2020. “Data-Driven Fault Identifiability Analysis for Discrete-Time Dynamic Systems.” International Journal of Systems Science 51 (2): 404–12. https://doi.org/10.1080/00207721.2020.1716101
• Fu, Li, Xi Yang, and LinLin Wang. 2012. “A Novel Optimal Redundant Inertial Sensor Configuration in Strapdown Inertial Navigation System.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236887
• Fu, Li, Xi Yang, and Ling Ling Wang. 2013. “A Novel Calibration Procedure for Dynamically Tuned Gyroscope Designed by D-Optimal Approach.” Measurement 46 (9): 3173–80. https://doi.org/10.1016/j.measurement.2013.05.026
• Fu, Zhenxian, Guangying Zhang, Yurong Lin, Yang Liu, and Jiubin Tan. 2016. “Calibration and Compensation of Inertial Sensor Errors in Portable Applications — A Review.” In 2016 UKACC 11th International Conference on Control (CONTROL). IEEE. https://doi.org/10.1109/control.2016.7737580
• Fujimori, Atsushi, Munerou Kurozumi, Peter N. Nikiforuk, and Madan M. Gupta. 2000. “Flight Control Design of an Automatic Landing Flight Experiment Vehicle.” Journal of Guidance, Control, and Dynamics 23 (2): 373–76. https://doi.org/10.2514/2.4536
• Fujimoto, Yusuke, Wataru Kasai, and Toshiharu Sugie. 2018. “Informative Input Design for Bayesian Identification of LPV Systems.” SICE Journal of Control, Measurement, and System Integration 11 (3): 214–20. https://doi.org/10.9746/jcmsi.11.214
• Fujimoto, Yusuke, and Toshiharu Sugie. 2016. “Informative Input Design for Kernel-Based System Identification.” In 2016 IEEE 55th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2016.7798975
• Fujimoto, Yusuke, and Toshiharu Sugie. 2017. “Goal-Oriented Input Design for Kernel-Based System Identification.” In 2017 IEEE 56th Annual Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2017.8264157
• Fujimoto, Yusuke, and Toshiharu Sugie. 2018. “Informative Input Design for Kernel-Based System Identification.” Automatica 89: 37–43. https://doi.org/10.1016/j.automatica.2017.11.019
• Fujita, K., S. Sawai, H. Kobayashi, et al. 2006. “Precooled Turbojet Engine Flight Experiment Using Balloon-Based Operation Vehicle.” Acta Astronautica 59 (1–5): 263–70. https://doi.org/10.1016/j.actaastro.2006.02.023
• Fukushima, Yosuke. 2018. “Onboard 7DOF Motion Stage as an Inertial Platform for Payloads on Sounding Rockets.” In 2018 IEEE 15th International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2019.8371095
• Fusini, Lorenzo, Tor A. Johansen, and Thor I. Fossen. 2017. “Dead Reckoning of a Fixed-Wing UAV with Inertial Navigation Aided by Optical Flow.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991433
• Gagnon, Eric, Alexandre Vachon, and Yanick Beaudoin. 2018. “Data Fusion Architectures for Orthogonal Redundant Inertial Measurement Units.” Sensors 18 (6): 1910. https://doi.org/10.3390/s18061910
• Gai, Eliezer G., and Renwicke E. Curry. 1977. “Failure Detection by Pilots during Automatic Landing: Models and Experiments.” Journal of Aircraft 14 (2): 135–41. https://doi.org/10.2514/3.44580
• Gallo, Eduardo, and Antonio Barrientos. 2022. “Reduction of GNSS-Denied Inertial Navigation Errors for Fixed Wing Autonomous Unmanned Air Vehicles.” Aerospace Science and Technology 120: 107237. https://doi.org/10.1016/j.ast.2021.107237
• Gallo, Eduardo, and Antonio Barrientos. 2023a. “GNSS-Denied Semi-Direct Visual Navigation for Autonomous UAVs Aided by PI-Inspired Inertial Priors.” Aerospace 10 (3): 220. https://doi.org/10.3390/aerospace10030220
• Gallo, Eduardo, and Antonio Barrientos. 2023b. “Long-Distance GNSS-Denied Visual Inertial Navigation for Autonomous Fixed-Wing Unmanned Air Vehicles: SO(3) Manifold Filter Based on Virtual Vision Sensor.” Aerospace 10 (8): 708. https://doi.org/10.3390/aerospace10080708
• Gan, Shengyong, Xingbo Fang, and Xiaohui Wei. 2021. “Parametric Analysis on Landing Gear Strut Friction of Light Aircraft for Touchdown Performance.” Applied Sciences 11 (12): 5445. https://doi.org/10.3390/app11125445
• Gan, Die, and Zhixin Liu. 2023. “Distributed Sparse Identification for Stochastic Dynamic Systems under Cooperative Non-Persistent Excitation Condition.” Automatica 151: 110958. https://doi.org/10.1016/j.automatica.2023.110958
• Gando, Ryunosuke, Daiki Ono, Shiori Kaji, Hiroshi Ota, Tetsuro Itakura, and Yasushi Tomizawa. 2020. “A Compact Microcontroller-Based MEMS Rate Integrating Gyroscope Module with Automatic Asymmetry Calibration.” In 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems46641.2020.9056317
• Gang Li, Yong Xian, and Minghai Wang. 2010. “Dynamic Separation Method of Strap-down Inertial Navigation Instrument Error.” In 2010 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2010.5498374
• Gao, Jianfeng. 2023. “Drag Reduction Analysis of Transonic RAE2822 Airfoil with Two-Dimensional Optimal Bump.” In 2023 3rd International Conference on Networking Systems of AI (INSAI). IEEE. https://doi.org/10.1109/insai60116.2023.00050
• Gao, Haitao, Zhigang Chen, Mingwei Sun, Zenghui Wang, and Zengqiang Chen. 2020b. “General Periodic Cruise Guidance Optimization for Hypersonic Vehicles.” Applied Sciences 10 (8): 2898. https://doi.org/10.3390/app10082898
• Gao, Mengya, Wanchun Chen, and Wenbin Yu. 2020a. “Analytical-Solution-Based Autopilot Design for Airdrop of Cruise Missile Equiped with Parachute.” In 2020 5th International Conference on Universal Village (UV). IEEE. https://doi.org/10.1109/uv50937.2020.9426211
• Gao, Tianhua, Xiao Han, Kohji Tomita, and Akiya Kamimura. 2022. “Nonlinear Model-Assisted Control for Autonomous Parachute Precision Landing Recovery System.” In 2022 61st Annual Conference of the Society of Instrument and Control Engineers (SICE). IEEE. https://doi.org/10.23919/sice56594.2022.9905766
• Gao, Duanyang, Baiqing Hu, Lubin Chang, Fangjun Qin, and Xu Lyu. 2021a. “An Aided Navigation Method Based on Strapdown Gravity Gradiometer.” Sensors 21 (3): 829. https://doi.org/10.3390/s21030829
• Gao, Wei, Baofeng Lu, Chunyang Yu, and Haiyu Lan. 2015a. “An Improved Gyrocompass Alignment Method for Large Azimuth Misalignment.” Mathematical Problems in Engineering 2015: 1–12. https://doi.org/10.1155/2015/783640
• Gao, Yang, Zhongyu Luo, Junhong Xiang, and Shuyuan Wen. 2025. “Binocular Pose Measurement Method for Automatic Landing of Fixed-Wing Aircraft.” Measurement 256: 118088. https://doi.org/10.1016/j.measurement.2025.118088
• Gao, Duanyang, Xu Lyu, Yunhai Zhong, and Hongjin Zhou. 2024a. “An Augmented State Robust Unscented Kalman Filtering for Gravity Gradient Matching Navigation.” IEEE Sensors Journal 24 (24): 41912–23. https://doi.org/10.1109/jsen.2024.3488733
• Gao, Wei, Qi Nie, Guofu Zai, and Hui Jia. 2007. “Gyroscope Drift Estimation in Tightly-Coupled INS/GPS Navigation System.” In 2007 2nd IEEE Conference on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/iciea.2007.4318437
• Gao, Kang, Shunqing Ren, Guoxing Yi, Jiapeng Zhong, and Zhenhuan Wang. 2018b. “An Improved ACKF/KF Initial Alignment Method for Odometer-Aided Strapdown Inertial Navigation System.” Sensors 18 (11): 3896. https://doi.org/10.3390/s18113896
• Gao, Shesheng, Wenhui Wei, Yongmin Zhong, and Zhihua Feng. 2014. “Rapid Alignment Method Based on Local Observability Analysis for Strapdown Inertial Navigation System.” Acta Astronautica 94 (2): 790–98. https://doi.org/10.1016/j.actaastro.2013.10.003
• Gao, Wei, Ya Zhang, and Jianguo Wang. 2015b. “Research on Initial Alignment and Self-Calibration of Rotary Strapdown Inertial Navigation Systems.” Sensors 15 (2): 3154–71. https://doi.org/10.3390/s150203154
• Gao, Qingwei, Guorong Zhao, and Xibin Wang. 2009. “The Model and Simulation of Transfer Alignment of Carrier Based Aircraft INS with Large Azimuth Misalign Angle.” In 2009 International Joint Conference on Computational Sciences and Optimization. IEEE. https://doi.org/10.1109/cso.2009.372
• Gao, Xiangguo, Yuchen Zheng, Xiaolei Du, Zezhong Shan, Baohui Jia, and Xiang Lu. 2024c. “Effect of Clearance Position of Torque Link Structure on Nose Landing Gear Shimmy.” International Journal of Non-Linear Mechanics 159: 104616. https://doi.org/10.1016/j.ijnonlinmec.2023.104616
• Gao Feng and Ma Cen Rui. 2011. “Evaluating Model of Cruise Missile Warhead Based on LMBP Neural Network.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5777308
• Gao Fuquan, Ding Chuanhong, and Liu Jianfeng. 2010. “Initial Alignment of Strap down Inertial Navigation System Using Kalman Filter.” In 2010 International Conference on Computer Application and System Modeling (ICCASM 2010). IEEE. https://doi.org/10.1109/iccasm.2010.5620546
• Gao Xin, Bian Hong-wei, and Fan Song-wei. 2013. “Optimal Damping Algorithm Design in Inertial Navigation System.” In Proceedings 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer (MEC). IEEE. https://doi.org/10.1109/mec.2013.6885534
• Garabedian, P. R. 1976. “Computation of Wave Drag for Transonic Flow.” Journal d’Analyse Mathématique 30 (1): 164–71. https://doi.org/10.1007/bf02786712
• Garcia, Juan Alberto Herreria. 2008. “Safe Automatic Flight Back and Landing of Aircraft Flight Reconfiguration Function (FRF).” In 2008 Design, Automation and Test in Europe. IEEE. https://doi.org/10.1109/date.2008.4484898
• Gardner, C. S., H. F. Ludloff, and F. Reiche. 1948. “Drag of an Airfoil in Accelerated, Supersonic Flight.” Journal of Applied Physics 19 (12): 1179–80. https://doi.org/10.1063/1.1715040
• Garg, Priyanka, and Abhishek Kumar Dodiyal. 2009. “Reducing RF Blackout during Re-Entry of the Reusable Launch Vehicle.” In 2009 IEEE Aerospace conference. IEEE. https://doi.org/10.1109/aero.2009.4839389
• Garg, Anumit, and K. S. Nagla. 2019. “Error Estimation in Ballistic Missile Trajectory Using Kalman Filter.” In 2019 IEEE International Conference on Innovations in Communication, Computing and Instrumentation (ICCI). IEEE. https://doi.org/10.1109/icci46240.2019.9404523
• Garrec, Christophe Le, and François Kubica. 2005. “In-Flight Structural Modes Identification for Comfort Improvement by Flight Control Laws.” Journal of Aircraft 42 (1): 90–92. https://doi.org/10.2514/1.3733
• Gatt, Antoine, Sébastien Besset, Louis Jézéquel, Abdelbasset Hamdi, and Jean-Frédéric Diebold. 2017. “Reduction Methods Applied to Aircraft Brake Squeal Prediction and Simulation.” Journal of Aircraft 54 (4): 1340–49. https://doi.org/10.2514/1.c034043
• Gautam, Alvika, P. B. Sujit, and Srikanth Saripalli. 2014. “A Survey of Autonomous Landing Techniques for UAVs.” In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2014.6842377
• Ge, Jingyu, Jianhua Cheng, and Bing Qi. 2024. “A Non-Rigid Terrain Transformation Particle Filter Suitable for Terrain-Aided Navigation without Sound Velocity Profile.” Ocean Engineering 294: 116858. https://doi.org/10.1016/j.oceaneng.2024.116858
• Ge, Howard H., John Y. Liu, and Bryan Buchanan. 2015. “Bias Self-Calibration Techniques Using Silicon Disc Resonator Gyroscope.” In 2015 IEEE International Symposium on Inertial Sensors and Systems (ISISS) Proceedings. IEEE. https://doi.org/10.1109/isiss.2015.7102375
• Geiss, G. 1969. “The Effect of Star Tracker Model Choice on Satellite Attitude Stability Analysis.” IEEE Transactions on Automatic Control 14 (6): 624–32. https://doi.org/10.1109/tac.1969.1099294
• Geller, Edward S. 1968. “Inertial System Platform Rotation.” IEEE Transactions on Aerospace and Electronic Systems AES-4 (4): 557–68. https://doi.org/10.1109/taes.1968.5409024
• Geneva, Patrick, Kevin Eckenhoff, Woosik Lee, Yulin Yang, and Guoquan Huang. 2020. “OpenVINS: A Research Platform for Visual-Inertial Estimation.” In 2020 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra40945.2020.9196524
• Geng, Hong, and Yuankai Li. 2023. “A Novel Data-Driven Approach to Parameter Identification for Flight Simulation.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10239932
• Georg, Jean-Michael, Johannes Feiler, Simon Hoffmann, and Frank Diermeyer. 2020. “Sensor and Actuator Latency during Teleoperation of Automated Vehicles.” In 2020 IEEE Intelligent Vehicles Symposium (IV). IEEE. https://doi.org/10.1109/iv47402.2020.9304802
• George, Michael, and Salah Sukkarieh. 2007. “Camera Aided Inertial Navigation in Poor GPS Environments.” In 2007 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2007.352849
• Gerencser, L., and H. Hjalmarsson. n.d. “Adaptive Input Design in System Identification.” In Proceedings of the 44th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2005.1582952
• Ghanizadegan, Khashayar, and Hashim A. Hashim. 2025a. “DeepUKF-VIN: Adaptively-Tuned Deep Unscented Kalman Filter for 3D Visual-Inertial Navigation Based on IMU-Vision-Net.” Expert Systems with Applications 271: 126656. https://doi.org/10.1016/j.eswa.2025.126656
• Ghanizadegan, Khashayar, and Hashim A. Hashim. 2025b. “Quaternion-Based Unscented Kalman Filter for 6-DoF Vision-Based Inertial Navigation in GPS-Denied Regions.” IEEE Transactions on Instrumentation and Measurement 74: 1–13. https://doi.org/10.1109/tim.2024.3509582
• Gheorghe, Marius, and John Neal. 2026. “Enhanced Architecture for Skew-Redundant Inertial Systems Using Triaxial Sensors.” In 2026 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial69196.2026.11557719
• Ghose, D., B. Dam, and U. R. Prasad. n.d. “A Spreader Acceleration Guidance Scheme for Command Guided Surface-to-Air Missiles.” In Proceedings of the IEEE National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1989.40214
• Ghosh, A. K., and S. C. Raisinghani. 2002. “Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks.” Journal of Aircraft 39 (5): 892–94. https://doi.org/10.2514/2.3012
• Gibart, Jules, Helene Piet-Lahanier, and Francois Farago. 2024. “Mass Flow Control Design for a Reusable Liquid Propelled Rocket Engine Using Contraction Theory.” In 2024 American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc60939.2024.10644942
• Gigleux, Benjamin, François Vincent, and Eric Chaumette. 2024. “Covariance Estimation of Generalized Monopulse for Radar Tracking.” In 2024 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar58436.2024.10994171
• Gilmore, J. P., L. Freier, E. Nolan, M. Perlmutter, M. Bowser, and J. Maglieri. 2000. “Three-Axis Nested Fiber Optic Gyroscope.” In IEEE 2000. Position Location and Navigation Symposium (Cat. No.00CH37062). IEEE. https://doi.org/10.1109/plans.2000.838333
• Gilmore, Jerold P., and Richard A. McKern. 1972. “A Redundant Strapdown Inertial Reference Unit (SIRU).” Journal of Spacecraft and Rockets 9 (1): 39–47. https://doi.org/10.2514/3.61628
• Gilster, G. 1994. “High Accuracy Performance Capabilities of the Military Standard Ring Laser Gyro Inertial Navigation Unit.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303351
• Giner, J., and K. Ono. 2018. “Adaptive Feedthrough Cancellation in MEMS Gyroscopes in Reconfigurable IC+FPGA Platform.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358157
• Givens, Matthew W., and Calvin Coopmans. 2020. “Exploring the Use of Reverse Thrust in a Dynamic UAS Landing Maneuver Using Kinodynamic RRT.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9213855
• Glaros, L. N. n.d. “Aided-Inertial Navigation and Alignment Performance of a Supersonic Target Missile.” In IEEE PLANS 92 Position Location and Navigation Symposium Record. IEEE. https://doi.org/10.1109/plans.1992.185845
• Godfrey, K. R., and J. J. DiStefano. 1985. “Identifiability of Model Parameter.” IFAC Proceedings Volumes 18 (5): 89–114. https://doi.org/10.1016/s1474-6670(17)60544-5
• Goktas, Polat, Satilmis Topcu, Ezhan Karasan, and Ayhan Altintas. 2016. “Short-Term Propagation Measurements and Modeling for Terrestrial Line-of-Sight Links.” In 2016 10th European Conference on Antennas and Propagation (EuCAP). IEEE. https://doi.org/10.1109/eucap.2016.7481271
• Goldenberg, F. 2006. “Geomagnetic Navigation beyond the Magnetic Compass.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650662
• Goldys, B., and B. Maslowski. 2002. “Parameter Estimation for Controlled Semilinear Stochastic Systems: Identifiability and Consistency.” Journal of Multivariate Analysis 80 (2): 322–43. https://doi.org/10.1006/jmva.2001.1989
• Golovan, A. A., E. V. Gorushkina, and I. A. Papusha. 2018. “On the Method of Instrumental Errors Parameterization for a Gravity Gradiometer.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405851
• Golovan, Andrey, Alexander Kozlov, and Ilya Tarygin. 2017. “Calibration of a 3-Axis Hemispherical Resonator Gyro Assembly.” In 2017 8th International Conference on Recent Advances in Space Technologies (RAST). IEEE. https://doi.org/10.1109/rast.2017.8002979
• Gomaa, Mahmoud A. K., Oscar De Silva, Awantha Jayasiri, and George K. I. Mann. 2022. “Disturbance Observer and Depth Enhanced Visual-Inertial Navigation System for Multi-Rotor MAVs: An Observability Analysis.” In 2022 IEEE 61st Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc51059.2022.9992446
• Gomez, Aitor Ramirez, and Anders la Cour-Harbo. 2021. “Emergency Landing Decision Method for Unmanned Aircraft.” In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas51884.2021.9476792
• Gonçalves, Tiago, José Azinheira, and Patrick Rives. 2010. “Homography-Based Visual Servoing of an Aircraft for Automatic Approach and Landing.” In 2010 IEEE International Conference on Robotics and Automation. IEEE. https://doi.org/10.1109/robot.2010.5509496
• Goncalves, A. C. V., M. F. D. Pinto, and P. C. Pellanda. 2018. “In-Motion Alignment Algorithm of Strapdown Inertial Navigation Systems.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577186
• Goncharenko, V. I. 2011. “Canonical Description of the Control System in the Shimmy Problem for the Landing Gear Wheels of an Aircraft.” International Applied Mechanics 47 (2): 215–24. https://doi.org/10.1007/s10778-011-0455-0
• Gong, Zheng, Zian Wang, Chengchuan Yang, Zhengxue Li, Mingzhe Dai, and Chengxi Zhang. 2022. “Performance Analysis on the Small-Scale Reusable Launch Vehicle.” Symmetry 14 (9): 1862. https://doi.org/10.3390/sym14091862
• Gopaul, Nilesh S., Jianguo Wang, and Baoxin Hu. 2017. “Loosely Coupled Visual Odometry Aided Inertial Navigation System Using Discrete Extended Kalman Filter with Pairwise Time Correlated Measurements.” In 2017 Forum on Cooperative Positioning and Service (CPGPS）. IEEE. https://doi.org/10.1109/cpgps.2017.8075140
• Gopmandal, Falguni, and Arun Ghosh. 2019. “LQ Optimal Multivariable PID Control Design for Skid-to-Turn Missile Autopilot.” In 2019 Fifth Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/indiancc.2019.8715634
• Gordon, James T. 2002. “Perturbation Analysis of Nonlinear Wheel Shimmy.” Journal of Aircraft 39 (2): 305–17. https://doi.org/10.2514/2.2928
• Gordon, James T., Steven Y. Liu, and M. Akif Ozbek. 1998. “Nonlinear Model for Aircraft Brake Squeal Analysis: Stability Analysis and Parametric Studies.” Journal of Aircraft 35 (4): 631–36. https://doi.org/10.2514/2.2347
• Gorstein, M., J. N. Hallock, and J. Valge. 1970. “Two Approaches to the Star Mapping Problem for Space Vehicle Attitude Determination.” Applied Optics 9 (2): 351. https://doi.org/10.1364/ao.9.000351
• Goshen-Meskin, D., and I. Y. Bar-Itzhack. 1990. “Observability Analysis of Piece-Wise Constant Systems with Application to Inertial Navigation.” In 29th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1990.203702
• Goshen-Meskin, D., and I. Y. Bar-Itzhack. 1992a. “Observability Analysis of Piece-Wise Constant Systems. II. Application to Inertial Navigation in-Flight Alignment (Military Applications).” IEEE Transactions on Aerospace and Electronic Systems 28 (4): 1068–75. https://doi.org/10.1109/7.165368
• Goshen-Meskin, Drora, and Itzhack Y. Bar-Itzhack. 1992b. “Unified Approach to Inertial Navigation System Error Modeling.” Journal of Guidance, Control, and Dynamics 15 (3): 648–53. https://doi.org/10.2514/3.20887
• Goto, Yuichiro, Shigeru Obayashi, and Yasuaki Kohama. 2007. “Wave Drag Characteristics of a Low-Drag Supersonic Formation Flying Concept.” Journal of Aircraft 44 (2): 675–79. https://doi.org/10.2514/1.23236
• Gottu Mukkula, Anwesh Reddy, and Radoslav Paulen. 2017. “Model-Based Optimal Experiment Design for Nonlinear Parameter Estimation Using Exact Confidence Regions.” IFAC-PapersOnLine 50 (1): 13760–65. https://doi.org/10.1016/j.ifacol.2017.08.2567
• Gottu Mukkula, Anwesh Reddy, and Radoslav Paulen. 2019. “Optimal Experiment Design in Nonlinear Parameter Estimation with Exact Confidence Regions.” Journal of Process Control 83: 187–95. https://doi.org/10.1016/j.jprocont.2019.01.004
• Gou, Wanxiang, Yinhu Zhan, Chonghui Li, et al. 2025b. “Star Extraction by Star Sensors for Daytime Images Affected by Atmospheric Turbulence.” Chinese Journal of Aeronautics 38 (8): 103571. https://doi.org/10.1016/j.cja.2025.103571
• Gouskov, Yu. P. 1972. “Automatic Landing as a Terminal Control Problem.” IFAC Proceedings Volumes 5 (1): 131–36. https://doi.org/10.1016/s1474-6670(17)68461-1
• Govindarajulu, Z. 1986. “A Note on Circular Error Probabilities.” Naval Research Logistics Quarterly 33 (3): 423–29. https://doi.org/10.1002/nav.3800330308
• Grammatikos, Anthony, Alfred R. Schuler, and Kenneth A. Fegley. 1967. “Damping Gimballess Inertial Navigation Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-3 (3): 481–93. https://doi.org/10.1109/taes.1967.5408813
• Graves, Ernald B., and Warner Robins. 1980. “Supersonic Aerodynamic Trade Data for a Monoplanar Missile Concept.” Journal of Aircraft 17 (2): 95–98. https://doi.org/10.2514/3.57879
• Green, David. 1992. “Inventing Accuracy a Historical Sociology of Nuclear Missile Guidance.” Space Policy 8 (3): 281. https://doi.org/10.1016/0265-9646(92)90057-3
• Grewal, M. S., R. S. Miyasako, and J. M. Smith. n.d. “Application of Fixed Point Smoothing to the Calibration, Alignment and Navigation Data of Inertial Navigation Systems.” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195521
• Grigorie, Teodor Lucian. 2008. “Some Considerations Concerning the Influence of the Inertial Sensors Errors on the Solution of Navigation for a Bidimensional Strap-down Inertial Navigation System.” In 2008 5th Workshop on Positioning, Navigation and Communication. IEEE. https://doi.org/10.1109/wpnc.2008.4510369
• Grigorie, Teodor Lucian, and Ruxandra Mihaela Botez. 2014. “Poster Abstract: Precision Improvement of Aircrafts Attitude Estimation through Gyro Sensors Data Fusion in a Redundant Inertial Measurement Unit.” In IPSN-14 Proceedings of the 13th International Symposium on Information Processing in Sensor Networks. IEEE. https://doi.org/10.1109/ipsn.2014.6846773
• Grine, Alejandro, Courtney L. H. Sovinec, Darwin Serkland, et al. 2026. “Heterogeneously Integrated MEMS Gyroscope with Fabry Perot Optical Readout.” In 2026 International Conference on Optical MEMS and Nanophotonics (OMN). IEEE. https://doi.org/10.1109/omn70392.2026.11646696
• Gringard, M., and A. Kroll. 2018. “Optimal Experiment Design for Identifying Dynamical Takagi-Sugeno Models with Minimal Parameter Uncertainty.” IFAC-PapersOnLine 51 (15): 353–58. https://doi.org/10.1016/j.ifacol.2018.09.163
• Gross, Jason N., Yu Gu, Matthew B. Rhudy, Srikanth Gururajan, and Marcello R. Napolitano. 2012. “Flight-Test Evaluation of Sensor Fusion Algorithms for Attitude Estimation.” IEEE Transactions on Aerospace and Electronic Systems 48 (3): 2128–39. https://doi.org/10.1109/taes.2012.6237583
• Grossir, Guillaume, Daniela Puorto, Zdeněk Ilich, et al. 2020. “Aerodynamic Characterization of Space Debris in the VKI Longshot Hypersonic Tunnel Using a Free-Flight Measurement Technique.” Experiments in Fluids 61 (7): 163. https://doi.org/10.1007/s00348-020-02995-7
• Gryte, Kristoffer, Torleiv H. Bryne, Sigurd M. Albrektsen, and Tor A. Johansen. 2019. “Field Test Results of GNSS-Denied Inertial Navigation Aided by Phased-Array Radio Systems for UAVs.” In 2019 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2019.8798057
• Gu, Zijie, Xukai Ding, Liye Zhao, and Hongsheng Li. 2025. “Modeling and Compensation of Readout, Actuation, and Damping Errors for Whole-Angle Hemispherical Resonator Gyroscope.” IEEE Sensors Journal 25 (6): 9421–31. https://doi.org/10.1109/jsen.2025.3529863
• Gu, H. Y., X. X. Liu, B. L. Zhao, and H. Zhou. 2018. “A Compensation Method for Long-Term Zero Bias Drift of MEMS Gyroscope Based on Improved CEEMD and ELM.” In 2018 IEEE 8th International Nanoelectronics Conferences (INEC). IEEE. https://doi.org/10.1109/inec.2018.8441932
• Gu, Haoyu, Xianxue Liu, Baolin Zhao, and Hao Zhou. 2019a. “The in-Operation Drift Compensation of MEMS Gyroscope Based on Bagging-ELM and Improved CEEMDAN.” IEEE Sensors Journal 19 (13): 5070–77. https://doi.org/10.1109/jsen.2019.2902912
• Gu, Nianzu, Fei Xing, and Zheng You. 2021a. “GNSS Spoofing Detection Based on Coupled Visual/Inertial/GNSS Navigation System.” Sensors 21 (20): 6769. https://doi.org/10.3390/s21206769
• Gu, Hong, Dan Yang, and WenBin Wang. 2021b. “Phase Bias in Dual-Axis Optical Gyroscope Based on a Double-Ring Structure.” In 2021 19th International Conference on Optical Communications and Networks (ICOCN). IEEE. https://doi.org/10.1109/icocn53177.2021.9563747
• Gu, Liutao, Weiping Zhang, Jun Feng, and Zhihan Zhang. 2022. “Development of a Novel Gear-like Disk Resonator Applied in Gyroscope.” Applied Sciences 12 (14): 7342. https://doi.org/10.3390/app12147342
• Gu, Haoyu, Baolin Zhao, Hao Zhou, Xianxue Liu, and Wei Su. 2019b. “MEMS Gyroscope Bias Drift Self-Calibration Based on Noise-Suppressed Mode Reversal.” Micromachines 10 (12): 823. https://doi.org/10.3390/mi10120823
• Guadagnini, Jacopo, Gabriele De Zaiacomo, and Michèle Lavagna. 2023. “Mission Performance Assessment of the Recovery and Vertical Landing of a Reusable Launch Vehicle.” Aerospace 11 (1): 35. https://doi.org/10.3390/aerospace11010035
• Guan, Yue, Shanshan Feng, Haibo Huang, and Liguo Chen. 2017a. “A Method for Improving Target Tracking Accuracy of Vehicle Radar.” In Computer Vision Systems. Springer International Publishing. https://doi.org/10.1007/978-3-319-68345-4_10
• Guan, Yadong, Xiaogang Li, Min Wang, and Jianhua Ye. 2017b. “Reliability Assessment of the Missile System Based on Bayesian Network.” In 2017 Second International Conference on Reliability Systems Engineering (ICRSE). IEEE. https://doi.org/10.1109/icrse.2017.8030741
• Guan, Zhiyuan, Yunpeng Ma, Zewei Zheng, and Na Guo. 2018b. “Prescribed Performance Control for Automatic Carrier Landing with Disturbance.” Nonlinear Dynamics 94 (2): 1335–49. https://doi.org/10.1007/s11071-018-4427-3
• Guan, Y. X., L. X. Wang, Q. Wang, and W. W. Qin. 2018a. “Analysis of Influential Factors of Inertial Navigation Platform Powering on Continuously.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019032
• Guerrier, Stephane, Roberto Molinari, and James Balamuta. 2016a. “Discussion on Maximum Likelihood-Based Methods for Inertial Sensor Calibration.” IEEE Sensors Journal 16 (14): 5522–23. https://doi.org/10.1109/jsen.2016.2565389
• Guerrier, Stephane, Roberto Molinari, and Yannick Stebler. 2016b. “Wavelet-Based Improvements for Inertial Sensor Error Modeling.” IEEE Transactions on Instrumentation and Measurement 65 (12): 2693–2700. https://doi.org/10.1109/tim.2016.2599437
• Guesmi, Besma, and David Moloney. 2024. “Hardware-Aware, Deep-Learning Approaches for Image Denoising and Star Detection for Star Tracker Sensor.” In 2024 10th International Conference on Control, Decision and Information Technologies (CoDIT), vol. 7. IEEE. https://doi.org/10.1109/codit62066.2024.10708467
• Gully, Sol. 1976. “Inertial Platform Synthesis Employing Observers to Accommodate Disturbances and Coupling.” In 1976 IEEE Conference on Decision and Control including the 15th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1976.267705
• Gundavarapu, Sarat, Tin Komljenovic, Minh A. Tran, Michael Belt, John E. Bowers, and Daniel J. Blumenthal. 2017. “Effect of Direct PRBS Modulation on Laser Driven Fiber Optic Gyroscope.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935669
• Gunderson, R. W. 1978. “Application of Fuzzy Isodata Algorithms to Star Tracker Pointing Systems.” IFAC Proceedings Volumes 11 (1): 1319–23. https://doi.org/10.1016/s1474-6670(17)66090-7
• Guner, Ufuk, and Janset Dasdemir. 2021. “Design and Implementation of Fault Tolerant Inertial Measurement Unit.” In 2021 8th International Conference on Electrical and Electronics Engineering (ICEEE). IEEE. https://doi.org/10.1109/iceee52452.2021.9415968
• Gunhan, Yesim, and Derya Unsal. 2014. “Polynomial Degree Determination for Temperature Dependent Error Compensation of Inertial Sensors.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851494
• Guo, Lei, Songyin Cao, Chuntang Qi, and Xiaoying Gao. 2012a. “Initial Alignment for Nonlinear Inertial Navigation Systems with Multiple Disturbances Based on Enhanced Anti-Disturbance Filtering.” International Journal of Control 85 (5): 491–501. https://doi.org/10.1080/00207179.2012.658523
• Guo, Zhanshe, Peng Fu, Defeng Liu, and Manguo Huang. 2017a. “Design and FEM Simulation for a Novel Resonant Silicon MEMS Gyroscope with Temperature Compensation Function.” Microsystem Technologies 24 (3): 1453–59. https://doi.org/10.1007/s00542-017-3524-4
• Guo, Hui, and Huajie Hong. 2019. “Research on Filtering Algorithm of MEMS Gyroscope Based on Information Fusion.” Sensors 19 (16): 3552. https://doi.org/10.3390/s19163552
• Guo, Dong, Zixuan Liang, Qingdong Li, and Zhang Ren. 2018a. “Analytical Geometry-Based Terminal Attack Area Calculation Method for Intercepting Hypersonic Cruise Target.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018874
• Guo, Lianyu, Shiqian Liu, Weizhi Lyu, Qian Zhang, and Yunxin Meng. 2026d. “L1 Adaptive Nonlinear Dynamic Inversion Based Automatic Landing Control of Civil Aircraft.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00489-8
• Guo, Qingyuan, Gang Liu, Biao Xiang, Tong Wen, and Hu Liu. 2016. “Robust Control of Magnetically Suspended Gimbals in Inertial Stabilized Platform with Wide Load Range.” Mechatronics 39: 127–35. https://doi.org/10.1016/j.mechatronics.2016.08.003
• Guo, Tongqing, Ennan Shen, Zhiliang Lu, Di Zhou, and Jiangpeng Wu. 2019. “Thermal Flutter Prediction at Trajectory Points of a Hypersonic Vehicle Based on Aerothermal Synchronization Algorithm.” Aerospace Science and Technology 94: 105381. https://doi.org/10.1016/j.ast.2019.105381
• Guo, Lijun, Bangren Shi, Chen Chen, and Meng Zhao. 2012b. “A Large-Size SiO2 Waveguide Resonator Used in Integration Optical Gyroscope.” Optik 123 (4): 302–5. https://doi.org/10.1016/j.ijleo.2011.02.030
• Guo, Zhibin, Yuegang Wang, Bin Shan, and Wuxing Huang. 2014. “Robust Initial Alignment Algorithm for Platform Inertial Navigation System on Disturbance Base.” In 2014 IEEE Workshop on Advanced Research and Technology in Industry Applications (WARTIA). IEEE. https://doi.org/10.1109/wartia.2014.6976425
• Guo, Weilin, Yong Xian, Yan Chang, Bing Li, and Leliang Ren. 2018b. “An on-Line Correction Method of Initial Alignment Error of SINS for Ballistic Missile.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018720
• Guo, Shiluo, JIangning Xu, and Zhang Cheng. 2017b. “Inertial Navigation System Alignment Based on Fading Kalman Filter and Fixed Point Smoother.” In 2017 10th International Symposium on Computational Intelligence and Design (ISCID). IEEE. https://doi.org/10.1109/iscid.2017.192
• Guo, Jin, Peng Yu, Yang Li, Yong Song, and Fengwei Jing. 2024b. “Optimal Period Input Design in FIR System Identification with Binary-Valued Observations and Event-Triggered Communication.” IEEE Transactions on Circuits and Systems II: Express Briefs 71 (1): 166–70. https://doi.org/10.1109/tcsii.2022.3223967
• Guo, Ruocheng, Hong Yuan, Xiao Chen, and Wen Li. 2026b. “APF-Driven Lightweight UAV Swarm Trajectory Optimization in GNSS-Denied Air–Terrestrial Navigation.” Electronics 15 (6): 1207. https://doi.org/10.3390/electronics15061207
• Guo, Qiang, Jianfei Zhou, Xuguang Yue, Jun Cheng, Chen Huang, and Changhong Chen. 2026a. “Adaptive Dual-Bias Estimation for Hybrid Inertial Navigation with Single-Axis Cold Atom Interferometric Gyroscope.” Sensors 26 (20): 6379. https://doi.org/10.3390/s26206379
• Guo Yi, Xavier Fito, and Carles Ferrer. 2007. “A Novel Real-Time System Platform Development Applied to an Integrated Inertial Navigation System.” In 2007 Mediterranean Conference on Control & Automation. IEEE. https://doi.org/10.1109/med.2007.4433939
• Guodong Ning, Shuguang Zhang, and Zhenping Fang. 2006. “Entry Control Allocation for Reusable Launch Vehicle.” In 2006 1st International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2006.1627416
• Guorong Zhao, Jixin Li, and Muqing Chen. 2006. “Design of Automatic Carrier Landing Control System Using Block Diagonal Controller.” In 2006 6th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2006.1712768
• Guotong Sun and Shuo Tang. 2010. “Warfighting Simulation System for System Effectiveness Analysis of Hypersonic Cruise Missile.” In 2010 International Conference on Educational and Network Technology. IEEE. https://doi.org/10.1109/icent.2010.5532272
• Gupta, K. K., S. B. Choi, and H. Ibrahim. 2016. “Development-Fluid-Dynamics-Based Aerothermoelastic Simulation Capability with Application to Flight Vehicles.” Journal of Aircraft 53 (2): 360–68. https://doi.org/10.2514/1.c033346
• Gupta, K. K., S. B. Choi, S. F. Lung, and A. Ibrahim. 2017. “Aerothermoelastic-Acoustics Simulation of Flight Vehicles.” AIAA Journal 55 (1): 49–56. https://doi.org/10.2514/1.j055088
• Gupta, Aditya, Prasenjit Sengupta, Richard Phernetton, and Andrew Sosanya. 2024. “Lower Bounds on Magnetic Navigation Performance as a Function of Magnetic Anomaly Map Quality.” In 2024 AIAA DATC/IEEE 43rd Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc62030.2024.10749342
• Gurung, Lokesh, Theo Miani, Guillermo Sobreviela-Falces, Douglas Young, Colin Baker, and Ashwin Seshia. 2023. “A High-Performance Resonant MEMS Accelerometer with a Residual Bias Error of 30 μg and Scale Factor Repeatability of 2 Ppm.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10103976
• Györfi, B., and J. F. Wagner. 2025. “A Novel IMU-Array Designed for MEMS-Gyrocompassing.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279361
• Ha, Cheolkeun. 2010. “Gain-Scheduled Directional Guidance Controller Design Using a Genetic Algorithm for Automatic Precision Landing.” International Journal of Control, Automation and Systems 8 (1): 107–17. https://doi.org/10.1007/s12555-010-0114-y
• Ha, ChangSu, and Dongjun Lee. 2013. “Vision-Based Teleoperation of Unmanned Aerial and Ground Vehicles.” In 2013 IEEE International Conference on Robotics and Automation. IEEE. https://doi.org/10.1109/icra.2013.6630764
• Habibi, Soheil, Stuart J. Cooper, Jean-Michel Stauffer, and Bertrand Dutoit. 2008. “Gun Hard Inertial Measurement Unit Based on MEMS Capacitive Accelerometer and Rate Sensor.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4569974
• Hagen, Ove. 2006. “TerrLab ¿ a Generic Simulation and Post-Processing Tool for Terrain Referenced Navigation.” In OCEANS 2006. IEEE. https://doi.org/10.1109/oceans.2006.306834
• Hager, Antonia, Torleiv H. Bryne, Nils Olsen, Jasper Simon Krauser, and Tor A. Johansen. 2025. “Magnetic Anomaly Navigation with a Lie-Group Error-State Kalman Filter.” In 2025 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc65951.2025.11187153
• Hager, Antonia, Sven Nebendahl, Alexej Klushyn, Jasper Krauser, Torleiv H. Bryne, and Tor Arne Johansen. 2026. “Airborne Magnetic Anomaly Navigation with Neural-Network-Augmented Online Calibration.” Journal of Guidance, Control, and Dynamics 49 (10): 2951–64. https://doi.org/10.2514/1.g009918
• Hägg, Per, and Bo Wahlberg. 2015. “On Optimal Input Design for Networked Systems.” Automatica 53: 275–81. https://doi.org/10.1016/j.automatica.2014.12.012
• Hagiwara, Y. 1972. “Truncation Error Formulas for the Geoidal Height and the Deflection of the Vertical.” Bulletin géodésique 106 (1): 453–66. https://doi.org/10.1007/bf02522052
• Haider, Syed. 2020. “Applying Model Based Safety Assessment for Aircraft Landing Gear System Certification.” In 2020 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams48030.2020.9153705
• Hailiang, Wen. 2026. “Predefined-Time Direct-Lift Control for Automatic Carrier Landing with Moving-Deck Prediction.” In 2026 International Russian Automation Conference (RusAutoCon). IEEE. https://doi.org/10.1109/rusautocon69876.2026.11707456
• Hailong, Zhu, Bin Liang, Tao Zhang, and Hua Junpeng. 2015. “Designing Considerations for Airborne Star Tracker during Daytime.” In The 27th Chinese Control and Decision Conference (2015 CCDC). IEEE. https://doi.org/10.1109/ccdc.2015.7162682
• Haipeng, Zhang, Fang Jiancheng, and Xun Xiangdong. 2007. “Real Time Compensation of Quartz MEMS Gyroscope Drift Periodic Error.” In 2007 8th International Conference on Electronic Measurement and Instruments. IEEE. https://doi.org/10.1109/icemi.2007.4350470
• Haipeng, Liu, Gao Shiqiao, Liang Xinjian, and Jin Lei. 2009. “Performance Analysis and Measurement of Micro-Machined Gyroscope.” In 2009 9th International Conference on Electronic Measurement & Instruments. IEEE. https://doi.org/10.1109/icemi.2009.5274868
• Hall, Charlie. 2019. “‘The Other End of a Trajectory’: Operation Backfire and the German Origins of Britain’s Ballistic Missile Programme.” International History Review 42 (6): 1118–36. https://doi.org/10.1080/07075332.2019.1690026
• Hall, John J., and Robert L. Williams. 2000. “Case Study: Inertial Measurement Unit Calibration Platform.” Journal of Robotic Systems 17 (11): 623–32. https://doi.org/10.1002/1097-4563(200011)17:11<623::aid-rob4>3.0.co;2-7
• Ham, Byoung S. 2022b. “A Quantum Ring Laser Gyroscope Based on Coherence De Broglie Waves.” Sensors 22 (22): 8687. https://doi.org/10.3390/s22228687
• Hameed, Aysha S., and G. R. Bindu. 2019. “A Novel Flare Maneuver Guidance for Approach and Landing Phase of a Reusable Launch Vehicle.” In 2019 Advances in Science and Engineering Technology International Conferences (ASET). IEEE. https://doi.org/10.1109/icaset.2019.8714376
• Hameed, Aysha S., and G. R. Bindu. 2021. “Single Segment Approach and Landing Guidance and Control for an Unpowered Reusable Launch Vehicle.” Aerospace Science and Technology 115: 106777. https://doi.org/10.1016/j.ast.2021.106777
• Hameed, Aysha S., and G. R. Bindu. 2022. “Gain Scheduled Finite Horizon LQR for Approach and Landing Phase of a Reusable Launch Vehicle.” Journal of The Institution of Engineers (India): Series C 103 (3): 381–88. https://doi.org/10.1007/s40032-021-00789-2
• Hamelin, Benoit, Vahid Tavassoli, and Farrokh Ayazi. 2013. “Eutectic Trimming of Polysilicon Micro Hemispherical Resonating Gyroscope.” In 2013 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2013.6688464
• Hammon, Robert L. 1962. “Effects on Inertial Guidance Systems of Random Error Sources.” IRE Transactions on Aeronautical and Navigational Electronics ANE-9 (4): 215–30. https://doi.org/10.1109/tane3.1962.4201892
• Han, Run-Fan, Gui-Ming Chen, Tian-Jun Liao, Xiao-Dong Ling, and Lei-Lei Chang. 2017. “Hidden Failure Prognosis for Navigation Inertial Platform Using Belief Rule Base Expert System.” In 2017 9th International Conference on Modelling, Identification and Control (ICMIC). IEEE. https://doi.org/10.1109/icmic.2017.8321644
• Han, Yang, Hongwu Guo, and Yuhai Chong. 2014b. “Integrated Guidance and Control with Terminal Angle Constraint.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007347
• Han, Chenglong, Zhuoyao He, Botao Duan, Hansong Xu, and Jun Wu. 2026e. “Vision-Based Aircraft Localization during the End Stage of Landing Approach via Runway Mark Determination.” International Journal of Aerospace Engineering 2026 (1): 1555047. https://doi.org/10.1155/ijae/1555047
• Han, Chulhee, Byung-Hyuk Kang, Seung-Bok Choi, Jun Mo Tak, and Jai-Hyuk Hwang. 2019. “Control of Landing Efficiency of an Aircraft Landing Gear System with Magnetorheological Dampers.” Journal of Aircraft 56 (5): 1980–86. https://doi.org/10.2514/1.c035298
• Han, Yongsu, and Youdan Kim. 2011. “Optimal Input Design for Online Parameter Estimation for Aircraft with Multiple Control Surfaces.” Engineering Optimization 43 (5): 559–80. https://doi.org/10.1080/0305215x.2010.502937
• Han, Shipeng, Zhen Meng, Olatunji Omisore, Toluwanimi Akinyemi, and Yuepeng Yan. 2020. “Random Error Reduction Algorithms for MEMS Inertial Sensor Accuracy Improvement—a Review.” Micromachines 11 (11): 1021. https://doi.org/10.3390/mi11111021
• Han, Yu, Fangjun Qin, Kailong Li, Yun Xiao, and Tiangao Zhu. 2026d. “A Topography-Constrained Marine Gravity Field Modeling Method for Gravity Matching-Aided Navigation.” IEEE Sensors Journal 26 (12): 19121–33. https://doi.org/10.1109/jsen.2026.3691309
• Han, Yongqiang, Michael G. Safonov, and Jiabin Chen. 2014a. “An in-Motion Alignment Method for Inertial Navigation System Based on Unfalsified Adaptive Control Theory.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007471
• Han, Kyung Jun, Chang-Ky Sung, ByungSu Park, Taeyun Kim, and Chan Gook Park. 2026b. “An IMM Extension of RBPMF for Terrain-Referenced Navigation under Radar Return Ambiguity.” Sensors 26 (19): 6024. https://doi.org/10.3390/s26196024
• Han, Yurong, Bo Wang, Zhihong Deng, and Mengyin Fu. 2018a. “A Combined Matching Algorithm for Underwater Gravity-Aided Navigation.” IEEE/ASME Transactions on Mechatronics 23 (1): 233–41. https://doi.org/10.1109/tmech.2017.2774296
• Han, Yurong, Bo Wang, Zhihong Deng, and Mengyin Fu. 2018b. “A Matching Algorithm Based on the Nonlinear Filter and Similarity Transformation for Gravity-Aided Underwater Navigation.” IEEE/ASME Transactions on Mechatronics 23 (2): 646–54. https://doi.org/10.1109/tmech.2018.2806350
• Han, Xiao, Bo Wang, Lei Liu, and Huijin Fan. 2024. “Adaptive-Critic-Design Based Tracking Controller for Boost Complement Glide Vehicle with Performance Constraint and Input Saturation.” Aerospace Science and Technology 145: 108839. https://doi.org/10.1016/j.ast.2023.108839
• Han, Zengyu, Gong Xu, and Yongwen Shan. 2026c. “Moving-Window Weighted Least Squares with Edge Optimization for Schuler Oscillation Suppression in Inertial Navigation Systems.” Sensors 26 (20): 6481. https://doi.org/10.3390/s26206481
• Han, Songlai, Mingcun Zhao, Kai Wang, Jing Dong, and Ang Su. 2023. “Cross-Modal Images Matching Based Enhancement to MEMS INS for UAV Navigation in GNSS Denied Environments.” Applied Sciences 13 (14): 8238. https://doi.org/10.3390/app13148238
• Hanisch, Bernard. 1967. “Inertial Platform Stabilization Criteria for Arbitrary Vehicle Maneuvers.” Journal of Aircraft 4 (6): 534–36. https://doi.org/10.2514/3.43883
• Hansen, J., R. Rajkumar, J. Lehoczky, and S. Ghosh. 2006. “Resource Management for Radar Tracking.” In 2006 IEEE Conference on Radar. IEEE. https://doi.org/10.1109/radar.2006.1631788
• Hanson, M., K. Tibbetts, R. Wohlers, and J. D. Hart. 2000. “Missile Impact Location Prediction Using Noisy Range Data.” In 2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484), vol. 3. IEEE. https://doi.org/10.1109/aero.2000.879861
• Hao, Yan-ling, Ming-hui Chen, Liang-jun Li, and Bo Xu. 2008. “Comparison of Robust H∞ Filter and Kalman Filter for Initial Alignment of Inertial Navigation System.” Journal of Marine Science and Application 7 (2): 116–21. https://doi.org/10.1007/s11804-008-7041-9
• Hao, Wang, and Weifeng Tian. 2005. “Modeling the Random Drift of Micro-Machined Gyroscope with Neural Network.” Neural Processing Letters 22 (3): 235–47. https://doi.org/10.1007/s11063-005-6800-8
• Hao, Liu, and Liang Yongqi. 2024. “Tracking Hypersonic Glide Vehicle Based on the MaRV Model with Multiple-Model Approach.” In 2024 43rd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc63176.2024.10662106
• Hao, Rui, Huijun Yu, Bei Peng, Haixiang Zhan, and Wu Zhou. 2020b. “Impacts of Residual Stress on Micro Vibratory Platform Used for Inertial Sensor Calibration.” Sensors 20 (14): 3959. https://doi.org/10.3390/s20143959
• Hao, Shiwen, Zhili Zhang, Zhaofa Zhou, Junyang Zhao, Zhenjun Chang, and Zhihao Xu. 2020a. “Analysis of Deflection of Vertical Compensation for Inertial Navigation System.” Mathematical Problems in Engineering 2020: 1–15. https://doi.org/10.1155/2020/1975672
• Harding, John T., and Donald B. Lawson. 1968. “Superconducting Gyroscope: Drift Data and Mathematical Model.” AIAA Journal 6 (2): 305–11. https://doi.org/10.2514/3.4494
• Harl, Nathan, and S. N. Balakrishnan. 2010. “Reentry Terminal Guidance through Sliding Mode Control.” Journal of Guidance, Control, and Dynamics 33 (1): 186–99. https://doi.org/10.2514/1.42654
• Harlin, W. J., and D. A. Cicci. 2007. “Ballistic Missile Trajectory Prediction Using a State Transition Matrix.” Applied Mathematics and Computation 188 (2): 1832–47. https://doi.org/10.1016/j.amc.2006.11.048
• Harris, Joshua, Frank Arthurs, James V. Henrickson, and John Valasek. 2016. “Aircraft System Identification Using Artificial Neural Networks with Flight Test Data.” In 2016 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2016.7502624
• Harrison, J., J. Gallagher, and E. Grace. 1971. “An Algorithm Providing All-Attitude Capability for Three-Gimballed Inertial Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-7 (3): 532–43. https://doi.org/10.1109/taes.1971.310296
• Hart, Pierce L., and Sven Schmitz. 2022b. “Partial Pressure Field for Airfoil Wave Drag.” AIAA Journal 60 (10): 5791–5804. https://doi.org/10.2514/1.j061690
• Hartzer, Jacob, and Srikanth Saripalli. 2023. “Online Multi-IMU Calibration Using Visual-Inertial Odometry.” In 2023 IEEE Symposium Sensor Data Fusion and International Conference on Multisensor Fusion and Integration (SDF-MFI). IEEE. https://doi.org/10.1109/sdf-mfi59545.2023.10361310
• Hattis, Philip D. 1990. “Hypersonic Vehicle Air Data Collection: Assessing the Relationship between the Sensor and Guidance and Control System Requirements.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4791043
• Hayes, J. E., and W. E. Vander Velde. 1962. “Satellite Landing Control System Using Drag Modulation.” ARS Journal 32 (5): 722–30. https://doi.org/10.2514/8.6135
• Haykin, Simon, Amin Zia, Ienkaran Arasaratnam, and Yanbo Xue. 2010. “Cognitive Tracking Radar.” In 2010 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2010.5494383
• Hayner, David. 2018. “Decoupled Rate and Quadrature Servos in a MEMS Gyroscope.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358153
• Hayner, David, and Dorian Challoner. 2023. “A Navigation Grade, Software Defined Gyroscope and Extensions for Generic Vibratory Inertial Sensors.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10104002
• He, Shaoming, and Chang-Hun Lee. 2018. “Optimality of Error Dynamics in Missile Guidance Problems.” Journal of Guidance, Control, and Dynamics 41 (7): 1624–33. https://doi.org/10.2514/1.g003343
• He, Yangchao, Jiong Li, Lei Shao, Chijun Zhou, and Xiangwei Bu. 2025. “A Trajectory Prediction Method for Reentry Glide Vehicles via Adaptive Cost Function.” Aerospace 12 (1): 62. https://doi.org/10.3390/aerospace12010062
• He, Yangchao, Jiong Li, Lei Shao, Chijun Zhou, Shili Tan, and Jikun Ye. 2026. “Intelligent Trajectory Prediction Algorithm for Reentry Glide Vehicle via Physics-Informed Constraints and State Predictive Control.” Electronics 15 (14): 3132. https://doi.org/10.3390/electronics15143132
• He, Ruizhi, Luhua Liu, Guojian Tang, and Weimin Bao. 2016. “Rapid Generation of Multi-Target Entry Trajectory for Hypersonic Glide Vehicles.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554181
• He, Ruizhi, Luhua Liu, Guojian Tang, and Weimin Bao. 2017. “Maneuver Trajectory Design for Hypersonic Glide Vehicles in Dive Phase.” In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2017.7978630
• He, Xuejun, Aijun Wang, Tianle Zhou, Xuxing Zhao, and Ning Yu. 2020b. “High Precision Measurement of Dynamic Angular Rate for Turntable in the Calibration Application of Airborne Inertial Sensor.” In 2020 International Conference on Sensing, Measurement & Data Analytics in the era of Artificial Intelligence (ICSMD). IEEE. https://doi.org/10.1109/icsmd50554.2020.9261686
• He, Hongyang, Jiangning Xu, Fangjun Qin, and Feng Li. 2015b. “Genetic Algorithm Based Fast Alignment Method for Strap-down Inertial Navigation System with Large Azimuth Misalignment.” Review of Scientific Instruments 86 (11): 115004. https://doi.org/10.1063/1.4935934
• He, Qinyuan, Huapeng Yu, Dalei Liang, and Xiaozhuo Yang. 2024. “Enhancing Pure Inertial Navigation Accuracy through a Redundant High-Precision Accelerometer-Based Method Utilizing Neural Networks.” Sensors 24 (8): 2566. https://doi.org/10.3390/s24082566
• He, Dongxu, Xinle Zang, and Lei Ge. 2020a. “Effect of East Gyro Drift and Initial Azimuth Error on the Compass Azimuth Alignment Convergence Time.” Mathematical Problems in Engineering 2020: 1–10. https://doi.org/10.1155/2020/9042197
• He, Hongyang, Bing Zhu, and Feng Zha. 2019. “Particle Swarm Optimization-Based Gyro Drift Estimation Method for Inertial Navigation System.” IEEE Access 7: 55788–96. https://doi.org/10.1109/access.2019.2912871
• Heck, Michael L., John T. Findlay, G. M. Kelly, and Harold R. Compton. 1984. “Adaptation of a Strapdown Formulation for Processing Inertial Platform Data.” Journal of Guidance, Control, and Dynamics 7 (1): 15–19. https://doi.org/10.2514/3.8539
• Heeg, Jennifer, Michael G. Gilbert, and Anthony S. Pototzky. 1993a. “Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft.” Journal of Aircraft 30 (4): 453–58. https://doi.org/10.2514/3.56890
• Heij, Christiaan. 1992. “Exact Modelling and Identifiability of Linear Systems.” Automatica 28 (2): 325–44. https://doi.org/10.1016/0005-1098(92)90119-z
• Hein, G. W., K. Hehl, H. Landau, and M. Ertel. n.d. “Experiments for an Integrated Precise Airborne Navigation and Gravity Recovery System.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66189
• Heinssen, Sascha, Nico Hellwege, Nils Heidmann, Steffen Paul, and Dagmar Peters-Drolshagen. 2015. “Robust Digital Calibration Engine for MEMS Inertial Sensor Systems.” In 2015 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2015.7370520
• Heitzman-Breen, Nora, Vanja Dukic, and David M. Bortz. 2026. “A Practical Identifiability Criterion Leveraging Weak-Form Parameter Estimation.” Bulletin of Mathematical Biology 88 (5): 70. https://doi.org/10.1007/s11538-026-01639-x
• Heller, D. M. 1955. “Making a Guided Missile.” Journal of Jet Propulsion 25 (9): 8–9. https://doi.org/10.2514/8.6755
• Heller, Warren G., and Stanley K. Jordan. 1976. “Error Analysis of Two New Gradiometer-Aided Inertial Navigation Systems.” Journal of Spacecraft and Rockets 13 (6): 340–47. https://doi.org/10.2514/3.57095
• Hemann, Garrett, Sanjiv Singh, and Michael Kaess. 2016. “Long-Range GPS-Denied Aerial Inertial Navigation with LIDAR Localization.” In 2016 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros.2016.7759267
• Henley, A. J. n.d. “Terrain Aided Navigation: Current Status, Techniques for Flat Terrain and Reference Data Requirements.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66235
• Henry, J., F. Guyon, and J. P. Yvon. 1989. “Optimal Weighting for Improving Practical Identifiability in DPS Parameter Estimation Problems.” IFAC Proceedings Volumes 22 (4): 361–65. https://doi.org/10.1016/s1474-6670(17)53571-5
• Herget, Charles. 1974. “Regions of Parameter Identifiability.” In 1974 IEEE Conference on Decision and Control including the 13th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1974.270478
• Hernandez, Joshua, Konstantine Tsotsos, and Stefano Soatto. 2015. “Observability, Identifiability and Sensitivity of Vision-Aided Inertial Navigation.” In 2015 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2015.7139507
• Herrmann, U. 2008. “Multiple Discipline Optimization and Aerodynamic off-Design Analysis of Supersonic Transport Aircraft.” Journal of Aircraft 45 (5): 1474–80. https://doi.org/10.2514/1.32673
• Hervas, Jaime Rubio, Mahmut Reyhanoglu, and Hui Tang. 2014a. “Automatic Landing Control of Unmanned Aerial Vehicles on Moving Platforms.” In 2014 IEEE 23rd International Symposium on Industrial Electronics (ISIE). IEEE. https://doi.org/10.1109/isie.2014.6864588
• Hess, Ronald A., and Thomas M. Judd. 1976. “Improved Automatic Carrier Landing Using Deck Motion Prediction.” Journal of Aircraft 13 (2): 153–55. https://doi.org/10.2514/3.44514
• Hiba, Antal, Attila Gáti, and Augustin Manecy. 2021. “Optical Navigation Sensor for Runway Relative Positioning of Aircraft during Final Approach.” Sensors 21 (6): 2203. https://doi.org/10.3390/s21062203
• Hicks, S. 1993. “Advanced Cruise Missile Guidance System Description.” In Proceedings of the IEEE 1993 National Aerospace and Electronics Conference-NAECON 1993. IEEE. https://doi.org/10.1109/naecon.1993.290941
• Hildebrand, R., and M. Gevers. n.d. “Identification for Control: Optimal Input Design with Respect to a Worst-Case v-Gap Cost Function.” In 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475), vol. 1. IEEE. https://doi.org/10.1109/cdc.2003.1272697
• Hill, D. A., J. R. Strunk, B. J. Purslow, and R. W. Bass. n.d. “Robust Controller Design and Mechaneza Tion for Precision Platform Alignment of the Trident II Inertial Measurement Unit (IMU).” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.720902
• Hiller, Tobias, Zsigmond Pentek, Jan-Timo Liewald, Alexander Buhmann, and Hubert Roth. 2019. “Origins and Mechanisms of Bias Instability Noise in a Three-Axis Mode-Matched MEMS Gyroscope.” Journal of Microelectromechanical Systems 28 (4): 586–96. https://doi.org/10.1109/jmems.2019.2921607
• Hinchliffe, Benjamin, and Ning Qin. 2017. “Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction.” AIAA Journal 55 (3): 818–31. https://doi.org/10.2514/1.j055319
• Hindman, R., and W. M. Shell. 2005a. “Design of a Missile Autopilot Using Adaptive Nonlinear Dynamic Inversion.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1469954
• Hindman, R., and W. M. Shell. 2005b. “Missile Autopilot Design Using Adaptive Nonlinear Dymanic Inversion.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1470587
• Hiret, A., G. Duc, and J. P. Bonnet. 1998. “The Application of Gain-Scheduling H ∞ Controllers for a Missile Autopilot.” IFAC Proceedings Volumes 31 (21): 59–64. https://doi.org/10.1016/s1474-6670(17)41059-7
• Hiromi Suzukit and Toshiharu Sugie. 2007. “Optimal Input Design for System Identification in the Presence of Undermodeling.” In 2007 46th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2007.4435001
• Hjalmarsson, Hakan, and Jonas Martensson. 2007. “Optimal Input Design for Identification of Non-Linear Systems: Learning from the Linear Case.” In 2007 American Control Conference. IEEE. https://doi.org/10.1109/acc.2007.4282525
• Ho Chul Lee, Jae Weon Choi, Taek Lyul Song, and Chan Ho Song. 2004. “Agile Missile Autopilot Design via Time-Varying Eigenvalue Assignment.” In ICARCV 2004 8th Control, Automation, Robotics and Vision Conference, 2004., vol. 3. IEEE. https://doi.org/10.1109/icarcv.2004.1469437
• Hoang, Minh Long, and Antonio Pietrosanto. 2021. “Yaw/Heading Optimization by Drift Elimination on MEMS Gyroscope.” Sensors and Actuators A: Physical 325: 112691. https://doi.org/10.1016/j.sna.2021.112691
• Hodson, A. E. 1963. “Optimal Levelling and Gyrocompassing of Inertial Systems.” IEEE Transactions on Aerospace and Navigational Electronics ANE-10 (1): 18–26. https://doi.org/10.1109/tane.1963.4502074
• Hoflinger, F., J. Muller, M. Tork, L. M. Reindl, and W. Burgard. 2012. “A Wireless Micro Inertial Measurement Unit (IMU).” In 2012 IEEE International Instrumentation and Measurement Technology Conference Proceedings. IEEE. https://doi.org/10.1109/i2mtc.2012.6229271
• Holovatyy, Andriy, Mykhaylo Lobur, and Vasyl Teslyuk. 2008. “VHDL-AMS Model of Mechanical Elements of MEMS Tuning Fork Gyroscope for the Schematic Level of Computer-Aided Design.” In 2008 International Conference on Perspective Technologies and Methods in MEMS Design. IEEE. https://doi.org/10.1109/memstech.2008.4558762
• Hong, Kyungwoo. 2025. “Parallel Resampling for Accelerated Particle Filters in Vision-Based Terrain-Referenced Navigation.” Journal of Aerospace Information Systems 22 (10): 898–910. https://doi.org/10.2514/1.i011570
• Hong, Wooram, and Chongam Kim. 2014. “Computational Study on Hysteretic Inlet Buzz Characteristics under Varying Mass Flow Conditions.” AIAA Journal 52 (7): 1357–73. https://doi.org/10.2514/1.j052481
• Hong, Kyungwoo, Youngjoo Kim, and Hyochoong Bang. 2017. “Comparison of Solutions for Measurement Ambiguity in Terrain Referenced Navigation.” In 2017 European Navigation Conference (ENC). IEEE. https://doi.org/10.1109/euronav.2017.7954207
• Hongyang He, Jiangning Xu, Fangjun Qin, and Feng Li. 2015. “Platform Bench Strap-down Algorithm-Inertial Navigation System.” In 2015 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2015.7382747
• Horing, Jennifer A., Iain D. Boyd, and Kurt K. Maute. 2024. “Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet.” Journal of Propulsion and Power 40 (2): 181–93. https://doi.org/10.2514/1.b39345
• Horsfall, R. B. 1958. “Stellar Inertial Navigation.” IRE Transactions on Aeronautical and Navigational Electronics ANE-5 (2): 106–14. https://doi.org/10.1109/tane3.1958.4201596
• Hörsting, Marian, and Matthias Wenzel. 2025. “Design Optimization of the Quadrature Error in a MEMS Gyroscope.” In 2025 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors59705.2025.11330509
• Hosseini-Pishrobat, Mehran, Ahmet Arif Aslan, and Erdinc Tatar. 2026. “Exploring the Boundaries of MEMS Gyroscope Scale Factor Temperature Stability via Distributed on-Chip Strain Measurements.” Journal of Microelectromechanical Systems 35 (1): 54–66. https://doi.org/10.1109/jmems.2025.3626121
• Hosseini-Pishrobat, Mehran, Derin Erkan, and Erdinc Tatar. 2024. “On Temperature Effects in a MEMS Ring Gyroscope.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502078
• Hosseini-Pishrobat, Mehran, Derin Erkan, and Erdinc Tatar. 2025. “Achieving below 200ppm Scale Factor Temperature Stability in an Am Gyroscope with on-Chip Stress Sensing.” In 2025 IEEE 38th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems61431.2025.10917391
• Hosseini-Pishrobat, Mehran, and Erdinc Tatar. 2025a. “Estimating Temperature-Dependent Glass Substrate CTE via Frequency Measurements in a MEMS Gyroscope.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037086
• Hosseini-Pishrobat, Mehran, and Erdinc Tatar. 2025b. “Modeling Temperature Effects in a MEMS Ring Gyroscope: Toward Physics-Aware Drift Compensation.” Journal of Microelectromechanical Systems 34 (2): 150–63. https://doi.org/10.1109/jmems.2024.3524796
• Hosseini-Pishrobat, Mehran, Baha Erim Uzunoglu, and Erdinc Tatar. 2023. “Modeling Stress Effects on Frequencies of a Mems Ring Gyroscope.” In 2023 IEEE 36th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems49605.2023.10052439
• Hotate, Kazuo, and Kunio Tabe. 1986b. “Drift of an Optical Fiber Gyroscope Caused by the Faraday Effect: Influence of the Earth’s Magnetic Field.” Applied Optics 25 (7): 1086. https://doi.org/10.1364/ao.25.001086
• Hotate, K., and K. Tabe. 1987. “Drift of an Optical Fiber Gyroscope Caused by the Faraday Effect: Experiment.” Journal of Lightwave Technology 5 (7): 997–1001. https://doi.org/10.1109/jlt.1987.1075591
• Hou, Bowen, Zhangming He, Haiyin Zhou, and Jiongqi Wang. 2019. “Integrated Design and Accuracy Analysis of Star Sensor and Gyro on the Same Benchmark for Satellite Attitude Determination System.” IEEE/CAA Journal of Automatica Sinica 6 (4): 1074–80. https://doi.org/10.1109/jas.2019.1911600
• Howard, Michael L. 1984. “Missile Deployment Module Accuracy Verification.” Journal of Guidance, Control, and Dynamics 7 (2): 231–34. https://doi.org/10.2514/3.8571
• Howell, Ronald H., and Helmut H. Korst. 1971. “Separation Controlled Transonic Drag-Rise Modification for V-Shaped Notches.” AIAA Journal 9 (10): 2051–57. https://doi.org/10.2514/3.6460
• Hsu, D. Y. n.d. “Comparison of Four Gravity Models.” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509138
• Hsu, Tzu-Hsuan, Yuan-Jen Chang, He-Kai Hsu, Tsung-Ti Chen, and Po-Wen Hwang. 2022. “Predicting the Remaining Useful Life of Landing Gear with Prognostics and Health Management (PHM).” Aerospace 9 (8): 462. https://doi.org/10.3390/aerospace9080462
• Hsu, Yu-Liang, Po-Huan Chou, and Yu-Chen Kuo. 2017. “Drift Modeling and Compensation for MEMS-Based Gyroscope Using a Wiener-Type Recurrent Neural Network.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935653
• Hu, Yue, Yuan Cao, and Shifeng Zhang. 2013a. “Design of Sliding Mode Control with Disturbance Observers for Inertial Platform.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561775
• Hu, Jichao, Juntao Chang, Lei Wang, Shibin Cao, and Wen Bao. 2013b. “Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet.” Scientific World Journal 2013 (1): 254376. https://doi.org/10.1155/2013/254376
• Hu, Peida, Bingxu Chen, Chenxi Zhang, and Qiuping Wu. 2019. “Correlation-Averaging Methods and Kalman Filter Based Parameter Identification for a Rotational Inertial Navigation System.” IEEE Transactions on Industrial Informatics 15 (3): 1321–28. https://doi.org/10.1109/tii.2018.2850756
• Hu, Zhongxu, and Barry Gallacher. 2015. “Control and Damping Imperfection Compensation for a Rate Integrating MEMS Gyroscope.” In 2015 DGON Inertial Sensors and Systems Symposium (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2015.7314258
• Hu, Zhongxu, and Barry Gallacher. 2016. “Extended Kalman Filtering Based Parameter Estimation and Drift Compensation for a MEMS Rate Integrating Gyroscope.” Sensors and Actuators A: Physical 250: 96–105. https://doi.org/10.1016/j.sna.2016.09.019
• Hu, Zhongxu, and Barry J. Gallacher. 2018. “Precision Mode Tuning towards a Low Angle Drift MEMS Rate Integrating Gyroscope.” Mechatronics 56: 306–17. https://doi.org/10.1016/j.mechatronics.2017.04.007
• Hu, Zhongxu, and Barry J. Gallacher. 2019. “Effects of Nonlinearity on the Angular Drift Error of an Electrostatic MEMS Rate Integrating Gyroscope.” IEEE Sensors Journal 19 (22): 10271–80. https://doi.org/10.1109/jsen.2019.2929352
• Hu, Z. X., B. J. Gallacher, J. S. Burdess, C. P. Fell, and K. Townsend. 2011. “Precision Mode Matching of MEMS Gyroscope by Feedback Control.” In 2011 IEEE SENSORS Proceedings. IEEE. https://doi.org/10.1109/icsens.2011.6126998
• Hu, Kaibo, and Yaxuan Liu. 2012. “Adaptive Noise Cancellation Method for Fiber Optic Gyroscope.” Procedia Engineering 29: 1338–43. https://doi.org/10.1016/j.proeng.2012.01.137
• Hu, Yudong, Zichu Liu, Chunwang Jiang, Wuxing Jing, and Changsheng Gao. 2025. “Maneuver Mode Parametric Modeling Based on Trajectory Curve Evolution Laws for Hypersonic Glide Vehicles.” Aerospace Science and Technology 157: 109856. https://doi.org/10.1016/j.ast.2024.109856
• Hu, Zhiyong, Haiyang Quan, Fuqiang Zhang, and Peisheng Wang. 2009. “Ultra-Low Noise Charge Sensitive Amplifier for MEMS Gyroscope.” In 2009 Fifth International Conference on MEMS NANO, and Smart Systems. IEEE. https://doi.org/10.1109/icmens.2009.20
• Hu, Yunpeng, Inna Sharf, and Lei Chen. 2020c. “Three-Spacecraft Autonomous Orbit Determination and Observability Analysis with Inertial Angles-Only Measurements.” Acta Astronautica 170: 106–21. https://doi.org/10.1016/j.actaastro.2020.01.005
• Hu, X., and Zh. Wang. 2019. “A New Method Based on Dual-State Chi-Square Fault-Tolerant to Inertial/Acoustic Range Integrated Navigation System with Single Transponder.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769379
• Hu, Xiaoqiang, Xiaoli Zhang, Xiafu Peng, and Delong Yang. 2020b. “A Novel Algorithm for the Fault Diagnosis of a Redundant Inertial Measurement Unit.” IEEE Access 8: 46081–91. https://doi.org/10.1109/access.2020.2978521
• Hua, Ruhao, Qi Chen, Zhao Wan, and Hao Chen. 2023. “Study on the Aerothermoelastic Characteristics of a Body Flap Considering the Nozzle–Jet Interference.” Aerospace 10 (10): 829. https://doi.org/10.3390/aerospace10100829
• Hua, A. Zong, and B. Liu Yan. 2018. “A Method of Improving the Precision of Geocentric Vector Aided by Inertial Navigation Information.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018695
• Hua-Ming, Qian, Li Hao, and Wang Hai-Yong. 2015. “Design and Verification of Star-Map Simulation Software Based on CCD Star Tracker.” In 2015 8th International Conference on Intelligent Computation Technology and Automation (ICICTA). IEEE. https://doi.org/10.1109/icicta.2015.103
• Huaming Qian, Quanxi Xia, Bo Jiang, and Chong Wang. 2009. “On Modeling of Random Drift of MEMS Gyroscope and Design of Kalman Filter.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246601
• Huang, Mingyang. 2019. “Control Strategy of Launch Vehicle and Lander with Adaptive Landing Gear for Sloped Landing.” Acta Astronautica 161: 509–23. https://doi.org/10.1016/j.actaastro.2019.03.073
• Huang, Chunbing, Federica Cattani, and Federico Galvanin. 2023b. “An Optimal Experimental Design Strategy for Improving Parameter Estimation in Stochastic Models.” Computers & Chemical Engineering 170: 108133. https://doi.org/10.1016/j.compchemeng.2023.108133
• Huang, Qingxuan, Pu Chen, and Nan Xiao. 2026b. “Least-Squares-Based Extrinsic Calibration Method for Point-Source Polarized Light Sensors and Inertial Navigation Systems.” In 2026 2nd International Conference on Navigation, Detection and Control (CNDC). IEEE. https://doi.org/10.1109/cndc70899.2026.11708272
• Huang, Yingwu, and Yan Cui. 2012. “Analysis and Optimum Design for Inertial Navigation Platform Frame Structure.” In 2012 International Conference on Systems and Informatics (ICSAI2012). IEEE. https://doi.org/10.1109/icsai.2012.6223127
• Huang, Daning, and Peretz P. Friedmann. 2020a. “An Aerothermoelastic Analysis Framework with Reduced-Order Modeling Applied to Composite Panels in Hypersonic Flows.” Journal of Fluids and Structures 94: 102927. https://doi.org/10.1016/j.jfluidstructs.2020.102927
• Huang, Daning, and Peretz P. Friedmann. 2020b. “Multi-Objective Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws and Its Application.” AIAA Journal 58 (7): 3250–57. https://doi.org/10.2514/1.j059308
• Huang, Daning, Peretz P. Friedmann, and Tomer Rokita. 2019a. “Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation.” AIAA Journal 57 (10): 4377–92. https://doi.org/10.2514/1.j057499
• Huang, Chuan, Gustaf Hendeby, and Isaac Skog. 2024b. “An Observability-Constrained Magnetic Field-Aided Inertial Navigation System.” In 2024 14th International Conference on Indoor Positioning and Indoor Navigation (IPIN). IEEE. https://doi.org/10.1109/ipin62893.2024.10786170
• Huang, Keqi, Yikang Li, Xiaomin Liu, et al. 2026d. “Research on High-Precision Navigation Technology for UAV under GNSS-Denied Scenarios.” In 2026 5th International Symposium on Semiconductor and Electronic Technology (ISSET). IEEE. https://doi.org/10.1109/isset70600.2026.11682537
• Huang, Chunfu, An Li, Fangjun Qin, Lin Tong, and Zhi Wang. 2019c. “Temperature Error Compensation Method for Fiber Optic Gyroscope Considering Heat Transfer Delay.” In 2019 3rd International Conference on Electronic Information Technology and Computer Engineering (EITCE). IEEE. https://doi.org/10.1109/eitce47263.2019.9094814
• Huang, Xisheng, Guangjun Liu, and Yugang Liu. 2025a. “Collision Detection and Recovery Control of Drones Using Onboard Inertial Measurement Unit.” Drones 9 (5): 380. https://doi.org/10.3390/drones9050380
• Huang, Ming, Yuanyuan Liu, Gongliu Yang, and Xiao Zhou. 2016b. “An Innovation Based DFA and EMD Method for Denoising Fiber Optic Gyroscope Drift Signal.” In 2016 3rd International Conference on Information Science and Control Engineering (ICISCE). IEEE. https://doi.org/10.1109/icisce.2016.270
• Huang, Tenglong, Huihui Pan, and Weichao Sun. 2023c. “A Sensor Fault Detection, Isolation, and Estimation Method for Intelligent Vehicles.” Control Engineering Practice 139: 105620. https://doi.org/10.1016/j.conengprac.2023.105620
• Huang, Daning, Tomer Rokita, and Peretz P. Friedmann. 2018c. “Integrated Aerothermoelastic Analysis Framework with Application to Skin Panels.” AIAA Journal 56 (11): 4562–81. https://doi.org/10.2514/1.j056677
• Huang, Lan, Jianmei Song, and Chunyan Zhang. 2017b. “Observability Analysis and Filter Design for a Vision Inertial Absolute Navigation System for UAV Using Landmarks.” Optik 149: 455–68. https://doi.org/10.1016/j.ijleo.2017.09.060
• Huang, Junjie, Chenghao Sun, Jinhui Chen, and Xiaoqiang Hu. 2026a. “Error Compensation-Enhanced Robust Filter for Inertial-Based Integrated Navigation System.” In 2026 5th International Symposium on Aerospace Engineering and Systems (ISAES). IEEE. https://doi.org/10.1109/isaes70982.2026.11669248
• Huang, Xianlin, and Zhenkai Wang. 2011. “Adaptive Unscented Kalman Filter in Inertial Navigation System Alignment.” In 2011 2nd International Conference on Intelligent Control and Information Processing. IEEE. https://doi.org/10.1109/icicip.2011.6008402
• Huang, Ciying, Ziao Wang, Juntao Chang, Chengkun Lv, and Chen Kong. 2026c. “Numerical Investigation of Axisymmetric Supersonic Inlet-Isolator Unstart under Upstream-Propagating Pressure Wave.” Aerospace Science and Technology 177: 112309. https://doi.org/10.1016/j.ast.2026.112309
• Huang, Huimin, Wenbo Wang, Lanxin Zhu, et al. 2025b. “An Interferometric Fiber Optic Gyroscope Based on Fiber Delay with Reduced Bias Instability and Enhanced Sensitivity.” Journal of Lightwave Technology 43 (9): 4290–97. https://doi.org/10.1109/jlt.2025.3535798
• Huang, Jiaoyan, Aiguo Xia, Shenao Zou, Cong Han, and Guoan Yang. 2020. “An Efficient Approach for Identification of the Inlet Distortion of Engine Based on Acoustic Emission Technique.” Applied Sciences 10 (22): 8240. https://doi.org/10.3390/app10228240
• Huang, Hongqiao, Wen Ye, Li Liu, Wenjing Wang, Yan Wang, and Huiliang Cao. 2025c. “Temperature Compensation Method for MEMS Ring Gyroscope Based on PSO-TVFEMD-SE-TFPF and FTTA-LSTM.” Micromachines 16 (5): 507. https://doi.org/10.3390/mi16050507
• Huang, Chao, Guoxing Yi, Qingshuang Zen, Ziyang Qi, and Mingyang Yang. 2016c. “Methods of Evaluation of Navigation Errors in Platform Inertial Navigation Systems Based on PSVR.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531442
• Huang, Chao, Guoxing Yi, Qingshuang Zeng, and Nan Yi. 2016a. “The Establishment and Analysis of the High-Order Error Model of Platform Inertial Navigation System in Mobile Conditions.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554225
• Huang, Jingshuai, Hongbo Zhang, Guanghua Li, and Guojian Tang. 2016d. “Terminal Guidance and Control for Kinetic Kill Vehicle Adopting Side Window Detection.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828812
• Huang, Jingshuai, Hongbo Zhang, Guojian Tang, and Weimin Bao. 2017c. “Radar Tracking for Hypersonic Glide Vehicle Based on Aerodynamic Model.” In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2017.7978679
• Huang Weiquan, Hao Yanling, Cheng Jianhua, Li Gang, Fu Jiangang, and Bu Xiaobing. n.d. “Research of the Inertial Navigation System with Variable Damping Coefficients Horizontal Damping Networks.” In Oceans ‘04 MTS/IEEE Techno-Ocean ‘04 (IEEE Cat. No.04CH37600), vol. 3. IEEE. https://doi.org/10.1109/oceans.2004.1405762
• Huang Xiaokai, Chen Yunxia, Lin Fengchun, and Kang Rui. 2011b. “Inertial Platform Systems Parameters Degradation Finite Element Modeling.” In 2011 Prognostics and System Health Managment Confernece. IEEE. https://doi.org/10.1109/phm.2011.5939509
• Huang Xiaokai, Chen Yunxia, Xu Dan, and Kang Rui. 2011a. “Inertial Platform System Parameters Drift Finite Element Modeling.” In 2011 Third International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2011.388
• Hubbartt, J. E., and W. C. Strahle. 1981. “External/Base Burning for Base Drag Reduction at Mach 3.” AIAA Journal 19 (11): 1502–4. https://doi.org/10.2514/3.60088
• Huddle, James. 1978a. “Application of Inertial Navigation Systems to Geodetic Postion and Gravity Vector Survey.” In 1978 IEEE Conference on Decision and Control including the 17th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1978.267967
• Huddle, James K. 1978b. “Theory and Performance for Position and Gravity Survey with an Inertial System.” Journal of Guidance and Control 1 (3): 183–88. https://doi.org/10.2514/3.55762
• Hughes, E. J., A. Tsourdos, and B. A. White. n.d. “Multiobjective Design of a Fuzzy Controller for a Nonlinear Missile Autopilot.” In Proceedings. IEEE International Symposium on Computer Aided Control System Design. IEEE. https://doi.org/10.1109/cacsd.2002.1036922
• Hui, F., M. Li Tianjin, L. Ma, W. Zuo, S. Zhang, and X. M. Zhang. 2017. “Investigation on near Gaussian-Shaped Spectrum Erbium-Doped Fiber Source Which Applied to the Fiber Optic Gyroscope.” In 2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2017.7995669
• Hui Qin, Zhiyong Lin, Weidong Liu, and Zhenguo Wang. 2010. “A Review of Principles and Key Techniques for Supersonic Pulsed Detonation Ramjet Engine (SPDRE).” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633997
• Hull, R. A., and Zhihua Qu. 1997. “Dynamic Robust Recursive Control Design and Its Application to a Nonlinear Missile Autopilot.” In Proceedings of the 1997 American Control Conference (Cat. No.97CH36041). IEEE. https://doi.org/10.1109/acc.1997.611921
• Hung, J. C., and H. V. White. 1979. “Identification of IMU Parameters for High Accuracy Gyrocompassing.” IFAC Proceedings Volumes 12 (8): 1067–72. https://doi.org/10.1016/s1474-6670(17)65528-9
• Huo, Lin, Xing-Hua Cheng, and Tao Yang. 2015. “Aerothermoelastic Response Analysis for C/SiC Panel of Ceramic Matrix Composite Shingle Thermal Protection System.” Advances in Space Research 55 (9): 2352–71. https://doi.org/10.1016/j.asr.2015.02.008
• Hurak, Zdenek, and Martin Rezac. 2009. “Combined Line-of-Sight Inertial Stabilization and Visual Tracking: Application to an Airborne Camera Platform.” In Proceedings of the 48h IEEE Conference on Decision and Control (CDC) held jointly with 2009 28th Chinese Control Conference. IEEE. https://doi.org/10.1109/cdc.2009.5400793
• Hutchins, Kelley E., Maruthi R. Akella, Noel T. Clemens, Jeffrey M. Donbar, and Sivaram Gogineni. 2014. “Experimental Identification of Transient Dynamics for Supersonic Inlet Unstart.” Journal of Propulsion and Power 30 (6): 1605–12. https://doi.org/10.2514/1.b35230
• Hutchinson, Charles E., and John H. Fagan. 1973. “Kalman Filter Design Considerations for Space-Stable Inertial Navigation Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-9 (2): 306–19. https://doi.org/10.1109/taes.1973.309800
• Hyötyniemi, Heikki. 1997. “On Structural Identifiability of Dynamic Models.” IFAC Proceedings Volumes 30 (11): 257–62. https://doi.org/10.1016/s1474-6670(17)42856-4
• Ignagni, Mario. 2021. “Accuracy Limits on Strapdown Velocity and Position Computations.” Journal of Guidance, Control, and Dynamics 44 (3): 654–58. https://doi.org/10.2514/1.g005538
• Ignagni, Mario. 2025. “Accuracy Limits in Strapdown Attitude Determination.” Journal of Guidance, Control, and Dynamics 48 (9): 2113–17. https://doi.org/10.2514/1.g009206
• Igreja, J. M., and J. M. Lemos. 2022. “Oracle for Guidance with Deep Neural Networks in Reusable Launch Vehicle Landing.” In 2022 International Conference on Control, Automation and Diagnosis (ICCAD). IEEE. https://doi.org/10.1109/iccad55197.2022.9854017
• “II. Modern Cruise Missile Programmes.” 1987. Adelphi Papers 28 (226): 5–12. https://doi.org/10.1080/05679328708457562
• Ikawa, Hideo. 1991. “Rapid Methodology for Design and Performance Prediction of Integrated Supersonic Combustion Ramjet Engine.” Journal of Propulsion and Power 7 (3): 437–44. https://doi.org/10.2514/3.23345
• Ilango, Harun Surej, and R. Ramanathan. 2020. “A Performance Study of Bio-Inspired Algorithms in Autonomous Landing of Unmanned Aerial Vehicle.” Procedia Computer Science 171: 1449–58. https://doi.org/10.1016/j.procs.2020.04.155
• Iliev, Ilia, and Ivaylo Nachev. 2022. “Automatic Landing of Unmanned Aerial Vehicles via Wireless Positioning System with Pseudo-Conical Scanning.” Sensors 22 (17): 6451. https://doi.org/10.3390/s22176451
• Iliff, Kenneth W., and Richard E. Maine. 1983. “Uses of Parameter Estimation in Flight Test.” Journal of Aircraft 20 (12): 1043–49. https://doi.org/10.2514/3.48210
• Indiresan, P. V. 1965. “A Method for Improving the Accuracy of Tracking Radar.” IETE Journal of Research 11 (12): 483–86. https://doi.org/10.1080/03772063.1965.11485234
• “Inertial Navigation Systems.” 1986. IEEE Control Systems Magazine 6 (6): 25–25. https://doi.org/10.1109/mcs.1986.1105163
• “An Integrated Missile Reliability Growth Program.” 1984. Microelectronics Reliability 24 (6): 1097. https://doi.org/10.1016/0026-2714(84)90909-0
• Iozan, Lucian Ioan, Corneliu Rusu, Jussi Collin, and Jarmo Takala. 2010. “A Study of the External Factors That Affect the Measurement Data of a MEMS Gyroscope Sensor — Towards an Inertial Navigation System.” In 2010 9th International Symposium on Electronics and Telecommunications. IEEE. https://doi.org/10.1109/isetc.2010.5679313
• Ipas, O., M. Przylecki, E. Soria, A. Albeniz, A. Bernardini, and A. Barrio. 2022. “Autonomous Landing and Avoidance System Virtual Validation Approach.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836209
• Ito, Keitaro, Shota Harada, Yusuke Kawai, and Hiroyuki Wado. 2024. “Precision Mode-Matching Gyroscope Using in-Run Adjustment of Spring Azimuth.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502086
• Ivanov, Danil, Uliana Monakhova, Yaroslav Mashtakov, and Sergey Shestakov. 2026. “Earth-Point Stabilization Performance Using Asynchronous Star Tracker and Angular Velocity Sensor Measurements.” Aerospace 13 (8): 694. https://doi.org/10.3390/aerospace13080694
• Iwase, Masami, Makoto Shigi, and Shoshiro Hatakeyama. 2005. “Optimal Input Design for Identification of Continuous-Time Systems.” IFAC Proceedings Volumes 38 (1): 482–87. https://doi.org/10.3182/20050703-6-cz-1902.00081
• Iwase, Masami, Makoto Shigi, and Shoshiro Hatakeyama. 2006. “Fft-Based Optimal Input Design for Identification of Continuous-Time Systems.” IFAC Proceedings Volumes 39 (1): 1145–49. https://doi.org/10.3182/20060329-3-au-2901.00184
• Izadmehr, Meysam, and Mehdi Khakian Ghomi. 2020. “An Accuracy of Better than 200 m in Positioning Using a Portable Star Tracker.” New Astronomy 74: 101272. https://doi.org/10.1016/j.newast.2019.04.004
• Jackson, P. 1990. “Applying Mu -Synthesis to Missile Autopilot Design.” In 29th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1990.203333
• Jacob, Joel Varghese, Murali Mohan Gade, R. Jeyasenthil, and Samran. 2023. “Design of Missile Roll Autopilot Based on Quantitative Feedback Theory.” In 2023 International Conference on Power, Instrumentation, Energy and Control (PIECON). IEEE. https://doi.org/10.1109/piecon56912.2023.10085891
• Jacquez, John A. 1991. “Identifiability and Parameter Estimation.” Journal of Parenteral and Enteral Nutrition 15 (3). https://doi.org/10.1177/014860719101500355s
• Jacquez, John A., and Peter Greif. 1985. “Numerical Parameter Identifiability and Estimability: Integrating Identifiability, Estimability, and Optimal Sampling Design.” Mathematical Biosciences 77 (1–2): 201–27. https://doi.org/10.1016/0025-5564(85)90098-7
• Jaewon Seo, Jang Gyu Lee, and Chan Gook Park. 2004. “Bias Suppression of GPS Measurement in Inertial Navigation System Vertical Channel.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308986
• Jafari, Mehdi. 2015. “Optimal Redundant Sensor Configuration for Accuracy Increasing in Space Inertial Navigation System.” Aerospace Science and Technology 47: 467–72. https://doi.org/10.1016/j.ast.2015.09.017
• Jafari, Soheil, and Theoklis Nikolaidis. 2018. “Turbojet Engine Industrial Min–Max Controller Performance Improvement Using Fuzzy Norms.” Electronics 7 (11): 314. https://doi.org/10.3390/electronics7110314
• Jain, Priyanshi, Rohaan Qureshi, and Raghava Nallanthighal. 2023. “UAV Swarm Navigation in GNSS Denied Region with Formation Control.” In 2023 4th International Conference for Emerging Technology (INCET). IEEE. https://doi.org/10.1109/incet57972.2023.10170669
• Jakowluk, Wiktor, and Mirosław Świercz. 2025. “Optimal Input Design for Fractional-Order System Identification Using an LMI-Based Frequency Error Criterion.” Applied Sciences 15 (23): 12665. https://doi.org/10.3390/app152312665
• James, Jintu K., and Heuy Dong Kim. 2022. “Study on the Mechanism of the Buzz Flow in a Supersonic Intake.” Aerospace Science and Technology 131: 107982. https://doi.org/10.1016/j.ast.2022.107982
• James, Jintu K., Abhilash Suryan, and Heuy Dong Kim. 2021. “Buzz Characteristics and Separation Bubble Dynamics in Supersonic Intake.” Aerospace Science and Technology 115: 106795. https://doi.org/10.1016/j.ast.2021.106795
• Jami’in, Mohammad Abu. 2020. “The Cascade Linear Quadratic Gaussian (LQG) Controller for Automatic Landing Systems in Aircraft.” In 2020 International Conference on Applied Science and Technology (iCAST). IEEE. https://doi.org/10.1109/icast51016.2020.9557592
• Jang, Dongjin, Jinyong Park, and Dongjin Lee. 2017. “Accelerated Point Mass Filter for Vision-Aided Terrain Referenced Navigation.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991521
• Jankovitz, J., and J. Perdzock. n.d. “Laboratory and Flight Evaluation of the Integrated Inertial Sensor Assembly (IISA).” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195475
• Jantawong, Jirayuth, and Chirdpong Deelertpaiboon. 2018. “Automatic Landing Control Based on GPS for Fixed-Wing Aircraft.” In 2018 15th International Conference on Electrical Engineering/Electronics, Computer, Telecommunications and Information Technology (ECTI-CON). IEEE. https://doi.org/10.1109/ecticon.2018.8620037
• Jarraya, Imen, Abdulrahman Al-Batati, Muhammad Bilal Kadri, et al. 2025. “Gnss-Denied Unmanned Aerial Vehicle Navigation: Analyzing Computational Complexity, Sensor Fusion, and Localization Methodologies.” Satellite Navigation 6 (1): 9. https://doi.org/10.1186/s43020-025-00162-z
• Jarraya, Imen, Fatimah Alahmed, Mohamed Abdelkader, Khaled Gabr, Muhammad Bilal Kadri, and Wadii Boulila. 2026. “CLAK:CNN-LSTM-Attention and Kolmogorov-Arnold Networks for Non-Visual UAV Localization in GNSS-Denied Environments.” Satellite Navigation 7 (1): 6. https://doi.org/10.1186/s43020-026-00192-1
• Jategaonkar, Ravindra, Dietrich Fischenberg, and Wolfgang von Gruenhagen. 2004. “Aerodynamic Modeling and System Identification from Flight Data-Recent Applications at DLR.” Journal of Aircraft 41 (4): 681–91. https://doi.org/10.2514/1.3165
• Jategaonkar, R. V., W. Monnich, D. Fischenberg, and B. Krag. 1997. “Identification of Speed Brake, Air-Drop, and Landing Gear Effects from Flight Data.” Journal of Aircraft 34 (2): 174–80. https://doi.org/10.2514/2.2169
• Jauberthie, C., L. Belkoura, and L. Denis-Vidal. 2003a. “Aircraft Parameter and Delay Identifiability.” In 2003 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2003.7085230
• Jauberthie, Carine, François Bournonville, Patricia Coton, and Frank Rendell. 2006. “Optimal Input Design for Aircraft Parameter Estimation.” Aerospace Science and Technology 10 (4): 331–37. https://doi.org/10.1016/j.ast.2005.08.002
• Jauberthie, C., and E. Chanthery. 2013. “Optimal Input Design for a Nonlinear Dynamical Uncertain Aerospace System.” IFAC Proceedings Volumes 46 (23): 469–74. https://doi.org/10.3182/20130904-3-fr-2041.00060
• Jauberthie, Carine, Lilianne Denis-Vidal, and Ghislaine Joly-Blanchard. 2003b. “Aircraft Parameter Estimation by Using the Optimal Input Design and Linear Matrix Inequalities.” IFAC Proceedings Volumes 36 (16): 657–62. https://doi.org/10.1016/s1474-6670(17)34836-x
• Jauberthie, Carine, Lilianne Denis-Vidal, Qiaochu Li, and Zohra Cherfi-Boulanger. 2018. “Optimal Input Design for Parameter Estimation in a Bounded-Error Context for Nonlinear Dynamical Systems.” Automatica 92: 86–91. https://doi.org/10.1016/j.automatica.2018.03.003
• Jauberthie, Carine, Nathalie Verdière, and Louise Travé-Massuyès. 2012. “Set-Membership Identifiability and Guaranteed Parameter Estimation for Nonlinear Uncertain Dynamical Systems.” IFAC Proceedings Volumes 45 (16): 434–39. https://doi.org/10.3182/20120711-3-be-2027.00224
• Jayaraman, Balaji, Vikram Kumar Saini, and Ajoy Kanti Ghosh. 2022. “Robust Time-Delayed PID Flight Control for Automatic Landing Guidance under Actuator Loss-Of-Control.” IFAC-PapersOnLine 55 (22): 189–94. https://doi.org/10.1016/j.ifacol.2023.03.032
• Jeerage, M. K. n.d. “Reliability Analysis of Fault-Tolerant IMU Architectures with Redundant Inertial Sensors.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66232
• Jeerage, M. K. 1990. “Reliability Analysis of Fault-Tolerant IMU Architectures with Redundant Inertial Sensors.” IEEE Aerospace and Electronic Systems Magazine 5 (7): 23–28. https://doi.org/10.1109/62.134217
• Jekeli, Christopher. 2006. “Precision Free-Inertial Navigation with Gravity Compensation by an Onboard Gradiometer.” Journal of Guidance, Control, and Dynamics 29 (3): 704–13. https://doi.org/10.2514/1.15368
• Jenila, C., Sakthi S. Viswanath, M. Chandru, M. Karkuvel, and Hemand M. Surya. 2023. “Design and Link Budget Analysis of Efficient Missile Telemetry Data Transmission during Re-Entry Blackout.” In 2023 International Conference on Intelligent Technologies for Sustainable Electric and Communications Systems (iTech SECOM). IEEE. https://doi.org/10.1109/itechsecom59882.2023.10435081
• Jenn, A. A., and H. F. Nelson. 1989. “Wing Vertical Position Effects on Lift for Supersonic Delta Wing Missiles.” Journal of Spacecraft and Rockets 26 (4): 210–16. https://doi.org/10.2514/3.26056
• Jeon, Hyun Cheol, Young Bum Park, and Chan Gook Park. 2016. “Robust Performance of Terrain Referenced Navigation Using Flash LiDAR.” In 2016 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2016.7479796
• Jeon, Hyun Cheol, Woo Jung Park, and Chan Gook Park. 2018a. “Grid Design for Efficient and Accurate Point Mass Filter-Based Terrain Referenced Navigation.” IEEE Sensors Journal 18 (4): 1731–38. https://doi.org/10.1109/jsen.2017.2779463
• Jerebets, S. 2006. “Star Tracker Focal Plane Evaluation for the JIMO Mission.” In 2006 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2006.1655976
• Jesudasan, Rejish, John Doherty, and Simão Marques. 2026. “Enhancing Rapid Drag Analysis for Transonic Aircraft Configuration Trade Studies.” Aerospace Science and Technology 168: 110727. https://doi.org/10.1016/j.ast.2025.110727
• Ji, XunSheng, Shourong Wang, Yishen Xu, Qin Shi, and Dunzhu Xia. 2006. “Application of the Digital Signal Procession in the MEMS Gyroscope De-Drift.” In 2006 1st IEEE International Conference on Nano/Micro Engineered and Molecular Systems. IEEE. https://doi.org/10.1109/nems.2006.334690
• Jia, Jia, Xukai Ding, Zhengcheng Qin, et al. 2021. “Overview and Analysis of MEMS Coriolis Vibratory Ring Gyroscope.” Measurement 182: 109704. https://doi.org/10.1016/j.measurement.2021.109704
• Jia, Yong, Suilao Li, Yongyuan Qin, and Richeng Cheng. 2018. “Error Analysis and Compensation of MEMS Rotation Modulation Inertial Navigation System.” IEEE Sensors Journal 18 (5): 2023–30. https://doi.org/10.1109/jsen.2018.2789884
• Jia, Jichao, Suilao Li, Changshan Zhao, and Rui Long. 2009. “Research on Instrumental Error Compensation of Strap-down Inertial Navigation System.” In 2009 International Asia Conference on Informatics in Control, Automation and Robotics. IEEE. https://doi.org/10.1109/car.2009.30
• Jia, Weichen, Peiqiang Yan, Ascar Shen, and Yanying Feng. 2025. “Closed-Loop Atomic Interferometric Inertial Sensor for Dynamic Measurement.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037051
• Jia, Weichen, Peiqiang Yan, Shengzhe Wang, and Yanying Feng. 2024. “A Dual Atomic Interferometric Inertial Sensor Utilizing Transversely Cooled Atomic Beams.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502115
• Jia, Hui, JianKun Yang, XiuJian Li, et al. 2010. “Systematic Error Analysis and Compensation for High Accuracy Star Centroid Estimation of Star Tracker.” Science China Technological Sciences 53 (11): 3145–52. https://doi.org/10.1007/s11431-010-4129-7
• Jia, Yu, PingHuang Zhou, Yu Peng, Shibo Wang, Haoran Sun, and Ruihua Yang. 2026. “A Gravity-Matching Navigation Algorithm Based on Relative Gravity Changes.” In 2026 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma69663.2026.11647517
• Jia-qiang Xu, Yi-ming Bi, and Guang-yu Zheng. 2010. “Degradation Models of Inertial Platform Based on the Possibility Distribution.” In 2010 International Conference on Intelligent Computing and Integrated Systems. IEEE. https://doi.org/10.1109/iciss.2010.5656083
• Jiali, Yang, and Zhu Jihong. 2015. “Dynamic Modelling of a Small Scale Turbojet Engine.” In 2015 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2015.7330954
• Jian, Wu, Zhang Kun, Chen Lin, and Jin Bo. 2014. “Analytical Redundancy Reconstruction and Redundancy Management for Singular Fault of Normal Accelerometer in FBW System.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007227
• Jian, Zhou, Wang Xin-Min, and Wang Xiao-Yan. 2012. “Automatic Landing Control of UAV Based on Optical Guidance.” In 2012 International Conference on Industrial Control and Electronics Engineering. IEEE. https://doi.org/10.1109/icicee.2012.48
• Jian, Zhou, and Long Xingwu. 2010. “Research on Laser Doppler Velocimeter for Vehicle Self-Contained Inertial Navigation System.” Optics & Laser Technology 42 (3): 477–83. https://doi.org/10.1016/j.optlastec.2009.09.001
• Jian-bo, Sun, Pan Xing-hua, and Zhao Yu-shan. 2017. “Initial Descent Phase Guidance for Hypersonic Glide Vehicle.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028297
• Jianan, Yang, Liu Yong, Han Fei, Feng Qian, and Pan Quan. 2015. “Pico-Satellite Attitude Determination Using a Star Tracker with Compressive Sensing.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260472
• Jianbin Zhang and Yu Zhang. 2012. “Performance Analysis of Three-Axis Inertial Platform Based on ANSYS.” In 2012 7th IEEE Conference on Industrial Electronics and Applications (ICIEA). IEEE. https://doi.org/10.1109/iciea.2012.6361084
• Jiang, Yifu, Zhihong Deng, and Yongqing Zhang. 2025a. “Azimuth Alignment Error Analysis and Process Optimization of Rate-Bias Laser-Gyroscope Inertial Measurement System.” IEEE Sensors Journal 25 (5): 8841–48. https://doi.org/10.1109/jsen.2025.3532257
• Jiang, Yiyao, Guang Feng, Panglun Liu, Li Yuan, Jianbin Ding, and Bingyan Jiang. 2023c. “Evaluation of Joint Clearance Effects on the Shimmy of Nose Landing Gear.” Aerospace 10 (8): 722. https://doi.org/10.3390/aerospace10080722
• Jiang, Yiyao, Guang Feng, Haihong Tang, Jie Zhang, and Bingyan Jiang. 2023b. “Effect of Coulomb Friction on Shimmy of Nose Landing Gear under Time-Varying Load.” Tribology International 188: 108828. https://doi.org/10.1016/j.triboint.2023.108828
• Jiang, Guoqing, and Fengming Li. 2018. “Aerothermoelastic Analysis of Composite Laminated Trapezoidal Panels in Supersonic Airflow.” Composite Structures 200: 313–27. https://doi.org/10.1016/j.compstruct.2018.05.138
• Jiang, Yifu, Sihai Li, Qiangwen Fu, Gongmin Yan, and Bo Xie. 2022b. “Heading-Sensitive Azimuth Error Analysis and Scheme Modification for the Multi-Position Alignment of a Fiber-Optic Gyro Strapdown Inertial Navigation System.” Applied Optics 61 (15): 4259. https://doi.org/10.1364/ao.451199
• Jiang, Xiong, Tao Liu, Jie Duan, and Maosheng Hou. 2024. “Attitude Algorithm of Gyroscope-Free Strapdown Inertial Navigation System Using Kalman Filter.” Micromachines 15 (3): 346. https://doi.org/10.3390/mi15030346
• Jiang, Yao, Qiang Miao, Dewei Wu, Jing He, and Chenhao Zhao. 2026. “GNSS-Denied UAV Terrain Matching Navigation Based on the Autoencoder Network with Contrastive Learning.” Drones 10 (5): 339. https://doi.org/10.3390/drones10050339
• Jiang, Liang, Ying Nan, Yu Zhang, and Zhihan Li. 2022a. “Anti-Interception Guidance for Hypersonic Glide Vehicle: A Deep Reinforcement Learning Approach.” Aerospace 9 (8): 424. https://doi.org/10.3390/aerospace9080424
• Jiang, Junxiang, Xiaoji Niu, Ruonan Guo, and Jingnan Liu. 2019. “A Hybrid Sliding Window Optimizer for Tightly-Coupled Vision-Aided Inertial Navigation System.” Sensors 19 (15): 3418. https://doi.org/10.3390/s19153418
• Jiang, Zhesheng, and Raul Ordonez. 2008. “Robust Approach and Landing Trajectory Generation for Reusable Launch Vehicles in Winds.” In 2008 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2008.4629595
• Jiang, Zhesheng, and Raúl Ordóñez. 2009. “On-Line Robust Trajectory Generation on Approach and Landing for Reusable Launch Vehicles.” Automatica 45 (7): 1668–78. https://doi.org/10.1016/j.automatica.2009.03.017
• Jiang, Yiyao, Jiyong Sun, Sheng Zhong, and Bingyan Jiang. 2025c. “Nose Landing Gear Shimmy Analysis with Variable System Stiffness under Time-Varying Load.” Aerospace 12 (10): 926. https://doi.org/10.3390/aerospace12100926
• Jiang, Deyin, Fangyi Wan, Weimin Cui, Shuhai Jiang, Yajie Han, and Tianyu Chen. 2023d. “Failure Simulation and Reliability Modelling Analysis of Aircraft Drag Parachute Lock System.” In 2023 Prognostics and Health Management Conference (PHM). IEEE. https://doi.org/10.1109/phm58589.2023.00043
• Jiang, Weiping, Li Wang, Xiaoji Niu, et al. 2014. “High-Precision Image Aided Inertial Navigation with Known Features: Observability Analysis and Performance Evaluation.” Sensors 14 (10): 19371–19401. https://doi.org/10.3390/s141019371
• Jiang, Jie, Hao Wang, and Guangjun Zhang. 2018a. “High-Accuracy Synchronous Extraction Algorithm of Star and Celestial Body Features for Optical Navigation Sensor.” IEEE Sensors Journal 18 (2): 713–23. https://doi.org/10.1109/jsen.2017.2777493
• Jiang, Rui, Gongliu Yang, Rui Zou, Jing Wang, and Jing Li. 2017a. “Accurate Compensation of Attitude Angle Error in a Dual-Axis Rotation Inertial Navigation System.” Sensors 17 (3): 615. https://doi.org/10.3390/s17030615
• Jiang, Jie, Wenbo Yu, and Guangjun Zhang. 2017b. “High-Accuracy Decoupling Estimation of the Systematic Coordinate Errors of an INS and Intensified High Dynamic Star Tracker Based on the Constrained Least Squares Method.” Sensors 17 (10): 2285. https://doi.org/10.3390/s17102285
• Jiang, Shuoying, Ziyang Zhen, Ju Jiang, and Zheng Yang. 2018b. “A Preview Control Scheme for Carrier-Based Aircraft Automatic Landing.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483965
• Jiang Cheng Fang and De Jun Wan. 1996. “A Fast Initial Alignment Method for Strapdown Inertial Navigation System on Stationary Base.” IEEE Transactions on Aerospace and Electronic Systems 32 (4): 1501–4. https://doi.org/10.1109/7.543871
• JiangHua, SunYong-Bo, and Ren De-Sheng. 2001. “The Conversion of Different Accuracy Performance Parameters in Navigation System.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984921
• Jianguo, Guo, Wang Guoqing, and Zhou Jun. 2016. “Attitude Control for Reentry Reusable Launch Vehicle.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7532005
• Jianhua, Cheng, Dong Mingtao, and Liu Jiaxin. 2019. “Accuracy Performance Evaluation Method of Integrated Navigation System Based on Two-Level FCE.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866447
• Jianli, Li, and Du Min. 2010. “Fuzzy Modeling and Compensation of Scale Factor for MEMS Gyroscope.” In 2010 International Conference on Digital Manufacturing & Automation. IEEE. https://doi.org/10.1109/icdma.2010.203
• Jianmao, Xu, Zhang Haipeng, and Sun Junzhong. 2007. “Periodic Error Compensation for Quartz MEMS Gyroscope Drift of INS.” Chinese Journal of Aeronautics 20 (6): 539–45. https://doi.org/10.1016/s1000-9361(07)60079-x
• Jianxin, Guo, and Xie Yongcbun. 2004. “Observability Analysis of a Geostationary Satellite Autonomous Navigation System.” IFAC Proceedings Volumes 37 (6): 281–85. https://doi.org/10.1016/s1474-6670(17)32187-0
• Jiao, Xiaoliang, Juntao Chang, Zhongqi Wang, and Daren Yu. 2015. “Mechanism Study on Local Unstart of Hypersonic Inlet at High Mach Number.” AIAA Journal 53 (10): 3102–12. https://doi.org/10.2514/1.j053913
• Jiao, Zhaonan, Shengwu Zhao, Yu Wang, and Zhihong Deng. 2025. “Suitable Matching Area Selection Algorithm Based on Terrain Triangulation Model for Terrain-Aided Inertial Navigation.” IEEE Sensors Journal 25 (17): 33339–49. https://doi.org/10.1109/jsen.2025.3592681
• Jie, Chen, Pan Changpeng, and Gu Wenjin. 2006. “The Pitch Channel Slide Control System Design for Supersonic Cruise Missile.” In 2007 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.4347225
• Jih-Gau Juang, Bo-Shian Lin, and Kuo-Chih Chin. 2005. “Automatic Landing Control Using Particle Swarm Optimization.” In IEEE International Conference on Mechatronics, 2005. ICM ‘05.. IEEE. https://doi.org/10.1109/icmech.2005.1529350
• Jih-Gau Juang and Hao-Hsiang Chang. n.d. “Application of Time Delay Neural Network to Automatic Landing Control.” In Proceedings of the International Conference on Control Applications, vol. 1. IEEE. https://doi.org/10.1109/cca.2002.1040177
• Jin, Sangwook, Hojin Choi, Jong-Ryul Byun, and Gisu Park. 2024. “Combustion Characteristics of a Dual-Mode Ramjet Engine with a Supersonic Aerodynamic Ramp Injector.” Experimental Thermal and Fluid Science 150: 111050. https://doi.org/10.1016/j.expthermflusci.2023.111050
• Jin, Yi, Huijun Tan, Hao Zhang, Gaojie Zheng, Shu Sun, and Yue Zhang. 2023b. “Experimental Investigation on Unstart-Restart Hysteresis of a Supersonic Inlet during Throat Regulation.” Chinese Journal of Aeronautics 36 (11): 135–52. https://doi.org/10.1016/j.cja.2023.08.004
• Jin, Jing, Haiting Tian, Chunxi Zhang, Ningfang Song, and Song Lin. 2010. “Stellar Sensor Based Nonlinear Model Error Filter for Gyroscope Drift Extraction.” Optik 121 (22): 2017–22. https://doi.org/10.1016/j.ijleo.2009.07.003
• Jin, Yi, Xunzhong Wu, Nie Xie, and Bin Yang. 2014. “Closed-Loop Alignment on Strap-down Inertial Navigation.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007315
• Jin, Yuqiang, Wen-An Zhang, and Ling Shi. 2025a. “Learning to Estimate Probabilistic Attitude via Matrix Fisher Distribution with Inertial Sensor.” Information Fusion 119: 103001. https://doi.org/10.1016/j.inffus.2025.103001
• Jing, Ma. 2006. “Adaptive Control of the Aircraft Turbojet Engine Based on the Neural Network.” In 2006 International Conference on Computational Intelligence and Security. IEEE. https://doi.org/10.1109/iccias.2006.294277
• Jing, Chen, Wang Lei, Liu Zengjun, Su Guohua, and Cao Guojie. 2016a. “Calibration and Data Processing Technology of Gyroscope in Dual Axis Rotational Inertial Navigation System.” Microsystem Technologies 23 (8): 3301–9. https://doi.org/10.1007/s00542-016-3171-1
• Jing, Wei, Zhu Xinhua, and Su Yan. 2013. “Design of Micro Inertial Measurement Unit Based on Micromachined Thermal Expansion Gas Gyroscope.” In 2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control. IEEE. https://doi.org/10.1109/imccc.2013.11
• Jing Zhang, Liuqiu You, and Wanchun Chen. 2015. “Boost-Phase Guidance with Neural Network for Interception of Ballistic Missile.” In 2015 International Conference on Control, Automation and Information Sciences (ICCAIS). IEEE. https://doi.org/10.1109/iccais.2015.7338706
• Jingyu Cao, Jianxun Tang, Yu Wang, and Guo Wei. 2011. “Observability Analysis of Four-Position Alignment for Laser Gyroscope Strap-down Inertial Navigation System.” In Proceedings of 2011 International Conference on Electronics and Optoelectronics. IEEE. https://doi.org/10.1109/iceoe.2011.6013345
• Jo, Byeong-Un, and Jaemyung Ahn. 2022. “Optimal Staging of Reusable Launch Vehicles for Minimum Life Cycle Cost.” Aerospace Science and Technology 127: 107703. https://doi.org/10.1016/j.ast.2022.107703
• Jo, Hyunseup, and Sang Won Yoon. 2024. “Visual and Inertial Sensor Fusion Approach for Visual Inertial Odometry Used in Vehicle Localization.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10785070
• Johansen, Tor A., and Thor I. Fossen. 2015. “Nonlinear Observer for Inertial Navigation Aided by Pseudo-Range and Range-Rate Measurements.” In 2015 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2015.7330778
• Johnson, C. 1971. “Accomodation of External Disturbances in Linear Regulator and Servomechanism Problems.” IEEE Transactions on Automatic Control 16 (6): 635–44. https://doi.org/10.1109/tac.1971.1099830
• Johnson, B., K. Christ, D. Endean, et al. 2015. “Tuning Fork MEMS Gyroscope for Precision Northfinding.” In 2015 DGON Inertial Sensors and Systems Symposium (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2015.7314273
• Johnson, Ethan C., and Venkateswaran Narayanaswamy. 2024. “High-Bandwidth Pressure Field Imaging of Stream-Traced Inlet Unstart Dynamics.” AIAA Journal 62 (11): 4494–99. https://doi.org/10.2514/1.j064324
• Johnson, N., W. Tang, and G. Howell. n.d. “Terrain Aided Navigation Using Maximum a Posteriori Estimation.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66215
• Johnston, S. L. 1956. “A Survey of Navigational Measurements Methods for Missile Guidance Systems.” IRE Transactions on Instrumentation PGI-5 (0): 60–65. https://doi.org/10.1109/ire-i.1956.5007003
• Jolly, Olivier, Thomas Kerrien, Steven Fosset, Pierrick Cheiney, Stephanie Michel, and Alexandre Cadu. 2022. “Miniaturized Navigation Grade Quartz Vba Accelerometer for Space Applications.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787528
• Jones, Lim Jen Nee, Rini Akmeliawati, and Chee Pin Tan. 2010. “Automatic Aircraft Landing Control Using Nonlinear Energy Method.” In 2010 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2010.5611294
• Jones, P., E. A. Mickle, and G. D. Swetnam. 1971. “Homing Radar Tracking Accuracy Improvement with Frequency Diversity.” Journal of Spacecraft and Rockets 8 (9): 983–89. https://doi.org/10.2514/3.59757
• Jones, R. A., and C. B. Richie. 1974. “Effect of Wall Temperature Spatial Variations on Aerodynamic Heating to an Actively Cooled Aircraft.” Journal of Aircraft 11. https://ntrs.nasa.gov/citations/19740057119
• Joshi, Ashok. 1996. “Transonic Drag Effect of Single-Stage Space Vehicles.” Journal of Spacecraft and Rockets 33 (2): 308–308. https://doi.org/10.2514/3.55724
• Joshi, Ashok, and C. J. Robin Jiss. 2011. “Measurement-Based Modeling Methodology for Ballistic Missile Trajectory Simulation.” Journal of Spacecraft and Rockets 48 (1): 213–18. https://doi.org/10.2514/1.48666
• Joy, Salna, Siddharth Rajesh, and Vinayak S. Bangarshetar. 2025. “High Precision Star Tracker with Dynamic Post-Calibration Framework.” In 2025 International Conference on Frontier Technologies and Solutions (ICFTS). IEEE. https://doi.org/10.1109/icfts62006.2025.11031717
• Juan, He, He Xiaorong, Liu Shuxi, and Yang Shaorong. 2011. “Robust Networks for Initial Alignment of Strap-down Inertial Navigation Systems.” Energy Procedia 11: 1691–1700. https://doi.org/10.1016/j.egypro.2011.10.449
• Juang, Jih-Gau, and Li-Hsiang Chien. 2008. “Automatic Landing System Using Adaptive Resource Allocating Network.” In 2008 3rd International Conference on Innovative Computing Information and Control. IEEE. https://doi.org/10.1109/icicic.2008.178
• Juang, J.-C., C.-F. Lin, J. R. Cloutier, and J. H. Evers. 1992. “Robust Full-Envelope Missile Autopilot Design.” In [Proceedings 1992] The First IEEE Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.1992.269871
• Juang , Jih-Gau, and Jern-Zuin Chio. 2005. “Fuzzy Modelling Control for Aircraft Automatic Landing System.” International Journal of Systems Science 36 (2): 77–87. https://doi.org/10.1080/0020772042000325961
• Jumper, E. J. 1983. “Wave Drag Prediction Using a Simplified Supersonic Area Rule.” Journal of Aircraft 20 (10): 893–95. https://doi.org/10.2514/3.44961
• Jun, Zhang, Hao Yuncai, Wang Li, and Liu Da. 2015. “Studies on Dynamic Motion Compensation and Positioning Accuracy on Star Tracker.” Applied Optics 54 (28): 8417. https://doi.org/10.1364/ao.54.008417
• Jun Che and Degang Chen. n.d. “Automatic Landing Control Using H/sub ∞/ Control and Stable Inversion.” In Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228). IEEE. https://doi.org/10.1109/.2001.980105
• Jung, Sunghun. 2024. “Precision Landing of Unmanned Aerial Vehicle under Wind Disturbance Using Derivative Sliding Mode Nonlinear Disturbance Observer-Based Control Method.” Aerospace 11 (4): 265. https://doi.org/10.3390/aerospace11040265
• Jung, Roland, Christian Brommer, and Stephan Weiss. 2020. “Decentralized Collaborative State Estimation for Aided Inertial Navigation.” In 2020 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra40945.2020.9197178
• Jung, Yongsu, and Ikjin Lee. 2021. “Optimal Design of Experiments for Optimization-Based Model Calibration Using Fisher Information Matrix.” Reliability Engineering & System Safety 216: 107968. https://doi.org/10.1016/j.ress.2021.107968
• Jung, Roland, and Stephan Weiss. 2021. “Scalable Recursive Distributed Collaborative State Estimation for Aided Inertial Navigation.” In 2021 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra48506.2021.9561203
• Jungen, Daniel, Jan-Frederic Laub, and Alexander Mitsos. 2026. “Optimal Experimental Design for Guaranteed Parameter Estimation with Rigorous Formulation of the Embedded Liquid-Liquid Equilibrium.” Chemical Engineering Science 326: 123437. https://doi.org/10.1016/j.ces.2026.123437
• Junlong, Bai, Chen Wenjie, and Cai Tao. 2013. “Compensation for MEMS Gyroscope Zero Bias Stability.” In 2013 Chinese Automation Congress. IEEE. https://doi.org/10.1109/cac.2013.6775833
• Jurado, Juan, Kenneth Fisher, and Michael Veth. 2012. “Inertial and Imaging Sensor Fusion for Image-Aided Navigation with Affine Distortion Prediction.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236922
• Jwo, Dah-Jing, Ta-Shun Cho, and Birhanu Ayalew Demssie. 2025. “Dynamic Modeling and Its Impact on Estimation Accuracy for GPS Navigation Filters.” Sensors 25 (3): 972. https://doi.org/10.3390/s25030972
• Kada, B. 2011. “Outer-Loop Sliding Mode Control Approach to Longitudinal Autopilot Missile Design.” IFAC Proceedings Volumes 44 (1): 11157–64. https://doi.org/10.3182/20110828-6-it-1002.03818
• Kahraman, Ozgur, and Halil Ersin Soken. 2023. “Incorporating Delayed Star Tracker Measurements in Gokturk-2 Satellite Attitude Filter.” Advances in Space Research 72 (2): 200–210. https://doi.org/10.1016/j.asr.2023.03.005
• Kaicheng Chang and M. P. F. Liang. 2005. “Design and Testing of Dual-Axial Gyroscope.” In 2005 IEEE International Conference on Robotics and Biomimetics - ROBIO. IEEE. https://doi.org/10.1109/robio.2005.246367
• Kaiser, K. 1970. “Temperature Control of the Inertial-Grade Floated Rate-Integrating Gyroscope.” IEEE Transactions on Automatic Control 15 (5): 521–29. https://doi.org/10.1109/tac.1970.1099542
• Kaiser, Jacques, Agostino Martinelli, Flavio Fontana, and Davide Scaramuzza. 2017. “Simultaneous State Initialization and Gyroscope Bias Calibration in Visual Inertial Aided Navigation.” IEEE Robotics and Automation Letters 2 (1): 18–25. https://doi.org/10.1109/lra.2016.2521413
• Kajahusain Abdul Suban. 2007. “Error Analysis of Initial Alignment Method for Inertial Platform Using Kalman Filter Based Fusion Algorithm.” In 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.2007.4391895
• Kaji, Shiori, Ryunosuke Gando, Kei Masunishi, et al. 2020. “A <100 PPB/K Frequency-Matching Temperature Stability MEMS Rate Integrating Gyroscope Enabled by Donut-Mass Structure.” In 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems46641.2020.9056333
• Kajioka, H., N. Ashizuka, T. Kumagai, and H. Nakai. n.d. “Experimental Investigation on Direction Sensor Using a Fiber Optic Gyroscope with High Resolution.” In 8th Optical Fiber Sensors Conference. IEEE. https://doi.org/10.1109/ofs.1992.762954
• Kallinen, Valtteri, Terry Martin, and Aaron McFadyen. 2020. “Required Navigation Performance Specifications for Unmanned Aircraft Based on UTM Flight Trials.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9213980
• Kamali, Soudeh, Dimitri Mavriplis, and Evan Anderson. 2022. “Development and Validation of an Aerothermoelastic Analysis Capability.” AIAA Journal 60 (1): 287–301. https://doi.org/10.2514/1.j060279
• Kamali, C., Amitabh Saraf, and A. A. Pashilkar. 2012. “Online Health Monitoring of Simplex Inertial Navigation System of a High Performance Aircraft.” IFAC Proceedings Volumes 45 (1): 1–6. https://doi.org/10.3182/20120213-3-in-4034.00003
• Kamat, A. R. 1962. “Some More Estimates of Circular Probable Error.” Journal of the American Statistical Association 57 (297): 191–95. https://doi.org/10.1080/01621459.1962.10482161
• Kamer, Y., and S. Ikizoglu. 2013. “Effective Accelerometer Test Beds for Output Enhancement of an Inertial Navigation System.” Measurement 46 (5): 1641–49. https://doi.org/10.1016/j.measurement.2012.12.020
• Kaminer, I., and P. P. Khargonekar. 1990. “Design of the Flare Control Law for Longitudinal Autopilot Using H/sub Infinity / Synthesis.” In 29th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1990.203331
• Kandemir, Gorkem, and Haluk Erdem Bingol. 2017. “Terrain Aided Navigation Application for Airborne Platforms.” In 2017 25th Signal Processing and Communications Applications Conference (SIU). IEEE. https://doi.org/10.1109/siu.2017.7960217
• Kandemir, Gorkem, and Haluk Erdem Bingol. 2018. “A Probabilistic Measurement Method for Terrain Aided Navigation for Airborne Platforms.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373512
• Kang, Donghoon, Cheongjae Jang, and Frank C. Park. 2019. “Unscented Kalman Filtering for Simultaneous Estimation of Attitude and Gyroscope Bias.” IEEE/ASME Transactions on Mechatronics 24 (1): 350–60. https://doi.org/10.1109/tmech.2019.2891776
• Kang, Baowen, Feng Shang, and HaoYi Liu. 2023. “Design of a Four Arm Spiral Antenna for Missile Based Telemetry.” In 2023 IEEE 11th Asia-Pacific Conference on Antennas and Propagation (APCAP). IEEE. https://doi.org/10.1109/apcap59480.2023.10470335
• Kang, Suktae, Kijeong Yoo, Kyungdon Ryu, Sunghyuk Choi, and Jin Seung Lee. 2025. “Performance Evaluation of High-Grade HRG-Based INS with ZUPT & NHC Aiding for Land Vehicle Navigation in GNSS-Denied Environments.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028428
• Kantue, Paulin. 2017. “Design and Flight Testing of a Gain-Scheduled Autopilot Based on Reduced Model Constraints.” IFAC-PapersOnLine 50 (2): 187–92. https://doi.org/10.1016/j.ifacol.2017.12.034
• Karachun, Volodimir, Viktorij Mel’nick, Igor Korobiichuk, Michał Nowicki, Roman Szewczyk, and Svitlana Kobzar. 2016. “The Additional Error of Inertial Sensors Induced by Hypersonic Flight Conditions.” Sensors 16 (3): 299. https://doi.org/10.3390/s16030299
• Karagöz, Ercan, Fatma Yasemin Aşık, Mutlu Gökkavas, et al. 2024. “Reduction in Temperature-Dependent Fiber-Optic Gyroscope Bias Drift by Using Multifunctional Integrated Optical Chip Fabricated on Pre-Annealed LiNbO3.” Photonics 11 (11): 1057. https://doi.org/10.3390/photonics11111057
• Kariminejad, Mohammad Mahdi, Mohammad Ali Sharifi, Mir Abolfazl Mostafavi, and Alireza Amiri-Simkooei. 2026. “Precision and Error Propagation in Static MEMS-IMU Inertial Navigation: A Stochastic Time-Series Analysis.” Sensors 26 (15): 4685. https://doi.org/10.3390/s26154685
• Karlsson, Johan, Milena Anguelova, and Mats Jirstrand. 2012. “An Efficient Method for Structural Identifiability Analysis of Large Dynamic Systems.” IFAC Proceedings Volumes 45 (16): 941–46. https://doi.org/10.3182/20120711-3-be-2027.00381
• Karwacki, F. A., M. Shishkov, Z. Hasan, M. Sanzari, and Hong-Ling Cui. 1998. “Optical Biasing of a Ring Laser Gyroscope with a Quantum Well Mirror.” In IEEE 1998 Position Location and Navigation Symposium (Cat. No.98CH36153). IEEE. https://doi.org/10.1109/plans.1998.670037
• Kashwani, Fatima, Bilal Hassan, Majid Khonji, and Jorge Dias. 2023. “Collision-Free Path Generation for Teleoperation of Unmanned Vehicles.” In 2023 21st International Conference on Advanced Robotics (ICAR). IEEE. https://doi.org/10.1109/icar58858.2023.10406579
• Kasouf, G., and D. Weiss. 1984. “An Integrated Missile Reliability Growth Program.” In Annual Reliability and Maintainability Symposium, 1984. Proceedings.. IEEE. https://doi.org/10.1109/rams.1984.764336
• Kasper, Joseph, and Raymond Nash. 1975. “Doppler Radar Error Equations for Damped Inertial Navigation System Analysis.” IEEE Transactions on Aerospace and Electronic Systems AES-11 (4): 600–607. https://doi.org/10.1109/taes.1975.308125
• Kaswekar, P., and J. F. Wagner. 2015. “Sensor Fusion Based Vibration Estimation Using Inertial Sensors for a Complex Lightweight Structure.” In 2015 DGON Inertial Sensors and Systems Symposium (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2015.7314265
• Kato, Hajime, Hirobumi Saito, and Sin-ichiro Sakai. 2010. “Shupe Effect Compensation of Temperature Controlled Fiber Optical Gyroscope.” In 2010 11th IEEE International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2010.5463990
• Katolicky, Zdenek, Bohuslav Busov, and Milada Bartlova. 2014. “Turbojet Engine Innovation and TRIZ.” In Proceedings of the 16th International Conference on Mechatronics - Mechatronika 2014. IEEE. https://doi.org/10.1109/mechatronika.2014.7018230
• Kau, S., and S. Steadman. 1976. “Update Strategy for a Strapdown Stellar-Inertial Navigation System.” In 1976 IEEE Conference on Decision and Control including the 15th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1976.267704
• Kaya, Tarik. 1998. “Influence of Inlet Pressure Distortion on a Convertible Engine Fan.” Journal of Propulsion and Power 14 (1): 82–89. https://doi.org/10.2514/2.5253
• Kaya, Onurcan, Talha Kose, and Kivanc Azgin. 2019. “Integrated Temperature Sensor for Temperature Compensation of Inertial Sensors.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739559
• Kaye, Joseph, and Victor C. M. Yeh. 1955. “Design Charts for Transient Temperature Distribution Resulting from Aerodynamic Heating at Supersonic Speeds.” Journal of the Aeronautical Sciences 22 (11): 755–62. https://doi.org/10.2514/8.3454
• Kazel, S., and J. N. Faraone. 1961. “Improvement in Tracking Accuracy of Pulse Radar by Coherent Techniques.” IRE Transactions on Military Electronics MIL-5 (4): 286–93. https://doi.org/10.1109/iret-mil.1961.5008369
• Kazemi, Laila, and John Enright. 2019. “Accurate Star Tracker Simulation with on-Orbit Data Verification.” In 2019 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2019.8741999
• Kazemi, Laila, John Enright, and Tom Dzamba. 2015. “Improving Star Tracker Centroiding Performance in Dynamic Imaging Conditions.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119226
• Ke, Long Shi, and Li Hui Feng. 2015. “A New Online Trajectory Generation Solution for Reusable Launch Vehicles during Approach and Landing.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260494
• Ke, Lu, Wang Zhengzhong, and Yuan Suozhong. 2014. “Automatic Landing on Carrier Method of Unmanned Air Vehicle.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007248
• Ke, Zhaorong, Yi Zhou, Peng Sun, Xi Wang, Tong Zhou, and Yan Su. 2025. “3.54-Million Q-Factor Micro Hemispherical Resonator Gyroscope with Segmented Displacement Startup.” In 2025 IEEE 20th International Conference on Nano/Micro Engineered and Molecular Systems (NEMS). IEEE. https://doi.org/10.1109/nems67320.2025.11170014
• Kedong, Wang, and Yong Yang. 2010. “Influence of Application Conditions on Terrain-Aided Navigation.” In 2010 8th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2010.5555067
• Keesman, Karel J. 2015. “Optimal Input Design for Parameter Estimation in Nonlinear State-Space Models Using Pontryagin’s Minimum Principle.” IFAC-PapersOnLine 48 (28): 1319–24. https://doi.org/10.1016/j.ifacol.2015.12.314
• Kelly, Patrick, Manoranjan Majji, and Felipe Guzmán. 2021. “Estimation and Error Analysis for Optomechanical Inertial Sensors.” Sensors 21 (18): 6101. https://doi.org/10.3390/s21186101
• Kelly, Jonathan, and Gaurav S. Sukhatme. 2009. “Visual-Inertial Simultaneous Localization, Mapping and Sensor-to-Sensor Self-Calibration.” In 2009 IEEE International Symposium on Computational Intelligence in Robotics and Automation - (CIRA). IEEE. https://doi.org/10.1109/cira.2009.5423178
• Kendall, P. J., and J. I. Gonzalez. 1965. “An Analytical Model for Predicting Thermal Response in Honeycomb Sandwich Panels.” Journal of Aircraft 2 (6): 551–53. https://doi.org/10.2514/3.43696
• Kendoul, Farid, and Bilal Ahmed. 2012. “Bio-Inspired TauPilot for Automated Aerial 4D Docking and Landing of Unmanned Aircraft Systems.” In 2012 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2012.6385586
• Kerr, Thomas H. 2007. “Comment on �Precision Free-Inertial Navigation with Gravity Compensation by an Onboard Gradiometer�.” Journal of Guidance, Control, and Dynamics 30 (4): 1214–15. https://doi.org/10.2514/1.29808
• Khalifa, Mohamed, and Hashim A. Hashim. 2026. “Dual Quaternion-Based Unscented Kalman Filter with Visual Inertial Odometry for Navigation in GPS-Denied Environments.” Measurement 283: 121964. https://doi.org/10.1016/j.measurement.2026.121964
• Khodadadi, Hamed, Mohammad Reza Jahed Motlagh, and Mohammad Gorji. 2011. “Robust Control and Modeling a 2-DOF Inertial Stabilized Platform.” In International Conference on Electrical, Control and Computer Engineering 2011 (InECCE). IEEE. https://doi.org/10.1109/inecce.2011.5953880
• Kiehn, Daniel. 2020. “Stability Analysis and Flight Control Design of the Winged Reusable Launch Vehicle ReFEx.” CEAS Space Journal 13 (1): 51–64. https://doi.org/10.1007/s12567-020-00319-3
• Killian, K. 1994a. “Pointing Grade Fiber Optic Gyroscope.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303310
• Killian, K. M. 1994b. “Pointing Grade Fiber Optic Gyroscope.” IEEE Aerospace and Electronic Systems Magazine 9 (7): 6–10. https://doi.org/10.1109/62.295115
• Kim, Sang Dug. 2009. “Aerodynamic Design of a Supersonic Inlet with a Parametric Bump.” Journal of Aircraft 46 (1): 198–202. https://doi.org/10.2514/1.37416
• Kim, Cheonjoong, Juneon An, Haesung Yu, Inseop Lee, and JunMin Park. 2026a. “Amplitude Enhancement Methods of the Cluster Dither in a Ring Laser Gyro Based Inertial Measurement Unit.” In 2026 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial69196.2026.11557658
• Kim, Dennis, Amir Behbahani, Robert M’closkey, Phil Stupar, and Jeffrey Denatale. 2015b. “Wafer-Scale Etch Process for Precision Frequency Tuning of MEMS Gyros.” In 2015 IEEE International Symposium on Inertial Sensors and Systems (ISISS) Proceedings. IEEE. https://doi.org/10.1109/isiss.2015.7102391
• Kim, Myeongseop, Bobae Cho, Hansol Lee, Taeil Yoon, and Byeongha Lee. 2022b. “Implementation of Hemispherical Resonator Gyroscope with 3 × 3 Optical Interferometers for Analysis of Resonator Asymmetry.” Sensors 22 (5): 1971. https://doi.org/10.3390/s22051971
• Kim, Hyun-Seung, Ju-Hyeon Hong, Woo-sung Park, and Chang-Kyung Ryoo. 2015a. “Satellite Celestial Navigation Using Star-Tracker and Earth Sensor.” In 2015 15th International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.1109/iccas.2015.7364961
• Kim, Eung Ju, Yong Hun Kim, Joo Han Lee, So Jin Park, Jin Woo Song, and So Young Park. 2022a. “Gyroscope Bias Estimation Method Using Iterated State Transition Fusion Algorithm.” In 2022 13th Asian Control Conference (ASCC). IEEE. https://doi.org/10.23919/ascc56756.2022.9828294
• Kim, Seung-Hwan, Yoon-Sik Kim, and Chanho Song. 2004c. “A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design.” Control Engineering Practice 12 (2): 149–54. https://doi.org/10.1016/s0967-0661(03)00016-9
• Kim, Jinseong, Gunwoo Lee, Hyunseok Choi, Younghun Heo, and Sangmoon Lee. 2026c. “Rapid Indirect Diagnosis of MEMS Gyroscope Initial Bias with on-Board Capability for Guided Missiles.” IEEE Transactions on Aerospace and Electronic Systems 62: 10223–33. https://doi.org/10.1109/taes.2026.3687822
• Kim, Taeyun, Seongho Nam, Hyungsub Lee, and Juhyun Oh. 2025b. “Verification of Vision-Based Terrain-Referenced Navigation Using the Iterative Closest Point Algorithm through Flight Testing.” Sensors 25 (18): 5813. https://doi.org/10.3390/s25185813
• Kim, Yongchan, Junyeop Nam, Tae-Seong Roh, and Hyoung Jin Lee. 2023a. “Base Flow and Drag Characteristics of a Supersonic Vehicle with Cold and Hot Jet Flows of Nozzles.” Aerospace 10 (10): 836. https://doi.org/10.3390/aerospace10100836
• Kim, Kwangjin, and Chan Gook Park. 2008. “A New Initial Alignment Algorithm for Strapdown Inertial Navigation System Using Sensor Output.” IFAC Proceedings Volumes 41 (2): 13034–39. https://doi.org/10.3182/20080706-5-kr-1001.02204
• Kim, Heyone, Jae-Hoon Son, Sang-Heon Oh, and Dong-Hwan Hwang. 2023d. “Note on Coarse Alignment of Gyro-Free Inertial Navigation System.” Sensors 23 (12): 5763. https://doi.org/10.3390/s23125763
• Kim, Seung-Hwan, and Chanho Song. 1998. “A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design.” IFAC Proceedings Volumes 31 (21): 49–52. https://doi.org/10.1016/s1474-6670(17)41057-3
• Kim, Jong-Han, Ick Ho Whang, and Boo Min Kim. 2016. “Finite Horizon Integrated Guidance and Control for Terminal Homing in Vertical Plane.” Journal of Guidance, Control, and Dynamics 39 (5): 1104–12. https://doi.org/10.2514/1.g001699
• Kimishima, Masato, Tsutomu Sawada, Akihiro Sonoura, Toru Amano, Hiroyuki Kamata, and Kosei Yamashita. 2023. “Highly Accurate Inertial Navigation That Compensates for the Earth’s Rotation and Sensor BIAS Using Non-Holonomic Constraints.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10103969
• Kimmel, Elliot S., Daning Huang, Vansh Sharma, Jagmohan Singh, Venkat Raman, and Peretz P. Friedmann. 2026. “Reduced-Order Modeling of Turbulent Flows for High-Speed Aerothermoelastic Analysis.” AIAA Journal 64 (4): 2230–52. https://doi.org/10.2514/1.j065721
• Kirnos, Vasilii, Aleksander Vagachev, and Oleg Morozov. 2020. “Micro-Machined Vibrating Ring Gyroscope Testing.” In 2020 26th Conference of Open Innovations Association (FRUCT). IEEE. https://doi.org/10.23919/fruct48808.2020.9087387
• Kishi, Yuki, Risato Yashiro, and Masahiro Kanazaki. 2023. “Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method.” Aerospace 10 (8): 717. https://doi.org/10.3390/aerospace10080717
• Kistyarev, Mikhail, and Xinhua Wang. 2025. “Unmanned F/A-18 Aircraft Landing Control on Aircraft Carrier in Adverse Conditions.” Aerotecnica Missili & Spazio 104 (6): 475–86. https://doi.org/10.1007/s42496-025-00249-5
• Kitamura, Shinzo, and Shin-ichi Nakagiri. 1977a. “Identifiability of Internal and Boundary Parameters in Distributed Systems of Parabolic Type.” IFAC Proceedings Volumes 10 (5): 381–92. https://doi.org/10.1016/s1474-6670(17)66972-6
• Kitsios, I., and J. Lygeros. n.d. “Final Glide-Back Envelope Computation for Reusable Launch Vehicle Using Reachability.” In Proceedings of the 44th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2005.1582797
• Klein, Dominik, and Chamil Abeykoon. 2015. “Modelling of a Turbojet Gas Turbine Engine.” In 2015 Internet Technologies and Applications (ITA). IEEE. https://doi.org/10.1109/itecha.2015.7317395
• Klein, V., and E. A. Morelli. 1992. “Parameter Estimation of a Highly Augmented Aircraft from Flight Data.” IFAC Proceedings Volumes 25 (15): 181–86. https://doi.org/10.1016/s1474-6670(17)50630-8
• Kleinert, Markus, and Sebastian Schleith. 2010. “Inertial Aided Monocular SLAM for GPS-Denied Navigation.” In 2010 IEEE Conference on Multisensor Fusion and Integration. IEEE. https://doi.org/10.1109/mfi.2010.5604453
• Kleinert, Markus, and Uwe Stilla. 2013. “A Sensor-Centric EKF for Inertial-Aided Visual Odometry.” In International Conference on Indoor Positioning and Indoor Navigation. IEEE. https://doi.org/10.1109/ipin.2013.6817915
• Kline, M. H., Y.-C. Yeh, B. Eminoglu, et al. 2013. “MEMS Gyroscope Bias Drift Cancellation Using Continuous-Time Mode Reversal.” In 2013 Transducers & Eurosensors XXVII: The 17th International Conference on Solid-State Sensors, Actuators and Microsystems (TRANSDUCERS & EUROSENSORS XXVII). IEEE. https://doi.org/10.1109/transducers.2013.6627152
• Kluever, C. A. 2007. “Terminal Guidance for an Unpowered Reusable Launch Vehicle with Bank Constraints.” Journal of Guidance, Control, and Dynamics 30 (1): 162–68. https://doi.org/10.2514/1.24864
• Kluever, Craig A. 2022. “Simple Analytical Terminal Area Guidance for an Unpowered Reusable Launch Vehicle.” Journal of Guidance, Control, and Dynamics 45 (4): 740–47. https://doi.org/10.2514/1.g006338
• Kluever, Craig A., and David A. Neal. 2015. “Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle.” Journal of Guidance, Control, and Dynamics 38 (11): 2057–66. https://doi.org/10.2514/1.g000909
• Kobayashi, Toshihiro. 1980. “Parameter Identifiability for Distributed Parameter Systems of Hyperbolic Type.” International Journal of Systems Science 11 (2): 247–59. https://doi.org/10.1080/00207728008967011
• Kocak, S., and A. F. Ergenc. 2023. “Damping of the Shimmy Behavior in Nose Landing Gear System via PIR Controller.” In 2023 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc57647.2023.10178363
• Koelle, Dietrich E. 1993. “Cost Analysis for Single-Stage (SSTO) Reusable Ballistic Launch Vehicles.” Acta Astronautica 30: 415–21. https://doi.org/10.1016/0094-5765(93)90132-g
• Koelle, D. E. 2000. “The Cost-Optimal Size of Future Reusable Launch Vehicles.” Acta Astronautica 47 (2–9): 205–13. https://doi.org/10.1016/s0094-5765(00)00060-6
• Koenig, S., S. Rombach, W. Gutmann, et al. 2019. “Towards a Navigation Grade Si-MEMS Gyroscope.” In 2019 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss46986.2019.8943770
• Koifman, M., and I. Y. Bar-Itzhack. 1999. “Inertial Navigation System Aided by Aircraft Dynamics.” IEEE Transactions on Control Systems Technology 7 (4): 487–93. https://doi.org/10.1109/87.772164
• Kollodge, J. C., and J. A. Sand. 1984. “Advanced Star Tracker Design Using the Charge Injection Device.” Automatica 20 (6): 787–91. https://doi.org/10.1016/0005-1098(84)90087-6
• Kolumbán, Sándor, and Balázs Csanád Csáji. 2018. “Towards D-Optimal Input Design for Finite-Sample System Identification.” IFAC-PapersOnLine 51 (15): 215–20. https://doi.org/10.1016/j.ifacol.2018.09.136
• Konigseder, F., W. Kemmetmuller, and A. Kugi. 2016. “Attitude Estimation Using Redundant Inertial Measurement Units for the Control of a Camera Stabilization Platform.” IEEE Transactions on Control Systems Technology 24 (5): 1837–44. https://doi.org/10.1109/tcst.2015.2510324
• Koppe, Enrico, Daniel Augustin, Achim Liers, and Jochen Schiller. 2014. “Self-Calibration-Method for an Inertial Navigation System with Three 3D Sensors.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782522
• Kordos, Damian, Paweł Krzaczkowski, Paweł Rzucidło, Zbigniew Gomółka, Ewa Zesławska, and Bogusław Twaróg. 2023. “Vision System Measuring the Position of an Aircraft in Relation to the Runway during Landing Approach.” Sensors 23 (3): 1560. https://doi.org/10.3390/s23031560
• Korobiichuk, Igor, Viktorij Mel’Nick, Nonna Gnateiko, and Galyna Boiko. 2022. “The Additional Error Emergence of Inertial Sensors in the Operational Conditions of Hypersonic Flight.” In 2022 IEEE 11th International Conference on Intelligent Systems (IS). IEEE. https://doi.org/10.1109/is57118.2022.10019695
• Kou, Kunhu, Bin Li, and Daquan Tang. 2014. “An INS Error Estimation Method Based on Passive Observation to Single Feature Target for Cruise Missile.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007558
• Kouba, James T., and Lemuel W. Mason. 1962. “Gyrocompass Alignment of an Inertial Platform to Arbitrary Attitudes.” ARS Journal 32 (7): 1029–33. https://doi.org/10.2514/8.6197
• Kourepenis, A., A. Petrovich, and M. Weinberg. 1991. “Low Cost Quartz Resonant Accelerometer for Aircraft Inertial Navigation.” In TRANSDUCERS ‘91: 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers. IEEE. https://doi.org/10.1109/sensor.1991.148935
• Kowal, B. W. 2000. “A Variable Structure Control System for the Propulsion Controlled Automatic Landing of a Contemporary Large Transport Aircraft.” In Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093). IEEE. https://doi.org/10.1109/naecon.2000.894909
• Kozlov, Alexander, Sergey Fedorov, and Fedor Kapralov. 2026. “Empirical Long-Term Stability of Industrial-Grade STM ISM330DHCX MEMS Inertial Sensor Calibration Parameters.” IEEE Sensors Letters 10 (1): 1–4. https://doi.org/10.1109/lsens.2025.3641436
• Kozlov, A., F. Kapralov, and A. Fomichev. 2019. “Calibration of a Timing Skew between Gyroscope Measurements in a Strapdown Inertial Navigation System.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769417
• Krabacher, William E. 1996a. “A Comparison of the Moreland and Von Schlippe-Dietrich Landing Gear Tire Shimmy Models.” Vehicle System Dynamics 27: 335–38. https://doi.org/10.1080/00423119608969667
• Krabacher, William E. 1997. “A Comparison of the Moreland and Von Schlippe-Dietrich Landing Gear Tire Shimmy Models.” Vehicle System Dynamics 27 (sup001): 335–38. https://doi.org/10.1080/00423119708969667
• Krieger, Robert J. 1983. “Supersonic Missile Aerodynamic and Performance Relationships for Long Range Mission Profiles.” In 1983 American Control Conference. IEEE. https://doi.org/10.23919/acc.1983.4788274
• Krishnan, V., and K. Grobert. 1970. “Initial Alignment of a Gimballess Inertial Navigation System.” IEEE Transactions on Automatic Control 15 (6): 667–71. https://doi.org/10.1109/tac.1970.1099597
• Krishnaswamy, Kailash, Sara Susca, Rob McCroskey, et al. 2008. “Sensor Fusion for GNSS Denied Navigation.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570062
• KrÜGer, W., I. Besselink, D. Cowling, D. B. Doan, W. KortÜM, and W. Krabacher. 1997. “Aircraft Landing Gear Dynamics: Simulation and Control.” Vehicle System Dynamics 28 (2–3): 119–58. https://doi.org/10.1080/00423119708969352
• Krüger, Wolf R., and Marco Morandini. 2011. “Recent Developments at the Numerical Simulation of Landing Gear Dynamics.” CEAS Aeronautical Journal 1 (1–4): 55–68. https://doi.org/10.1007/s13272-011-0003-y
• Kuang, Yunbin, Zhanqiang Hou, Dunxiang Jian, et al. 2022. “Research on the Temperature-Dependent Bias Instability Improvement of Mems Butterfly Gyroscope Based on Real-Time Demodulation Phase Compensation.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.4161323
• Kuang, Yunbin, Zhanqiang Hou, Gao Liu, Dingbang Xiao, and Xuezhong Wu. 2023. “Real-Time Phase Compensation for Scale Factor Nonlinearity Improvement over Temperature Variations for MEMS Gyroscope.” Journal of Microelectromechanical Systems 32 (4): 305–13. https://doi.org/10.1109/jmems.2023.3279653
• Kuba, R., and L. Kazda. 1958. “The Design and Performance of a Model, Second-Order, Nonlinear Servomechanism.” IRE Transactions on Automatic Control 5 (1): 43–48. https://doi.org/10.1109/tac.1958.1104980
• Kucherov, Alexander, and Vladimir Kurenkov. 2017. “Use of Cluster Analysis for Development of Star Tracker Mass Statistical Model.” Procedia Engineering 185: 227–30. https://doi.org/10.1016/j.proeng.2017.03.304
• Kugler, Martin E., and Florian Holzapfel. 2017. “Online Self-Monitoring of Automatic Take-off and Landing Control of a Fixed-Wing UAV.” In 2017 IEEE Conference on Control Technology and Applications (CCTA). IEEE. https://doi.org/10.1109/ccta.2017.8062764
• Kuhn, T. 2004. “Aspects of Pure and Satellite-Aided Inertial Navigation for Gun-Launched Munitions.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1309013
• Kulfan, Brenda. 2009. “New Supersonic Wing Far-Field Composite-Element Wave-Drag Optimization Method.” Journal of Aircraft 46 (5): 1740–58. https://doi.org/10.2514/1.42823
• Kulikov, Roman, Oleg Denisenko, Igor Merkuryev, and Oleg Glukhov. 2022. “Modeling the Influence of Time Scale Instability on Inertial Navigation Error.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815338
• Kumar, Prem, Prashant G. Bhale, Abhijit Bhattacharyya, and Radhakant Padhi. 2016. “Gimbal Angle Bias Free State Estimator for Anti-Ballistic Missile Using Additional Accelerometers.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7526067
• Kumar, G. Naresh, D. Penchalaiah, A. K. Sarkar, and S. E. Talole. 2018. “Hypersonic Boost Glide Vehicle Trajectory Optimization Using Genetic Algorithm.” IFAC-PapersOnLine 51 (1): 118–23. https://doi.org/10.1016/j.ifacol.2018.05.020
• Kumar, Ankit, Raina Raj, Dharmaraja Selvamuthu, and Sufal Chandra Swar. 2026. “Reliability and Maintainability Analysis of Unmanned Aerial Vehicle under Varied Environmental Conditions.” Reliability Engineering & System Safety 275: 112826. https://doi.org/10.1016/j.ress.2026.112826
• Kumar, Shashi Ranjan, Sachit Rao, and Debasish Ghose. 2012. “Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints.” Journal of Guidance, Control, and Dynamics 35 (4): 1230–46. https://doi.org/10.2514/1.55242
• Kumar, S. Varun, P. V. Yokeshraj, and R. Kotteeswaran. 2019. “Optimized Inertial Navigation System with Kalman Filter Based Altitude Determination for Aircraft in GPS Deprived Regions.” In 2019 3rd International Conference on Computing Methodologies and Communication (ICCMC). IEEE. https://doi.org/10.1109/iccmc.2019.8819646
• Kunisch, K., and L. White. 1991. “Stability and Identifiability of Parameters in Galerkin Approximation of Distributed Systems under Multiple Inputs.” Optimal Control Applications and Methods 12 (1): 63–71. https://doi.org/10.1002/oca.4660120106
• Kunpeng He, Jitao Han, and Yuping Shao. 2013. “A Novel Redundant Inertial Measurement Unit and Calibration Algorithm.” In 2013 International Conference on Optoelectronics and Microelectronics (ICOM). IEEE. https://doi.org/10.1109/icoom.2013.6626481
• Kurilova, Marina, and Howard Li. 2026. “Time-Frequency Wavelet Transformer Forecasting for Hypersonic Glide Vehicle Trajectory Prediction.” In 2026 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero66936.2026.11519972
• Kuroswiski, André Rossi, Neusa Maria Franco de Oliveira, and Élcio Hideiti Shiguemori. 2018. “Autonomous Long-Range Navigation in GNSS-Denied Environment with Low-Cost UAV Platform.” In 2018 Annual IEEE International Systems Conference (SysCon). IEEE. https://doi.org/10.1109/syscon.2018.8369592
• Kuznetsov, Ivan M., Konstantin K. Veremeenko, Maxim V. Zharkov, and Andrey N. Pronkin. 2023. “Using Functionally Redundant Inertial Measurement Units to Increase Reliability and Ensure Fault Tolerance.” Inventions 8 (6): 159. https://doi.org/10.3390/inventions8060159
• Kwon, Hyukjin, Seyeong Seok, and Geunbae Lim. 2017. “System Modeling of a MEMS Vibratory Gyroscope and Integration to Circuit Simulation.” Sensors 17 (11): 2663. https://doi.org/10.3390/s17112663
• LaBatte, J. J. 1964. “400 Cycle to 400 Cycle Buffer Power Supply for Inertial Guidance System.” IEEE Transactions on Aerospace 2 (2): 1006–12. https://doi.org/10.1109/ta.1964.4319692
• Labowski, Michal, Piotr Kaniewski, and Piotr Serafin. 2016. “Inertial Navigation System for Radar Terrain Imaging.” In 2016 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2016.7479792
• Lacambre, Jean-Baptiste, Michel Narozny, and Jean-Marie Louge. 2013. “Limitations of the Unscented Kalman Filter for the Attitude Determination on an Inertial Navigation System.” In 2013 IEEE Digital Signal Processing and Signal Processing Education Meeting (DSP/SPE). IEEE. https://doi.org/10.1109/dsp-spe.2013.6642588
• Lagerstrom, P. A., and M. E. Graham. 1951. “Remarks on Low-Aspect-Ratio Configurations in Supersonic Flow.” Journal of the Aeronautical Sciences 18 (2): 91–96. https://doi.org/10.2514/8.1864
• Lai, Zhongyi, Zhengyu Chen, Xuelei Wang, Jianli Li, and Rui Feng. 2026. “A Novel Estimation Technique for Bias Magnetic Field in NMR Gyroscope Based on Nonlinear Disturbance Observer.” Measurement 257: 119004. https://doi.org/10.1016/j.measurement.2025.119004
• Lai, Yuwang, Defeng Gu, Junhong Liu, Wenping Li, and Dongyun Yi. 2016. “Low-Frequency Error Extraction and Compensation for Attitude Measurements from STECE Star Tracker.” Sensors 16 (10): 1669. https://doi.org/10.3390/s16101669
• Lai, Yuwang, Junhong Liu, Yonghe Ding, Defeng Gu, and Dongyun Yi. 2014b. “In-Flight Quality Evaluation of Attitude Measurements from STECE APS-01 Star Tracker.” Acta Astronautica 102: 207–16. https://doi.org/10.1016/j.actaastro.2014.06.009
• Laita, Gabriele, Andrea Buffoli, Philippe Robert, and Giacomo Langfelder. 2024. “Origin and Compensation of Nonlinearity in near-Navigation Grade Piezoresistive MEMS Gyroscope.” IEEE Sensors Journal 24 (21): 34162–69. https://doi.org/10.1109/jsen.2024.3462598
• Lambert, Walter D., and Frederic W. Darling. 1938. “Formulas and Tables for the Deflection of the Vertical.” Bulletin Géodésique 57 (1): 29–71. https://doi.org/10.1007/bf03029856
• Lambrecht, Stefan, Samuel Nogueira, Magdo Bortole, et al. 2016. “Inertial Sensor Error Reduction through Calibration and Sensor Fusion.” Sensors 16 (2): 235. https://doi.org/10.3390/s16020235
• Lamorte, Nicolas, and Peretz P. Friedmann. 2014. “Hypersonic Aeroelastic and Aerothermoelastic Studies Using Computational Fluid Dynamics.” AIAA Journal 52 (9): 2062–78. https://doi.org/10.2514/1.j053018
• Lamorte, Nicolas, Peretz P. Friedmann, Bryan Glaz, Adam J. Culler, Andrew R. Crowell, and Jack J. McNamara. 2014. “Uncertainty Propagation in Hypersonic Aerothermoelastic Analysis.” Journal of Aircraft 51 (1): 192–203. https://doi.org/10.2514/1.c032233
• Lamy Au Rousseau, G., J. Bostel, and B. Mazari. 2005. “Star Recognition Algorithm for APS Star Tracker: Oriented Triangles.” IEEE Aerospace and Electronic Systems Magazine 20 (2): 27–31. https://doi.org/10.1109/maes.2005.1397146
• Lan, Haoze, and Yingjie Xu. 2026. “Data-Driven Fusion Algorithms for Temperature-Drift Compensation of MEMS Gyroscopes: A Mini Review.” Micromachines 17 (8): 924. https://doi.org/10.3390/mi17080924
• Lancelle, D., O. Bozic, and H. Koke. 2012. “Flight Test Results of Investigation of Acceleration Effects on a Gun Launched Rocket Engine.” In 2012 16th International Symposium on Electromagnetic Launch Technology. IEEE. https://doi.org/10.1109/eml.2012.6325034
• Lantagne, R., J. Grady, and G. Miller. 1979. “Air Launch Cruise Missile Instrumentation Antennas.” In 1979 Antennas and Propagation Society International Symposium, vol. 17. Institute of Electrical and Electronics Engineers. https://doi.org/10.1109/aps.1979.1148030
• Larin, V. B., and A. A. Tunik. 2012b. “On Inertial Navigation System Error Correction.” International Applied Mechanics 48 (2): 213–23. https://doi.org/10.1007/s10778-012-0517-y
• Larsen, Michael, and Michael Bulatowicz. 2014. “Nuclear Magnetic Resonance Gyroscope: For DARPA’s Micro-Technology for Positioning, Navigation and Timing Program.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782506
• Larsson, Christian A., Mariette Annergren, and Hakan Hjalmarsson. 2011. “On Optimal Input Design in System Identification for Model Predictive Control.” In IEEE Conference on Decision and Control and European Control Conference. IEEE. https://doi.org/10.1109/cdc.2011.6161156
• Lashley, M., J. Y. Hung, D. Lawrence, and L. T. Lowe. 2006. “Split-Gate Tracking Accuracy for Phase Coded CW Radar.” In 2006 IEEE Conference on Radar. IEEE. https://doi.org/10.1109/radar.2006.1631811
• Latif, A., J. Masud, S. R. Sheikh, and K. Pervez. 2007. “Robust Design of an Aerodynamic Compensation Pitot-Static Tube for Supersonic Aircraft.” Journal of Aircraft 44 (1): 163–69. https://doi.org/10.2514/1.22775
• Laube, Tomasz, and Janusz Piechna. 2019. “Analytical and Numerical Feasibility Analysis of a Contra-Rotary Ramjet Engine.” Energies 13 (1): 163. https://doi.org/10.3390/en13010163
• LaViolette, K. D., and F. B. Bossler. n.d. “Phase Modulation Control for an Interferometric Fiber Optic Gyroscope.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66152
• Lawrence, H. R. 1953. “The Aerodynamic Characteristics of Low Aspect Ratio Wing-Body Combinations in Steady Subsonic Flow.” Journal of the Aeronautical Sciences 20 (8): 541–48. https://doi.org/10.2514/8.2724
• Lawrence, P. J., and M. P. Berarducci. n.d. “Navigation Sensor, Filter, and Failure Mode Simulation Results Using the Distributed Kalman Filter Simulator (DKFSIM).” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509147
• Le, Wenxin, Hanyu Liu, Ruiyuan Zhao, and Jian Chen. 2023. “Attitude Control of a Hypersonic Glide Vehicle Based on Reduced-Order Modeling and NESO-Assisted Backstepping Variable Structure Control.” Drones 7 (2): 119. https://doi.org/10.3390/drones7020119
• Le Bras, Florent, Tarek Hamel, Christian Barat, and Robert Mahony. 2009. “Nonlinear Image-Based Visual Servo Controller for Automatic Landing Guidance of a Fixed-Wing Aircraft.” In 2009 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2009.7074670
• Le Traon, O., J. Guerard, M. Pernice, et al. 2018. “The NG DIVA: A Navigation Grade Differential Inertial Vibrating Beam Accelerometer.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373360
• Leavitt, L. E., and B. L. Peters. n.d. “Low Cost High Accuracy Integrated GPS-Inertial Navigator for Reconnaissance Missions.” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195509
• Lebell, D. 1956. “Nonlinear Compensation of an Aircraft Instrument Servomechanism by Analog Simulation.” IRE Transactions on Automatic Control 1 (1): 10–18. https://doi.org/10.1109/tac.1956.1100816
• Lebsock, K. L. 1980. “High Pointing Accuracy with a Momentum Bias Attitude Control System.” Journal of Guidance and Control 3 (3): 195–202. https://doi.org/10.2514/3.55972
• Lee, Bernard. 1976a. “Integrated Inertial Reference: Inertial Navigation System.” Journal of Aircraft 13 (7): 449–53. https://doi.org/10.2514/3.58677
• Lee, Hsing-Juin, and Cheng-Yi Chiou. 1994. “Aircraft Landing Gear Positioning Concerning Abnormal Landing Cases.” Journal of Aircraft 31 (2): 446–49. https://doi.org/10.2514/3.46508
• Lee, Dongwook, Hyunkeun Cho, and Jinwhan Kim. 2026c. “Gaussian Process-Based Underwater Geomagnetic Mapping under Inertial Navigation Drift.” In 2026 23rd International Conference on Ubiquitous Robots (UR). IEEE. https://doi.org/10.1109/ur69537.2026.11626761
• Lee, Ho Chul, and Jae Weon Choi. 2005. “Autopilot Design for Agile Missile Using Ltv Control and Nonlinear Dynamic Inversion.” IFAC Proceedings Volumes 38 (1): 205–10. https://doi.org/10.3182/20050703-6-cz-1902.01995
• Lee, Ho Chul, Yong Seok Choi, and Jae Weon Choi. 2004. “Autopilot Design for Agile Missile Using Time-Varying Control Technique.” IFAC Proceedings Volumes 37 (6): 665–70. https://doi.org/10.1016/s1474-6670(17)32252-8
• Lee, Chih-hsiao, and Charles Herget. 1975. “Regions of Constrained Maximum Likelihood Parameter Identifiability.” In 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1975.270609
• Lee, Geun-Jeong, Min-Seon Jo, and Jeong-Yeol Choi. 2026a. “Comparison of Second-Stage Recovery Methods for Reusable Launch Vehicles across Vehicle Scales.” Aerospace 13 (1): 79. https://doi.org/10.3390/aerospace13010079
• Lee, Kyuman, and Eric N. Johnson. 2020. “Robust Outlier-Adaptive Filtering for Vision-Aided Inertial Navigation.” Sensors 20 (7): 2036. https://doi.org/10.3390/s20072036
• Lee, Hanseob, Seokwoo Jung, and David Hyunchul Shim. 2016c. “Vision-Based UAV Landing on the Moving Vehicle.” In 2016 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2016.7502574
• Lee, Bokwon, and Ryan L. Karkkainen. 2018. “Failure Investigation of in-Flight Separation of Afterburner Nozzle Flap in a Turbojet Engine.” Engineering Failure Analysis 94: 1–12. https://doi.org/10.1016/j.engfailanal.2018.07.023
• Lee, Y. -K., and H. -D. Kim. 2006. “Optimization of Mass Bleed Control for Base Drag Reduction of Supersonic Flight Bodies.” Journal of Thermal Science 15 (3): 206–12. https://doi.org/10.1007/s11630-006-0206-4
• Lee, Dongjin, Yeongju Kim, and Hyochoong Bang. 2012b. “Vision-Based Terrain Referenced Navigation for Unmanned Aerial Vehicles Using Homography Relationship.” Journal of Intelligent & Robotic Systems 69 (1–4): 489–97. https://doi.org/10.1007/s10846-012-9750-1
• Lee, Youngjun, Jinrae Kim, and Youdan Kim. 2025a. “Missile Autopilot Design via Neural Koopman Embedding.” Journal of Aerospace Information Systems 22 (10): 804–15. https://doi.org/10.2514/1.i011660
• Lee, Jisun, Jay Kwon, and Myeongjong Yu. 2015b. “Performance Evaluation and Requirements Assessment for Gravity Gradient Referenced Navigation.” Sensors 15 (7): 16833–47. https://doi.org/10.3390/s150716833
• Lee, Chang June, and Jung Keun Lee. 2024. “Analysis of Effects of Sensor Error Factors on Attitude and Heading Errors for Inertial/Magnetic Sensor-Based Stationary Alignment.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10785060
• Lee, Chang June, and Jung Keun Lee. 2025. “Euler Error Analysis According to Sensor Error Factors for Accelerometer- and Magnetometer- Based Arbitrary Stationary Alignment.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11036921
• Lee, Hyung Keun, Jang Gyu Lee, and Gyu-In Jee. 2002. “Calibration of Measurement Delay in Global Positioning System/Strapdown Inertial Navigation System.” Journal of Guidance, Control, and Dynamics 25 (2): 240–47. https://doi.org/10.2514/2.4904
• Lee, Taehoon, Byungjin Lee, and Sangkyung Sung. 2024a. “Invariant Kalman Filter Design for Securing Robust Performance of Magnetic–Inertial Integrated Navigation System under Measurement Uncertainty.” Aerospace 11 (4): 268. https://doi.org/10.3390/aerospace11040268
• Lee, Feng-Yu, Kai-Chih Liang, Emerson Cheng, Sheng-Shian Li, and Weileun Fang. 2016a. “Acceleration-Insensitive Fully-Decoupled Tuning Fork (FDTF) MEMS Vibratory Gyroscope with 1°/HR BIAS Instability.” In 2016 IEEE 29th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2016.7421788
• Lee, Jiyun, Sam Pullen, Seebany Datta-Barua, and Per Enge. 2007a. “Assessment of Ionosphere Spatial Decorrelation for Global Positioning System-Based Aircraft Landing Systems.” Journal of Aircraft 44 (5): 1662–69. https://doi.org/10.2514/1.28199
• Lee, Jiyun, Sam Pullen, Per Enge, Boris Pervan, and Livio Gratton. 2006. “Monitoring Global Positioning System Satellite Orbit Errors for Aircraft Landing Systems.” Journal of Aircraft 43 (3): 799–808. https://doi.org/10.2514/1.17339
• Lee, In, Jin-Ho Roh, and Il-Kwon Oh. 2003. “Aerothermoelastic Phenomena of Aerospace and Composite Structures.” Journal of Thermal Stresses 26 (6): 525–46. https://doi.org/10.1080/713855957
• Lee, S. J., Y. H. Shim, D. H. Kim, et al. 1998. “RGPS: Based Automatic Landing System for Light and Commuter Aircraft.” IFAC Proceedings Volumes 31 (21): 413–18. https://doi.org/10.1016/s1474-6670(17)41111-6
• Lee, Jungshin, Changky Sung, and Juhyun Oh. 2019. “Terrain Referenced Navigation Using a Multilayer Radial Basis Function-Based Extreme Learning Machine.” International Journal of Aerospace Engineering 2019: 1–11. https://doi.org/10.1155/2019/9142694
• Lee, Woosik, Yulin Yang, and Guoquan Huang. 2021. “Efficient Multi-Sensor Aided Inertial Navigation with Online Calibration.” In 2021 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra48506.2021.9561254
• Lee, Jungshin, Sung Yun, and Jaewook Rhim. 2016b. “Design and Verification of a Digital Controller for a 2-Piece Hemispherical Resonator Gyroscope.” Sensors 16 (4): 555. https://doi.org/10.3390/s16040555
• Lefèvre, Hervé C. 1997. “Fundamentals of the Interferometric Fiber-Optic Gyroscope.” Optical Review 4 (1): A20. https://doi.org/10.1007/bf02935984
• Lefèvre, Hervé C. 2013. “The Fiber-Optic Gyroscope: Challenges to Become the Ultimate Rotation-Sensing Technology.” Optical Fiber Technology 19 (6): 828–32. https://doi.org/10.1016/j.yofte.2013.08.007
• Lehtinen, Bruce, and John R. Zeller. 1972. “Application of Quadratic Optimization to Supersonic Inlet Control.” Automatica 8 (5): 563–74. https://doi.org/10.1016/0005-1098(72)90027-1
• Lei, Ming, Lishuang Feng, and Yinzhou Zhi. 2014b. “Temperature-Dependent, Polarization-Induced Bias Errors in a Resonator Integrated Optical Gyroscope.” Journal of Modern Optics 61 (5): 397–402. https://doi.org/10.1080/09500340.2014.890250
• Lei, Ren, Du Jian-bang, and Han Li-jun. 2014a. “Investigation on Azimuth Effect of FOG INS Multi-Position Alignment in Magnetic Field.” In 2014 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2014.7049476
• Lei, Juanmian, Shuai Zhao, and Suozhu Wang. 2016. “Numerical Study of Aerodynamic Characteristics of FSW Aircraft with Different Wing Positions under Supersonic Condition.” Chinese Journal of Aeronautics 29 (4): 914–23. https://doi.org/10.1016/j.cja.2016.06.006
• Leland, R. P. 2002. “Lyapunov Based Adaptive Control of a MEMS Gyroscope.” In Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301). IEEE. https://doi.org/10.1109/acc.2002.1024513
• Lenoble, A., Y. Lenoir, J-A. Chenilleau, P. Morin, and H. Baudry. 2023. “Navkite™: Protection of Inertial Navigation System Based on Interference Detection and Mitigation Solution.” In 2023 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss58390.2023.10361936
• Lenzner, M., J. Hendrie, H. Afkhamiardakani, et al. 2018. “Sensitivity Enhancement of a Mode-Locked Ring Laser Gyroscope by Giant Intracavity Dispersion.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577105
• Leonardson, R., and S. Foote. 1998. “SiMMA/sup TM/ Accelerometer for Inertial Guidance and Navigation.” In IEEE 1998 Position Location and Navigation Symposium (Cat. No.98CH36153). IEEE. https://doi.org/10.1109/plans.1998.670036
• Leondes, Cornelius T. 1970. “Inertial Navigation for Aircraft.” Scientific American 222 (3): 80–86. https://doi.org/10.1038/scientificamerican0370-80
• Leondes, Cornelius T., and Hiroshi Nakano. 1966. “Nonlinear Inertial Guidance Platform Control Systems Analysis.” IEEE Transactions on Aerospace and Electronic Systems AES-2 (5): 595–607. https://doi.org/10.1109/taes.1966.4501937
• Leondes, Cornelius T., and Robert R. Rankine. 1972. “Modeling the Effects of Pilot Performance on Weapon Delivery Accuracy.” Journal of Aircraft 9 (4): 286–93. https://doi.org/10.2514/3.58972
• Leontiev, A. I., and A. M. Pavlyuchenko. 2004. “The Problem of Relaminarization of Supersonic Turbulent Boundary Layers on Axisymmetric Bodies under Flight Conditions in the Presence of Heat Transfer.” High Temperature 42 (5): 727–42. https://doi.org/10.1023/b:hite.0000046528.21488.73
• Lepsien, Arthur, Philipp Kügler, and Alexander Schaum. 2025. “On the Structural Analysis and Optimal Input Design for Joint State and Parameter Estimation.” IEEE Access 13: 211944–59. https://doi.org/10.1109/access.2025.3636666
• Letty, L. Le, and S. K. Jang. 1997. “Comparative Study of H ∞ Robust Control Methods in Missile Autopilot Design.” IFAC Proceedings Volumes 30 (16): 407–12. https://doi.org/10.1016/s1474-6670(17)42640-1
• Levin, D. 1997. “Vortex Flaps Canard Configuration for Improved Maneuverability.” Journal of Aircraft 34 (5): 693–95. https://doi.org/10.2514/2.2232
• Levy, S. A., R. E. Zinkham, and G. E. Spangler. 1974. “X2048, a High Strength, High Toughness Aluminum Alloy for Aircraft Applications.” Journal of Aircraft 11 (4): 202–6. https://doi.org/10.2514/3.59220
• Lhachemi, H., D. Saussie, and G. Zhu. 2016a. “Gain-Scheduling Control Design in the Presence of Hidden Coupling Terms via Eigenstructure Assignment: Application to a Pitch-Axis Missile Autopilot.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7525556
• Li, Guanghua. 2021. “Skip Trajectory Characteristics Analysis for Hypersonic Glide Vehicles.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9549545
• Li, Yuchen. 2026b. “Research on Deep Learning–Based Error Compensation Methods for Mobile Inertial Navigation.” In 2026 International Conference on Digital Analysis and Processing, Intelligent Computation (DAPIC). IEEE. https://doi.org/10.23919/dapic.2026.00059
• Li, Xin, Guangbin Cai, Hui Xu, Jianwen Zhu, and Chaoxu Mu. 2025g. “Longitudinal Optimal Analytical Midcourse Guidance for Cruise-Glide Integrated Hypersonic Vehicles.” Defence Technology 50: 288–303. https://doi.org/10.1016/j.dt.2025.04.020
• Li, Xiao-Yang, Wen-Bin Chen, and Rui Kang. 2021e. “Performance Margin-Based Reliability Analysis for Aircraft Lock Mechanism Considering Multi-Source Uncertainties and Wear.” Reliability Engineering & System Safety 205: 107234. https://doi.org/10.1016/j.ress.2020.107234
• Li, Nan, Jiabin Chen, Yan Yuan, Yongqiang Han, and Xiaochun Tian. 2016b. “Compensation of FOG Temperature Drift Based on LS-SVM Modeling.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554214
• Li, Yu, and Nai-gang Cui. 2009. “Optimal Attack Trajectory for Hypersonic Boost-Glide Missile in Maximum Reachable Domain.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246695
• Li, Ao, Ke Cui, Daren An, Xiaoyi Wang, and Huiliang Cao. 2024g. “Multi-Frame Vibration MEMS Gyroscope Temperature Compensation Based on Combined GWO-VMD-TCN-LSTM Algorithm.” Micromachines 15 (11): 1379. https://doi.org/10.3390/mi15111379
• Li, Zhong, Yuchen Cui, Yikuan Gu, et al. 2023j. “Temperature Drift Compensation for Four-Mass Vibration MEMS Gyroscope Based on EMD and Hybrid Filtering Fusion Method.” Micromachines 14 (5): 971. https://doi.org/10.3390/mi14050971
• Li, Jianli, Pengfei Dang, Yiqi Li, and Bin Gu. 2018c. “A General Euler Angle Error Model of Strapdown Inertial Navigation Systems.” Applied Sciences 8 (1): 74. https://doi.org/10.3390/app8010074
• Li, Yixuan, Wanshuang Ding, Jiating Su, Wenbin Yu, and Wanchun Chen. 2026a. “Analytical Solutions for Flight Time and States of Hypersonic Glide Vehicle Considering Earth’s Rotation.” In 2026 17th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae70752.2026.11709044
• Li, Teng-fei, Run-han Ding, Wei-xing Wang, and Wen-zhong Xie. 2023c. “Comparison of the Unstart/restart Processes of a Two-Dimensional Twin-Duct Supersonic Inlet Induced by the Plug Throttling and Thermal Choking at the Sideslip State.” Aerospace Science and Technology 142: 108667. https://doi.org/10.1016/j.ast.2023.108667
• Li, Zemin, and Fengyang Duan. 2012. “Low Cost and Automatic Calibration for MEMS Gyroscope.” In 2012 Spring Congress on Engineering and Technology. IEEE. https://doi.org/10.1109/scet.2012.6341968
• Li, Jintao, and Jiancheng Fang. 2013. “Sliding Average Allan Variance for Inertial Sensor Stochastic Error Analysis.” IEEE Transactions on Instrumentation and Measurement 62 (12): 3291–3300. https://doi.org/10.1109/tim.2013.2272841
• Li, D., W. Gao, Z. Li, Y. Yang, and G. Chen. 2018d. “Noise Suppression Method of Rotating Accelerometer Gravity Gradiometer Instrument Based on Oversampling.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577130
• Li, Da, Hongwei Gao, Hongguang Liu, Wei Wang, and Li Li. 2021h. “Self-Gradient Calculation Method of Gravity Gradiometer Platform Based on Finite Element.” In 2021 28th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43216.2021.9470874
• Li, Shutong, Yanbin Gao, Gong Meng, Gang Wang, and Lianwu Guan. 2019a. “Accelerometer-Based Gyroscope Drift Compensation Approach in a Dual-Axial Stabilization Platform.” Electronics 8 (5): 594. https://doi.org/10.3390/electronics8050594
• Li, Jiong, Yangchao He, Lei Shao, and Xianhai Feng. 2025j. “Reentry Glide Vehicle Trajectory Prediction Method via Multidimensional Intention Fusion.” Aerospace Science and Technology 159: 109960. https://doi.org/10.1016/j.ast.2025.109960
• Li, Anliang, Cai Hong, Shifeng Zhang, and Cao Yuan. 2013c. “High-Precision Stabilization Control for a Floated Inertial Platform.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561106
• Li, Yuan, Chris Howcroft, Simon A. Neild, and Jason Zheng Jiang. 2017h. “Using Continuation Analysis to Identify Shimmy-Suppression Devices for an Aircraft Main Landing Gear.” Journal of Sound and Vibration 408: 234–51. https://doi.org/10.1016/j.jsv.2017.07.028
• Li, Maomao, and Jun Hu. 2018. “An Approach and Landing Guidance Design for Reusable Launch Vehicle Based on Adaptive Predictor–corrector Technique.” Aerospace Science and Technology 75: 13–23. https://doi.org/10.1016/j.ast.2017.12.037
• Li, Zhenhua, Chen Hu, Chibiao Ding, Gang Liu, and Bing He. 2018g. “Stochastic Gradient Particle Swarm Optimization Based Entry Trajectory Rapid Planning for Hypersonic Glide Vehicles.” Aerospace Science and Technology 76: 176–86. https://doi.org/10.1016/j.ast.2018.01.033
• Li, Xiaojie, Xiaobin Huang, Hong Liu, and Jianke Du. 2020a. “Fuel Reactivity Controlled Self-Starting and Propulsion Performance of a Scramjet: A Model Investigation.” Energy 195: 116920. https://doi.org/10.1016/j.energy.2020.116920
• Li, B., and D. Hullender. 1998. “Self-Tuning Controller for Nonlinear Inertial Stabilization Systems.” IEEE Transactions on Control Systems Technology 6 (3): 428–34. https://doi.org/10.1109/87.668043
• Li, Qiaochu, Carine Jauberthie, Lilianne Denis-Vidal, and Zohra Cherfi. 2017f. “Parameter Estimation Enhanced by Optimal Input Design in a Bounded-Error Context.” IFAC-PapersOnLine 50 (1): 6277–82. https://doi.org/10.1016/j.ifacol.2017.08.862
• Li, Wenyuan, Yi Ji, and Guanghui Sun. 2026i. “Reusable Launch Vehicle Landing Online Guidance and Control Based on ESO-MPC and Convex Optimization.” IEEE Access 14: 30860–71. https://doi.org/10.1109/access.2026.3667479
• Li, Xiaoxuan, Zhanyuan Jiang, Jianquan Ge, and Tao Yang. 2021b. “A Cooperative Reentry Trajectory Optimization Method for Hypersonic Glide Vehicles.” In 2021 3rd International Academic Exchange Conference on Science and Technology Innovation (IAECST). IEEE. https://doi.org/10.1109/iaecst54258.2021.9695560
• Li, Yuan, Jason Zheng Jiang, and Simon Neild. 2017c. “Inerter-Based Configurations for Main-Landing-Gear Shimmy Suppression.” Journal of Aircraft 54 (2): 684–93. https://doi.org/10.2514/1.c033964
• Li, Jian, Qing Li, and Nong Cheng. 2018a. “A Combined Visual-Inertial Navigation System of MSCKF and EKF-SLAM.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018998
• Li, Xin, Yuan Li, and Chao Hong. 2022d. “Novel Adaptive MEMS Gyroscope Filtering Algorithm.” In 2022 European Conference on Communication Systems (ECCS). IEEE. https://doi.org/10.1109/eccs54035.2022.00024
• Li, Kailin, Jiansheng Li, Ancheng Wang, Haolong Luo, Xueqiang Li, and Zidi Yang. 2022i. “A Resilient Method for Visual–Inertial Fusion Based on Covariance Tuning.” Sensors 22 (24): 9836. https://doi.org/10.3390/s22249836
• Li, Huiping, Ding Li, Bin Zhang, et al. 2025m. “Temperature Field Analysis and Optimization Design of the Dithered Ring Laser Gyroscope in Strapdown Inertial Navigation Systems.” Scientific Reports 15 (1): 17597. https://doi.org/10.1038/s41598-025-02028-5
• Li, Jianbin, Jianhan Liang, Mingbo Sun, Zun Cai, and Lin Zhang. 2023b. “Combustion Enhancement Subjected to the Inlet Distortion in a Cavity-Based Supersonic Combustor.” Aerospace Science and Technology 142: 108636. https://doi.org/10.1016/j.ast.2023.108636
• Li, Bin, Defu Lin, Hui Wang, and Jiang Wang. 2018b. “Gain-Scheduling Autopilot Design Based on Fixed-Structure Synthesis.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019133
• Li, Ziqiang, Xiaohui Liu, and Panpan An. 2017b. “Error Modeling and Analyzing of Scalar Deeply-Coupled Global Navigation Satellite System and Inertial Navigation System.” In 2017 IEEE 17th International Conference on Communication Technology (ICCT). IEEE. https://doi.org/10.1109/icct.2017.8359810
• Li, Xuyou, Pan Liu, Xingxing Guang, Zhenlong Xu, Lianwu Guan, and Guangchun Li. 2017g. “Temperature Dependence of Faraday Effect-Induced Bias Error in a Fiber Optic Gyroscope.” Sensors 17 (9): 2046. https://doi.org/10.3390/s17092046
• Li, Long-Yue, Fu-Xian Liu, and Ying-Ying Mei. 2012c. “Modeling and Simulation System Design of Tactical Ballistic Missile Interception Based on UML.” In 2012 Fourth International Conference on Computational and Information Sciences. IEEE. https://doi.org/10.1109/iccis.2012.186
• Li, Kun, Peidong Liu, Tao Pang, Zhaolin Yang, and Ben M. Chen. 2015b. “Development of an Unmanned Aerial Vehicle for Rooftop Landing and Surveillance.” In 2015 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2015.7152368
• Li, Jinxing, Tianyuan Liu, Guangya Zhu, Yunzhu Li, and Yonghui Xie. 2023k. “Uncertainty Quantification and Aerodynamic Robust Optimization of Turbomachinery Based on Graph Learning Methods.” Energy 273: 127289. https://doi.org/10.1016/j.energy.2023.127289
• Li, Zhenliang, Peili Lu, Daijun Zhang, and Tian Zhang. 2018e. “Practical Identifiability Analysis and Optimal Experimental Design for the Parameter Estimation of the ASM2d-Based EBPR Anaerobic Submodel.” Mathematical Problems in Engineering 2018: 1–9. https://doi.org/10.1155/2018/9201085
• Li, Chuanjun, Jingquan Ma, Xiao Liang, and Yuhang Guo. 2024h. “A Segmented Trajectory Planning and Guidance Method for Hypersonic Glide Vehicles Considering Target Detection Performance.” Aerospace Science and Technology 153: 109461. https://doi.org/10.1016/j.ast.2024.109461
• Li, Jianli, Yanhai Ma, and Chen Xiyuan. 2013b. “Error Modeling, Calibration, and Nonlinear Interpolation Compensation Method of Ring Laser Gyroscope Inertial Navigation System.” Abstract and Applied Analysis 2013: 1–7. https://doi.org/10.1155/2013/359675
• Li, Kelu, Jiahao Ma, Zhiyong Yu, Qihui Bian, and Tao Tang. 2026e. “Nonlinear Dual Disturbance Observer with Acceleration Control for Dual-Stage Inertial Stabilization Platform.” IEEE Transactions on Industrial Electronics 73 (3): 4725–34. https://doi.org/10.1109/tie.2025.3613646
• Li, Jingshu, Ning Mao, Yifeng Liang, Jiangning Xu, and Hongyang He. 2026f. “A Novel 2-D Marine Gravity Anomaly Matching Navigation Method.” IEEE Transactions on Instrumentation and Measurement 75: 8510312–8510312. https://doi.org/10.1109/tim.2026.3706210
• Li, Xuyou, Qingwen Meng, Meng Liu, and Yanda Guo. 2021c. “A Fast Robust Kalman Filter for Initial Alignment of Strapdown Inertial Navigation System.” Optik 237: 166541. https://doi.org/10.1016/j.ijleo.2021.166541
• Li, J. J., T. Q. Miao, Q. S. Li, et al. 2023a. “The Analysis and Suppressing Method of Frequency Drift in Honeycomb Disk Resonator Gyroscope.” In 2023 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss58390.2023.10361921
• Li, An, FangJun Qin, JiangNing Xu, and SaiJiang. 2009a. “Gyroscope Free Strapdown Inertial Navigation System Using Rotation Modulation.” In 2009 Second International Conference on Intelligent Computation Technology and Automation. IEEE. https://doi.org/10.1109/icicta.2009.613
• Li, Rujie, Wei Quan, Wenfeng Fan, Li Xing, and Jiancheng Fang. 2017d. “Influence of Magnetic Fields on the Bias Stability of Atomic Gyroscope Operated in Spin-Exchange Relaxation-Free Regime.” Sensors and Actuators A: Physical 266: 130–34. https://doi.org/10.1016/j.sna.2017.09.023
• Li, Pei, Helmut Sobieczky, and Richard Seebass. 1999. “Manual Aerodynamic Optimization of an Oblique Wing Supersonic Transport.” Journal of Aircraft 36 (6): 907–13. https://doi.org/10.2514/2.2547
• Li, Maochun, Yizhi Sun, Shoufei Gao, et al. 2025h. “Navigation-Grade Interferometric Air-Core Antiresonant Fibre Optic Gyroscope with Enhanced Thermal Stability.” Nature Communications 16 (1): 3449. https://doi.org/10.1038/s41467-025-58381-6
• Li, Xuelian, Yao Sun, Hongwei Mo, and Kejun Wang. 2009b. “Study of the GM(1,1) Model and Improved Model of the Trend Term of Micromechanical Gyroscope Drift.” In 2009 International Joint Conference on Computational Sciences and Optimization. IEEE. https://doi.org/10.1109/cso.2009.137
• Li, Yan, Jindong Tan, Yinlong Zhang, Wei Liang, and Hongsheng He. 2018f. “Spatial Calibration for Thermal-RGB Cameras and Inertial Sensor System.” In 2018 24th International Conference on Pattern Recognition (ICPR). IEEE. https://doi.org/10.1109/icpr.2018.8546111
• Li, Jie, and Ruiping Tao. 2010. “Initial Alignment Technology of Strapdown Inertial Navigation System Based-on Stationary Base.” In 2010 International Conference on Intelligent Control and Information Processing. IEEE. https://doi.org/10.1109/icicip.2010.5564204
• Li, Xun, and Jinling Wang. 2012. “Multi-Image Matching for 3D Mapping in Vision-Based Navigation Applications.” In 2012 Ubiquitous Positioning, Indoor Navigation, and Location Based Service (UPINLBS). IEEE. https://doi.org/10.1109/upinlbs.2012.6409766
• Li, Tianjiao, Bo Wang, Zhihong Deng, and Mengyin Fu. 2024c. “Genetic Algorithm-Based Weighted Comprehensive Image Matching Algorithm for Underwater Gravity Gradient-Aided Navigation.” IEEE Journal of Oceanic Engineering 49 (4): 1647–56. https://doi.org/10.1109/joe.2024.3379484
• Li, Chendi, Jiang Wang, and Peng Huang. 2022e. “Optimal Cooperative Line-of-Sight Guidance for Defending a Guided Missile.” Aerospace 9 (5): 232. https://doi.org/10.3390/aerospace9050232
• Li, Jing, Shanpeng Wang, Panpan Huang, and Xiao Zhang. 2022j. “A Tightly Coupled Polarization Compass and VIO Integrated Navigation for Applications in GNSS-Denied Environments.” In 2022 5th International Symposium on Autonomous Systems (ISAS). IEEE. https://doi.org/10.1109/isas55863.2022.9757349
• Li, Tianjiao, Bo Wang, Bao Song, Zhihong Deng, and Mengyin Fu. 2025c. “GGIMN: Gravity Gradient Image Matching Network with Adaptive Adjoint Smoothing for AUV Navigation.” IEEE Transactions on Vehicular Technology 74 (8): 11751–61. https://doi.org/10.1109/tvt.2025.3554543
• Li, Zhihua, Jing Wang, Kunlun Wu, and Wenxue Liu. 2026g. “A PIO-GD-Assisted Calibration Procedure for Multi-Redundant Inertial Measurement Units.” Measurement 290: 122730. https://doi.org/10.1016/j.measurement.2026.122730
• Li, Yueting, Chenglong Wang, Jia Zhang, and Bo Wang. 2020c. “Selection Method of the Matching Area of Underwater Gravity-Aided Inertial Navigation Based on Vector Characteristics.” In 2020 39th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc50068.2020.9189262
• Li, Jiaxin, Zhigang Wu, Yanqi Feng, Guan Wang, and Kai Liu. 2025f. “Intelligent Model Correction and Trajectory Planning for Air-Breathing Hypersonic Vehicle Considering Inlet Unstart.” Aerospace Science and Technology 164: 110401. https://doi.org/10.1016/j.ast.2025.110401
• Li, Bin, Xiang Xi, Kun Lu, Yan Shi, Dingbang Xiao, and Xuezhong Wu. 2023i. “Study of Electrode Ablation for Femtosecond Laser Trimming of Micro Hemispherical Resonator Gyroscope.” IEEE Sensors Journal 23 (3): 1933–42. https://doi.org/10.1109/jsen.2022.3224000
• Li, Yuan-Xi, Bo-Qi Xi, Shun-Qing Ren, and Chang-Hong Wang. 2023f. “Precision Enhancement by Compensation of Hemispherical Resonator Gyroscope Dynamic Output Errors.” IEEE Transactions on Instrumentation and Measurement 72: 1–10. https://doi.org/10.1109/tim.2023.3277998
• Li, Wenyin, Dingbang Xiao, Xuezhong Wu, et al. 2016c. “Enhanced Temperature Stability of Sensitivity for MEMS Gyroscope Based on Frequency Mismatch Control.” Microsystem Technologies 23 (8): 3311–17. https://doi.org/10.1007/s00542-016-3114-x
• Li, Leyao, Yiqing Xie, Yufeng Wang, and Jianpeng Li. 2025d. “In-Orbit Data Analysis and Evaluation of Gyroscope Random Drift.” In 2025 37th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc65474.2025.11090388
• Li, KaiHan, Ling Xiong, Long Cheng, and Jie Ma. 2014c. “The Research of Matching Area Selection Criterion for Gravity Gradient Aided Navigation.” In Pattern Recognition. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-45646-0_3
• Li, Jinghang, Shuting Xu, Yu Wu, and Zhe Zhang. 2024b. “Automatic Landing Control for Fixed-Wing UAV in Longitudinal Channel Based on Deep Reinforcement Learning.” Drones 8 (10): 568. https://doi.org/10.3390/drones8100568
• Li, Haiquan, Wenzhe Xu, Yun Zhao, et al. 2025b. “Dynamics Modeling and Analysis of a Vertical Landing Mechanism for Reusable Launch Vehicle.” Aerospace 12 (4): 280. https://doi.org/10.3390/aerospace12040280
• Li, Cun, Hong Xue, Yuhang Zhang, Jiabin Ai, and Yulong Zhao. 2024f. “A Laterally Sensitive Quartz Vibrating Beam Accelerometer for Inertial Navigation Application.” Sensors and Actuators A: Physical 366: 115015. https://doi.org/10.1016/j.sna.2024.115015
• Li, Qing, and PeiPei Yang. 2009. “Study on Initial Alignment for Inertial Navigation System.” In 2009 International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2009.5364370
• Li, Jian, Gongliu Yang, Qingzhong Cai, Haofei Niu, and Jing Li. 2022a. “Cooperative Navigation for UAVs in GNSS-Denied Area Based on Optimized Belief Propagation.” Measurement 192: 110797. https://doi.org/10.1016/j.measurement.2022.110797
• Li, Zhengnan, Tao Yang, and Zhiwei Feng. 2016e. “The Multiobjective Trajectory Optimization for Hypersonic Glide Vehicle Based on Normal Boundary Intersection Method.” Mathematical Problems in Engineering 2016: 1–8. https://doi.org/10.1155/2016/9407238
• Li, Jianhang, Zhenglin Yang, Qing Li, and Lei Liu. 2025a. “Design and Control of Micro-Radian Inertial Stabilization Laser Platform.” IFAC-PapersOnLine 59 (20): 2642–47. https://doi.org/10.1016/j.ifacol.2025.11.558
• Li, Ailun, Yixing Yang, Jinming Yun, et al. 2026m. “Tactical-Grade Compact Fiber Optic Gyroscope Based on a Multifunctional Hybrid Integrated Chip.” Applied Optics 65 (21): 7245. https://doi.org/10.1364/ao.597707
• Li, He, Hong Yi, Ang Li, Kai Yang, and Xi Wang. 2025i. “A Novel Method for Observing Blowtorch Reflow of Micro Hemispherical Gyroscope Resonators.” In 2025 IEEE 3rd International Conference on Sensors, Electronics and Computer Engineering (ICSECE). IEEE. https://doi.org/10.1109/icsece65727.2025.11256864
• Li, Mingyang, Hongsheng Yu, Xing Zheng, and Anastasios I. Mourikis. 2014a. “High-Fidelity Sensor Modeling and Self-Calibration in Vision-Aided Inertial Navigation.” In 2014 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2014.6906889
• Li, Tao, Gannan Yuan, Haiyu Lan, and Martin Mintchev. 2015a. “Design and Algorithm Verification of a Gyroscope-Based Inertial Navigation System for Small-Diameter Spaces in Multilateral Horizontal Drilling Applications.” Micromachines 6 (12): 1946–70. https://doi.org/10.3390/mi6121467
• Li, Chanying, and Xian Zhang. 2022. “On Identifiability of Discrete-Time Nonlinearly Parameterized Systems.” Systems & Control Letters 160: 105128. https://doi.org/10.1016/j.sysconle.2021.105128
• Li, Tianqi, Chunxi Zhang, Yizhuo Tian, and Yanqiang Yang. 2023h. “Star Centroid Error Compensation Based on the Star Triangle Internal Angles for Celestial Navigation with Aero-Optical Degradation.” Measurement 206: 112229. https://doi.org/10.1016/j.measurement.2022.112229
• Li, Guangchen, Shuting Zhang, Haowen Wang, Yuyang Sun, Zhaohui Wang, and Bocheng Zhu. 2026d. “MC-GVIO: Motion Consistency Aided GNSS-Visual-Inertial Odometry for Land Vehicle Navigation in Urban Environments.” IEEE Transactions on Vehicular Technology 75 (10): 23015–31. https://doi.org/10.1109/tvt.2026.3707622
• Li, Geng, Pengfei Zhang, Guo Wei, Yuanping Xie, Xudong Yu, and Xingwu Long. 2015c. “Multiple-Point Temperature Gradient Algorithm for Ring Laser Gyroscope Bias Compensation.” Sensors 15 (12): 29910–22. https://doi.org/10.3390/s151229777
• Li, Geng, Pengfei Zhang, Guo Wei, Xudong Yu, Yuanping Xie, and Xingwu Long. 2015d. “Ring Laser Gyroscope Drift-Error Compensation Using Support Vector Machine with Kernel-Based Data Fusion.” In 2015 2nd International Conference on Opto-Electronics and Applied Optics (IEM OPTRONIX). IEEE. https://doi.org/10.1109/optronix.2015.7345525
• Li, Jing, GuoXin Zhao, and Pei Yu. 2019b. “A Novel Loop Control Method of Full Attitude Inertial Stabilization Platform.” In 2019 4th International Conference on Robotics and Automation Engineering (ICRAE). IEEE. https://doi.org/10.1109/icrae48301.2019.9043812
• Li, Zhaowei, Wei Zheng, and Fan Wu. 2020b. “Improving the Reliability of Underwater Gravity Matching Navigation Based on a Priori Recursive Iterative Least Squares Mismatching Correction Method.” IEEE Access 8: 8648–57. https://doi.org/10.1109/access.2020.2964014
• Li, Hairun, Ge Zhou, Weijun Hu, Xianlong Ma, Jiale Quan, and Zhikui You. 2026b. “Ballistic Missile Parameter Identification and Trajectory Reconstruction Method Based on PI-LSTM.” In 2026 9th International Conference on Artificial Intelligence and Big Data (ICAIBD). IEEE. https://doi.org/10.1109/icaibd69640.2026.11637279
• Li, Mingjie, Chijun Zhou, Lei Shao, and Humin Lei. 2022b. “An Intelligent Trajectory Prediction Algorithm for Hypersonic Glide Targets Based on Maneuver Mode Identification.” International Journal of Aerospace Engineering 2022: 1–17. https://doi.org/10.1155/2022/4625001
• Li, Linfeng, Xingqi Zhu, Xiaolong Yuan, Feng Zhang, and Guanghua Liu. 2026j. “A Review of Inertial Navigation Error Compensation Methods in GNSS-Denied Environments.” In 2026 2nd International Conference on Navigation, Detection and Control (CNDC). IEEE. https://doi.org/10.1109/cndc70899.2026.11708199
• Li Yun, Luo Bing, Wang Xu, and Wu Wenqi. 2011. “Quadrature Control of Hemispherical Resonator Gyro Based on FPGA.” In IEEE 2011 10th International Conference on Electronic Measurement & Instruments. IEEE. https://doi.org/10.1109/icemi.2011.6037926
• Lian, Chengbin, Cheng Bai, Zhang Ren, and Xingyue Shao. 2013a. “The Design of Nonlinear Flight Control System of Hypersonic Cruise Vehicle Based on Nonlinear Disturbance Observer.” In 2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control. IEEE. https://doi.org/10.1109/imccc.2013.328
• Lian, Lin, Shenpeng Li, Guojun Huang, Yang Wu, and Qin Ren. 2026. “Robust Direction-of-Arrival Estimation Using Zero-Crossing-Based Time Delay Measurement for Navigation in GNSS-Denied Environments.” Sensors 26 (5): 1600. https://doi.org/10.3390/s26051600
• Lian, Chengbin, Liubao Shi, Zhang Ren, and Xingyue Shao. 2012. “Fuzzy Sliding Mode Variable Structure Controller for Hypersonic Cruise Vehicle.” In System Simulation and Scientific Computing. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-34381-0_16
• Liang, Xinru, Changsheng Gao, and Wuxing Jing. 2025. “Trajectory Prediction Algorithm Based on Maneuver Analysis for Hypersonic Glide Vehicles in a Deep Neural Network.” Astrodynamics 9 (6): 933–52. https://doi.org/10.1007/s42064-024-0257-x
• Liang, Jianjian, Shoukun Wang, and Bo Wang. 2023. “Online Motion Planning for Fixed-Wing Aircraft in Precise Automatic Landing on Mobile Platforms.” Drones 7 (5): 324. https://doi.org/10.3390/drones7050324
• Liang, Zhiyuan, and Jianqing Zhang. 2009. “A Dynamic Balance Testing Framework for Gyroscope Based on Embedded System.” In 2009 International Conference on Artificial Intelligence and Computational Intelligence. IEEE. https://doi.org/10.1109/aici.2009.479
• Liang, Cui, Yanru Zhou, Dengwei Zhang, Xuan She, Tengchao Huang, and Xiaowu Shu. 2018. “Research on the Temperature Characteristic of Magnetic Sensor in the Magnetic Drift Compensation Fiber-Optic Gyroscope.” Optik 172: 91–96. https://doi.org/10.1016/j.ijleo.2018.07.015
• Liao, Jingxian, and Hyochoong Bang. 2022. “Precise Missile Autopilot Design Using Nonlinear Sliding Mode Control.” In 2022 13th Asian Control Conference (ASCC). IEEE. https://doi.org/10.23919/ascc56756.2022.9828101
• Liao, Fang, Jian Liang Wang, Eng Kee Poh, and Dong Li. 2005. “Fault-Tolerant Robust Automatic Landing Control Design.” Journal of Guidance, Control, and Dynamics 28 (5): 854–71. https://doi.org/10.2514/1.12611
• Liao, Wei, Lubin Weng, and Xianqing Tai. 2010. “Terrain Aided Navigation Algorithm Using Gaussian Sum Particle Filter.” In 2010 Chinese Conference on Pattern Recognition (CCPR). IEEE. https://doi.org/10.1109/ccpr.2010.5659307
• Libero, Yaakov, and Itzik Klein. 2026. “Gauge Freedom Optimization for Truncation Error Reduction in Inertial Navigation.” IEEE Transactions on Instrumentation and Measurement 75: 8514712–8514712. https://doi.org/10.1109/tim.2026.3738213
• Liebe, C. C. 1995. “Star Trackers for Attitude Determination.” IEEE Aerospace and Electronic Systems Magazine 10 (6): 10–16. https://doi.org/10.1109/62.387971
• Liebe, C. C., E. W. Dennison, B. Hancock, R. C. Stirbl, and B. Pain. 1998. “Active Pixel Sensor (APS) Based Star Tracker.” In 1998 IEEE Aerospace Conference Proceedings (Cat. No.98TH8339), vol. 1. IEEE. https://doi.org/10.1109/aero.1998.686811
• Liewald, J.-T., B. Kuhlmann, T. Balslink, and Y. Manoli. 2012. “A 100 kHz Vibratory MEMS Rate Gyroscope with Experimental Verification of System Model’s Frequency Scaling.” In 2012 IEEE 25th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2012.6170245
• Lijun, Zeng, and Min Fang. 2019. “Temperature Drift Compensation of MEMS Gyroscope Array Based on Elman Neural Networks.” In 2019 IEEE 3rd Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC). IEEE. https://doi.org/10.1109/imcec46724.2019.8984059
• Lin, Tony C. 2003. “Development of U.S. Air Force Intercontinental Ballistic Missile Weapon Systems.” Journal of Spacecraft and Rockets 40 (4): 491–509. https://doi.org/10.2514/2.3990
• Lin, De-fu, and Jun-fang Fan. 2009. “Missile Autopilot Design Using Backstepping Approach.” In 2009 Second International Conference on Computer and Electrical Engineering. IEEE. https://doi.org/10.1109/iccee.2009.51
• Lin, Ying-Xi, and Ying-Chih Lai. 2025. “Deep Learning-Based Navigation System for Automatic Landing Approach of Fixed-Wing UAVs in GNSS-Denied Environments.” Aerospace 12 (4): 324. https://doi.org/10.3390/aerospace12040324
• Lin, Shih-Tin, and Chun-Mo Lee. 1996. “Multivariable Control of the J-85 Turbojet Engine for Full Flight Envelope Operation.” Journal of Guidance, Control, and Dynamics 19 (4): 913–20. https://doi.org/10.2514/3.21718
• Lin, David, Robert MacDonald, Dorin Calbaza, et al. 2021. “Polaris: A Low Cost MEMS Fabrication Platform for Navigation-Grade Inertial Sensors.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430465
• Lin, Yusen, Lingjuan Miao, and Zhiqiang Zhou. 2022. “A High-Accuracy Initial Alignment Method Based on Backtracking Process for Strapdown Inertial Navigation System.” Measurement 201: 111712. https://doi.org/10.1016/j.measurement.2022.111712
• Lin, Xin, and Xiaoli Zhang. 2020. “Random Error Compensation of MEMS Gyroscope Based on Adaptive Kalman Filter.” In 2020 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc49329.2020.9164752
• Lind, Rick. 2002. “Linear Parameter-Varying Modeling and Control of Structural Dynamics with Aerothermoelastic Effects.” Journal of Guidance, Control, and Dynamics 25 (4): 733–39. https://doi.org/10.2514/2.4940
• Linder, Jonas, Martin Enqvist, Fredrik Gustafsson, and Johan Sjöberg. 2014. “Identifiability of Physical Parameters in Systems with Limited Sensors.” IFAC Proceedings Volumes 47 (3): 6454–59. https://doi.org/10.3182/20140824-6-za-1003.02272
• Ling, Chong K. 1970. “Quasi-Optimum Design of an Aircraft Landing Control System.” Journal of Aircraft 7 (1): 38–43. https://doi.org/10.2514/3.44119
• Liqun, Ma, Duan Chaoyang, and Zhang Gongping. 2017. “Interception of Hypersonic Vehicle Based on Integrated Guidance and Control.” In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2017.7979401
• Lithin, M. G., Gyanendra Kumar Kashyap, B. Sudha, et al. 2013. “Design of Very Low Noise Amplifier for High Accuracy Star Tracker in GEO Missions.” In 2013 International Conference on Advanced Electronic Systems (ICAES). IEEE. https://doi.org/10.1109/icaes.2013.6659366
• Litvinenko, Alexander, and Hermann G. Matthies. 2012. “Uncertainty Quantification in Numerical Aerodynamic via Low-Rank Response Surface.” PAMM 12 (1): 781–84. https://doi.org/10.1002/pamm.201210379
• Liu, John Y. 2024. “Auxiliary Gyroscope Approach for Balanced Performance via Gyro Self-Calibration.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502051
• Liu, Zhuoqi, Yuanli Cai, Yihang Liu, Yifan Deng, and Haonan Jiang. 2023j. “Trajectory Optimization of Hypersonic Glide Vehicle Based on Pseudospectral Method Assisted by BP Neural Network.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10450472
• Liu, Ming, and Guobin Chang. 2015. “Gravity Matching Aided Inertial Navigation Technique Based on Marginal Robust Unscented Kalman Filter.” Mathematical Problems in Engineering 2015: 1–9. https://doi.org/10.1155/2015/592480
• Liu, Di, Xiyuan Chen, and Bingbo Cui. 2025f. “An Improved Cubature Kalman Filter for GNSS-Denied and System-Noise-Varying INS/GNSS Navigation.” Micromachines 16 (10): 1116. https://doi.org/10.3390/mi16101116
• Liu, Yating, Jingbo Duan, Yihang Gao, and Buqing Xu. 2023g. “Nonlinear Supersonic Aerothermoelastic Analysis of as Ymmetrically Curved-Fiber Composite Panels with Nonuniform Temperature Distributions.” Journal of Mechanical Science and Technology 37 (3): 1325–37. https://doi.org/10.1007/s12206-023-0219-x
• Liu, Junbing, Xiaoqiang Fan, Yuan Tao, and Weidong Liu. 2019. “Experimental and Numerical Study on the Local Unstart Mechanism of Hypersonic Inlet.” Acta Astronautica 160: 216–21. https://doi.org/10.1016/j.actaastro.2019.04.041
• Liu, Mengxiang, Qi Fan, Jian Zhao, and Yan Su. 2020d. “A Phase Compensation Method for MEMS Quadruple Mass Gyroscope in Zero Bias Drift.” IEEE Sensors Journal: 1–1. https://doi.org/10.1109/jsen.2020.3026754
• Liu, Jili, Mingrui Fu, Chao Meng, et al. 2020b. “Consideration of Thermo-Vacuum Stability of a MEMS Gyroscope for Space Applications.” Sensors 20 (24): 7172. https://doi.org/10.3390/s20247172
• Liu, Meng, Yanbin Gao, Guangchun Li, Xingxing Guang, and Shutong Li. 2016c. “An Improved Alignment Method for the Strapdown Inertial Navigation System (SINS).” Sensors 16 (5): 621. https://doi.org/10.3390/s16050621
• Liu, Steven Y., James T. Gordon, and M. Akif Ozbek. 1998. “Nonlinear Model for Aircraft Brake Squeal Analysis: Model Description and Solution Methodology.” Journal of Aircraft 35 (4): 623–30. https://doi.org/10.2514/2.2346
• Liu, Qiang, Bo Han, Jiang-ning Xu, and Miao Wu. 2011a. “Random Drift Modeling for MEMS Gyroscope Based on Lifting Wavelet and Wavelet Neural Network.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5778009
• Liu, Jian-xia, Zhong-xi Hou, and Xiao-qing Chen. 2010b. “Research on Thermal Control System of Hypersonic Glide Vehicle.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633608
• Liu, Gao, Zhanqiang Hou, Xuan Wang, et al. 2026c. “Bias Drift Compensation of Butterfly Gyroscope under Temperature Change with Two-Stage Hybrid Deep Learning Model.” Mechanical Systems and Signal Processing 247: 113937. https://doi.org/10.1016/j.ymssp.2026.113937
• Liu, Gao, Zhanqiang Hou, Mi Zeng, et al. 2025b. “Bias Error Suppression of the Butterfly Gyroscope under Random Vibration Perturbation.” Measurement 256: 118208. https://doi.org/10.1016/j.measurement.2025.118208
• Liu, Hongwu, Shuling Hu, Qingzhong Cai, Yongfeng Zhang, and Kun Zhang. 2022b. “Backstepping Terminal Sliding Mode Control of FOG Inertial Platform Stability Loop Based on Extended State Observer.” In 2022 7th International Conference on Control, Robotics and Cybernetics (CRC). IEEE. https://doi.org/10.1109/crc55853.2022.10041229
• Liu, Hui, Rui Jiang, Han Cheng, and Yuhang Liu. 2026l. “Underwater Gravity-Matching Navigation Algorithm Based on Adaptive-Scale Feature Descriptor.” Actuators 15 (9): 475. https://doi.org/10.3390/act15090475
• Liu, Changwu, Chen Jiang, and Haowen Wang. 2022m. “Variable Observability Constrained Visual-Inertial-GNSS EKF-Based Navigation.” IEEE Robotics and Automation Letters 7 (3): 6677–84. https://doi.org/10.1109/lra.2022.3175600
• Liu, Ping, Xinxin Jiang, Yating Wang, and Fenghua Huang. 2022k. “Outfield Calibration Scheme for Tri-Axis MEMS Gyroscope.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9902818
• Liu, Qili, Kyungrae Kang, and Hyungrok Do. 2022i. “Inlet Buzz Phenomenon Driven by Flow Choking in High-Enthalpy Mach 4.5 Flows Using Circular Scramjet Models.” Acta Astronautica 193: 406–17. https://doi.org/10.1016/j.actaastro.2022.01.030
• Liu, John Y., Edward Konefat, Howard Ge, and Stephen Schein. 2026e. “Hardware Validation of a Bias Self-Calibration Based Virtual Gyro.” In 2026 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial69196.2026.11557959
• Liu, Chen, Min Kong, Fang Tao, et al. 2026j. “A Review on Gravity Matching Navigation and Positioning Technology.” In 2026 2nd International Conference on Navigation, Detection and Control (CNDC). IEEE. https://doi.org/10.1109/cndc70899.2026.11708545
• Liu, Min, Jizhou Lai, Zhimin Li, and Jianye Liu. 2016a. “An Adaptive Cubature Kalman Filter Algorithm for Inertial and Land-Based Navigation System.” Aerospace Science and Technology 51: 52–60. https://doi.org/10.1016/j.ast.2016.01.010
• Liu, Ruyuan, Tianjiao Li, and Zhongli Bai. 2026a. “An Adaptive Candidate Probabilistic Matching Method for Underwater Gravity-Aided Navigation.” In 2026 IEEE 27th China Conference on System Simulation Technology and its Applications (CCSSTA). IEEE. https://doi.org/10.1109/ccssta69471.2026.11635608
• Liu, Zhongguan, Wei Li, Honglei Che, Lu Pan, and Shuaidong Yuan. 2026b. “Azimuth-LIO: Robust LiDAR-Inertial Odometry via Azimuth-Aware Voxelization and Probabilistic Fusion.” IEEE Robotics and Automation Letters 11 (3): 3158–65. https://doi.org/10.1109/lra.2026.3655291
• Liu, Pan, Xuyou Li, Xingxing Guang, Zhenlong Xu, Weiwei Ling, and Hanrui Yang. 2017d. “Drift Suppression in a Dual-Polarization Fiber Optic Gyroscope Caused by the Faraday Effect.” Optics Communications 394: 122–28. https://doi.org/10.1016/j.optcom.2017.03.030
• Liu, Yunfei, Zhitian Li, Shuaikang Zheng, Pengcheng Cai, and Xudong Zou. 2022d. “An Evaluation of MEMS-IMU Performance on the Absolute Trajectory Error of Visual-Inertial Navigation System.” Micromachines 13 (4): 602. https://doi.org/10.3390/mi13040602
• Liu, Mingming, and Jinlai Liu. 2026. “Initial Alignment Method for Strapdown Inertial Navigation System Based on High-Order Taylor Expansion.” In 2026 7th International Conference on Electrical Technology and Automatic Control (ICETAC). IEEE. https://doi.org/10.1109/icetac70565.2026.11636163
• Liu, Chongchong, Xiaochuan Liu, and Yong Xu. 2026g. “Landing Gear Shimmy Analysis for a Delayed Tire Model with Transient Modes.” Journal of Aircraft: 1–11. https://doi.org/10.2514/1.c038663
• Liu, Hui, Yuhang Liu, Shuqiang Xue, Han Cheng, and Wang Zhang. 2026d. “A Data-Driven Matching Error Compensation Framework for Underwater Gravity Aided Inertial Navigation.” Journal of Marine Science and Engineering 14 (17): 1608. https://doi.org/10.3390/jmse14171608
• Liu, Jian, Yunhe Liu, and Di Yan. 2018b. “Research of Inertial Instrument Error Identification Algorithm for Spacecraft Test.” In 2018 Eighth International Conference on Instrumentation & Measurement, Computer, Communication and Control (IMCCC). IEEE. https://doi.org/10.1109/imccc.2018.00374
• Liu, Zhenming, Yaoyao Long, Charlotte Wehner, Haoran Wen, and Farrokh Ayazi. 2024a. “4H Silicon Carbide Bulk Acoustic Wave Gyroscope with Ultra-High Q-Factor for on-Chip Inertial Navigation.” Communications Engineering 3 (1): 87. https://doi.org/10.1038/s44172-024-00234-z
• Liu, Jiahui, Qi Luo, Jiaxin Lou, and Yuankai Li. 2020a. “An Adaptive Infrared Tracking Method for Spacebased Surveillance to a Hypersonic Cruise Vehicle.” In 2020 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac51589.2020.9327809
• Liu, Jiahui, Qi Luo, Jiaxin Lou, and Yuankai Li. 2020e. “Space Infrared Tracking of a Hypersonic Cruise Vehicle Using an Adaptive Scaling UKF.” Aerospace Systems 3 (4): 287–96. https://doi.org/10.1007/s42401-020-00061-y
• Liu, Yue, Philip K. Maini, and Ruth E. Baker. 2026i. “Optimal Experiment Design for Practical Parameter Identifiability and Model Discrimination.” Mathematical Biosciences 399: 109710. https://doi.org/10.1016/j.mbs.2026.109710
• Liu, Lili, Rongjun Mu, and Naigang Cui. 2025m. “A Trajectory Tracking Algorithm of Ballistic Missile in the Ascent Phase with Unknown Noise Statistical Characteristics.” Mechanical Systems and Signal Processing 235: 112952. https://doi.org/10.1016/j.ymssp.2025.112952
• Liu, Qili, Andrea Passaro, Damiano Baccarella, and Hyungrok Do. 2014c. “Ethylene Flame Dynamics and Inlet Unstart in a Model Scramjet.” Journal of Propulsion and Power 30 (6): 1577–85. https://doi.org/10.2514/1.b35214
• Liu, Shanzhong, Xiumin Qu, and Yongbin Liu. 2016b. “Design of Missile Autopilot Based on Fuzzy Control.” In 2016 IEEE International Conference on Information and Automation (ICIA). IEEE. https://doi.org/10.1109/icinfa.2016.7832027
• Liu, Bangshang, Vasko Sazdovski, and Klaus Janschek. 2022l. “Relative Flash LiDAR Aided-Inertial Navigation Using Surfel Grid Maps.” In 2022 IEEE Aerospace Conference (AERO). IEEE. https://doi.org/10.1109/aero53065.2022.9843616
• Liu, Xinfu, and Zuojun Shen. 2015. “Rapid Smooth Entry Trajectory Planning for High Lift/Drag Hypersonic Glide Vehicles.” Journal of Optimization Theory and Applications 168 (3): 917–43. https://doi.org/10.1007/s10957-015-0831-8
• Liu, Tianbo, and Shaojie Shen. 2017. “High Altitude Monocular Visual-Inertial State Estimation: Initialization and Sensor Fusion.” In 2017 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2017.7989528
• Liu, Xinge, Haibin Sun, and Jiayuan Shan. 2017c. “Composite Anti-Disturbance Autopilot Design for Missile System with Angle Constraint.” In IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society. IEEE. https://doi.org/10.1109/iecon.2017.8217053
• Liu, Yu, Baisheng Sun, Ping Yue, Qinwen Yan, and Fuxue Zhang. 2010c. “Study of a MEMS Gyroscope Sensing Unit Simulate and Process.” In ICCAS 2010. IEEE. https://doi.org/10.1109/iccas.2010.5669734
• Liu, Kan, and Xinxin Tian. 2012. “Portable Air Defence Missile System Reliability Analysis and Design.” In 2012 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering. IEEE. https://doi.org/10.1109/icqr2mse.2012.6246429
• Liu, Zhe, Pengyu Wang, Rongfeng Cui, Bolin Pan, and Liangjie Gao. 2026k. “Uncertainty Quantification of Aerodynamic Coefficients Based on Improved Kolmogorov–Arnold Networks.” Journal of Aircraft: 1–10. https://doi.org/10.2514/1.c038847
• Liu, Meiqi, Bo Wang, Zhihong Deng, and Mengyin Fu. 2014d. “Improved ICCP Algorithm and Its Application in Gravity Matching Aided Inertial Navigation System.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896685
• Liu, Xin, Bo Wang, Zhihong Deng, and Shunting Wang. 2012b. “Rapid Alignment Method of INS with Large Initial Azimuth Uncertainty under Complex Dynamic Disturbances.” In Proceedings of 2012 UKACC International Conference on Control. IEEE. https://doi.org/10.1109/control.2012.6334781
• Liu, Xin, Bo Wang, Zhihong Deng, Shunting Wang, and Hua Liu. 2013b. “Rapid Alignment Method of INS with Large Initial Azimuth Error under Uncertain Flexure Disturbances.” In 2013 9th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc.2013.6606104
• Liu, Wenbin, Youshan Wang, and Yuchen Ji. 2023c. “Landing Impact Load Analysis and Validation of a Civil Aircraft Nose Landing Gear.” Aerospace 10 (11): 953. https://doi.org/10.3390/aerospace10110953
• Liu, Bing, Yibing Wang, Jian Liu, and Anjing Chen. 2023i. “Self-Calibration Method of Circular Grating Error in Rotary Inertial Navigation.” In 2023 2nd International Symposium on Sensor Technology and Control (ISSTC). IEEE. https://doi.org/10.1109/isstc59603.2023.10280887
• Liu, Taiyang, Shicheng Wang, Zhiguo Liu, Haibo Min, and Renbing Li. 2010a. “Multi-Kernel SVM Based Star Pattern Recognition for Celestial Navigation.” In 9th IEEE International Conference on Cognitive Informatics (ICCI’10). IEEE. https://doi.org/10.1109/coginf.2010.5599814
• Liu, Feng, Hua Wang, Qingli Shi, Hengxian Wang, Mengying Zhang, and Hailong Zhao. 2017b. “Comparison of an ANFIS and Fuzzy PID Control Model for Performance in a Two-Axis Inertial Stabilized Platform.” IEEE Access 5: 12951–62. https://doi.org/10.1109/access.2017.2723541
• Liu, Da, Jianhua Wang, Peng Wang, and Guojian Tang. 2016d. “Partial Integrated Guidance and Control for Hypersonic Vehicle in Initial Reentry Phase.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7555029
• Liu, Zhuoran, Caizheng Wang, Ke Zhang, Zhuo Zhao, and Zhifeng Xie. 2021c. “Research on Computational Method of Supersonic Inlet/Isolator Internal Flow.” Applied Sciences 11 (19): 9272. https://doi.org/10.3390/app11199272
• Liu, Zhenming, Haoran Wen, and Farrokh Ayazi. 2023d. “A Low-Voltage Wideband AlN-on-Si Gyroscope with Sub 10-DPH Bias Instability Mode Matched Using Laser Trimming.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10104003
• Liu, Pei-Qing, Rui-Ying Wen, Zhen-Gang Liu, and Shu Wu. 2008. “Experimental Study of Canard-Spanwise Pulsed Blowing on a Canard Configuration.” Journal of Aircraft 45 (5): 1816–20. https://doi.org/10.2514/1.36854
• Liu, Bin, and Xiaoyue Wu. 2011. “Mission Reliability Analysis of Missile Defense System Based on DODAF and Bayesian Networks.” In 2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering. IEEE. https://doi.org/10.1109/icqr2mse.2011.5976725
• Liu, Hui, Lin Wu, Lifeng Bao, Qianqian Li, Panpan Zhang, and Yong Wang. 2022h. “Gravity Matching Navigation Algorithm Based on Multiscale Search and Hadamard Transformed Difference.” ISA Transactions 128: 409–22. https://doi.org/10.1016/j.isatra.2021.10.013
• Liu, Shi, Lin Wu, Qianqian Li, Lifeng Bao, and Yong Wang. 2025e. “Gravity Matching Navigation Algorithm Based on Spatial-Frequency Multidimensional Feature Fusion.” IEEE Transactions on Instrumentation and Measurement 74: 1–12. https://doi.org/10.1109/tim.2025.3593611
• Liu, Zhi, Yong Xian, Leliang Ren, Ming Wang, and Liying Qian. 2026h. “Layered Inertial-Terrain-Visual Navigation for UAVs under GNSS-Denied Conditions: A Case Study over the Tibetan Plateau.” Electronics 15 (16): 3559. https://doi.org/10.3390/electronics15163559
• Liu, Yang, Yu Xie, Wei Li, and Yuanlong Zhang. 2021b. “Real-Time Trajectory Prediction for Hypersonic Glide Vehicle Based on 3-D Flight Corridor.” In 2021 6th International Conference on Automation, Control and Robotics Engineering (CACRE). IEEE. https://doi.org/10.1109/cacre52464.2021.9501317
• Liu, Ning, Yuedong Xie, Zhong Su, Zhenyu Zhao, and Wensong Wang. 2025a. “Adaptive Kalman Filter-Integrated Navigation Measurement Using Inertial Sensor for Vehicle Motion State Recognition.” Measurement 248: 116907. https://doi.org/10.1016/j.measurement.2025.116907
• Liu, Haiyang, Junhui Xu, and Zhanchang Zhen. 2018c. “Research on Swaying Base Initial Alignment of Strapdown Inertial Navigation System.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018723
• Liu, Yang, Gongliu Yang, Qingzhong Cai, Lifen Wang, and Suier Wang. 2020c. “Design of External Damping Network and Discretization Algorithm for Long-Endurance Inertial Navigation System.” In 2020 7th International Conference on Information Science and Control Engineering (ICISCE). IEEE. https://doi.org/10.1109/icisce50968.2020.00110
• Liu, Zhen, Tao Yang, Zhongjian Li, and Zhipeng Li. 2022a. “Automatic Landing Trajectory Control of Aircraft Based on Iterative-LQR Algorithm.” In 2022 9th International Forum on Electrical Engineering and Automation (IFEEA). IEEE. https://doi.org/10.1109/ifeea57288.2022.10038260
• Liu, Xiangyang, Jun Yang, and Pengyu Qiao. 2022g. “Gain Function-Based Visual Tracking Control for Inertial Stabilized Platform with Output Constraints and Disturbances.” Electronics 11 (7): 1137. https://doi.org/10.3390/electronics11071137
• Liu, Hai-bo, Jian-kun Yang, Jiong-qi Wang, Ji-chun Tan, and Xiu-jian Li. 2011b. “Star Spot Location Estimation Using Kalman Filter for Star Tracker.” Applied Optics 50 (12): 1735. https://doi.org/10.1364/ao.50.001735
• Liu, Chaojun, Shuai Yu, Shengzhi Zhang, Xuebing Yuan, and Sheng Liu. 2014b. “An Effective Unscented Kalman Filter for State Estimation of a Gyro-Free Inertial Measurement Unit.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851380
• Liu, Jinlai, Tianran Zhang, Lubin Chang, and Pinglan Li. 2025d. “Error Prediction and Simulation of Strapdown Inertial Navigation System Based on Deep Neural Network.” Electronics 14 (13): 2622. https://doi.org/10.3390/electronics14132622
• Liu, Yu, Yuanyuan Zhang, and Renfu Li. 2024d. “Fixed-Time Command-Filtered Adaptive Neural Control for Automatic Carrier Landing.” In 2024 43rd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc63176.2024.10662356
• Liu, Xiangdong, Fengdi Zhang, Zhen Li, and Yao Zhao. 2017a. “Approach and Landing Guidance Design for Reusable Launch Vehicle Using Multiple Sliding Surfaces Technique.” Chinese Journal of Aeronautics 30 (4): 1582–91. https://doi.org/10.1016/j.cja.2017.06.008
• Liu, Shuo, Zhiheng Zhang, Chushu Yi, Jing Chen, and Lina Lu. 2025g. “Mamba-Based Prediction Method for Trajectory Control Parameters of Hypersonic Glide Vehicles.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487632
• Liu, Tianhao, Tianshang Zhao, Huijun Zhao, and Chenguang Wang. 2024b. “Adaptive Cubature Kalman Filter for Inertial/Geomagnetic Integrated Navigation System Based on Long Short-Term Memory Network.” Applied Sciences 14 (13): 5905. https://doi.org/10.3390/app14135905
• Liu, Simin, Zewei Zheng, Zhiyuan Guan, and Kang Lin. 2021a. “Image-Based Visual Servoing Control for Automatic Carrier Landing.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550644
• Liu, Xinyu, Qingfeng Zhou, Xiang Chen, Lisheng Fan, and Chi-Tsun Cheng. 2022c. “Bias-Error Accumulation Analysis for Inertial Navigation Methods.” IEEE Signal Processing Letters 29: 299–303. https://doi.org/10.1109/lsp.2021.3129151
• Liu, Jiawei, Yongkai Zhu, Haitao Wang, Rui Li, Cheng Chen, and Limin Ma. 2026f. “An Integrated FBG Pressure Sensing and Profile Matching Method for Supersonic Inlet Terminal Shock Monitoring.” IEEE Transactions on Instrumentation and Measurement 75: 1–11. https://doi.org/10.1109/tim.2026.3666019
• Liu, Jiawei, Yongkai Zhu, Haitao Wang, Rui Li, Cheng Chen, and Huijun Tan. 2025h. “Measurement of Buzz Flows in a Supersonic Inlet by FBG Sensors.” IEEE Transactions on Instrumentation and Measurement 74: 1–10. https://doi.org/10.1109/tim.2025.3547093
• Lloyd, K. H., and D. P. Brown. 1979. “Instability of Spinning Projectiles during Terminal Guidance.” Journal of Guidance and Control 2 (1): 65–70. https://doi.org/10.2514/3.55833
• Lo, J. T.-H. 1986. “Optimal Estimation for the Satellite Attitude Using Star Tracker Measurements.” Automatica 22 (4): 477–82. https://doi.org/10.1016/0005-1098(86)90052-x
• Logsdon, John M., and Ray A. Williamson. 1997. “The Reusable Launch Vehicle Program.” Space Policy 13 (2): 95–96. https://doi.org/10.1016/s0265-9646(97)00010-6
• Lombardi, G. 1995. “Canard Tip Vortex Splitting in a Canard-Wing Configuration: Experimental Observations.” Journal of Aircraft 32 (4): 875–77. https://doi.org/10.2514/3.46804
• Lopez, R. G. n.d. “An Expert Systems Approach for Automating Performance Analysis of the Air Launch Cruise Missile Tests.” In Proceedings of AUTOTESTCON ‘94. IEEE. https://doi.org/10.1109/autest.1994.381574
• Lorenzini, Enrico C., Gordon E. Gullahorn, and Franco Fuligni. 1988. “Recent Developments in Gravity Gradiometry from the Space-Shuttle-Borne Tethered Satellite System.” Journal of Applied Physics 63. https://ntrs.nasa.gov/citations/19880034304
• Loret, T., G. Hardy, C. Vallee, et al. 2014. “Navigation Grade Accelerometer with Quartz Vibrating Beam.” In 2014 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2014.7049404
• Lou, Qixin, Ding Li, Jingyu Li, et al. 2026. “A Novel Hybrid Mode for Hemispherical Resonator Gyroscope Inertial Navigation Systems: Principle and System-Level Calibration Method.” IEEE Transactions on Industrial Informatics 22 (10): 9212–21. https://doi.org/10.1109/tii.2026.3698512
• Lou, Jing-mei, and Ke Zhang. 2009. “An Intelligent Parameter Space Approach Applicable to Engineering Design of Missile Autopilot.” In 2009 International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2009.5362647
• Lu, Xiaochun, and Juntao Fei. 2014. “Adaptive Iterative Learning Control for MEMS Gyroscope.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896470
• Lu, Cheng, and Juntao Fei. 2015. “Adaptive Backstepping Control of MEMS Gyroscope Based on Neural State Observer.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7259667
• Lu, Pong-Jeu, and Ling-Tzong Jain. 1998. “Numerical Investigation of Inlet Buzz Flow.” Journal of Propulsion and Power 14 (1): 90–100. https://doi.org/10.2514/2.5254
• Lu, Jiazhen, Chaohua Lei, Shufang Liang, and Yanqiang Yang. 2017a. “An All-Parameter System-Level Calibration for Stellar-Inertial Navigation System on Ground.” IEEE Transactions on Instrumentation and Measurement 66 (8): 2065–73. https://doi.org/10.1109/tim.2017.2674758
• Lu, Jiazhen, Chaohua Lei, and Yanqiang Yang. 2017b. “A Dynamic Precision Evaluation Method for the Star Sensor in the Stellar-Inertial Navigation System.” Scientific Reports 7 (1): 4356. https://doi.org/10.1038/s41598-017-04061-5
• Lu, Kun, Bin Li, Xiang Xi, et al. 2024. “Achieving Sub-5-mHz Frequency Split Trimming of Micro Hemispherical Resonator Gyroscope with Method of Mass–Stiffness Decoupling.” IEEE Sensors Journal 24 (15): 23622–31. https://doi.org/10.1109/jsen.2024.3415408
• Lu, Binwen, Jianjun Ma, and Zhiqiang Zheng. 2019. “Adaptive Closed-Loop Control Allocation-Based Fault Tolerant Flight Control for an Overactuated Aircraft.” IEEE Access 7: 179505–16. https://doi.org/10.1109/access.2019.2956818
• Lu, Kewen, Xinlong Wang, Bin Wang, Xiaokun Ding, and Xiaodong Hu. 2023. “A High-Precision Online Compensation Method for Random Errors of Optical Gyroscope.” Measurement 222: 113616. https://doi.org/10.1016/j.measurement.2023.113616
• Lu, Tian, Gangyi Wang, Xinguo Wei, and Qiyuan Zhang. 2026. “High-Accuracy Attitude Estimation with Anisotropic Error Weighting for Star Sensors under Dynamic Conditions.” Measurement 286: 122405. https://doi.org/10.1016/j.measurement.2026.122405
• Lü, Shaolin, Ling Xie, and Jiabin Chen. 2009. “New Techniques for Initial Alignment of Strapdown Inertial Navigation System.” Journal of the Franklin Institute 346 (10): 1021–37. https://doi.org/10.1016/j.jfranklin.2009.09.003
• Lu, Jiazhen, and Lie Yang. 2018. “Optimal Scheme of Star Observation of Missile-Borne Inertial Navigation System/stellar Refraction Integrated Navigation.” Review of Scientific Instruments 89 (5): 054501. https://doi.org/10.1063/1.5020226
• Lu, Han, Jing Zhan-rong, Wei Ming-ming, and Zhang Li-xin. 2009. “Adaptive Extended Kalman Filter Based on Genetic Algorithm for Tightly-Coupled Integrated Inertial and GPS Navigation.” In 2009 Second International Conference on Intelligent Computation Technology and Automation. IEEE. https://doi.org/10.1109/icicta.2009.132
• Lu Keke, Yu Jinyong, and Kou Kunhu. 2016. “The Top-Level Design Study for the Automatic Carrier Landing System.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7829047
• Lubin Chang, Jingshu Li, and Shengyong Chen. 2015. “Initial Alignment by Attitude Estimation for Strapdown Inertial Navigation Systems.” IEEE Transactions on Instrumentation and Measurement 64 (3): 784–94. https://doi.org/10.1109/tim.2014.2355652
• Ludher, Ajay Singh, Marium Tawhid, and Hashim A. Hashim. 2021. “Nonlinear Deterministic Filter for Inertial Navigation and Bias Estimation with Guaranteed Performance.” In 2021 IEEE International Intelligent Transportation Systems Conference (ITSC). IEEE. https://doi.org/10.1109/itsc48978.2021.9565015
• Lungu, Mihai. 2022. “Backstepping and Dynamic Inversion Control Techniques for Automatic Landing of Fixed Wing Unmanned Aerial Vehicles.” Aerospace Science and Technology 120: 107261. https://doi.org/10.1016/j.ast.2021.107261
• Lungu, Romulus, and Mihai Lungu. 2015a. “Automatic Control of Aircraft in Lateral-Directional Plane during Landing.” Asian Journal of Control 18 (2): 433–46. https://doi.org/10.1002/asjc.1133
• Lungu, Mihai, and Romulus Lungu. 2016. “Automatic Control of Aircraft Lateral-Directional Motion during Landing Using Neural Networks and Radio-Technical Subsystems.” Neurocomputing 171: 471–81. https://doi.org/10.1016/j.neucom.2015.06.084
• Luo, Kaixin, Shaokun Cai, Ruihang Yu, Juliang Cao, and Yan Guo. 2022. “Robust Two-Stage Filtering for INS/Gravity Matching Passive Integrated Navigation Systems.” IEEE Sensors Journal 22 (4): 3370–81. https://doi.org/10.1109/jsen.2021.3138793
• Luo, Wenguo, Yuqing Wei, Ke Dai, Jianfeng Zhu, and Yancheng You. 2020. “Spatiotemporal Characterization and Suppression Mechanism of Supersonic Inlet Buzz with Proper Orthogonal Decomposition Method.” Energies 13 (1): 217. https://doi.org/10.3390/en13010217
• Luo, Delin, Jinpeng Zhang, and Yong Liu. 2016. “Autopilot Design for Bank to Turn Missile.” In 2016 12th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2016.7505310
• Luong, Quoc-Viet, Quang-Ngoc Le, Jai-Hyuk Hwang, and Thi-My-Nu Ho. 2025. “6DOF Aircraft Landing Gear System with Magnetorheological Damper in Various Taxing and Touchdown Scenarios.” Micromachines 16 (3): 355. https://doi.org/10.3390/mi16030355
• Lutgring, Stephen, and Emil Tchilian. 2022. “Performance Testing a New Medium Accuracy Star Tracker.” In 2022 IEEE Aerospace Conference (AERO). IEEE. https://doi.org/10.1109/aero53065.2022.9843644
• Lux, P., and M. Eibert. n.d. “ISS: A Combined Terrain Topography Referenced Navigation System.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66216
• Luz, Rute, Jose Luis Silva, and Rodrigo Ventura. 2023. “Enhanced Teleoperation Interfaces for Multi-Second Latency Conditions: System Design and Evaluation.” IEEE Access 11: 10935–53. https://doi.org/10.1109/access.2023.3240307
• Lv, Ding, Qian Long-jun, Sun Rui-sheng, and Yu Ting. 2019. “Autopilot Design for Elastic Missile Systems.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865914
• Lv, Jinan, Fangjian Wang, Li Guo, and Ziqiang Liu. 2015. “CFD/CSD Approach to Predict Hypersonic Aerothermoelastic Response of a Wing.” Procedia Engineering 126: 123–27. https://doi.org/10.1016/j.proeng.2015.11.192
• Lykken, Lowell O., and Naren M. Shah. 1972. “Direct Lift Control for Improved Automatic Landing and Performance of Transport Aircraft LOWELL.” Journal of Aircraft 9 (5): 325–32. https://doi.org/10.2514/3.58988
• Lynch, M. F., and D. J. Weber. n.d. “Flight Test Results of a Tightly Integrated RLG-Based Global Positioning System/inertial Navigation System.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66209
• Lyons, Lawrence W. 1972. “New Method for the Alignment of Inertial Navigation Systems.” Journal of Aircraft 9 (6): 433–37. https://doi.org/10.2514/3.59008
• Lyu, Weiwei, and Xianghong Cheng. 2017. “A Novel Adaptive H∞ Filtering Method with Delay Compensation for the Transfer Alignment of Strapdown Inertial Navigation Systems.” Sensors 17 (12): 2753. https://doi.org/10.3390/s17122753
• Lyu, Donghui, Jiongqi Wang, Zhangming He, Yuyun Chen, and Bowen Hou. 2020. “Landmark-Based Inertial Navigation System for Autonomous Navigation of Missile Platform.” Sensors 20 (11): 3083. https://doi.org/10.3390/s20113083
• Lyu, Huitao, Yong Yin, Zheng Gong, Yongliang Chen, Yalei Bai, and Xueqiang Liu. 2023. “Short Landing for Flying-Wing Unmanned Aircraft with Thrust Vector.” Applied Sciences 13 (6): 3518. https://doi.org/10.3390/app13063518
• Lyu, Pin, Chengyou Yong, Jizhou Lai, Cheng Yuan, Qianqian Zhu, and Adong Han. 2024a. “A Low-Altitude UAV Dataset Based on Visual–Inertial Navigation.” IEEE Sensors Journal 24 (24): 41904–11. https://doi.org/10.1109/jsen.2024.3488289
• Lyu, Xu, Jiupeng Zhu, Jungang Wang, Ruiqi Dong, Shiyi Qian, and Baiqing Hu. 2024b. “A Novel Method for Damping State Switching Based on Machine Learning of a Strapdown Inertial Navigation System.” Electronics 13 (17): 3439. https://doi.org/10.3390/electronics13173439
• Ma, Liheng, Dongkai Dai, and Yuanman Ni. 2025a. “How to Improve the Attitude Accuracy of the Star Sensor under Dynamic Conditions: A Review.” Acta Astronautica 233: 42–54. https://doi.org/10.1016/j.actaastro.2025.03.043
• Ma, Yunpeng, Zhiyuan Guan, and Zewei Zheng. 2018. “Nonlinear Control for Automatic Carrier Landing with Deck Motion Compensation.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8482717
• Ma, Chongyang, Jie Lin, Yang Zhao, et al. 2024a. “Low Noise Temperature Compensation Strategy for North-Finding MEMS Gyroscope.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10784590
• Ma, Yunqian, and John B. McKitterick. 2012. “Range Sensor Aided Inertial Navigation Using Cross Correlation on the Evidence Grid.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236911
• Ma, Zixuan, and Bo Wang. 2019. “An Improved Vector Matching Algorithm for Underwater Gravity Aided Navigation.” In 2019 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac48633.2019.8996871
• Ma, Zixuan, Bo Wang, Liu Huang, Fang Cui, Zhihong Deng, and Mengyin Fu. 2023a. “Dimension-Expanded-Based Matching Method with Siamese Convolutional Neural Networks for Gravity-Aided Navigation.” IEEE Transactions on Industrial Electronics 70 (10): 10496–10505. https://doi.org/10.1109/tie.2022.3222591
• Ma, Liheng, Dejun Zhan, Guangwen Jiang, et al. 2015. “Attitude-Correlated Frames Approach for a Star Sensor to Improve Attitude Accuracy under Highly Dynamic Conditions.” Applied Optics 54 (25): 7559. https://doi.org/10.1364/ao.54.007559
• Maarten Uijt de Haag, A. Vadlamani, J. L. Campbell, and J. Dickman. 2006. “Application of Laser Range Scanner Based Terrain Referenced Navigation Systems for Aircraft Guidance.” In Third IEEE International Workshop on Electronic Design, Test and Applications (DELTA’06). IEEE. https://doi.org/10.1109/delta.2006.15
• MACKlNNON, Duncan, and Paul Madden. 1972. “Performance Limits of a Radio-Inertial Lateral Control System for Automatic Landing.” Journal of Aircraft 9 (8): 513–20. https://doi.org/10.2514/3.59028
• Madhumitha, R., and Srinibas Karmakar. 2024. “Boron-Loaded Gel Fuel as Potential Fuel for Ramjet and Scramjet Engines- Recent Advancements.” FirePhysChem 4 (3): 185–200. https://doi.org/10.1016/j.fpc.2023.07.003
• Maeda, D., K. Ono, J. Giner, et al. 2017. “MEMS Gyroscope with Less than 1-Deg/h Bias Instability Variation in Temperature Range from —40 °C to 125 °C.” IEEE Sensors Journal: 1–1. https://doi.org/10.1109/jsen.2017.2781225
• Maghsoudi, Iman, Mohammad Ali Vaziry, and Mostafa Mahmoodi. 2020. “Experimental Investigation of Flow and Distortion Mitigation by Mechanical Vortex Generators in a Coupled Serpentine Inlet-Turbofan Engine System.” Chinese Journal of Aeronautics 33 (5): 1375–91. https://doi.org/10.1016/j.cja.2019.12.002
• Magree, Daniel, and Eric N. Johnson. 2016. “Factored Extended Kalman Filter for Monocular Vision-Aided Inertial Navigation.” Journal of Aerospace Information Systems 13 (12): 475–90. https://doi.org/10.2514/1.i010419
• Mahdianfar, Hessam, and Emmanuel Prempain. 2016. “Adaptive Augmenting Control Design for a Generic Longitudinal Missile Autopilot.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7525400
• Mahi, Zoubida. 2025b. “Star Spots Extraction Method for Star Tracker in Dynamic Imaging Conditions.” In 2025 2nd International conference on Advances in Electronics, Control and Communication Systems (ICAECCS). IEEE. https://doi.org/10.1109/icaeccs68240.2025.11384770
• Mahi, Zoubida, and Moussa Sofiane Karoui. 2019. “A Comparative Study of Star Detection Methods for a Satellite-Onboard Star Tracker.” In 2019 International Conference on Advanced Electrical Engineering (ICAEE). IEEE. https://doi.org/10.1109/icaee47123.2019.9015160
• Mahi, Zoubida, Moussa Sofiane Karoui, and Mokhtar Keche. 2023. “A New Star Detection Approach for a Satellite-Onboard Star Tracker.” Advances in Space Research 72 (6): 2336–50. https://doi.org/10.1016/j.asr.2023.06.010
• Malakar, Bidhan, and B. K. Roy. 2014. “A Novel Application of Adaptive Filtering for Initial Alignment of Strapdown Inertial Navigation System.” In 2014 International Conference on Circuits, Systems, Communication and Information Technology Applications (CSCITA). IEEE. https://doi.org/10.1109/cscita.2014.6839257
• Malanowski, Mateusz, and Krzysztof Kulpa. 2009. “Analysis of Bistatic Tracking Accuracy in Passive Radar.” In 2009 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2009.4976972
• Malmuth, N., C. C. Wu, and J. D. Cole. 1987. “Transonic Wave Drag Estimation and Optimization Using the Nonlinear Area Rule.” Journal of Aircraft 24 (3): 203–10. https://doi.org/10.2514/3.45417
• Manchester, Ian R. 2010. “Input Design for System Identification via Convex Relaxation.” In 49th IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2010.5717097
• Mandour, I. A., and M. M. El-Dakiky. 1988. “Inertial Navigation System Synthesis Approach and Gravity-Induced Error Sensitivity.” IEEE Transactions on Aerospace and Electronic Systems 24 (1): 40–50. https://doi.org/10.1109/7.1034
• Manjarrez, Hector, Jorge Davila, and Rogelio Lozano. 2018. “Low Level Control Architecture for Automatic Takeoff and Landing of Fixed Wing UAV.” In 2018 Annual American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc.2018.8430789
• Mann, Michael J., and Harry W. Carlson. 1994. “Aerodynamic Design of Supersonic Cruise Wings with a Calibrated Linearized Theory.” Journal of Aircraft 31 (1): 35–41. https://doi.org/10.2514/3.46452
• Mao, Xiangyu, and Jianping He. 2022. “Distributed Input Design with Combination of System Identification and Reinforcement Learning.” In 2022 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus55513.2022.9987073
• Mao, Ning, An Li, Jiangning Xu, and Fangjun Qin. 2025. “A Multi-Resolution Sequence Method with Strong Constraints for Marine Gravity Matching Navigation.” Journal of Marine Science and Engineering 13 (3): 542. https://doi.org/10.3390/jmse13030542
• Mao, Ning, Jiangning Xu, Jingshu Li, and Hongyang He. 2021. “A LSTM-RNN-Based Fiber Optic Gyroscope Drift Compensation.” Mathematical Problems in Engineering 2021: 1–10. https://doi.org/10.1155/2021/1636001
• Mao, Jianliang, Jun Yang, Qi Li, and Shihua Li. 2017. “Extended-State-Observer-Based Output Feedback Sliding Mode Control of Inertial Stabilized Platform.” In 2017 12th IEEE Conference on Industrial Electronics and Applications (ICIEA). IEEE. https://doi.org/10.1109/iciea.2017.8283081
• Mapurunga, Eduardo, and Alexandre Sanfelice Bazanella. 2021. “Identifiability of Dynamic Networks from Structure.” IFAC-PapersOnLine 54 (7): 55–60. https://doi.org/10.1016/j.ifacol.2021.08.334
• Marbel, Revital, Boaz Ben-Moshe, and Roi Yozevitch. 2016. “Star Tracker for Mobile Applications.” In 2016 IEEE International Conference on the Science of Electrical Engineering (ICSEE). IEEE. https://doi.org/10.1109/icsee.2016.7806068
• Marchesoni, Fabio. 1986. “Harmonic Mixing Signal: Doubly Dithered Ring Laser Gyroscope.” Physics Letters A 119 (5): 221–24. https://doi.org/10.1016/0375-9601(86)90452-4
• Marconi, Jacopo, Giacomo Bonaccorsi, Daniele Giannini, Luca Falorni, and Francesco Braghin. 2021. “Exploiting Nonlinearities for Frequency-Matched MEMS Gyroscopes Tuning.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430478
• Margun, Alexey, Radda Iureva, and Daniil Antonov. 2024. “Machine Learning Approaches for Failures Detection in Inertial Navigation Systems.” In 2024 International Russian Smart Industry Conference (SmartIndustryCon). IEEE. https://doi.org/10.1109/smartindustrycon61328.2024.10515549
• Marin, Mikael, and Hyochoong Bang. 2018. “High Update Rate Star Tracker for Gyroless Spacecraft Operation.” In 2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2018.8453507
• Marin, Mikaël, and Hyochoong Bang. 2020. “Design and Simulation of a High-Speed Star Tracker for Direct Optical Feedback Control in ADCS.” Sensors 20 (8): 2388. https://doi.org/10.3390/s20082388
• Marino, Alexis, Robert Pöhlmann, and Emanuel Staudinger. 2026. “Observability Analysis of Simultaneous Localization & Calibration for Cooperative Radio Navigation.” In 2026 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero66936.2026.11519855
• Marinushkin, Pavel S., and Ilya A. Podshivalov. 2015. “MEMS-Based Non-Orthogonal Redundant Inertial Measurement Unit for Miniature Navigation Systems.” In 2015 International Siberian Conference on Control and Communications (SIBCON). IEEE. https://doi.org/10.1109/sibcon.2015.7147138
• Marjoux, D., Ph Ullah, N. Frantz-Rodriguez, et al. 2020. “Silicon MEMS by Safran: Navigation Grade Accelerometer Ready for Mass Production.” In 2020 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss50053.2020.9244881
• Markley, F. L. 1982. “Geopositioning Accuracy of an Autonomous Navigation System Using Landmarks.” In 1982 American Control Conference. IEEE. https://doi.org/10.23919/acc.1982.4787929
• Markó, Norbert, Tamás Szirányi, and Áron Ballagi. 2023. “Terrain Depth Estimation for Improved Inertial Data Prediction in Autonomous Navigation Systems.” In 2023 IEEE International Automated Vehicle Validation Conference (IAVVC). IEEE. https://doi.org/10.1109/iavvc57316.2023.10328139
• Markopoulos, Nikos, and Kenneth D. Mease. 1996. “Altitude for Maximum Angular Velocity about the Earth during Hypersonic Cruise.” Journal of Guidance, Control, and Dynamics 19 (5): 1193–95. https://doi.org/10.2514/3.21767
• Marolleau, E., P. Martin, P. Rouchon, and P. Ullah. 2024. “Can a Perfect Vibratory Gyroscope Provide a Drift-Free Angle Estimation?” In 2024 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa62769.2024.10786089
• Marom, Hagay, Yaakov Bar-Shalom, and Benny Milgrom. 2023. “Bistatic Radar Tracking with Significantly Improved Bistatic Range Accuracy.” IEEE Transactions on Aerospace and Electronic Systems 59 (1): 52–62. https://doi.org/10.1109/taes.2022.3189332
• Marquette, Brandeis, John Miller, J. Doug Jordan, Ted Kim, and Armin Doerry. 2010. “SAR Image Feedback for Improved Inertial Measurement Unit Alignment.” In 2010 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2010.5494536
• Marsh, B. W., and G. A. Sears. 1954. “Introduction to the Analysis of Supersonic Ramjet Power Plants.” Journal of Jet Propulsion 24 (3): 155–61. https://doi.org/10.2514/8.6480
• Marstrander, J., and R. Lueg. 1969. “Limit Cycle Determination for Instrument Servomechanism with Backlash.” IEEE Transactions on Automatic Control 14 (6): 756–57. https://doi.org/10.1109/tac.1969.1099322
• Marti, L. M. n.d. “Integration of Local Area Augmentation System and Inertial Navigation System for Aircraft Surface Movement Guidance.” In 19th DASC. 19th Digital Avionics Systems Conference. Proceedings (Cat. No.00CH37126), vol. 1. IEEE. https://doi.org/10.1109/dasc.2000.886916
• Martinenq, Jean-Pascal. 2021. “Inertial Measurement Unit for Trajectography.” In 2021 2nd International Conference on Range Technology (ICORT). IEEE. https://doi.org/10.1109/icort52730.2021.9581522
• Maruyama, D., K. Matsushima, K. Kusunose, and K. Nakahashi. 2009. “Three-Dimensional Aerodynamic Design of Low-Wave-Drag Supersonic Biplane Using Inverse Problem Method.” Journal of Aircraft 46 (6): 1906–18. https://doi.org/10.2514/1.40313
• Marwan, Tedjini, Alexandre Kechaf, Alain Giani, et al. 2019. “A New Gas Flow Gyroscope MEMS for Harsh Environment Applications.” In 2019 Symposium on Design, Test, Integration & Packaging of MEMS and MOEMS (DTIP). IEEE. https://doi.org/10.1109/dtip.2019.8752676
• Marx, M., S. Bange, X. Cuignet, et al. 2025. “A Closed-Loop MEMS Gyroscope with Optimized Electronics for Achieving Sub-2 M°/√h Angular Random Walk and Sub-4 M°/h Bias Instability.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279638
• Marx, Maximilian, Daniel De Dorigo, Sebastian Nessler, Stefan Rombach, and Yiannos Manoli. 2018. “A 27 µ W 0.06 mm2 Background Resonance Frequency Tuning Circuit Based on Noise Observation for a 1.71 mW CT- Δ σ MEMS Gyroscope Readout System with 0.9 °/h Bias Instability.” IEEE Journal of Solid-State Circuits 53 (1): 174–86. https://doi.org/10.1109/jssc.2017.2747215
• Marx, Maximilian, Daniel De Dorigo, Sebastian Nessler, Stefan Rombach, Michael Maurer, and Yiannos Manoli. 2017. “9.4 a 27µW 0.06mm2 Background Resonance Frequency Tuning Circuit Based on Noise Observation for a 1.71mW CT-ΔΣ MEMS Gyroscope Readout System with 0.9°/h Bias Instability.” In 2017 IEEE International Solid-State Circuits Conference (ISSCC). IEEE. https://doi.org/10.1109/isscc.2017.7870312
• Masafumi Morimoto, Kenji Uchiyama, Yuzo Shimada, and Akio Abe. 2007. “Adaptive Attitude Control with Reduced Number of Estimated Parameters for Automatic Landing System.” In 2007 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2007.4406858
• Maslov, A. A., D. A. Maslov, and I. V. Merkuryev. 2023. “The Effect of the Reference Voltage on the Drift of a Wave Solid-State Gyroscope with Flat Electrodes.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168316
• Masood-Ur-Rehman, Fang Jiancheng, Faycal Saffih, and Quan Wei. 2008. “Single Star Identification and Attitude Determination in Tracking Mode.” In 2008 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2008.4694319
• Massoumnia, Mohammad-Ali. 1991. “Optimal Test Procedures for Evaluating Circular Probable Error.” Journal of Guidance, Control, and Dynamics 14 (6): 1326–28. https://doi.org/10.2514/3.20794
• Mateus, Carlos F. R., Camila D. Sardeto, and Carmem Lucia Barbosa. 2009. “Low Drift and High Sensitivity Fiber Optic Gyroscope Using Tunable VCSEL as Optical Source.” In 2009 IEEE LEOS Annual Meeting Conference Proceedings. IEEE. https://doi.org/10.1109/leos.2009.5343255
• Mathews, Kenneth C. 1960. “Missile Orientation Errors in Command Guidance Systems.” ARS Journal 30 (1): 46–50. https://doi.org/10.2514/8.4983
• Mathisen, Pal H., and Thor I. Fossen. 2019. “Robust Navigation System for UAVs in GNSS-and Magnetometer-Denied Environments.” In 2019 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2019.8797933
• Matt, Justin J., Haiyang Chao, Mosarruf H. Shawon, Benjamin C. Svoboda, and Steven G. Hagerott. 2025. “System Identification for Small Flying-Wing Unmanned Aircraft Using Open-Loop and Closed-Loop Flight Data.” Journal of Aircraft 62 (4): 961–77. https://doi.org/10.2514/1.c038147
• Matthews, A., and F. J. Rybak. 1992. “Comparison of Hemispherical Resonator Gyro and Optical Gyros.” IEEE Aerospace and Electronic Systems Magazine 7 (5): 40–46. https://doi.org/10.1109/62.257091
• Matveev, V. V. 2017. “Strapdown Inertial Navigation System of a Rotating Carrier.” In 2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2017.7995628
• Maulani, Rizal, Zulkifli Hidayat, and Abdullah Alkaff. 2026. “Missile Roll and Acceleration Autopilot Design Based on Linear Active Disturbance Rejection Control.” Aerospace Systems 9 (2): 439–52. https://doi.org/10.1007/s42401-026-00488-9
• Mavriplis, Dimitri J., and David W. Levy. 2005. “Transonic Drag Prediction Using an Unstructured Multigrid Solver.” Journal of Aircraft 42 (4): 887–93. https://doi.org/10.2514/1.8233
• May, M., J. A. Lowrey, and M. Aikawa. n.d. “VERDICT-a Plan for Gravity Compensation of Inertial Navigation Systems.” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195495
• Mayer, David W., and Gerald C. Paynter. 1995. “Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances.” AIAA Journal 33 (2): 266–75. https://doi.org/10.2514/3.12418
• Mayr, Simon, Gernot Grabmair, and Johann Reger. 2017. “Input Design and Online System Identification Based on Poisson Moment Functions for System Outputs with Quantization Noise.” In 2017 25th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med.2017.7984090
• Mazhar, Muhammad Fawad, Muhammad Wasim, Manzar Abbas, et al. 2025. “Aerodynamic Model Identification of Supersonic Aircraft Using Bayesian Approach-Based Box–Jenkins Structure.” Alexandria Engineering Journal 127: 472–85. https://doi.org/10.1016/j.aej.2025.04.059
• McBryde, C. R., and E. G. Lightsey. 2012. “A Star Tracker Design for CubeSats.” In 2012 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2012.6187242
• McClelland, Matthew, Zachary Cohen, Michael D. M. Kutzer, and Levi DeVries. 2025. “Global Navigation Satellite System (GNSS) Emulator for Test and Evaluation of Flight Controller Performance.” In 2025 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas65942.2025.11007919
• McComb, Harvey G., and John A. Tanner. 1988. “Topics in Landing Gear Dynamics Research at NASA Langley.” Journal of Aircraft 25 (1): 84–93. https://doi.org/10.2514/3.45545
• McFarland and D’Souza. 1994. “Missile Autopilot Design Using Dynamic Inversion and Structured Singular Value Synthesis.” In Proceedings of IEEE International Conference on Control and Applications CCA-94. IEEE. https://doi.org/10.1109/cca.1994.381180
• McGeer, T., and I. Kroo. 1983. “A Fundamental Comparison of Canard and Conventional Configurations.” Journal of Aircraft 20. https://ntrs.nasa.gov/citations/19840028263
• McNamara, Jack J., and Peretz P. Friedmann. 2011. “Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future.” AIAA Journal 49 (6): 1089–1122. https://doi.org/10.2514/1.j050882
• McNamara, Jack J., Peretz P. Friedmann, Kenneth G. Powell, Biju J. Thuruthimattam, and Robert E. Bartels. 2008. “Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow.” AIAA Journal 46 (10): 2591–2610. https://doi.org/10.2514/1.36711
• Medaglia, Emanuele. 2016. “Autonomous on-Orbit Calibration of a Star Tracker.” In 2016 IEEE Metrology for Aerospace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2016.7573258
• Medianu, Silviu, and Laurent Lefèvre. 2021. “Structural Identifiability of Linear Port Hamiltonian Systems.” Systems & Control Letters 151: 104915. https://doi.org/10.1016/j.sysconle.2021.104915
• Medrano-Cerda, G. A., and A. J. Pritchard. 1988. “Parameter Estimation Algorithms and Robust Identifiability.” International Journal of Control 48 (5): 1915–36. https://doi.org/10.1080/00207178808906296
• Mehrabian, A. R., and J. Roshanian. 2006. “Design of Gain-Scheduled Autopilot for a Highly-Agile Missile.” In 2006 1st International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2006.1627599
• Meisl, Claus J. 1988. “Life-Cycle-Cost Considerations for Launch Vehicle Liquid Propellant Rocket Engine.” Journal of Propulsion and Power 4 (2): 118–26. https://doi.org/10.2514/3.23039
• Mejias, Luis. 2014. “Classifying Natural Aerial Scenery for Autonomous Aircraft Emergency Landing.” In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2014.6842380
• Melamed, Dennis, Connor Hashemi, and Scott McCloskey. 2025. “Quantifying Accuracy of an Event-Based Star Tracker via Earth’s Rotation.” In 2025 IEEE/CVF International Conference on Computer Vision Workshops (ICCVW). IEEE. https://doi.org/10.1109/iccvw69036.2025.00487
• Mele, Benedetto, Mario Ostieri, and Renato Tognaccini. 2017. “Aircraft Lift and Drag Decomposition in Transonic Flows.” Journal of Aircraft 54 (5): 1933–44. https://doi.org/10.2514/1.c034288
• Meng, Hao, and Yingzhen Li. 2014. “Fuzzy Controller Design for Automatic Carrier Landing of Aircraft.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6895687
• Meng, Fan-Qing, Kang-Sheng Tian, and Chang-Fei Wu. 2021. “Distributed Target Assignment Method of Phased-Array Radar Network for Detecting Hypersonic-Glide Vehicle.” In 2021 5th International Conference on Robotics and Automation Sciences (ICRAS). IEEE. https://doi.org/10.1109/icras52289.2021.9476537
• Meng, Xianzong, Qiaochu Wang, Ruoshuai Zhao, Zebin Zhang, and Zhengyin Ye. 2025. “Aerothermoelastic Analysis on the Interaction between Flexible Panels and Swept Shock-Wave/boundary-Layer Interactions Induced by Sharp Fins.” Advances in Aerodynamics 7 (1): 16. https://doi.org/10.1186/s42774-025-00214-7
• Meng, Min, Kai Yang, Wei Su, et al. 2022b. “A Novel Modeling Method Based on 3D CT Images for Dynamics Analysis of the Micro-Hemispherical Resonator Gyroscope.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787721
• Menon, Karthika Jayasankar, Akhil Ck, K. Balaji, and Kailash Karunakaran. 2025. “Analysis of Sand Grain Roughness Effect on Blunt Reusable Launch Vehicle.” Discover Space 129 (1): 14. https://doi.org/10.1007/s11038-025-09574-y
• Menon, P. K., and E. J. Ohlmeyer. 2001. “Integrated Design of Agile Missile Guidance and Autopilot Systems.” Control Engineering Practice 9 (10): 1095–1106. https://doi.org/10.1016/s0967-0661(01)00082-x
• Merkli, Peter E. 1976. “Pressure Recovery in Rectangular Constant Area Supersonic Diffusers.” AIAA Journal 14 (2): 168–72. https://doi.org/10.2514/3.61352
• Merkulov, Gleb, Vitaly Shalumov, and Tal Shima. 2025. “Integrated Midcourse-Terminal Guidance with Delayed Target Selection.” Journal of Guidance, Control, and Dynamics 48 (10): 2243–56. https://doi.org/10.2514/1.g009009
• Mertens, Josef, Karl D. Klevenhusen, and Heinz Jakob. 1987. “Accurate Transonic Wave Drag Prediction Using Simple Physical Models.” AIAA Journal 25 (6): 799–805. https://doi.org/10.2514/3.9703
• Mettler, G. P., and P. D. Towner. 1991. “A Successful Program for Missile Reliability.” In Annual Reliability and Maintainability Symposium. 1991 Proceedings. IEEE. https://doi.org/10.1109/arms.1991.154484
• Meyer, A. D., and D. M. Rozelle. 2012. “Milli-HRG Inertial Navigation System.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236860
• Meyer-Hilberg, J., and T. Jacob. 1994a. “High Accuracy Navigation and Landing System Using GPS/IMU System Integration.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303327
• Meyer-Hilberg, J., and T. Jacob. 1994b. “High Accuracy Navigation and Landing System Using GPS/IMU System Integration.” IEEE Aerospace and Electronic Systems Magazine 9 (7): 11–17. https://doi.org/10.1109/62.295117
• Miani, Theo, Lokesh Gurung, Douglas Young, Guillermo Sobreviela-Falces, Colin Baker, and Ashwin Seshia. 2025. “Effect of Resonator Nonlinearity on the Vibration Rectification Error of a Vibrating Beam Accelerometer.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279495
• Miani, Theo, Niall MacCarthy, Callisto Pili, et al. 2026. “Improvement of Full Scale Range Error in Vibrating Beam Accelerometer Using Scale Factor Cubic Term Correction Method.” In 2026 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial69196.2026.11557786
• Miani, Theo, Thierry Verdot, Audrey Berthelot, et al. 2022. “Nanoresonator-Based Accelerometer with Large Bandwidth and Improved Bias Stability.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787526
• Miao, Tongqiao, Qingsong Li, Xiaoping Hu, Xuezhong Wu, Wenqi Wu, and Dingbang Xiao. 2022b. “Virtual Rotating MEMS Gyrocompassing with Honeycomb Disk Resonator Gyroscope.” IEEE Electron Device Letters 43 (8): 1331–34. https://doi.org/10.1109/led.2022.3185985
• Miao, Tongqiao, Yi Xu, Qingsong Li, et al. 2022a. “Temperature Drift Self-Calibration for Honeycomb-like Disk Resonator Gyroscope.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787729
• Michael A. Bolender. 2006. “Application of Piecewise Linear Control Allocation to Reusable Launch Vehicle Guidance and Control.” In 2006 14th Mediterranean Conference on Control and Automation. IEEE. https://doi.org/10.1109/med.2006.235846
• Michaels, D., and J. Speed. 2005. “Ball Aerospace Star Tracker Achieves High Tracking Accuracy for a Moving Star Field.” In 2005 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2005.1559572
• Mickle, M. C., and J. J. Zhu. n.d.-a. “Nonlinear Missile Planar Autopilot Design Based on PD-Spectrum Assignment.” In Proceedings of the 36th IEEE Conference on Decision and Control, vol. 4. IEEE. https://doi.org/10.1109/cdc.1997.652474
• Miedziński, Dariusz, Kacper Kaczmarek, Piotr Rodo, Nezar Sahbon, Mateusz Sochacki, and Martyna Łukasiewicz. 2023. “Missile Aerodynamics Model Identification Using Flight Data.” In 2023 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero55745.2023.10115928
• Migadel, Tyson E., Derek K. Lastiwka, Artem Korobenko, and Craig T. Johansen. 2026. “Performance Impacts of Preheating the Primary Fuel Jet of an Ejector Ramjet.” Journal of Propulsion and Power 42 (4): 574–89. https://doi.org/10.2514/1.b40070
• Mikko Saukoski. 2006. “Readout and Control Electronics for a Microelectromechanical Gyroscope.” In 2006 IEEE Instrumentation and Measurement Technology Conference Proceedings. IEEE. https://doi.org/10.1109/imtc.2006.235199
• Miles, John W. 1953. “On the Transonic Drag of a Cone Cylinder.” Journal of the Aeronautical Sciences 20 (9): 651–52. https://doi.org/10.2514/8.2780
• Miles, John W. 1954. “On the Transonic Drag of Accelerated Bodies.” Journal of the Aeronautical Sciences 21 (9): 644–45. https://doi.org/10.2514/8.3162
• Miller, Brent A., and Jack J. McNamara. 2018. “Impact of Aerothermodynamic Model Fidelity on Aerothermoelastic Response of a Skin Panel.” AIAA Journal 56 (12): 5028–32. https://doi.org/10.2514/1.j057176
• Minato, Ryojiro. 2016. “Advantage of Ethanol Fuel for Gas Generator Cycle Air Turbo Ramjet Engine.” Aerospace Science and Technology 50: 161–72. https://doi.org/10.1016/j.ast.2015.12.026
• Minato, Ryojiro. 2019. “Alcohol and Alkane Fuel Performance for Gas Generator Cycle Air Turbo Ramjet Engine.” Aerospace Science and Technology 91: 337–56. https://doi.org/10.1016/j.ast.2019.05.023
• Minato, Ryojiro, and Shusei Tamura. 2025. “Preload Characteristics of Metal Particle Damper for Air Turbo Ramjet Engine.” Journal of Vibration Engineering & Technologies 13 (5): 321. https://doi.org/10.1007/s42417-025-01906-6
• Ming, Li, Li Jie, and Zhang Renqiang. 2016. “Unbalance Disturbance Restraining for Inertial Stabilized Platform.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531444
• Ming, Zeng, Zou Zhongxian, Yu Zhiwei, and Zhang Xin. 2015. “An Investigation on the Second-Order Drift Error Coefficient Calibration of Gyroscope by Vibration Table.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260479
• Ming Xin and S. N. Balakrishnan. 2003. “Nonlinear H/sub ∞/ Missile Longitudinal Autopilot Design with θ-D Method.” In Proceedings of the 2003 American Control Conference, 2003., vol. 1. IEEE. https://doi.org/10.1109/acc.2003.1238983
• Minnaar, Nick, and Willie J. Smit. 2017. “Removing Accelerometer Redundancy in Non-Gyro Inertial Measurement Unit.” In 2017 IEEE Africon. IEEE. https://doi.org/10.1109/afrcon.2017.8095695
• Miranda, Martin, Nobuyuki Takei, Yuki Miyazawa, and Mikio Kozuma. 2023. “Multi-Harmonic Modulation in a Fiber-Optic Gyroscope.” Sensors 23 (9): 4442. https://doi.org/10.3390/s23094442
• “Missile Autopilot Design Based on Robust LPV Control.” 2017. Journal of Systems Engineering and Electronics 28 (3): 536. https://doi.org/10.21629/jsee.2017.03.13
• Mitani, Shinji, Kenichiro Nigo, Satoshi Karasawa, Yusaku Tottori, Haruyuki Ehdo, and Taketoshi Takahata. 2018. “Interferometric Fiber-Optic Gyroscope Using Multi-Core Fiber.” In 2018 European Conference on Optical Communication (ECOC). IEEE. https://doi.org/10.1109/ecoc.2018.8535276
• Mithun IM, Shravan Mohan, and Bharath Bhikkaji. 2015. “D-Optimal Input Design for Identification of a Continuous System Using Sum of Squares Polynomial.” In 2015 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2015.7330837
• Mitsutomi, T. 1958. “Characteristics and Stabilization of an Inertial Platform.” IRE Transactions on Aeronautical and Navigational Electronics ANE-5 (2): 95–105. https://doi.org/10.1109/tane3.1958.4201595
• Mizobata, Kazuhide, Taichi Mio, and Katsuya Miyamoto. 2024. “Drag Reduction on the Basis of the Area Rule of the Small-Scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Second Report).” Aerospace 11 (9): 777. https://doi.org/10.3390/aerospace11090777
• Mo, Fan, Zhihong Deng, Bo Wang, and Mengyin Fu. 2010. “Field Calibration for Platform Inertial Navigation System Based on RHKF.” In 2010 International Conference on Intelligent Control and Information Processing. IEEE. https://doi.org/10.1109/icicip.2010.5565272
• Mo, Chen, Xu Jianhua, and Yu Pei. 2018. “Research on the Integrated Navigation Technology of Inertial-Aided Visual Odometry.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019152
• Mohammadkarimi, Hamed, Mahdi Mobtaker, and Mohammad Hossein Alizadeh. 2025. “Theoretical Error Modeling and Analysis of Strapdown Inertial Navigation System Alignment under Zero-Velocity Conditions.” Scientific Reports 15 (1): 41320. https://doi.org/10.1038/s41598-025-25054-9
• Mohan, Shravan, I. M. Mithun, and Bharath Bhikkaji. 2018. “Optimal Input Design for System Identification Using Spectral Decomposition.” International Journal of Control 93 (4): 980–92. https://doi.org/10.1080/00207179.2018.1498597
• Molchanov, A. V., M. V. Chirkin, A. E. Serebryakov, V. V. Klimakov, H. N. Dao, and V. Yu. Mishin. 2018. “The Effect of Slow Fluctuation Processes in the Ring Laser Gyroscope on Its Bias Instability.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405898
• Molinari, Roberto, James Balamuta, Stephane Guerrier, and Jan Skaloud. 2015. “An Inertial Sensor Calibration Platform to Estimate and Select Error Models.” In 2015 International Association of Institutes of Navigation World Congress (IAIN). IEEE. https://doi.org/10.1109/iain.2015.7352255
• Molnar, Szilard, Cosmin Marcu, Ioan Dragomir, and Levente Tamas. 2026. “Camera-Inertial Sensor Extrinsic Calibration.” In 2026 IEEE International Conference on Automation, Quality and Testing, Robotics (AQTR). IEEE. https://doi.org/10.1109/aqtr70159.2026.11577983
• Monaco, Frank A. 1990. “Applied Safety Analysis on Missile Firing Range Project through the Use of the Safety Network.” Safety and Reliability 10 (4): 6–13. https://doi.org/10.1080/09617353.1990.11690571
• Mondal, Sabyasachi, and Radhakant Padhi. 2018. “Angle-Constrained Terminal Guidance Using Quasi-Spectral Model Predictive Static Programming.” Journal of Guidance, Control, and Dynamics 41 (3): 783–91. https://doi.org/10.2514/1.g002893
• Moody, M. V., H. A. Chan, and H. J. Paik. 1986. “Superconducting Gravity Gradiometer for Space and Terrestrial Applications.” Journal of Applied Physics 60. https://ntrs.nasa.gov/citations/19870039926
• Moody, M. V., and H. J. Paik. 2004. “A Superconducting Gravity Gradiometer for Inertial Navigation.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1309073
• Moon, Kyujin, Hojun Kwon, Chang-Kyung Ryoo, and Hongchul Sim. 2018. “Trajectory Estimation for a Ballistic Missile in Ballistic Phase Using IR Images.” In 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2018.8467635
• Moore, J. E. 1984. “A Modern Control Approach to Inertial Instrument Capture Loop Design.” In 1984 American Control Conference. IEEE. https://doi.org/10.23919/acc.1984.4788418
• Moraes, Luiz Felipe M. V., Fabio N. Carvalho, and Henrique P. P. Pereira. 2019. “Characterization and Wave Motion Simulations of MEMS Inertial Sensors Using 6DOF Platform.” In OCEANS 2019 - Marseille. IEEE. https://doi.org/10.1109/oceanse.2019.8867298
• Moranda, P. B. 1959. “Comparison of Estimates of Circular Probable Error.” Journal of the American Statistical Association 54 (288): 794–800. https://doi.org/10.1080/01621459.1959.11683599
• Moranda, P. B. 1960. “Effect of Bias on Estimates of the Circular Probable Error.” Journal of the American Statistical Association 55 (292): 732–35. https://doi.org/10.1080/01621459.1960.10483373
• Moreland, William J. 1964. “Comment on ‘‘Mathematical Analysis of Corotating Nose-Gear Shimmy Phenomenon.’.” AIAA Journal 2 (2): 415–16. https://doi.org/10.2514/3.2329
• Mortari, D., and A. Romoli. n.d. “StarNav III: A Three Fields of View Star Tracker.” In Proceedings, IEEE Aerospace Conference, vol. 1. IEEE. https://doi.org/10.1109/aero.2002.1036827
• Mostafa, Mostafa, Shady Zahran, Adel Moussa, Naser El-Sheimy, and Abu Sesay. 2018a. “Radar and Visual Odometry Integrated System Aided Navigation for UAVS in GNSS Denied Environment.” Sensors 18 (9): 2776. https://doi.org/10.3390/s18092776
• Motohara, S., and A. Ohno. n.d. “Fiber Optic Gyroscope with Single Mode Fiber Coil.” In 8th Optical Fiber Sensors Conference. IEEE. https://doi.org/10.1109/ofs.1992.762950
• Mou, Jiapeng, Jingjing Su, and Tengchao Huang. 2021b. “Research on Data Synchronization Technology between Rotary Table and Fiber Optic Gyroscope.” Measurement 173: 108579. https://doi.org/10.1016/j.measurement.2020.108579
• Mou, Jiapeng, Jingjing Su, Lijun Miao, and Tengchao Huang. 2021a. “Misalignment Angle Measurement and Angle Measurement Deviation Compensation of Fiber Optic Gyroscope Based on Tilt Sensor.” Optical Fiber Technology 63: 102509. https://doi.org/10.1016/j.yofte.2021.102509
• Mourikis, Anastasios I., and Stergios I. Roumeliotis. 2007. “A Multi-State Constraint Kalman Filter for Vision-Aided Inertial Navigation.” In Proceedings 2007 IEEE International Conference on Robotics and Automation. IEEE. https://doi.org/10.1109/robot.2007.364024
• Mourousias, Nikolaos, Adrián García-Gutiérrez, Ahmed Malim, Diego Domínguez Fernández, Benoît G. Marinus, and Mark C. Runacres. 2023. “Uncertainty Quantification Study of the Aerodynamic Performance of High-Altitude Propellers.” Aerospace Science and Technology 133: 108108. https://doi.org/10.1016/j.ast.2023.108108
• Mousa, Mustafa, Kapil Sharma, and Christian Claudel. 2016. “Poster Abstract: Automatic Calibration of Device Attitude in Inertial Measurement Unit Based Traffic Probe Vehicles.” In 2016 15th ACM/IEEE International Conference on Information Processing in Sensor Networks (IPSN). IEEE. https://doi.org/10.1109/ipsn.2016.7460698
• Moussa, Mohamed, Shady Zahran, Mostafa Mostafa, Adel Moussa, Naser El-Sheimy, and Mohamed Elhabiby. 2020. “Optical and Mass Flow Sensors for Aiding Vehicle Navigation in GNSS Denied Environment.” Sensors 20 (22): 6567. https://doi.org/10.3390/s20226567
• Mravec, Tomas, and Peter Vestenicky. 2014. “Increasing Objects Localization Precision by Determination of Inertial Sensor Calibration Constants Using Differential Evolution Algorithm.” In Proceedings of the 2014 15th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/carpathiancc.2014.6843628
• Mu, Biqiang, and Tianshi Chen. 2018. “On Input Design for Regularized LTI System Identification: Power-Constrained Input.” Automatica 97: 327–38. https://doi.org/10.1016/j.automatica.2018.08.010
• Mu, Biqiang, Tianshi Chen, He Kong, Bo Jiang, Lei Wang, and Junfeng Wu. 2023. “On Embeddings and Inverse Embeddings of Input Design for Regularized System Identification.” Automatica 147: 110673. https://doi.org/10.1016/j.automatica.2022.110673
• Mu, Biqiang, Tianshi Chen, and Lennart Ljung. 2017. “On the Input Design for Kernel-Based Regularized LTI System Identification: Power-Constrained Inputs.” In 2017 IEEE 56th Annual Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2017.8264437
• Muchmore, R., and A. Wheelon. 1955. “Line-of-Sight Propagation Phenomena-I. Ray Treatment.” Proceedings of the IRE 43 (10): 1437–49. https://doi.org/10.1109/jrproc.1955.277960
• Mufti, Alfatirta, and Sayed Muchallil. 2017. “Cruise Missile Altitude Control System Design Using Phase-Lead Compensator.” In 2017 International Conference on Electrical Engineering and Informatics (ICELTICs). IEEE. https://doi.org/10.1109/iceltics.2017.8253253
• Mukhina, Maryna, Svitlana Ilnytska, and D. O. Shevchuk. 2020. “Estimation of Image Quality in Visual Aided Navigation System.” In 2020 IEEE 6th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc50359.2020.9255576
• Muller, George L., and William F. Gasko. 1967. “Subsonic-Transonic-Drag of Supersonic Inlets.” Journal of Aircraft 4 (3): 231–36. https://doi.org/10.2514/3.43825
• Mumm, Nils Christian, and Florian Holzapfel. 2017. “Vertical Speed Command Performance Improvement of a Load Factor Command Based Autopilot for Automatic Landing by Shaping the Desired Command during Flare.” In 2017 IEEE Conference on Control Technology and Applications (CCTA). IEEE. https://doi.org/10.1109/ccta.2017.8062608
• Muniraj, Devaprakash, Dany Abou Jaoude, and Mazen Farhood. 2020. “On Using Composability Tools for Reliability Analysis of Unmanned Multi-Aircraft Systems: A Case Study.” IEEE Access 8: 16331–49. https://doi.org/10.1109/access.2020.2966763
• Murakami, A. 2002. “GPS Guided Short Range Missile Launching System.” In 2002 IEEE Position Location and Navigation Symposium (IEEE Cat. No.02CH37284). IEEE. https://doi.org/10.1109/plans.2002.998905
• Murphy, Charles H., and Maynard J. Piddington. 1960. “Aerodynamic Properties of Ring Airfoils in Supersonic Flight.” Journal of the Aerospace Sciences 27 (12): 954–55. https://doi.org/10.2514/8.8820
• Mustafazade, Arif, and Ashwin A. Seshia. 2018. “Compact High-Precision Analog Temperature Controller for MEMS Inertial Sensors.” In 2018 IEEE International Frequency Control Symposium (IFCS). IEEE. https://doi.org/10.1109/fcs.2018.8597565
• Mustashin, Mir Sakib, Mohsen Rahmani, and Kamran Behdinan. 2021. “Experimental Characterization of a Novel Nose Landing Gear Shimmy Damper Using a Small-Scale Test Rig.” Aerospace Science and Technology 112: 106625. https://doi.org/10.1016/j.ast.2021.106625
• Muzumdar, Dinesh V., and David G. Hull. 1996. “Midcourse Guidance for a Short-Range Attack Missile Using Error Compensation.” Journal of Spacecraft and Rockets 33 (2): 191–97. https://doi.org/10.2514/3.26740
• Myers, George H. 1965. “Experience with the Applications of Radio Command Guidance to Satellite Launch Vehicles.” IFAC Proceedings Volumes 2 (1): 51–59. https://doi.org/10.1016/s1474-6670(17)69066-9
• Myers, Dale D. 1992. “The Navaho Cruise Missile—a Burst of Technology.” Acta Astronautica 26 (8–10): 741–48. https://doi.org/10.1016/0094-5765(92)90164-e
• Mynbaev, D. K. 1994. “Errors of an Inertial Navigation Unit Caused by Ring Laser Gyros Errors.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303398
• Nadig, Sachin, Serhan Ardanuc, Bill Clark, and Amit Lal. 2014. “DOME-DISC: Diffractive Optics Metrology Enabled Dithering Inertial Sensor Calibration.” In 2014 IEEE 27th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2014.6765714
• Nakagiri, Shin-ichi. 1997. “Regional Identifiability of Spatially-Varying Parameters in Distributed Parameter Systems of Parabolic Type.” IFAC Proceedings Volumes 30 (11): 353–58. https://doi.org/10.1016/s1474-6670(17)42872-2
• Nan, Fangbo, Zhongxing Gao, Yingbing Han, Haoyu Cui, Lituo Shang, and Yonggang Zhang. 2025. “Self-Calibration for Phase Shift in Coriolis Vibratory Gyroscope with Whole-Angle Mode Operation.” Measurement 242: 116043. https://doi.org/10.1016/j.measurement.2024.116043
• Nan, Tian, Xiang-Ying Guo, Yao Chen, Wei-Xing Zhang, Stefano Lenci, and Lei-Yu Zhang. 2026a. “Multi-Parameter Bifurcation Analysis of Shimmy in a New Configuration Dual-Wheel Nose Landing Gear.” Nonlinear Dynamics 114 (7): 513. https://doi.org/10.1007/s11071-026-12385-z
• Nan, Tian, Stefano Lenci, Yao Chen, Yu-nan Zhu, and Xiang-Ying Guo. 2026b. “Reducing Shimmy Oscillation of Nose Landing Gear Based on a Torsional Nonlinear Energy Sink and an Annular Granular Damper.” European Journal of Mechanics - A/Solids 120: 106210. https://doi.org/10.1016/j.euromechsol.2026.106210
• Napolitano, Marcello R., Yongkyu Song, and Brad Seanor. 2001. “On-Line Parameter Estimation for Restructurable Flight Control Systems.” Aircraft Design 4 (1): 19–50. https://doi.org/10.1016/s1369-8869(00)00023-9
• Narasimhan, Sridharakumar, and Xavier Bombois. 2012. “Plant Friendly Input Design for System Identification in Closed Loop.” IFAC Proceedings Volumes 45 (16): 1335–40. https://doi.org/10.3182/20120711-3-be-2027.00124
• Narasimhan, Sridharakumar, and Raghunathan Rengaswamy. 2006. “Multiobjective Input Design for System Identification- Frequency Selection for Identification of Nonlinear Systems.” IFAC Proceedings Volumes 39 (1): 1139–44. https://doi.org/10.3182/20060329-3-au-2901.00183
• Narasimhan, S., and R. Rengaswamy. 2008. “Multi-Objective Optimal Input Design for Plant Friendly Identification.” In 2008 American Control Conference. IEEE. https://doi.org/10.1109/acc.2008.4586673
• Nash, R. 1968. “The Estimation and Control of Terrestrial Inertial Navigation System Errors Due to Vertical Deflections.” IEEE Transactions on Automatic Control 13 (4): 329–38. https://doi.org/10.1109/tac.1968.1098937
• Nash, Raymond, and Charles Hutchinson. 1973. “Altitude Damping of Space-Stable Inertial Navigation Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-9 (1): 18–27. https://doi.org/10.1109/taes.1973.309696
• Nasir, Muhammad, Dan Xie, Zijun Yi, Tamina Perveen, and Adnan Maqsood. 2026. “Comparative Aerothermoelastic Performance Assessment of Advanced TPS Materials for Hypersonic Vehicles.” Aerospace Science and Technology 173: 111792. https://doi.org/10.1016/j.ast.2026.111792
• Natale, T., P. Peliti, F. Berton, F. Fornari, and F. Dell’Olio. 2023. “Preliminary Assessment of the New Routes towards a Navigation Grade Photonic Chip-Scale Gyroscope.” In 2023 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss58390.2023.10361929
• “National Advisory Committee for Aeronautics. Report No. 518, the Drag of Airplane Wheels, Wheel Fairings, and Landing Gears. II—Nonretractable and Partly Retractable Landing Gears.” 1935. Journal of the Franklin Institute 220 (5): 678. https://doi.org/10.1016/s0016-0032(35)90058-8
• Navarro-Tapia, D., P. Simplício, A. Iannelli, and A. Marcos. 2017. “Robust Flare Control Design Using Structured H∞ Synthesis: A Civilian Aircraft Landing Challenge.” IFAC-PapersOnLine 50 (1): 3971–76. https://doi.org/10.1016/j.ifacol.2017.08.769
• Nazdrowicz, Jacek, and Andrzej Napieralski. 2019. “Modelling, Simulations and Performance Analysis of MEMS Vibrating Gyroscope in Coventor MEMS+ Environment.” In 2019 20th International Conference on Thermal, Mechanical and Multi-Physics Simulation and Experiments in Microelectronics and Microsystems (EuroSimE). IEEE. https://doi.org/10.1109/eurosime.2019.8724520
• Nazemipour, Ali, Mohammad Taghi Manzuri, Danial Kamran, and Mahdi Karimian. 2020. “MEMS Gyro Bias Estimation in Accelerated Motions Using Sensor Fusion of Camera and Angular-Rate Gyroscope.” IEEE Transactions on Vehicular Technology 69 (4): 3841–51. https://doi.org/10.1109/tvt.2020.2976975
• Nebot, Eduardo, and Hugh Durrant-Whyte. 1999. “Initial Calibration and Alignment of Low-Cost Inertial Navigation Units for Land Vehicle Applications.” Journal of Robotic Systems 16 (2): 81–92. https://doi.org/10.1002/(sici)1097-4563(199902)16:2<81::aid-rob2>3.0.co;2-9
• Needham, Timothy G., and Michael S. Braasch. 2020. “Stochastic Modeling of Gravity Compensation Error in GNSS-Aided Inertial Navigation Systems.” In 2020 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans46316.2020.9110195
• Negre, Y. 1977. “All-Weather Automatic Landing Concepts and Operations: Review of Aerospatiale Experience.” Journal of Aircraft 14 (4): 323–26. https://doi.org/10.2514/3.58780
• Negrea, Petre. 2021. “An Overview of Acceleration Detection in Inertial Navigation Systems.” In 2021 International Conference on Applied and Theoretical Electricity (ICATE). IEEE. https://doi.org/10.1109/icate49685.2021.9464969
• Neill, Stephen, and Apostolos Pesyridis. 2017. “Modeling of Supersonic Combustion Systems for Sustained Hypersonic Flight.” Energies 10 (11): 1900. https://doi.org/10.3390/en10111900
• Nejad, Shahram Mohammad, and Maryam Pourmahyabadi. 2006. “The Performance Modeling of Ring Laser Gyro in Inertial Navigation.” In 2006 13th IEEE International Conference on Electronics, Circuits and Systems. IEEE. https://doi.org/10.1109/icecs.2006.379789
• Nelson, H. F., and Brent W. Bossi. 1995. “Aerodynamic Interference for Supersonic Low-Aspect-Ratio Missiles.” Journal of Spacecraft and Rockets 32 (2): 270–78. https://doi.org/10.2514/3.26606
• Nelson, K. D., and F. L. Macklin. 1992. “Flight Results of the Ring Laser Gyro Based Inertial Navigation System for Atlas/Centaur.” In [1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.1992.282119
• Nesline, F. William. 1979. “Missile Guidance for Low-Altitude Air Defense.” Journal of Guidance and Control 2 (4): 283–89. https://doi.org/10.2514/3.55876
• Nesline, F. William, and Mark L. Nesline. 1986. “An Analysis of Optimal Command Guidance vs. Optimal Semi-Active Homing Missile Guidance.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4789100
• Neumann, Richard D., and Delma C. Freeman. 2012. “Experimental Measurement of Aerodynamic Heating about Complex Shapes at Supersonic Mach Numbers.” Journal of Spacecraft and Rockets 49 (6): 1080–87. https://doi.org/10.2514/1.a32201
• Ng, T. S., G. C. Goodwin, and B. D. O. Anderson. 1977. “Identifiability of MIMO Linear Dynamic Systems Operating in Closed Loop.” Automatica 13 (5): 477–85. https://doi.org/10.1016/0005-1098(77)90068-1
• Ng, T. S., and Z. H. Qureshi. 1981. “Optimal Input Design for Parameter Estimation for an Autoregressive Model with Output Power Constraints.” IFAC Proceedings Volumes 14 (2): 643–48. https://doi.org/10.1016/s1474-6670(17)63557-2
• Ng, M., F. Vanegas, K. Morton, J. Sandino, and F. Gonzalez. 2022. “Design and Flight Test of an Aerial Manipulator for Applications in GPS-Denied Environments.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836060
• Nghiem, Cuong P., and Helge Norstrud. 1989. “Design of Axisymmetric Bodies with Minimum Transonic Drag.” AIAA Journal 27 (12): 1818–20. https://doi.org/10.2514/3.10339
• Ngo, A. D., and D. B. Doman. 2002. “Footprint Calculation Methods for a Reusable Launch Vehicle.” In Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301). IEEE. https://doi.org/10.1109/acc.2002.1023917
• Nguyen, D. Dung, Salamatov Dauren, Q. Tru Vu, M. Duc Duong, Kinzhikeeva Dina, and Kinzhikeyev Sergey. 2026. “Design of a Non-Orthogonal Redundant Sensor Block and a Fault Detection and Isolation Algorithm for Inertial Navigation Systems.” In 2026 IEEE 6th International Conference on Smart Information Systems and Technologies (SIST). IEEE. https://doi.org/10.1109/sist61674.2026.11596216
• Nguyen, Trung, George K. I. Mann, Andrew Vardy, and Raymond G. Gosine. 2017a. “Developing a Cubature Multi-State Constraint Kalman Filter for Visual-Inertial Navigation System.” In 2017 14th Conference on Computer and Robot Vision (CRV). IEEE. https://doi.org/10.1109/crv.2017.19
• Nguyen, Trung, George K. I. Mann, Andrew Vardy, and Raymond G. Gosine. 2017b. “Likelihood-Based Iterated Cubature Multi-State-Constraint Kalman Filter for Visual Inertial Navigation System.” In 2017 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros.2017.8206305
• Nguyen, E., and E. Ogier. 2024. “INS Alignment Duration Reduction Using GNSS Heading.” In 2024 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa62769.2024.10786060
• Nho, Kyungmoon, and Ramesh K. Agarwal. 2000. “Automatic Landing System Design Using Fuzzy Logic.” Journal of Guidance, Control, and Dynamics 23 (2): 298–304. https://doi.org/10.2514/2.4522
• Ni, Yuanman, Dongkai Dai, Wenfeng Tan, Xingshu Wang, and Shiqiao Qin. 2023. “Installation Error Calibration Method of Stellar/inertial Integrated Navigation System for Star Tracker with Narrow Field of View.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168471
• Ni, Yuanman, Wenfeng Tan, Dongkai Dai, Xingshu Wang, and Shiqiao Qin. 2021. “A Stellar/inertial Integrated Navigation Method Based on the Observation of the Star Centroid Prediction Error.” Review of Scientific Instruments 92 (3): 035001. https://doi.org/10.1063/5.0027530
• Ni, Yuanman, Xingshu Wang, Dongkai Dai, Wenfeng Tan, and Shiqiao Qin. 2022. “Adaptive Section Non-Uniformity Correction Method of Short-Wave Infrared Star Images for a Star Tracker.” Applied Optics 61 (24): 6992. https://doi.org/10.1364/ao.457458
• Nieminen, Tuukka, Jari Kangas, and Lauri Kettunen. 2011. “Use of Tikhonov Regularization to Improve the Accuracy of Position Estimates in Inertial Navigation.” International Journal of Navigation and Observation 2011: 1–10. https://doi.org/10.1155/2011/450269
• Nieminen, Tuukka, Jari Kangas, Saku Suuriniemi, and Lauri Kettunen. 2010. “Accuracy Improvement by Boundary Conditions for Inertial Navigation.” International Journal of Navigation and Observation 2010: 1–10. https://doi.org/10.1155/2010/869127
• Nieuwenhuisen, Matthias, David Droeschel, Marius Beul, and Sven Behnke. 2015a. “Autonomous MAV Navigation in Complex GNSS-Denied 3D Environments.” In 2015 IEEE International Symposium on Safety, Security, and Rescue Robotics (SSRR). IEEE. https://doi.org/10.1109/ssrr.2015.7443012
• Nieuwenhuisen, Matthias, David Droeschel, Marius Beul, and Sven Behnke. 2015b. “Autonomous Navigation for Micro Aerial Vehicles in Complex GNSS-Denied Environments.” Journal of Intelligent & Robotic Systems 84 (1–4): 199–216. https://doi.org/10.1007/s10846-015-0274-3
• Niknamian, Sorush. 2018. “‘The Optimization of a Jet Turbojet Engine by PSO and Searching Algorithms’.” SSRN Electronic Journal. https://doi.org/10.2139/ssrn.3503740
• Nikolic, Janosch, Michael Burri, Igor Gilitschenski, Juan Nieto, and Roland Siegwart. 2016. “Non-Parametric Extrinsic and Intrinsic Calibration of Visual-Inertial Sensor Systems.” IEEE Sensors Journal 16 (13): 5433–43. https://doi.org/10.1109/jsen.2016.2556662
• Nilsson, John-Olof, Dave Zachariah, Magnus Jansson, and Peter Handel. 2012. “Realtime Implementation of Visual-Aided Inertial Navigation Using Epipolar Constraints.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236948
• Ninalalov, Ibragim, Igor Merkuryev, Oleg Kubryak, and Sergey Astakhov. 2022. “Methods for Improving the Accuracy of an Autonomous Orientation and Navigation System Based on Micromechanical Gyroscopes and Optoelectronic Sensors.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815361
• Ning, Xiaoge, Jixun Huang, and Jianxun Li. 2022b. “A New Method for Inertial Strapdown Navigation System Alignment under Large Misalignment Based on a Velocity Error Transformation.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815407
• Ning, Xiaoge, Jixun Huang, and Jianxun Li. 2023. “Influence of the Kalman Filtering Initial Setting on SINS Initial Alignment and an Improved Method for the Alignment of Large Misalignment Angles.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168421
• Ning, Xiaolin, Xiaohan Sun, and Wen Chao. 2019. “Integration of Star Pixel Coordinates and Their Time Differential Measurement in Satellite Stellar Refraction Navigation.” Acta Astronautica 159: 286–93. https://doi.org/10.1016/j.actaastro.2019.03.052
• Ning, Youhuan, Changhong Wang, Boqi Xi, Zhen Tian, and Boda Zhang. 2025a. “Identification and Correction of Phase Delay Errors for Hemispherical Resonator Gyroscopes.” Scientific Reports 15 (1): 2078. https://doi.org/10.1038/s41598-025-86288-1
• Ning, Youhuan, Changhong Wang, Boqi Xi, Zhen Tian, Boda Zhang, and Wei Cheng. 2025b. “Suppression and Compensation of Damping Asymmetry Errors in Whole-Angle Hemispherical Resonator Gyroscope.” IEEE Sensors Journal 25 (13): 23888–98. https://doi.org/10.1109/jsen.2025.3572313
• Nitzan, S., T-H. Su, C. Ahn, et al. 2014. “Impact of Gyroscope Operation above the Critical Bifurcation Threshold on Scale Factor and Bias Instability.” In 2014 IEEE 27th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2014.6765749
• Niu, Xiaoji, You Li, Hongping Zhang, Qingjiang Wang, and Yalong Ban. 2013. “Fast Thermal Calibration of Low-Grade Inertial Sensors and Inertial Measurement Units.” Sensors 13 (9): 12192–12217. https://doi.org/10.3390/s130912192
• Niu, Yadong, Xuedong Yu, Huabo Zhu, and Wei Zhou. 2024. “Research on Estimation Method for Airport Runway Friction Coefficient Based on Numerical Analysis.” IEEE Access 12: 37615–30. https://doi.org/10.1109/access.2024.3373779
• Niu, Yadong, Sixiang Zhang, Guangjun Tian, Huabo Zhu, and Wei Zhou. 2020. “Estimation for Runway Friction Coefficient Based on Multi-Sensor Information Fusion and Model Correlation.” Sensors 20 (14): 3886. https://doi.org/10.3390/s20143886
• Norton, J. P. 1982. “Parameter Identifiability Analysis by Modal Methods.” IFAC Proceedings Volumes 15 (4): 875–80. https://doi.org/10.1016/s1474-6670(17)63104-5
• Novara, Carlo, Tyrone L. Vincent, and Kameshwar Poolla. 2009. “Implementation of Input Design for Structured Nonlinear System Identification via Linear IMC Control.” IFAC Proceedings Volumes 42 (10): 168–73. https://doi.org/10.3182/20090706-3-fr-2004.00028
• Nowak, Dariusz, Grzegorz Kopecki, Damian Kordos, and Tomasz Rogalski. 2022. “The PAPI Lights-Based Vision System for Aircraft Automatic Control during Approach and Landing.” Aerospace 9 (6): 285. https://doi.org/10.3390/aerospace9060285
• Nunes, Gabriel F. S., and João M. S. Sakamoto. 2024. “Passive Interferometric Fiber-Optic Gyroscope for Aerospace Applications.” In 2024 Latin American Workshop on Optical Fiber Sensors (LAWOFS). IEEE. https://doi.org/10.23919/lawofs62242.2024.10560851
• Nunzi, E. 2006. “A Demodulation Technique for the Sensing Circuit of a MEMS Gyroscope.” In 2006 IEEE Instrumentation and Measurement Technology Conference Proceedings. IEEE. https://doi.org/10.1109/imtc.2006.235198
• Nygren, I., and M. Jansson. 2004. “Terrain Navigation Using the Correlator Method.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1309055
• O’Neil, Stephen J. 1956. “A Servomechanism Approach to the Problem of Communication for Aircraft Control.” IRE Transactions on Aeronautical and Navigational Electronics ANE-3 (2): 55–66. https://doi.org/10.1109/tane3.1956.4201448
• Ober, R. J., Zhiping Lin, and Qiyue Zou. 2005. “On the Identifiability of Bilinear Systems.” In 2005 IEEE International Symposium on Circuits and Systems. IEEE. https://doi.org/10.1109/iscas.2005.1465450
• Oberpeilsteiner, Stefan, Thomas Lauss, Karin Nachbagauer, and Wolfgang Steiner. 2016. “Optimal Input Design for Multibody Systems by Using an Extended Adjoint Approach.” Multibody System Dynamics 40 (1): 43–54. https://doi.org/10.1007/s11044-016-9541-8
• Ochi, Y., and K. Kanai. 1999. “Automatic Approach and Landing for Propulsion Controlled Aircraft by H/sub ∞/ Control.” In Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328), vol. 2. IEEE. https://doi.org/10.1109/cca.1999.800951
• Oderland, I., S. Nordlof, and B. Leijon. n.d. “EAGLE-a High Accuracy 35 GHz Tracking Radar.” In IEEE International Conference on Radar. IEEE. https://doi.org/10.1109/radar.1990.201209
• Oelschlaeger, J. M., and L. O. Thielman. n.d. “GG1308 Ring Laser Gyro Inertial Measurement Systems: Honeywell’s Low-Cost Solution for Tactical Applications.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66224
• Oh, Jongtaek, and Sunghoon Kim. 2024. “Azimuth Estimation Based on CNN and LSTM for Geomagnetic and Inertial Sensors Data.” ICT Express 10 (3): 626–31. https://doi.org/10.1016/j.icte.2024.01.003
• Oh, Juhyun, Chang-Ky Sung, Jungshin Lee, Sang Woo Lee, Sang Jeong Lee, and Myeong-Jong Yu. 2019. “Accurate Measurement Calculation Method for Interferometric Radar Altimeter-Based Terrain Referenced Navigation.” Sensors 19 (7): 1688. https://doi.org/10.3390/s19071688
• Ohno, Masahiro, Yasuhiro Yamaguchi, Takashi Hata, Morio Takahama, Yoshikazu Miyazawa, and Tatsushi Izumi. 1998. “Robust Flight Control Law Design for Automatic Landing Flight Experiment.” IFAC Proceedings Volumes 31 (21): 265–70. https://doi.org/10.1016/s1474-6670(17)41088-3
• Ohno, Masahiro, Yasuhiro Yamaguchi, Takashi Hata, Morio Takahama, Yoshikazu Miyazawa, and Tatsushi Izumi. 1999. “Robust Flight Control Law Design for an Automatic Landing Flight Experiment.” Control Engineering Practice 7 (9): 1143–51. https://doi.org/10.1016/s0967-0661(99)00085-4
• Ohta, Hirobumi, and Ichiro Sugiura. 1973. “Optimal Landing Flare Control of Aircrafts with Sensitivity Consideration.” IFAC Proceedings Volumes 6 (2): 251–59. https://doi.org/10.1016/s1474-6670(17)68196-5
• Ohtsuka, Y. 1985. “Analysis of a Fiber-Optic Passive Loop-Resonator Gyroscope: Dependence on Resonator Parameters and Light-Source Coherence.” Journal of Lightwave Technology 3 (2): 378–84. https://doi.org/10.1109/jlt.1985.1074196
• Okon, Isaak. 2019. “Auto-Compensation Bias and Calibration of Vibrating Coriolis Gyroscope.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769342
• Olivier, Audrey, and Andrew W. Smyth. 2017. “On the Performance of Online Parameter Estimation Algorithms in Systems with Various Identifiability Properties.” Frontiers in Built Environment 3. https://doi.org/10.3389/fbuil.2017.00014
• Ono, Daiki, Ryunosuke Gando, and Yasushi Tomizawa. 2020. “Demonstration of Trajectory Estimation Using a Mobile MEMS Rate Integrating Gyroscope Module.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090025
• Oosterom, M., and R. Babuska. n.d. “Fuzzy Gain Scheduling for Flight Control Laws.” In 10th IEEE International Conference on Fuzzy Systems. (Cat. No.01CH37297), vol. 3. IEEE. https://doi.org/10.1109/fuzz.2001.1009055
• Opitz, Felix. 2006. “Re-Entry Vehicles: Dynamic Modeling and Radar Tracking.” In 2006 International Radar Symposium. IEEE. https://doi.org/10.1109/irs.2006.4338077
• Opromolla, Roberto, Giancarmine Fasano, Giancarlo Rufino, Michele Grassi, Claudio Pernechele, and Cesare Dionisio. 2017. “A New Star Tracker Concept for Satellite Attitude Determination Based on a Multi-Purpose Panoramic Camera.” Acta Astronautica 140: 166–75. https://doi.org/10.1016/j.actaastro.2017.08.020
• “Optimal Disturbance Rejection in Missile Autopilot Design Using Projective Controls.” 1992. IEEE Control Systems 12 (5): 43–49. https://doi.org/10.1109/37.158897
• “Optimal Experiment Design for Dynamic System Identification.” 1981. Mathematics and Computers in Simulation 23 (3): 313. https://doi.org/10.1016/0378-4754(81)90104-x
• Orlando, Calogero. 2020. “Nose Landing Gear Simple Adaptive Shimmy Suppression System.” Journal of Guidance, Control, and Dynamics 43 (7): 1298–1312. https://doi.org/10.2514/1.g004832
• Ornedo, R. S., K. A. Farnsworth, and G. S. Sandhoo. 1998. “GPS and Radar Aided Inertial Navigation System for Missile System Applications.” In IEEE 1998 Position Location and Navigation Symposium (Cat. No.98CH36153). IEEE. https://doi.org/10.1109/plans.1998.670222
• Ostroumov, I. V., and N. S. Kuzmenko. 2016. “Accuracy Estimation of Alternative Positioning in Navigation.” In 2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc.2016.7783164
• Osunluk, B., S. Ogut, and E. Ozbay. 2018. “Reduction of Thermal Strain Induced Rate Error for Navigation Grade Fiber Optic Gyroscope.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577074
• Osunluk, Berk, Serdar Ogut, and Ekmel Ozbay. 2020. “Thermally Induced Bias Error Due to Strain Inhomogeneity through the Fiber Optic Gyroscope Coil.” Applied Optics 59 (33): 10416. https://doi.org/10.1364/ao.406045
• Ou, Min, Li Yan, Jing-feng Tang, Wei Huang, and Xiao-qian Chen. 2017. “Thermodynamic Performance Analysis of Ramjet Engine at Wide Working Conditions.” Acta Astronautica 132: 1–12. https://doi.org/10.1016/j.actaastro.2016.11.036
• Ouda, A. N. 2017. “A Robust Adaptive Control Approach to Missile Autopilot Design.” International Journal of Dynamics and Control 6 (3): 1239–71. https://doi.org/10.1007/s40435-017-0352-4
• Ouyang, Mujiao, Jilin Gao, Ao Li, Xiaoguo Zhang, Chong Shen, and Huiliang Cao. 2024. “Micromechanical Gyroscope Temperature Compensation Based on Combined LSTM-SVM-DBN Algorithm.” Sensors and Actuators A: Physical 369: 115128. https://doi.org/10.1016/j.sna.2024.115128
• Ouyang, W., and Y. Wu. 2022a. “Motion Representation and Inertial Navigation in Clifford Algebras.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926412
• Ouyang, Wei, and Yuanxin Wu. 2022b. “A Trident Quaternion Framework for Inertial-Based Navigation—Part II: Error Models and Application to Initial Alignment.” IEEE Transactions on Aerospace and Electronic Systems 58 (3): 2421–37. https://doi.org/10.1109/taes.2021.3133219
• Ouyang, Xiaofeng, Fangling Zeng, Daqian Lv, Tianbao Dong, and Haibing Wang. 2021. “Cooperative Navigation of UAVs in GNSS-Denied Area with Colored RSSI Measurements.” IEEE Sensors Journal 21 (2): 2194–2210. https://doi.org/10.1109/jsen.2020.3021561
• Pachwicewicz, Marek, and Jerzy Weremczuk. 2018. “Accuracy Estimation of the Sounding Rocket Navigation System.” In 2018 XV International Scientific Conference on Optoelectronic and Electronic Sensors (COE). IEEE. https://doi.org/10.1109/coe.2018.8435180
• Packard, Capt. A. C., and Royal Weiler. 1952. “The Reliability Problems in Guided Missile Development.” Transactions of the IRE Professional Group on Quality Control PGQC-1: 34–41. https://doi.org/10.1109/ire-pgqc.1952.6539077
• Padmanabhan, Madhusudan A., and Earl H. Dowell. 2015. “Landing Gear Design/Maintenance Analysis for Nonlinear Shimmy.” Journal of Aircraft 52 (5): 1707–10. https://doi.org/10.2514/1.c033027
• Pagani, Leonardo Gaffuri, Luca Guerinoni, Luca Falorni, Patrick Fedeli, and Giacomo Langfelder. 2020. “Investigation of Gyroscopes Mechanical and Electronic Phase Drift with 2 μrad/√Hz Resolution and 12 μrad/K Accuracy.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090017
• Pai, P., F. K. Chowdhury, Carlos H. Mastrangelo, and M. Tabib-Azar. 2012. “MEMS-Based Hemispherical Resonator Gyroscopes.” In 2012 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2012.6411346
• Paik, H. J. 1981c. “Superconducting Tensor Gravity Gradiometer for Satellite Geodesy and Inertial Navigation.” Journal of the Astronautical Sciences 29. https://ntrs.nasa.gov/citations/19810045389
• Pain, S., and K. Tiwari. 2013. “A Graphical Design Methodology of Missile Autopilot.” In 2013 International Mutli-Conference on Automation, Computing, Communication, Control and Compressed Sensing (iMac4s). IEEE. https://doi.org/10.1109/imac4s.2013.6526490
• Pakniyat, Ali, and Hassan Salarieh. 2013. “A Parametric Study on Design of a Microrate-Gyroscope with Parametric Resonance.” Measurement 46 (8): 2661–71. https://doi.org/10.1016/j.measurement.2013.03.022
• Pal, Madhumita, and M. Seetharama Bhat. 2009. “Star Camera Calibration Combined with Independent Spacecraft Attitude Determination.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160502
• Pal, Madhumita, and M. Seetharama Bhat. 2013. “Star Sensor Based Spacecraft Angular Rate Estimation Independent of Attitude Determination.” In 2013 IEEE International Conference on Control Applications (CCA). IEEE. https://doi.org/10.1109/cca.2013.6662812
• Pal, Nitai, Roshan Kumar, and Milan Kumar. 2014. “Design of Missile Autopilot Using Backstepping Controller.” In International Conference on Electronics, Communication and Instrumentation (ICECI). IEEE. https://doi.org/10.1109/iceci.2014.6917606
• Pan, Xiong, Pengcheng Liu, Shaobo Zhang, Jing Jin, and Ningfang Song. 2017. “Novel Compensation Scheme for the Modulation Gain to Suppress the Quantization-Induced Bias in a Fiber Optic Gyroscope.” Sensors 17 (4): 823. https://doi.org/10.3390/s17040823
• Pan, Jianye, Chunxi Zhang, Yanxiong Niu, and Zhe Fan. 2014. “Accurate Calibration for Drift of Fiber Optic Gyroscope in Multi-Position North-Seeking Phase.” Optik 125 (24): 7244–46. https://doi.org/10.1016/j.ijleo.2014.07.126
• Panahandeh, Ghazaleh, Chao X. Guo, Magnus Jansson, and Stergios I. Roumeliotis. 2013. “Observability Analysis of a Vision-Aided Inertial Navigation System Using Planar Features on the Ground.” In 2013 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2013.6696956
• Panahandeh, Ghazaleh, Seth Hutchinson, Peter Händel, and Magnus Jansson. 2015. “Planar-Based Visual Inertial Navigation: Observability Analysis and Motion Estimation.” Journal of Intelligent & Robotic Systems 82 (2): 277–99. https://doi.org/10.1007/s10846-015-0257-4
• Panahandeh, Ghazaleh, and Magnus Jansson. 2011. “Vision-Aided Inertial Navigation Using Planar Terrain Features.” In 2011 First International Conference on Robot, Vision and Signal Processing. IEEE. https://doi.org/10.1109/rvsp.2011.64
• Panahandeh, Ghazaleh, Nasser Mohammadiha, and Magnus Jansson. 2012. “Ground Plane Feature Detection in Mobile Vision-Aided Inertial Navigation.” In 2012 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2012.6385503
• Panahandeh, G., I. Skog, and M. Jansson. 2010. “Calibration of the Accelerometer Triad of an Inertial Measurement Unit, Maximum Likelihood Estimation and Cramér-Rao Bound.” In 2010 International Conference on Indoor Positioning and Indoor Navigation. IEEE. https://doi.org/10.1109/ipin.2010.5646832
• Pandit, Milind, Chun Zhao, Guillermo Sobreviela, Arif Mustafazade, Xudong Zou, and Ashwin A. Seshia. 2018. “A Mode-Localized MEMS Accelerometer with 7μg Bias Stability.” In 2018 IEEE Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2018.8346719
• Panten, P., U. Bestmann, and P. Hecker. 2022. “Navigation Sensor Failure Detection without Sensor Redundancy.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926336
• Panzieri, S., F. Pascucci, and G. Ulivi. 2001. “An Outdoor Navigation System Using GPS and Inertial Platform.” In 2001 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. Proceedings (Cat. No.01TH8556), vol. 2. IEEE. https://doi.org/10.1109/aim.2001.936925
• Papa, Umberto. 2023. “Unmanned Aircraft Systems with Autonomous Navigation.” Electronics 12 (7): 1591. https://doi.org/10.3390/electronics12071591
• Papadimitriou, Costas, and Costas Argyris. 2017. “Bayesian Optimal Experimental Design for Parameter Estimation and Response Predictions in Complex Dynamical Systems.” Procedia Engineering 199: 972–77. https://doi.org/10.1016/j.proeng.2017.09.205
• Parajuli, Madan, Guillermo Sobreviela, and Ashwin A. Seshia. 2022. “Silicon MEMS Gyroscope with Quatrefoil Suspension System Achieving 1 Million Quality Factor.” In 2022 IEEE 35th International Conference on Micro Electro Mechanical Systems Conference (MEMS). IEEE. https://doi.org/10.1109/mems51670.2022.9699510
• Paris, S. W., L. E. Fink, and B. K. Joosten. 1980. “Application of an Advanced Trajectory Optimization Method to Ramjet Propelled Missiles.” Optimal Control Applications and Methods 1. https://ntrs.nasa.gov/citations/19810030613
• Park, Gary D. 1977. “Parameter Identification Technology Used in Determining in-Flight Airload Parameters.” Journal of Aircraft 14 (3): 251–56. https://doi.org/10.2514/3.58770
• Park, Junwoo, and Hyochoong Bang. 2022. “Evenly Weighted Particle Filter for Terrain-Referenced Navigation Using Gaussian Mixture Proposal Distribution.” In 2022 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas54217.2022.9836197
• Park, Junwoo, and Hyochoong Bang. 2023. “Tight Integration of Inertial and Terrain-Referenced Navigation under Biased Odometry and Measurements via Factor Graph Optimization.” In 2023 23rd International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.23919/iccas59377.2023.10317042
• Park, Junwoo, and Hyochoong Bang. 2024. “Sparse Instantiation of Bias Nodes for Factor Graph-Based Terrain-Referenced Navigation.” International Journal of Control, Automation and Systems 22 (11): 3364–76. https://doi.org/10.1007/s12555-023-0784-x
• Park, Junwoo, and Hyochoong Bang. 2025. “Contours-Seeking Proposal Density Particle Filter and Resilient Terrain-Referenced Navigation.” IEEE Transactions on Aerospace and Electronic Systems 61 (6): 15627–41. https://doi.org/10.1109/taes.2025.3588823
• Park, Chan Gook, Jaehyuck Cha, and Hojin Ju. 2019. “Long-Term Stability Analysis of Vertical Channel Damping and Kalman Filtering for Inertial Navigation System/Vertical Gauge.” In 2019 16th International Conference on Electrical Engineering/Electronics, Computer, Telecommunications and Information Technology (ECTI-CON). IEEE. https://doi.org/10.1109/ecti-con47248.2019.8955209
• Park, S. W., and D. M. Himmelblau. 1982. “Parameter Estimation and Unique Identifiability.” Chemical Engineering Journal 25 (2): 163–74. https://doi.org/10.1016/0300-9467(82)80085-3
• Park, Junwoo, Youngjoo Kim, and Hyochoong Bang. 2017. “A New Measurement Model of Interferometric Radar Altimeter for Terrain Referenced Navigation Using Particle Filter.” In 2017 European Navigation Conference (ENC). IEEE. https://doi.org/10.1109/euronav.2017.7954173
• Park, Ji Hoon, Chang June Lee, and Jung Keun Lee. 2026. “Effects of Gyroscope Bias Augmentation on Recurrent Neural Network Model Performance for Attitude Estimation.” IEEE Access 14: 71836–44. https://doi.org/10.1109/access.2026.3691717
• Park, Yong-Gonjong, and Chan Gook Park. 2018. “Grid Support Adaptation for Point Mass Filter Based Terrain Referenced Navigation Using Mutual Information.” IEEE Sensors Journal 18 (18): 7603–10. https://doi.org/10.1109/jsen.2018.2862941
• Park, Yong-gonjong, and Chan Gook Park. 2019. “Two Stage Particle Filter Based Terrain Referenced Navigation for Computational Efficiency.” IEEE Sensors Journal 19 (23): 11396–11402. https://doi.org/10.1109/jsen.2019.2934651
• Park, Yong-gonjong, and Chan Gook Park. 2020. “Two-Stage Point Mass Filter on Terrain Referenced Navigation for State Augmentation.” Journal of Guidance, Control, and Dynamics 43 (5): 1003–8. https://doi.org/10.2514/1.g003936
• Park, Jungmin, Yong-gonjong Park, and Chan Gook Park. 2020. “Parameter Estimation of Radar Noise Model for Terrain Referenced Navigation Using a New EM Initialization Method.” IEEE Transactions on Aerospace and Electronic Systems 56 (1): 107–12. https://doi.org/10.1109/taes.2019.2911766
• Parkhi, Prasad, Bijnan Bandyopadhyay, and Mahendra Jha. 2010. “Design of Roll Autopilot for a Tail Controlled Missile Using Sliding Mode Technique.” In 2010 11th International Workshop on Variable Structure Systems (VSS). IEEE. https://doi.org/10.1109/vss.2010.5544718
• Parnian, Neda, and Farid Golnaraghi. 2010. “Integration of a Multi-Camera Vision System and Strapdown Inertial Navigation System (SDINS) with a Modified Kalman Filter.” Sensors 10 (6): 5378–94. https://doi.org/10.3390/s100605378
• Parrish, Austin R., Lois Meira Lopez, Mohammad H. Asadian, Esther Wong, and Andrei M. Shkel. 2025a. “Laser Patterned Self-Aligned Electrodes for Dual-Shell Hemispherical Resonator Gyroscope.” In 2025 23rd International Conference on Solid-State Sensors, Actuators and Microsystems (Transducers). IEEE. https://doi.org/10.1109/transducers61432.2025.11109164
• Parrish, Austin R., Nicholas A. Strnad, Zachariah J. Klutts, et al. 2025b. “Non-Metallized Dual-Shell Hemispherical Resonator Gyroscope.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028339
• Parsa, K., T. A. Lasky, and B. Ravani. 2005. “Design and Mechatronic Implementation of an Accelerometer-Based, Kinematically Redundant Inertial Measurement Unit.” In Proceedings, 2005 IEEE/ASME International Conference on Advanced Intelligent Mechatronics.. IEEE. https://doi.org/10.1109/aim.2005.1511055
• Parsa, Javad, Cristian R. Rojas, and Hakan Hjalmarsson. 2022. “Optimal Input Design for Sparse System Identification.” In 2022 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc55457.2022.9838242
• Parvin, Richard H. 1962. “Inertial Navigation Systems: Prelaunch Alignment.” IRE Transactions on Aeronautical and Navigational Electronics ANE-9 (3): 141–45. https://doi.org/10.1109/tane3.1962.4201872
• Patel, Ujjval N., and Imraan A. Faruque. 2021. “Sensor Fusion to Improve State Estimate Accuracy Using Multiple Inertial Measurement Units.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430484
• Patel, Chandradip, and Patrick McCluskey. 2012. “Modeling and Simulation of the MEMS Vibratory Gyroscope.” In 13th InterSociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems. IEEE. https://doi.org/10.1109/itherm.2012.6231524
• Patterson, R. A., E. L. Goldner, A. Cordova, and D. M. Rozelle. 1994. “Test Results over Extended Environments for Litton’s Inertial Navigation Grade Interferometric Fiber Optic Gyro.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303312
• Paul, Preema, and Lijo Paul. 2023. “An Overview on the Parachute Recovery Systems with Additive Manufacturing for UAV Safe Landing.” Materials Today: Proceedings 72: 3158–62. https://doi.org/10.1016/j.matpr.2022.10.229
• Pavesi, Davide, Lois Meira Lopez, Eudald Sangenis, Valentina Zega, and Andrei M. Shkel. 2025. “Design, Fabrication and Characterization of a High-Quality Factor Fused Silica Toroidal Ring Gyroscope.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11036882
• Pawase, Ramesh, and N. P. Futane. 2015. “Angular Rate Error Compensation of MEMS Based Gyroscope Using Artificial Neural Network.” In 2015 International Conference on Pervasive Computing (ICPC). IEEE. https://doi.org/10.1109/pervasive.2015.7087129
• Payne, Robert L., and Graham C. Goodwin. 1974. “On the Identifiability of Linear Dynamic Systems.” International Journal of Control 20 (5): 865–68. https://doi.org/10.1080/00207177408932788
• Pecinka, Jiri, Gabriel T. Bugajski, Adolf Jilek, and Petr Kmoch. 2015. “Small Engine Inlet Distortion Testing Device.” In International Conference on Military Technologies (ICMT) 2015. IEEE. https://doi.org/10.1109/miltechs.2015.7153691
• Pecora, Rosario. 2021. “A Rational Numerical Method for Simulation of Drop-Impact Dynamics of Oleo-Pneumatic Landing Gear.” Applied Sciences 11 (9): 4136. https://doi.org/10.3390/app11094136
• Peebles, Peyton. 1969. “Signal Processors and Accuracy of Three-Beam Monopulse Tracking Radar.” IEEE Transactions on Aerospace and Electronic Systems AES-5 (1): 52–57. https://doi.org/10.1109/taes.1969.309820
• Peebles, Peyton. 1985. “Monopulse Radar Angle Tracking Accuracy with Sum Channel Limiting.” IEEE Transactions on Aerospace and Electronic Systems AES-21 (1): 137–43. https://doi.org/10.1109/taes.1985.310547
• Peebles, Peyton, and Hajime Sakamoto. 1980. “Conopulse Radar Angle Tracking Accuracy.” IEEE Transactions on Aerospace and Electronic Systems AES-16 (6): 870–74. https://doi.org/10.1109/taes.1980.309015
• Peebles, Peyton, and Hajime Sskamoto. 1980. “On Conopulse Radar Theoretical Angle Tracking Accuracy.” IEEE Transactions on Aerospace and Electronic Systems AES-16 (3): 399–402. https://doi.org/10.1109/taes.1980.308910
• Pei, Fujun, Su Yang, and Shunan Yin. 2021. “In-Motion Initial Alignment Using State-Dependent Extended Kalman Filter for Strapdown Inertial Navigation System.” IEEE Transactions on Instrumentation and Measurement 70: 1–12. https://doi.org/10.1109/tim.2020.3027405
• Peng, Jiping, Xin Huo, Kemao Ma, Jipeng Dong, and Jinpeng Zhang. 2017. “Autopilot Design of Missile with Input Delay Based on Self-Stable Region Approach.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028282
• Peng, Xu, Yan Li, and Zhong Wang. 2025a. “Observer-Enhanced Sliding Mode Control for Fixed-Wing Aircraft Automatic Carrier Landing.” ISA Transactions 167: 1431–45. https://doi.org/10.1016/j.isatra.2025.10.052
• Peng, Chao, Zhengbin Li, and Anshi Xu. 2007. “‘Slow Light’ Gyroscope Based on Coupled Resonator Waveguide Structure.” In 2007 International Nano-Optoelectronics Workshop. IEEE. https://doi.org/10.1109/inow.2007.4302967
• Peng, Jincheng, Dongjie Wu, Pengchao Yao, Xiafu Peng, Gongliu Yang, and Xiaoli Zhang. 2025b. “Schuler Period Oscillation Error Suppression for Inertial Navigation Systems Based on Reverse Navigation and Wavelet Transforms.” Measurement 242: 115862. https://doi.org/10.1016/j.measurement.2024.115862
• Peng, Jincheng, Xiaoli Zhang, Xiafu Peng, Pengchao Yao, Jinwen Chen, and Gongliu Yang. 2024. “RODM-Alignment: An Inertial Alignment Algorithm for Sliding Window Reverse Optimization Delayed Marginalization.” IEEE Transactions on Instrumentation and Measurement 73: 1–12. https://doi.org/10.1109/tim.2024.3438852
• Peng, Jincheng, Xiaoli Zhang, Gongliu Yang, and Xiafu Peng. 2026. “Three-Point Calibration for Long-Endurance Inertial Navigation Systems Based on Limited Position Observations and Reverse Navigation.” Measurement 258: 118911. https://doi.org/10.1016/j.measurement.2025.118911
• Peng-fei, Jiang, Xu Jiang-ning, and Zhu Bing. 2018. “Genetic Algorithm-Particle Swarm Optimization Algorithm Based Compass Initial Alignment of Strapdown Inertial Navigation System.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019218
• Pengjun, Qian, and Lu Zhengliang. 2021. “Adaptive Backstepping Terminal Sliding Mode Attitude Stabilization Control for Moving Mass Rocket-Propelled CubeSat.” In 2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS). IEEE. https://doi.org/10.1109/icmeas54189.2021.00014
• Pepe, M., G. Prezioso, and R. Santamaria. 2014. “Impact of Vertical Deflection on Direct Georeferencing of Airborne Images.” Survey Review 47 (340): 71–76. https://doi.org/10.1179/1752270614y.0000000087
• Perelyaev, S. E., B. P. Bodunov, and S. B. Bodunov. 2017. “Solid-State Wave Gyroscope: A New-Generation Inertial Sensor.” In 2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2017.7995651
• Pérez, Ramón, Ignacio Álvarez, and José Enguita. 2016. “Theoretical Design of a Depolarized Interferometric Fiber-Optic Gyroscope (IFOG) on SMF-28 Single-Mode Standard Optical Fiber Based on Closed-Loop Sinusoidal Phase Modulation with Serrodyne Feedback Phase Modulation Using Simulation Tools for Tactical and Industrial Grade Applications.” Sensors 16 (5): 604. https://doi.org/10.3390/s16050604
• Pérez, C., and F. R. Rubio. 2001. “Inertial Stabilization Controller for a 2 DOF Platform.” IFAC Proceedings Volumes 34 (29): 97–102. https://doi.org/10.1016/s1474-6670(17)32800-8
• Perrier, Thomas, Olivier Le Traon, Raphael Levy, Jean Guerard, Amandine Andrieux Ledier, and Pierre Lavenus. 2022. “Gytrix, a Novel Axisymmetric Quartz MEMS Gyroscope for Navigation Purpose.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787719
• Pessanha Santos, Nuno, Victor Lobo, and Alexandre Bernardino. 2023. “Fixed-Wing Unmanned Aerial Vehicle 3D-Model-Based Tracking for Autonomous Landing.” Drones 7 (4): 243. https://doi.org/10.3390/drones7040243
• Petritoli, Enrico, and Fabio Leccese. 2021. “Navigation Equations, Uncertainty and Error Budget in Inertial Navigation Systems.” In 2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace51421.2021.9511784
• Petritoli, Enrico, Fabio Leccese, and Mariagrazia Leccisi. 2019. “Inertial Navigation Systems for UAV: Uncertainty and Error Measurements.” In 2019 IEEE 5th International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2019.8869618
• Pfeifer, L. n.d. “Orthogonalization of Nonorthogonal Vector Components (Inertial Navigation).” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195533
• Pham, M. D., K. S. Low, Chen Shoushun, and Y. T. Xing. 2012. “A Star Pattern Recognition Algorithm for Satellite Attitude Determination.” In 2012 IEEE Symposium on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/isiea.2012.6496636
• Phillips, C. L., E. R. Graf, and S. A. Starks. n.d. “An Aircraft Landing System Employing Kalman Filters.” In Conference Proceedings Southeastcon ‘81.. IEEE. https://doi.org/10.1109/secon.1981.673416
• Phillips, Charles L., Robert F. Wilson, Edward R. Graf, and Scott A. Starks. 1983b. “Observers as Noise Filters in an Automatic Aircraft Landing System.” Journal of Guidance, Control, and Dynamics 6 (2): 119–20. https://doi.org/10.2514/3.56345
• Pierson, B. L. 1985. “Optimal Aircraft Landing-Approach Trajectories: A Comparison of Two Dynamic Models.” Annual Review in Automatic Programming 13: 139–45. https://doi.org/10.1016/0066-4138(85)90475-6
• Pilyugin, N. N., and V. S. Khlebnikov. 2010. “Development of a Parachute System for Deceleration of Flying Vehicles in Supersonic Regimes.” Journal of Applied Mechanics and Technical Physics 51 (5): 323–32. https://doi.org/10.1007/s10808-010-0080-4
• Pilyugin, S. Yu., and V. S. Shalgin. 2024. “Local Parameter Identifiability: Case of Discrete Infinite-Dimensional Parameter.” Journal of Dynamical and Control Systems 30 (2): 14. https://doi.org/10.1007/s10883-024-09699-9
• Pirooz, Mehran, Seyed Hossein Mirmahdi, and Ahmad Reza Khoogar. 2021. “Robust Force and Displacement Control of an Active Landing Gear for Vibration Reduction at Touchdown and during Taxiing.” SN Applied Sciences 3 (4): 410. https://doi.org/10.1007/s42452-021-04320-1
• Pisarski, Dominik, Błażej Popławski, Łukasz Jankowski, and Rami Faraj. 2026. “Magnetic Anomaly Navigation Using Particle Filtering and an Enhanced Velocity Propagation Model.” Measurement 278: 121656. https://doi.org/10.1016/j.measurement.2026.121656
• Pish, F., Rasoul Moradi, Amirhossein Edalatpour, and M. Barzegar Gerdroodbary. 2019. “The Effect of Coolant Injection from the Tip of Spike on Aerodynamic Heating of Nose Cone at Supersonic Flow.” Acta Astronautica 154: 52–60. https://doi.org/10.1016/j.actaastro.2018.10.021
• Pishrobat, M. Hoseini, and J. Keighobadi. 2014. “Model Predictive Control of MEMS Vibratory Gyroscope.” IFAC Proceedings Volumes 47 (3): 7278–83. https://doi.org/10.3182/20140824-6-za-1003.02322
• Plaetschke, E., J. A. Mulder, and J. H. Breeman. 1982. “Flight Test Results of Five Input Signals for Aircraft Parameter Identification.” IFAC Proceedings Volumes 15 (4): 1149–54. https://doi.org/10.1016/s1474-6670(17)63152-5
• Plakhtienko, N. P., and B. M. Shifrin. 2006. “Critical Shimmy Speed of Nonswiveling Landing-Gear Wheels Subject to Lateral Loading.” International Applied Mechanics 42 (9): 1077–84. https://doi.org/10.1007/s10778-006-0179-8
• Poddar, Shashi, and Amod Kumar. 2019. “Scale-Free PSO for in-Run and Infield Inertial Sensor Calibration.” Measurement 147: 106849. https://doi.org/10.1016/j.measurement.2019.07.077
• Podder, Itilekha, Tamas Fischl, and Udo Bub. 2024. “Smart Calibration and Monitoring: Leveraging Artificial Intelligence to Improve MEMS-Based Inertial Sensor Calibration.” Complex & Intelligent Systems 10 (6): 7451–74. https://doi.org/10.1007/s40747-024-01531-y
• Point, N., A. Vande Wouwer, and M. Remy. 1996. “Practical Issues in Distributed Parameter Estimation: Gradient Computation and Optimal Experiment Design.” Control Engineering Practice 4 (11): 1553–62. https://doi.org/10.1016/0967-0661(96)00169-4
• Pollack, Joshua. 2011. “BALLISTIC TRAJECTORY: The Evolution of North Korea’s Ballistic Missile Market.” Nonproliferation Review 18 (2): 411–29. https://doi.org/10.1080/10736700.2011.583120
• Polli, Gian Mario, Franco Mastroddi, Liviu Librescu, and Claudia Di Trapani. 2008. “Aerothermoelastic Stability of Composite Aerovehicle Wings Subjected to Heat Inputs.” AIAA Journal 46 (4): 992–1001. https://doi.org/10.2514/1.32397
• Polz, Anne-Sophie, Fabian Frickenstein, and Maarten Uijt de Haag. 2025. “Flight Test Evaluation of a LIDAR/inertial Navigator for Autonomous Drone Operations in GNSS-Denied Urban Environments.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028504
• Poulose, M. M. 1992. “Microwave Landing System Modeling with Application to Air Traffic Control Automation.” Journal of Aircraft 29 (3): 348–54. https://doi.org/10.2514/3.46168
• Pourtakdoust, S. H., and S. A. Fazelzadeh. 2005. “Nonlinear Aerothermoelastic Behavior of Skin Panel with Wall Shear Stress Effect.” Journal of Thermal Stresses 28 (2): 147–69. https://doi.org/10.1080/014957390523714
• Praczyk, Tomasz, and Jacek Zalewski. 2026. “Optical Coastal GNSS-Denied Navigation for Reduction in AUV Underwater Navigation Error.” Sensors 26 (14): 4601. https://doi.org/10.3390/s26144601
• “Preparation of Turbojet Engine Fuel.” 2002. Fuel and Energy Abstracts 43 (1): 25. https://doi.org/10.1016/s0140-6701(02)80255-7
• Priel, B. 1992. “The Effect of Gyro Nonorthogonality Error on Gyrocompassing.” IEEE Transactions on Aerospace and Electronic Systems 28 (3): 890–93. https://doi.org/10.1109/7.256312
• Priestley, N. n.d. “Terrain Referenced Navigation.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66218
• Prikhodko, Igor P., Jeffrey A. Gregory, and Michael W. Judy. 2017. “Virtually Rotated MEMS Gyroscope with Angle Output.” In 2017 IEEE 30th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2017.7863406
• Prikhodko, Igor P., Jeffrey A. Gregory, Daniel Shin, Ryan Kwon, Thomas W. Kenny, and Michael W. Judy. 2019. “Pseudo-Extensional Mode MEMS Ring Gyroscope.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739576
• Prikhodko, Igor P., Sergei A. Zotov, Alexander A. Trusov, and Andrei M. Shkel. 2013. “What Is MEMS Gyrocompassing? Comparative Analysis of Maytagging and Carouseling.” Journal of Microelectromechanical Systems 22 (6): 1257–66. https://doi.org/10.1109/jmems.2013.2282936
• Pritchard, Robert E. 1969. “Base Drag Effects on Maximum Lift-to-Drag Ratio Airfoils at Moderate Supersonic Speeds.” Journal of Optimization Theory and Applications 3 (2): 115–36. https://doi.org/10.1007/bf00932462
• Pritchard, Jocelyn. 2001. “Overview of Landing Gear Dynamics.” Journal of Aircraft 38 (1): 130–37. https://doi.org/10.2514/2.2744
• Priydarshi, Raman Jaiswal, Renju C. Nair, Naveen Krishna Yarlagadda, A. Ashok Kumar Senapati, and Prabhushetty Mulage. 2016. “Adaptive Gyroscope Drift Compensation Based on Temporal Noise Modelling.” In 2016 International Conference on Microelectronics, Computing and Communications (MicroCom). IEEE. https://doi.org/10.1109/microcom.2016.7522471
• Prohortsov, Alexey, Alexander Soloviev, and Vladimir Smirnov. 2020. “Mathematical Model of Semianalytic Gyrocompassing.” In 2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43215.2020.9133819
• Prokhorov, Y. G. 1995. “Observability of Gravimeter-Aided Inertial Navigation Systems.” Journal of Guidance, Control, and Dynamics 18 (6): 1416–19. https://doi.org/10.2514/3.21562
• Provost, François, Faisal Hawlader, Mehdi Testouri, and Raphaël Frank. 2026. “Motion-to-Motion Latency Measurement Framework for Connected and Autonomous Vehicle Teleoperation.” In 2026 21st Wireless On-Demand Network Systems and Services Conference (WONS). IEEE. https://doi.org/10.23919/wons68803.2026.11501834
• Puckett, Allen E. 1946. “Supersonic Wave Drag of Thin Airfoils.” Journal of the Aeronautical Sciences 13 (9): 475–84. https://doi.org/10.2514/8.11425
• Qasem, Haytham, Omar Gorgis, and Leonhard Reindl. 2008. “Design and Calibration of an Inertial Sensor System for Precise Vehicle Navigation.” In 2008 5th Workshop on Positioning, Navigation and Communication. IEEE. https://doi.org/10.1109/wpnc.2008.4510379
• Qayyum, Usman, and Jonghyuk Kim. 2021. “Depth-Camera-Aided Inertial Navigation Utilizing Directional Constraints.” Sensors 21 (17): 5913. https://doi.org/10.3390/s21175913
• Qi, Jie, and Ruth E. Baker. 2026. “Optimal Experimental Design for Parameter Estimation in the Presence of Observation Noise.” Mathematical Biosciences 392: 109571. https://doi.org/10.1016/j.mbs.2025.109571
• Qi, Zhenxiang, Jie Gu, Bingchen Zhu, et al. 2026a. “Design, Modeling, and Fabrication of a High-Q AlN Annular Gyroscope with Sub-10°/h Bias Instability.” Micromachines 17 (2): 268. https://doi.org/10.3390/mi17020268
• Qi, Pei, Guanyu Li, Weixing Qian, et al. 2021. “Initial Alignment Method for Rotating Strapdown Inertial Navigation System Based on Fuzzy Adaptive Kalman Filter.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550366
• Qi, Lingling, and Mengyao Wang. 2024. “Suppression Method of Gyroscope Drift Applied in Intelligent Devices.” In 2024 4th International Conference on Electronics, Circuits and Information Engineering (ECIE). IEEE. https://doi.org/10.1109/ecie61885.2024.10626376
• Qi, Zhenxiang, Kunfeng Wang, Zhaoyang Zhai, et al. 2026b. “A High-Q ALN Wide Annular Gyroscope with Sub 10 Deg per Hour Bias Instability.” In 2026 IEEE 39th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems64181.2026.11419592
• Qi, Bing, Fuzhong Wen, Fanming Liu, and Jianhua Cheng. 2020. “Modification of MTEA-Based Temperature Drift Error Compensation Model for MEMS-Gyros.” Sensors 20 (10): 2906. https://doi.org/10.3390/s20102906
• Qi, Pengyuan, Xiaowei Zhao, Yinan Wang, Rafael Palacios, and Andrew Wynn. 2018. “Automatic Landing Control of a Very Flexible Flying Wing.” In 2018 Annual American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc.2018.8431539
• Qian, Jun, Madiha Nadri, Petru-Daniel Morosan, and Pascal Dufour. 2014. “Closed Loop Optimal Experiment Design for on-Line Parameter Estimation.” In 2014 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2014.6862468
• Qian, Xuewu, Jianlong Qiu, Zhaodong Liu, Weiling Yang, and Yang Zheng. 2018. “Matching Method of Accelerometer Scale Factor for Gravity Gradiometer.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019217
• Qian, Li, Guoping Xu, Weifeng Tian, and Junpu Wang. 2009. “A Novel Hybrid EMD-Based Drift Denoising Method for a Dynamically Tuned Gyroscope (DTG).” Measurement 42 (6): 927–32. https://doi.org/10.1016/j.measurement.2009.01.017
• Qian, Wei-xing, Xin-hua Zhu, and Yan Su. 2010. “A Method Improving the Alignment Accuracy of Medium Accuracy MEMS Inertial Navigation System on Revolving Base.” In 2010 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2010.5589044
• Qiang, Huang, Wang Wei-kui, Wang Yun-hao, and Rong Peng-hui. 2012. “Research on Computer Emulation of Store Reliability of the Drag Parachute System.” In 2012 International Conference on Industrial Control and Electronics Engineering. IEEE. https://doi.org/10.1109/icicee.2012.421
• Qiao, Yongjun, Xiaofang Xie, Lei Shi, and Dedong Li. 2010. “The Application of Spatial Scene Matching Based on SURF in Cruise Missile Terminal Guidance.” In 2010 International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2010.127
• Qin, Chong, Jiabin Chen, Yongqiang Han, and Chunlei Song. 2016. “Design and Analysis of Dual-Axis Rotating Scheme for Ring Laser Strapdown Inertial Navigation System.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554205
• Qin, Honglei, Li Cong, and Xingli Sun. 2012. “Accuracy Improvement of GPS/MEMS-INS Integrated Navigation System during GPS Signal Outage for Land Vehicle Navigation.” Journal of Systems Engineering and Electronics 23 (2): 256–64. https://doi.org/10.1109/jsee.2012.00033
• Qin, Z., X. Ding, J. Jia, and H. Li. 2021. “Vibration Model of Mode Order Optimized Vibrating Ring Gyroscope.” In 2021 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss52949.2021.9619807
• Qin, Yunpeng, Peiqing Liu, Qiulin Qu, and Tianxiang Hu. 2017. “Wing/canard Interference of a Close-Coupled Canard Configuration in Static Ground Effect.” Aerospace Science and Technology 69: 60–75. https://doi.org/10.1016/j.ast.2017.06.012
• Qin, Fangjun, Jiangning Xu, and Jiang Sai. 2009. “A New Scheme of Gyroscope Free Inertial Navigation System Using 9 Accelerometers.” In 2009 International Workshop on Intelligent Systems and Applications. IEEE. https://doi.org/10.1109/iwisa.2009.5072652
• Qiu, Ziyi, Defu Lin, Ren Jin, Junning Lv, and Zhangxiong Zheng. 2022a. “A Global ArUco-Based Lidar Navigation System for UAV Navigation in GNSS-Denied Environments.” Aerospace 9 (8): 456. https://doi.org/10.3390/aerospace9080456
• Qiu, Ziyi, Junning Lv, Defu Lin, Yinan Yu, Zhiwen Sun, and Zhangxiong Zheng. 2022b. “A Lidar-Inertial Navigation System for UAVs in GNSS-Denied Environment with Spatial Grid Structures.” Applied Sciences 13 (1): 414. https://doi.org/10.3390/app13010414
• Qu, Shi, Cangzhen Meng, Hongbin Jin, and Weiqiang Deng. 2024. “A Method for Ballistic Missile Trajectory Correlation Based on Trajectory State Estimation.” In 2024 IEEE 2nd International Conference on Sensors, Electronics and Computer Engineering (ICSECE). IEEE. https://doi.org/10.1109/icsece61636.2024.10729576
• Qu Pingping, Fu Li, and Zhao Xin. 2009. “Design of Inertial Navigation System Based on Micromechanical Gyroscope and Accelerometer.” In 2009 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2009.5194612
• Quan, Wei, Lin Lv, and Baiqi Liu. 2014. “Modeling and Optimizing of the Random Atomic Spin Gyroscope Drift Based on the Atomic Spin Gyroscope.” Review of Scientific Instruments 85 (11): 113104. https://doi.org/10.1063/1.4900946
• Quan, Enqian, Min Xu, Weigang Yao, and Xiang Cheng. 2021. “Analysis of the Post-Flutter Aerothermoelastic Characteristics of Hypersonic Skin Panels Using a CFD-Based Approach.” Aerospace Science and Technology 118: 107076. https://doi.org/10.1016/j.ast.2021.107076
• Quarmyne, James, and Meir Pachter. 2014. “Inertial Navigation System Aiding Using Vision.” In 2014 American Control Conference. IEEE. https://doi.org/10.1109/acc.2014.6858678
• Quynh, Nga Vu, Phat Nguyen Huu, and Thanh Han-Trong. 2026. “Navigation Methods for UAVs in GNSS-Denied Environments Using Artificial Intelligence.” In 2026 Eleventh International Conference on Communications and Electronics (ICCE). IEEE. https://doi.org/10.1109/icce70609.2026.11658445
• Rad, Amir Moghtadaei. 2015. “Compensating and Analysis Error in Height Channel of Inertial Navigation System Using Star Sensors.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7118874
• Rad, Amir Moghtadaei, Jafar Heyrani Nobari, and Amir Ali Nikkhah. 2014. “Optimal Attitude and Position Determination by Integration of INS, Star Tracker, and Horizon Sensor.” IEEE Aerospace and Electronic Systems Magazine 29 (4): 20–33. https://doi.org/10.1109/maes.2014.130093
• Radkey, R. L., H. R. Welge, and R. L. Roensch. 1978. “Aerodynamic Design of a Mach 2.2 Supersonic Cruise Aircraft.” Journal of Aircraft 15 (6): 351–57. https://doi.org/10.2514/3.58369
• Rafajlowicz, E. 1983. “Optimal Experiment Design for Identification of Linear Distributed-Parameter Systems: Frequency Domain Approach.” IEEE Transactions on Automatic Control 28 (7): 806–8. https://doi.org/10.1109/tac.1983.1103309
• Rafajlowicz, Ewaryst. 1984. “Unbounded Power Input Signals in Optimum Experiment Design for Parameter Estimation in Linear Systems.” International Journal of Control 40 (2): 383–91. https://doi.org/10.1080/00207178408933281
• Ragel, B. A., and M. Farooq. 2005. “Comparison of Forward vs. Feedback Kalman Filter for Aided Inertial Navigation System.” In 2005 7th International Conference on Information Fusion. IEEE. https://doi.org/10.1109/icif.2005.1591871
• Rahma, Sidahmed, and Ibraheem AlQadi. 2025. “Supersonic Base Drag Reduction via Forced and Natural Bleed.” Arabian Journal for Science and Engineering 51 (7): 9917–35. https://doi.org/10.1007/s13369-025-10543-w
• Rahmani, Mehran. 2018. “MEMS Gyroscope Control Using a Novel Compound Robust Control.” ISA Transactions 72: 37–43. https://doi.org/10.1016/j.isatra.2017.11.009
• Rahmani, Mohsen, and Kamran Behdinan. 2019a. “Parametric Study of a Novel Nose Landing Gear Shimmy Damper Concept.” Journal of Sound and Vibration 457: 299–313. https://doi.org/10.1016/j.jsv.2019.06.008
• Rahmani, Mohsen, and Kamran Behdinan. 2020. “Interaction of Torque Link Freeplay and Coulomb Friction Nonlinearities in Nose Landing Gear Shimmy Scenarios.” International Journal of Non-Linear Mechanics 119: 103338. https://doi.org/10.1016/j.ijnonlinmec.2019.103338
• Raimbault, Nathalie, Christian Bes, and Pierre Fabre. 2001. “Neural Aircraft Autopilot Gain Adjuster.” IFAC Proceedings Volumes 34 (15): 404–9. https://doi.org/10.1016/s1474-6670(17)40761-0
• Raisinghani, S. C., and A. K. Adak. 1983. “Aircraft Parameter Identification by Gauss-Newton Minimization Technique Using Flight Test Data.” International Journal of Systems Science 14 (12): 1395–1409. https://doi.org/10.1080/00207728308926538
• Rajagopal, K. R., N. Vedachalam, B. Singh, and B. P. Singh. n.d. “Permanent Magnet Torquer with Temperature Compensation for Gyroscope Used in Space Application.” In Proceedings of IEEE/IAS International Conference on Industrial Automation and Control. IEEE. https://doi.org/10.1109/iacc.1995.465877
• Ramachandra, Lusitha S., Ian K. Jennions, and Nicolas P. Avdelidis. 2026b. “An in-Depth Review on Sensing, Heat-Transfer Dynamics, and Predictive Modeling for Aircraft Wheel and Brake Systems.” Sensors 26 (3): 921. https://doi.org/10.3390/s26030921
• Ramakrishna, Raksha, Yuqi Shao, György Dán, and Nicole Kringos. 2023. “Sequential Experiment Design for Parameter Estimation of Nonlinear Systems Using a Neural Network Approximator.” European Journal of Control 74: 100859. https://doi.org/10.1016/j.ejcon.2023.100859
• Ramanandan, Arvind, Anning Chen, and Jay A. Farrell. 2011. “Observability Analysis of an Inertial Navigation System with Stationary Updates.” In Proceedings of the 2011 American Control Conference. IEEE. https://doi.org/10.1109/acc.2011.5991282
• Ramírez, Germán, Rodolfo Verdín, and Gerardo Flores. 2024. “Real-Time Mapping for Teleoperation Systems in VR of Unmanned Aerial Vehicles.” In 2024 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas60882.2024.10556921
• “Ramjet Supersonic “Flight Tests”.” 1958. Journal of the Franklin Institute 265 (2): 164–65. https://doi.org/10.1016/0016-0032(58)90466-6
• Ramos, J. Humberto, Jaejeong Shin, Kyle Volle, Paul Buzaud, Kevin Brink, and Prashant Ganesh. 2022. “Information-Aware Guidance for Magnetic Anomaly Based Navigation.” In 2022 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros47612.2022.9981709
• Ramprakash, A., and T. M. Muruganandam. 2016. “Experimental Study on Internal Flowfield Characteristics and Start-Unstart Behaviour in a Two-Dimensional Variable Geometry Inlet.” In 2016 7th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2016.7549585
• Ran, Yulin, Tao Jiang, and Qingbiao Kuang. 2019. “Fixed-Structure Synthesis for Gain Scheduling Control of Missile Autopilot.” In 2019 IEEE 3rd Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC). IEEE. https://doi.org/10.1109/imcec46724.2019.8984097
• Ranji, Ahmad Rahbar, Vijayakanthan Damodaran, Kevin Li, Zilang Chen, Shahpour Alirezaee, and Mohammed Jalal Ahamed. 2022. “Recent Advances in MEMS-Based 3D Hemispherical Resonator Gyroscope (HRG)—a Sensor of Choice.” Micromachines 13 (10): 1676. https://doi.org/10.3390/mi13101676
• Rapoport, Ilia, and Amit Brandes. 2010. “Analysis of Sculling Motion Errors Caused by Sensor Transfer Function Imperfections in Strapdown Inertial Navigation Systems.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507184
• Rashed, Mohammed Irfan, Seunghan Lim, and Hyochoong Bang. 2013. “Numerical Modeling, Testing and Bias Drift Analysis of MEMS Based Three-Axis Gyroscope for Accurate Angular Rate Estimation for Attitude Determination of Nano-Satellites.” In 2013 13th International Conference on Control, Automation and Systems (ICCAS 2013). IEEE. https://doi.org/10.1109/iccas.2013.6703928
• Raspopov, V. Ya., and I. A. Volchikhin. 2018. “Solid-State Wave Gyroscope Ensuring the Required Accuracy Parameters.” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405893
• Rataczak, Jens A., Ross S. Chaudhry, Jay W. McMahon, and Iain D. Boyd. 2024. “Investigation of Surface-Catalycity Effects on Hypersonic Glide Vehicle Trajectory Optimization.” Journal of Spacecraft and Rockets 61 (4): 1019–31. https://doi.org/10.2514/1.a35764
• Rauch, Lawrence L. 1957. “Ballistic Missile Telemetry.” IRE Transactions on Telemetry and Remote Control TRC-3 (2): 2–5. https://doi.org/10.1109/irettrc.1957.6540504
• Ravanbod, L., and D. Noll. 2012. “Gain-Scheduled Two-Loop Autopilot for an Aircraft.” IFAC Proceedings Volumes 45 (13): 772–77. https://doi.org/10.3182/20120620-3-dk-2025.00060
• Rawashedeh, Samir A., and James E. Lumpp. 2014. “Visual Approach for MEMS Gyroscope Drift Compensation.” In 2014 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2014.6836352
• Reardon, Jonathan P., Joseph A. Schetz, and Kevin Todd Lowe. 2021. “Computational Analysis of Unstart in Variable-Geometry Inlet.” Journal of Propulsion and Power 37 (4): 564–76. https://doi.org/10.2514/1.b38214
• Reed, Matthew, Francis Neill, and Colin Baker. 2025. “MEMS Vibrating Beam Gravimeter for Inertial Navigation Applications.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037169
• Rehage, Dominick, Udo B. Carl, and Andreas Vahl. 2005. “Redundancy Management of Fault Tolerant Aircraft System Architectures – Reliability Synthesis and Analysis of Degraded System States.” Aerospace Science and Technology 9 (4): 337–47. https://doi.org/10.1016/j.ast.2005.02.002
• Reichert, Carl E. 1947. “Supersonic and Transonic Aircraft Problems.” Journal of the American Rocket Society 00 (69): 24–33. https://doi.org/10.2514/8.4133
• Reichert, R. T. 1991. “Dynamic Scheduling of Modern-Robust-Control Autopilot Designs for Missiles.” In [1991] Proceedings of the 30th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1991.261095
• Reis, Matheus F., Guilherme P. S. Carvalho, Alex F. Neves, and Alessandro J. Peixoto. 2018a. “Dynamic Model and Line of Sight Control of a 3-DOF Inertial Stabilization Platform via Feedback Linearization.” In 2018 Annual American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc.2018.8430907
• Reis, Matheus F., Joao C. Monteiro, Ramon R. Costa, and Antonio C. Leite. 2018b. “Super-Twisting Control with Quaternion Feedback for a 3-DoF Inertial Stabilization Platform.” In 2018 IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2018.8619292
• Remmler, Karl L., and Richard T. Theobald. 1967. “An Error Analysis of Navigation Using Inertial Guidance and Radar Tracking.” Journal of Spacecraft and Rockets 4 (4): 417–23. https://doi.org/10.2514/3.28881
• Ren, Hongguang, Jieping Gao, Yunxia Chen, and Fengli Deng. 2009. “A New Method of Calculating Generalized Correlation Coefficient for Reliability Analysis of Missile.” In 2009 8th International Conference on Reliability, Maintainability and Safety. IEEE. https://doi.org/10.1109/icrms.2009.5270217
• Ren, Yingjie, and Yanguang Hu. 2018. “Failure Diagnosis for UAV-Born Inertial Navigation Device Based on BP-Adaboost Model.” In 2018 5th International Conference on Dependable Systems and Their Applications (DSA). IEEE. https://doi.org/10.1109/dsa.2018.00020
• Ren, Jihuan, Xiang Wu, Yi Liu, Feng Ni, Yuming Bo, and Changhui Jiang. 2023. “Long-Term Trajectory Prediction of Hypersonic Glide Vehicle Based on Physics-Informed Transformer.” IEEE Transactions on Aerospace and Electronic Systems 59 (6): 9551–61. https://doi.org/10.1109/taes.2023.3322977
• Ren, Zikun, Yong Xu, Shixuan Duan, and Lizhi Wang. 2024c. “Research on Fault Diagnosis Technology of Inertial Navigation Systems on Aircraft.” In 2024 Global Reliability and Prognostics and Health Management Conference (PHM-Beijing). IEEE. https://doi.org/10.1109/phm-beijing63284.2024.10874653
• Ren, X. M., Ming Zhang, and Hong Nie. 2021. “Optimization of Multilayer Thermal Protection System by Using Phase Change Material under Aerodynamic Heating.” Applied Thermal Engineering 191: 116677. https://doi.org/10.1016/j.applthermaleng.2021.116677
• Ren-Young Liu, G. Adams, E. Lindquist, and L. Atherton. n.d. “Test Results from a Tactical Grade IMU Using Fiber Optic Gyros and Quartz Accelerometers.” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509055
• Renault, S., A. Le Meur, and D. Meizel. 2005. “GPS/GIS Localization for Management of Vision Referenced Navigation in Urban Environments.” In Proceedings. 2005 IEEE Intelligent Transportation Systems, 2005.. IEEE. https://doi.org/10.1109/itsc.2005.1520117
• Reuther, J., J. J. Alonso, M. J. Rimlinger, and A. Jameson. 1999. “Aerodynamic Shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Distributed Memory Parallel Computers.” Computers & Fluids 28 (4–5): 675–700. https://doi.org/10.1016/s0045-7930(98)00050-4
• Rezaifard, Elahe, and Pouya Abbasi. 2017. “Inertial Navigation System Calibration Using GPS Based on Extended Kalman Filter.” In 2017 Iranian Conference on Electrical Engineering (ICEE). IEEE. https://doi.org/10.1109/iraniancee.2017.7985144
• Rhudy, Matthew B., Mario L. Fravolini, and Marcello R. Napolitano. 2024. “GPS-Free Roll and Pitch Estimation through Pressure Altitude Aided Inertial Navigation System for a Jet Aircraft.” Aerospace Science and Technology 146: 108975. https://doi.org/10.1016/j.ast.2024.108975
• Richalet, J., S. Abu el Ata-Doss, and A. Coïc. 1991. “Global Identification and Optimal Input Design.” IFAC Proceedings Volumes 24 (3): 1121–26. https://doi.org/10.1016/s1474-6670(17)52500-8
• Riley, Zachary B., Ricardo A. Perez, Gregory W. Bartram, S. Michael Spottswood, Benjamin P. Smarslok, and Timothy J. Beberniss. 2019. “Aerothermoelastic Experimental Design for the AEDC/VKF Tunnel C: Challenges Associated with Measuring the Response of Flexible Panels in High-Temperature, High-Speed Wind Tunnels.” Journal of Sound and Vibration 441: 96–105. https://doi.org/10.1016/j.jsv.2018.10.022
• Rizk, Mostafa, Ahmad Mroue, Mohammad Farran, and Jamal Charara. 2020. “Real-Time SLAM Based on Image Stitching for Autonomous Navigation of UAVs in GNSS-Denied Regions.” In 2020 2nd IEEE International Conference on Artificial Intelligence Circuits and Systems (AICAS). IEEE. https://doi.org/10.1109/aicas48895.2020.9073793
• Roache, Patrick J. 1973. “Base Drag Calculations in Supersonic Turbulent Axisymmetric Flows.” Journal of Spacecraft and Rockets 10 (4): 285–87. https://doi.org/10.2514/3.27756
• Roberts, B., B. Sridhar, and B. Bhanu. n.d. “Inertial Navigation Sensor Integrated Motion Analysis for Obstacle Detection.” In IEEE/AIAA 10th Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.1991.177155
• Roberts, B. A., and L. C. Vallot. n.d. “Vision-Aided Inertial Navigation.” In IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences. IEEE. https://doi.org/10.1109/plans.1990.66198
• Rodiegard, H., D. Sandstrom, P. Pelin, N. Hedenstierna, D. Eckerberl, and G. I. Andersson. 2005. “A Digitally Controlled Mems Gyroscope with 3.2 DEG/HR Stability.” In The 13th International Conference on Solid-State Sensors, Actuators and Microsystems, 2005. Digest of Technical Papers. TRANSDUCERS ‘05., vol. 1. IEEE. https://doi.org/10.1109/sensor.2005.1496472
• Rodríguez-Martínez, Sebastián, and Giancarlo Troni. 2024. “Towards a Factor Graph-Based Method Using Angular Rates for Full Magnetometer Calibration and Gyroscope Bias Estimation.” In 2024 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros58592.2024.10801438
• Rogers, Jonathan, and Nathan Slegers. 2013. “Robust Parafoil Terminal Guidance Using Massively Parallel Processing.” Journal of Guidance, Control, and Dynamics 36 (5): 1336–45. https://doi.org/10.2514/1.59782
• Roithmayr, Carlos M., and Jing Pei. 2024. “Effects of Propellant Slosh on Touchdown Stability for Landing Vehicles.” Journal of Spacecraft and Rockets 61 (2): 512–25. https://doi.org/10.2514/1.a35791
• Rojas, Cristian R. 2011. “Identifiability of Multivariable Dynamic Errors-in-Variables Systems.” In 2011 9th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2011.6137999
• Rojas, Cristian R., James S. Welsh, Graham C. Goodwin, and Arie Feuer. 2007. “Robust Optimal Experiment Design for System Identification.” Automatica 43 (6): 993–1008. https://doi.org/10.1016/j.automatica.2006.12.013
• Roloff, H. A. 1957. “Telemetering Receiving System at the Air Force Missile Test Center.” IRE Transactions on Telemetry and Remote Control TRC-3 (3): 6–9. https://doi.org/10.1109/irettrc.1957.6538853
• Roman, Ionuţ-Dragoş, and Petru Dobra. 2026. “Motion-Based Calibration of MEMS Gyroscope.” In 2026 Advanced Topics on Measurement and Simulation (ATOMS). IEEE. https://doi.org/10.1109/atoms69836.2026.11583518
• Rong Huang, Yingzi Guan, and Panxing Huang. 2015. “Study of on-Board Trajectory Generation of Powered Glide Vehicle Based on Footprint Analysis.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119000
• Roshanian, J., Sh. Yazdani, Sh. Bekran Behesht, and M. Ebrahimi. 2015. “2MASS Infrared Star Catalog Data Mining for Use Onboard a Daytime Star Tracker.” In 2015 7th International Conference on Recent Advances in Space Technologies (RAST). IEEE. https://doi.org/10.1109/rast.2015.7208319
• Rott, N. 1953. “Minimum Drag Cambered Rectangular Wing for Supersonic Speeds.” Journal of the Aeronautical Sciences 20 (9): 642–43. https://doi.org/10.2514/8.2770
• Roux, Alicia, Sébastien Changey, Jean-Philippe Lauffenburger, and Jonathan Weber. 2023. “Mortar Trajectory Estimation by a Deep Error-State Kalman Filter in a GNSS-Denied Environment.” In 2023 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans53410.2023.10140013
• Ru, Xu, Nian Gu, Hang Shang, and Heng Zhang. 2022. “MEMS Inertial Sensor Calibration Technology: Current Status and Future Trends.” Micromachines 13 (6): 879. https://doi.org/10.3390/mi13060879
• Rúa, Santiago, Rafael E. Vásquez, Naveen Crasta, Manuel J. Betancur, and Antonio Pascoal. 2022. “Observability Analysis for a Cooperative Range-Based Navigation System That Uses a Rotating Single Beacon.” Ocean Engineering 248: 110697. https://doi.org/10.1016/j.oceaneng.2022.110697
• Ruan, Zhihu, Xukai Ding, Yang Gao, Zhengcheng Qin, and Hongsheng Li. 2023a. “Analysis and Compensation of Bias Drift of Force-to-Rebalanced Micro-Hemispherical Resonator Gyroscope Caused by Assembly Eccentricity Error.” Journal of Microelectromechanical Systems 32 (1): 16–28. https://doi.org/10.1109/jmems.2022.3228268
• Ruan, Zhihu, Xukai Ding, Yunfei Pu, Yang Gao, and Hongsheng Li. 2022. “In-Run Automatic Mode-Matching of Whole-Angle Micro-Hemispherical Resonator Gyroscope Based on Standing Wave Self-Precession.” IEEE Sensors Journal 22 (14): 13945–57. https://doi.org/10.1109/jsen.2022.3181302
• Ruan, Zhihu, Xukai Ding, Zhengcheng Qin, Jia Jia, and Hongsheng Li. 2021b. “Modeling and Compensation of Assembly Inclination Error of Micro Hemispherical Resonator Gyroscope under Force-to-Rebalance Mode.” IEEE Sensors Journal 21 (13): 14726–38. https://doi.org/10.1109/jsen.2021.3072046
• Ruan, Zhihu, Xukai Ding, Zhengcheng Qin, and Hongsheng Li. 2021a. “Compensation of Assembly Eccentricity Error of Micro Hemispherical Resonator Gyroscope.” In 2021 IEEE International Symposium on Robotic and Sensors Environments (ROSE). IEEE. https://doi.org/10.1109/rose52750.2021.9611757
• Ruan, Zhihu, Di Liu, and Yang Gao. 2025. “Identification and Compensation of Driving Electrode Imbalance Errors of Force-to-Rebalanced Micro-Hemispherical Resonator Gyroscope.” IEEE Sensors Journal 25 (5): 8053–66. https://doi.org/10.1109/jsen.2025.3528466
• Ruan, Shuang, Ming Zhang, and Hong Nie. 2024b. “Research and Analysis of Coulomb Friction in Landing Gear Shimmy.” Journal of Aircraft 61 (4): 1143–54. https://doi.org/10.2514/1.c037140
• Ruan, Shuang, Ming Zhang, Shaofei Yang, Xiaohang Hu, and Hong Nie. 2024c. “Research on the Stability and Bifurcation Characteristics of a Landing Gear Shimming Dynamics System.” Aerospace 11 (2): 104. https://doi.org/10.3390/aerospace11020104
• Rubio, Francisco R., Manuel G. Ortega, Francisco Gordillo, and Manuel Vargas. 2010. “Application of Position and Inertial-Rate Control to a 2-DOF Gyroscopic Platform.” Robotics and Computer-Integrated Manufacturing 26 (4): 344–53. https://doi.org/10.1016/j.rcim.2009.11.012
• Rudolph, P. E., and G. Herrendörfer. 1995. “Optimal Experimental Design and Accuracy of Parameter Estimation for Nonlinear Regression Models Used in Long-Term Selection.” Biometrical Journal 37 (2): 183–90. https://doi.org/10.1002/bimj.4710370209
• Ruffin, Stephen M., Anurag Gupta, and David Marshall. 2000. “Supersonic Channel Airfoils for Reduced Drag.” AIAA Journal 38 (3): 480–86. https://doi.org/10.2514/2.985
• Rufino, Giancarlo, and Domenico Accardo. 2003. “Enhancement of the Centroiding Algorithm for Star Tracker Measure Refinement.” Acta Astronautica 53 (2): 135–47. https://doi.org/10.1016/s0094-5765(02)00199-6
• Ruimin, Jiang, Zhou Jun, and Guo Jianguo. 2015. “Autopilot Design for BTT Missile Based on CADET.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260433
• Rupniewski, Marek W. 2025. “SVD Calibration of Inertial Sensors.” Measurement 256: 117929. https://doi.org/10.1016/j.measurement.2025.117929
• Rusnak, Ilan, Allon Guez, and Izhak Bar-Kana. 1993. “Simultaneous State Observability and Parameters Identifiability of Discrete Stochastic Linear Systems.” In 1993 American Control Conference. IEEE. https://doi.org/10.23919/acc.1993.4793065
• Rusnak, I., A. Guez, and I. BarKana. n.d. “State Observability and Parameters Identifiability of Stochastic Linear Systems.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.721052
• Russell, William T. 1958. “Inertial Guidance for Rocket-Propelled Missiles.” Journal of Jet Propulsion 28 (1): 17–24. https://doi.org/10.2514/8.7215
• Ruxton-davies, W. T., and F. Powell. 1970. “A Self Adaptive Automatic Carrier Landing System (ACLS).” In 1970 IEEE Symposium on Adaptive Processes (9th) Decision and Control. IEEE. https://doi.org/10.1109/sap.1970.269969
• Saab, S. S., and K. T. Gunnarsson. 1994. “Automatic Alignment and Calibration of an Inertial Navigation System.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303400
• Saahar, Vithya, and Raja Durai. 2013. “Designing MEMS Based Tuning Fork Gyroscope for Navigation Purpose.” In 2013 International Conference on Communication and Signal Processing. IEEE. https://doi.org/10.1109/iccsp.2013.6577227
• Sabatelli, S., F. Sechi, L. Fanucci, and A. Rocchi. 2011. “A Sensor Fusion Algorithm for an Integrated Angular Position Estimation with Inertial Measurement Units.” In 2011 Design, Automation & Test in Europe. IEEE. https://doi.org/10.1109/date.2011.5763273
• Sabater, Andrew B., Eric Bozeman, and Stephen Hobbs. 2022. “Towards Real-Time Frequency Modulated Accelerometer Bias Calibration.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787522
• Sabatini, Angelo Maria. 2011. “Kalman-Filter-Based Orientation Determination Using Inertial/Magnetic Sensors: Observability Analysis and Performance Evaluation.” Sensors 11 (10): 9182–9206. https://doi.org/10.3390/s111009182
• Sachs, Gottfried. 1977. “A New Concept of Static Stability and Its Flight Testing in Supersonic Flight.” Journal of Aircraft 14 (9): 874–80. https://doi.org/10.2514/3.44623
• Sadr, Negar Elmi, and Hamid Reza Momeni. 2011. “Fuzzy Sliding Mode Control for Missile Autopilot Design.” In 2011 IEEE GCC Conference and Exhibition (GCC). IEEE. https://doi.org/10.1109/ieeegcc.2011.5752563
• Safarinejadian, Behrouz, and Mojtaba Yousefi. 2015. “Static Alignment of Inertial Navigation Systems Using an Adaptive Multiple Fading Factors Kalman Filter.” Systems Science & Control Engineering 3 (1): 351–59. https://doi.org/10.1080/21642583.2015.1025148
• Safeer, Jacob, and Donald Costello. 2026. “Flight Test Evaluation of a Standardized Interface Framework for Autonomous Drone Functionality.” In 2026 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas69441.2026.11598721
• Saglam, Asli, and Derya Yilmaz. 2018. “Increasing the Efficiency of Missile Telemetry Tests by Using Data Compression Techniques.” In 2018 6th International Conference on Control Engineering & Information Technology (CEIT). IEEE. https://doi.org/10.1109/ceit.2018.8751944
• Saini, Vinod K., and Hari B. Hablani. 2014. “Air-to-Air Tracking Performance with Inertial Navigation and Gimballed Radar: A Kinematic Scenario.” IFAC Proceedings Volumes 47 (1): 234–41. https://doi.org/10.3182/20140313-3-in-3024.00029
• Sajjad, Faiza, Muhammad Ihtisham Babar, and Muneeb Ahsan. 2021. “PanAir Study of Variation in Canard Location and Dihedral on Lift Characteristics of a Close-Coupled Wing-Canard Configuration.” In 2021 Seventh International Conference on Aerospace Science and Engineering (ICASE). IEEE. https://doi.org/10.1109/icase54940.2021.9904264
• Sajjadi, Sina, Jacopo Panerati, Sina Soleymanpour, Varunkumar Mehta, Farrokh Janabi-Sharifi, and Iraj Mantegh. 2026. “Evidence-Based Landing Site Selection and Vison-Based Landing for UAVs in Unstructured Environments.” In 2026 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas69441.2026.11598712
• Sakaki, Ryoga, and Masazumi Ueba. 2025. “Short Landing Control Techniques Using Optimization of Flare Time Constant for High-Speed Fixed-Wing UAV.” Aerospace 12 (4): 318. https://doi.org/10.3390/aerospace12040318
• Sakr, Mostafa, and Amr Wassal. 2010. “An Optimized DSP Architecture for MEMS Gyroscope Platforms.” In 2010 International Conference on Energy Aware Computing. IEEE. https://doi.org/10.1109/iceac.2010.5702290
• Salamci, Metin U., and Beyza Gökbilen. 2007. “SDRE Missile Autopilot Design Using Sliding Mode Control with Moving Sliding Surfaces.” IFAC Proceedings Volumes 40 (7): 768–73. https://doi.org/10.3182/20070625-5-fr-2916.00131
• Salazar, Francisco J. T., and Fabricio Galende M. de Carvalho. 2014. “Star Tracker Orientation Optimization Using Non-Dominated Sorting Genetic Algorithm (NSGA).” In 2014 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2014.6836461
• Saleem Yusoof, M., M. Sivapragasam, and M. D. Deshpande. 2016. “Strip Distortion Generator for Simulating Inlet Flow Distortion in Gas Turbine Engine Ground Test Facilities.” Propulsion and Power Research 5 (4): 287–301. https://doi.org/10.1016/j.jppr.2016.11.004
• Saletović, Enes, and Malik Kriještorac. 2025. “A Method for Geolocating Distant Objects Using a MEMS Gyroscope.” In 2025 24th International Symposium INFOTEH-JAHORINA (INFOTEH). IEEE. https://doi.org/10.1109/infoteh64129.2025.10959211
• Salib, A., M. Moussa, A. Moussa, and N. El-Sheimy. 2020. “Visual Odometry/Inertial Integration for Enhanced Land Vehicle Navigation in GNSS Denied Environment.” In 2020 IEEE 92nd Vehicular Technology Conference (VTC2020-Fall). IEEE. https://doi.org/10.1109/vtc2020-fall49728.2020.9348698
• Salman, Ahmed M., Sherif Hammad, Shady A. Maged, and Mohamed A. E. Mahmoud. 2022. “MEMS Gyroscope Drift Performance Enhancement Using Single Axis Rotation Modulation Technique.” In 2022 18th International Computer Engineering Conference (ICENCO). IEEE. https://doi.org/10.1109/icenco55801.2022.10032461
• Salmaniw, Yurij, and Alexander P. Browning. 2025. “Structural Identifiability of Linear-in-Parameter Parabolic PDEs through Auxiliary Elliptic Operators.” Journal of Mathematical Biology 91 (1): 4. https://doi.org/10.1007/s00285-025-02225-w
• Samirbhai, Mehta Deval, Shoushun Chen, and Kay Soon Low. 2016. “A High Accuracy Star Tracker Using Running Sequential Angular Match Technique.” In 2016 IEEE Region 10 Conference (TENCON). IEEE. https://doi.org/10.1109/tencon.2016.7848747
• Samuel, A. 2003. “Integration of Inertial Navigation System and Global Positioning System.” In 7th International Multi Topic Conference, 2003. INMIC 2003.. IEEE. https://doi.org/10.1109/inmic.2003.1416733
• Sanatdoost, N. N., V. Masek, and Lihong Zhang. 2013. “A Z-Axis MEMS Gyroscope with Improved Sensitivity.” In 2013 IEEE Sensors Applications Symposium Proceedings. IEEE. https://doi.org/10.1109/sas.2013.6493574
• Sanches, Leonardo, Thiago A. M. Guimarães, and Flávio D. Marques. 2021. “Nonlinear Energy Sink to Enhance the Landing Gear Shimmy Performance.” Acta Mechanica 232 (7): 2605–22. https://doi.org/10.1007/s00707-021-02985-8
• Sang, Peng, Wenbo Liu, Yang Cao, Hongbo Xue, and Baoquan Li. 2024. “Research on Precise Attitude Measurement Technology for Satellite Extension Booms Based on the Star Tracker.” Sensors 24 (20): 6671. https://doi.org/10.3390/s24206671
• Sankar, Ram B., Bijnan Bandyopadhyay, and Hemendra Arya. 2016. “Roll Autopilot Design of a Tactical Missile Using Higher Order Sliding Mode Technique.” In 2016 Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/indiancc.2016.7441143
• Şanlan, Abdülbaki, Hasan Taha Bağcı, and Emre Koyuncu. 2025. “Particle Filter-Based Localization Using Visual Feature Synchronization in GNSS-Denied Navigation.” In 2025 Integrated Communications, Navigation and Surveillance Conference (ICNS). IEEE. https://doi.org/10.1109/icns65417.2025.10976891
• Sarapuloff, Sergii A., Huinam Rhee, and Taras G. Bondarenko. 2016. “Simulations and Experiments of Low-Frequency Spectrum of Hemispherical Resonator Gyroscope.” In 2016 IEEE International Symposium on Inertial Sensors and Systems. IEEE. https://doi.org/10.1109/isiss.2016.7435558
• Saratayon, Peerayudh, and Somrak Petchartee. 2015. “IRIG S-Band Missile Telemetry.” In 2015 Asian Conference on Defence Technology (ACDT). IEEE. https://doi.org/10.1109/acdt.2015.7111597
• Sarrafian, A. Harrison. 1966. “A Versatile Stellar-Referenced Inertial Platform.” IEEE Transactions on Aerospace and Electronic Systems AES-2 (6): 497–501. https://doi.org/10.1109/taes.1966.4502047
• Sarvi, Mehdi Nasiri, Dariush Abbasi-Moghadam, Mojtaba Abolghasemi, and Heshmatollah Hoseini. 2020. “Design and Implementation of a Star-Tracker for LEO Satellite.” Optik 208: 164343. https://doi.org/10.1016/j.ijleo.2020.164343
• Sato, Masayuki. 2013. “Robust Gain-Scheduled Flight Controller Using Inexact Scheduling Parameters.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6580911
• Sato, Tetsuya, Hideyuki Taguchi, Hiroaki Kobayashi, et al. 2007. “Development Study of Precooled-Cycle Hypersonic Turbojet Engine for Flight Demonstration.” Acta Astronautica 61 (1–6): 367–75. https://doi.org/10.1016/j.actaastro.2007.01.012
• Savage, Paul G. 2002. “Analytical Modeling of Sensor Quantization in Strapdown Inertial Navigation Error Equations.” Journal of Guidance, Control, and Dynamics 25 (5): 833–42. https://doi.org/10.2514/2.4963
• Savage, Paul G. 2018. “Improved Strapdown Inertial Measurement Unit Calibration Procedures.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373422
• Savino, Raffaele, and Giuseppe Pezzella. 2003. “Numerical Analysis of Supersonic Combustion Ramjet with Upstream Fuel Injection.” International Journal for Numerical Methods in Fluids 43 (2): 165–81. https://doi.org/10.1002/fld.602
• Scherzinger, B. M. n.d. “Inertial Navigator Error Models for Large Heading Uncertainty.” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509118
• Scherzinger, B. M., and D. B. Reid. 1994. “Modified Strapdown Inertial Navigator Error Models.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303345
• Schleich, W., and P. Dobiasch. 1984. “Noise Analysis of Ring-Laser Gyroscope with Arbitrary Dither.” Optics Communications 52 (1): 63–68. https://doi.org/10.1016/0030-4018(84)90074-9
• Schmidt, George T. 2015b. “Navigation Sensors and Systems in GNSS Degraded and Denied Environments.” Chinese Journal of Aeronautics 28 (1): 1–10. https://doi.org/10.1016/j.cja.2014.12.001
• Schmidt, G. T. 2018. “Navigation Sensors and Systems in GNSS Degraded and Denied Environments 2018: (Or How i Learned to Stop Worrying about GPS).” In 2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2018.8405890
• Schmidt, G. T., and R. H. Setterlund. 1980. “Cruise-Missile-Carrier Navigation Requirements.” Journal of Guidance and Control 3 (6): 487–93. https://doi.org/10.2514/3.19720
• Schmidtbauer, Bengt. 1978. “High-Accuracy Sounding Rocket Attitude Estimation Using Star Sensor Data.” IEEE Transactions on Aerospace and Electronic Systems AES-14 (6): 891–98. https://doi.org/10.1109/taes.1978.308553
• Schmitt, Lorenz, and Walter Fichter. 2016. “Observability Criteria and Null-Measurement Kalman Filter for Vision-Aided Inertial Navigation.” Journal of Guidance, Control, and Dynamics 39 (4): 770–80. https://doi.org/10.2514/1.g001146
• Schnerr, Guenter H., and Ulrich Dohrmann. 1994. “Drag and Lift in Nonadiabatic Transonic Flow.” AIAA Journal 32 (1): 101–7. https://doi.org/10.2514/3.11956
• Scholz, Felix, Aaron Theuser, Andreas Hupfer, and Isabel Bayerdörfer. 2026. “Manufacture-Oriented Design of a Topology-Optimized Nose Landing Gear Fork for a Small Aircraft with Retractable Landing Gear.” CEAS Aeronautical Journal. https://doi.org/10.1007/s13272-026-00958-y
• Schouler, Marc, Ysolde Prévereaud, and Luc Mieussens. 2021. “Atmospheric Model Effect on Flight Data Reconstruction: Application to the Early Phase of the IXV Reentry.” International Journal of Computational Fluid Dynamics 35 (8): 594–609. https://doi.org/10.1080/10618562.2021.2016720
• Schram, Matt, and Venkat Narayanaswamy. 2026. “Unstart Dynamics of Hypersonic Busemann Inlet at Non-Zero Angles of Attack.” Experiments in Fluids 67 (6): 64. https://doi.org/10.1007/s00348-026-04215-0
• Schreiber, K. U., A. Gebauer, A. Velikoseltsev, and J.-P. R. Wells. 2014. “Precision Cavity Control for the Stable Operation of a Large Ring Laser Gyroscope.” In 2014 International Conference Laser Optics. IEEE. https://doi.org/10.1109/lo.2014.6886320
• Schrempf, A., and L. del Re. 2001. “Linear in Parameters Identifiability of Extended Bilinear Systems.” In 2001 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2001.7075852
• Schreutelkamp, Frank, and Christian Hirt. 2026. “A New Vertical Deflection Dataset Combining Modern TZK2-D and Historical Visual Observations: Analysis and Comparison with the Gravimetric Quasi-Geoid Model for the Netherlands.” Journal of Geodesy 100 (8): 64. https://doi.org/10.1007/s00190-026-02089-y
• Schuck, Walter H. 1966. “Vidicon Star Tracker.” Applied Optics 5 (4): 489. https://doi.org/10.1364/ao.5.000489
• Schuler, P., C. Kupitz, V. Hofmeister, A. Younas, and T. Martin. 2022. “Influence of IMU Parameters on Navigation Performance in Network-Based Collaborative Navigation Scenarios.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926329
• Schulte, Peter Z., and David A. Spencer. 2020. “State Machine Fault Protection Architecture for Aerospace Vehicle Guidance, Navigation, and Control.” Journal of Aerospace Information Systems 17 (2): 70–85. https://doi.org/10.2514/1.i010673
• Schumacher, C., and P. Khargonekar. 1997. “A Comparison of Missile Autopilot Designs Using /Spl Hscr//sub /Spl Infin// Control with Gain Scheduling and Nonlinear Dynamic Inversion.” In Proceedings of the 1997 American Control Conference (Cat. No.97CH36041). IEEE. https://doi.org/10.1109/acc.1997.611957
• Schumacher, Corey, and Pramod P. Khargonekar. 1998. “Missile Autopilot Designs Using H8 Control with Gain Scheduling and Dynamic Inversion.” Journal of Guidance, Control, and Dynamics 21 (2): 234–43. https://doi.org/10.2514/2.4248
• Schumacher, D. A., and N. H. McClamroch. 1994. “Planar Autopilot Design for the EMRAAT Missile Using Sliding Modes.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 3. IEEE. https://doi.org/10.1109/acc.1994.735180
• Schwartz, Sylvain, Gilles Feugnet, and Jean-Paul Pocholle. 2007a. “Diode-Pumped Solid-State Ring Laser Gyroscope.” In 2007 Conference on Lasers and Electro-Optics (CLEO). IEEE. https://doi.org/10.1109/cleo.2007.4453345
• Screenuch, T., A. Tsourdos, E. Hughes, and B. White. 2006. “Fuzzy Gain-Scheduled Missile Autopilot Design Using Evolutionary Algorithms.” IEEE Transactions on Aerospace and Electronic Systems 42 (4): 1323–39. https://doi.org/10.1109/taes.2006.314575
• Sebastin, J. Sarathkumar, and Naga Hari Vignesh N. 2026. “Numerical Investigation of Aerothermochemical Processes in a Dual-Combustion Ramjet Engine Using Advanced Reactive Flow Simulation.” Interactions 247 (1): 375. https://doi.org/10.1007/s10751-026-02719-z
• Sedlmair, Nicolas, Julian Theis, and Frank Thielecke. 2019. “Automatic Three-Point Landing of a UAV with H∞-Control in D-Implementation.” IFAC-PapersOnLine 52 (12): 316–21. https://doi.org/10.1016/j.ifacol.2019.11.262
• Sedlmair, Nicolas, Julian Theis, and Frank Thielecke. 2022. “Flight Testing Automatic Landing Control for Unmanned Aircraft Including Curved Approaches.” Journal of Guidance, Control, and Dynamics 45 (4): 726–39. https://doi.org/10.2514/1.g005917
• Sedov, L. I. 1977. “Inertial Navigation Equations Based on Relativistic Effects.” Acta Astronautica 4 (3–4): 231–35. https://doi.org/10.1016/0094-5765(77)90048-0
• Selezneva, Maria Sergeevna, Konstantin Avenirovich Neusypin, and Surkova Anastasiia Dmitrievna. 2026. “Study of the Inertial Navigation System Error Estimation Accuracy for a Spacecraft Re-Entering the Atmosphere.” In 2026 International Conference on Integrated Intelligence and Cognitive Engineering (ICIICE). IEEE. https://doi.org/10.1109/iciice69672.2026.11565315
• Sells, Ray. 2015. “A Novel Missile Autopilot with Remarkable Robustness.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119223
• Selvaggio, Mario, Federico Esposito, Vincenzo Lippiello, and Fabio Ruggiero. 2024. “Shared-Control Teleoperation Methods for a Cable-Suspended Dual-Arm Unmanned Aerial Manipulator.” In 2024 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas60882.2024.10557097
• Sen, M. De La. 1983. “Application of the Non-Periodic Sampling to the Identifiability and Model Matching Problems in Dynamic Systems.” International Journal of Systems Science 14 (4): 367–83. https://doi.org/10.1080/00207728308926464
• Sengupta, N., and M. D. Gupta. 1984. “Effect of Thunderstorm on Microwave Line-of-Sight Propagation.” IEEE Transactions on Antennas and Propagation 32 (2): 196–200. https://doi.org/10.1109/tap.1984.1143291
• Senkal, D., E. J. Ng, V. Hong, et al. 2015. “Parametric Drive of a Toroidal MEMS Rate Integrating Gyroscope Demonstrating < 20 PPM Scale Factor Stability.” In 2015 28th IEEE International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2015.7050878
• Senkel, Luise, Andreas Rauh, and Harald Aschemann. 2013. “Optimal Input Design for Online State and Parameter Estimation Using Interval Sliding Mode Observers.” In 52nd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2013.6759931
• Seo, Yeong-Bin, Haesung Yu, Kyungdon Ryu, et al. 2022. “Analysis of Gyro Bias Depending on the Position of Inertial Measurement Unit in Rotational Inertial Navigation Systems.” Sensors 22 (21): 8355. https://doi.org/10.3390/s22218355
• Seong, Sang. 2006. “A Compensation Method for Setting Misalignment Error in Gyroscope Deterministic Error Estimation Test.” In 2006 SICE-ICASE International Joint Conference. IEEE. https://doi.org/10.1109/sice.2006.314867
• Sepahi-Younsi, Javad. 2022. “Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Buzz.” Aerospace Science and Technology 120: 107246. https://doi.org/10.1016/j.ast.2021.107246
• Sepahi-Younsi, Javad. 2025. “Experimental Study of the Buzz Phenomenon in a Supersonic Inlet with and without the Bleed.” Aerospace Science and Technology 163: 110346. https://doi.org/10.1016/j.ast.2025.110346
• Sepahi-Younsi, Javad, and Safa Esmaeili. 2023. “Source of Buzz Instability in a Supersonic Air Inlet.” Aerospace Science and Technology 138: 108334. https://doi.org/10.1016/j.ast.2023.108334
• Seraj, Sabet, Anil Yildirim, and Joaquim R. R. A. Martins. 2025. “Aerodynamic Shape Optimization of a Supersonic Transport Including a Subsonic Static Margin Constraint.” Aerospace Science and Technology 166: 110565. https://doi.org/10.1016/j.ast.2025.110565
• Serban, R., and J. S. Freeman. 2001. “Identification and Identifiability of Unknown Parameters in Multibody Dynamic Systems.” Multibody System Dynamics 5 (4): 335–50. https://doi.org/10.1023/a:1011434711375
• Seren, C., G. Hardier, and C. Roos. 2013. “Swarm Intelligence & System Identification: A Hybrid Discrete Jumping Frogs Algorithm for Optimal Input Design.” IFAC Proceedings Volumes 46 (20): 671–76. https://doi.org/10.3182/20130902-3-cn-3020.00062
• Shaaban, Ghadeer, Hassen Fourati, Christophe Prieur, and Alain Kibangou. 2024. “Q-Learning-Based Noise Covariance Matrices Adaptation in Kalman Filter for Inertial Navigation.” IFAC-PapersOnLine 58 (21): 96–101. https://doi.org/10.1016/j.ifacol.2024.10.150
• Shachar, Sahar, Joseph Z. Ben-Asher, and Johannes Diepolder. 2025. “Optimal Trajectory for a Hypersonic Cruise Missile with a Nonconvex Control Set.” Journal of Guidance, Control, and Dynamics 48 (6): 1241–52. https://doi.org/10.2514/1.g008439
• Shaffer, Phillip L. 1989. “Experience with Implementation of a Turbojet Engine Control Program on a Multiprocessor.” In 1989 American Control Conference. IEEE. https://doi.org/10.23919/acc.1989.4790648
• Shah, M. Zamurad, Raza Samar, and A. I. Bhatti. 2010. “Adaptive Sliding Mode Roll Control of a Canard-Controlled Missile.” In 2010 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2010.5498705
• Shahkar, Shahram, and Khashayar Khorasani. 2023. “Optimization of Localization Error in Multi-Agent Systems through Cooperative Positioning: Autonomous Navigation in Partially Denied GNSS Environments.” In 2023 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial56358.2023.10103968
• Shakhov, Vladimir V. 2013. “Experiment Design for Parameter Estimation in Sensing Models.” In Wireless Access Flexibility. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-39805-6_13
• Shakhov, Vladimir V., and Insoo Koo. 2017. “Experiment Design for Parameter Estimation in Probabilistic Sensing Models.” IEEE Sensors Journal 17 (24): 8431–37. https://doi.org/10.1109/jsen.2017.2766089
• Shamma, Jeff S., and James R. Cloutier. 1992a. “A Linear Parameter Varying Approach to Gain Scheduled Missile Autopilot Design.” In 1992 American Control Conference. IEEE. https://doi.org/10.23919/acc.1992.4792317
• Shamma, J. S., and J. R. Cloutier. 1992b. “Trajectory Scheduled Missile Autopilot Design.” In [Proceedings 1992] The First IEEE Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.1992.269870
• Shamma, Jeff S., and James R. Cloutier. 1993. “Gain-Scheduled Missile Autopilot Design Using Linear Parameter Varying Transformations.” Journal of Guidance, Control, and Dynamics 16 (2): 256–63. https://doi.org/10.2514/3.20997
• Shan, Bin, Yongyuan Qin, Yuegang Wang, Bo Yang, and Zhibin Guo. 2014. “SINS/geomagnetic Matching/barometric Altimeter Integrated Navigation Method for Land Vehicle.” In 2014 IEEE International Conference on Signal Processing, Communications and Computing (ICSPCC). IEEE. https://doi.org/10.1109/icspcc.2014.6986146
• Shang, Kejun, Ming Lei, Haowei Li, et al. 2025. “Tactical-Grade Three-Axis Interferometric Fiber-Optic Gyroscope with a Silica Integrated Optical Chip.” IEEE Sensors Journal 25 (7): 10957–63. https://doi.org/10.1109/jsen.2025.3541109
• Shang, Kejun, Ming Lei, Qiang Xiang, Yonglin Na, and Lizhe Zhang. 2021. “Tactical-Grade Interferometric Fiber Optic Gyroscope Based on an Integrated Optical Chip.” Optics Communications 485: 126729. https://doi.org/10.1016/j.optcom.2020.126729
• Shankar, Atava Somu, and Suresh E. Kumar. 2023. “Simulation and Analysis of Accelerometer Bias Estimation in Inertial Navigation System.” In 2023 International Conference on Circuit Power and Computing Technologies (ICCPCT). IEEE. https://doi.org/10.1109/iccpct58313.2023.10245630
• Shao, Yi-han, Bin Han, and Ying Luo. 2023. “A Method Based on CNN-BiLSTM for UAV Navigation Error Compensation in GNSS Denied Environment.” In 2023 9th International Conference on Computer and Communications (ICCC). IEEE. https://doi.org/10.1109/iccc59590.2023.10507546
• Sharma, Mrigank, Elie H. Sarraf, and Edmond Cretu. 2011. “A Novel Dynamic Pull-in MEMS Gyroscope.” Procedia Engineering 25: 55–58. https://doi.org/10.1016/j.proeng.2011.12.014
• Shaw, S. W., and J. F. Arnold. n.d. “Design and Implementation of a Fully Automated OTH Radar Tracking System.” In Proceedings International Radar Conference. IEEE. https://doi.org/10.1109/radar.1995.522561
• Sheffels, M. L. 1992. “A Fault-Tolerant Air Data/inertial Reference Unit.” In [1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.1992.282171
• Shehabaz, S. M. D., S. K. Gugulothu, Raju Muthyala, R. Harish, and Praveen Barmavatu. 2026. “Multi-Angle Forward-Slide Cavity Design Optimization for Improved Hydrogen Mixing and Flame-Holding in High-Speed Air-Breathing Propulsion Systems.” Aerospace Science and Technology 177: 112277. https://doi.org/10.1016/j.ast.2026.112277
• Sheikhpour, Soroush, and Mohamed M. Atia. 2020. “An Enhanced Visual-Inertial Navigation System Based on Multi-State Constraint Kalman Filter.” In 2020 IEEE 63rd International Midwest Symposium on Circuits and Systems (MWSCAS). IEEE. https://doi.org/10.1109/mwscas48704.2020.9184501
• Shen, S. C., C. J. Chen, and H. J. Huang. 2010b. “A New Calibration Method for MEMS Inertial Sensor Module.” In 2010 11th IEEE International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2010.5464015
• Shen, Chong, Xiyuan Chen, Jing Yu, and Jun Wu. 2011. “Random Drift Modeling and Compensation for Fiber Optic Gyroscope under Vibration.” In 2011 IEEE International Instrumentation and Measurement Technology Conference. IEEE. https://doi.org/10.1109/imtc.2011.5944202
• Shen, Qiang, He Li, Yongcun Hao, Weizheng Yuan, and Honglong Chang. 2016. “Bias Contribution Modeling for a Symmetrical Micromachined Coriolis Vibratory Gyroscope.” IEEE Sensors Journal 16 (3): 723–33. https://doi.org/10.1109/jsen.2015.2489241
• Shen, Kai, Tingxin Liu, Yuelun Li, Ning Liu, and Wenhao Qi. 2023. “Robust Multi-Model Estimation for Reliable Relative Navigation Based on Observability and Abnormity Analysis.” IEEE Transactions on Intelligent Transportation Systems 24 (5): 5144–58. https://doi.org/10.1109/tits.2023.3245104
• Shen, Xiang, Liye Zhao, and Dunzhu Xia. 2019. “Research on the Disc Sensitive Structure of a Micro Optoelectromechanical System (MOEMS) Resonator Gyroscope.” Micromachines 10 (4): 264. https://doi.org/10.3390/mi10040264
• Shen, Yaojie, Xudong Zheng, Chen Fang, Junjie Zeng, Wenjie Hu, and Zhonghe Jin. 2026. “A Temperature Self-Calibrated MEMS Gyroscope with 0.007°/h/K Bias Drift Coefficient Using Real-Time Parametric Quality Factor Control and Mode Matching.” Microsystems & Nanoengineering 12 (1): 102. https://doi.org/10.1038/s41378-026-01181-9
• Shen Yong and Wu Yang-bo. 2011. “Sensor Installation Error Analysis and Correction in Vehicle Inertial Positioning System.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5777905
• Shi, Luqiang, Yigang He, Bing Li, Yuting Wu, Yuan Huang, and Tongtong Cheng. 2019c. “On-Line Measurement of Dynamic Tilt Angle by Compensating Gyroscope Drift Error.” IEEE Transactions on Instrumentation and Measurement 68 (9): 3244–52. https://doi.org/10.1109/tim.2018.2878073
• Shi, Qiongnan, Jiajun Ma, Zhuo Zhang, Bin Long, and Shan Xiao. 2026. “Research on Temperature Error Compensation of Fiber Optic Gyroscope Based on Viscoelastic Dynamic Mechanism.” IEEE Photonics Journal 18 (3): 7100807–7100807. https://doi.org/10.1109/jphot.2026.3692503
• Shi, Haoming, Zhiqi Niu, Lu Hun, Penghui Zhang, Feifei Wang, and Liangyu Zhao. 2023. “A Full-Trajectory Design Method for a Waverider Hypersonic Vehicle with Boost-Glide-Attack Process.” In 2023 38th Youth Academic Annual Conference of Chinese Association of Automation (YAC). IEEE. https://doi.org/10.1109/yac59482.2023.10401454
• Shi, Qin, Anping Qiu, Yang Zhao, and Guoming Xia. 2020. “Silicon Micro Gyroscope with 10°/h Stability in Wide Temperature Range.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090083
• Shi, H., W. Wang, H. Yu, and Z. Zhao. 2017. “A Method of Starting Fiber Optic Gyroscope outside Its Optical Measuring Range.” In 2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2017.7995667
• Shi, Yan, Xiang Xi, Wei Li, et al. 2019b. “An Improved Fabrication Process for Micro Hemispherical Resonator Gyroscope.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739642
• Shi, Zhen, Jie Yang, Peng Yue, and Zijian Cheng. 2010a. “A New Calibration and Compensation Method for Installation Errors of Accelerometers in Gyroscope Free Strap-down Inertial Navigation System.” In The 2010 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2010.5512138
• Shi, Lei, Wenzhe Zhang, Yuan Cheng, and Zhihong Deng. 2019a. “Gravity Aided Inertial Navigation Path Planning Algorithm Based on Underwater Vehicle Constraint and Bezier Curve.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866183
• Shi Qiang Liu, Rong Zhu, and Heng Gao Ding. 2015. “A Temperature Compensation Method for Micromachined Thermal Gas Gyroscope.” In 2015 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2015.7370336
• Shiau, Le-Chung, Shih-Yao Kuo, and Yen-Pin Liu. 2012. “Aerothermoelastic Analysis of Composite Laminated Plates.” Composite Structures 94 (6): 1982–90. https://doi.org/10.1016/j.compstruct.2012.01.022
• Shibata, Minoru. 1986. “Error Analysis Strapdown Inertial Navigation Using Quaternions.” Journal of Guidance, Control, and Dynamics 9 (3): 379–81. https://doi.org/10.2514/3.20119
• Shijie, Tu, and Chen Hang. 2015. “Design of Missile Autopilot Controller by Use of Optimized Fuzzy/PID Combined Method.” In 2015 IEEE International Conference on Signal Processing, Communications and Computing (ICSPCC). IEEE. https://doi.org/10.1109/icspcc.2015.7338842
• Shima, Tal, Yaakov Oshman, and Josef Shinar. 2002. “Efficient Multiple Model Adaptive Estimation in Ballistic Missile Interception Scenarios.” Journal of Guidance, Control, and Dynamics 25 (4): 667–75. https://doi.org/10.2514/2.4961
• Shiryaev, Alexandr, and Sergey Serebryansky. 2022. “Methods for Reducing Temperature Heating in Supersonic Aircraft Structures.” In 2022 15th International Conference Management of large-scale system development (MLSD). IEEE. https://doi.org/10.1109/mlsd55143.2022.9934688
• Shmyglevskii, Iu. D. 1958. “Supersonic Profiles with Minimum Drag.” Journal of Applied Mathematics and Mechanics 22 (2): 368–74. https://doi.org/10.1016/0021-8928(58)90116-3
• Shooshtari, Pooneh, Albert Leung, and John Jones. 2012. “Suppression of Spurious Signals in Thermal MEMS Gyroscope.” In 2012 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2012.6411394
• Shpagin, Pavel, and Taras Panchenko. 2026. “NaviLoc: Trajectory-Level Visual Localization for GNSS-Denied UAV Navigation.” Drones 10 (2): 97. https://doi.org/10.3390/drones10020097
• Shtessel, Y. B. n.d. “Sliding Mode Stabilization of Three Axis Inertial Platform.” In Proceedings of 26th Southeastern Symposium on System Theory. IEEE. https://doi.org/10.1109/ssst.1994.287911
• Shtessel, Yu., and D. Krupp. 1997. “Reusable Launch Vehicle Trajectory Control in Sliding Modes.” In Proceedings of the 1997 American Control Conference (Cat. No.97CH36041). IEEE. https://doi.org/10.1109/acc.1997.609256
• Shu, Yunyi, Yoshikazu Hirai, and Toshiyuki Tsuchiya. 2020. “Scale-Factor Analysis of a Geometrically Compensated (100) Single-Crystal Silicon Vibratory Ring Gyroscope.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090073
• Shu, Yunyi, Yoshikazu Hirai, Toshiyuki Tsuchiya, and Osamu Tabata. 2018. “Geometrical Compensation of (100) Single-Crystal Silicon Mode-Matched Vibratory Ring Gyroscope.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358156
• Shu-Ping, Xu, and Wang Zhi. 2011. “Control System Design Based on ADRC Techniques for Low Speed Spinning Ballistic Missile.” Energy Procedia 13: 8469–76. https://doi.org/10.1016/j.egypro.2011.12.611
• Shue, Shyh-Pyng, and Ramesh K. Agarwal. 1999. “Design of Automatic Landing Systems Using Mixed H/H Control.” Journal of Guidance, Control, and Dynamics 22 (1): 103–14. https://doi.org/10.2514/2.4356
• Shujah, Adnan, Syed Ali Raza Bukhari, and Muhammad Mubasher Saleem. 2021. “Design of a Multi-DoF MEMS Gyroscope for Inertial Navigation Considering SOI-MUMPs Microfabrication Process Constraints.” In 2021 International Conference on Robotics and Automation in Industry (ICRAI). IEEE. https://doi.org/10.1109/icrai54018.2021.9651390
• Shupe, David M. 1981. “Fiber Resonator Gyroscope: Sensitivity and Thermal Nonreciprocity.” Applied Optics 20 (2): 286. https://doi.org/10.1364/ao.20.000286
• Shuster, Malcolm D. 2004. “SCAD—a Fast Algorithm for Star Camera Attitude Determination.” Journal of the Astronautical Sciences 52 (3): 391–404. https://doi.org/10.1007/bf03546370
• Si, Fan, Yan Zhao, and Xiaolei Zhang. 2017. “The Estimation of Wing Flexure Deformation in Transfer Alignment Based on Inertial Sensors Network.” In 2017 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2017.7943568
• Sidar, M., and Y. Bar-Shlomo. 1972. “A Comparison of the Effectiveness of Some Adaptive Optimal Filtering Techniques Applied to the Gyrocompassing Problem.” IFAC Proceedings Volumes 5 (1): 251–59. https://doi.org/10.1016/s1474-6670(17)68339-3
• Siemes, Christian, Moritz Rexer, and Roger Haagmans. 2019. “GOCE Star Tracker Attitude Quaternion Calibration and Combination.” Advances in Space Research 63 (3): 1133–46. https://doi.org/10.1016/j.asr.2018.10.030
• Sierociuk, Dominik, Michal Macias, and Konrad Andrzej Markowski. 2024. “Fractional-Order Identification of Gyroscope MEMS Noise under Various Temperature Conditions.” Sensors 24 (23): 7504. https://doi.org/10.3390/s24237504
• Sierociuk, Dominik, Michal Macias, and Konrad Andrzej Markowski. 2025. “Fractional-Order Identification of Gyroscope MEMS Noise under Helium Exposure.” Sensors 25 (22): 6954. https://doi.org/10.3390/s25226954
• Siguerdidjane, Houria, and Emmanuel Devaud. 2000. “Nonlinear Missile Autopilot Design Based on Angle of Attack Normal Form.” European Journal of Control 6 (2): 154–64. https://doi.org/10.1016/s0947-3580(00)70923-x
• Silva, Tiago, and Pedro Batista. 2019. “Long Baseline Aided Inertial Navigation System with Clock Offset Estimation.” In 2019 18th European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2019.8796139
• Silva, Felipe O., Elder M. Hemerly, and Waldemar C. L. Filho. 2014. “Influence of Latitude in Coarse Self-Alignment of Strapdown Inertial Navigation Systems.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851496
• Silva, Felipe O., and Leonardo A. Vieira. 2022. “Optimizing the Gains of Baro-Inertial Vertical Channel Mechanizations.” In 2022 IEEE 31st International Symposium on Industrial Electronics (ISIE). IEEE. https://doi.org/10.1109/isie51582.2022.9831633
• Simak, Vojtech, Jan Andel, Dusan Nemec, and Juraj Kekelak. 2024. “Online Calibration of Inertial Sensors Based on Error Backpropagation.” Sensors 24 (23): 7525. https://doi.org/10.3390/s24237525
• Sineglazov, Viktor. 2014. “Main Features of Terrain-Aided Navigation Systems.” In 2014 IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc.2014.6979728
• Sineglazov, V. M., and V. S. Ischenko. 2019. “Intelligent Visual Navigation System of High Accuracy.” In 2019 IEEE 5th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD). IEEE. https://doi.org/10.1109/apuavd47061.2019.8943916
• Sinelnikov, A. O., N. V. Tikhmenev, A. A. Ushanov, and S. I. Nazarov. 2023. “Interaction of the Dither of a Ring Laser Gyroscope with an External Mechanical Disturbance.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168376
• Singh, Jaskirat, Neel Adwani, Harikumar Kandath, and K. Madhava Krishna. 2023. “RHFSafeUAV: Real-Time Heuristic Framework for Safe Landing of UAVs in Dynamic Scenarios.” In 2023 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas57906.2023.10156604
• Singh, Shashiprakash, and Radhakant Padhi. 2009. “Automatic Path Planning and Control Design for Autonomous Landing of UAVs Using Dynamic Inversion.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160444
• Singh, Sajal, Jong-Kwan Woo, Guohong He, Jae Yoong Cho, and Khalil Najafi. 2020. “0.0062^circ/sqrthr Angle Random Walk and 0.027^circ/hr Bias Instability from a Micro-Shell Resonator Gyroscope with Surface Electrodes.” In 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems46641.2020.9056391
• Singla, Puneet, D. Todd Griffith, Anup Katake, and John L. Junkins. 2007. “Attitude and Interlock Angle Estimation Using Split-Field-of-View Star Tracker.” Journal of the Astronautical Sciences 55 (1): 85–105. https://doi.org/10.1007/bf03256516
• Sithara, S. S., and P. S. Shenil. 2022. “Recovery of Spent Stage of Reusable Launch Vehicle on a Droneship.” In 2022 International Conference on Computing, Communication, and Intelligent Systems (ICCCIS). IEEE. https://doi.org/10.1109/icccis56430.2022.10037641
• Skarpetis, M. G., F. N. Koumboulis, and X. Loutas. 2018. “Missile Autopilot Design Using a Robust Asymptotic Tracking Controller.” In 2018 IEEE 22nd International Conference on Intelligent Engineering Systems (INES). IEEE. https://doi.org/10.1109/ines.2018.8523970
• Skog, Isaac, John-Olof Nilsson, and Peter Handel. 2014. “An Open-Source Multi Inertial Measurement Unit (MIMU) Platform.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782523
• Skog, Isaac, Adrian Schumacher, and Peter Handel. 2006. “A Versatile PC-Based Platform for Inertial Navigation.” In Proceedings of the 7th Nordic Signal Processing Symposium - NORSIG 2006. IEEE. https://doi.org/10.1109/norsig.2006.275238
• Skoogh, D., and A. Lennartsson. 2006. “A Method for Multiple Fault Detection and Isolation of Redundant Inertial Navigation Sensor Configurations.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650631
• Slabospitskii, A. S. 1993. “Energy Interpretation of Identifiability Conditions in Dynamic Systems.” Journal of Soviet Mathematics 66 (2): 2218–20. https://doi.org/10.1007/bf01098611
• Slifka, R. 1960. “An Inertial Guidance System Field Test Program for a Ballistic Missile Weapon System.” Proceedings of the IRE 48 (4): 554–57. https://doi.org/10.1109/jrproc.1960.287405
• Smeltzer, D. B., D. A. Durston, and V. R. Stewart. 1983. “Experimental Wing and Canard Jet-Flap Aerodynamics.” Journal of Aircraft 20 (10): 833–34. https://doi.org/10.2514/3.44950
• Smirnov, N. N., V. F. Nikitin, L. I. Stamov, E. V. Mikhalchenko, and V. V. Tyurenkova. 2019. “Three-Dimensional Modeling of Rotating Detonation in a Ramjet Engine.” Acta Astronautica 163: 168–76. https://doi.org/10.1016/j.actaastro.2019.02.016
• Smith, F. E., M. E. Campbell, T. J. Blucker, C. E. Manry, and I. Saulietis. 1983. “Shuttle Orbiter Stellar-Inertial Reference System.” Journal of Guidance, Control, and Dynamics 6 (6): 424–31. https://doi.org/10.2514/3.8520
• Smith, J. M., P. B. Schoonmaker, E. E. Pyron, and R. L. Benbow. 1972b. “Principles of Performance Monitoring with Application to Automatic Landing.” Journal of Aircraft 9 (5): 339–46. https://doi.org/10.2514/3.58990
• Snyder, S., B. Schipper, L. Vallot, N. Parker, and C. Spitzer. n.d.-a. “Differential GPS/inertial Navigation Approach/landing Flight Test Results.” In IEEE PLANS 92 Position Location and Navigation Symposium Record. IEEE. https://doi.org/10.1109/plans.1992.185863
• Snyder, Scott, Brian Schipper, Larry Vallot, Nigel Parker, and Cary Spitzer. 1992. “Differential GPS/inertial Navigation Approach/landing Flight Test Results.” IEEE Aerospace and Electronic Systems Magazine 7 (5, Ma). https://ntrs.nasa.gov/citations/19920068385
• Snyder, S., L. Vallot, B. Schipper, N. Parker, and C. Spitzer. n.d.-b. “Differential GPS/inertial Navigation Terminal Area Guidance Flight Test Results.” In NTC ‘91 - National Telesystems Conference Proceedings. IEEE. https://doi.org/10.1109/ntc.1991.148020
• Sohrabi, Ali, and Sadra Rafatnia. 2024. “Optimizing the Integration of Inertial Navigation Systems and Air Data for Enhanced Vertical Channel Stability in Autonomous Ground Vehicles.” In 2024 12th RSI International Conference on Robotics and Mechatronics (ICRoM). IEEE. https://doi.org/10.1109/icrom64545.2024.10903607
• Sokolov, Sergey, Andrey Sukhanov, and Marianna Polyakova. 2022. “High-Precision Navigation on Analytical Trajectories Using Strapdown Inertial-Satellite Navigation System.” In 2022 International Russian Automation Conference (RusAutoCon). IEEE. https://doi.org/10.1109/rusautocon54946.2022.9896308
• Soloviev, Andrey. 2008. “Tight Coupling of GPS, Laser Scanner, and Inertial Measurements for Navigation in Urban Environments.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570059
• Soltani, Mohammad Reza, and Mohammad Farahani. 2012. “Effects of Angle of Attack on Inlet Buzz.” Journal of Propulsion and Power 28 (4): 747–57. https://doi.org/10.2514/1.b34209
• Somieski, Gerhard. 1997. “Shimmy Analysis of a Simple Aircraft Nose Landing Gear Model Using Different Mathematical Methods.” Aerospace Science and Technology 1 (8): 545–55. https://doi.org/10.1016/s1270-9638(97)90003-1
• Somov, Yevgeny, Sergey Buryrin, and Sergey Somov. 2011. “Methods for Stellar-Inertial Navigation and Gyromoment Guidance of the Agile Land-Survey Satellites.” In Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011. IEEE. https://doi.org/10.1109/rast.2011.5966975
• Sonawane, Hemant R., and Shripad P. Mahulikar. 2013. “Effect of Missile Turn Rate on Aircraft Susceptibility to Infrared-Guided Missile.” Journal of Aircraft 50 (2): 663–67. https://doi.org/10.2514/1.c031902
• Song, Rui, and Xiyuan Chen. 2017. “Error Estimation of Airborne Strapdown Inertial Navigation System Based on Neural Network.” In 2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace). IEEE. https://doi.org/10.1109/metroaerospace.2017.7999564
• Song, Zhi-Guang, and Feng-Ming Li. 2014. “Aerothermoelastic Analysis of Nonlinear Composite Laminated Panel with Aerodynamic Heating in Hypersonic Flow.” Composites Part B: Engineering 56: 830–39. https://doi.org/10.1016/j.compositesb.2013.09.019
• Song, Zhi-Guang, and Feng-Ming Li. 2015. “Aerothermoelastic Analysis of Lattice Sandwich Composite Panels in Supersonic Airflow.” Meccanica 51 (4): 877–91. https://doi.org/10.1007/s11012-015-0240-y
• Song, Tianxiao, Kui Li, Lei Wang, Jie Sui, and Lingcao Wang. 2017b. “A Rapid and High-Precision Initial Alignment Scheme for Dual-Axis Rotational Inertial Navigation System.” Microsystem Technologies 23 (12): 5515–25. https://doi.org/10.1007/s00542-017-3286-z
• Song, Jia, Yuxie Luo, Mingfei Zhao, Yunlong Hu, and Yanxue Zhang. 2022. “Fault-Tolerant Integrated Guidance and Control Design for Hypersonic Vehicle Based on PPO.” Mathematics 10 (18): 3401. https://doi.org/10.3390/math10183401
• Song, Ningfang, Pan Ma, Jing Jin, and Jingming Song. 2012. “Reduced Phase Error of a Fiber Optic Gyroscope Using a Polarization Maintaining Photonic Crystal Fiber.” Optical Fiber Technology 18 (4): 186–89. https://doi.org/10.1016/j.yofte.2012.04.002
• Song, Jianshuang, Xun Song, and Zhang Ren. 2011. “New Robust Disturbance Rejection Control Method for Reusable Launch Vehicle.” In 2011 International Conference on Electrical and Control Engineering. IEEE. https://doi.org/10.1109/iceceng.2011.6057472
• Song, Xun, Jianshuang Song, and Zhang Ren. 2013. “Robust LPV Missile Autopilot Design with Parameter Dependent Performance.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561262
• Song, Ningfang, Zhengguo Yuan, and Xiong Pan. 2019. “Adaptive Kalman Filter Based on Random-Weighting Estimation for Denoising the Fiber-Optic Gyroscope Drift Signal.” Applied Optics 58 (35): 9505. https://doi.org/10.1364/ao.58.009505
• Song, Yuning, Weizhong Zhang, and Yan Ding. 2023. “An Automatic Landing Control Approach for Naval Aircraft via Backstepping Sliding Mode Trajectory Angle Control.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10239989
• Song, Mingliang, Bin Zhou, Tian Zhang, Bo Hou, and Rong Zhang. 2017a. “Parametric Drive of a Micro Rate Integrating Gyroscope Using Discrete Electrodes.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935680
• Sonmez, Tolga, and Haluk Erdem Bingol. 2008. “Modeling and Simulation of a Terrain Aided Inertial Navigation Algorithm for Land Vehicles.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570078
• Sonmezoglu, S., S. E. Alper, and T. Akin. 2012. “An Automatically Mode-Matched MEMS Gyroscope with 50 Hz Bandwidth.” In 2012 IEEE 25th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2012.6170231
• Sonmezoglu, S., S. E. Alper, and T. Akin. 2013. “A High Performance Automatic Mode-Matched MEMS Gyroscope with an Improved Thermal Stability of the Scale Factor.” In 2013 Transducers & Eurosensors XXVII: The 17th International Conference on Solid-State Sensors, Actuators and Microsystems (TRANSDUCERS & EUROSENSORS XXVII). IEEE. https://doi.org/10.1109/transducers.2013.6627318
• Sonmezoglu, S., H. D. Gavcar, K. Azgin, S. E. Alper, and T. Akin. 2014. “Simultaneous Detection of Linear and Coriolis Accelerations on a Mode-Matched MEMS Gyroscope.” In 2014 IEEE 27th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/memsys.2014.6765566
• Soon, B. K. H., and S. Scheding. 2006. “Sensitivity Analysis of an Integrated Vision and Inertial System.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650666
• Sotomayer, W. A., and T. M. Weeks. 1978. “Aerodynamic Analysis of Supersonic Aircraft with Subsonic Leading Edges.” Journal of Aircraft 15 (7): 399–406. https://doi.org/10.2514/3.58378
• Soumekh, M. 1996. “Automatic Aircraft Landing Using Interferometric Inverse Synthetic Aperture Radar Imaging.” IEEE Transactions on Image Processing 5 (9): 1335–45. https://doi.org/10.1109/83.535845
• Sözer, Onuralp, and Tufan Kumbasar. 2023. “Quality-Aware Autonomous Navigation with Dynamic Path Cost for Vision-Based Mapping toward Drone Landing.” Drones 7 (4): 278. https://doi.org/10.3390/drones7040278
• Spottswood, S. Michael, Benjamin P. Smarslok, Ricardo A. Perez, et al. 2021. “Supersonic Aerothermoelastic Experiments of Aerospace Structures.” AIAA Journal 59 (12): 5029–48. https://doi.org/10.2514/1.j060403
• “Sprint Missile Subsystem Reliability Achievements.” 1977. Microelectronics Reliability 16 (6): 650. https://doi.org/10.1016/0026-2714(77)90526-1
• Sreenuch, T., A. Tsourdos, E. J. Hughes, and B. A. White. 2005. “Fuzzy Gain-Scheduled Missile Autopilot Design Using Evolutionary Algorithms.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1469957
• Srikant, S., J. L. Wagner, A. Valdivia, M. R. Akella, and N. Clemens. 2010. “Unstart Detection in a Simplified-Geometry Hypersonic Inlet-Isolator Flow.” Journal of Propulsion and Power 26 (5): 1059–71. https://doi.org/10.2514/1.46937
• St-Pierre, M., and D. Gingras. 2004. “Comparison between the Unscented Kalman Filter and the Extended Kalman Filter for the Position Estimation Module of an Integrated Navigation Information System.” In IEEE Intelligent Vehicles Symposium, 2004. IEEE. https://doi.org/10.1109/ivs.2004.1336492
• Stachiw, Terrin, Fidel Khouli, Robert G. Langlois, and Fred F. Afagh. 2021. “Landing Gear Mechanical Network Synthesis for Improving Comfort at Landing Considering Aircraft Flexibility.” Journal of Aircraft 58 (6): 1242–53. https://doi.org/10.2514/1.c035921
• Staley, R. M. 1963. “Performance Analysis of an Optical-Inertial Midcourse Guidance System on a Circumlunar Mission.” IEEE Transactions on Military Electronics MIL-7 (1): 70–79. https://doi.org/10.1109/tme.1963.4323044
• Staley, R. M., and P. C. Yue. 1970. “On System Parameter Identifiability.” Information Sciences 2 (2): 127–38. https://doi.org/10.1016/s0020-0255(70)80046-9
• Stamenkovich, M., and J. Carvil. 2000. “Application of the Digital Nautical Chart (DNC) Database to Help Identify Areas of Vertical Deflection in the Ring Laser Gyro Inertial Navigator (AN/WSN-7).” In IEEE 2000. Position Location and Navigation Symposium (Cat. No.00CH37062). IEEE. https://doi.org/10.1109/plans.2000.838317
• Stanov, Stepan D. 2026. “Inertial Navigation System Based on Multidimensional Kalman Filter.” In 2026 ElCon Conference of Young Researchers in Electrical Engineering, Automation & Control Systems (ElCon-EE). IEEE. https://doi.org/10.1109/elcon-ee69794.2026.11453007
• Stark, Valter J. E. 1989. “Canard-Wing Interaction in Unsteady Supersonic Flow.” Journal of Aircraft 26 (10): 951–52. https://doi.org/10.2514/3.45867
• Stebler, Yannick, Stephane Guerrier, Jan Skaloud, and Maria-Pia Victoria-Feser. 2012. “A Framework for Inertial Sensor Calibration Using Complex Stochastic Error Models.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236827
• Stepanov, Oleg, and Andrei Motorin. 2019. “Performance Criteria for the Identification of Inertial Sensor Error Models.” Sensors 19 (9): 1997. https://doi.org/10.3390/s19091997
• Stepanov, O. A., A. S. Nosov, and A. B. Toropov. 2017. “Navigation Informativity of Geophysical Fields in Map-Aided Navigation.” In 2017 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2017.8171509
• Sternberg, Joseph. 1952. “A Free-Flight Investigation of the Possibility of High Reynolds Number Supersonic Laminar Boundary Layers.” Journal of the Aeronautical Sciences 19 (11): 721–33. https://doi.org/10.2514/8.2456
• Sternberg, David, Kevin Lo, and John Baker. 2022. “Night Sky Testing of the Lunar Flashlight Star Tracker.” In 2022 IEEE Aerospace Conference (AERO). IEEE. https://doi.org/10.1109/aero53065.2022.9843416
• Stewart, Chris, Mina Shokr, Gokhan Ibal, and Terry Caelli. 2016. “Circular Error Probables for Moving Targets: The Dynamic Error Probable.” Journal of Guidance, Control, and Dynamics 39 (7): 1690–93. https://doi.org/10.2514/1.g001706
• Stigter, J. D., D. Vries, and K. J. Keesman. 2003. “On Adaptive Optimal Input Design.” In 2003 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2003.7084986
• Stilwell, Daniel J. 2001. “State-Space Interpolation for a Gain-Scheduled Autopilot.” Journal of Guidance, Control, and Dynamics 24 (3): 460–65. https://doi.org/10.2514/2.4766
• Stimac, L., D. Bina, J. Page, F. Schermers, and D. Sugarbaker. 1994. “A Tactical Grade Depolarized Fiber Optic Gyroscope.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303313
• Stimac, L. W., and T. A. Kennedy. n.d. “Sensor Alignment Kalman Filters for Inertial Stabilization Systems.” In IEEE PLANS 92 Position Location and Navigation Symposium Record. IEEE. https://doi.org/10.1109/plans.1992.185861
• Stojanovic, Vladimir, and Novak Nedic. 2016. “Robust Identification of OE Model with Constrained Output Using Optimal Input Design.” Journal of the Franklin Institute 353 (2): 576–93. https://doi.org/10.1016/j.jfranklin.2015.12.007
• Stoller, David S. 1961. “Measuring Missile Reliability in Prelaunch Environments.” IRE Transactions on Reliability and Quality Control RQC-10 (1): 19–25. https://doi.org/10.1109/ire-pgrqc.1961.5007250
• Stovner, Bard N., and Tor A. Johansen. 2019. “GNSS-Antenna Lever Arm Compensation in Aided Inertial Navigation of UAVs.” In 2019 18th European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2019.8795760
• Strachan, R. L., and J. M. Evans. n.d. “Testing of the High Accuracy Inertial Navigation System in the Shuttle Avionics Integration Laboratory.” In IEEE PLANS 92 Position Location and Navigation Symposium Record. IEEE. https://doi.org/10.1109/plans.1992.185820
• Su, T.-H., S. Nitzan, P. Taheri-Tehrani, M. Kline, B. Boser, and D. A. Horsley. 2013a. “MEMS Disk Resonator Gyroscope with Integrated Analog Front-End.” In 2013 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2013.6688164
• Su, Zikang, and Honglun Wang. 2015. “A Novel Robust Hybrid Gravitational Search Algorithm for Reusable Launch Vehicle Approach and Landing Trajectory Optimization.” Neurocomputing 162: 116–27. https://doi.org/10.1016/j.neucom.2015.03.063
• Subrahmanyam, M. B. 1994. “H-Infinity Design of F/A-18A Automatic Carrier Landing System.” Journal of Guidance, Control, and Dynamics 17 (1): 187–91. https://doi.org/10.2514/3.21177
• “A Successful Program for Missile Reliability.” 1992. Microelectronics Reliability 32 (4): 588. https://doi.org/10.1016/0026-2714(92)90532-p
• Sufleta, Z. 1982. “Identifiability of Time-Varying Parameters in a Class of Linear Dynamical Systems.” IEEE Transactions on Automatic Control 27 (5): 1114–16. https://doi.org/10.1109/tac.1982.1103072
• Sugisaka, M., and S. Sagara. 1979. “Imbedding Approach for Optimal Input Design of Linear System Identification.” IFAC Proceedings Volumes 12 (8): 611–18. https://doi.org/10.1016/s1474-6670(17)65471-5
• Suh, Young Soo. 2009. “Inertial and Magnetic Sensor Data Compression Considering the Estimation Error.” Sensors 9 (8): 5919–32. https://doi.org/10.3390/s90805919
• Sui, Qi SHeng, Xin Li, and Yong Hua Fan. 2008. “Design of Autopilot for Aerodynamic/Reaction-Jet Multiple Control Missile.” In 2008 International Conference on Intelligent Computation Technology and Automation (ICICTA). IEEE. https://doi.org/10.1109/icicta.2008.101
• Sun, Qiming. 2026. “Multi-Agent Reinforcement Learning for Cooperative Trajectory Planning of Hypersonic Glide Vehicles in Dynamic Restricted Airspace.” In 2026 Technology and Innovation Conference (TIC). IEEE. https://doi.org/10.1109/tic68483.2026.11702886
• Sun, Xiaojian, Jianquan Ge, Tao Yang, Qiangqiang Xu, and Bin Zhang. 2019a. “Multifidelity Multidisciplinary Design Optimization of Integral Solid Propellant Ramjet Supersonic Cruise Vehicles.” International Journal of Aerospace Engineering 2019: 1–18. https://doi.org/10.1155/2019/5192424
• Sun, Jiarui, Chuanjiang Li, Guangtao Ran, Rong Su, and Yanning Guo. 2026c. “Two-Stage Cooperative Trajectory Planning for Hypersonic Glide Vehicles: A Bio-Inspired Optimization Approach.” Aerospace Science and Technology 174: 111909. https://doi.org/10.1016/j.ast.2026.111909
• Sun, Jiarui, Chuanjiang Li, Guangtao Ran, Bohui Wang, and Yanning Guo. 2026b. “Online Trajectory Planning for Hypersonic Glide Vehicle under Multiple No-Fly Zones: An Attention Mechanism-Based BiGRU Framework.” IEEE Transactions on Aerospace and Electronic Systems 62: 10020–32. https://doi.org/10.1109/taes.2026.3687820
• Sun, Liguo, Shidan Li, Desheng Wang, and Xiaolin Zhao. 2009b. “Measuring Terrain Information Using Multifractal and Wavelets in Terrain Navigation.” In 2009 2nd International Congress on Image and Signal Processing. IEEE. https://doi.org/10.1109/cisp.2009.5304758
• Sun, Ping, and Kun Liu. 2009. “Missile Autopilot Design Based on State Dependent Riccati Equation.” In 2009 International Asia Conference on Informatics in Control, Automation and Robotics. IEEE. https://doi.org/10.1109/car.2009.20
• Sun, Yu, Xiaojie Liu, Xiaochen Liu, et al. 2025c. “Variational Bayesian Innovation Saturation Kalman Filter for Micro-Electro-Mechanical System–Inertial Navigation System/Polarization Compass Integrated Navigation.” Micromachines 16 (9): 1036. https://doi.org/10.3390/mi16091036
• Sun, Weibo, Ping Ma, Songyan Wang, and Tao Chao. 2024a. “Analytical Solutions for Hypersonic Glide Trajectory Based on Altitude–Velocity Profile.” IEEE Transactions on Aerospace and Electronic Systems 60 (5): 7423–36. https://doi.org/10.1109/taes.2024.3417425
• Sun, Jiarui, Guangtao Ran, Chuanjiang Li, Yanning Guo, and Ju H. Park. 2025b. “Discontinuous Trajectory Tracking of Hypersonic Glide Reentry Vehicle: An Intention Inference Approach.” IEEE Sensors Journal 25 (19): 36594–36606. https://doi.org/10.1109/jsen.2025.3598737
• Sun, Shoucai, Chunlei Song, Junhou Wang, Xingtai Yao, and Ling Xie. 2010. “Central Difference Gaussian Particle Filter for Initial Alignment of Strapdown Inertial Navigation System.” In 2010 International Conference on Intelligent Control and Information Processing. IEEE. https://doi.org/10.1109/icicip.2010.5564317
• Sun, Feng, Tong Cao, Bo Xu, Yueyang Ben, and Yudan Wang. 2009a. “Initial Alignment for Strapdown Inertial Navigation System Based on Inertial Frame.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246606
• Sun, Feng, and Qiuying Wang. 2012. “Researching on the Compensation Technology of Rotating Mechanism Error in Single-Axis Rotation Strapdown Inertial Navigation System.” In 2012 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2012.6285089
• Sun, Zonghua, Liaoni Wu, and Yancheng You. 2023. “Robust Gain-Scheduled Missile Autopilot Design Based on Multifrequency Extended State Observers.” Chinese Journal of Aeronautics 36 (12): 390–407. https://doi.org/10.1016/j.cja.2023.07.028
• Sun, Feng, Jianzhong Xia, Haiyu Lan, and Xintao Liu. 2012. “Research on Integrated Alignment of Rotary Strapdown Inertial Navigation System.” In 2012 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2012.6283232
• Sun, Jin, Xiao-Su Xu, Yi-Ting Liu, Tao Zhang, and Yao Li. 2015. “Initial Alignment of Large Azimuth Misalignment Angles in SINS Based on Adaptive UPF.” Sensors 15 (9): 21807–23. https://doi.org/10.3390/s150921807
• Sun, Silu, Kaikai Yu, and Jinglei Xu. 2026d. “The Unstart and Restart Dynamic Processes of an Inlet Caused by Instantaneous Velocity Change.” Aerospace Science and Technology 177: 112248. https://doi.org/10.1016/j.ast.2026.112248
• Sun, Xiaoliang, Zhuo Zhang, Jun Liu, Qiufu Wang, and Jiexin Zhou. 2022. “Visual Pose Measurement for Automatic Landing on an Aircraft Carrier.” In 2022 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus55513.2022.9986607
• Sun, Qian, Ya Zhang, Jianguo Wang, and Wei Gao. 2017. “An Improved FAST Feature Extraction Based on RANSAC Method of vision/SINS Integrated Navigation System in GNSS-Denied Environments.” Advances in Space Research 60 (12): 2660–71. https://doi.org/10.1016/j.asr.2017.05.017
• Sung, Bu-Kyeng, Min-Seon Jo, Jeong-Yeol Choi, Umesh Unnikrishnan, and Vigor Yang. 2026. “Supersonic Combustion and Flow Evolution in Dual-Combustion Ramjet Engine.” Journal of Propulsion and Power 42 (2): 363–77. https://doi.org/10.2514/1.b40184
• Suozhong Yuan and Yidong Yang. n.d. “Design of Automatic Carrier Landing System Using H/sub ∞/ Control.” In Proceedings of the 3rd World Congress on Intelligent Control and Automation (Cat. No.00EX393), vol. 5. IEEE. https://doi.org/10.1109/wcica.2000.863180
• Sura, Niranjan K., and S. Suryanarayan. 2009. “Lateral Stability of Aircraft Nose-Wheel Landing Gear with Closed-Loop Shimmy Damper.” Journal of Aircraft 46 (2): 505–9. https://doi.org/10.2514/1.37626
• Surber, Lewis E., and Dennis Sedlock. 1979. “Effects of Airframe-Inlet Integration on Half -Axisymmetric and Two-Dimensional Supersonic Inlet Performance.” Journal of Aircraft 16 (9): 612–19. https://doi.org/10.2514/3.58575
• Suryanarayana, G. K., D. B. Singh, Sumukh Surya, and G. Jagadeesh. 2022. “Nonlinear Damping Model for Supersonic Air-Intake Buzz.” Aerospace Science and Technology 126: 107567. https://doi.org/10.1016/j.ast.2022.107567
• Sushchenko, Olha. 2026. “Research on the Gimballed Inertial Navigation System Based on Mathematical Description of Platform Motion.” In Computational Science and Its Applications – ICCSA 2026 Workshops. Springer Nature Switzerland. https://doi.org/10.1007/978-3-032-30521-3_3
• Sushchenko, Olha, Yurii Bezkorovainyi, Oleksandr Solomentsev, et al. 2024. “Algorithm of Determining Errors of Gimballed Inertial Navigation System.” In Computational Science and Its Applications – ICCSA 2024 Workshops. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-65223-3_14
• Sushchenko, Olha, and Yurii Melnyk. 2026. “Modelling of Multimode Inertial Navigation System with Stabilized Platform.” In 2026 16th International Conference on Advanced Computer Information Technologies (ACIT). IEEE. https://doi.org/10.1109/acit69831.2026.11700080
• Sussman, Mark B. 1968. “A Remark Concerning Engine-Inlet Distortion.” Journal of Aircraft 5 (1): 95–96. https://doi.org/10.2514/3.43914
• Suthakar, Vithurshan, Perushan Kunalakantha, Regina S. K. Lee, and Gunho Sohn. 2026. “An on-Orbit Star Tracker Benchmark for Resident Space Object Detection and Attitude Estimation.” Scientific Data. https://doi.org/10.1038/s41597-026-07736-9
• Suzuki, Hiromi, and Toshiharu Sugie. 2007. “On Input Design for System Identification in Time Domain.” In 2007 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2007.7068340
• Suzuki, Hiroshi, and Masaki Yamakita. 2011. “Input Design for Hybrid System Identification for Accurate Estimation of Submodel Regions.” In Proceedings of the 2011 American Control Conference. IEEE. https://doi.org/10.1109/acc.2011.5990780
• Sviestins, E. n.d. “True Multi-Radar Tracking for Air Defence C/sup 3/ Systems.” In IEEE International Conference on Radar. IEEE. https://doi.org/10.1109/radar.1990.201097
• Swaszek, Peter F., Richard J. Hartnett, and Kelly C. Seals. 2020. “Celestial Navigation: Correcting the Folklore.” In 2020 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans46316.2020.9109928
• Sweat, Tyler, Willie K. Harrison, Michael Rice, and Randal W. Beard. 2025. “Low-SWaP GNSS-Denied Navigation Using LTE Signals of Opportunity.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028479
• Syed, Z. F., P. Aggarwal, Xiaoji Niu, and N. El-Sheimy. 2008. “Civilian Vehicle Navigation: Required Alignment of the Inertial Sensors for Acceptable Navigation Accuracies.” IEEE Transactions on Vehicular Technology 57 (6): 3402–12. https://doi.org/10.1109/tvt.2008.921616
• Szabo, Bela. 1962. “Comparison of the Deflection of the Vertical Components Computed by Astro-Geodetic, Gravimetric and Topographic-Isostatic Techniques.” Bulletin géodésique 65 (1): 227–42. https://doi.org/10.1007/bf02529720
• “T03 — Radar Tracking.” 2014. In 2014 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2014.6875529
• Tabatabaei, Sajad, Shahab-o-din Tohidi, Mokhtar Sha Sadeghi, and Parinaz Sadat Mirjafari. 2010. “Fuzzy Self-Tuning Gain Scheduled Control Design for an Autopilot Missile.” In 2010 International Conference on Computer Applications and Industrial Electronics. IEEE. https://doi.org/10.1109/iccaie.2010.5735074
• Tadic, Srdjan, and Milan B. Vukajlovic. 2013. “Coarse Azimuth Alignment of Inertial Measurement Unit for Use in Telematics.” In 2013 21st Telecommunications Forum Telfor (TELFOR). IEEE. https://doi.org/10.1109/telfor.2013.6716292
• Taghi-Abad, Sohrab Panahandeh, Mohammad Hossein Moghimi Esfand-Abadi, and Javad Sepahi-Younsi. 2026. “Delaying the Buzz Onset in a Supersonic Inlet by Multi-Row Disk Concept.” Aerospace Science and Technology 168: 110963. https://doi.org/10.1016/j.ast.2025.110963
• Tahk, M., M. M. Briggs, and P. K. A. Menon. n.d. “Applications of Plant Inversion via State Feedback to Missile Autopilot Design.” In Proceedings of the 27th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1988.194405
• Tai, Shang, Lixin Wang, Yanling Wang, Chen Bu, and Ting Yue. 2023. “Flight Dynamics Modeling and Aerodynamic Parameter Identification of Four-Degree-of-Freedom Virtual Flight Test.” AIAA Journal 61 (6): 2652–65. https://doi.org/10.2514/1.j062188
• Taibi, Rachid, Olivier Jolly, Thomas Kerrien, et al. 2021. “SWaP Reduction for High Dynamic Navigation Grade Accelerometer Based on Quartz VBA Technology.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430477
• Takahashi, Ayumu, Shuya Okayama, Amit Banerjee, Jun Hirotani, and Toshiyuki Tsuchiya. 2024. “Theoretical Analysis of (100) Silicon Ring Gyroscope with Chamfered Rectangle Springs.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502107
• Takahashi, Ayumu, Masaki Shimofuri, Amit Banerjee, Jun Hirotani, and Toshiyuki Tsuchiya. 2025. “(100) Silicon Ring Gyroscope with Rectangle Spring Aiming at Frequency and Thermoelastic Q-Factor Matching.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037046
• Takahashi, M., S. Tai, and K. Kyuma. 1990. “Effect of Reflections on the Drift Characteristics of a Fiber-Optic Passive Ring-Resonator Gyroscope.” Journal of Lightwave Technology 8 (5): 811–16. https://doi.org/10.1109/50.54492
• Takehira, Tetsuya, Nguyen X. Vinh, and Pierre T. Kabamba. 1998. “Analytical Solution of Missile Terminal Guidance.” Journal of Guidance, Control, and Dynamics 21 (2): 342–48. https://doi.org/10.2514/2.4241
• Tan, Hui-jun, Liu-gang Li, Yu-fen Wen, and Qi-fan Zhang. 2011. “Experimental Investigation of the Unstart Process of a Generic Hypersonic Inlet.” AIAA Journal 49 (2): 279–88. https://doi.org/10.2514/1.j050200
• Tan, Tian, Ao Peng, Junjun Huang, Lingxiang Zheng, and Gang Ou. 2018. “A Gyroscope Bias Estimation Algorithm Based on Map Specific Information.” Sensors 18 (8): 2534. https://doi.org/10.3390/s18082534
• Tan, Wenbo, Yan Wang, and Xinwang Wang. 2026. “A Novelty Temperature Compensation Model for Dual-Mass Vibration MEMS Gyroscope Based on Machine Learning and TTAO-VMD Algorithm.” Micromachines 17 (1): 120. https://doi.org/10.3390/mi17010120
• Tanenhaus, Martin, Tim Geis, Dean Carhoun, and Alex Holland. 2010. “Accurate Real Time Inertial Navigation Device by Application and Processing of Arrays of MEMS Inertial Sensors.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507137
• Tang, Jian, Yuwei Chen, Xiaoji Niu, et al. 2015a. “LiDAR Scan Matching Aided Inertial Navigation System in GNSS-Denied Environments.” Sensors 15 (7): 16710–28. https://doi.org/10.3390/s150716710
• Tang, Xiao, Bing Xiong, Xiaoqiang Fan, Junbing Liu, and Jian Zhao. 2024a. “Experimental Research on the Flow Mechanism of Dual-Separation Unstart Phenomenon in Hypersonic Inlet.” Aerospace Science and Technology 150: 109189. https://doi.org/10.1016/j.ast.2024.109189
• Tang, Xiao, Bing Xiong, Xiaoqiang Fan, and Liang Wang. 2023. “Self-Start Characteristics of Hypersonic Inlet When Multiple Unstart Modes Exist.” Applied Sciences 13 (17): 9752. https://doi.org/10.3390/app13179752
• Tang, Xingyuan, Libin Zeng, Kaixin Deng, et al. 2024b. “A Rate Hemispherical Resonator Gyroscope with Bias Stability of 0.0056°/h with Compensation of Phase Delay.” Sensors and Actuators A: Physical 375: 115494. https://doi.org/10.1016/j.sna.2024.115494
• Tanno, Marie, and Hideyuki Tanno. 2021. “Aerodynamic Characteristics of a Free-Flight Scramjet Vehicle in Shock Tunnel.” Experiments in Fluids 62 (7): 150. https://doi.org/10.1007/s00348-021-03229-0
• Tanıl, Çağatay, Samer Khanafseh, and Boris Pervan. 2017. “Detecting Global Navigation Satellite System Spoofing Using Inertial Sensing of Aircraft Disturbance.” Journal of Guidance, Control, and Dynamics 40 (8): 2006–16. https://doi.org/10.2514/1.g002547
• Tao, Cui, Yu Daren, Chang Juntao, and Bao Wen. 2008. “Topological Geometry Interpretation of Supersonic Inlet Start/Unstart Based on Catastrophe Theory.” Journal of Aircraft 45 (4): 1464–68. https://doi.org/10.2514/1.34125
• Tao, Cui, Yu Daren, Chang Juntao, and Bao Wen. 2009. “Catastrophe Model for Supersonic Inlet Start/Unstart.” Journal of Aircraft 46 (4): 1160–66. https://doi.org/10.2514/1.38926
• Tao, Yongkang, Yunfeng Liu, and Jingxin Dong. 2014. “Recovery Procedure and Bias Shift Analysis of MEMS High Overload Accelerometer Due to Shock.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007430
• Tao, Zhou, Tan Zhouwen, Wang Weixiang, Wu Xiaolong, and Liu Yiming. 2025. “Inertial Navigation System Based on Six-Axis Gyroscope and Encode.” In 2025 10th International Conference on Information and Network Technologies (ICINT). IEEE. https://doi.org/10.1109/icint65528.2025.11030877
• Tariq, Ikrama, Muhammad Wasim, and Muhammad Umer Sohail. 2026. “Design of a Gain-Scheduled LQR Controller for Landing of a Reusable Launch Vehicle.” Processes 14 (15): 2458. https://doi.org/10.3390/pr14152458
• Tashtay, Yerlan, Nurzhigit Smailov, Kalmukhamed Tazhen, Akezhan Sabibolda, Aruzhan Nazarova, and Aidana Bazarbay. 2025. “Integration of GNSS and Fiber-Optic Gyroscope: Improving Navigation Robustness under Satellite Signal Loss.” In 2025 International Conference on Electrical Engineering and Photonics (EExPolytech). IEEE. https://doi.org/10.1109/eexpolytech66949.2025.11253802
• Tatar, Erdinc, Tamal Mukherjee, and Gary K. Fedder. 2014. “Simulation of Stress Effects on Mode-Matched MEMS Gyroscope Bias and Scale Factor.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851352
• Tatar, Erdinc, Tamal Mukherjee, and Gary K. Fedder. 2017. “Stress Effects and Compensation of Bias Drift in a MEMS Vibratory-Rate Gyroscope.” Journal of Microelectromechanical Systems 26 (3): 569–79. https://doi.org/10.1109/jmems.2017.2675452
• Tatry, Ph., F. Deneu, and J. L. Simonotti. 1997. “RAMS Approach for Reusable Launch Vehicle Advanced Studies.” Acta Astronautica 41 (11): 791–97. https://doi.org/10.1016/s0094-5765(97)00194-x
• Tavares, Adalberto J. A., Jr., and Neusa M. F. Oliveira. 2024. “A Novel Approach for Kalman Filter Tuning for Direct and Indirect Inertial Navigation System/Global Navigation Satellite System Integration.” Sensors 24 (22): 7331. https://doi.org/10.3390/s24227331
• Taylor, Clark N. 2012a. “An Analysis of Observability-Constrained Kalman Filtering for Vision-Aided Navigation.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236980
• Tazartes, Daniel. 2014. “An Historical Perspective on Inertial Navigation Systems.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782505
• Te-Chang Li. 2004. “Analysis of Inertial Navigation System Errors from Van Testing Using an Optimal Kalman Filter/smoother.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308983
• Teague, Samuel, and Javaan Chahl. 2023. “Strapdown Celestial Attitude Estimation from Long Exposure Images for UAV Navigation.” Drones 7 (1): 52. https://doi.org/10.3390/drones7010052
• Teague, Samuel, and Javaan Chahl. 2024. “An Algorithm for Affordable Vision-Based GNSS-Denied Strapdown Celestial Navigation.” Drones 8 (11): 652. https://doi.org/10.3390/drones8110652
• “Telemetry Standards for Guided Missiles.” 1957. IRE Transactions on Telemetry and Remote Control TRC-3 (3): 13–18. https://doi.org/10.1109/irettrc.1957.6538856
• Telny, A. V. 2021. “On the Estimation of the Measurement Accuracy of Satellite Navigation Systems Using Dynamic Recursive Correction.” In 2021 28th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43216.2021.9470807
• Templeman, J. E., and R. H. Parker. 1968. “Boeing/Sperry Automatic Landing System 727 Airplane.” Journal of Aircraft 5 (3): 285–91. https://doi.org/10.2514/3.43940
• Teng, Fei, Jing Jin, Yunlong Huang, Zuchen Zhang, and Chunxi Zhang. 2015b. “Noise Analysis and Measurement of High Sensitivity Photonic Crystal Fiber-Optic Gyroscope.” Optical Fiber Technology 25: 1–6. https://doi.org/10.1016/j.yofte.2015.06.002
• Tennstedt, Benjamin, and Steffen Schön. 2025. “Assessment of IMU Quality Requirements in Integrated Quantum Inertial Navigation Systems.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037122
• Tereshkov, Vasiliy M. 2013. “An Intuitive Approach to Inertial Sensor Bias Estimation.” International Journal of Navigation and Observation 2013: 1–6. https://doi.org/10.1155/2013/762758
• “Terrain Navigation Using Bayesian Statistics.” 1999. IEEE Control Systems 19 (3): 33–40. https://doi.org/10.1109/37.768538
• Thai, Sovanna, Spilios Theodoulis, Clément Roos, and Jean-Marc Biannic. 2023. “Robust Gain-Scheduled Autopilot Design with Anti-Windup Compensation for a Guided Projectile.” CEAS Aeronautical Journal 14 (3): 765–86. https://doi.org/10.1007/s13272-023-00668-9
• Thai, Sovanna, Spilios Theodoulis, Clement Roos, Jean-Marc Biannic, and Michael Proff. 2020. “Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile.” In 2020 IEEE Conference on Control Technology and Applications (CCTA). IEEE. https://doi.org/10.1109/ccta41146.2020.9206311
• Thakur, Saumya Basu, Siddhartha Mukhopadhyay, and Shraboni Ghosh. 2019. “Development of a Decision Algorithm for Range Safety during Missile Flight Test.” In 2019 International Conference on Range Technology (ICORT). IEEE. https://doi.org/10.1109/icort46471.2019.9069664
• Thawait, Amit K., Parag Tandaiya, Prakash C. Jain, and Abhilash J. Chandy. 2023b. “Numerical Investigation of Aerothermoelastic Characteristics of a Thin Heated Panel in High Supersonic and Hypersonic Flow.” Acta Mechanica 234 (5): 2269–91. https://doi.org/10.1007/s00707-023-03495-5
• Thawait, Amit K., Parag Tandaiya, Prakash C. Jain, and Abhilash J. Chandy. 2024b. “Nonlinear Aerothermoelastic Analysis of Deployable Control Fin with Actuator Stiffness Subjected to High-Speed Compressible Flows.” Acta Mechanica 235 (12): 7661–86. https://doi.org/10.1007/s00707-024-04118-3
• Theodoulis, Spilios, and Gilles Duc. 2007a. “Gain-Scheduling Techniques for Missile Autopilot Synthesis.” In 2007 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2007.7068374
• Theodoulis, Spilios, and Gilles Duc. 2007b. “Missile Autopilot Design Using Observer-Based Gain Scheduling.” IFAC Proceedings Volumes 40 (7): 798–803. https://doi.org/10.3182/20070625-5-fr-2916.00136
• Theodoulis, Spilios, and Gilles Duc. 2009. “Missile Autopilot Design: Gain-Scheduling and the Gap Metric.” Journal of Guidance, Control, and Dynamics 32 (3): 986–96. https://doi.org/10.2514/1.34756
• Theodoulis, Spilios, Florian Sève, and Philippe Wernert. 2015. “Robust Gain-Scheduled Autopilot Design for Spin-Stabilized Projectiles with a Course-Correction Fuze.” Aerospace Science and Technology 42: 477–89. https://doi.org/10.1016/j.ast.2014.12.027
• Theunissen, D. J., and R. Owen Holbrook. 1998. “Effects of Environment and Aging upon Missile Reliability.” In Annual Reliability and Maintainability Symposium. 1998 Proceedings. International Symposium on Product Quality and Integrity. IEEE. https://doi.org/10.1109/rams.1998.653798
• “A Thick Film Guidance Unit for the Rapier Missile.” 1974. Microelectronics Reliability 13 (3): 166. https://doi.org/10.1016/0026-2714(74)90269-8
• Thies, Christoph. 2022. “Investigation of the Landing Dynamics of a Reusable Launch Vehicle and Derivation of Dimension Loading for the Landing Leg.” CEAS Space Journal 14 (3): 565–76. https://doi.org/10.1007/s12567-022-00456-x
• Thillai, Nishanth, Amit Thakur, K. Srikrishnateja, and J. Dharani. 2021. “Analysis of Flow-Field in a Dual Mode Ramjet Combustor with Boundary Layer Bleed in Isolator.” Propulsion and Power Research 10 (1): 37–47. https://doi.org/10.1016/j.jppr.2020.10.004
• Thornton, Earl A., J. Tinsley Oden, W. Woytek Tworzydlo, and Sung-Kie Youn. 1990. “Thermoviscoplastic Analysis of Hypersonic Structures Subjected to Severe Aerodynamic Heating.” Journal of Aircraft 27 (9): 826–35. https://doi.org/10.2514/3.45943
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2008a. “Interaction of Torsion and Lateral Bending in Aircraft Nose Landing Gear Shimmy.” Nonlinear Dynamics 57 (3): 455–67. https://doi.org/10.1007/s11071-008-9455-y
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2010a. “Bifurcation Analysis of Nose-Landing-Gear Shimmy with Lateral and Longitudinal Bending.” Journal of Aircraft 47 (1): 87–95. https://doi.org/10.2514/1.43507
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2012. “Multi-Parameter Bifurcation Study of Shimmy Oscillations in a Dual-Wheel Aircraft Nose Landing Gear.” Nonlinear Dynamics 70 (2): 1675–88. https://doi.org/10.1007/s11071-012-0565-1
• Thota, Phanikrishna, Bernd Krauskopf, Mark Lowenberg, and Etienne Coetzee. 2010b. “Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy.” Journal of Aircraft 47 (5): 1697–1706. https://doi.org/10.2514/1.c000248
• Thowsen, Arild. 1978. “Identifiability of Dynamic Systems.” International Journal of Systems Science 9 (7): 813–25. https://doi.org/10.1080/00207727808941738
• Tian, Chungeng, Ning Hao, and Fenghua He. 2025. “T-ESKF: Transformed Error-State Kalman Filter for Consistent Visual-Inertial Navigation.” IEEE Robotics and Automation Letters 10 (2): 1808–15. https://doi.org/10.1109/lra.2024.3524905
• Tian, Zhen, Jian Li, Qing Li, and Nong Cheng. 2017. “A Visual-Inertial Navigation System Based on Multi-State Constraint Kalman Filter.” In 2017 9th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC). IEEE. https://doi.org/10.1109/ihmsc.2017.52
• Tian, Haiting, Ruiming Yuan, Chunxi Zhang, Jing Jin, Ningfang Song, and Song Lin. 2011. “Nonlinear Empirical Mode Predictive Drift Extraction on Fiber Optical Gyroscope.” Optik 122 (5): 415–21. https://doi.org/10.1016/j.ijleo.2010.02.024
• Tianyu, Hou. 2024. “Impact of Gravitational Anomalies and Vertical Deviations on the Accuracy of Inertial Navigation Systems and Compensation Methods.” In 2024 International Ural Conference on Electrical Power Engineering (UralCon). IEEE. https://doi.org/10.1109/uralcon62137.2024.10718983
• Tie, Junbo, Juliang Cao, Meiping Wu, Junxiang Lian, Shaokun Cai, and Lin Wang. 2018. “Compensation of Horizontal Gravity Disturbances for High Precision Inertial Navigation.” Sensors 18 (3): 906. https://doi.org/10.3390/s18030906
• Tie, Junbo, Meiping Wu, Juliang Cao, Junxiang Lian, and Shaokun Cai. 2017. “The Impact of Initial Alignment on Compensation for Deflection of Vertical in Inertial Navigation.” In 2017 IEEE International Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM). IEEE. https://doi.org/10.1109/iccis.2017.8274806
• Tiejun Qu, Xudong Yang, and Ziyun Tian. 2006. “A Self-Compensation Algorithm for Drift of Platform Inertial Navigation System.” In 2006 1st International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2006.1627711
• Tijing, Tsai. 1998. “A Platformles s Inertial Navigation System Based on a Canonical Gravitational Gradiometer.” Journal of Applied Mathematics and Mechanics 62 (5): 819–22. https://doi.org/10.1016/s0021-8928(98)00104-x
• Titov, Egor, and Sergey Serebryansky. 2026. “Approach to the Main Landing Gear Linkage Design for the Requirement of Ultimate Loads on Links during Emergency Landing.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00486-x
• Tiwari, Shivendra N., and Ketan P. Detroja. 2024. “Flexibility Modeling and Autopilot Design of Interceptor Missile Using Multiple Sensing.” Franklin Open 9: 100184. https://doi.org/10.1016/j.fraope.2024.100184
• Tiwari, Shivendra N., and Ketan P. Detroja. 2025. “Adaptive Roll Autopilot Design for Interceptor Missile.” In 2025 11th International Conference on Control, Decision and Information Technologies (CoDIT). IEEE. https://doi.org/10.1109/codit66093.2025.11321814
• Tiwari, S. N., P. N. Dwivedi, and A. Bhattacharyya. 2018. “Robust Scheduling of Nonlinear Time-Scale Separated Autopilot Using Online Static Margin Estimation.” IFAC-PapersOnLine 51 (1): 621–26. https://doi.org/10.1016/j.ifacol.2018.05.104
• Tkhorenko, Maxim, and Evgeny Karshakov. 2022. “Estimating the Potential Accuracy of Magnetic Navigation Based on Magnetic Survey Data.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815357
• Toda, Atsumi, and Yoshikazu Koike. 2021. “Simulation Design of Thermopile and Magnetometer Aided INS/GPS Navigation System for UAV Navigation.” In 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial51137.2021.9430487
• Tokta, Aybars, and Alı Köksal Hocaoǧlu. 2023. “A Novel Multi-Hypothesis Filter for Terrain Aided Navigation.” IEEE Access 11: 62758–70. https://doi.org/10.1109/access.2023.3288832
• Tola, Engin. 2016. “A Self Calibrating Star Tracker System.” In 2016 24th Signal Processing and Communication Application Conference (SIU). IEEE. https://doi.org/10.1109/siu.2016.7495892
• Tong, Bingming, Wei Chen, and Luyao Du. 2025. “Adaptive Navigation Strategy for Low-Cost IMU-Assisted Vehicles in GNSS-Denied Traffic Environment.” Journal of Advanced Transportation 2025 (1): 2762711. https://doi.org/10.1155/atr/2762711
• Tonhauser, C., and P. Hecker. 2016. “Mixed H2/H∞ Filter for Automatic Aircraft Landing with Optical Sensors.” In 2016 DGON Intertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2016.7745677
• Toth, Charles, Dorota A. Grejner-Brzezinska, and Young-Jin Lee. 2008. “Terrain-Based Navigation: Trajectory Recovery from LiDAR Data.” In 2008 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2008.4570067
• Tourajizadeh, H., and S. Zare. 2016. “Robust and Optimal Control of Shimmy Vibration in Aircraft Nose Landing Gear.” Aerospace Science and Technology 50: 1–14. https://doi.org/10.1016/j.ast.2015.12.019
• Trapier, S., S. Deck, and P. Duveau. 2008. “Delayed Detached-Eddy Simulation and Analysis of Supersonic Inlet Buzz.” AIAA Journal 46 (1): 118–31. https://doi.org/10.2514/1.32187
• Trapier, Simon, Sébastien Deck, Philippe Duveau, and Pierre Sagaut. 2007b. “Time-Frequency Analysis and Detection of Supersonic Inlet Buzz.” AIAA Journal 45 (9): 2273–84. https://doi.org/10.2514/1.29196
• Trapier, Simon, Philippe Duveau, and Sebastien Deck. 2006. “Experimental Study of Supersonic Inlet Buzz.” AIAA Journal 44 (10): 2354–65. https://doi.org/10.2514/1.20451
• Traub, Lance W. 2001. “Lift and Drag Characteristics of a Supersonic Biplane Configuration.” Journal of Aircraft 38 (5): 963–66. https://doi.org/10.2514/2.2862
• Tripathi, Amit Kumar, Vijay V. Patel, and Radhakant Padhi. 2018. “Vision Based Automatic Landing with Runway Identification and Tracking.” In 2018 15th International Conference on Control, Automation, Robotics and Vision (ICARCV). IEEE. https://doi.org/10.1109/icarcv.2018.8581208
• Tripathi, Amit Kumar, Vijay V. Patel, and Radhakant Padhi. 2024. “Vision Based Runway Identification with Marked or Unmarked Terrain for Automatic Landing Applications of UAV.” IFAC-PapersOnLine 57: 125–30. https://doi.org/10.1016/j.ifacol.2024.05.022
• Troiani, Chiara, and Agostino Martinelli. 2012. “Vision-Aided Inertial Navigation Using Virtual Features.” In 2012 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2012.6386140
• Truesdale, Nicholas A., Kevin J. Dinkel, Zach J. B. Dischner, Jed H. Diller, and Eliot F. Young. 2013a. “DayStar: Modeling and Test Results of a Balloon-Borne Daytime Star Tracker.” In 2013 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2013.6497411
• Truong, Cong-Thanh, and Vinh-Hao Nguyen. 2024. “Neural Network Based PID Control for Two-Axis Inertial Stabilized Platform.” In 2024 9th International Conference on Applying New Technology in Green Buildings (ATiGB). IEEE. https://doi.org/10.1109/atigb63471.2024.10717677
• Tse, Edison, and John Anton. 1971. “On the Identifiability of Parameters.” In 1971 IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1971.271048
• Tse, E., and J. Anton. 1972. “On the Identifiability of Parameters.” IEEE Transactions on Automatic Control 17 (5): 637–46. https://doi.org/10.1109/tac.1972.1100091
• Tsien, S. H. 1955. “The Supersonic Conical Wing of Minimum Drag.” Journal of the Aeronautical Sciences 22 (12): 805–17. https://doi.org/10.2514/8.3476
• Tsipis, Kosta. 1975. “The Long-Range Cruise Missile.” Bulletin of the Atomic Scientists 31 (4): 14–26. https://doi.org/10.1080/00963402.1975.11458225
• Tsoukalas, Athanasios, Halil Utku Unlu, Nikolaos Evangeliou, and Anthony Tzes. 2026. “Unmanned Aerial Vehicle Safe Autonomous Landing.” In 2026 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas69441.2026.11598570
• Tsourdos, Antonios, Evan J. Hughes, and Brian A. White. 2006. “Fuzzy Multi-Objective Design for a Lateral Missile Autopilot.” Control Engineering Practice 14 (5): 547–61. https://doi.org/10.1016/j.conengprac.2005.01.009
• Tsukamoto, Takashiro, Fumito Miyazaki, Yasushi Tomizawa, and Shuji Tanaka. 2024. “Real Time Mismatch Monitoring Using Software Defined Frequency Modulation and Rate Integrating Gyroscope.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502049
• Tsukamoto, Takashiro, and Shuji Tanaka. 2017. “FM/rate Integrating MEMS Gyroscope Using Independently Controlled CW/CCW Mode Oscillations on a Single Resonator.” In 2017 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2017.7935661
• Tsukamoto, Takashiro, and Shuji Tanaka. 2019. “MEMS Rate Integrating Gyroscope with Temperature Corrected Virtual Rotation.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739625
• Tsukamoto, Takashiro, and Shuji Tanaka. 2022. “Real Time Q-Factor Mismatch Detection for Rate Integrating Gyroscope Using Amplitude Modulated Driving Signal.” In 2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial53425.2022.9787723
• Tsung-Lin Chen. 2008. “Design and Analysis of a Fault-Tolerant Coplanar Gyro-Free Inertial Measurement Unit.” Journal of Microelectromechanical Systems 17 (1): 201–12. https://doi.org/10.1109/jmems.2007.911372
• Tu, Eugene L. 1994. “Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics.” Journal of Aircraft 31 (1): 138–45. https://doi.org/10.2514/3.46466
• Tu, Yi-Hsuan, and Chao-Chung Peng. 2021. “An ARMA-Based Digital Twin for MEMS Gyroscope Drift Dynamics Modeling and Real-Time Compensation.” IEEE Sensors Journal 21 (3): 2712–24. https://doi.org/10.1109/jsen.2020.3028140
• Tucker, Shirley J., and Henry E. Stern. 1986. “An Application of Error-Covariance Analysis to Inertial Platform Errors.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4789102
• Tudosie, Alexandru-Nicolae. 2024. “Aircraft Turbojet Engine with Afterburning as Controlled Object.” In 2024 25th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/iccc62069.2024.10569513
• Tukizi, O. 1959. “Diffraction Theory of Tropospheric Propagation near and beyond the Radio Horizon: Part I–Theory.” IRE Transactions on Antennas and Propagation 7 (3): 261–67. https://doi.org/10.1109/tap.1959.1144684
• Tulembayev, Alizhan, Alexandr Dolya, Ainur Kuttybayeva, Timur Jussupbekov, and Kalmukhamed Tazhen. 2026. “Energy-Aware Adaptive Communication Topology with Edge-AI Navigation for UAV Swarms in GNSS-Denied Environments.” Drones 10 (4): 273. https://doi.org/10.3390/drones10040273
• Tunik, Yu V., G. Ya Gerasimov, V. Yu Levashov, and V. O. Mayorov. 2022. “Busemann Diffuser for Supersonic Ramjet on Detonation Combustion of Kerosene Vapor.” Acta Astronautica 198: 495–501. https://doi.org/10.1016/j.actaastro.2022.06.027
• Tunik, Yu. V., and V. O. Mayorov. 2022a. “Busemann Diffuser for Supersonic Ramjet Engine with Detonation Combustion of Hydrogen-Air Mixture.” International Journal of Hydrogen Energy 47 (51): 21828–40. https://doi.org/10.1016/j.ijhydene.2022.05.023
• Tunik, Yu. V., and V. O. Mayorov. 2022b. “Energy Efficiency of Detonation Combustion in Supersonic Ramjet Engines.” Acta Astronautica 194: 488–95. https://doi.org/10.1016/j.actaastro.2021.09.038
• Turan, Burak. 2020. “Comparison of Nonlinear Filtering Methods for Terrain Referenced Aircraft Navigation.” In 2020 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans46316.2020.9109984
• Turan, Burak, and Ali Turker Kutay. 2016. “Particle Filter Studies on Terrain Referenced Navigation.” In 2016 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2016.7479793
• Turan, Burak, and Halil Ozan Ünsal. 2023. “Flight Test Results of Terrain Referenced Aircraft Navigation with Laser Altimeter.” In 2023 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans53410.2023.10139978
• Tyren, C. 1987. “Magnetic Terrain Navigation.” In Proceedings of the 1987 5th International Symposium on Unmanned Untethered Submersible Technology, vol. 5. Institute of Electrical and Electronics Engineers. https://doi.org/10.1109/uust.1987.1158556
• Uijt_de_Haag, M., and A. Vadlamani. 2006. “Flight Test Evaluation of Various Terrain Referenced Navigation Techniques for Aircraft Approach Guidance.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650633
• Ullah, P., V. Ragot, P. Zwahlen, and F. Rudolf. 2015. “A New High Performance Sigma-Delta MEMS Accelerometer for Inertial Navigation.” In 2015 DGON Inertial Sensors and Systems Symposium (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2015.7314257
• Ulman, N. 1989. “Computers Make Celestial Navigation Less Celestial?” IEEE Aerospace and Electronic Systems Magazine 4 (3): 39–40. https://doi.org/10.1109/62.17936
• Ulukır, Talha, Ufuk Dursun, and İlker Üstoğlu. 2025. “Automatic Landing of Fixed-Wing Aircraft with Constrained Algebraic Model Predictive Control.” Control Theory and Technology 23 (4): 688–701. https://doi.org/10.1007/s11768-025-00275-5
• Ünal, Doruk, İlker Murat Koç, Ukte Aksen, and Osman Taha Şen. 2025. “A Generic Interacting Multiple Model Approach for Ballistic Missile Threat Tracking without Prior Missile Information.” IFAC-PapersOnLine 59 (30): 49–54. https://doi.org/10.1016/j.ifacol.2025.12.211
• Unsal, Halil Ozan, and Mehmet Ercin Ozgeneci. 2017. “Error Budgeting for Inertial Measurement Units Based on System Scenario and Navigation Specifications.” In 2017 25th Signal Processing and Communications Applications Conference (SIU). IEEE. https://doi.org/10.1109/siu.2017.7960582
• Unterberg, Walter. 1957. “An Analysis of Heating Problems in Supersonic Ramjet Tailpipes.” Journal of Jet Propulsion 27 (5): 514–21. https://doi.org/10.2514/8.12848
• Uosaki, Katsuji, and Toshiharu Hatanaka. 2005. “Multi-Objective Optimization Approach to Optimal Input Design for Autoregressive Model Identification.” IFAC Proceedings Volumes 38 (1): 476–81. https://doi.org/10.3182/20050703-6-cz-1902.00080
• Uosaki, Katsuji, Toshiharu Hatanaka, and Kazuyoshi Kondo. 2006. “Optimal Input Design for Linear Stochastic Model Identification from Viewpoint of Multi-Objective Optimization.” IFAC Proceedings Volumes 39 (1): 1150–55. https://doi.org/10.3182/20060329-3-au-2901.00185
• Urban, T. J., P. Iwaskiw, and P. A. Iglesias. 1999. “Understanding Missile Autopilot Design Using the H/sub ∞/ Loop Shaping Design Procedure.” In Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328), vol. 1. IEEE. https://doi.org/10.1109/cca.1999.806205
• Urnes, J. M., and R. K. Hess. 1985. “Development of the F/A-18A Automatic Carrier Landing System.” Journal of Guidance, Control, and Dynamics 8 (3): 289–95. https://doi.org/10.2514/3.19978
• Urnes, R. K. Hess J. M., R. F. Moomaw, and R. W. Huff. 1981. “H-Dot Automatic Carrier Landing System for Approach Control in Turbulence.” Journal of Guidance and Control 4 (2): 177–83. https://doi.org/10.2514/3.56069
• Uygar Yengin, Ziya, and Emre Koyuncu. 2025. “Cooperative Terrain-Based GNSS-Denied Navigation with Particle Filter.” IEEE Access 13: 106129–39. https://doi.org/10.1109/access.2025.3580462
• Vadlamani, A. K., and M. U. de Haag. 2004. “Improved Downward-Looking Terrain Database Integrity Monitor and Terrain Navigation.” In 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720). IEEE. https://doi.org/10.1109/aero.2004.1367934
• Vafanejad, Arash, and Eun Sok Kim. 2015. “Effect of Diaphragm Perforation on Quality Factor of Hemispherical Resonator Gyroscope.” In 2015 Transducers - 2015 18th International Conference on Solid-State Sensors, Actuators and Microsystems (TRANSDUCERS). IEEE. https://doi.org/10.1109/transducers.2015.7180852
• Valdivia, A., K. B. Yuceil, J. L. Wagner, N. T. Clemens, and D. S. Dolling. 2014. “Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators.” AIAA Journal 52 (6): 1207–18. https://doi.org/10.2514/1.j052214
• Valenti, Roberto G., Ivan Dryanovski, and Jizhong Xiao. 2013. “A Non-Inertial Acceleration Suppressor for Low Cost Inertial Measurement Unit Attitude Estimation.” In 2013 IEEE International Conference on Robotics and Biomimetics (ROBIO). IEEE. https://doi.org/10.1109/robio.2013.6739531
• Valles, Federico Paredes, Daniel P. Magree, and Eric N. Johnson. 2017. “Direct Feature Correspondence in Vision-Aided Inertial Navigation for Unmanned Aerial Vehicles.” In 2017 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2017.7991446
• Vaman, D. 2012. “Terrain Referenced Navigation: History, Trends and the Unused Potential.” In 2012 IEEE/AIAA 31st Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc.2012.6382949
• van Bezooijen, R. W. H. 1989. “A Star Pattern Recognition Algorithm for Autonomous Attitude Determination.” IFAC Proceedings Volumes 22 (7): 51–58. https://doi.org/10.1016/s1474-6670(17)53386-8
• van Bezooijen, R. W. H. 1992. “Autonomous Star Tracker Development.” IFAC Proceedings Volumes 25 (22): 513–18. https://doi.org/10.1016/s1474-6670(17)49697-2
• van der Klauw, A. C., G. J. P. De Reuver, and P. P. J. van den Bosch. 1994. “Optimal Input Design Based on Global Identification.” IFAC Proceedings Volumes 27 (8): 1459–64. https://doi.org/10.1016/s1474-6670(17)47916-x
• van Slagmaat, M. T. P. 1992. “Tire Models in Aircraft Landing Gear Simulation.” Vehicle System Dynamics 21 (sup001): 108–15. https://doi.org/10.1080/00423119208970002
• van Slagmaat, M. T. P. 2004. “Tire Models in Aircraft Landing Gear Simulation.” Vehicle System Dynamics 21: 108–15. https://doi.org/10.1080/00423110408970002
• Vanderwerf, K. n.d. “Schuler Pumping of Inertial Velocity Errors Due to Gravity Anomalies along a Popular North Pacific Airway.” In Proceedings of Position, Location and Navigation Symposium - PLANS ‘96. IEEE. https://doi.org/10.1109/plans.1996.509140
• Vargas Venegas, Carlos, and Daning Huang. 2023. “Physics-Infused Reduced-Order Modeling of Aerothermal Loads for Hypersonic Aerothermoelastic Analysis.” AIAA Journal 61 (3): 1002–20. https://doi.org/10.2514/1.j062214
• Vasilyuk, N., and D. Tokarev. 2020. “GNSS+inertial+odometer Navigation System for Land Vehicles with an Extended Odometer’s Model Identification.” In 2020 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss50053.2020.9244893
• Vatanparvar, D., and A. M. Shkel. 2022. “Rate-Integrating Gyroscope Operation in the Non-Linear Regime.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926373
• Vathsal, S. 1986. “Design and Simulation of Closed-Loop Ground Alignment of Inertial Platforms with Sway Motion.” Journal of Guidance, Control, and Dynamics 9. https://ntrs.nasa.gov/citations/19860054302
• Vathsal, S. 1991. “Estimation of Circular Error Probability of Strapped down Inertial Navigation System by Propagation of Error Covariance Matrix.” In Proceedings IECON ‘91: 1991 International Conference on Industrial Electronics, Control and Instrumentation. IEEE. https://doi.org/10.1109/iecon.1991.239282
• Vau, Bernard, Damien Ponceau, and Mehdi Bussutil. 2018. “A Control Strategy for Coriolis and Centrifugal Effects Reduction in an Inertial System Test Equipment.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358114
• Vedder, John D. 1993. “Star Trackers, Star Catalogs, and Attitude Determination: Probabilistic Aspects of System Design.” Journal of Guidance, Control, and Dynamics 16 (3): 498–504. https://doi.org/10.2514/3.21037
• Veeran, Sasha, Apostolos Pesyridis, and Lionel Ganippa. 2018. “Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine.” Energies 11 (10): 2558. https://doi.org/10.3390/en11102558
• Venkataraman, Raghu, and Peter Seiler. 2019. “Fault-Tolerant Flight Control Using One Aerodynamic Control Surface.” Journal of Guidance, Control, and Dynamics 42 (3): 570–84. https://doi.org/10.2514/1.g003824
• Venkateswara Rao, D. M. K. K., and Tiauw Hiong Go. 2014. “Automatic Landing System Design Using Sliding Mode Control.” Aerospace Science and Technology 32 (1): 180–87. https://doi.org/10.1016/j.ast.2013.10.001
• Veresnikov, Georgy, and Vladimir Goncharenko. 2025. “Optimization Algorithms for Aerodynamic Design of a Supersonic Passenger Aircraft Using Uncertainty Theory.” Aerospace Systems. https://doi.org/10.1007/s42401-025-00371-z
• Vergez, Paul L. 1981. “Linear Optimal Guidance for an AIM-9L Missile.” Journal of Guidance and Control 4 (5): 662–63. https://doi.org/10.2514/3.56125
• Veselý, Miloš, Jindřich Duník, and Tomáš Béda. 2025. “Barometer-Free Aircraft Terrain-Aided Navigation System: Prototype Design and Flight-Test Validation.” In 2025 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans61210.2025.11028522
• Videmsek, Andrew, and Maarten Uijt de Haag. 2020. “Terrain Referenced Integrity Monitor for an Unmanned Aircraft Systems Precision Approach.” In 2020 AIAA/IEEE 39th Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc50938.2020.9256636
• Vieira, Leonardo A., and Felipe O. Silva. 2023. “Vertical Channel Stabilization of Barometer-Aided Inertial Navigation Systems by Optimal Control.” Asian Journal of Control 25 (5): 3395–3411. https://doi.org/10.1002/asjc.3058
• Vieweg, S. 1994. “Integrity Monitoring and Failure Identification within an Integrated Satellite/inertial Navigation System.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303386
• Vincent, Tyrone L., Carlo Novara, Kenneth Hsu, and Kameshwar Poolla. 2009. “Input Design for Structured Nonlinear System Identification.” IFAC Proceedings Volumes 42 (10): 174–79. https://doi.org/10.3182/20090706-3-fr-2004.00029
• Vincent, Tyrone L., Carlo Novara, Kenneth Hsu, and Kameshwar Poolla. 2010. “Input Design for Structured Nonlinear System Identification.” Automatica 46 (6): 990–98. https://doi.org/10.1016/j.automatica.2010.02.029
• Vio, Gareth A., David J. Munk, and Dries Verstraete. 2018. “Transient Temperature Effects on the Aerothermoelastic Response of a Simple Wing.” Aerospace 5 (3): 71. https://doi.org/10.3390/aerospace5030071
• “Vision-Aided Inertial Navigation Based on Ground Plane Feature Detection.” 2014. IEEE/ASME Transactions on Mechatronics 19 (4): 1206–15. https://doi.org/10.1109/tmech.2013.2276404
• Viswanath, P. R. 1988. “Passive Devices for Axisymmetric Base Drag Reduction at Transonic Speeds.” Journal of Aircraft 25 (3): 258–62. https://doi.org/10.2514/3.45586
• Viswanath, Devan, Srinivasan Krishnaswamy, and Dipankar Deb. 2015. “Homing Missile Guidance Using LOS Rate and Relative Range Measurement.” In 2015 Annual IEEE India Conference (INDICON). IEEE. https://doi.org/10.1109/indicon.2015.7443715
• Vodicheva, L., and Yu. Parysheva. 2019. “Error Analysis Technique for Indirect Method of Calibration of a Strapdown Inertial Measurement Unit.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769361
• Voirol, Lionel, Stephane Guerrier, Yuming Zhang, Mucyo Karemera, and Ahmed Radi. 2020. “Optimally Weighted Wavelet Variance-Based Estimation for Inertial Sensor Stochastic Calibration.” In 2020 12th International Conference on Electrical Engineering (ICEENG). IEEE. https://doi.org/10.1109/iceeng45378.2020.9171715
• von Eggers Rudd, Lael, Darryll J. Pines, and Preston H. Carter. 2000. “Long-Range Performance of Suboptimal Periodic Hypersonic Cruise Trajectories.” Journal of Guidance, Control, and Dynamics 23 (4): 756–58. https://doi.org/10.2514/2.4598
• Wagner, J. L., K. B. Yuceil, and N. T. Clemens. 2010. “Velocimetry Measurements of Unstart of an Inlet-Isolator Model in Mach 5 Flow.” AIAA Journal 48 (9): 1875–88. https://doi.org/10.2514/1.j050037
• Wagner, J. L., K. B. Yuceil, A. Valdivia, N. T. Clemens, and D. S. Dolling. 2009a. “Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow.” AIAA Journal 47 (6): 1528–42. https://doi.org/10.2514/1.40966
• Wagstaff, Brandon, and Jonathan Kelly. 2018. “LSTM-Based Zero-Velocity Detection for Robust Inertial Navigation.” In 2018 International Conference on Indoor Positioning and Indoor Navigation (IPIN). IEEE. https://doi.org/10.1109/ipin.2018.8533770
• Wahab Memon, Zohaib, and Hai Zhang. 2023. “Vehicle Trajectory Estimation in GNSS Denied Environments: An Analysis of Extended Kalman Filter Approach for Monocular Vision Aided Inertial Navigation.” In 2023 20th International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast59916.2023.10712838
• Wahlberg, Bo, Hakan Hjalmarsson, and Mariette Annergren. 2010. “On Optimal Input Design in System Identification for Control.” In 49th IEEE Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2010.5717863
• Wahlberg, Bo, Håkan Hjalmarsson, and Märta Barenthin. 2006. “On Optimal Input Design in System IDENTIFICATION1.” IFAC Proceedings Volumes 39 (1): 499–504. https://doi.org/10.3182/20060329-3-au-2901.00076
• Wainer, Gabriel, Joseph Boi-Ukeme, and Vedant Paranjape. 2023. “Sensor Fusion Devs for Angle Estimation on Inertial Measurement Unit.” In 2023 Winter Simulation Conference (WSC). IEEE. https://doi.org/10.1109/wsc60868.2023.10407940
• Waldmann, Jacques, Raul Ikeda Gomes da Silva, and Ronan Arraes Jardim Chagas. 2016. “Observability Analysis of Inertial Navigation Errors from Optical Flow Subspace Constraint.” Information Sciences 327: 300–326. https://doi.org/10.1016/j.ins.2015.08.017
• Walker, B. J., and F. L. Heltsley. n.d. “Nonintrusive Diagnostics of Supersonic Missile Afterbody Flows.” In International Congress on Instrumentation in Aerospace Simulation Facilities,. IEEE. https://doi.org/10.1109/iciasf.1993.687683
• Wall, Robert. 1983. “Terminal Guidance.” Nature 306 (5940): 220–220. https://doi.org/10.1038/306220c0
• Walther, Arnaud, Christophe Le Blanc, Nicolas Delorme, Yannick Deimerly, Romain Anciant, and Jerome Willemin. 2013. “Bias Contributions in a MEMS Tuning Fork Gyroscope.” Journal of Microelectromechanical Systems 22 (2): 303–8. https://doi.org/10.1109/jmems.2012.2221158
• Waltrup, P. J., F. S. Billig, and M. C. Evans. 1981. “Critical Considerations in the Design of Supersonic Combustion Ramjet /Scramjet/ Engines.” Journal of Spacecraft and Rockets 18 (4): 350–56. https://doi.org/10.2514/3.28060
• Wan, Quan, Honghua Gu, Bo Fan, Heming Zhao, Dacheng Xu, and Shuwen Guo. 2017. “A High Symmetry Polysilicon Micro Hemispherical Resonating Gyroscope with Spherical Electrodes.” In 2017 IEEE Sensors. IEEE. https://doi.org/10.1109/icsens.2017.8233984
• Wan, Xiaoyun, Ming Li, Panpan Chen, and Faisal Hussain. 2025b. “Performance of Invariants of Gravity Gradient Tensor in Matching Navigation: A Case Study in South China Sea.” Geodesy and Geodynamics 16 (3): 341–49. https://doi.org/10.1016/j.geog.2024.11.001
• Wan, Zhiqiang, Liang Ma, Xiaozhe Wang, Zhan Sun, and Chao Yang. 2025a. “Aerothermoelastic Problems of Hypersonic Vehicles and Their Recent Research Progress.” Acta Astronautica 236: 982–1011. https://doi.org/10.1016/j.actaastro.2025.06.055
• Wan, ZhiQiang, YaoKun Wang, YunZhen Liu, and Chao Yang. 2014. “A High-Efficiency Aerothermoelastic Analysis Method.” Science China Physics, Mechanics & Astronomy 57 (6): 1111–18. https://doi.org/10.1007/s11433-014-5410-8
• Wang, Xinlong. 2009. “Fast Alignment and Calibration Algorithms for Inertial Navigation System.” Aerospace Science and Technology 13 (4–5): 204–9. https://doi.org/10.1016/j.ast.2009.04.002
• Wang, Shihe, Muhammad Salman Al Farisi, Takashiro Tsukamoto, and Shuji Tanaka. 2020l. “Roll/Pitch Rate Integrating MEMS Gyroscope Using Dynamically Balanced Dual-Mass Resonator.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090078
• Wang, Yong, Hanyan Bian, Yin Yin, and Xiaohui Wei. 2026d. “Enhancing Nose Landing Gear Shimmy Performance Using Torsional Inerter-Based Dynamic Vibration Absorber.” Chinese Journal of Aeronautics 39 (9): 104120. https://doi.org/10.1016/j.cja.2026.104120
• Wang, Yong, Hanyan Bian, Yin Yin, and Xiaohui Wei. 2026l. “Suppressing Aircraft Nose Landing Gear Shimmy Using Semi-Active Torsional Inerter-Based Dynamic Vibration Absorber with On–off Control Strategy.” Nonlinear Dynamics 114 (8): 571. https://doi.org/10.1007/s11071-026-12441-8
• Wang, Bo, and Tijing Cai. 2022. “A Joint Gravity Matching Algorithm with Less Constraint by Gravity Fields.” In 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51784.2022.9815403
• Wang, Bo, Tijing Cai, and Ke Fang. 2022k. “The Quantification Method of Matching Capability of Areas in Gravity-Aided Inertial Navigation.” IEEE Sensors Journal 22 (21): 20958–67. https://doi.org/10.1109/jsen.2022.3209341
• Wang, Bo, Tijing Cai, and Ke Fang. 2024l. “Observation-Differenced Point Mass Filter in Gravity-Aided Inertial Navigation.” IEEE/ASME Transactions on Mechatronics 29 (2): 1601–6. https://doi.org/10.1109/tmech.2023.3304197
• Wang, Xinwang, and Huiliang Cao. 2022. “Improved VMD-ELM Algorithm for MEMS Gyroscope of Temperature Compensation Model Based on CNN-LSTM and PSO-SVM.” Micromachines 13 (12): 2056. https://doi.org/10.3390/mi13122056
• Wang, Jun-Hou, and Jia-Bin Chen. 2010. “Adaptive Unscented Kalman Filter for Initial Alignment of Strapdown Inertial Navigation Systems.” In 2010 International Conference on Machine Learning and Cybernetics. IEEE. https://doi.org/10.1109/icmlc.2010.5580847
• Wang, Wei, and Xiyuan Chen. 2016. “Temperature Drift Modeling and Compensation of Fiber Optical Gyroscope Based on Improved Support Vector Machine and Particle Swarm Optimization Algorithms.” Applied Optics 55 (23): 6243. https://doi.org/10.1364/ao.55.006243
• Wang, Wei, and Xiyuan Chen. 2018a. “Application of Improved 5th-Cubature Kalman Filter in Initial Strapdown Inertial Navigation System Alignment for Large Misalignment Angles.” Sensors 18 (2): 659. https://doi.org/10.3390/s18020659
• Wang, Wei, and Xiyuan Chen. 2018b. “Multiscale Modeling of Fiber Optic Gyroscope Temperature Drift Based on Improved Ensemble Empirical Mode Decomposition.” Applied Optics 57 (28): 8443. https://doi.org/10.1364/ao.57.008443
• Wang, Wei, and Xiyuan Chen. 2018c. “Self-Alignment for Inertial System in Vibration Environment Based on Improved EEMD.” In 2018 IEEE International Conference on Electro/Information Technology (EIT). IEEE. https://doi.org/10.1109/eit.2018.8500183
• Wang, Chen, Jinbao Chen, Shan Jia, and Heng Chen. 2020h. “Parameterized Design and Dynamic Analysis of a Reusable Launch Vehicle Landing System with Semi-Active Control.” Symmetry 12 (9): 1572. https://doi.org/10.3390/sym12091572
• Wang, Shihe, Jianlin Chen, Takashiro Tsukamoto, and Shuji Tanaka. 2023g. “Multi-Ring Disk Resonator with Elliptic Spokes for Frequency-Modulated Gyroscope.” Sensors 23 (6): 2937. https://doi.org/10.3390/s23062937
• Wang, Yujie, Qingyang Chen, Peng Wang, Yafei Lu, and Gaowei Jia. 2020k. “Research on Inertial/visual Navigation with Heading-Position Constraints and the Observability Analysis.” In 2020 5th International Conference on Automation, Control and Robotics Engineering (CACRE). IEEE. https://doi.org/10.1109/cacre50138.2020.9229993
• Wang, Haijun, Xuedi Chen, Haiyang Zhan, Xinyuan Liu, Fei Xing, and Qun Hao. 2026e. “Full-Field Numerical on-Orbit Autonomous Calibration Method and Accuracy Assessment of Star Tracker.” IEEE Sensors Journal 26 (8): 11888–94. https://doi.org/10.1109/jsen.2026.3672650
• Wang, Huaxia, Yongmei Cheng, Nan Liu, and Zeyu Kang. 2018f. “A Method of Scene Matching Navigation in Urban Area Based on Shadow Matching.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018902
• Wang, Jinlin, Guo Chuang, and Chen Ming. 2006. “Design of Frequency Stability and Lock Stability Control System for Ring Laser Gyroscope.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.346014
• Wang, Jinchun, and Joohwan Chun. 2006. “Attitude Determination Using a Single Star Sensor and a Star Density Table.” Journal of Guidance, Control, and Dynamics 29 (6): 1329–38. https://doi.org/10.2514/1.17249
• Wang, Xinwang, Ying Cui, and Huiliang Cao. 2023n. “Temperature Drift Compensation of Fiber Optic Gyroscopes Based on an Improved Method.” Micromachines 14 (9): 1712. https://doi.org/10.3390/mi14091712
• Wang, Cong, Chaolei Dang, Chan Ha, Jiang Qin, and Hongyan Huang. 2022p. “Thermodynamic Analysis for a Novel Steam Rankine Cycle Based Indirect Chemical Precooled Engine Used for Supersonic Flight.” Fuel 321: 123956. https://doi.org/10.1016/j.fuel.2022.123956
• Wang, Hairong, Zhihong Deng, and Bo Wang. 2014b. “Analysis of Error Suppression Performance in the Carrier Angle Motion Status for Rotation for FOG Inertial Navigation System.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896768
• Wang, Yu, Zhihong Deng, Peiyuan Zhang, Bo Wang, and Shengwu Zhao. 2024e. “A Gravity-Aided Navigation Matching Algorithm Based on Triangulation.” IEEE Sensors Journal 24 (21): 34851–61. https://doi.org/10.1109/jsen.2024.3439607
• Wang, Minlin, Xueming Dong, Chaojun Qin, and Jingya Liu. 2021a. “Adaptive H∞ Kalman Filter Based Random Drift Modeling and Compensation Method for Ring Laser Gyroscope.” Measurement 167: 108170. https://doi.org/10.1016/j.measurement.2020.108170
• Wang, Fan, Pengfei Fan, Yonghua Fan, Bin Xu, and Jie Yan. 2022m. “Robust Adaptive Control of Hypersonic Vehicle Considering Inlet Unstart.” Journal of Systems Engineering and Electronics 33 (1): 188–96. https://doi.org/10.23919/jsee.2022.000019
• Wang, Fan, Pengfei Fan, Jin Zhang, Yonghua Fan, and Jie Yan. 2023i. “Preventing Inlet Unstart in Air-Breathing Hypersonic Vehicles Using Adaptive Backstepping Control with State Constraints.” Acta Astronautica 211: 498–509. https://doi.org/10.1016/j.actaastro.2023.06.043
• Wang, Xin, Dongzhu Feng, and Yunfeng Yu. 2007. “Modeling Method and CFD Simulation of a Hypersonic Cruise Vehicle.” In 2007 2nd IEEE Conference on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/iciea.2007.4318625
• Wang, Shuang, and Yunhai Geng. 2014. “Large Field and High Precision Optical System for Star Tracker.” In 2014 IEEE International Conference on Information and Automation (ICIA). IEEE. https://doi.org/10.1109/icinfa.2014.6932704
• Wang, Jie, and Hongqiang Gu. 2008. “Compensation Algorithm of Device Error for Rate Strapdown Inertial Navigation System.” In 2008 First International Conference on Intelligent Networks and Intelligent Systems. IEEE. https://doi.org/10.1109/icinis.2008.137
• Wang, Jianbo, Jinyun Guo, Xin Liu, Yi Shen, and Qiaoli Kong. 2017f. “Local Oceanic Vertical Deflection Determination with Gravity Data along a Profile.” Marine Geodesy 41 (1): 24–43. https://doi.org/10.1080/01490419.2017.1380091
• Wang, Shunyue, and Fengtian Han. 2020. “Analysis and Compensation of Bias Drift for a Micromachined Spinning-Rotor Gyroscope with Electrostatic Suspension.” Sensors 20 (6): 1799. https://doi.org/10.3390/s20061799
• Wang, Wenkai, Zhongxi Hou, Xianzhong Gao, and Lili Chen. 2019d. “Lowest-Technical-Merit Design Methodology of Hypersonic Cruise Vehicle.” IEEE Access 7: 56480–91. https://doi.org/10.1109/access.2019.2913989
• Wang, Wenkai, Zhongxi Hou, Shangqiu Shan, and Lili Chen. 2019h. “Optimal Periodic Control of Hypersonic Cruise Vehicle: Trajectory Features.” IEEE Access 7: 3406–21. https://doi.org/10.1109/access.2018.2885597
• Wang, Zhao, Yulong Huang, Maosong Wang, Jin Wu, and Yonggang Zhang. 2022d. “A Computationally Efficient Outlier-Robust Cubature Kalman Filter for Underwater Gravity Matching Navigation.” IEEE Transactions on Instrumentation and Measurement 71: 1–18. https://doi.org/10.1109/tim.2022.3141153
• Wang, K. Charles, and Kenneth W. Iliff. 2004. “Retrospective and Recent Examples of Aircraft Parameter Identification at NASA Dryden Flight Research Center.” Journal of Aircraft 41 (4): 752–64. https://doi.org/10.2514/1.332
• Wang, Keke, Shuhai Jiang, and Weimin Cui. 2024d. “Fatigue Life Analysis and Optimization of Key Components of Certain Drag Parachute Lock System.” In 2024 15th International Conference on Reliability, Maintenance and Safety (ICRMS). IEEE. https://doi.org/10.1109/icrms63553.2024.00055
• Wang, Zhen, Jie Jiang, and Yan Ma. 2022a. “Adaptive Dynamic Adjustment Star Identification Threshold Estimation for a Terrestrial Star Tracker.” Applied Optics 61 (28): 8248. https://doi.org/10.1364/ao.470116
• Wang, Yong, Xianyu Jin, and Yin Yin. 2022q. “Using Nonlinear Feedback Control to Improve Aircraft Nose Landing Gear Shimmy Performance.” Meccanica 57 (9): 2395–2411. https://doi.org/10.1007/s11012-022-01560-2
• Wang, Bo, Tianjiao Li, Zhihong Deng, and Mengyin Fu. 2023c. “Comprehensive Image Matching Algorithm Based on Local GLCM for Gravity-Gradient-Aided Navigation.” IEEE/ASME Transactions on Mechatronics 28 (5): 2728–37. https://doi.org/10.1109/tmech.2023.3242232
• Wang, Bo, Tianjiao Li, Zhihong Deng, and Mengyin Fu. 2023o. “Wavelet Transform Based Morphological Matching Area Selection for Underwater Gravity Gradient-Aided Navigation.” IEEE Transactions on Vehicular Technology 72 (3): 3015–24. https://doi.org/10.1109/tvt.2022.3218998
• Wang, Pengfei, Guangchun Li, and Yanbin Gao. 2022c. “A Compensation Method for Gyroscope Random Drift Based on Unscented Kalman Filter and Support Vector Regression Optimized by Adaptive Beetle Antennae Search Algorithm.” Applied Intelligence 53 (4): 4350–65. https://doi.org/10.1007/s10489-022-03734-7
• Wang, Yawen, Qifu Li, and Bei Lu. 2018b. “Automatic Landing System Design via Multivariable Model Reference Adaptive Control.” Aerospace Systems 1 (1): 63–71. https://doi.org/10.1007/s42401-018-0006-z
• Wang, Bo, Jie Li, Yan Meng, Qiao Jiang, and Gui-Zhen Li. 2010c. “Temperature Compensation for Gyroscope Free Micro Inertial Measurement Unit.” In 2010 First International Conference on Pervasive Computing, Signal Processing and Applications. IEEE. https://doi.org/10.1109/pcspa.2010.317
• Wang, Peng, Qingsong Li, Yongmeng Zhang, Yulie Wu, Xuezhong Wu, and Dingbang Xiao. 2023b. “Bias Thermal Stability Improvement of Mode-Matching MEMS Gyroscope Using Mode Deflection.” Journal of Microelectromechanical Systems 32 (1): 1–3. https://doi.org/10.1109/jmems.2022.3218723
• Wang, Feng, Lulu Ling, and Zerui Qi. 2020j. “Research on Data Drift Suppression Method of Gyroscope Sensor Based on First-Order Inertia and Low Pass Filter.” In 2020 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc49329.2020.9164184
• Wang, Zhihua, Chengrui Liu, and Huimin Fu. 2011a. “Correlation Coefficient Stationary Series Method for Gyroscope Random Drift.” In 2011 6th IEEE Conference on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/iciea.2011.5975969
• Wang, JianHua, LuHua Liu, Peng Wang, and GuoJian Tang. 2016c. “Guidance and Control System Design for Hypersonic Vehicles in Dive Phase.” Aerospace Science and Technology 53: 47–60. https://doi.org/10.1016/j.ast.2016.03.010
• Wang, Jiaqi, Xin Liu, Yu Yuan, and Keyu Zhang. 2026j. “A Second-Order State-Sensitivity Propagation Method for Inertial Navigation Error Analysis under Static-Base Conditions.” In 2026 3rd International Conference on Intelligent Systems and Robotics (CISR). IEEE. https://doi.org/10.1109/cisr70722.2026.11680166
• Wang, Tong, Xi Liu, Sheng Zhong, and Hangzai Luo. 2022n. “A Simplified Model MEMS Gyroscope Zero Bias Temperature Drift Calibration Method Based on BP Neural Network.” In 2022 2nd International Conference on Frontiers of Electronics, Information and Computation Technologies (ICFEICT). IEEE. https://doi.org/10.1109/icfeict57213.2022.00034
• Wang, Weihui, Zhang Luo, Ming Wen, Qiang Dan, and Sheng Liu. 2014e. “Thermal Effect on Performance of Micromachined Hemispherical Gyroscope.” In 2014 15th International Conference on Electronic Packaging Technology. IEEE. https://doi.org/10.1109/icept.2014.6922736
• Wang, Wei, Xiaoyong Lv, and Feng Sun. 2013b. “Design of a Novel MEMS Gyroscope Array.” Sensors 13 (2): 1651–63. https://doi.org/10.3390/s130201651
• Wang, Wei, Xiaoyong Lv, and Dingjie Xu. 2014c. “Design of Multi-Degree-of-Freedom Micromachined Vibratory Gyroscope with Double Sense-Modes.” Measurement 58: 6–11. https://doi.org/10.1016/j.measurement.2014.08.030
• Wang, Hong-wei, Yuan-wei Lyu, Jing-yang Zhang, and Si-Fang Liu. 2023h. “Numerical Investigation of Inlet Distortion in a Jet Engine Coupled with Ski-Jump of Carrier-Based Aircraft.” Thermal Science and Engineering Progress 43: 101961. https://doi.org/10.1016/j.tsep.2023.101961
• Wang, Bo, Zixuan Ma, Liu Huang, Zhihong Deng, and Mengyin Fu. 2022f. “A Filtered-Marine Map-Based Matching Method for Gravity-Aided Navigation of Underwater Vehicles.” IEEE/ASME Transactions on Mechatronics 27 (6): 4507–17. https://doi.org/10.1109/tmech.2022.3159596
• Wang, Xiaozhe, Liang Ma, Zhan Sun, and Zhiqiang Wan. 2026a. “Aerothermoelastic Analysis and Topology Optimization Based on the Meshfree Method.” Journal of Aircraft: 1–16. https://doi.org/10.2514/1.c038837
• Wang, Ru, and Wei-feng Meng. 2008. “DA Simulator Design of Inertial Platform in Self-Calibration.” In 2008 International Symposium on Intelligent Information Technology Application Workshops. IEEE. https://doi.org/10.1109/iita.workshops.2008.187
• Wang, Lei, Romeo Ortega, Alexey Bobtsov, Jose Guadalupe Romero, and Bowen Yi. 2023e. “Identifiability Implies Robust, Globally Exponentially Convergent on-Line Parameter Estimation.” International Journal of Control 97 (9): 1967–83. https://doi.org/10.1080/00207179.2023.2246595
• Wang, Yuxin, Linhua Piao, Bei Li, and Xia Ding. 2021d. “Compensation of Temperature Drift of Micro Gyroscope by BP Neural Network Algorithm.” In 2021 IEEE 5th Information Technology,Networking,Electronic and Automation Control Conference (ITNEC). IEEE. https://doi.org/10.1109/itnec52019.2021.9587312
• Wang, Lei, and Junjian Qi. 2024. “Parameter Subset Selection for Power System Model Calibration Using Both Sensitivity and Identifiability.” IEEE Access 12: 153783–95. https://doi.org/10.1109/access.2024.3481318
• Wang, Si, and Jiayuan Shan. 2020. “Three-Channel Autopilot Design for Spinning Missile.” In 2020 IEEE 5th Information Technology and Mechatronics Engineering Conference (ITOEC). IEEE. https://doi.org/10.1109/itoec49072.2020.9141931
• Wang, Xinlong, and Gongxun Shen. 2005. “A Fast and Accurate Initial Alignment Method for Strapdown Inertial Navigation System on Stationary Base.” Journal of Control Theory and Applications 3 (2): 145–49. https://doi.org/10.1007/s11768-005-0007-4
• Wang, Ziyi, Xiaojun Shen, Jie Li, Juan Li, Xueyong Wu, and Yu Yang. 2025c. “Enhancing Integrated Navigation with a Self-Attention LSTM Hybrid Network for UAVs in GNSS-Denied Environments.” Drones 9 (4): 279. https://doi.org/10.3390/drones9040279
• Wang, Jiangtao, Liang Shen, Rui Yang, Lianjie Yue, Jian Jiao, and Zhengmao Yang. 2026c. “Dynamic Roughness Evolution and Vortex-Induced Shear-Accelerated Failure in CMCs Subjected to Cyclic Supersonic Aerothermal Shocks.” Extreme Mechanics Letters 86: 102494. https://doi.org/10.1016/j.eml.2026.102494
• Wang, Xiaowei, Ningfang Song, Jingming Song, and Weile Li. 2020i. “A Photonic Crystal Fiber with Optimized Birefringence-Stress Stability for Fiber Optic Gyroscope.” Optik 206: 163488. https://doi.org/10.1016/j.ijleo.2019.163488
• Wang, Lixin, Shang Tai, Ting Yue, Hailiang Liu, Yanling Wang, and Chen Bu. 2022i. “Longitudinal Aerodynamic Parameter Identification for Blended-Wing-Body Aircraft Based on a Wind Tunnel Virtual Flight Test.” Aerospace 9 (11): 689. https://doi.org/10.3390/aerospace9110689
• Wang, Ziyao, Shengjing Tang, and Jie Guo. 2022e. “Entry Guidance Command Generation for Hypersonic Glide Vehicles under Threats and Multiple Constraints.” IEEE Access 10: 1–15. https://doi.org/10.1109/access.2021.3137641
• Wang, Miaomiao, and Abdelhamid Tayebi. 2019. “Nonlinear Observers for Stereo-Vision-Aided Inertial Navigation.” In 2019 IEEE 58th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc40024.2019.9029563
• Wang, Meiyu, Dapeng Tian, Cailing Wang, Bing Ge, and Fuchao Wang. 2026g. “Inertial Stability Control Method for the Task Space of Inertially Stabilized Platform for Spherical Mechanism.” ISA Transactions 170: 348–64. https://doi.org/10.1016/j.isatra.2026.01.029
• Wang, Xiaoyun, and Liang Wang. 2018. “Time-Serial Modeling and Kalman Filter of MEMS Gyroscope Random Drift Compensation.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019215
• Wang, Boyang, and Zhenjie Wang. 2025. “Adaptive Kalman Filter under Minimum Error Entropy with Fiducial Points for Strap-Down Inertial Navigation System/Ultra-Short Baseline Integrated Navigation Systems.” Journal of Marine Science and Engineering 13 (5): 990. https://doi.org/10.3390/jmse13050990
• Wang, Chenglong, Bo Wang, Zhihong Deng, and Mengyin Fu. 2020f. “A Matching Algorithm with Gravity Field Matching Characteristic for Underwater Gravity-Aided Inertial Navigation.” In 2020 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac51589.2020.9326830
• Wang, Chenglong, Bo Wang, Zhihong Deng, and Mengyin Fu. 2021f. “A Delaunay Triangulation-Based Matching Area Selection Algorithm for Underwater Gravity-Aided Inertial Navigation.” IEEE/ASME Transactions on Mechatronics 26 (2): 908–17. https://doi.org/10.1109/tmech.2020.3012499
• Wang, Zhixin, Chen Wang, Xian Du, Lingcong Nie, Ximing Sun, and Xinyue Wang. 2024p. “Robust H∞ Control and Smooth Transition of Thrust Closed-Loop and Inlet Unstart for Scramjet.” In 2024 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac63892.2024.10865158
• Wang, HuBiao, Yong Wang, Jian Fang, Hua Chai, and Hui Zheng. 2011e. “Simulation Research on a Minimum Root-Mean-Square Error Rotation-Fitting Algorithm for Gravity Matching Navigation.” Science China Earth Sciences 55 (1): 90–97. https://doi.org/10.1007/s11430-011-4308-9
• Wang, Yukun, Qiang Wang, Zhonghu Hao, and Puhua Chen. 2025f. “An Integrated Navigation Method Based on the Strapdown Inertial Navigation System/Scene-Matching Navigation System for UAVs.” Sensors 25 (11): 3379. https://doi.org/10.3390/s25113379
• Wang, Hao, Xiupu Wang, and Jianbing Xie. 2020e. “First-Order Linear Mechatronics Model for Closed-Loop MEMS Disk Resonator Gyroscope.” Sensors 20 (22): 6455. https://doi.org/10.3390/s20226455
• Wang, Tiantian, Congchen Wang, Junying Yang, et al. 2024f. “High Q-Factor and Mode-Matching Disk Ring Gyroscope Using (100) Single Crystal Silicon.” In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial60399.2024.10502052
• Wang, L., W. Wang, H. Yu, and Q. Zhang. 2018c. “Improvement on Azimuth in Rotary Inertial Navigation System Using Photoelectric Encoder and Fiber Optic Gyro.” MAPAN 33 (4): 385–89. https://doi.org/10.1007/s12647-018-0278-0
• Wang, Guochen, Qiuying Wang, Bo Zhao, and Zhenpeng Wang. 2016a. “Compensation Method for Temperature Error of Fiber Optical Gyroscope Based on Relevance Vector Machine.” Applied Optics 55 (5): 1061. https://doi.org/10.1364/ao.55.001061
• Wang, Wenjie, Xinguo Wei, Jian Li, and Gangyi Wang. 2017g. “Noise Suppression Algorithm of Short-Wave Infrared Star Image for Daytime Star Sensor.” Infrared Physics & Technology 85: 382–94. https://doi.org/10.1016/j.infrared.2017.08.002
• Wang, Mingze, Changzhu Wei, Jialun Pu, and Naigang Cui. 2022j. “Predefined-Time Nonsingular Attitude Control for Vertical-Takeoff Horizontal-Landing Reusable Launch Vehicle.” Applied Sciences 12 (19): 10153. https://doi.org/10.3390/app121910153
• Wang, Hubiao, Lin Wu, Hua Chai, Yaofei Xiao, Houtse Hsu, and Yong Wang. 2017a. “Characteristics of Marine Gravity Anomaly Reference Maps and Accuracy Analysis of Gravity Matching-Aided Navigation.” Sensors 17 (8): 1851. https://doi.org/10.3390/s17081851
• Wang, Xu, Wenqi Wu, Zhen Fang, Bing Luo, Yun Li, and Qingan Jiang. 2012e. “Temperature Drift Compensation for Hemispherical Resonator Gyro Based on Natural Frequency.” Sensors 12 (5): 6434–46. https://doi.org/10.3390/s120506434
• Wang, Maosong, Wenqi Wu, Xiaofeng He, and Xianfei Pan. 2019i. “State Transformation Extended Kalman Filter for SINS Based Integrated Navigation System.” In 2019 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss46986.2019.8943781
• Wang, Zhuo, Zhenyu Wu, Tao Wang, and Bo Zhang. 2021g. “Development of Infrared-Guided Missile Precision Detection Simulator.” Machines 9 (9): 198. https://doi.org/10.3390/machines9090198
• Wang, Xin, and Lu Xiao. 2017. “Gyroscope-Reduced Inertial Navigation System for Flight Vehicle Motion Estimation.” Advances in Space Research 59 (1): 413–24. https://doi.org/10.1016/j.asr.2016.09.001
• Wang, Qi, Weinan Xie, Boqi Xi, Hanshi Li, and Guoxing Yi. 2025b. “A Drive Error Identification and Compensation Method for Whole Angle Mode Hemispherical Resonator Gyroscope.” Sensors and Actuators A: Physical 387: 116402. https://doi.org/10.1016/j.sna.2025.116402
• Wang, Qi, Weinan Xie, Boqi Xi, Hanshi Li, and Guoxing Yi. 2025j. “A Novel Closed-Loop Single-Channel Time Division Multiplexing Detection Circuit for Hemispherical Resonator Gyroscope.” Micromachines 16 (3): 273. https://doi.org/10.3390/mi16030273
• Wang, Qi, Weinan Xie, Boqi Xi, Yiwei Sun, and Guoxing Yi. 2023k. “Rate Integrating Hemispherical Resonator Gyroscope Detection Error Analysis and Compensation.” IEEE Sensors Journal 23 (7): 7068–76. https://doi.org/10.1109/jsen.2023.3246044
• Wang, Rong, Zhi Xiong, Jianye Liu, and Lijuan Shi. 2017j. “A Robust Astro-Inertial Integrated Navigation Algorithm Based on Star-Coordinate Matching.” Aerospace Science and Technology 71: 68–77. https://doi.org/10.1016/j.ast.2017.09.013
• Wang, Jiongqi, Kai Xiong, and Haiyin Zhou. 2012b. “Low-Frequency Periodic Error Identification and Compensation for Star Tracker Attitude Measurement.” Chinese Journal of Aeronautics 25 (4): 615–21. https://doi.org/10.1016/s1000-9361(11)60426-3
• Wang, Haiyong, Ershuai Xu, Zhifeng Li, Jingjin Li, and Tianmu Qin. 2015a. “Gaussian Analytic Centroiding Method of Star Image of Star Tracker.” Advances in Space Research 56 (10): 2196–2205. https://doi.org/10.1016/j.asr.2015.08.027
• Wang, Dixing, Tianhe Xu, Min Li, and Yali Shi. 2024j. “Navigation Performance Analysis of Earth–Moon Spacecraft Using GNSS, INS, and Star Tracker.” Satellite Navigation 5 (1): 16. https://doi.org/10.1186/s43020-024-00140-x
• Wang, Shenhang, Qi Xu, Mengyu Liu, Yang Tang, and Ruishi Lin. 2018e. “Initial Alignment Algorithm for Platform Inertial Navigation System Based on Fuzzy Kalman Filter.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019079
• Wang, Xi, Yong Ping Xu, Guo Ming Xia, et al. 2018a. “A 27μW MEMS Silicon Oscillating Accelerometer with Bias Instability and 10-μg/√Hz Noise Floor.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358117
• Wang, Di, Xiaosu Xu, and Yongyun Zhu. 2019b. “An Error Correction Approach Based on AR Model and RLS for Inertial Navigation System.” In 2019 7th International Conference on Control, Mechatronics and Automation (ICCMA). IEEE. https://doi.org/10.1109/iccma46720.2019.8988615
• Wang, Chengpeng, Longsheng Xue, and Keming Cheng. 2019f. “Novel Inducement to Unstart of a Parallel Modular Hypersonic Inlet.” AIAA Journal 57 (2): 760–71. https://doi.org/10.2514/1.j057352
• Wang, Jinwen, Li Yang, and Yuming Bo. 2025e. “IANet: A Deep Learning Inertial Navigation Initial Alignment Framework.” IEEE Internet of Things Journal 12 (22): 47860–68. https://doi.org/10.1109/jiot.2025.3603219
• Wang, Jianpeng, Gongliu Yang, Fumin Liu, Qingzhong Cai, Ningfang Song, and Yi Zhou. 2026h. “An Innovative Multi-Parameter Fusion Compensation Algorithm for ZRO Drift of MEMS Gyroscope under Full-Temperature Conditions.” Measurement 257: 118892. https://doi.org/10.1016/j.measurement.2025.118892
• Wang, Meng, Li Yang, Hongyang Shi, and Shaolei Zhai. 2024o. “Research on the Influence of Biased Structure in Hybrid Inertial Navigation System Based on Rate Biased Ring Laser Gyroscope.” IEEE Sensors Journal 24 (23): 39669–76. https://doi.org/10.1109/jsen.2024.3476668
• Wang, Qi, Chang-song Yang, and Yu-xiang Wang. 2018i. “Terrain-Aided Strapdown Inertial Navigation System with Improved ICCP.” In Cloud Computing and Security. Springer International Publishing. https://doi.org/10.1007/978-3-030-00021-9_11
• Wang, Yibin, Chengwei Yang, and Cheng Zhang. 2021k. “Loose Coupled Initialization Method for Visual Inertial Navigation in Outdoor Low Altitude Flight Environment.” In 2021 6th International Conference on Robotics and Automation Engineering (ICRAE). IEEE. https://doi.org/10.1109/icrae53653.2021.9657780
• Wang, Jianpeng, Gongliu Yang, Yi Zhou, Jiangyuan Zhang, Fumin Liu, and Qingzhong Cai. 2024h. “An in-Run Automatic Demodulation Phase Error Compensation Method for MEMS Gyroscope in Full Temperature Range.” Micromachines 15 (7): 825. https://doi.org/10.3390/mi15070825
• Wang, Zishuai, Yingmin Yi, Chunyi Su, Jinsheng Zhang, and Xiaoli Xi. 2025o. “Universal Time Solution Based on Fiber Optic Gyroscope Error Correction.” Measurement 249: 116995. https://doi.org/10.1016/j.measurement.2025.116995
• Wang, Ruiqi, Guoxing Yi, Weinan Xie, and Changhong Wang. 2024g. “High-Precision Identification and Compensation of Nonlinear Error in Hemispherical Resonator Gyro.” Measurement 237: 114945. https://doi.org/10.1016/j.measurement.2024.114945
• Wang, Ruiqi, Guoxing Yi, Weinan Xie, Zhennan Wei, and Shengwei Dong. 2025l. “Self-Calibration Method for Assembly Errors of Hemispherical Resonator Gyroscope.” International Journal of Mechanical Sciences 306: 110811. https://doi.org/10.1016/j.ijmecsci.2025.110811
• Wang, Ruiqi, Guoxing Yi, Weinan Xie, Zihao Wu, and Longkai Zheng. 2026f. “High-Precision Identification Method for Phase Errors in Whole-Angle Mode Hemispherical Resonator Gyroscope.” In 2026 IEEE International Instrumentation and Measurement Technology Conference (I2MTC). IEEE. https://doi.org/10.1109/i2mtc66907.2026.11694669
• Wang, Bo, Li Yu, Zhihong Deng, and Mengyin Fu. 2016e. “A Particle Filter-Based Matching Algorithm with Gravity Sample Vector for Underwater Gravity Aided Navigation.” IEEE/ASME Transactions on Mechatronics 21 (3): 1399–1408. https://doi.org/10.1109/tmech.2016.2519925
• Wang, Min, Leilei Zeng, Changying Zhao, Shupeng Sun, and Yang Yang. 2023a. “Aerothermoelastic Analysis of Conical Shell in Supersonic Flow.” Applied Sciences 13 (8): 4850. https://doi.org/10.3390/app13084850
• Wang, Jiawei, and Ran Zhang. 2018. “Terminal Guidance for a Hypersonic Vehicle with Impact Time Control.” Journal of Guidance, Control, and Dynamics 41 (8): 1790–98. https://doi.org/10.2514/1.g003540
• Wang, Kaiqiang, and Bainan Zhang. 2021. “Bilevel Trajectory Optimization for Hypersonic Cruise Vehicle Using Bilevel Directed Search Domain.” Journal of Spacecraft and Rockets 58 (2): 375–85. https://doi.org/10.2514/1.a34728
• Wang, Yong, Tao Zhang, Hanyan Bian, Yin Yin, and Xiaohui Wei. 2024q. “Shimmy Performance Analysis and Parameter Optimization of a Dual-Wheel Nose Landing Gear Coupled with Torsional Nonlinear Energy Sink and Considering Structural Nonlinear Factor.” Chaos, Solitons & Fractals 187: 115330. https://doi.org/10.1016/j.chaos.2024.115330
• Wang, Bo, Zihan Zhang, Zhihong Deng, and Mengyin Fu. 2025a. “An Analytic Quantification Method of Matching Accuracy Based on Particle Filter in Gravity-Assisted Inertial Navigation.” IEEE Sensors Journal 25 (10): 18543–52. https://doi.org/10.1109/jsen.2025.3557902
• Wang, Wei, Tingkai Zhang, Dongqing Fan, and Chaoyang Xing. 2013f. “Study on Frequency Stability of a Linear-Vibration MEMS Gyroscope.” Microsystem Technologies 20 (12): 2147–55. https://doi.org/10.1007/s00542-013-1951-4
• Wang, Zi-Hao, Te Zhang, Kai-Yu Qin, and Bo Zhu. 2018j. “A Vision-Aided Navigation System by Ground-Aerial Vehicle Cooperation for UAV in GNSS-Denied Environments.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019191
• Wang, Yong, Tao Zhang, Yin Yin, and Xiaohui Wei. 2024n. “Reducing Shimmy Oscillation of a Dual-Wheel Nose Landing Gear Based on Torsional Nonlinear Energy Sink.” Nonlinear Dynamics 112 (6): 4027–62. https://doi.org/10.1007/s11071-023-09267-z
• Wang, Nannan, Guoqing Zhang, and S. C. M. Yu. 2026b. “Classification of Unstart Flow in a Two-Dimensional Hypersonic Inlet.” Aerospace Science and Technology 172: 111678. https://doi.org/10.1016/j.ast.2026.111678
• Wang, Yu-Jie, and Yong-Ping Zhao. 2026. “Cross-Modal Schlieren-like Image Reconstruction of Supersonic Inlet Flows from Wall-Pressure Signals Using a Pressure-Guided StyleGAN Framework.” Measurement 292: 123286. https://doi.org/10.1016/j.measurement.2026.123286
• Wang, Yu-Jie, Yong-Ping Zhao, and Yi Jin. 2025i. “Multi-Level and Multi-Scale Cross Attention Network of Wavelet Packet Transform for Supersonic Inlet Unstart Prediction.” Expert Systems with Applications 272: 126782. https://doi.org/10.1016/j.eswa.2025.126782
• Wang, Mi, Jianping Zhao, Shuying Jin, and Yufeng Cheng. 2020c. “Attitude Computation Algorithm for Star Camera Based on Combining Calibration and Attitude Determination Processes.” Applied Optics 59 (21): 6399. https://doi.org/10.1364/ao.391448
• Wang, Yu-Jie, Yong-Ping Zhao, Huan Wu, and Yi Jin. 2022l. “A Real-Time Online Unstart Prediction Approach for Supersonic Inlet.” Aerospace Science and Technology 130: 107883. https://doi.org/10.1016/j.ast.2022.107883
• Wang, Yu-Jie, Yong-Ping Zhao, Huan Wu, and Yi Jin. 2023l. “Real-Time Online Unstart Prediction of Supersonic Inlet Based on Pressure Fluctuations.” Aerospace Science and Technology 140: 108420. https://doi.org/10.1016/j.ast.2023.108420
• Wang, Lixin, Rong Zhao, and Yi Zhang. 2022b. “Aircraft Lateral-Directional Aerodynamic Parameter Identification and Solution Method Using Segmented Adaptation of Identification Model and Flight Test Data.” Aerospace 9 (8): 433. https://doi.org/10.3390/aerospace9080433
• Wang, Qiong, Chen Zheng, Peili Wu, and Xiaoyu Wang. 2022g. “Geomagnetic/inertial Navigation Integrated Matching Navigation Method.” Heliyon 8 (11): e11249. https://doi.org/10.1016/j.heliyon.2022.e11249
• Wang, Mengchen, Wei Zheng, Shijie Zhao, Xiaoping Li, and Chuangxin He. 2025k. “A Novel Curvature Directional Feature-Based Matching Area Clustering Method for Underwater Gravity-Aided Navigation.” IEEE Transactions on Instrumentation and Measurement 74: 1–10. https://doi.org/10.1109/tim.2025.3626957
• Wang, Mengchen, Wei Zheng, Shijie Zhao, Xiaoping Li, and Chuangxin He. 2026i. “A Novel Enhanced Boundary-Connected Matching Area Selection Method for Underwater Gravity Aided Navigation.” IEEE Transactions on Vehicular Technology 75 (6): 9380–88. https://doi.org/10.1109/tvt.2025.3647468
• Wang, Bo, Minglong Zhou, Zhihong Deng, and Mengyin Fu. 2019j. “Sum Vector-Difference-Based Matching Area Selection Method for Underwater Gravity-Aided Navigation.” IEEE Access 7: 123616–24. https://doi.org/10.1109/access.2019.2938413
• Wang, Bo, Yuwei Zhu, Zhihong Deng, and Mengyin Fu. 2016b. “The Gravity Matching Area Selection Criteria for Underwater Gravity-Aided Navigation Application Based on the Comprehensive Characteristic Parameter.” IEEE/ASME Transactions on Mechatronics 21 (6): 2935–43. https://doi.org/10.1109/tmech.2016.2587804
• Wang, Bo, Jingwei Zhu, Zhihong Deng, and Mengyin Fu. 2019a. “A Characteristic Parameter Matching Algorithm for Gravity-Aided Navigation of Underwater Vehicles.” IEEE Transactions on Industrial Electronics 66 (2): 1203–12. https://doi.org/10.1109/tie.2018.2831171
• Wang, Bo, Jingwei Zhu, Zixuan Ma, Zhihong Deng, and Mengyin Fu. 2021h. “Improved Particle Filter-Based Matching Method with Gravity Sample Vector for Underwater Gravity-Aided Navigation.” IEEE Transactions on Industrial Electronics 68 (6): 5206–16. https://doi.org/10.1109/tie.2020.2988227
• Wang Kedong, Gu Qitai, and Yan Lei. 2004. “Experimental Research on Counter-Balanced Dither Mechanism for Ring Laser Gyroscope.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308979
• Wang Xinlong, Shen Gongxun, and Tang Delin. n.d. “A Fast Initial Alignment Method of Inertial Navigation System on Stationary Base.” In Proceedings of the 4th World Congress on Intelligent Control and Automation (Cat. No.02EX527), vol. 2. IEEE. https://doi.org/10.1109/wcica.2002.1020809
• Wannas, Akeel Ali, Mohammed Qasim Sulttan, Hussein Al-Jeshami, and Auday Shaker Hadi. 2026. “Gyroscope Calibration Using a Constant Velocity Vector and Magnetometer Data as a Reference.” Measurement 258: 119421. https://doi.org/10.1016/j.measurement.2025.119421
• Wanner, L. D., and J. Hopkins. n.d. “Reconciling the Navigational Grid with the Inertial Navigation System.” In IEEE PLANS ‘88.,Position Location and Navigation Symposium, Record. ‘Navigation into the 21st Century’.. IEEE. https://doi.org/10.1109/plans.1988.195523
• Ward, K. E. 1968. “Contour Plotting for the Transonic Flight-Test Drag Polar.” Journal of Aircraft 5 (2): 191–92. https://doi.org/10.2514/3.43928
• Watanabe, Yoko, Augustin Manecy, Alexandre Amiez, Shin Aoki, and Sho Nagai. 2020. “Fault-Tolerant Final Approach Navigation for a Fixed-Wing UAV by Using Long-Range Stereo Camera System.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9213996
• Watts, A. B., K. Horai, and N. M. Ribe. 1984. “On the Determination of the Deflection of the Vertical by Satellite Altimetry.” Marine Geodesy 8 (1–4): 85–127. https://doi.org/10.1080/15210608409379499
• Weber, Daniel, Clemens Guhmann, and Thomas Seel. 2020. “Neural Networks versus Conventional Filters for Inertial-Sensor-Based Attitude Estimation.” In 2020 IEEE 23rd International Conference on Information Fusion (FUSION). IEEE. https://doi.org/10.23919/fusion45008.2020.9190634
• Weerts, Harm H. M., Paul M. J. Van den Hof, and Arne G. Dankers. 2018. “Identifiability of Linear Dynamic Networks.” Automatica 89: 247–58. https://doi.org/10.1016/j.automatica.2017.12.013
• Wei, Kai, Shaosong Chen, Dongdong Tang, Yihang Xu, Xujian Lyu, and Qing Chen. 2024. “The Influence of Roll Angles on Unsteady Aerodynamics in a Canard-Configured Missile.” International Journal of Mechanical System Dynamics 4 (2): 213–25. https://doi.org/10.1002/msd2.12104
• Wei, D., B. F. Guan, S. H. Li, and Q. W. Fu. 2020. “Study on Strapdown Inertial Navigation Initial Alignment Method Based on Uniaxial Rotation Modulation.” In 2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins43215.2020.9133944
• Wei, Dong, Sihai Li, and Qiangwen Fu. 2022a. “A New Initial Alignment Scheme for Dual-Axis Rotational Inertial Navigation System.” IEEE Transactions on Instrumentation and Measurement 71: 1–10. https://doi.org/10.1109/tim.2022.3180424
• Wei, Guo, Geng Li, Yan Wu, and Xingwu Long. 2011. “Application of Least Squares-Support Vector Machine in System-Level Temperature Compensation of Ring Laser Gyroscope.” Measurement 44 (10): 1898–1903. https://doi.org/10.1016/j.measurement.2011.08.032
• Wei, Jian, Hangming Liu, Jiahao Zhang, Shixing Zhu, Shuangbao Li, and Hengjia Zhu. 2026a. “Dual-Boundary Mechanism of Shimmy over the Full Speed Range in Nose Landing Gear and Inerter-Based Shimmy Suppression Design.” Aerospace 13 (7): 657. https://doi.org/10.3390/aerospace13070657
• Wei, Jian, Shidong Ma, Jing Tian, Yangjing Zhang, and Zhe Zhao. 2026b. “Nonlinear Shimmy Dynamics Analysis of Fuselage-Nose Landing Gear Coupled Systems with Structural Clearance.” Journal of Vibration Engineering & Technologies 14 (5): 263. https://doi.org/10.1007/s42417-025-02274-x
• Wei, Xiao-Hui, and Hong Nie. 2005. “Dynamic Analysis of Aircraft Landing Impact Using Landing-Region-Based Model.” Journal of Aircraft 42 (6): 1631–37. https://doi.org/10.2514/1.6801
• Wei, Yang, Haojun Xu, and Yuan Xue. 2018. “A Longitudinal Automatic Landing System Design Based on Recursive Sliding Mode Dynamic Surface Control with Nonlinear Gains under Icing Condition.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019194
• Wei, Zhennan, Guoxing Yi, Yan Huo, Ziyang Qi, and Zeyuan Xu. 2019. “The Synthesis Model of Flat-Electrode Hemispherical Resonator Gyro.” Sensors 19 (7): 1690. https://doi.org/10.3390/s19071690
• Wei Gao, Bing Cao, Yueyang Ben, and Bo Xu. 2009. “Analysis of Gyro’s Slope Drift Affecting Inertial Navigation System Error.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246609
• Wei Gao, Guofu Zhai, Yueyang Ben, and Qi Nie. 2007. “Practical Velocity-Updating Algorithm of Strapdown Inertial Navigation System with Ring Laser Gyro.” In 2007 IEEE International Conference on Control and Automation. IEEE. https://doi.org/10.1109/icca.2007.4376617
• Wei Gao, Zhilan Xiong, Yanling Hao, and Feng Sun. 2006. “Comparison of INS Transfer Alignments through Observability Analysis.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650680
• Wei Wang and Xiyuan Chen. 2016. “The Temperature Compensation Method of Fiber Optic Gyroscope Based on EEMD, B-Spline and SVM.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828838
• Wei-wei, Cal, Yang Le-ping, Liu Xin-jian, and Zhu Yan-wei. 2013. “Robust Optimal Guidance for Hypersonic Glide Vehicle with Hinge Moment Constraint.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6560984
• Weidong, Zhang, Huang Xianlin, Gao Xiao-Zhi, and Pang Hongjun. 2015. “Multi-Objective Longitudinal Trajectory Optimization for Hypersonic Reentry Glide Vehicle Based on PSO Algorithm.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260001
• Weil, R. D., and K. A. Wise. 1991. “Blended Aero and Reaction Jet Missile Autopilot Design Using VSS Techniques.” In [1991] Proceedings of the 30th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1991.261051
• Weiner, Storm, Xuejian Wu, Zachary Pagel, et al. 2020. “A Flight Capable Atomic Gravity Gradiometer with a Single Laser.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090014
• Weintraub, Milton M. 1962. “Some Restrictions on Nuclear Ramjet Engine Performance Imposed by Control System Component Limitations.” IRE Transactions on Nuclear Science 9 (1): 52–59. https://doi.org/10.1109/tns2.1962.4315890
• Welker, Troy C., Meir Pachter, and Richard E. Huffman. 2013. “Gravity Gradiometer Integrated Inertial Navigation.” In 2013 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2013.6669109
• Wells, William R., Siva S. Banda, and David L. Quam. 1982. “Aircraft Lateral Parameter Estimation from Flight Data with Unsteady Aerodynamic Modeling.” Journal of Aircraft 19 (3): 206–10. https://doi.org/10.2514/3.57377
• Wen, Haoran, Anosh Daruwalla, Chang-Shun Liu, and Farrokh Ayazi. 2020. “A Hermetically-Sealed 2.9MHz N=3 Disk BAW Gyroscope with Sub-Degree-Per-Hour Bias Instability.” In 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems46641.2020.9056407
• Wen, Kai, Chee Kiat Seow, and Soon Yim Tan. 2016. “Inertial Navigation System Positioning Error Analysis and Cramér-Rao Lower Bound.” In 2016 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2016.7479704
• Wenbiao, Zhu, Li Dong, Min Yong, and Chen Yicheng. 2014. “Method of Velocity Controller Design for an Airbreathing Hypersonic Cruise Vehicle.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007458
• Weng, Jun, Xiaoyun Bian, Ke Kou, and Tianhong Lian. 2020. “Optimization of Ring Laser Gyroscope Bias Compensation Algorithm in Variable Temperature Environment.” Sensors 20 (2): 377. https://doi.org/10.3390/s20020377
• Weng, Zheng-Xin, and Song-Jiao Shi. 1999. “H ∞ Robust Performance Design to Missile Autopilot.” IFAC Proceedings Volumes 32 (2): 3142–47. https://doi.org/10.1016/s1474-6670(17)56536-2
• Wenkai, Wang, Hou Zhongxi, Shan Shangqiu, Guo Tianhao, and Chen Lili. 2017b. “Optimal Periodic Control of Hypersonic Cruise Vehicle.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027732
• Wenming Li, Qingxiu Du, and Peng Mi. 2011. “A MEMS Inertial Sensor and AMR Magnetic Sensor Calibration Method.” In 2011 8th International Conference on Information, Communications & Signal Processing. IEEE. https://doi.org/10.1109/icics.2011.6174221
• Werner, Michal, David Čapek, Tomáš Musil, Ondřej Franek, Tomáš Báča, and Martin Saska. 2026. “Kilometer-Scale GNSS-Denied UAV Navigation via Heightmap Gradients: A Winning System from the SPRIN-D Challenge.” In 2026 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra57385.2026.11697278
• Wheelon, A. 1955. “Near-Field Corrections to Line-of-Sight Propagation.” Proceedings of the IRE 43 (10): 1459–66. https://doi.org/10.1109/jrproc.1955.277962
• Wheelon, A. 1956. “Near-Field Corrections to Line-of-Sight Propagation.” IRE Transactions on Antennas and Propagation 4 (3): 322–29. https://doi.org/10.1109/tap.1956.1144433
• Wheelon, Albert D. 1959. “Free Flight of a Ballistic Missile.” ARS Journal 29 (12): 915–26. https://doi.org/10.2514/8.4944
• Wheelon, A., and R. Muchmore. 1955. “Line-of-Sight Propagation Phenomena-II. Scattered Components.” Proceedings of the IRE 43 (10): 1450–58. https://doi.org/10.1109/jrproc.1955.277961
• White, D. P., J. G. Wozniak, and D. A. Lawrence. n.d. “Missile Autopilot Design Using a Gain Scheduling Technique.” In Proceedings of 26th Southeastern Symposium on System Theory. IEEE. https://doi.org/10.1109/ssst.1994.287805
• Wi, Junsung, Kiwook Baeck, and Hyosang Yoon. 2023. “Modeling and Filtering Colored Noise of a Star Tracker.” Journal of the Astronautical Sciences 70 (2): 8. https://doi.org/10.1007/s40295-023-00376-w
• Wibben, Daniel R., and Roberto Furfaro. 2016. “Terminal Guidance for Lunar Landing and Retargeting Using a Hybrid Control Strategy.” Journal of Guidance, Control, and Dynamics 39 (5): 1168–72. https://doi.org/10.2514/1.g001411
• Widnall, William S., Peter A. Grundy, and Walter G. Murch. 1976. “Inertial Navigation System Tests Having Improved Observability of Error Sources.” Journal of Aircraft 13 (1): 12–21. https://doi.org/10.2514/3.58624
• Wilcox, Z. D., W. MacKunis, S. Bhat, R. Lind, and W. E. Dixon. 2009b. “Robust Nonlinear Control of a Hypersonic Aircraft in the Presence of Aerothermoelastic Effects.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160480
• Wilcox, Z. D., W. MacKunis, S. Bhat, R. Lind, and W. E. Dixon. 2010. “Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects.” Journal of Guidance, Control, and Dynamics 33 (4): 1213–24. https://doi.org/10.2514/1.46785
• Williams, D. E., B. Friedland, and J. Richman. 1988. “Integrated Guidance and Control for Combined Command/Homing Guidance.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789781
• Williams, J. G., and E. A. Pohl. n.d. “Missile Reliability Analysis with Censored Data.” In Annual Reliability and Maintainability Symposium. IEEE. https://doi.org/10.1109/rams.1997.571679
• Wilson, R. F., C. L. Phillips, E. R. Graf, and S. A. Starks. n.d. “An Aircraft Landing System Employing Observers.” In Conference Proceedings Southeastcon ‘81.. IEEE. https://doi.org/10.1109/secon.1981.673447
• Wimpress, John K., and John M. Swihart. 1964. “Influence of Aerodynamic Research on the Performance of Supersonic Airplanes.” Journal of Aircraft 1 (2): 71–76. https://doi.org/10.2514/3.43561
• Wise, Kevin A. 1990a. “A Comparison of Six Robustness Tests Evaluating Missile Autopilot Robustness to Uncertain Aerodynamics.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4790834
• Wise, K. A., and E. S. Hamby. 1994. “H/sub ∞/ Missile Autopilot Design with and without Imaginary Axis Zeros.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 2. IEEE. https://doi.org/10.1109/acc.1994.752355
• Wise, Kevin A., Barry C. Mears, and Kameshwar Poolia. 1990. “Missile Autopilot Design Using H∞ Optimal Control with μ-Synthesis.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4791150
• Wise, K. A., and T. Nguyen. 1991. “Optimal Disturbance Rejection in Missile Autopilot Design Using Projective Controls.” In [1991] Proceedings of the 30th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1991.261094
• Wise, K. A., and J. L. Sedwick. 1994. “Missile Autopilot Design Using Nonlinear H ∞ Optimal Control.” IFAC Proceedings Volumes 27 (13): 133–39. https://doi.org/10.1016/s1474-6670(17)45789-2
• Wislicenus, Jan, and Nihad E. Daidzic. 2022. “Estimation of Transport-Category Jet Airplane Maximum Range and Airspeed in the Presence of Transonic Wave Drag.” Aerospace 9 (4): 192. https://doi.org/10.3390/aerospace9040192
• Wolf, H. 1954. “On the Absolute Deflection of the Vertical at Potsdam.” Bulletin géodésique 31 (1): 47–51. https://doi.org/10.1007/bf02526780
• Won, Dae-Yeon, Min-Jea Tahk, and H. Jin Kim. 2011. “A Multi-Model Approach to Gain-Scheduling Control for Agile Missile Autopilot Design.” IFAC Proceedings Volumes 44 (1): 7462–67. https://doi.org/10.3182/20110828-6-it-1002.02534
• Woodbury, Timothy, and John Valasek. 2016. “Synthesis and Flight Test of Automatic Landing Controller Using Quantitative Feedback Theory.” Journal of Guidance, Control, and Dynamics 39 (9): 1994–2010. https://doi.org/10.2514/1.g001758
• Wright, J. L., and J. C. Ruscus. 1959. “A Super-Fast, Carrier Quieted Telemetry System for Missile Impact Instrumentation.” IRE Transactions on Space Electronics and Telemetry SET-5 (2): 76–81. https://doi.org/10.1109/iret-set.1959.5008660
• Wu, Yuanxin. 2014. “Versatile Land Navigation Using Inertial Sensors and Odometry: Self-Calibration, in-Motion Alignment and Positioning.” In 2014 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2014.7049412
• Wu, Y. 2019. “iNavFIter: “Zero Error” Inertial Navigation Computation.” In 2019 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss46986.2019.8943626
• Wu, Yuanxin. 2025a. “Crossroads of Inertial Navigation Computation across Five Decade.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279331
• Wu, Yuan-Ting, and Yi-Cheng Huang. 2026. “Real-Time Autonomous UAV Navigation with SLAM-Based Mapping and Direction-Oriented Exploration in Forest-like GNSS-Denied Scenarios.” Drones 10 (6): 399. https://doi.org/10.3390/drones10060399
• Wu, Lin, Jie Ma, and Jinwen Tian. 2010b. “A Self-Adaptive Unscented Kalman Filtering for Underwater Gravity Aided Navigation.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507294
• Wu, Xiangyu, and Mark Mueller. 2018. “Towards a Consequences-Aware Emergency Landing System for Unmanned Aerial Systems.” In 2018 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas.2018.8453347
• Wu, Fen, Andy Packard, and Gary Balas. 2002b. “Systematic Gain-Scheduling Control Design: A Missile Autopilot Example.” Asian Journal of Control 4 (3): 341–47. https://doi.org/10.1111/j.1934-6093.2002.tb00362.x
• Wu, Weisheng, Chunlei Song, Junhou Wang, and Zhenzhen Long. 2010a. “Cubature Gaussian Particle Filter for Initial Alignment of Strapdown Inertial Navigation System.” In 2010 First International Conference on Pervasive Computing, Signal Processing and Applications. IEEE. https://doi.org/10.1109/pcspa.2010.294
• Wu, Xu, and Feng Sun. 2012. “Simulation Study for FOG Strapdown Inertial Navigation Nonlinear Alignment Based on SVD-Cubature Kalman Filter.” In 2012 Symposium on Photonics and Optoelectronics. IEEE. https://doi.org/10.1109/sopo.2012.6270539
• Wu, Siyuan, Bailing Tian, and Zhiyu Li. 2020b. “Full-Stage Reentry Trajectory Optimization for Reusable Launch Vehicle.” In 2020 39th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc50068.2020.9188640
• Wu, Lin, Hubiao Wang, Hua Chai, Lu Zhang, Houtse Hsu, and Yong Wang. 2017. “Performance Evaluation and Analysis for Gravity Matching Aided Navigation.” Sensors 17 (4): 769. https://doi.org/10.3390/s17040769
• Wu, Xianju, and Zhijun Wei. 2023. “Analysis of the Characteristics of Scramjet Mode and Ramjet Mode of Axisymmetric Dual-Combustion Ramjet.” Acta Astronautica 203: 125–34. https://doi.org/10.1016/j.actaastro.2022.11.034
• Wu, Xianju, Zhijun Wei, Yun Wang, Ling Zhou, Yunhui Wang, and Ningfei Wang. 2026a. “Performance Comparison of Full-Scale Ramjet and Scramjet Using Boron-Based Propellant.” Defence Technology 56: 206–17. https://doi.org/10.1016/j.dt.2025.08.013
• Wu, Ruonan, Qiuping Wu, Fengtian Han, Tianyi Liu, Peida Hu, and Haixia Li. 2016. “Gravity Compensation Using EGM2008 for High-Precision Long-Term Inertial Navigation Systems.” Sensors 16 (12): 2177. https://doi.org/10.3390/s16122177
• Wu, Qiuping, Ruonan Wu, Fengtian Han, and Rong Zhang. 2018b. “A Three-Stage Accelerometer Self-Calibration Technique for Space-Stable Inertial Navigation Systems.” Sensors 18 (9): 2888. https://doi.org/10.3390/s18092888
• Wu, Liang, Qian Xu, Haojing Wang, Hongwu Lyu, and Kaipeng Li. 2019a. “Guide Star Selection for the Three-FOV Daytime Star Sensor.” Sensors 19 (6): 1457. https://doi.org/10.3390/s19061457
• Wu, Huan-ming, Hai-gang Yang, Tao Yin, and Hui Zhang. 2011b. “Stability Analysis of MEMS Gyroscope Drive Loop Based on CPPLL.” In 2011 Asia Pacific Conference on Postgraduate Research in Microelectronics & Electronics. IEEE. https://doi.org/10.1109/primeasia.2011.6075067
• Wu, Kevin, Shujie Zhang, Mingyi Luan, and Jianping Wang. 2020a. “Effects of Flow-Field Structures on the Stability of Rotating Detonation Ramjet Engine.” Acta Astronautica 168: 174–81. https://doi.org/10.1016/j.actaastro.2019.12.022
• Wu, Haibin, Xudong Zheng, Yaojie Shen, Xuetong Wang, Zhonghe Jin, and Zhipeng Ma. 2021b. “A Sub-0.1°/h Bias-Instability MEMS Gyroscope Using Resonant Constant-Frequency Driving Technique.” In 2021 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors47087.2021.9639632
• Wu, Haibin, Xudong Zheng, Xuetong Wang, Yaojie Shen, Zhipeng Ma, and Zhonghe Jin. 2021a. “A 0.09°/h Bias-Instability MEMS Gyroscope Working with a Fixed Resonance Frequency.” IEEE Sensors Journal 21 (21): 23787–98. https://doi.org/10.1109/jsen.2021.3110054
• Wu, Qilong, and Qidan Zhu. 2024. “Fault-Tolerant Control for Carrier-Based Aircraft Automatic Landing Subject to Multiple Disturbances and Actuator Faults.” International Journal of Aerospace Engineering 2024: 1–14. https://doi.org/10.1155/2024/2054883
• Wu Erhui, Gao Guohua, Shen Lincheng, and Chang Wensen. n.d. “A Probability-Based Terrain-Aided Navigation Approach and Its Relative Terrain Navigability Analysis.” In Proceedings of the IEEE International Conference on Industrial Technology (ICIT’96). IEEE. https://doi.org/10.1109/icit.1996.601704
• Wuju, Ma, Song Xiaodong, and Yao Xiaoxian. 2011. “Transitional Ballistic Trajectory Optimization of a Supersonic Target Cruise Missile.” In Proceedings of 2011 International Conference on Electronic & Mechanical Engineering and Information Technology. IEEE. https://doi.org/10.1109/emeit.2011.6023676
• Wurster, K. E., and H. W. Stone. 1993. “Aerodynamic Heating Environment Definition/thermal Protection System Selection for the HL-20.” Journal of Spacecraft and Rockets 30 (5). https://ntrs.nasa.gov/citations/19930069742
• Wyborny, W., and G. Requardt. 1975. “Gun Tunnel Free-Flight Model Test Calculation.” Journal of Spacecraft and Rockets 12 (2): 118–19. https://doi.org/10.2514/3.56956
• Xi, Ruiqing, and Jian Lan. 2017. “Joint Transfer Alignment and Fault Diagnosis of Inertial Navigation Network.” In 2017 20th International Conference on Information Fusion (Fusion). IEEE. https://doi.org/10.23919/icif.2017.8009817
• Xi, Liangliang, Jiale Li, and Ran An. 2023. “Research on Flight Test Evaluation Techniques for Unmanned Aircraft in Complex Environments.” In 2023 7th International Symposium on Computer Science and Intelligent Control (ISCSIC), vol. 41. IEEE. https://doi.org/10.1109/iscsic60498.2023.00069
• Xi, Wenxiong, Jian Liu, and Ren Mengfei. 2021. “Improvement of Mixing Efficiency in the Combustion Chamber of a Powder-Fuel Ramjet Engine.” Frontiers in Energy Research 9: 756905. https://doi.org/10.3389/fenrg.2021.756905
• Xi, Menghan, Lin Wu, Qianqian Li, et al. 2025. “Reference Composite Features Database Construction Method Based on Track Segmentation for Gravity Matching Aided Navigation.” ISA Transactions 159: 203–15. https://doi.org/10.1016/j.isatra.2025.01.046
• Xia, Bing, Tijing Cai, and Zhuopeng Yang. 2009. “Research and Simulation of a Fault Diagnosis and Tolerant Algorithm in Gravity Aided Inertial Navigation System.” In 2009 WRI Global Congress on Intelligent Systems. IEEE. https://doi.org/10.1109/gcis.2009.373
• Xia, Dunzhu, Lingchao Huang, and Liye Zhao. 2019. “A New Design of an MOEMS Gyroscope Based on a WGM Microdisk Resonator.” Sensors 19 (12): 2798. https://doi.org/10.3390/s19122798
• Xia, Xu, Ningfang Song, Tianze Wang, Jian Guo, Jingchao Ban, and Zhenpeng Wang. 2026. “A Bio-Inspired Multi-Scale Adaptive Particle Filter for Scalar Gravity Matching Navigation in GNSS-Denied Underwater Environments.” Biomimetics 11 (9): 651. https://doi.org/10.3390/biomimetics11090651
• Xia, Dunzhu, Bing Zhang, Hao Wu, and Tao Wu. 2020. “Optimization and Fabrication of an MOEMS Gyroscope Based on a WGM Resonator.” Sensors 20 (24): 7264. https://doi.org/10.3390/s20247264
• Xia Gang, Zhao You, and Wang Chang Hong. 2010. “A Rapid Calibration Scheme of Inertial Platform System Based on Navigation Algorithm.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633029
• Xian Lin Huang and Dong Ming Ge. 2010. “Robust and Anti-Windup Control of Air-Breathing Hypersonic Cruise Vehicle.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633123
• Xiang, Gang, Jing Miao, Langfu Cui, and Xiaoguang Hu. 2022a. “Intelligent Fault Diagnosis for Inertial Measurement Unit through Deep Residual Convolutional Neural Network and Short-Time Fourier Transform.” Machines 10 (10): 851. https://doi.org/10.3390/machines10100851
• Xiang, Biao, Zitong Shi, Tong Wen, and Hu Liu. 2025. “Attitude Stabilization Control of Three-Axis Inertial Stabilized Platform Using Magnetically Suspension System.” Measurement 253: 117858. https://doi.org/10.1016/j.measurement.2025.117858
• Xiang Li, Liu Yu, Su Baoku, and Jiang Xiaoxiong. 2008. “A Novel Nonlinear Filter for Initial Alignment in Strapdown Inertial Navigation System.” In 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2008.4776313
• Xiangming, Xing, V. V. Avrutov, and V. V. Meleshko. 2017. “Gyrocompassing Mode of the Strapdown Inertial Navigation System.” In 2017 IEEE 2nd Information Technology, Networking, Electronic and Automation Control Conference (ITNEC). IEEE. https://doi.org/10.1109/itnec.2017.8284753
• Xiao, Sheng-hong, and Shao-feng Bian. 2010. “Research on Regional Model of Continuous Fourier Series of Marine Magnetic Anomaly Field Using for the Geomagnetic Navigation.” In 2010 2nd International Conference on Industrial and Information Systems. IEEE. https://doi.org/10.1109/indusis.2010.5565746
• Xiao, Xuan, and Jianrui Lu. 2021. “Fault Detection and Isolation for Redundant Inertial Navigation System Based on Asymmetric Precision.” In 2021 4th International Conference on Robotics, Control and Automation Engineering (RCAE). IEEE. https://doi.org/10.1109/rcae53607.2021.9638917
• Xiao, Xuan, Jianrui Lu, Yuxuan Duan, Hanling Li, and Zhihong Deng. 2024a. “Asymmetric Dual Redundant Inertial Sensors: A Method for Fault Detection and Diagnosis.” IEEE Sensors Journal 24 (17): 28100–28110. https://doi.org/10.1109/jsen.2024.3425589
• Xiao, Yaqi, Xuanying Zhou, Jiongqi Wang, Zhangming He, and Haiyin Zhou. 2020. “Observability Analysis and Navigation Filter Optimization of High-Orbit Satellite Navigation System Based on GNSS.” Applied Sciences 10 (21): 7513. https://doi.org/10.3390/app10217513
• Xiaofang, Li, Mao Yuliang, Xie Ling, Chen Jiabin, and Song Chunlei. 2014. “Applications of Zero-Velocity Detector and Kalman Filter in Zero Velocity Update for Inertial Navigation System.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007449
• Xiaojiao Ma, Hongwei Liu, Di Xiao, and Hankui Li. 2009. “Key Technologies of Geomagnetic Aided Inertial Navigation System.” In 2009 IEEE Intelligent Vehicles Symposium. IEEE. https://doi.org/10.1109/ivs.2009.5164322
• Xiaonan Chen, Jingya Liu, Xuanming Pang, and Jiuhong Wang. 2011. “Research and Design of Ramcompressed Rotor for Rotary Ramjet Engine.” In 2011 Second International Conference on Mechanic Automation and Control Engineering. IEEE. https://doi.org/10.1109/mace.2011.5988400
• Xiaowei Shao and Changsheng Shao. n.d. “The Research of Fault-Detection Measure in the Redundant System with Inertial Measurement Unit on the Satellite.” In Proceedings of the 4th World Congress on Intelligent Control and Automation (Cat. No.02EX527), vol. 2. IEEE. https://doi.org/10.1109/wcica.2002.1020852
• Xiaoxia, Yang, and Huang Yi. 2006. “Systematic Calibration Method for the Laser Gyro Strapdown Inertial Navigation System.” In 2007 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.4347633
• Xie, Dan, Bin Dong, and Xingjian Jing. 2020. “Effect of Thermal Protection System Size on Aerothermoelastic Stability of the Hypersonic Panel.” Aerospace Science and Technology 106: 106170. https://doi.org/10.1016/j.ast.2020.106170
• Xie, Wen-zhong, Yan Ge, Hao Chen, Yu-fen Wen, and S. M. Guo. 2016. “Rapid Supersonic Performance Prediction for 2D Ramjet Inlets.” Aerospace Science and Technology 53: 220–31. https://doi.org/10.1016/j.ast.2016.03.025
• Xie, Jianbing, Yongcun Hao, and Weizheng Yuan. 2019a. “Energy Loss in a MEMS Disk Resonator Gyroscope.” Micromachines 10 (8): 493. https://doi.org/10.3390/mi10080493
• Xie, Fangtao, Yegao Qu, Wenming Zhang, Zhike Peng, and Guang Meng. 2019b. “Nonlinear Aerothermoelastic Analysis of Composite Laminated Panels Using a General Higher-Order Shear Deformation Zig-Zag Theory.” International Journal of Mechanical Sciences 150: 226–37. https://doi.org/10.1016/j.ijmecsci.2018.10.029
• Xie, Jietao, Juan Wu, and Yunda Zang. 2024. “Orientation Accuracy Test and Installation Error Calibration Technology for Vehicle Inertial Navigation System.” In 2024 4th International Conference on Electronic Information Engineering and Computer Science (EIECS). IEEE. https://doi.org/10.1109/eiecs63941.2024.10800389
• Xie, Jianbing, Jin Yang, and Jinqiu Zhou. 2018. “Vibrational Energy Loss Analysis of a MEMS Disk Resonator Gyroscope.” In 2018 IEEE/ASME International Conference on Advanced Intelligent Mechatronics (AIM). IEEE. https://doi.org/10.1109/aim.2018.8452237
• Xie, Yangfan, Xuebin Zhuang, Zepu Xi, and Hongbo Chen. 2021. “Dual-Channel and Bidirectional Neural Network for Hypersonic Glide Vehicle Trajectory Prediction.” IEEE Access 9: 92913–24. https://doi.org/10.1109/access.2021.3092515
• Xieyu, Xu, Cui Xiaoxi, Yu Wenbo, Luo Penghao, and Gao Mi. 2022. “Design of Missile Roll Autopilot Based on Linear Extended State Observer.” In 2022 34th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc55256.2022.10033507
• Xin, Lu, Hu Bai-qing, Zhang Guang-jun, and Xue Bo-yang. 2018. “Robust Sequential Kalman Filter for Inertial Integrated.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018644
• Xin Ma, S. Sukkarieh, and Jong-Hyuk Kim. 2003. “Vehicle Model Aided Inertial Navigation.” In Proceedings of the 2003 IEEE International Conference on Intelligent Transportation Systems, vol. 2. IEEE. https://doi.org/10.1109/itsc.2003.1252637
• Xing, Haifeng, Zhiyong Chen, Chengbin Wang, Meifeng Guo, and Rong Zhang. 2019b. “Quaternion-Based Complementary Filter for Aiding in the Self-Alignment of the MEMS IMU.” In 2019 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2019.8739728
• Xing, Haifeng, Zhiyong Chen, Xinxi Zhang, and Meifeng Guo. 2019a. “Observability Analysis of a Miniature Inertial Measurement Unit on a Continuous Rotating Base.” In 2019 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss46986.2019.8943758
• Xing, Xiaojun, Fenghao Li, Xiaoran Chen, Yilin Xun, Yiming Guo, and Qi Wei. 2020. “Research on the Inflation Process of the Drag Parachute in the Landing of First-Stage Booster and Its Key Parameters.” In 2020 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc49329.2020.9163957
• Xiong, Hao, Xingshu Wang, Jing Zhu, and Dongkai Dai. 2014. “Research on the Algorithm of Gravity Aided Inertial Navigation Based on CKF.” In 2014 12th International Conference on Signal Processing (ICSP). IEEE. https://doi.org/10.1109/icosp.2014.7015007
• Xiong, Ling, Lin Wei Xiao, Bin Bin Dan, and Jie Ma. 2013. “Full Tensor Gravity Gradient Aided Navigation Based on Nearest Matching Neural Network.” In 2013 Cross Strait Quad-Regional Radio Science and Wireless Technology Conference. IEEE. https://doi.org/10.1109/csqrwc.2013.6657455
• Xiong, Yufeng, Yu Zhang, Xiaoting Guo, et al. 2019. “Seamless Global Positioning System/inertial Navigation System Navigation Method Based on Square-Root Cubature Kalman Filter and Random Forest Regression.” Review of Scientific Instruments 90 (1): 015101. https://doi.org/10.1063/1.5079889
• Xiong, Hao, Yingwei Zhao, Xingshu Wang, Dongkai Dai, and Jiaxing Zheng. 2018a. “An Analysis of the Effect of Gravity Anomaly to Attitude Estimation in High-Precision GNSS/INS Integrated Navigation Systems under Overturning Cases.” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577185
• Xu, Da-Xin. 2005b. “Using Gravity Anomaly Matching Techniques to Implement Submarine Navigation.” Chinese Journal of Geophysics 48 (4): 886–91. https://doi.org/10.1002/cjg2.727
• Xu, Chenguang. 2021. “Temperature Drift Compensation of MEMS Inertial Sensor Based on IA-BP Algorithm.” In 2021 IEEE International Conference on Advances in Electrical Engineering and Computer Applications (AEECA). IEEE. https://doi.org/10.1109/aeeca52519.2021.9574304
• Xu, Jing, Kunlin Cheng, Chaolei Dang, et al. 2023b. “Performance Comparison of Liquid Metal Cooling System and Regenerative Cooling System in Supersonic Combustion Ramjet Engines.” Energy 275: 127488. https://doi.org/10.1016/j.energy.2023.127488
• Xu, Jingjing, Changhong Dong, and Lin Cheng. 2022b. “Deep Neural Network-Based Footprint Prediction and Attack Intention Inference of Hypersonic Glide Vehicles.” Mathematics 11 (1): 185. https://doi.org/10.3390/math11010185
• Xu, Ting-Xue, Qi Dong, Yong-Liang Zhang, and Ya-Wen Zhao. 2011. “The Research of Flight Reliability Evaluation of Missile.” In 2011 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering. IEEE. https://doi.org/10.1109/icqr2mse.2011.5976724
• Xu, Fan, and Jiancheng Fang. 2008. “Velocity and Position Error Compensation Using Strapdown Inertial Navigation System/celestial Navigation System Integration Based on Ensemble Neural Network.” Aerospace Science and Technology 12 (4): 302–7. https://doi.org/10.1016/j.ast.2007.08.005
• Xu, Chen, Chenggang Guan, Hui Lv, et al. 2026c. “Temperature Drift Error Compensation of Fiber Optic Gyroscope Based on CNN-BLSTM.” Optical Fiber Technology 102: 104768. https://doi.org/10.1016/j.yofte.2026.104768
• Xu, Haotian, Stephane Guerrier, Roberto Carlo Molinari, and Mucyo Karemera. 2019b. “Multivariate Signal Modeling with Applications to Inertial Sensor Calibration.” IEEE Transactions on Signal Processing 67 (19): 5143–52. https://doi.org/10.1109/tsp.2019.2935902
• Xu, Jian, Chenguang Guo, Yuewen Wang, Yong Xiao, and Xiaoxiang Hu. 2025c. “Fault-Tolerant Controller Design for Reusable Launch Vehicle.” Actuators 14 (11): 565. https://doi.org/10.3390/act14110565
• Xu, Jiangning, Hongyang He, Fangjun Qin, and Lubin Chang. 2017b. “A Novel Autonomous Initial Alignment Method for Strapdown Inertial Navigation System.” IEEE Transactions on Instrumentation and Measurement 66 (9): 2274–82. https://doi.org/10.1109/tim.2017.2692311
• Xu, Zewen, Yijia He, Hao Wei, and Yihong Wu. 2025b. “DOGE: An Extrinsic Orientation and Gyroscope Bias Estimation for Visual-Inertial Odometry Initialization.” In 2025 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra55743.2025.11127321
• Xu, Chen, Baoyin Hou, Ziqi Liao, and Lufeng Che. 2026a. “Implementation of a Digital Measurement and Control Circuit for Whole-Angle Mode Micro-Hemispherical Resonator Gyroscope Based on Zynq.” In 2026 International Conference on Electrical, Control and Information Technology (ECITech). IEEE. https://doi.org/10.1109/ecitech69277.2026.11601300
• Xu, Wenbiao, and Xuejing Lan. 2018. “Entry Trajectory Reconstruction for an Unpowered Reusable Launch Vehicle under the Change of Landing Field.” In 2018 10th International Conference on Modelling, Identification and Control (ICMIC). IEEE. https://doi.org/10.1109/icmic.2018.8529840
• Xu, Shenghong, Ruitao Li, and Wenjing Cao. 2014. “Research on Vehicle Inertial Navigation System Dynamic Correction Technology Based on Reference Object.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007510
• Xu, Xiaodong, Xiaowei Liu, and Yufeng Zhang. 2021a. “A Quick Start Method for MEMS Disk Resonant Gyroscope.” Sensors 21 (23): 7986. https://doi.org/10.3390/s21237986
• Xu, Qiaozhuang, Jie Lv, and Zhouzheng Gao. 2022c. “Evaluation on Low-Cost GNSS/IMU/Vision Integration System in GNSS-Denied Environments.” In 2022 IEEE 12th International Conference on Indoor Positioning and Indoor Navigation (IPIN). IEEE. https://doi.org/10.1109/ipin54987.2022.9918147
• Xu, Xin, Feng Shang, and Shuo Yang. 2022d. “Stainless Steel Stereo Inverted F Antenna Based on Missile Telemetry.” In 2022 14th International Conference on Measuring Technology and Mechatronics Automation (ICMTMA). IEEE. https://doi.org/10.1109/icmtma54903.2022.00116
• Xu, Zhi, and Shuo Tang. 2010. “RLV (Reusable Launch Vehicle) Reentry Nonlinear Controller Design.” In 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering. IEEE. https://doi.org/10.1109/cmce.2010.5610293
• Xu, Guoping, Weifeng Tian, and Li Qian. 2007a. “EMD- and SVM-Based Temperature Drift Modeling and Compensation for a Dynamically Tuned Gyroscope (DTG).” Mechanical Systems and Signal Processing 21 (8): 3182–88. https://doi.org/10.1016/j.ymssp.2007.05.006
• Xu, Shangcheng, Yi Wang, Zhenguo Wang, Xiaoqiang Fan, and Bing Xiong. 2022e. “Unsteady Behavior of Hypersonic Inlet Unstart Caused by High Angle of Attack.” Aerospace Science and Technology 130: 107884. https://doi.org/10.1016/j.ast.2022.107884
• Xu, Bo, Zhuofan Wen, Guoqing Zhang, and Peng Li. 2023a. “A Novel Fault Detection and Isolation Technology for Redundant Inertial Measurement Unit.” IEEE Transactions on Instrumentation and Measurement 72: 1–11. https://doi.org/10.1109/tim.2023.3284054
• Xu, Zeyuan, Boqi Xi, Guoxing Yi, and Danwei Wang. 2020b. “A Novel Model for Fully Closed-Loop System of Hemispherical Resonator Gyroscope under Force-to-Rebalance Mode.” IEEE Transactions on Instrumentation and Measurement 69 (12): 9918–30. https://doi.org/10.1109/tim.2020.3005282
• Xu, Zeyuan, Guoxing Yi, Meng Joo Er, and Chao Huang. 2019a. “Effect of Uneven Electrostatic Forces on the Dynamic Characteristics of Capacitive Hemispherical Resonator Gyroscopes.” Sensors 19 (6): 1291. https://doi.org/10.3390/s19061291
• Xu, Zeyuan, Guoxing Yi, Ziyang Qi, Chao Huang, and Haibin Fang. 2016b. “Structural Optimization Research on Hemispherical Resonator Gyro Based on Finite Element Analysis.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554253
• Xu, Zeyuan, Guoxing Yi, and Weidong Zhu. 2022a. “An Accurate Thermoelastic Model and Thermal Output Error Analysis of a Hemispherical Resonator Gyroscope under Varying Temperatures.” Mechanical Systems and Signal Processing 170: 108760. https://doi.org/10.1016/j.ymssp.2021.108760
• Xu, Xiaobin, Chunxi Zhang, and Jingming Song. 2009. “Bias Error Caused by Broad-Spectrum Source and Birefringence Effect in Fiber Optical Gyroscope.” Optik 120 (14): 726–30. https://doi.org/10.1016/j.ijleo.2008.03.002
• Xu, DaFu, Zhe Zhang, Ke Wu, et al. 2016a. “Recent Progress on Development Trend and Key Technologies of Vertical Take-off Vertical Landing Reusable Launch Vehicle.” Chinese Science Bulletin 61 (32): 3453–63. https://doi.org/10.1360/n972016-00537
• Xu, Chun, Qiancheng Zhao, and Jian Cui. 2025d. “Phase Compensation Method for the Drive Loop of MEMS Gyroscope Based on Dual Phase-Locked Loop Synchronous Tracking.” In 2025 IEEE 38th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems61431.2025.10917773
• Xu, Wangqiang, Rong Zhao, and Lixin Wang. 2017a. “Adjustment Method of Automatic Carrier Landing System Design Criterion for Scaled Model Aircraft.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028367
• Xu, Yun, and Tong Zhou. 2018. “Research on in-Flight Alignment for Micro Inertial Navigation System Based on Changing Acceleration Using Exponential Function.” Micromachines 10 (1): 24. https://doi.org/10.3390/mi10010024
• Xu Mingliang, Liu Luhua, Tang Guojian, and Chen Kejun. 2010. “Study on Guidance Approaches of Hypersonic Glide-Cruise Vehicle during Cruise and Attack Phases.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633205
• Xudan, Jin, Mao Zheng, Wei Fuling, and Wang Yali. 2007. “Research on Gyroscope Free Strapdown Inertial Navigation System Based on 3-Axis Accelerometer.” In 2007 8th International Conference on Electronic Measurement and Instruments. IEEE. https://doi.org/10.1109/icemi.2007.4350617
• Xudong Yu, Wen Lei, Zhenfang Fan, and Guangfeng Lu. 2016. “A Miniature Low Cost Ring Laser Gyroscope Inertial Measurement Unit.” In 2016 6th IEEE International Conference on Control System, Computing and Engineering (ICCSCE). IEEE. https://doi.org/10.1109/iccsce.2016.7893536
• Xue, Shiqin. 2026. “Design of an Online Compensation Model for Inertial Navigation Error Based on Deep Learning Enhancement.” In 2026 6th Asia-Pacific Conference on Communications Technology and Computer Science (ACCTCS). IEEE. https://doi.org/10.23919/acctcscps00012.2026.00052
• Xue, Kong, Ning Guodong, Yang Ming, and Wang Songyan. 2018. “A Maneuvering Penetration Strategy via Integrated Flight/propulsion Guidance and Control Method for Air-Breathing Hypersonic Vehicle.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018943
• Yaakov, Arazi, and Jose Luis Gruver. 2016. “Dynamic Hysteresis Calibration Algorithm for Inertial Grade Accelerometers.” In 2016 IEEE International Symposium on Inertial Sensors and Systems. IEEE. https://doi.org/10.1109/isiss.2016.7435567
• Yadav, Anup Lal, and Sandip Kumar Goyal. 2025. “A Sensitive Collision Avoidance System Improved for Terrain Navigation on Elevated Terrain.” In 2025 2nd International Conference on Computational Intelligence, Communication Technology and Networking (CICTN). IEEE. https://doi.org/10.1109/cictn64563.2025.10932625
• Yahalom, Ram, Behzad Moslehi, Levy Oblea, Vahid Sotoudeh, and J. C. Ha. 2010. “Low-Cost, Compact Fiber-Optic Gyroscope for Super-Stable Line-of-Sight Stabilization.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507131
• Yamamoto, Jun, Yoimi Kojima, Masaharu Kameda, Yasushi Watanabe, Atsushi Hashimoto, and Takashi Aoyama. 2020. “Prediction of the Onset of Supersonic Inlet Buzz.” Aerospace Science and Technology 96: 105523. https://doi.org/10.1016/j.ast.2019.105523
• Yampolsk, Zeev, and Itzik Klein. 2024. “Data-Driven Gyroscope Calibration.” In 2024 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa62769.2024.10786045
• Yampolsky, Zeev, and Itzik Klein. 2025. “AI-Aided Inertial Sensor.” In 2025 DGON Inertial Sensors and Applications (ISA). IEEE. https://doi.org/10.1109/isa67150.2025.11279319
• Yan, Rongyi, and Maoyin Chen. 2013. “Fault Detection Based on Distributed Redundant Sensors.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561668
• Yan, Pengpeng, Yonghua Fan, Zhe Liu, and Jin Zhang. 2017a. “The Dual Decoupling Fusion Control Design for the Lateral Motion of Hypersonic Glide Vehicle.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027935
• Yan, Huang, Li Shanshan, Zhou Chuyuan, et al. 2023b. “Research and Construction of a Global Hexagonal Marine Gravity Gradient Reference Map for Navigation.” Geofluids 2023: 1–22. https://doi.org/10.1155/2023/4141572
• Yan, Tingyang, Min Su, Lili Huang, and Shunru Zhang. 2023c. “Temperature Compensation for Fiber Optic Gyroscope Based on Bayesian Optimized Relevance Vector Regression.” In 2023 3rd International Conference on Electrical Engineering and Mechatronics Technology (ICEEMT). IEEE. https://doi.org/10.1109/iceemt59522.2023.10262994
• Yan, Kaichen, Xiaoxu Wang, Tianliang Qu, et al. 2026a. “Forgetting Filter-Based Real-Time Identification and Compensation of Whole-Angle Hemispherical Resonator Gyroscope Errors for Extensive Aerospace Applications.” Aerospace Science and Technology 168: 111283. https://doi.org/10.1016/j.ast.2025.111283
• Yan, Kaichen, Xiaoxu Wang, Chao Wang, et al. 2026b. “Modeling, Characterization, and Compensation of Detection Errors for Differential Frequency Modulation Whole-Angle Hemispherical Resonator Gyroscope.” IEEE Transactions on Instrumentation and Measurement 75: 1–13. https://doi.org/10.1109/tim.2026.3682829
• Yan, Kaichen, Xiaoxu Wang, Kang Zou, et al. 2024. “Self-Excitation Enabled Decoupling, Calibration, and Compensation of Errors for Whole-Angle Hemispherical Resonator Gyroscope.” IEEE Transactions on Instrumentation and Measurement 73: 1–13. https://doi.org/10.1109/tim.2023.3346525
• Yan, Xia, Chen Wenjie, and Peng Wenhui. 2013. “Research on Random Drift Modeling and a Kalman Filter Based on the Differential Signal of MEMS Gyroscope.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561504
• Yan Binbin, Lu Cunkan, Yu Weiwei, and Yan Jie. 2009. “Fuzzy CMAC Control Design for an Airbreathing Hypersonic Cruise Vehicle.” In 2009 4th IEEE Conference on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/iciea.2009.5138209
• Yan-zhu, Liu, and Xue Yun. 2004. “Drift Motion of Free-Rotor Gyroscope with Radial Mass-Unbalance.” Applied Mathematics and Mechanics 25 (7): 786–91. https://doi.org/10.1007/bf02437570
• Yanagihara, Masaaki, Masashi Shigemi, and Takanobu Suito. 1999. “Estimating Aerodynamic Characteristics of Automatic Landing Flight Experiment Vehicle Using Flight Data.” Journal of Aircraft 36 (6): 926–33. https://doi.org/10.2514/2.2553
• Yang, Feng, Ziheng Cheng, and Chengyu Zhao. 2026d. “Intelligent Trajectory Generation Method for Hypersonic Glide Vehicles Based on RBF Neural Networks.” Aerospace 13 (5): 477. https://doi.org/10.3390/aerospace13050477
• Yang, Haibing, Jian Cui, and Qiancheng Zhao. 2020b. “A Wheeled Horizontal Dual-Axis MEMS Gyroscope Based on Single Proof Mass with Mechanical Coupling Suppression Silicon Gratings.” In 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems46641.2020.9056355
• Yang, Bo, Bo Dai, Xiaojun Liu, Lu Xu, Yunpeng Deng, and Xingjun Wang. 2014. “The on-Chip Temperature Compensation and Temperature Control Research for the Silicon Micro-Gyroscope.” Microsystem Technologies 21 (5): 1061–72. https://doi.org/10.1007/s00542-014-2271-z
• Yang, Yuzheng, and Juntao Fei. 2013. “Adaptive Neural Sliding Mode Compensator for MEMS Gyroscope.” In 2013 10th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2013.6564894
• Yang, Ting, Yinghao Guan, Pengming Wang, et al. 2026e. “KE-DDPM: Kinematics-Enhanced Denoising Diffusion Probabilistic Model for Inertial Measurement Unit Anomaly Detection.” In 2026 IEEE International Instrumentation and Measurement Technology Conference (I2MTC). IEEE. https://doi.org/10.1109/i2mtc66907.2026.11694786
• Yang, Bainan, Qiqin Hu, Kaixin Luo, Xiaoyu Xie, and Juliang Cao. 2025b. “Impact of Deflection of Vertical on the Attitude of Strapdown Inertial Navigation System on a Swaying Base.” In 2025 44th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc64809.2025.11178340
• Yang, Bo, Qiuxia Hu, and Hanmei Wang. 2009b. “Research of Integrative GNC Design Simulation for Cruise Missile.” In 2009 Third International Conference on Genetic and Evolutionary Computing. IEEE. https://doi.org/10.1109/wgec.2009.88
• Yang, Yulin, and Guoquan Huang. 2018. “Aided Inertial Navigation with Geometric Features: Observability Analysis.” In 2018 IEEE International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2018.8460670
• Yang, Yulin, and Guoquan Huang. 2019. “Aided Inertial Navigation: Unified Feature Representations and Observability Analysis.” In 2019 International Conference on Robotics and Automation (ICRA). IEEE. https://doi.org/10.1109/icra.2019.8793507
• Yang, Jisan, Jie Jiang, Lingfeng Tian, and Guangjun Zhang. 2022c. “Joint Estimation of Stellar Atmospheric Refraction and Star Tracker Attitude.” IEEE Transactions on Instrumentation and Measurement 71: 1–12. https://doi.org/10.1109/tim.2021.3135343
• Yang, Zhihuai, Xiaojun Jin, Huilian Ma, and Zhonghe Jin. 2009a. “CORDIC Algorithm Based Digital Detection Technique Applied in Resonator Fiber Optic Gyroscope.” Optical Fiber Technology 15 (3): 328–31. https://doi.org/10.1016/j.yofte.2009.02.004
• Yang, Yanhao, Joe Khalife, Joshua J. Morales, and Zaher M. Kassas. 2022d. “UAV Waypoint Opportunistic Navigation in GNSS-Denied Environments.” IEEE Transactions on Aerospace and Electronic Systems 58 (1): 663–78. https://doi.org/10.1109/taes.2021.3103140
• Yang, Yanyu, Hansen Li, Ping Jia, and Yong Wang. 2016b. “RISE-Based Tracking Control of Inertial Stabilized Platform with Extended Disturbance Observer.” In 2016 12th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2016.7505349
• Yang, Hai, Wei Li, Chengming Luo, Jinyao Zhang, and Zhuoyin Si. 2016a. “Research on Error Compensation Property of Strapdown Inertial Navigation System Using Dynamic Model of Shearer.” IEEE Access 4: 2045–55. https://doi.org/10.1109/access.2016.2565638
• Yang, Gongliu, Yuanyuan Liu, Ming Li, and Shunguang Song. 2015. “AMA- and RWE- Based Adaptive Kalman Filter for Denoising Fiber Optic Gyroscope Drift Signal.” Sensors 15 (10): 26940–60. https://doi.org/10.3390/s151026940
• Yang, Yuan, Ying Liu, Yanghong Liu, and Xiaodong Zhao. 2019. “Temperature Compensation of MEMS Gyroscope Based on Support Vector Machine Optimized by GA.” In 2019 IEEE Symposium Series on Computational Intelligence (SSCI). IEEE. https://doi.org/10.1109/ssci44817.2019.9003139
• Yang, Jie, Pengbin Ma, and Nan Ye. 2020a. “A SINS Multi-Azimuth Alignment Method without Initial Location Parameters.” In 2020 39th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc50068.2020.9188612
• Yang, Donguk Max, Khalil Najafi, David F. Lemmerhirt, and Jay Mitchell. 2018c. “A Micro Thermal and Stress Isolation Platform for Inertial Sensors.” In 2018 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/isiss.2018.8358149
• Yang, Xiao-Dong, and Wen-Ming Shi. 2018. “Two-Point Calibration Accuracy Analysis Model of Inertial Navigation System.” In 2018 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2018.8484554
• Yang, Hang, Dingjie Wang, Hongbo Zhang, and Xu Yan. 2026a. “Autonomous Strapdown Inertial/Refractive Celestial Integrated Navigation Using Dual-Band Stellar Refraction Observations.” IEEE Transactions on Aerospace and Electronic Systems 62: 2900–2912. https://doi.org/10.1109/taes.2025.3642818
• Yang, Shu-zi, Wen-zhong Xie, Jiang-dong Pan, and Xiao-tao Tian. 2025c. “On the Evolution of the Unstart Flow during the Variable Angle-of-Attack Process of a Two-Dimensional Hypersonic Inlet.” Acta Astronautica 236: 599–615. https://doi.org/10.1016/j.actaastro.2025.07.024
• Yang, Xiaokang, Gongmin Yan, Fan Liu, Bofan Guan, and Sihai Li. 2022a. “Analysis Method of Strapdown Inertial Navigation Error Distribution Based on Covariance Matrix Decomposition.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9902729
• Yang, Mengni, Bo Yang, Guoqing Dai, Puchun Wang, Zhaozi Zu, and Zhongjun Qu. 2026f. “Non-Cooperative Target Measurement and Localization Based on Monocular Vision and Fixed-Wing Aircraft Height in Autonomous Landing Runway Scenarios.” Measurement 258: 118993. https://doi.org/10.1016/j.measurement.2025.118993
• Yang, Xiancheng, Ming Zhang, Peihui Yan, Qu Wang, Dongpeng Xie, and Yuntian Brian Bai. 2025a. “Cross-Path Planning of UAV Cluster Low-Altitude Flight Based on Inertial Navigation Combined with GPS Localization.” Electronics 14 (14): 2877. https://doi.org/10.3390/electronics14142877
• Yang, Wenhui, Xin Zhao, Jinhao Song, and Yong Li. 2026c. “Global Observability Analysis of Rotational MEMS Inertial Navigation System for Land Vehicle Applications.” Sensors 26 (9): 2599. https://doi.org/10.3390/s26092599
• YangZhou, ChenYunxia, and KangRui. 2011. “A Study of Aircraft Landing Gear Testing System on PHM.” In 2011 Prognostics and System Health Managment Confernece. IEEE. https://doi.org/10.1109/phm.2011.5939549
• Yanling Hao, Jing Gong, Wei Gao, and Liang Li. 2008. “Research on the Dynamic Error of Strapdown Inertial Navigation System.” In 2008 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2008.4798862
• Yao, Pengchao, Gongliu Yang, Xiafu Peng, and Jincheng Peng. 2024. “An Initial Alignment Algorithm Based on RSKF Single-Axis Rotational Inertial Navigation System.” IEEE Sensors Journal 24 (19): 30749–57. https://doi.org/10.1109/jsen.2024.3407063
• Yasue, Kanako. 2020. “Extraction of Monophasic Data from Flight Test Data via Cluster Analysis.” Journal of Aircraft 57 (3): 399–407. https://doi.org/10.2514/1.c035564
• Yates, John E., and Edmond F. E. Zeydel. 1963. “Unsteady Aerodynamic Forces on Slender Supersonic Aircraft with Flexible Wings and Bodies.” AIAA Journal 1 (2): 350–53. https://doi.org/10.2514/3.1536
• Yavuz, Ahmet Faruk, Kivanc Azgin, Gokhan Karapistik, et al. 2025. “Cost-Effective Metallic Hemispherical Resonator Gyroscope.” In 2025 Joint Conference of the European Frequency and Time Forum and IEEE International Frequency Control Symposium (EFTF/IFCS). IEEE. https://doi.org/10.1109/eftf/ifcs64367.2025.11194539
• Yavuz, Ahmet Faruk, Kivanc Azgin, Gokhan Karapistik, et al. 2026. “Design and Characterization of a Cost-Effective Metallic Hemispherical Resonator Gyroscope.” In 2026 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial69196.2026.11557915
• Ye, Jiangnan, Lei Wang, Hao Han, Zhi Zhan, and Lin Yan. 2023. “Alignment Scheme Optimization When Gyro Accuracy Inconsistency for Inertial Navigation System.” Measurement 216: 112893. https://doi.org/10.1016/j.measurement.2023.112893
• Ye, Kun, Zhengyin Ye, Zhenghao Feng, Yekai Pan, and Gang Wang. 2019b. “Numerical Investigation on the Aerothermoelastic Deformation of the Hypersonic Wing.” Acta Astronautica 160: 76–89. https://doi.org/10.1016/j.actaastro.2019.04.028
• Ye, Kun, Zhengyin Ye, Chunna Li, and Jie Wu. 2019a. “Effects of the Aerothermoelastic Deformation on the Performance of the Three-Dimensional Hypersonic Inlet.” Aerospace Science and Technology 84: 747–62. https://doi.org/10.1016/j.ast.2018.11.015
• Yeon Fuh Jiang and Yu Ping Lin. 1991. “Error Analysis of Quaternion Transformations (Inertial Navigation).” IEEE Transactions on Aerospace and Electronic Systems 27 (4): 634–39. https://doi.org/10.1109/7.85036
• Yi, Zhang, Dong Chun, and Yu Chunmei. 2014a. “An Approach of Misalignment Self-Inspect for Missile’s Inertial Platform.” In 2014 International Conference on Mechatronics and Control (ICMC). IEEE. https://doi.org/10.1109/icmc.2014.7231975
• Yi, Guo, and Carles Ferrer. 2007. “IMS/GPS Integration with a Novel Real-Time System Platform for Inertial Data Estimation.” In EUROCON 2007 - The International Conference on “Computer as a Tool”. IEEE. https://doi.org/10.1109/eurcon.2007.4400366
• Yi, Hu, and Chen Wanchun. 2014. “Trajectory Optimization of a Cruise Missile Using the Gauss Pseudospectral Method.” In The 26th Chinese Control and Decision Conference (2014 CCDC). IEEE. https://doi.org/10.1109/ccdc.2014.6852247
• Yi, Guoxing, Yangguang Xie, Changhong Wang, Ziyang Qi, and Zhen Fang. 2014b. “Modeling of Hemispherical Resonator Gyro Resonator Deformation under Acceleration.” In The 26th Chinese Control and Decision Conference (2014 CCDC). IEEE. https://doi.org/10.1109/ccdc.2014.6852382
• Yi-Fei, Zhang, and Yang Hui. 2018. “Study on Guidance Algorithm of Scene Matching Based on Different Source Images for Cruise Missile.” In 2018 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2018.8484583
• Yichie, Eldad., Ido. Peleg, Ronen. Maimon, et al. 2025. “Tuning Fork Vibratory MEMS Gyroscope with Optical Drive and Sense Modes Detection.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11037187
• Yigit, Hikmet, and Guray Yilmaz. 2012. “Development of a GPU Accelerated Terrain Referenced UAV Localization and Navigation Algorithm.” Journal of Intelligent & Robotic Systems 70 (1–4): 477–89. https://doi.org/10.1007/s10846-012-9735-0
• Yijie Dai, Li Xing, Zhi Xiong, Rong Wang, and Zhong Wan. 2016. “The Error Correction Method of the Inertial Altitude Based on Air Data.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828992
• Yin, Hang, and Lei Wang. 2018. “Effect of Compressive Sensing Star Image on Attitude Determination.” In 2018 10th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC). IEEE. https://doi.org/10.1109/ihmsc.2018.10108
• Yin, Tao, Huanming Wu, Qisong Wu, Haigang Yang, and Jiwei Jiao. 2011. “A TIA-Based Readout Circuit with Temperature Compensation for MEMS Capacitive Gyroscope.” In 2011 6th IEEE International Conference on Nano/Micro Engineered and Molecular Systems. IEEE. https://doi.org/10.1109/nems.2011.6017377
• Ying, Yuhang, Qiang Zhu, and Zheng Chen. 2025. “A Physics-Informed Neural Network Enhanced Kalman Filter Method for Inertial Navigation of Remotely Operated Vehicles.” IFAC-PapersOnLine 59 (30): 485–90. https://doi.org/10.1016/j.ifacol.2025.12.284
• Ying Kun Peng and M. F. Golnaraghi. 2004. “A Vector-Based Gyro-Free Inertial Navigation System by Integrating Existing Accelerometer Network in a Passenger Vehicle.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308999
• Yinqiang Zhang, ShouRong Wang, and Dunzhu Xia. 2010. “EMD-Based Denoising Methods in the MEMS Gyroscope De-Drift.” In 2010 IEEE 5th International Conference on Nano/Micro Engineered and Molecular Systems. IEEE. https://doi.org/10.1109/nems.2010.5592471
• Yoneyama, T., and Y. Mushiake. 1965. “Scintillation Fading in Line-of-Sight Propagation through a Statistically Anisotropic Turbulent Medium.” IEEE Transactions on Antennas and Propagation 13 (3): 476–77. https://doi.org/10.1109/tap.1965.1138425
• Yong, Luo, Yin Hongliang, Hao Qiang, and Wu Zuo-Cheng. 2023. “Research on Multi-Inertial Navigation Information Fusion Method Based on Kalman Filter.” In 2023 IEEE 11th International Conference on Computer Science and Network Technology (ICCSNT). IEEE. https://doi.org/10.1109/iccsnt58790.2023.10334559
• Yong, Shangguan, Chen Jiabin, Song Chunlei, and Han Yongqiang. 2015. “Research on the Compensation in MEMS Gyroscope Random Drift Based on Time-Series Analysis and Kalman Filtering.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7259955
• Yong Jia, Suilao Li, and Yefeng Xu. 2016. “Analysis and Compensation of Rotating Shaft Fluctuation on Rotation Inertial Navigation System.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828855
• Yongqiang, Han, Chen Jiabin, Tian Xiaochun, and Li Nan. 2015. “A Robust Data Driven Error Damping Method for Inertial Navigation System Based on Unfalsified Adaptive Control.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260492
• Yoo, Y. M., W. H. Lee, S. M. Lee, C. G. Park, and J. H. Kwon. 2012. “Improvement of TERCOM Aided Inertial Navigation System by Velocity Correction.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236851
• Yoo, Young Min, and Chan Gook Park. 2015. “Improvement of Terrain Referenced Navigation Using a Point Mass Filter with Grid Adaptation.” International Journal of Control, Automation and Systems 13 (5): 1173–81. https://doi.org/10.1007/s12555-013-0410-4
• Yu, Fei, Yueyang Ben, Qian Li, and Wei Gao. 2008. “Optimal Two-Position Alignment for Strapdown Inertial Navigation System.” In 2008 International Conference on Intelligent Computation Technology and Automation (ICICTA). IEEE. https://doi.org/10.1109/icicta.2008.162
• Yu, Ming Jui, and Dennis S. Bernstein. 2016. “Combined State and Parameter Estimation and Identifiability of State Space Realizations.” In 2016 IEEE 55th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2016.7798726
• Yu, Daren, Juntao Chang, Wen Bao, and Zongxia Xie. 2007. “Optimal Classification Criterions of Hypersonic Inlet Start/Unstart.” Journal of Propulsion and Power 23 (2): 310–16. https://doi.org/10.2514/1.24640
• Yu, Fei, Shiwei Fan, Ya Zhang, Pengfei Wu, and Jiachong Chang. 2017. “Compensation Method for Temperature Error of Fiber Optic Gyroscope Based on Support Vector Machine.” In 2017 Forum on Cooperative Positioning and Service (CPGPS）. IEEE. https://doi.org/10.1109/cpgps.2017.8075090
• Yu, Huapeng, Yanli Geng, Hai Zhu, Nuan Jiang, and Jianhua Chen. 2016a. “A Novel Filtering Model for DVL Aided Inertial Navigation System Based on Observability Degree Analysis.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828765
• Yu, Daocheng, and Cheinway Hwang. 2022. “Calibrating Error Variance and Scaling Global Covariance Function of Geoid Gradients for Optimal Determinations of Gravity Anomaly and Gravity Gradient from Altimetry.” Journal of Geodesy 96 (9): 61. https://doi.org/10.1007/s00190-022-01647-4
• Yu, H., X. Jin, X. H. Liu, et al. 2022b. “Pose Error Identification Algorithm Based on Hemispherical Resonant Gyroscope Assembly Capacitance Uniformity.” Measurement 198: 111426. https://doi.org/10.1016/j.measurement.2022.111426
• Yu, Haesung, Inseop Lee, Juhyun Oh, Chang-Ky Sung, TaeGyoo Lee, and Cheonjoong Kim. 2025c. “Performance Improvement of an Inertial Navigation System Based on FOG and SA Using a Two-Step Indirect Calibration Method.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11036733
• Yu, Jianqiao, Guanchen Luo, and Yuesong Mei. 2011. “Surface-to-Air Missile Autopilot Design Using LQG/LTR Gain Scheduling Method.” Chinese Journal of Aeronautics 24 (3): 279–86. https://doi.org/10.1016/s1000-9361(11)60033-2
• Yu, Jianqiao, Guan-chen Luo, and Wentao Yin. 2010a. “Missile Robust Gain Scheduling Autopilot Design Using Full Block Multipliers.” Journal of Systems Engineering and Electronics 21 (5): 883–91. https://doi.org/10.3969/j.issn.1004-4132.2010.05.024
• Yu, Wenbin, Pin Lyu, Xiyue Huan, and Jizhou Lai. 2023b. “Dynamic Adaptive Attitude Estimation Method Based on Inertial Sensor.” In 2023 6th International Symposium on Autonomous Systems (ISAS). IEEE. https://doi.org/10.1109/isas59543.2023.10164404
• Yu, Shutian, Xinyue Ni, Xiaoyan Li, Tingliang Hu, and Fansheng Chen. 2022c. “Real-Time Dynamic Optimized Band Detection Method for Hypersonic Glide Vehicle.” Infrared Physics & Technology 121: 104020. https://doi.org/10.1016/j.infrared.2022.104020
• Yu, Sheng, Xuezhong Wu, Yongmeng Zhang, Jiangkun Sun, and Dingbang Xiao. 2024. “A Fast Start Method for Whole-Angle Micro-Shell Resonator Gyroscope.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10784714
• Yu, Zhihao, Libin Zeng, Changda Xing, Lituo Shang, Xiuyue Yan, and Jingyu Li. 2025a. “Comparative Noise Analysis of Readout Circuit in Hemispherical Resonator Gyroscope.” Micromachines 16 (7): 802. https://doi.org/10.3390/mi16070802
• Yu, Xiang, Wenjuan Zhang, Yongjun Yang, Haifeng Lin, and Zhilin Wu. 2026. “Autocorrelation-Based Adaptive Kalman Filtering for Metrological Stabilization of MEMS Gyroscope Signals under Temperature Drift and Broadband Random Vibration.” Measurement 289: 122657. https://doi.org/10.1016/j.measurement.2026.122657
• Yuan, Mengfan, Zhongliang Deng, Guoqing Xu, and Pengqiang Xie. 2025a. “A Bayesian Optimized TCN-LSTM Hybrid Network for Inertial Sensor Error Correction.” In 2025 4th International Conference on Electronic Information Technology (EIT). IEEE. https://doi.org/10.1109/eit67313.2025.11232125
• Yuan, Shuai, Zhanpeng Gao, and Wenjun Yi. 2026a. “Piecewise Nonsingular Practical Prescribed-Time Control for Three-Dimensional Skip-Trajectory Tracking of Hypersonic Glide Vehicles.” Aerospace 13 (8): 705. https://doi.org/10.3390/aerospace13080705
• Yuan, Cheng, Jizhou Lai, Pin Lyu, Peng Shi, Wei Zhao, and Kai Huang. 2018. “A Novel Fault-Tolerant Navigation and Positioning Method with Stereo-Camera/Micro Electro Mechanical Systems Inertial Measurement Unit (MEMS-IMU) in Hostile Environment.” Micromachines 9 (12): 626. https://doi.org/10.3390/mi9120626
• Yuan, Chengzhi, Yang Liu, Fen Wu, and Chang Duan. 2016. “Hybrid Switched Gain-Scheduling Control for Missile Autopilot Design.” Journal of Guidance, Control, and Dynamics 39 (10): 2352–63. https://doi.org/10.2514/1.g001791
• Yuan, Zhen-Dong, and Lennart Ljung. 1984. “Black-Box Identification of Multivariable Transfer Functions—Asymptotic Properties and Optimal Input Design.” International Journal of Control 40 (2): 233–56. https://doi.org/10.1080/00207178408933270
• Yuan, Zhen-Dong, and Lennart Ljung. 1985. “Unprejudiced Optimal Open Loop Input Design for Identification of Transfer Functions.” Automatica 21 (6): 697–708. https://doi.org/10.1016/0005-1098(85)90043-3
• Yuan, Zhou, Yan Lu, Zhang Jinyun, and Yu Pei. 2015. “Specific Azimuth Self-Calibration of PIGA of Inertial Platform System.” In 2015 IEEE 28th Canadian Conference on Electrical and Computer Engineering (CCECE). IEEE. https://doi.org/10.1109/ccece.2015.7129201
• Yuan, Zhou, and Wang Ting. 2018. “A Method of Coarse Alignment for FOG Based Inertial Platform System Using Rotation Modulation.” In 2018 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2018.8407883
• Yuan, Lishan, Ning Wang, Ronghao Xie, Zhennan Wei, Qingshuang Zeng, and Changhong Wang. 2024c. “Study on the Mechanism of Energy Dissipation in Hemispherical Resonator Gyroscope.” Sensors 25 (1): 74. https://doi.org/10.3390/s25010074
• Yuan, Lishan, Zhennan Wei, Ning Wang, Ronghao Xie, and Qingshuang Zeng. 2024b. “Research on the Influence of Assembly Error of Hemispherical Resonator Gyroscope on Frequency Splitting.” In 2024 3rd International Conference on Advanced Sensing, Intelligent Manufacturing (ASIM). IEEE. https://doi.org/10.1109/asim66270.2024.00026
• Yuan, Chengzhi, and Fen Wu. 2016. “A New Hybrid LFT Control Method for Missile Autopilot Design.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554273
• Yuan-Hsi Cheng and J. C. Hung. 1991. “On the Control of the Inertial Platform for a Satellite Launch Vehicle Having Large Attitude Angles.” In Proceedings of the IEEE 1991 National Aerospace and Electronics Conference NAECON 1991. IEEE. https://doi.org/10.1109/naecon.1991.165778
• Yuanxin Wu, Xiaoping Hu, Meiping Wu, and Dewen Hu. 2004. “Error Analysis of Strapdown Inertial Navigation Using Dual Quaternion Algebra.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1309002
• Yue, Shuai, Qing Lin, Guang Zheng, and Zhonghua Du. 2022b. “Modeling and Experimental Validation of Vertical Landing Reusable Launch Vehicle under Symmetric Landing Conditions.” Chinese Journal of Aeronautics 35 (12): 156–72. https://doi.org/10.1016/j.cja.2022.06.022
• Yue, Shuai, Branislav Titurus, Zhiqian Li, Chunbo Wu, and Zhonghua Du. 2022a. “Analysis of Liquid Spring Damper for Vertical Landing Reusable Launch Vehicle with Network-Based Methodology.” Nonlinear Dynamics 111 (3): 2135–60. https://doi.org/10.1007/s11071-022-07944-z
• Yue, Shuai, Branislav Titurus, Hong Nie, and Ming Zhang. 2019. “Liquid Spring Damper for Vertical Landing Reusable Launch Vehicle under Impact Conditions.” Mechanical Systems and Signal Processing 121: 579–99. https://doi.org/10.1016/j.ymssp.2018.11.034
• Yue, Zhe, Mengshuo Zhang, Wenzhuo Ma, Wei Ding, Kezhao Li, and Chengkai Tang. 2026. “Adaptive State-Constrained Vehicle Navigation and Positioning in GNSS-Denied Environments.” IEEE Sensors Journal 26 (3): 4922–37. https://doi.org/10.1109/jsen.2025.3648759
• Yueh, John H. 1956. “A Developmental Approach to Reliability in Missile System Equipment.” IRE Transactions on Reliability and Quality Control PGRQC-8: 44–54. https://doi.org/10.1109/ire-pgrqc.1956.6540349
• Yufei, Liu, and Cui Pingyuan. 2006. “Observability Analysis of Deep-Space Autonomous Navigation System.” In 2006 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.280969
• Yuksel, Y., and H. B. Kaygisiz. 2006. “Analysis of Vision Aided Inertial Navigation Systems.” In 2006 IEEE 14th Signal Processing and Communications Applications. IEEE. https://doi.org/10.1109/siu.2006.1659722
• Yun, Se Hyun, Wonhee Lee, and Chan Gook Park. 2014. “Covariance Calculation for Batch Processing Terrain Referenced Navigation.” In 2014 IEEE/ION Position, Location and Navigation Symposium - PLANS 2014. IEEE. https://doi.org/10.1109/plans.2014.6851435
• Yun, Sukchang, Young Jae Lee, and Sangkyung Sung. 2013. “IMU/Vision/Lidar Integrated Navigation System in GNSS Denied Environments.” In 2013 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2013.6497403
• Yunhai, Geng, Wang Shuang, and Chen Binglong. 2012. “Calibration for Star Tracker with Lens Distortion.” In 2012 IEEE International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2012.6283224
• Yuta Akai, Kenji Uchiyama, Akio Abe, and Yuzo Shimada. 2007. “Automatic Landing System for Spaceplane Based on Model Predictive Control Using State Mapping.” In 2007 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2007.4406924
• Yuyan, Tang, and Huang Peikang. 2006. “Boost-Phase Ballistic Missile Trajectory Estimation with Ground Based Radar.” Journal of Systems Engineering and Electronics 17 (4): 705–8. https://doi.org/10.1016/s1004-4132(07)60001-2
• Zachariah, Dave, and Magnus Jansson. 2010. “Camera-Aided Inertial Navigation Using Epipolar Points.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507246
• Zaeim, R., M. A. Nekoui, and A. Zaeim. 2010. “Integration of Imaging Seeker Control in a Visually Guided Missile.” In IEEE Icca 2010. IEEE. https://doi.org/10.1109/icca.2010.5524418
• Zahednamazi, Mona, Alireza Toloei, and Reza Ghasemi. 2021. “Different Types of Star Identification Algorithms for Satellite Attitude Determination Using Star Sensor.” Aerospace Systems 4 (4): 315–21. https://doi.org/10.1007/s42401-021-00093-y
• Zahran, S., M. Mostafa, M. Moussa, A. Salib, A. Moussa, and N. El-Sheimy. 2021. “Augmented Radar Odometry by Nested Optimal Filter Aided Navigation for UAVS in GNSS Denied Environment.” In 2021 International Telecommunications Conference (ITC-Egypt). IEEE. https://doi.org/10.1109/itc-egypt52936.2021.9513978
• Zahran, S., A. Moussa, and N. El-Sheimy. 2018a. “Enhanced UAV Navigation in GNSS Denied Environment Using Repeated Dynamics Pattern Recognition.” In 2018 IEEE/ION Position, Location and Navigation Symposium (PLANS). IEEE. https://doi.org/10.1109/plans.2018.8373497
• Zahran, Shady, Adel Moussa, and Naser El-Sheimy. 2019. “Enhanced Drone Navigation in GNSS Denied Environment Using VDM and Hall Effect Sensor.” ISPRS International Journal of Geo-Information 8 (4): 169. https://doi.org/10.3390/ijgi8040169
• Zakharin, Feliks, and Sergiy Ponomarenko. 2019. “Method of the Autonomous Initial Alignment of Strapdown Inertial Navigation Systems with Preliminary Autocalibration of Inertical Sensors for Unmanned Aerial Vehicles.” In 2019 IEEE 5th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD). IEEE. https://doi.org/10.1109/apuavd47061.2019.8943936
• Zakharin, F., and S. Ponomarenko. 2023. “Advancing Universal Algorithmic Support for High-Precision Strapdown Inertial Navigation Systems in Aircraft and Rockets.” In 2023 IEEE 7th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc61017.2023.10329195
• Zakharin, Feliks, and Sergiy Ponomarenko. 2024. “Autonomous Initial Alignment of Strapdown Inertial Navigation Systems with Calibration of Sensors.” In 2024 IEEE 7th International Conference on Actual Problems of Unmanned Aerial Vehicles Development (APUAVD). IEEE. https://doi.org/10.1109/apuavd64488.2024.10765891
• Zaman, M. F., A. Sharma, B. V. Amini, and F. Ayazi. 2005. “The Resonating Star Gyroscope.” In 18th IEEE International Conference on Micro Electro Mechanical Systems, 2005. MEMS 2005.. IEEE. https://doi.org/10.1109/memsys.2005.1453940
• Zaman, Mohammad Faisal, Ajit Sharma, and Farrokh Ayazi. 2009. “The Resonating Star Gyroscope: A Novel Multiple-Shell Silicon Gyroscope with Sub-5 Deg/hr Allan Deviation Bias Instability.” IEEE Sensors Journal 9 (6): 616–24. https://doi.org/10.1109/jsen.2009.2020114
• Zaman, M. F., A. Sharma, Zhili Hao, and F. Ayazi. 2008. “A Mode-Matched Silicon-Yaw Tuning-Fork Gyroscope with Subdegree-Per-Hour Allan Deviation Bias Instability.” Journal of Microelectromechanical Systems 17 (6): 1526–36. https://doi.org/10.1109/jmems.2008.2004794
• Zang, Hongyan, Changsheng Gao, Yudong Hu, and Wuxing Jing. 2025a. “Trajectory Prediction Algorithm of Ballistic Missile Driven by Data and Knowledge.” Defence Technology 48: 187–203. https://doi.org/10.1016/j.dt.2025.02.001
• Zang, Zerun, Wei Hong, Xudong Hu, et al. 2023. “Research on Dead Zone Suppression of Fiber Optic Gyroscope Based on Cross-Coupling Intensity Calibration.” In 2023 30th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins51816.2023.10168331
• Zang, Yunzhao, Zhen Liao, Yinxi Lu, and Hongyuan Wang. 2026. “Analysis of Daytime Attitude Determination Accuracy Based on Polarization Star Sensor.” In 2026 6th International Conference on Electrical, Computer and Energy Technologies (ICECET). IEEE. https://doi.org/10.1109/icecet65726.2026.11632718
• Zang, Hongyan, Lili Liu, Yudong Hu, Changsheng Gao, and Wuxing Jing. 2025b. “Trajectory Tracking Algorithm of Ballistic Missile in the Ascent Phase Based on Deep Learning.” Aerospace Science and Technology 163: 110296. https://doi.org/10.1016/j.ast.2025.110296
• Zanj, Amir, Fangpo He, and Peter C. Breedveld. 2017. “Energy-Based Compressible Convective Model Proper for Aerothermoelastic Dynamic Investigations.” Journal of Thermophysics and Heat Transfer 31 (4): 889–900. https://doi.org/10.2514/1.t5100
• Zaragoza Prous, Guillermo, Enric Grustan-Gutierrez, and Leonard Felicetti. 2025. “A Decreasing Horizon Model Predictive Control for Landing Reusable Launch Vehicles.” Aerospace 12 (2): 111. https://doi.org/10.3390/aerospace12020111
• Zarrop, M. 1979a. “A Chebyshev System Approach to Optimal Input Design.” IEEE Transactions on Automatic Control 24 (5): 687–98. https://doi.org/10.1109/tac.1979.1102160
• Zarrop, M. B. 1981. “Optimal Input Design for the Identification of Linear Multivariable Systems with Disjoint Parametrization.” International Journal of Control 34 (2): 315–31. https://doi.org/10.1080/00207178108922532
• Zbrutsky, Alexander, and Viktor Trunov. 2020. “Forecasting and Compensation of Random Drift of the Micromechanical Gyroscope as Sensors of Strapdown Inertial Navigation System.” In 2020 IEEE 6th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC). IEEE. https://doi.org/10.1109/msnmc50359.2020.9255539
• Ze Peng, He, Yao Jun, Wei Wen Wei, and Ma Bei Zhi. 2018. “An Algorithm of Terrain Matching Aided Navigation for UAVs.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019162
• Zelenka, Richard E. 1994. “Design and Analysis of a Kalman Filter for Terrain-Referenced Positioning and Guidance.” Journal of Aircraft 31 (2): 339–44. https://doi.org/10.2514/3.46492
• Zeng, Libin, Jingyu Li, Yao Pan, et al. 2025b. “An Investigation on Influences of the Phase Delay and the Electrode Errors on a Mode-Reversal Hemispherical Resonator Gyroscope.” IEEE Transactions on Instrumentation and Measurement 74: 1–15. https://doi.org/10.1109/tim.2025.3566834
• Zeng, Qinghua, Jianye Liu, and Lei Sha. 2010. “Inertial Instrument Error Identification Algorithm Based on Reverse Navigation Data.” In IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2010.5507181
• Zeng, Libin, Yao Pan, Tao Xia, et al. 2025c. “Temperature-Dependent Bias Drift Compensation Based on a Dual Hemispherical Resonator Gyroscope System.” IEEE Sensors Journal 25 (16): 30524–35. https://doi.org/10.1109/jsen.2025.3587228
• Zeng, Boyu, Guan Wang, Jiaxin Li, Yiqiang Hou, Guoqiang Wu, and Kai Liu. 2026. “Airframe-Propulsion Integrated Learning Control for Hypersonic Vehicles with Inlet Unstart Protection.” Aerospace Science and Technology 178: 113306. https://doi.org/10.1016/j.ast.2026.113306
• Zeng, Kai, Yulie Wu, Dingbang Xiao, and Xuezhong Wu. 2020. “A Novel Electromagnetic Suspended Rate Integrating Vibratory Gyroscope.” In 2020 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial48129.2020.9090071
• Zeng, Xin, Sujie Xian, Zhilin Wu, and Kun Liu. 2025a. “Elman Neural Network–Based Nonlinear ARMA Model for MEMS Gyroscope Drift Modeling.” In 2025 5th International Conference on Measurement Control and Instrumentation (MCAI). IEEE. https://doi.org/10.1109/mcai66356.2025.11381937
• Zha, Feng, Lubin Chang, and Hongyang He. 2020. “Comprehensive Error Compensation for Dual-Axis Rotational Inertial Navigation System.” IEEE Sensors Journal 20 (7): 3788–3802. https://doi.org/10.1109/jsen.2019.2960532
• Zha, Ge-Cheng, Doyle Knight, and Donald Smith. 1998a. “Investigations of High-Speed Civil Transport Inlet Unstart at Angle of Attack.” Journal of Aircraft 35 (6): 851–56. https://doi.org/10.2514/2.2404
• Zhai, Hong-Qi, and Li-Hui Wang. 2020. “The Robust Residual-Based Adaptive Estimation Kalman Filter Method for Strap-down Inertial and Geomagnetic Tightly Integrated Navigation System.” Review of Scientific Instruments 91 (10): 104501. https://doi.org/10.1063/5.0019305
• Zhai, Sheng, and Jianying Yang. 2020. “Piecewise Analytic Optimized Ascent Trajectory Design and Robust Adaptive Finite-Time Tracking Control for Hypersonic Boost-Glide Vehicle.” Journal of the Franklin Institute 357 (9): 5485–5501. https://doi.org/10.1016/j.jfranklin.2020.03.002
• Zhan, Yinhu, Chao Zhang, Wenlong Zhou, Shaojie Chen, and Xinxing Li. 2025. “Theory and Precision Analysis of Astrogeodetic Vertical Deflection Determination Using an Imaging Total Station.” Journal of Geodesy 99 (6): 44. https://doi.org/10.1007/s00190-025-01940-y
• Zhang, Zhi-Qiang. 2014. “Two-Step Calibration Methods for Miniature Inertial and Magnetic Sensor Units.” IEEE Transactions on Industrial Electronics: 1–1. https://doi.org/10.1109/tie.2014.2375258
• Zhang, Zhi-Qiang. 2016. “Cameras and Inertial/Magnetic Sensor Units Alignment Calibration.” IEEE Transactions on Instrumentation and Measurement 65 (6): 1495–1502. https://doi.org/10.1109/tim.2016.2518418
• Zhang, Jian, and Weilian An. 2012. “Assessing Circular Error Probable When the Errors Are Elliptical Normal.” Journal of Statistical Computation and Simulation 82 (4): 565–86. https://doi.org/10.1080/00949655.2010.546797
• Zhang, Guowei, Xiaoping Chen, Jingquan Huang, Bowen Su, and Yuankai Li. 2026k. “Suboptimal Stochastic Differential Game Control for Sequential Evasive Maneuvers of a Hypersonic Glide Vehicle.” Aerospace Systems. https://doi.org/10.1007/s42401-026-00511-z
• Zhang, Xiang, Pu Chen, and Zhidong Lu. 2013b. “A Method for Star Extraction of the Air-Borne Star Sensor during the Daytime.” In 2013 International Conference on Information Science and Cloud Computing. IEEE. https://doi.org/10.1109/iscc.2013.16
• Zhang, Feilin, Xiyuan Chen, and Bo Yang. 2025i. “Optical Gyroscope Based on Mode Splitting in a Three-Turn Microfiber Coil Resonator.” Measurement 251: 117260. https://doi.org/10.1016/j.measurement.2025.117260
• Zhang, Huan, Weiping Chen, Liang Yin, and Qiang Fu. 2023c. “Design of MEMS Gyroscope Interface ASIC with on-Chip Temperature Compensation.” Measurement 220: 113331. https://doi.org/10.1016/j.measurement.2023.113331
• Zhang, Quan, Yuhang Dai, Tisheng Zhang, Chi Guo, and Xiaoji Niu. 2024f. “Road Semantic-Enhanced Land Vehicle Integrated Navigation in GNSS Denied Environments.” IEEE Transactions on Intelligent Transportation Systems 25 (12): 20889–99. https://doi.org/10.1109/tits.2024.3449892
• Zhang, Jie, Zhibo Fang, and Jiashuang Yan. 2026i. “Research on Inertial Navigation-Aided GNSS Integrity Monitoring Algorithm under Constraints.” Electronics 15 (6): 1333. https://doi.org/10.3390/electronics15061333
• Zhang, Fubin, Xiaohua Gao, and Wenbo Song. 2022l. “A Vision Aided Initial Alignment Method of Strapdown Inertial Navigation Systems in Polar Regions.” Sensors 22 (13): 4691. https://doi.org/10.3390/s22134691
• Zhang, Siqing, Lina Gao, Fuheng Zhou, Yulong Huang, and Yonggang Zhang. 2025b. “Asymmetric Dual-Branch Network for Gravity Anomaly Reference Map Super-Resolution in Underwater Gravity Matching Navigation.” IEEE Transactions on Instrumentation and Measurement 74: 1–16. https://doi.org/10.1109/tim.2025.3602540
• Zhang, Yaqiong, Jiandu Guo, Yi Liu, Jing Zhou, and Yu Sun. 2021i. “Research and Design of Fractional-Order PID Controller for Inertial Stabilized Platform via Internal Model Control.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9549439
• Zhang, Jing, Zhengyu He, Zhi Li, et al. 2025m. “A Wide-Range, High Stability Navigation-Grade MEMS Frequency-Modulated Accelerometer.” In 2025 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL). IEEE. https://doi.org/10.1109/inertial63280.2025.11036932
• Zhang, Bo, Changhua Hu, Silin Hou, Jianxun Zhang, Jianfei Zheng, and Xuan Liu. 2025j. “Research on Inertial Isolation Rotation Modulation of Dual-Axis Inertial Navigation Based on Multi-Error Coupling Characteristics.” Aerospace 12 (1): 47. https://doi.org/10.3390/aerospace12010047
• Zhang, Mengxuan, Wei Hu, Shude Ji, Qi Song, Peng Gong, and Lingpei Kong. 2021m. “Vision-Assisted Landing Method for Unmanned Powered Parachute Vehicle Based on Lightweight Neural Network.” IEEE Access 9: 130981–89. https://doi.org/10.1109/access.2021.3112185
• Zhang, Lilei, Zhipeng Huang, Chengwei Fu, Yuepeng Xu, Yunhe Wang, and Xiangdong Kong. 2021d. “Design and Verification of Two-Stage Brake Pressure Servo Valve for Aircraft Brake System.” Processes 9 (6): 979. https://doi.org/10.3390/pr9060979
• Zhang, Jianfeng, and Caijuan Jia. 2013. “Automatic Landing Controller Design and Simulation of Flying-Wing Unmanned Aerial Vehicle.” In Proceedings of 2013 2nd International Conference on Measurement, Information and Control. IEEE. https://doi.org/10.1109/mic.2013.6758104
• Zhang, Xu, Hu-Min Lei, Jiong Li, and Da-Yuan Zhang. 2014a. “Ballistic Missile Trajectory Prediction and the Solution Algorithms for Impact Point Prediction.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007325
• Zhang, Chunxi, Xianmu Li, Shuang Gao, Tie Lin, and Lu Wang. 2017d. “Performance Analysis of Global Navigation Satellite System Signal Acquisition Aided by Different Grade Inertial Navigation System under Highly Dynamic Conditions.” Sensors 17 (5): 980. https://doi.org/10.3390/s17050980
• Zhang, Peng, Wenbo Li, and Shengping Gong. 2025a. “Ascent Trajectory Optimization for Boost-Glide Vehicle Using Homotopy Approximation Function Sequential Convex Programming.” IEEE Transactions on Aerospace and Electronic Systems 61 (3): 7576–96. https://doi.org/10.1109/taes.2025.3539639
• Zhang, Jiayu, Jie Li, Xi Zhang, Xiaorui Che, Yugang Huang, and Kaiqiang Feng. 2018a. “Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.” Sensors 18 (5): 1430. https://doi.org/10.3390/s18051430
• Zhang, Qingyuan, Wenxi Li, Jian-An Zhang, Yi Jin, and Rui Kang. 2027. “Reliability Modeling and Analysis of Unmanned Aerial Vehicle Parachute Systems Considering Falling Dynamics and Failure Causality.” Reliability Engineering & System Safety 277: 113082. https://doi.org/10.1016/j.ress.2026.113082
• Zhang, Yanshun, Shanshan Liu, Yunqiang Xiong, Chunyu Li, and Ming Li. 2014e. “Stabilization Loop Modeling of Three-Axis Inertial Stabilized Platform with a New Gyro Installing Mode.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007241
• Zhang, Xiaoyue, Pengbo Liu, Xiaojing Yi, and Chunxi Zhang. 2014c. “Observability Analysis of SINS/odometer Integrated Navigation.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007231
• Zhang, Haotian, Ruoheng Ma, Zhenlin Xing, and Jianliang Ai. 2025d. “Design of Automatic Landing System for Carrier-Based Aircraft Based on Adaptive Fuzzy Sliding-Mode Control.” Actuators 14 (3): 114. https://doi.org/10.3390/act14030114
• Zhang, He, Cunxiao Miao, Linghao Zhang, Yunpeng Zhang, Yufeng Li, and Kaiwen Fang. 2023g. “A Real-Time Simulator for Navigation in GNSS-Denied Environments of UAV Swarms.” Applied Sciences 13 (20): 11278. https://doi.org/10.3390/app132011278
• Zhang, Hao, Yanxiong Niu, Jiazhen Lu, and Yanqiang Yang. 2018h. “System-Level Calibration for the Star Sensor Installation Error in the Stellar-Inertial Navigation System on a Swaying Base.” IEEE Access 6: 47288–94. https://doi.org/10.1109/access.2018.2866818
• Zhang, Yan, Linhua Piao, and Yuxin Wang. 2021c. “Compensation of Temperature Drift of Micro Gyroscope by Polynomial Fitting Algorithm.” In 2021 IEEE 5th Information Technology,Networking,Electronic and Automation Control Conference (ITNEC). IEEE. https://doi.org/10.1109/itnec52019.2021.9587304
• Zhang, Kai, Fei Qin, Xuanfei Yu, Shaohua Zhu, and Duo Zhang. 2024b. “Effect of Strut Schemes on Combustion Characteristics in Innovative Combined Ramjet Engine.” Acta Astronautica 222: 359–74. https://doi.org/10.1016/j.actaastro.2024.06.016
• Zhang, Junxian, Yegao Qu, Fangtao Xie, Zhike Peng, Wenming Zhang, and Guang Meng. 2021e. “Investigations on Nonlinear Aerothermoelastic Behaviors of Multilayered Composite Panels Subject to Frictional Boundaries and Random Acoustic Loads in Supersonic Flow.” Thin-Walled Structures 158: 107180. https://doi.org/10.1016/j.tws.2020.107180
• Zhang, Sen, Xingjing Ren, Ying Ouyang, and Xin Zhou. 2024g. “Singularity-Enhanced Deep Sub-Linewidth Mode Matching of the Disk Resonator Gyroscope.” In 2024 IEEE Sensors. IEEE. https://doi.org/10.1109/sensors60989.2024.10785205
• Zhang, X., M. S. Selezneva, and K. A. Neusypin. 2022e. “Implementation Method of Rendezvous Process of Unmanned Aerial Vehicle Landing on the Mobile Unmanned Vehicle.” In 2022 International Russian Automation Conference (RusAutoCon). IEEE. https://doi.org/10.1109/rusautocon54946.2022.9896327
• Zhang, L. W., Z. G. Song, and K. M. Liew. 2017b. “Modeling Aerothermoelastic Properties and Active Flutter Control of Nanocomposite Cylindrical Shells in Supersonic Airflow under Thermal Environments.” Computer Methods in Applied Mechanics and Engineering 325: 416–33. https://doi.org/10.1016/j.cma.2017.07.014
• Zhang, Rouhe, Zhili Sun, and Changzhu Wei. 2022j. “Trajectory Optimization with Polygonal No-Fly Zone Constraints for Hypersonic Glide Vehicle.” In 2022 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus55513.2022.9986788
• Zhang, Qi-Fan, Hui-Jun Tan, Hao Chen, Yong-Qing Yuan, and Yu-Chao Zhang. 2016c. “Unstart Process of a Rectangular Hypersonic Inlet at Different Mach Numbers.” AIAA Journal 54 (12): 3681–91. https://doi.org/10.2514/1.j055005
• Zhang, Qintuo, Zhenfan Tan, and Lidong Guo. 2009a. “Compensation of Temperature Drift of MEMS Gyroscope Using BP Neural Network.” In 2009 International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2009.5365140
• Zhang, Q. F., H. J. Tan, S. Sun, H. X. Bu, and C. Y. Rao. 2016b. “Unstart of a Hypersonic Inlet with Side Compression Caused by Downstream Choking.” AIAA Journal 54 (1): 28–38. https://doi.org/10.2514/1.j054095
• Zhang, Lingling, Chengkai Tang, Yi Zhang, and Houbing Song. 2019b. “Inertial-Navigation-Aided Single-Satellite Highly Dynamic Positioning Algorithm.” Sensors 19 (19): 4196. https://doi.org/10.3390/s19194196
• Zhang, Qiang, Lei Wan, and Yongjie Pang. 2009b. “Fault-Tolerant GPS/DR Integrated Navigation System Based on Heuristic Reduction of MEMS Inertial Measurement Unit Drift.” In 2009 International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2009.5366427
• Zhang, Peng, and Jing Wang. 2011a. “Design and Reliability Analysis on Tri-Redundancy Servo Actuator System.” In 2011 Fourth International Symposium on Computational Intelligence and Design. IEEE. https://doi.org/10.1109/iscid.2011.168
• Zhang, Yanshun, and Yuanyuan Wang. 2011c. “Research of Backlash Nonlinearity on Three-Axis Inertial Stabilized Platform.” Energy Procedia 11: 1224–30. https://doi.org/10.1016/j.egypro.2011.10.382
• Zhang, Chongmeng, and Guochen Wang. 2011d. “Transfer Alignment in Strapdown Inertial Navigation System Using CCD Star Tracker.” In 2011 IEEE International Conference on Signal Processing, Communications and Computing (ICSPCC). IEEE. https://doi.org/10.1109/icspcc.2011.6061610
• Zhang, Fan, and Yong Wang. 2013. “Automatic Landing of Unmanned Aerial Vehicle Using Fuzzy Control.” In 2013 IEEE International Conference on Information and Automation (ICIA). IEEE. https://doi.org/10.1109/icinfa.2013.6720345
• Zhang, Jun, and Jian Wang. 2016. “An Enhanced Cramér-Rao Bound Weighted Method for Attitude Accuracy Improvement of a Star Tracker.” Review of Scientific Instruments 87 (6): 063112. https://doi.org/10.1063/1.4953331
• Zhang, Zhuo, Qiufu Wang, Daoming Bi, Xiaoliang Sun, and Qifeng Yu. 2023e. “MC-LRF Based Pose Measurement System for Shipborne Aircraft Automatic Landing.” Chinese Journal of Aeronautics 36 (8): 298–312. https://doi.org/10.1016/j.cja.2023.01.006
• Zhang, Tong, Fenfen Wang, and Wenxing Fu. 2018c. “Fault Detection and Isolation for Redundant Inertial Measurement Unit under Quantization.” Applied Sciences 8 (6): 865. https://doi.org/10.3390/app8060865
• Zhang, Tao, Jian Wang, Bonan Jin, and Yao Li. 2019a. “Application of Improved Fifth-Degree Cubature Kalman Filter in the Nonlinear Initial Alignment of Strapdown Inertial Navigation System.” Review of Scientific Instruments 90 (1): 015111. https://doi.org/10.1063/1.5061790
• Zhang, Lixiang, Lei Wang, Zengiun Liu, and Jingxuan Ban. 2018f. “A Rotation Scheme for Dual-Unit Inertial Navigation System Based on MEMS Sensors.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019108
• Zhang, Zhongyu, Lihui Wang, Endong Liu, Ye Li, and Teng Ma. 2026e. “Mitigating Observability-Induced Inconsistency via State-Dependent Error Transformation for Underwater Integrated Navigation.” IEEE Transactions on Instrumentation and Measurement 75: 8510014–8510014. https://doi.org/10.1109/tim.2026.3704134
• Zhang, Chunxi, Xin Wang, Lailiang Song, and Longjun Ran. 2021k. “Temperature Hysteresis Mechanism and Compensation of Quartz Flexible Accelerometer in Aerial Inertial Navigation System.” Sensors 21 (1): 294. https://doi.org/10.3390/s21010294
• Zhang, Zihan, Bo Wang, Wei Xiao, Zhihong Deng, and Mengyin Fu. 2026f. “Nested Preanalyzed and Real-Time Corrected Matching Area Selection Method for Underwater Gravity-Aided Inertial Navigation.” IEEE Sensors Journal 26 (12): 19382–94. https://doi.org/10.1109/jsen.2026.3691705
• Zhang, Wei, Qiang Wang, Fanzhi Zeng, and Chao Yan. 2021a. “An Adaptive Sequential Enhanced PCE Approach and Its Application in Aerodynamic Uncertainty Quantification.” Aerospace Science and Technology 117: 106911. https://doi.org/10.1016/j.ast.2021.106911
• Zhang, Lu, Wenqi Wu, and Maosong Wang. 2019d. “Rapid SINS Two-Position Ground Alignment Scheme Based on Piecewise Combined Kalman Filter and Azimuth Constraint Information.” Sensors 19 (5): 1125. https://doi.org/10.3390/s19051125
• Zhang, Haoming, Xiao Xia, Maximilian Nitsch, and Dirk Abel. 2022a. “Continuous-Time Factor Graph Optimization for Trajectory Smoothness of GNSS/INS Navigation in Temporarily GNSS-Denied Environments.” IEEE Robotics and Automation Letters 7 (4): 9115–22. https://doi.org/10.1109/lra.2022.3189824
• Zhang, S., and F. Xing. 2018. “Attitude Measurement for Spacecraft with High Update Rate Based on the Rolling Shutter Mode of a Star Tracker.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019168
• Zhang, Junbiao, Jiajun Xiong, Xuhui Lan, Yanan Shen, Xin Chen, and Qiushi Xi. 2022k. “Trajectory Prediction of Hypersonic Glide Vehicle Based on Empirical Wavelet Transform and Attention Convolutional Long Short-Term Memory Network.” IEEE Sensors Journal 22 (5): 4601–15. https://doi.org/10.1109/jsen.2022.3143705
• Zhang, Junbiao, Jiajun Xiong, Lingzhi Li, Qiushi Xi, Xin Chen, and Fan Li. 2022g. “Motion State Recognition and Trajectory Prediction of Hypersonic Glide Vehicle Based on Deep Learning.” IEEE Access 10: 21095–21108. https://doi.org/10.1109/access.2022.3150830
• Zhang, Yanping, Tingyang Yan, Yuan Dongfeng, and Min Su. 2021j. “Temperature Compensation for Fiber Optic Gyroscope Based on Bayesian Optimized: Support Vector Regression.” In 2021 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac53003.2021.9727748
• Zhang, Yan-shun, and Tao Yang. 2012. “Modeling and Compensation of MEMS Gyroscope Output Data Based on Support Vector Machine.” Measurement 45 (5): 922–26. https://doi.org/10.1016/j.measurement.2012.02.001
• Zhang, Zhi-Qiang, and Guang-Zhong Yang. 2014. “Calibration of Miniature Inertial and Magnetic Sensor Units for Robust Attitude Estimation.” IEEE Transactions on Instrumentation and Measurement 63 (3): 711–18. https://doi.org/10.1109/tim.2013.2281562
• Zhang, Yi-Fei, and Hui Yang. 2022. “Study on Terrain Navigation Technology for Cruise Missile Based on Laser Echo Waveform Matching.” In 2022 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac57257.2022.10055446
• Zhang, Zhidong, Gongliu Yang, Qingzhong Cai, Jing Fan, and Tao Li. 2025c. “Design and Implementation of Disturbance Sliding Mode Observer for Enhancing the Dynamic Control Precision of Inertial Stabilization Platform.” Journal of Systems Engineering and Electronics 36 (3): 791–802. https://doi.org/10.23919/jsee.2025.000027
• Zhang, Yirui, Shibin Yang, and Xulong Xi. 2024h. “Study on Automatic Landing of Civil Aircraft Based on LADRC.” In 2024 11th International Forum on Electrical Engineering and Automation (IFEEA). IEEE. https://doi.org/10.1109/ifeea64237.2024.10878772
• Zhang, Jing, Zhiyong Yang, Wenwu Zhu, and Jian Xiao. 2026m. “Vision Inertial Stabilized Platform-Based Finite-Time Target Tracking Control for Multi-Rotor UAVs.” Actuators 15 (5): 261. https://doi.org/10.3390/act15050261
• Zhang, Xuwei, Zhilong Ye, Xunjiang Zheng, Shuodong Sun, and Huiping Zhang. 2021b. “Autonomous Navigation Algorithm Using All-Time Star Tracker, Accelerometer and Time.” In 2021 IEEE 15th International Conference on Electronic Measurement & Instruments (ICEMI). IEEE. https://doi.org/10.1109/icemi52946.2021.9679625
• Zhang, Ya, Fei Yu, Wei Gao, and Yanyan Wang. 2018d. “An Improved Strapdown Inertial Navigation System Initial Alignment Algorithm for Unmanned Vehicles.” Sensors 18 (10): 3297. https://doi.org/10.3390/s18103297
• Zhang, Chao, Yanjun Yu, and Huayi Li. 2026b. “Dual-Layer Factor-Graph Optimization for Delayed Star-Tracker/IMU Fusion in Highly Dynamic Spacecraft Attitude Estimation.” Sensors 26 (13): 4155. https://doi.org/10.3390/s26134155
• Zhang, Yongmeng, Sheng Yu, Jiangkun Sun, et al. 2021h. “A Rate-Integrating Honeycomb Disk Resonator Gyroscope with 0.038°/h Bias Instability and °7000°/s Measurement Range.” IEEE Electron Device Letters 42 (4): 581–84. https://doi.org/10.1109/led.2021.3062897
• Zhang, Wenbo, Xin Yu, Yihang Wang, et al. 2026d. “An Interface ASIC for MEMS Disk Resonator Gyroscope with 0.018°/h Bias Instability and 108 Ppm Scale Factor Nonlinearity.” IEEE Transactions on Circuits and Systems I: Regular Papers 73 (1): 113–25. https://doi.org/10.1109/tcsi.2025.3596470
• Zhang, Kai, Xuanfei Yu, Duo Zhang, Jian Guo, and Fei Qin. 2025g. “Evaluation of Multi-Mode Shared Combustor with Different Flame Holder Designs for an Innovative Turbo-Ramjet Combined Cycle Engine.” Energy 323: 135875. https://doi.org/10.1016/j.energy.2025.135875
• Zhang, Weike, and Naichang Yuan. 2015. “Error Suppressing in Phase-Coherent Active Radar Seeker Using Velocity Measurement of Inertial Navigation System.” In 2015 IEEE International Conference on Computer and Communications (ICCC). IEEE. https://doi.org/10.1109/compcomm.2015.7387595
• Zhang, Lei, Zhengjun Zhai, Lang He, Pengcheng Wen, and Wensheng Niu. 2019c. “Infrared-Inertial Navigation for Commercial Aircraft Precision Landing in Low Visibility and GPS-Denied Environments.” Sensors 19 (2): 408. https://doi.org/10.3390/s19020408
• Zhang, Han, Chen Zhang, Jing Chen, and Ang Li. 2022i. “A Review of Symmetric Silicon MEMS Gyroscope Mode-Matching Technologies.” Micromachines 13 (8): 1255. https://doi.org/10.3390/mi13081255
• Zhang, Haowei, Ran Zhang, and Huifeng Li. 2022b. “Control Contraction Metrics Based Robust Tracking Guidance for Hypersonic Glide Vehicle in Terminal Phase.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9901754
• Zhang, Zengping, Wei Zhang, Fuxue Zhang, and Biao Wang. 2015. “A New MEMS Gyroscope Used for Single-Channel Damping.” Sensors 15 (5): 10146–65. https://doi.org/10.3390/s150510146
• Zhang, Kefan, Zhili Zhang, Junyang Zhao, and Shenhua Lv. 2024a. “Barometric Altimeter Assisted SINS/DR Combined Land Vehicle Gravity Anomaly Method.” In 2024 4th International Conference on Electronic Information Engineering and Computer (EIECT). IEEE. https://doi.org/10.1109/eiect64462.2024.10866603
• Zhang, Zhihao, Jintao Zhang, Xiaohan Zhu, Yanchao Ren, Jingfeng Yu, and Huiliang Cao. 2024c. “MEMS Gyroscope Temperature Compensation Based on Improved Complete Ensemble Empirical Mode Decomposition and Optimized Extreme Learning Machine.” Micromachines 15 (5): 609. https://doi.org/10.3390/mi15050609
• Zhang, ShaoHua, Hua Zhao, AiMin Du, and Xin Cao. 2013a. “3-D Numerical Calculation of Magnetic Drag Parachute.” Science China Technological Sciences 56 (8): 2059–65. https://doi.org/10.1007/s11431-013-5283-5
• Zhang, Lantian, Yanlong Zhao, and Lei Guo. 2022d. “Identification and Adaptation with Binary-Valued Observations under Non-Persistent Excitation Condition.” Automatica 138: 110158. https://doi.org/10.1016/j.automatica.2022.110158
• Zhang, Kefan, Junyang Zhao, and Zhili Zhang. 2024d. “A Method for Land Vehicle Gravity Anomaly Measurement Combining an Inertial Navigation System, Odometer, and Geo-Information System.” World Electric Vehicle Journal 15 (8): 368. https://doi.org/10.3390/wevj15080368
• Zhang, Dengwei, Yuxiang Zhao, Wenqing Zhou, et al. 2014d. “A Software-Compensation Method to Orthogonal Magnetic Field Drift in a Depolarized Fiber-Optic Gyroscope.” Optik 125 (11): 2565–67. https://doi.org/10.1016/j.ijleo.2013.10.095
• Zhang, Q. Q., L. Zhao, J. H. Zhou, B. H. Wang, and Y. P. Zhang. 2017e. “A Real-Time Airborne Terrain Aided Inertial Navigation System and Its Performance Analysis.” Advances in Space Research 60 (12): 2751–62. https://doi.org/10.1016/j.asr.2017.10.038
• Zhang, Sen, and Xin Zhou. 2026. “Non-Hermitian Dynamics in a Frequency-Matched, Dissipation-Imbalanced MEMS Gyroscope.” In 2026 IEEE 39th International Conference on Micro Electro Mechanical Systems (MEMS). IEEE. https://doi.org/10.1109/mems64181.2026.11419258
• Zhang, Jingjuan, Wenxiang Zhou, and Xueyun Wang. 2021l. “UAV Swarm Navigation Using Dynamic Adaptive Kalman Filter and Network Navigation.” Sensors 21 (16): 5374. https://doi.org/10.3390/s21165374
• Zhang, Yunhao, Zhaofa Zhou, Zhili Zhang, Zhe Liang, Hui Duan, and Yongxu Li. 2026l. “Temperature Drift Compensation Method for Fiber-Optic Gyroscope Based on LSTM-PINN.” IEEE Photonics Technology Letters 38 (3): 184–87. https://doi.org/10.1109/lpt.2025.3614221
• Zhang, Chaofan, Qun Zong, Qi Dong, Bailing Tian, Zhiyu Li, and Jing Zong. 2017a. “Approach and Landing Trajectory Optimization for Reusable Launch Vehicle Using Adaptive Gauss Pseudo-Spectral Method.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027798
• Zhang Guanjie, Guo Min, and Bao Yongjie. 2001. “Silence Tracking Radar.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984637
• Zhang Xiangping, Yang Haiyan, and Liu Xiang. 2008. “A Lifetime Prediction Approach of Ring Laser Gyroscope without the Lifetime Test.” In 2008 27th Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2008.4605469
• Zhang Ze and Duan Guangren. 2008. “Attitude Determination with the Star Sensor under over-Determined Conditions.” In 2008 27th Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2008.4605016
• Zhao, Long. 2011. “An Algorithm for Terrain-Aided Inertial Navigation Based on Nonlinear Optimal Filtering.” Science China Physics, Mechanics and Astronomy 54 (6): 1083–88. https://doi.org/10.1007/s11433-011-4340-y
• Zhao, Xiangrui, Chunfang Deng, Xin Kong, Jinhong Xu, and Yong Liu. 2020a. “Learning to Compensate for the Drift and Error of Gyroscope in Vehicle Localization.” In 2020 IEEE Intelligent Vehicles Symposium (IV). IEEE. https://doi.org/10.1109/iv47402.2020.9304715
• Zhao, Shijie, Zhiyuan Dou, Huizhong Zhu, Wei Zheng, and Yifan Shen. 2025a. “Gravity-Aided Navigation of Underwater Vehicles via Alternating Line Small-Domain Matching Method.” IEEE Transactions on Instrumentation and Measurement 74: 1–9. https://doi.org/10.1109/tim.2025.3588992
• Zhao, Shuai, Chaofeng Guo, Cuineng Ke, Yilan Zhou, and Xiaowu Shu. 2022f. “Temperature Drift Compensation of Fiber Strapdown Inertial Navigation System Based on GSA-SVR.” Measurement 195: 111117. https://doi.org/10.1016/j.measurement.2022.111117
• Zhao, Jinyue, Kunpeng He, Le Kang, and Sixu Huang. 2026b. “A Dual-Path Gyroscope Calibration Framework Combining Residual Bias Optimization and Cross-Axis Coupling Compensation.” IEEE Transactions on Instrumentation and Measurement 75: 2515913–2515913. https://doi.org/10.1109/tim.2026.3714598
• Zhao, Jian, Xiangyue He, Haiyang Li, and Lin Lu. 2021a. “An Adaptive Optimization Algorithm Based on Clustering Analysis for Return Multi-Flight-Phase of VTVL Reusable Launch Vehicle.” Acta Astronautica 183: 112–25. https://doi.org/10.1016/j.actaastro.2021.02.036
• Zhao, Tun, Lei He, and Weiqi Qian. 2018. “Joint Design of Guidance and Control System for a Hypersonic Gliding Vehicle on Lie Groups.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019043
• Zhao, Siyuan, and Xiaobing Li. 2019. “Prescribed Performance Fault Tolerant Control for Hypersonic Flight Vehicles with Actuator Failures.” IEEE Access 7: 100187–100204. https://doi.org/10.1109/access.2019.2930658
• Zhao, Lin, Jiushun Li, and Yong Hao. 2017b. “Schuler Oscillation Error Compensation Method for Low-Speed SINS.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028288
• Zhao, Jian, Haiyang Li, Xiangyue He, Yuechen Huang, and Jianghui Liu. 2020c. “Uncertainty Analysis for Return Trajectory of Vertical Takeoff and Vertical Landing Reusable Launch Vehicle.” Mathematical Problems in Engineering 2020: 1–18. https://doi.org/10.1155/2020/4313758
• Zhao, Yuyang, Chen Li, Xiangteng Jia, Kuibao Zhu, and Fengshan Huang. 2025e. “Optimization of Heat Dissipation Structure for Fiber-Optic Gyroscope Inertial Navigation System Based on Fluid-Thermal Coupling Analysis.” IEEE Sensors Journal 25 (13): 25266–77. https://doi.org/10.1109/jsen.2025.3572951
• Zhao, Yujie, Shaobin Li, Lei Qi, and Zhiping Li. 2025c. “Multiphysics Coupled Modeling of Aero-Engine Aerodynamic Stability in Initial Design Phase: Integration of Inlet Distortion Effects.” In 2025 16th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae66341.2025.11277014
• Zhao, Jiaxin, Pingli Lu, Changkun Du, and Fangfei Cao. 2024a. “Active Fault-Tolerant Strategy for Flight Vehicles: Transfer Learning-Based Fault Diagnosis and Fixed-Time Fault-Tolerant Control.” IEEE Transactions on Aerospace and Electronic Systems 60 (1): 1047–59. https://doi.org/10.1109/taes.2023.3333763
• Zhao, Maosu, Lingjuan Miao, Haijun Shao, and Tian Dai. 2019b. “A Fuzzy Based Parallel Filtering Matching Algorithm for Gravity Aided Navigation.” In 2019 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2019.8816218
• Zhao, Yang, An Ping Qiu, Qin Shi, and Guo Ming Xia. 2016b. “Sub-Degree per Hour Split Mode Tuning Fork Gyroscope.” In 2016 IEEE International Symposium on Inertial Sensors and Systems. IEEE. https://doi.org/10.1109/isiss.2016.7435559
• Zhao, Changshan, Yongyuan Qin, and Gonming Yan. 2008. “On-the-Move Alignment for Strap-down Inertial Navigation System.” In 2008 International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2008.4608226
• Zhao, Xinxin, Jinguang Shi, Huajie Ren, and Zhongyuan Wang. 2025d. “Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft.” Aerospace 12 (6): 558. https://doi.org/10.3390/aerospace12060558
• Zhao, Yang, Qin Shi, Guaming Xia, and Anping Qiu. 2022b. “A Compact Stabilization Scheme for Quality Factor in Nondegenerate Mems Gyroscope.” In 2022 IEEE 35th International Conference on Micro Electro Mechanical Systems Conference (MEMS). IEEE. https://doi.org/10.1109/mems51670.2022.9699615
• Zhao, Haibin, Ruizhuo Song, and Qinglai Wei. 2026d. “Temperature Compensation Method for Fiber Optic Gyroscope Based on a Collaborative Architecture of sLSTM and mLSTM.” In 2026 15th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc70886.2026.11702475
• Zhao, Xi-jing, Li-xin Wang, Zhi-kun He, Bo Zhang, and Han Zhao. 2014a. “Initial Alignment of Large Misalignment Angle in Strapdown Inertial Navigation System Based on Gaussian Process Regression.” In The 26th Chinese Control and Decision Conference (2014 CCDC). IEEE. https://doi.org/10.1109/ccdc.2014.6852710
• Zhao, Xiaoxi, Lei Wang, Fei Qi, and Jinshun Wang. 2024d. “Research on Propagation Mechanism for Gyro Installation Error of Dual-Axis Rotational Inertial Navigation System in UAV Coordinated U-Turn.” Measurement 234: 114808. https://doi.org/10.1016/j.measurement.2024.114808
• Zhao, Y., Z. H. Wang, G. M. Xia, Q. Shi, and A. P. Qiu. 2017a. “Effect of Stress on Split Mode Gyroscope Bias: An Experimental Study.” In 2017 19th International Conference on Solid-State Sensors, Actuators and Microsystems (TRANSDUCERS). IEEE. https://doi.org/10.1109/transducers.2017.7994230
• Zhao, C. L., W. Q. Wu, and J. X. Lian. 2014b. “Research on Rotating Modulation Inertial Navigation System Error Characteristics Simulation Method in Polar Area.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007605
• Zhao, Shengwu, Xuan Xiao, Yu Wang, and Zhihong Deng. 2023b. “An Improved Particle Filter Based on Gravity Measurement Feature in Gravity-Aided Inertial Navigation System.” IEEE Sensors Journal 23 (2): 1423–35. https://doi.org/10.1109/jsen.2022.3226747
• Zhao, Junhu, Qifan Yang, and Huiping Li. 2024b. “Data-Driven MPC Scheme for Inertial Platform with Uncertain Systems against External Vibrations.” Electronics 13 (24): 4945. https://doi.org/10.3390/electronics13244945
• Zhao, Wanliang, Hao Yang, Fucheng Liu, Yan Su, and Chong Li. 2021c. “High Sensitivity Rate-Integrating Hemispherical Resonator Gyroscope with Dead Area Compensation for Damping Asymmetry.” Scientific Reports 11 (1): 2195. https://doi.org/10.1038/s41598-020-80885-y
• Zhao, Jianbo, Shuxing Yang, and Fenfen Xiong. 2019a. “Cooperative Guidance of Seeker-Less Missile Considering Localization Error.” Chinese Journal of Aeronautics 32 (8): 1933–45. https://doi.org/10.1016/j.cja.2019.03.005
• Zhao, Shijie, Wei Zheng, Zhaowei Li, Huizhong Zhu, and Aigong Xu. 2023c. “Improving Matching Efficiency and out-of-Domain Positioning Reliability of Underwater Gravity Matching Navigation Based on a Novel Domain-Center Adaptive-Transfer Matching Method.” IEEE Transactions on Instrumentation and Measurement 72: 1–11. https://doi.org/10.1109/tim.2023.3235452
• Zhao, Shijie, Wei Zheng, Zhaowei Li, Huizhong Zhu, and Aigong Xu. 2023d. “Improving the out-of-Domain Matching Reliability and Positioning Accuracy of Underwater Gravity Matching Navigation Based on a Novel Cyclic Boundary Semisquare-Domain Researching Method.” IEEE Sensors Journal 23 (10): 10758–66. https://doi.org/10.1109/jsen.2023.3265307
• Zhao, Shuai, Yilan Zhou, and Xiaowu Shu. 2022a. “Analysis of Fiber Optic Gyroscope Dynamic Error Based on CEEMDAN.” Optical Fiber Technology 69: 102835. https://doi.org/10.1016/j.yofte.2022.102835
• Zhao, Shuai, Yilan Zhou, and Xiaowu Shu. 2022e. “Study on Nonlinear Error Calibration of Fiber Optical Gyroscope Scale Factor Based on LSTM.” Measurement 190: 110783. https://doi.org/10.1016/j.measurement.2022.110783
• Zhao, W., L. Zhou, and G. Song. 2019c. “A Study on Alignment of Analytic Space Stable Inertial Navigation System.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769359
• Zhao, Jinqi, Zhaofa Zhou, and Zhili Zhang. 2026c. “A Review of Key Technologies in Gravity Matching Navigation.” Sensors 26 (13): 4208. https://doi.org/10.3390/s26134208
• Zhao Dawei, Chen Guangjun, and Xu Hualong. n.d. “Identification and Compensation of Strategic Missile Guidance System Error Model Based on the BP Neural Network.” In Proceedings of the 4th World Congress on Intelligent Control and Automation (Cat. No.02EX527), vol. 1. IEEE. https://doi.org/10.1109/wcica.2002.1022227
• Zhao Hongbo, Ren Shunqing, and Wang Changhong. 2013. “Quadrature Control Principle of Hemispherical Resonator Gyro.” In Proceedings 2013 International Conference on Mechatronic Sciences, Electric Engineering and Computer (MEC). IEEE. https://doi.org/10.1109/mec.2013.6885115
• Zhaoqing, Xu, and Pei Hailong. 2016. “Dynamic Characteristics Analysis of Cruise Missile Controlled by Grid Fin.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531012
• Zharkov, Maksim, Konstantin Veremeenko, Ivan Kuznetsov, and Andrei Pronkin. 2023. “Global Navigation Satellite System Spoofing Detection in Inertial Satellite Navigation Systems.” Inventions 8 (6): 158. https://doi.org/10.3390/inventions8060158
• Zhen, Ziyang, Shuoying Jiang, and Kun Ma. 2018. “Automatic Carrier Landing Control for Unmanned Aerial Vehicles Based on Preview Control and Particle Filtering.” Aerospace Science and Technology 81: 99–107. https://doi.org/10.1016/j.ast.2018.07.039
• Zhen, Ziyang, Miao Peng, Yixuan Xue, and Shuoying Jiang. 2019. “Robust Preview Control and Autoregressive Prediction for Aircraft Automatic Carrier Landing.” IEEE Access 7: 181273–83. https://doi.org/10.1109/access.2019.2957740
• Zhen Shi, Zijian Cheng, and Jie Yang. 2010. “Study of Independent Initial Alignment Based on Gyroscope Free Strapdown Inertial Navigation System.” In 2010 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2010.5498853
• Zheng, Jianqiang, Qinghua Ma, Lin Gao, and Shujun Yang. 2019. “Self-Compensation Method of Constant Drift Error of Gyroscope.” In 2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence (ICUSAI). IEEE. https://doi.org/10.1109/icusai47366.2019.9124873
• Zheng, Xiang, and Wang Wei. 2009. “Reliability Study of Redundant Configuration of IMU Fiber Optic Gyroscope Inertial Measurement Unit.” In 2009 8th International Conference on Reliability, Maintainability and Safety. IEEE. https://doi.org/10.1109/icrms.2009.5270232
• Zheng, Jieji, Xin Xie, Baoyu Li, Ziping Wan, Ning Chen, and Dapeng Fan. 2023. “Adaptive Multi-Parameter Estimation of Inertial Stabilization Platform with Unknown Load.” Actuators 12 (4): 176. https://doi.org/10.3390/act12040176
• Zhesheng Jiang and Raul Ordonnez. 2007. “On-Line Approach/landing Trajectory Generation with Input Deviation Bound Uncertainty for Reusable Launch Vehicles.” In 2007 46th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2007.4434529
• Zhi, Wang, Zhang Ran, and Li Huifeng. 2015. “Hybrid Re-Entry Guidance for Reusable Launch Vehicle.” Procedia Engineering 99: 999–1004. https://doi.org/10.1016/j.proeng.2014.12.633
• Zhiru, Fan, and Yang Jing. 2013. “A Research of Gyro/Star-Sensor Integrated Attitude Determination Based on Particle Filter.” In 2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control. IEEE. https://doi.org/10.1109/imccc.2013.61
• Zhixiong, Zhang, Feng Lihui, and Sun Yu-nan. 2011. “Temperature Modeling and Compensation of Double h Quartz Tuning Fork Gyroscope.” Procedia Engineering 15: 752–56. https://doi.org/10.1016/j.proeng.2011.08.140
• Zhong, Shaoyuan, Xinguo Wei, Jie Jiang, Jian Li, and Gangyi Wang. 2026. “Daytime Star Spot Detection Based on Spatial–temporal Feature Context Enhancement for Optical Star Sensors.” Applied Optics 65 (6): 2028. https://doi.org/10.1364/ao.579973
• Zhong, Liu, and Jia Xiaohong. 2008. “Novel Backstepping Design for Blended Aero and Reaction-Jet Missile Autopilot.” Journal of Systems Engineering and Electronics 19 (1): 148–53. https://doi.org/10.1016/s1004-4132(08)60060-2
• Zhong, Jingjia, Gongliu Yang, Yuanyuan Liu, and Jing Xu. 2017. “Initial Alignment of Strapdown Inertial Navigation System with the Aid of Doppler Velocity Log.” In 2017 4th International Conference on Information Science and Control Engineering (ICISCE). IEEE. https://doi.org/10.1109/icisce.2017.212
• Zhong, Jie, Heng Zhang, and Qiang Miao. 2025. “Enhancing Aircraft Reliability with Information Redundancy: A Sensor-Modal Fusion Approach Leveraging Deep Learning.” Reliability Engineering & System Safety 261: 111068. https://doi.org/10.1016/j.ress.2025.111068
• Zhou, Bochao, Yong Li, and Shihang Cui. 2023a. “Autonomous Navigation and Observability Analysis for Satellites during Orbital Maneuver.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10241038
• Zhou, Weizheng, Xuefeng Li, and Saijun Zhao. 2018a. “Condition Monitoring and Information Management for Skew Redundant Strapdown Inertial Measurement Unit.” In 2018 13th IEEE Conference on Industrial Electronics and Applications (ICIEA). IEEE. https://doi.org/10.1109/iciea.2018.8398178
• Zhou, Weizheng, Xuefeng Li, Saijun Zhao, and Jiansheng Tao. 2018b. “FDI and Navigation Integration Algorithm Design for Skew Redundant Strapdown Inertial Measurement Unit.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018940
• Zhou, Zhibo, Xinghui Liang, Zhimin Shi, Guocheng Wang, Junjian Lang, and Lintao Liu. 2022. “A New Method to Restrain Schuler Periodic Oscillation in Inertial Navigation System Based on Normal Time–Frequency Transform.” IEEE Transactions on Instrumentation and Measurement 71: 1–15. https://doi.org/10.1109/tim.2022.3170993
• Zhou, Qiang, and Yabin Liu. 2009. “Novel Barometric Altimeter System for Vehicular Testing of SINS.” In 2009 9th International Conference on Electronic Measurement & Instruments. IEEE. https://doi.org/10.1109/icemi.2009.5274518
• Zhou, Jian, Xiaoming Nie, and Jun Lin. 2014. “A Novel Laser Doppler Velocimeter and Its Integrated Navigation System with Strapdown Inertial Navigation.” Optics & Laser Technology 64: 319–23. https://doi.org/10.1016/j.optlastec.2014.06.001
• Zhou, Xingyu, Tong Qin, Malcolm Macdonald, and Dong Qiao. 2023c. “Observability Analysis of Cooperative Orbit Determination Using Inertial Inter-Spacecraft Angle Measurements.” Acta Astronautica 210: 289–302. https://doi.org/10.1016/j.actaastro.2023.05.019
• Zhou, Ruihu, Mengqi Tong, and Yongxin Gao. 2025b. “Vision-Aided Inertial Navigation for Low Altitude Aircraft with a Downward-Viewing Camera.” Journal of Systems Engineering and Electronics 36 (3): 825–34. https://doi.org/10.23919/jsee.2025.000067
• Zhou, Fansen, Lei Wang, Wei Zheng, Xiang Zhou, and Xin Wen. 2026. “Physics-Informed Ensemble Informerstack for Hypersonic Glide Vehicle Trajectory Prediction.” IEEE Transactions on Aerospace and Electronic Systems 62: 12890–12908. https://doi.org/10.1109/taes.2026.3705024
• Zhou, Xiaocong, Jiaqiang Wen, Shasha Han, and Chong Li. 2025a. “Compensation of Temperature-Induced Bias Drift in Hemispherical Resonator Gyroscopes: An Inherent Data-Driven Architecture.” Micromachines 16 (4): 357. https://doi.org/10.3390/mi16040357
• Zhou, Shaolei, Hualong Xu, Hongde Dai, and Guangbin Wu. 2011. “Novel Rapid Transfer Alignment Algorithm for Strapdown Inertial Navigation System.” In 2011 International Conference on Electrical and Control Engineering. IEEE. https://doi.org/10.1109/iceceng.2011.6057277
• Zhou, Qifan, Guizhen Yu, Huazhi Li, and Na Zhang. 2020b. “A Novel MEMS Gyroscope in-Self Calibration Approach.” Sensors 20 (18): 5430. https://doi.org/10.3390/s20185430
• Zhou, Guanwu, Qinghong Zhang, and Jiao Li. 2023b. “A Hybrid Model for Random Drift Compensation of 3-Axis MEMS Gyroscope.” In 2023 8th International Conference on Intelligent Computing and Signal Processing (ICSP). IEEE. https://doi.org/10.1109/icsp58490.2023.10248793
• Zhou, Hang, Yongjie Zhang, Linyin Luo, Jiyong Sun, and Lei Ren. 2024a. “Research Progress on Aircraft Landing Gear Dynamics Modeling and Simulation Methods.” In 2024 2nd Asian Aerospace and Astronautics Conference (AAAC). IEEE. https://doi.org/10.1109/aaac63570.2024.11027352
• Zhou, Chun-Lei, Qi Zhang, Shu-Hua Yan, Lei Gao, and Guo-Chao Wang. 2009. “Modeling and Compensation for Temperature Errors of Interferometric Fiber Optic Gyroscope.” In 2009 International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2009.5205143
• Zhou, Haitong, Zewei Zheng, Zhiyuan Guan, and Yunpeng Ma. 2020a. “Control Barrier Function Based Nonlinear Controller for Automatic Carrier Landing.” In 2020 16th International Conference on Control, Automation, Robotics and Vision (ICARCV). IEEE. https://doi.org/10.1109/icarcv50220.2020.9305317
• Zhu, J., D. Dai, W. Wu, X. Wang, and J. Wang. 2019. “Assessment of the Impact of the Measurement Noise on the Gravity Anomaly Matching Technique.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769339
• Zhu, Bing, and Hongyang He. 2020. “Integrated Navigation for Doppler Velocity Log Aided Strapdown Inertial Navigation System Based on Robust IMM Algorithm.” Optik 217: 164871. https://doi.org/10.1016/j.ijleo.2020.164871
• Zhu, Yijia, and Biao Huang. 2010. “Constrained Receding-Horizon Experiment Design and Parameter Estimation in the Presence of Poor Initial Conditions.” AIChE Journal 57 (10): 2808–20. https://doi.org/10.1002/aic.12479
• Zhu, Jiupeng, An Li, Fangjun Qin, and Dongyi Li. 2021c. “Research on Adaptive Damping Method for Inertial Navigation System Attitude Error Suppression Algorithm.” In 2021 International Conference on Control Science and Electric Power Systems (CSEPS). IEEE. https://doi.org/10.1109/cseps53726.2021.00027
• Zhu, Hailong, Bin Liang, and Tao Zhang. 2016a. “High Accuracy Star Centroid Acquisition Method of Airborne Star Sensor during Daytime.” In 2016 12th World Congress on Intelligent Control and Automation (WCICA). IEEE. https://doi.org/10.1109/wcica.2016.7578473
• Zhu, Yongkai, Jiawei Liu, Rui Li, Ziyu Wang, and Haitao Wang. 2026a. “Integrated Fiber-Optic Sensing and Deep Learning for Supersonic Inlet Flow Reconstruction and Buzz Diagnosis.” IEEE Sensors Journal 26 (18): 27402–15. https://doi.org/10.1109/jsen.2026.3720626
• Zhu, Jianwen, Luhua Liu, Guojian Tang, and Weimin Bao. 2014. “Optimal Diving Maneuver Strategy Considering Guidance Accuracy for Hypersonic Vehicle.” Acta Astronautica 104 (1): 231–42. https://doi.org/10.1016/j.actaastro.2014.07.026
• Zhu, Shihao, Yiming Luo, Yonglei Jia, et al. 2025b. “Gas Outgassing and Mitigation in Hemispherical Resonator Gyroscope for High Vacuum Maintenance.” Vacuum 242: 114732. https://doi.org/10.1016/j.vacuum.2025.114732
• Zhu, Jianfeng, Wenguo Luo, Yuqing Wei, Cheng Yan, and Yancheng You. 2020a. “Acoustic Modeling and Vibration Characteristics of Supersonic Inlet Buzz.” Energies 13 (8): 2048. https://doi.org/10.3390/en13082048
• Zhu, Hongyuan, Jing Ni, Nan Yang, Boyang Gao, and Xiaoxiong Liu. 2026d. “Research on Vision-Based Autonomous Landing Fusion Positioning Algorithm for Unmanned Aerial Vehicle.” Machines 14 (5): 460. https://doi.org/10.3390/machines14050460
• Zhu, Maolin, and Ning Qin. 2021. “Balancing Laminar Extension and Wave Drag for Transonic Swept Wings.” AIAA Journal 59 (5): 1660–72. https://doi.org/10.2514/1.j059914
• Zhu, Feng, Yiduo Qin, Qinqing Cai, Xi Chen, and Xiaohong Zhang. 2025a. “Combining Star Tracker and Gyroscope for Remote Sensing Satellite Attitude Determination: Algorithm Design and Performance Evaluation with Real Data.” IEEE Transactions on Instrumentation and Measurement 74: 1–15. https://doi.org/10.1109/tim.2025.3548235
• Zhu, Tiangao, Fangjun Qin, Zhiwei Li, et al. 2026c. “A Novel Matching Algorithm Based on SE2(3) in Local-Level Frame for Underwater Gravity-Aided Navigation.” Measurement 281: 122032. https://doi.org/10.1016/j.measurement.2026.122032
• Zhu, Tiangao, Fangjun Qin, An Li, Kailong Li, Jiujiang Yan, and Leiyuan Qian. 2025c. “The Novel Gravity-Matching Algorithm Based on Modified Adaptive Transformed Cubature Quaternion Estimation for Underwater Navigation.” Journal of Marine Science and Engineering 13 (6): 1150. https://doi.org/10.3390/jmse13061150
• Zhu, Ting, Yuan Ren, Lifen Wang, and Xuerui Zhai. 2021b. “Data Fusion in Redundant Inertial Measurement Unit Using a Fruit-Fly-Optimized Weighted Least Squares Algorithm.” IEEE Sensors Journal 21 (24): 27612–22. https://doi.org/10.1109/jsen.2021.3111647
• Zhu, Ting, Yuan Ren, Lifen Wang, Xuerui Zhai, Fandong Lu, and Tao Zou. 2021a. “Accuracy Improvement of a Redundant Inertial Measurement Unit Brought about by the Dual-Axis Rotational Motion.” In 2021 International Conference on Computer, Control and Robotics (ICCCR). IEEE. https://doi.org/10.1109/icccr49711.2021.9349375
• Zhu, Yijun, and Huilin Shang. 2023. “Jump and Pull-in Instability of a MEMS Gyroscope Vibrating System.” Micromachines 14 (7): 1396. https://doi.org/10.3390/mi14071396
• Zhu, Weibin, Casey S. Wallace, and Navid Yazdi. 2016b. “A Tri-Fold Inertial Measurement Unit Fabricated with a Batch 3-D Assembly Process.” In 2016 IEEE International Symposium on Inertial Sensors and Systems. IEEE. https://doi.org/10.1109/isiss.2016.7435547
• Zhu, M., and Y. Wu. 2023. “Accuracy Assessment of Inertial Navigation Computation without Initial Attitude Alignment.” In 2023 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss58390.2023.10361916
• Zhu, Bing, Miao Wu, Jiangning Xu, and Jingshu Li. 2018. “Robust Adaptive Unscented Kalman Filter and Its Application in Initial Alignment for Body Frame Velocity Aided Strapdown Inertial Navigation System.” Review of Scientific Instruments 89 (11): 115102. https://doi.org/10.1063/1.5046760
• Zhu, Ying, Rong Zhang, Qiuping Wu, and Guocheng Wang. 2026e. “Suppression of Schuler-Mode Navigation Errors in Inertial Navigation Systems Using FBPBPF.” IEEE Transactions on Instrumentation and Measurement: 1–1. https://doi.org/10.1109/tim.2026.3742048
• Zhu Qi-dan, Wang Tong, Zhang Wen, and Zhou Fang. 2009. “Variable Structure Approach Power Compensation System Design of an Automatic Carrier Landing System.” In 2009 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2009.5191918
• Zhuang, Xuye, Xinpeng Zou, Jianing Zhang, and Pinghua Li. 2025. “Improve the Performance of MEMS Gyroscope by Combination of Virtual Gyroscope and Improved Sage-Husa Adaptive Filtering Algorithm.” Measurement 244: 116538. https://doi.org/10.1016/j.measurement.2024.116538
• Zhuo, Chao, Jianbang Du, Haihong Tang, and Qingqing Liu. 2019. “Special Thermal Compensation Experiment and Algorithm Design for Inertial Navigation System.” In 2019 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss46986.2019.8943667
• Zhuo, Xiaobin, Xiangyin Zhang, and Yue Yu. 2023. “Integrated Guidance and Control System Design for Hypersonic Vehicle Based on Backstepping High-Order Sliding Mode Approach.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10240010
• Zhuolun, Li, Hu Jiwen, and Bai Jin. 2014. “Preliminary Study on the Attitude Determination System for Cruise Missile Based on IMM-UKF.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007443
• Zhuravlev, V. Ph., S. E. Perelvaev, B. P. Bodunov, and S. B. Bodunov. 2019. “New-Generation Small-Size Solid-State Wave Gyroscope for Strapdown Inertial Navigation Systems of Unmanned Aerial Vehicle.” In 2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). IEEE. https://doi.org/10.23919/icins.2019.8769344
• Zhuravlev, Ph., S. Perelyaev, and D. Borodulin. 2018. “Strapdown Inertial Navigation System of Minimum Dimension (3D Oscillator as a Complete Inertial Sensor).” In 2018 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2018.8577161
• Zichen Zhu, Shenshu Xiong, and Zhaoying Zhou. n.d. “A Micro Barometric Altimeter with Applications in Altitude-Holding Flight Control for MAVs.” In Proceedings of the 21st IEEE Instrumentation and Measurement Technology Conference (IEEE Cat. No.04CH37510). IEEE. https://doi.org/10.1109/imtc.2004.1351240
• Zijian, Cheng, Liang Bingbing, and Duan Jinlei. 2014. “Application of Digital Filter in Fiber Optic Gyroscope Inertial Navigation System.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007224
• Zimmer, Zachary, DoHwan Park, and Thomas Mathew. 2016. “Tolerance Limits under Normal Mixtures: Application to the Evaluation of Nuclear Power Plant Safety and to the Assessment of Circular Error Probable.” Computational Statistics & Data Analysis 103: 304–15. https://doi.org/10.1016/j.csda.2016.05.015
• Zimmer, Zachary, and Casey Turner. 2017. “Regression Based Circular Error Probable: An Application to Ballistic Systems.” Communications in Statistics: Case Studies, Data Analysis and Applications 3 (1–2): 48–54. https://doi.org/10.1080/23737484.2017.1406317
• Zipoy, David M. 1986. “Star Tracker for the Infrared.” Applied Optics 25 (16): 2845. https://doi.org/10.1364/ao.25.002845
• Zorn, A. H. 2002. “A Merging of System Technologies: All-Accelerometer Inertial Navigation and Gravity Gradiometry.” In 2002 IEEE Position Location and Navigation Symposium (IEEE Cat. No.02CH37284). IEEE. https://doi.org/10.1109/plans.2002.998890
• Zotov, S., R. Moore, S. Shtigluz, A. Lu, and A. Popp. 2022. “Quartz MEMS Accelerometer for EMCORE Inertial Technology from Tactical to High-End Navigation.” In 2022 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/iss55898.2022.9926393
• Zotov, S. A., I. P. Prikhodko, B. R. Simon, A. A. Trusov, and A. M. Shkel. 2014a. “Self-Calibrated MEMS Gyroscope with AM/FM Operational Modes, Dynamic Range of 180 dB and in-Run Bias Stability of 0.1 Deg/hr.” In 2014 DGON Inertial Sensors and Systems (ISS). IEEE. https://doi.org/10.1109/inertialsensors.2014.7049406
• Zotov, Sergei A., Brenton R. Simon, Gunjana Sharma, Alexander A. Trusov, and Andrei M. Shkel. 2014b. “Utilization of Mechanical Quadrature in Silicon MEMS Vibratory Gyroscope to Increase and Expand the Long Term in-Run Bias Stability.” In 2014 International Symposium on Inertial Sensors and Systems (ISISS). IEEE. https://doi.org/10.1109/isiss.2014.6782536
• Zou, Jiasheng, and Tijing Cai. 2022. “Improved Particle Swarm Optimization Screening Iterative Algorithm in Gravity Matching Navigation.” IEEE Sensors Journal 22 (21): 20866–76. https://doi.org/10.1109/jsen.2022.3208114
• Zou, Tao, Lifen Wang, Ting Zhu, Xuerui Zhai, and Chuchu Liu. 2022. “Fine Alignment Algorithm of Regular Tetrahedral Redundant Strapdown Inertial Navigation System Base on Kalman Filter.” In 2022 2nd International Conference on Electrical Engineering and Mechatronics Technology (ICEEMT). IEEE. https://doi.org/10.1109/iceemt56362.2022.9862624
• Zuber, Kamil, Duncan Wright, Jebum Choi, Joni Sytsma, and Colin Hall. 2026. “Compact Monolithic Star Tracker System.” Optics 7 (2): 25. https://doi.org/10.3390/opt7020025
• Zuo, Jingying, Jingjia Xue, Silong Zhang, et al. 2025. “Thermal Protection and Drag Reduction Performances of Shock-Combustion-Hydrocarbon Fueled Supersonic Film Cooling Interaction under Flight Mach 9.” Energy 336: 138526. https://doi.org/10.1016/j.energy.2025.138526
• Zuoming, Sun, Wang Shuhua, Li Junwei, Zhang Yazhou, and Chen Dapeng. 2016. “Analysis of Bias Thermal Stability of Interferometer Fiber-Optic Gyroscope Using a Solid-Core Polarization-Maintaining Photonic Crystal Fiber.” Optical Review 23 (6): 968–75. https://doi.org/10.1007/s10043-016-0280-0
• Zwahlen, P., Y. Dong, A-M. Nguyen, et al. 2012. “Breakthrough in High Performance Inertial Navigation Grade Sigma-Delta MEMS Accelerometer.” In Proceedings of the 2012 IEEE/ION Position, Location and Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2012.6236858

Primary Sources, Non-Peer-Reviewed

• “2 Optimal Experiment Design for Linear Regression Models – a Primer.” 2022. In Optimal Input Signals for Parameter Estimation. De Gruyter. https://doi.org/10.1515/9783110351040-002
• “3 Inertial Measurement Units.” 2001. In Inertial Navigation Systems with Geodetic Applications. DE GRUYTER. https://doi.org/10.1515/9783110800234.51
• “3 Inertial Measurement Units.” 2023. In Inertial Navigation Systems with Geodetic Applications. De Gruyter. https://doi.org/10.1515/9783110784329-003
• “3. Theater Ballistic Missile Defense Concepts.” 2020. In Regional Missile Defense from a Global Perspective. Stanford University Press. https://doi.org/10.1515/9780804796569-006
• “3D Problems of Rotating Detonation Wave in a Ramjet Engine Modeled on a Supercomputer.” 2018. Supercomputing Frontiers and Innovations 5 (2). https://doi.org/10.14529/jsfi180207
• “4 Inertial Navigation System.” 2001. In Inertial Navigation Systems with Geodetic Applications. DE GRUYTER. https://doi.org/10.1515/9783110800234.101
• “4 Inertial Navigation System.” 2023. In Inertial Navigation Systems with Geodetic Applications. De Gruyter. https://doi.org/10.1515/9783110784329-004
• “5. Strategic Force Planning during the Missile Gap Period.” 2019. In Eisenhower and the Missile Gap. Cornell University Press. https://doi.org/10.7591/9781501744785-007
• “8 Ballistic Missile Defense.” 2020. In Securing Freedom in the Global Commons. Stanford University Press. https://doi.org/10.1515/9780804775991-012
• \xd6ttl, Christoph, and Reinhard Willinger. 2021. “Thermodynamic and Mechanical Design Concept for Micro-Turbojet to Micro-Turboshaft Engine Conversion.” Preprint, . https://doi.org/10.1115/1.0002756v
• Abahre, A., Elbhar, D., and Kupervasser, O. 2019. “Fusion of Inertial Navigation System with 10 Axes and Computer Vision for UAV Navigation.” Functional Differential Equations, no. 26: 141–66. https://doi.org/10.26351/fde/26/3-4/1
• Abarbanel, Saul S. 1977. The Numerical Computations of Supersonic Flow past Blunt Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada035568
• Abate, Gregg, Ralf Duckerschein, and Wayne Hathaway. 2000. “Subsonic/transonic Free-Flight Tests of a Generic Missile with Grid Fins.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-937
• Abate, Gregg, and Arno Klomfass. 2005. “Affect upon Aeroballistic Parameter Identification from Flight Data Errors.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-439
• Abbas, Laith K., Chen Qian, and Piergiovanni Marzocca. 2014c. “Aerothermoelastic Control of Lifting Surfaces.” In Encyclopedia of Thermal Stresses. Springer Netherlands. https://doi.org/10.1007/978-94-007-2739-7_867
• Abbas, Mohammad, and David W. Riggins. 2016. “Exergy-Based Performance Analysis of a Turbojet Engine.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-4638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4638
• Abbas, Laith K., Rui Xiaoting, and Piergiovanni Marzocca. 2014a. “Aerothermoelastic Behavior of Flat and Curved Panels.” In Encyclopedia of Thermal Stresses. Springer Netherlands. https://doi.org/10.1007/978-94-007-2739-7_869
• Abbas, Laith K., Rui Xiaoting, and Piergiovanni Marzocca. 2014b. “Aerothermoelastic Behavior of Lifting Surfaces.” In Encyclopedia of Thermal Stresses. Springer Netherlands. https://doi.org/10.1007/978-94-007-2739-7_866
• Abdallah Mohamed, Mohamed. 2019. “Linearization of Anti-Tank Guided Missile.” Automation, Control and Intelligent Systems 7 (1): 9. https://doi.org/10.11648/j.acis.20190701.12
• Abdelfattah, Hesham, Peter Stechlinski, and Sameh Eisa. 2026. “Identifiability, Observability, Parameter Reduction, and State Estimation for Nonsmooth Dynamical Systems.” In 2026 LSU Symposium on Control, Learning, and Intelligent Systems Abstracts. LSU Libraries. https://doi.org/10.31390/lsucontrol.26.40
• Abdhul Rahuman, Mohomad Aqeel, and Kyuman Lee. 2026. “A Review of Vision-Based Terrain Relative Navigation for Planetary Descent and Landing of Space Vehicles.” International Journal of Aeronautical and Space Sciences 27 (4): 3482–3501. https://doi.org/10.1007/s42405-026-01139-1
• Abdulhamitbilal, Erkan, Sinan Şal, and Elbrous M. Jafarov. 2022. “Identification and Stability Analysis of a Turbojet Engine in Start-Up Mode.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2022-77985
• Abney, Eric, and Melissa McDaniel. 2005. “High Angle of Attack Aerodynamic Predictions Using Missile Datcom.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-5086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5086
• Abraham, Troy, Douglas F. Hunsaker, and David S. Lazzara. 2023. “Multi-Fidelity Comparison of Supersonic Wave Drag Prediction Methods Using Axisymmetric Bodies.” In AIAA SCITECH 2023 Forum. AIAA 2023-1899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1899
• Abrahamm, P. K., and B. Valsa. 2018. “Quality Assurance Challenges in Testing and Evaluation of Reusable Launch Vehicle Systems.” Current Science 114 (01): 144. https://doi.org/10.18520/cs/v114/i01/144-147
• Abreu, Rene. 1993. “Stellar Attitude Determination Accuracy with Multiple-Star-Tracking Advanced Star Tracker.” In SPIE Proceedings, vol. 1949, edited by George E. Sevaston, Richard H. Stanton. SPIE. https://doi.org/10.1117/12.157084
• Abu-Akeel, A. 1968. “Damping of High Frequency Brake Vibrations in Aircraft Landing Gear.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-312
• Abuaf, Nesim. 1976. Straight Duct Supersonic Diffuser Flow in a Ludwieg Tube with Upstream Diaphragm. Defense Technical Information Center. https://doi.org/10.21236/ada037674
• Abzug, Malcolm. 1999. “An Unconventional Tricycle Landing Gear.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4018
• Abzug, M., J. Craigie, and N. Morishita. 1970. “Satellite-Based Navigation/air Traffic Control Systems for Short Range Aircraft.” In 7th Annual Meeting and Technical Display. AIAA 1970-1338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1338
• Adami, Tony, and J. Zhu. 2007. “Control of a Flexible, Hypersonic Scramjet Vehicle Using a Differential Algebraic Approach.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6328
• Adami, Tony, and J. Zhu. 2008. “Control of a Flexible, Hypersonic Scramjet Vehicle Using a Differential Algebraic Approach.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7464
• Adams, D. E. 1956. “Introduction to Inertial Navigation.” Journal of Navigation 9 (3): 249–59. https://doi.org/10.1017/s0373463300036341
• Adams, D. E. 1960. “Inertial Methods in Hybrid Navigation Systems.” Journal of Navigation 13 (1): 61–70. https://doi.org/10.1017/s0373463300037243
• Adams, Richard, James Buffington, and Siva Banda. 1992. “Gain Scheduled Linear PID Autopilot for the AIAA Controls Design Challenge Aircraft.” In Astrodynamics Conference. AIAA 1992-4629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4629
• Adams, Gary W., and Michael J. Hadfield. 1983. “Breaking the Precision Barrier for Aircraft Inertial Systems.” Navigation 30 (4): 301–8. https://doi.org/10.1002/j.2161-4296.1983.tb00849.x
• Adams, N. C., E. M. Keberle, and W. Silsby. 1966. Electrostatic Charge Densities on an Electro- Optical Star Tracker. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/19670008976
• Adams, Richard H., and Eugene S. Rubin. 1958. A High Temperature Stream Tube for a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0200634
• Adams, J., Jr., W. Martindale, and M. Varner. 1984. “One-Dimensional Unsteady Modeling of Supersonic Inlet Unstart/restart.” In 22nd Aerospace Sciences Meeting. AIAA 1984-439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-439
• “Adaptive Neural Network–Based Autopilot Design.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-12
• “The Admiralty Gyro-Magnetic Compass—Type.” 1955. Journal of Navigation 8 (1): 83–83. https://doi.org/10.1017/s0373463300015526
• “Advances in Image Enhancement Techniques at the Atlantic Missile Range.” 1965. Optical Engineering 3 (5): 175–78. https://doi.org/10.1117/12.7971317
• Advisory Group for Aerospace Research and Development. 1984. Flight Test Techniques. AD-A147625. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19840026325
• Advisory Group for Aerospace Research and Development. 1999. System Identification for Integrated Aircraft Development and Flight Testing [l’Identification Des Systemes Pour Le Developpement Integre Des Aeronefs Et Les Essais En Vol]. AC/323(SCI)TP/7. North Atlantic Treaty Organization. https://ntrs.nasa.gov/citations/19990032449
• The Aegis Ballistic Missile Defense (BMD) System. 2010. https://doi.org/10.5040/9798216957508.0008
• Aerodynamic and Base Heating Studies on Space Shuttle Configurations. 1974. NASA-CR-120718. NASA. https://ntrs.nasa.gov/citations/19750012376
• Aerodynamic Heating of Blunt Nose Shapes at Mach Numbers up to 14. 1958. L-316. Langley Research Center. https://ntrs.nasa.gov/citations/20070030958
• “Aerothermodynamic Base Heating.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0049.0065
• Afonin, A. A., A. S. Sulakov, M. S. Maamo, and N. A. Shapovalov. 2022. “The Development and Evaluation of a Combined Initial Alignment Algorithm for Strapdown Inertial Navigation System.” Journal of Physics: Conference Series 2373 (7): 072023. https://doi.org/10.1088/1742-6596/2373/7/072023
• Agarwal, Ramesh, and Justin Augustinus. 1999. “Numerical Simulation of Compressible Viscous MHD Flows for Reducing Supersonic Drag of Blunt Bodies.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-601
• Agarwal, Ritvik, and Hao Xu. 2026. “Investigating the Efficacy of Simulated Quantum Computers for Drift Compensation in Inertial Navigation Systems.” In Sensors and Systems for Space Applications XIX, edited by Khanh D. Pham, Genshe Chen. SPIE. https://doi.org/10.1117/12.3098601
• Agarwalla, Soumik. 2025. “Comparative Analysis of Landing-Leg Architectures for Reusable Launch Vehicles.” International Journal For Multidisciplinary Research 7 (5): 58723. https://doi.org/10.36948/ijfmr.2025.v07i05.58723
• Aggarwal, Romesh, and Charles Moore. 1996. “A Terminal Guidance Algorithm for Ramjet-Powered Missiles.” In Guidance, Navigation, and Control Conference. AIAA 1996-3738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3738
• Agnone, A. 1984. “High Angle of Attack Aerodynamics of a Cruciformed Missile.” In 22nd Aerospace Sciences Meeting. AIAA 1984-507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-507
• Agrell, N., and L. Elmeland. 1984. “Transonic Aerodynamic Computations for a Canard Configuration.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2158
• Agterberg, Frits. 2023. “Circular Error Probability.” In Encyclopedia of Earth Sciences Series. Springer International Publishing. https://doi.org/10.1007/978-3-030-85040-1_58
• Aguiar, Ricardo Gonçalves de. n.d. “Adaptive Inertial Navigation System Based on Continual Learning in GPS-Denied Environments.” PhD diss., Universidade de São Paulo. https://doi.org/10.11606/d.55.2025.tde-29102025-191417
• Ahmad, J., S. Shanks, and P. Buning. 1993. “Aerodynamics of Powered Missile Separation from F/A-18 Aircraft.” In 31st Aerospace Sciences Meeting. AIAA 1993-766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-766
• “Aided INS: Observability and Feedback.” 2022. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch22
• Air Force Armament Lab Eglin AFB FL. 1988. Conference Proceedings of the America Institute for Aeronautics and Astronautics Missile Sciences Held in Monterey, California on 29 November: 1 December 1988. Volume 6. Navy Ballistic Missile Technology. Defense Technical Information Center. https://doi.org/10.21236/ada204865
• Air Force Flight Test Center Edwards AFB CA. 1974. Stability and Control. Volume 1. Stability and Control Flight Test Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada011561
• Air Force Research Lab Edwards AFB CA. 2000. KLIN Cycle Engine: Deeply Cooled Turbojet (DCTJ) Engine Performance Formulation. Defense Technical Information Center. https://doi.org/10.21236/ada404927
• “The Air Force Strategic Missile Program.” 2002. In Titan II. University of Arkansas Press. https://doi.org/10.2307/j.ctvvng4n.7
• “Aircraft Automatic Approach and Landing Using GPS.” 1996. In Global Positioning System: Theory and Applications, Volume II. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866395.0397.0425
• “Aircraft Landing Measurement System: A Description of the ALMS System That Can Continuously Monitor Aircraft Landing Performance in the Final Approach and Touchdown Phases.” 1971. Aircraft Engineering and Aerospace Technology 43 (1): 24–25. https://doi.org/10.1108/eb034716
• “Aircraft Landing Procedure.” 1998. Aircraft Engineering and Aerospace Technology 70 (4). https://doi.org/10.1108/aeat.1998.12770dad.002
• “Aircraft Type Air Scoops for Rotating Undercarriage Wheel.” 2002. Aircraft Engineering and Aerospace Technology 74 (2). https://doi.org/10.1108/aeat.2002.12774bad.002
• Akmeliawati, Rini, and Iven M. Y. Mareels. 2007. “Complex Stability Radius for Automatic Design of Gain-Scheduled Control Part II: Example on Autopilot Design.” In Studies in Computational Intelligence. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-73424-6_29
• Aksoy, Serra. 2025. “Python-Based Performance and Emissions Analysis of Turbojet and Turbofan Engines.” International Journal For Multidisciplinary Research 7 (4). https://doi.org/10.36948/ijfmr.2025.v07i04.54828
• Aksteter, J. W., E. K. Parks, and R. E. Bach Jr. 1995. Parameter Identification and Modeling of Longitudinal Aerodynamics. NASA-TM-111272. NASA. https://ntrs.nasa.gov/citations/19960027449
• Al Bakri, Fawaz. n.d. “Semi-Analytical Terminal and Automatic Approach and Landing Trajectory Planners for Unpowered Reusable Launch Vehicle.” PhD diss., University of Missouri–Columbia. https://doi.org/10.32469/10355/70012
• Al-Amari, Farah, Marwa Kaeber, and Saleh Alkhodari. 2022. “Mathematical Modelling and Performance Evaluation of the CM14 Turbojet Engine.” Journal of Engineering Research (Libya) 34: 1–16. https://doi.org/10.66411/jer.v34i.56
• AL-Bakri, Fawaz F., and Craig A. Kluever. 2017. “Automatic Approach and Landing Trajectory Planner for Unpowered Reusable Launch Vehicle.” Advances in Aerospace Science and Technology 02 (04): 31–47. https://doi.org/10.4236/aast.2017.24004
• Alaimo, Samantha, Lorenzo Pollini, and Heinrich Bülthoff. 2011. “Admittance-Based Bilateral Teleoperation with Time Delay for an Unmanned Aerial Vehicle Involved in an Obstacle Avoidance Task.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2011-6243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6243
• Alaverdi, Omeed, and Alfonso Paris. 2001. “Nonlinear Aerodynamic Model Extraction from Flight Test Data for the S-3B Viking.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4015. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4015
• Albayrak, Müge, Kerem Halıcıoğlu, Mustafa Tevfik Özlüdemir, et al. 2019. “The Use of the Automated Digital Zenith Camera System in Istanbul for the Determination of Astrogeodetic Vertical Deflection.” Boletim de Ciências Geodésicas 25 (4): e2019025. https://doi.org/10.1590/s1982-21702019000400025
• Aldrich, G., and W. Krabill. 1972. “A Versatile Kalman Technique for Aircraft or Missile State Estimation and Error Analysis Using Radar Tracking Data.” In Guidance and Control Conference. AIAA 1972-838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-838
• Aleinik, A. S., S. A. Volkovsky, V. S. Oshlakov, A. B. Mukhtubaev, and V. E. Strigalev. 2025. “Navigation-Grade Laser-Driven Fiber-Optic Gyroscope.” Gyroscopy and Navigation 16 (3): 279–83. https://doi.org/10.1134/s2075108725700257
• Alendar, A. D., A. N. Grunin, A. A. Evstigneev, A. I. Lanshin, and M. V. Siluyanova. 2022. “Influence of Inlet Pressure Distortion on the Engine Performance of a Supersonic Passenger Aircraft.” Russian Engineering Research 42 (7): 705–9. https://doi.org/10.3103/s1068798x2207005x
• Alexander, W. 1968. “A Discussion of Governing Decelerator Performance and Design Parameters in the Supersonic Flight Regime.” In 2nd Aerodynamic Deceleration Systems Conference. AIAA 1968-938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-938
• Alexander, N. 1969. “Miniature Floated Inertial Platform.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-835
• Alexander, Tolochko. 2024. “Our Journey to Poplar Grove Began with This Missile (on Flight Tests of the RT-2 Intercontinental Ballistic Missile on the Plesetsk Proving Ground).” TECHNOLOGOS, no. 2: 111–24. https://doi.org/10.15593/perm.kipf/2024.2.09
• Alexandrov, A. D., V. V. Kazakov, and K. T. Tsaturian. 1980. “Aircraft Landing Digital Control System.” In Automatic Control in Space. Elsevier. https://doi.org/10.1016/b978-0-08-024449-5.50044-8
• Alexandrov, V., A. Kraiko, and K. Reent. 2001. “Determination of the Integral and Local Characteristics of Supersonic Pulsed Detonation Ramjet Engine (SPDRE).” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1788. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1788
• Alford, Joseph S., and Earl L. Auyer. 1954. “Turbojet-Engine Design Problems for Supersonic Flight.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/540253
• Alford, J. S., D. P. Davies, and L. C. Young. 1962. “Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/620300
• Alford, J. S., and H. P. Durand. 1964. “Application of Dynamic Simulation Techniques to Engine-Inlet Compatibility Problems on the SST.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/640304
• “The Algorithm of the Color Signal Recognition at Landing an Unmanned Aerial Vehicle on an Aircraft Carrier in Autonomous Mode.” 2020. Automation Modern Techologies: 78. https://doi.org/10.36652/0869-4931-2020-74-2-78-84
• Alharam, Aysha, Yaqoob Alqassab, and Basel Altawil. 2024. A Low-Cost Star Tracker System with High Accuracy for Nanosatellites Applications. https://doi.org/10.52202/078372-0099
• Alhassan, Hassan Majed, and Nemat Allah Ghahremani. 2021. “A new predictive filter for nonlinear alignment model of stationary MEMS inertial sensors.” Metrology and Measurement Systems: 673–91. https://doi.org/10.24425/mms.2021.137702
• Ali, Jamshaid. 2007. “Performance Comparison of Nonlinear Filters for Astro-Inertial Integrated Navigation System.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6662. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6662
• Ali, Afrah A., Nizar H. Abbas, and Ahmed Hameed Kaleel. 2024. “Automatic Aircraft Landing System: A Review.” Journal of Engineering 30 (9): 165–89. https://doi.org/10.31026/j.eng.2024.09.09
• Ali Rahgoshay, Mohammad, Paknoosh Karimaghaie, and Fereidoon Shabaninia. 2017. “Initial Alignment of Fiber-Optic Inertial Navigation System with Large Misalignment Angles Based on Generalized Proportional-Integral-Derivative Filter.” International Journal on Smart Sensing and Intelligent Systems 10 (3): 1–17. https://doi.org/10.21307/ijssis-2017-226
• Alikiotis, Dimitri. 1987. “Inertial/multisensor Navigation.” In NASA, Langley Research Center, Joint University Program for Air Transportation Research, 1985. https://ntrs.nasa.gov/citations/19870018169
• Alizad, Meysam, and Hadi Hadi. 2023. “Decentralized Triangular Relative Navigation of Multiple UAVs Based on Relative Range and Inertial Measurements.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3306085/v1
• “All Things Must End: The Death of Cruise Missile Testing.” 2006. In Just Dummies. University of Calgary Press. https://doi.org/10.1515/9781552383780-011
• Allen, F. C. 1954. “Unsymmetrical Flight Loads Problems in Supersonic Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/540162
• Allen, H. J. 1964. The Aerodynamic Heating of Atmosphere Entry Vehicles: A Review. NASA-TM-X-54056. NASA. https://ntrs.nasa.gov/citations/19640013352
• Allen, H. J. 1966. The Aerodynamic Heating of Atmosphere Entry Vehicles: A Review. NASA. https://ntrs.nasa.gov/citations/19660045863
• Allen, J. M. 1981. “Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19810036403
• Allen, J. L., and Andrew Beke. 1953. Force and Pressure Recovery Characteristics at Supersonic Speeds of a Conical Spike Inlet with a Bypass Discharging from the Top or Bottom of the Diffuser in an Axial Direction. NACA-RM-E53A29. NASA. https://ntrs.nasa.gov/citations/19930087574
• Allen, D. E., Sidney M. Bennett, J. Brunner, Richard B. Dyott, and Steven R. Emge. 1995. “All-Fiber Gyroscope for Land Navigation.” In SPIE Proceedings, vol. 2510, edited by Ramon P. DePaula, John W. Berthold III. SPIE. https://doi.org/10.1117/12.221715
• Allen, Julian H., and A. J. Eggers Jr. 1957. A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth’s Atmosphere at High Supersonic Speeds. NACA-TN-4047. NASA. https://ntrs.nasa.gov/citations/19930084817
• Allen, H. Julian, and A. J. Eggers Jr. 1958. A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth’s Atmosphere at High Supersonic Speeds. NACA-TR-1381. NASA. https://ntrs.nasa.gov/citations/19930091020
• Allen, F. C., H. D. Meriwether, and L. B. Mosby. 1962. Landing Loads Investigation Laboratory Drop Tests. Defense Technical Information Center. https://doi.org/10.21236/ad0404489
• Allen, J., and J. Pittman. 1983. “Analysis of Surface Pressure Distributions on Two Elliptic Missile Configurations.” In Applied Aerodynamics Conference. AIAA 1983-1841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1841
• Allen, F. C., D. M. Rehder, and L. B. Mosby. 1963b. A Study of Rough-Terrain-Induced Structural Landing Loads. Phases 1 and 2. Defense Technical Information Center. https://doi.org/10.21236/ad0430063
• Allen, B., D. Sauvageau, and C. Joyner. 1994. “Reusable Launch Vehicle Design Flexibility.” In Space Programs and Technologies Conference and Exhibit. AIAA 1994-4499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-4499
• Allen, H. J., A. Seiff, and W. Winovich. 1963a. Aerodynamic Heating of Conical Entry Vehicles at Speeds in Excess of Earth Parabolic Speed. NASA-TR-R-185. NASA. https://ntrs.nasa.gov/citations/19640002198
• Allen, E. C., and T. Tuttle. 1973. Static Stability and Control Effectiveness of Models 12-0 and 34-0 of the Vehicle 3 Configuration, Volume 3. NASA-CR-128780-VOL-3. NASA. https://ntrs.nasa.gov/citations/19740004405
• Allen, Jerry M., and Carolyn B. Watson. 1994. Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails. NASA-TM-4582. NASA. https://ntrs.nasa.gov/citations/19950009654
• Allerton, D. J., and M. C. Gia. 1996. “Oct-Tree Terrain Modelling Methods for Terrain Reference Navigation Systems.” Aeronautical Journal 100 (995): 157–64. https://doi.org/10.1017/s0001924000027469
• Alpert, Joel. 1987. “Miss Distance Analysis for Command Guided Missiles.” In Guidance, Navigation and Control Conference. AIAA 1987-2582. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2582
• Alsaraj, Adel, and Gene Stuffle. 2015. “Missile Autopilot Design Using Artificial Neural Networks.” International Journal of Engineering Trends and Technology 29 (6): 284–89. https://doi.org/10.14445/22315381/ijett-v29p253
• Althsuler, E. E. 1983. “A Review of Tropospheric Refraction Effects on Earth-to-Satellite Systems.” In NASA. Goddard Space Flight Center Proc. of the 16th Ann. Precise Time and Time Interval (PTTI) Appl. and Planning Meeting. https://ntrs.nasa.gov/citations/19850020923
• Altman, J. 1965. “Some Considerations Associated with Flight Testing the Commercial Supersonic Transport.” In Flight Testing Conference. AIAA 1965-220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-220
• Altunkaya, Ege C., and Ibrahim Ozkol. 2023. “Auto-Landing Fault-Tolerant Control System Design for a Light Aircraft.” In AIAA SCITECH 2023 Forum. AIAA 2023-2510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2510
• Aly, Mohsen. 1999. “Linear Model Evaluation of Command Guidance System.” International Conference on Aerospace Sciences and Aviation Technology 8 (ASAT CONFERENCE): 1–13. https://doi.org/10.21608/asat.1999.25158
• Amacker, J. Z. 1967. “Inertial Navigation System Testing 1967.” Journal of Navigation 20 (4): 432–49. https://doi.org/10.1017/s0373463300030769
• Amacker, Jefferson, and John Graff. 1965. “Inertial Navigation System Testing at Holloman AFB.” In Guidance Control Conference. AIAA 1965-1247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1247
• Amin, N., and D. Hollweger. 1981. “F/A-18A Inlet/engine Compatibility Flight Test Results.” In 17th Joint Propulsion Conference. AIAA 1981-1393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1393
• Ammons, E. 1979. “F-16 Flight Control System Redundancy Concepts.” In Guidance and Control Conference. AIAA 1979-1771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1771
• An, Shi Qi, and Jun Kai Zhang. 2015. “The Study of Kalman Filtering Algorithm in the Initial Alignment of Strapdown Inertial Navigation System.” Applied Mechanics and Materials 740: 596–99. https://doi.org/10.4028/www.scientific.net/amm.740.596
• Ananthapadmanaban, Ramprakash, and T. M. Murganandam. 2016. “Experimental Study on Start/Unstart Behavior of Two Dimensional Mixed Compression Inlet by Cowl Actuation.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-5072. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5072
• Anderson, Adrian. 1958. Aerodynamic Test Results of Two Configurations of a Proposed Bomber Defense Missile at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0305026
• Anderson, A. 1960. Force Tests of Lenticular Configurations at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0315671
• Anderson, G. 1970. “Air-to-Air Missile Trajectories for Maximization of Launch Range.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-980. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-980
• Anderson, William P. 1979. Target Missile Airframe Costs. Defense Technical Information Center. https://doi.org/10.21236/ada073314
• Anderson, R. 1983. “Aircraft Engine Inlet Pressure Distortion Testing in a Ground Test Facility.” In 19th Joint Propulsion Conference. AIAA 1983-1233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1233
• Anderson, S. 1984a. “Handling Qualities Related to Stall/spin Accidents of Supersonic Fighter Aircraft.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2093
• Anderson, B. 1984b. “Three-Dimensional Viscous Design Methodology for Advanced Technologyaircraft Supersonic Inlet Systems.” In 22nd Aerospace Sciences Meeting. AIAA 1984-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-194
• Anderson, Seth B. 1986. A Look at Handling Qualities of Canard Configurations. NASA-TM-88354. NASA. https://ntrs.nasa.gov/citations/19870013196
• Anderson, Bernhard H. 2014. “The Origin of Inlet Buzz in a Mach 1.7 Low Boom Inlet Design.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3799
• Anderson, B. H., D. N. Bowditch, and W. K. Tabata. 1960. Performance of a Turbojet Engine in Combination with an External-Internal-Compression Inlet to Mach 2.88. NASA-TM-X-254. NASA. https://ntrs.nasa.gov/citations/19630002315
• Anderson, R. C., J. A. Davenport, and C. Jekeli. 2000. “Determination of Gravity Data Spacing Required for Inertial Navigation.” Navigation 47 (1): 1–6. https://doi.org/10.1002/j.2161-4296.2000.tb02417.x
• Anderson, S. B., and T. W. Feistel. 1985. “A Historic Review of Canard Configurations.” In Atmospheric Flight Mechanics Conference. https://ntrs.nasa.gov/citations/19850061703
• Anderson, R., C. Gillard, N. Buholz, and K. Pettipiece. 1983. “New Concept for a Guide Star Tracker.” In Guidance and Control Conference. AIAA 1983-2288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2288
• Anderson, Bernhard, and Ralph Levy. 1991. “A Design Strategy for the Use of Vortex Generators to Manage Inlet-Engine Distortion Using Computational Fluid Dynamics.” In 27th Joint Propulsion Conference. AIAA 1991-2474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2474
• Andrade, Luis, Robin Langley, and Jiannan Yang. 2025. “Sensitivity Analysis Based on the Fisher Information Matrix Applied to Systems with Random Design Inputs.” Journal of Mechanical Design 147 (8): 081704. https://doi.org/10.1115/1.4067867
• Andre, M., and J. Czaja. 1982. “Minuteman Inertial Guidance Assessment: The Next Best Thing to Flight Tests.” In Guidance and Control Conference. AIAA 1982-1550. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1550
• Andreadis, Dean, Alan Drake, Joseph L. Garrett, Christopher D. Gettinger, and Stephen S. Hoxie. 2002. Design Considerations of Istar Hydrocarbon Fueled Combustor Operating in Air Augmented Rocket, Ramjet and Scramjet Modes. Pratt and Whitney Space Propulsion. https://ntrs.nasa.gov/citations/20030068741
• Andresen, F. P., and L. S. Davis. 1984. Visual Position Determination for Autonomous Vehicle Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada156007
• Andrews, Gregory L. n.d. “Implementation Considerations for Vision-Aided Inertial Navigation.” PhD diss., Northeastern University. https://doi.org/10.17760/d10017173
• Andrews, W. H. 1977. “Space Shuttle Orbiter Approach and Landing Program Status.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19770061462
• Andrews, J. 1998. “Status of the Kistler Reusable Launch Vehicle.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3955
• Andreyev, S. V., В. В. Ильиных, O. A. Ilinykh, М. С. Чертков, and A. V. Klyuchnikov. 2018. “Estimation of Inertial Sensors Error Impact on Platformless Inertial Navigation System Accuracy.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 2: 29–34. https://doi.org/10.38013/2542-0542-2018-2-29-34
• Andrisani, ck, Dominick, II. 1995. “Optically Aided Homing Missile Guidance.” In Guidance, Navigation, and Control Conference. AIAA 1995-3280. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3280
• Andronikou, A. M., G. A. Bekey, and F. Y. Hadaegh. 1983. “Identifiability of Nonlinear Systems with Hysteretic Elements.” Journal of Dynamic Systems, Measurement, and Control 105 (4): 209–14. https://doi.org/10.1115/1.3140660
• Andrus, Jan F. 1979. Nonlinear Guidance of Air-to-Air Missiles. Defense Technical Information Center. https://doi.org/10.21236/ada214688
• Angelucci, S., G. Roffe, and P. Baronti. 1979. “The Single Throat Ramjet and Its Application to Cruising and Accelerating Systemscruise Missile Ramjet Engine Performance.” In 4th International Symposium on Air Breathing Engines. AIAA 1979-7043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-7043
• Anggoro, Annga Ardi. 2021. “Identification of Damage Gear Landing System of Cessna Aircraft.” Vortex 2 (1): 39. https://doi.org/10.28989/vortex.v2i1.933
• Anguelova, Milena, and Bernt Wennberg. 2009. “Input-Output Representation and Identifiability of Delay Parameters for Nonlinear Systems with Multiple Time-Delays.” In Lecture Notes in Control and Information Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-02897-7_21
• Annan, Richard Fiifi, Xiaoyun Wan, Ruijie Hao, and Fei Wang. 2023. “Global Marine Gravity Gradient Tensor Inverted from Altimetry-Derived Deflection of the Vertical: CUGB2023GRAD.” Preprint, . https://doi.org/10.5194/essd-2023-85
• Aoyagi, K., and W. H. Tolhurst. 1964. Large-Scale Low-Speed Wind-Tunnel Tests of a Delta Winged Supersonic Transport Model to Determine Aerodynamic Effects of Forward or Reverse Thrust. NASA-TM-X-1017. NASA. https://ntrs.nasa.gov/citations/19670022812
• Apochkina, A. F., T. V. Prokofieva, and U. A. Aparovich. 2025. “Recognition of Ballistic Missile Types Using Neural Networks Based on Trajectory Information.” Doklady BGUIR 23 (5): 58–65. https://doi.org/10.35596/1729-7648-2025-23-5-58-65
• “Apparatus for Rotating an Aircraft Wheel Prior to Landing.” 1998. Aircraft Engineering and Aerospace Technology 70 (2). https://doi.org/10.1108/aeat.1998.12770bad.003
• “Appendix B: Identifiability of Initial Conditions and Bias Parameters.” 2006. In Flight Vehicle System Identification. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866852.0493.0496
• “Appendix B: Inertial Navigation System Error Budgets.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_appendixb
• “Appendix C: Inertial System Configurations.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_appendixc
• “Appendix F. Procecdure for Generating Gravity Disturbance Realizations.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0317.0320
• “Application of Strongly Tracking Kalman Filter in MEMS Gyroscope Bias Compensation.” 2017. In 2017 6th International Conference on Advanced Materials and Computer Science (ICAMCS 2017). Clausius Scientific Press Inc. https://doi.org/10.23977/icamcs.2017.1004
• Arbabmir, Mohammadvali, and Masoud Ebrahimi. 2020. “Simultaneous Filter Tuning and Calibration of the Camera and Inertial Measurement Unit Camera for a Vision Inertial Navigation System.” IET Image Processing 14 (12): 2756–67. https://doi.org/10.1049/iet-ipr.2019.0007
• Arbic, Richard G., and Warren Gillespie Jr. 1953. Summary of Rocket-Model Tests at Zero Lift of the Northrop MX-775B Missile Configuration from Mach Numbers of 0.9 to 1.8. NACA-RM-SL53J02. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026523
• Arbic, Richard G., George White, and Warren Gillespie Jr. 1953. Some Approximate Methods for Estimating the Effects of Aeroelastic Bending of Rocket-Propelled Model-Booster Combinations. NACA-RM-L53A08. NASA. https://ntrs.nasa.gov/citations/19930089134
• Aretskin-Hariton, Eliot D., and Aaron J. Swank. 2015. “Star Tracker Performance Estimate with IMU.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20150002107
• Arif, A. A., and R. A. Sasongko. 2021. “Flight Test Evaluation for Tilt Rotor Unmanned Aerial Vehicle Development.” AVIA 3 (1). https://doi.org/10.47355/avia.v3i1.39
• Arlinger, Bert G. 1976. “Axisymmetric Inlet Flow at Low Supersonic Mach Numbers.” In Symposium Transsonicum II. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_21
• Armenise, M. N. 2010a. “Emerging Gyroscope Technologies.” In Advances in Gyroscope Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-15494-2_7
• Armenise, M. N. 2010b. “Fiber Optic Gyroscopes.” In Advances in Gyroscope Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-15494-2_4
• Armenise, M. N. 2010c. “He–Ne and Solid-State Ring Laser Gyroscopes.” In Advances in Gyroscope Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-15494-2_3
• Armenise, M. N. 2010d. “MEMS Gyroscopes.” In Advances in Gyroscope Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-15494-2_6
• Armenta, Francisco X., and Timothy T. Takahashi. 2021. “Revisiting the Transonic Area Rule for Conceptual Aerodynamic Design.” In AIAA Aviation 2021 Forum. AIAA 2021-2441. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2441
• Armstrong, Johnny G. 1977. Flight Planning and Conduct of the X-24B Research Aircraft Flight Test Program. Defense Technical Information Center. https://doi.org/10.21236/adb029224
• Army Aviation Board Fort Rucker Al. 1962. Evaluation of RYANA IV Doppler Navigation System. Defense Technical Information Center. https://doi.org/10.21236/ada030561
• Army Missile Command Redstone Arsenal AL. 1961. Development of the Corporal: The Embryo of the Army Missile Program, Volume II: Supporting Data. Documents 1 through 31. Defense Technical Information Center. https://doi.org/10.21236/ada434478
• Army Scientific Advisory Panel Washington Dc. 1975a. Report II of the Army Scientific Advisory Panel Ad Hoc Group on White Sands Missile Range Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ada020372
• Army Scientific Advisory Panel Washington Dc. 1975b. Report of the Army Scientific Advisory Panel AD HOC Group on White Sands Missile Range Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ada007836
• Arora, Rajesh, and M. Ananthasayanam. 2003. “Trajectory Design for a Reusable Launch Vehicle Demonstrator during Re-Entry Phase.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5547
• Arora, Rajesh, J. George, and X. Athnasius. 2003. “Trajectory Design for a Flyback Mission of a Reusable Launch Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5546
• Arslanova, M. L., and G. A. Trutnev. 2017. “Basics of Simulation Solid-State Wave Gyroscope Resonator.” Intellekt. Sist. Proizv. 15 (3): 4. https://doi.org/10.22213/2410-9304-2017-3-4-17
• Arunachalam, B. 2025. “Stellar Navigation and Location Fix: A Manual Extract.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781003724162-5
• Arvind Suthar, Nishant Gawade, Yash Kava, Nathen Tuscano, and Nitika Rai. 2024. “Inertial Navigation System for Aircraft and Spacecraft.” International Journal For Multidisciplinary Research 6 (6). https://doi.org/10.36948/ijfmr.2024.v06i06.32836
• Arık, Ahmet Enes, and Boğaç Bilgiç. 2022. “Fuzzy Control of a Landing Gear System with Oleo-Pneumatic Shock Absorber to Reduce Aircraft Vibrations by Landing Impacts.” Aircraft Engineering and Aerospace Technology 95 (2): 284–91. https://doi.org/10.1108/aeat-01-2022-0028
• Aschaffenburg, Hans W. 1962. The Design and Development of an Inertial Altitude System. Defense Technical Information Center. https://doi.org/10.21236/ad0400701
• Ash, Michael, Harold Morris, and Rex Peters. 1998. “Proposed IEEE Accelerometer Standard and Other Inertial Sensor Standards.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4405. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4405
• Ashry, Mahmoud M., Mohamed K. Kamel, and Ahmed M. Shehata. 2019. “Modeling of Micro Turbojet Engine.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-3911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3911
• Asim, Muhammad Farhat, Jehanzeb Masud, Suhail Akhtar, Bilal Malik, Taimur Ali Shams, and Ibrahim Sher. 2022. “On Improvement of Flight Dynamic Model of a Supersonic Aircraft Using Wind Tunnel to Flight Corrections.” In AIAA SCITECH 2022 Forum. AIAA 2022-0690. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0690
• Askar, Naiel, Hong Xiong, and Guoqing Liu. 2018. “Multi-Hypothesis Post-Processing for Improving Air-to-Air Radar Tracking Accuracy.” In Radar Sensor Technology XXII, edited by Kenneth I. Ranney, Armin Doerry. SPIE. https://doi.org/10.1117/12.2304000
• Askari, Rasoul, Mohammad Reza Soltani, and Afshin Khajeh Fard. 2017. “Geometrical Scaling Effects on Supersonic Inlet Performance.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2017-71912
• Atabay, Elmas, and Ibrahim Ozkol. 2013. “Application of a Magnetorheological Damper Modeled Using the Current–dependent Bouc–Wen Model for Shimmy Suppression in a Torsional Nose Landing Gear with and without Freeplay.” Journal of Vibration and Control 20 (11): 1622–44. https://doi.org/10.1177/1077546312468925
• Atay, Görkem, and Can Kumartaslioglu. 2024. “An Engineering Approach to Calculate Aerodynamic Heating on Supersonic Missiles.” In AIAA SCITECH 2024 Forum. AIAA 2024-1877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1877
• Atmeh, Ghassan M., Wahba I. Al-Taq, and Zeaid Hasan. 2011. “A Nonlinear Automatic Landing Control System for a UAV.” In Volume 7: Dynamic Systems and Control; Mechatronics and Intelligent Machines, Parts A and B. ASMEDC. https://doi.org/10.1115/imece2011-63264
• Audric, Derren, M. S. Dzaki Fayyadh, Javensius Sembiring, and Idris Eko Putro. 2023. “Dynamic Characteristics Analysis of Missile in Ballistic Flight.” In AIP Conference Proceedings, vol. 2981. AIP Publishing. https://doi.org/10.1063/5.0182689
• Auman, Lamar. 1993. “Wind Tunnel Investigation with an Operational Turbojet Engine.” In 31st Aerospace Sciences Meeting. AIAA 1993-36. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-36
• Auman, Lamar, and Richard Kreeger. 1998. “Aerodynamic Characteristics of a Canard-Controlled Missile with a Free-Spinning Tail.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-410
• Auman, Lamar, and Brett Wilks. 2003. “Supersonic and Hypersonic Minimum Drag for Bodies of Revolution.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3417
• Auman, Lamar, Gary Winn, and Jon Hall. 1994. “Wind Tunnel Investigation of a Spinning Missile with Active Canard Control.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-722
• Author, Not Given. 1981. Space and Missile Reliability and Safety Programs. Technical Service Agreement TSA 79-286. Final Report. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/5598781
• “Automatic Detection and Suppression of Inlet Buzz.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0453.0460
• “Automatic Landing: A Report on the Progress towards Category Three.” 1969. Aircraft Engineering and Aerospace Technology 41 (4): 29–31. https://doi.org/10.1108/eb034494
• “Automatic Landing: An Introduction to the Requirement for Autoflare for the Trident, a Description of Smiths SEP.5 Flight Control System and Typical Operating Instructions for Approach and Landing.” 1964. Aircraft Engineering and Aerospace Technology 36 (6): 160–65. https://doi.org/10.1108/eb033884
• Automatic Take-off and Landing System. 2011. Wiley. https://doi.org/10.1002/9781118601808.ch16
• Avanesov, G. A., R. V. Bessonov, A. N. Kurkina, M. B. Lyudomirskii, I. S. Kayutin, and N. E. Yamshchikov. 2013. “Autonomous Strapdown Stellar-Inertial Navigation Systems: Design Principles, Operating Modes and Operational Experience.” Gyroscopy and Navigation 4 (4): 204–15. https://doi.org/10.1134/s2075108713040032
• Avery, D. E., P. A. Kerr, and A. R. Wieting. 1983. “Experimental Aerodynamic Heating to Simulated Shuttle Tiles.” In AIAA Thermophys. Conf.. https://ntrs.nasa.gov/citations/19830014276
• Averyanov, Igor O. 2022. “Cargo with Dampers Parachute Vertical Landing Dynamics Research.” Trudy MAI, no. 127. https://doi.org/10.34759/trd-2022-127-02
• Avrutov, Vadym, Nadiia Bouraou, Sergii Davydenko, et al. 2022. “Wavelet De-Noising of Mems Inertial Measurement Unit for Autonomous Latitude Determination.” Preprint, . https://doi.org/10.2139/ssrn.4042780
• Awin, Otman Ali. 2013. “Application of Extended Kalman Filter Algorithm in SDINS/GPS Integrated Inertial Navigation System.” Applied Mechanics and Materials 367: 528–35. https://doi.org/10.4028/www.scientific.net/amm.367.528
• Axelson, J. A., J. J. Brownson, E. D. Katzen, J. G. Marvin, and H. L. Seegmiller. 1970. Static Aerodynamics, Flow Fields and Aerodynamic Heating of Space Shuttle Orbiters. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19700028518
• Ayaz, Süleyman Kağan, and Önder Altuntaş. 2017. “Assessment of a Ramjet Engine for Different Mach Numbers.” International Journal of Sustainable Aviation 3 (4): 325. https://doi.org/10.1504/ijsa.2017.090299
• Aygun, Hakan. 2022. “Investigation of Effects of Several Design Parameters on Exergo-Sustainability Metrics for Twin-Spool Turbojet Engine at Different Flight Conditions.” International Journal of Exergy 37 (2): 200. https://doi.org/10.1504/ijex.2022.120572
• Baals, D., and R. Harris Jr. 1968. “Aerodynamic Design Integration of Supersonic Aircraft.” In 5th Annual Meeting and Technical Display. AIAA 1968-1018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1018
• Baba, Yoriaki, Hiroyuki Takano, and Kichiro Takao. 1991. “Missile Guidance System against a Ballistic Missile.” In Navigation and Control Conference. AIAA 1991-2702. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2702
• Baber, H. T., Jr., and M. T. Moul. 1955. Longitudinal Stability and Control Characteristics as Determined by the Rocket-Model Technique for an Inline, Cruciform, Canard Missile Configuration with a Low-Aspect-Ratio Wing Having Trailing-Edge Flap Controls for a Mach Number Range of 0.7 to 1.8. NACA-RM-L54B12. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19690067250
• Babinsky, Holger. 2014. Flow Control for Supersonic Inlet Applications. Defense Technical Information Center. https://doi.org/10.21236/ada602774
• Babish, Charles, III. 1966. “Drag Let-l Staging through Modification of Supersonic Wake Fiews by Trailing Aerodynamic Decelerators.” In Aerodynamic Deceleration Systems Conference. AIAA 1966-1506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1506
• Babu, V. 2021a. “Ramjet and Scramjet Engine.” In Fundamentals of Propulsion. Springer International Publishing. https://doi.org/10.1007/978-3-030-79945-8_8
• Babu, V. 2021b. “The Turbojet Engine.” In Fundamentals of Propulsion. Springer International Publishing. https://doi.org/10.1007/978-3-030-79945-8_5
• Bacon, David. 2012. “Terrestrial Line-of-Sight Links.” In Propagation of Radiowaves. Institution of Engineering and Technology. https://doi.org/10.1049/pbew056e_ch14
• Badekas, John, and Ivan I. Mueller. 1968. “Interpolation of the Vertical Deflection from Horizontal Gravity Gradients.” Journal of Geophysical Research 73 (22): 6869–78. https://doi.org/10.1029/jb073i022p06869
• Bae, Jonghee, Youdan Kim, and Hee Seob Kim. 2010. “Satellite Attitude Determination and Estimation Using Two Star Trackers.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8447
• Bae, Sungkoo, and Bob Schutz. 2002. “ICESAT/GLAS Attitude Determination Using a Batch Least Squares Estimator during Star Tracker Starless Periods.” In AIAA/AAS Astrodynamics Specialist Conference and Exhibit. AIAA 2002-4915. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4915
• Baer, A. L. 1966. The Effects of Flow through an Aircraft Pitot-Static Probe at Supersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ad0477832
• Baerst, C., and N. Hughes. 1978. “Status of an Ultra-Low-Cost Turbojet Engine.” In 14th Joint Propulsion Conference. AIAA 1978-965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-965
• Bahrami, K. 1977. “Inertial Attitude Control of Voyager Spacecraft Using Dry Tuned Rotor Gyro.” In Guidance and Control Conference. AIAA 1977-1112. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1112
• Bai, Xian Lin, Yong Le Lu, and Yu Liu. 2011. “Research on the Short-Time Bias Stability of the Solid Vibration Beam Gyroscope.” Advanced materials research 179-180: 86–91. https://doi.org/10.4028/www.scientific.net/amr.179-180.86
• Bai, Chengchao, Fei Lu, and Xibao Xu. 2017. “Hybrid BTT/STT Missile Autopilot Design.” Aircraft Engineering and Aerospace Technology 89 (6): 809–14. https://doi.org/10.1108/aeat-05-2015-0134
• Bai, Lijian, and Yue Wang. 2017. “An Anti-Disturbance High-Precision Alignment for Distributed POS Based on Inertial Reference Frame.” In AIP Conference Proceedings, vol. 1808. Author(s). https://doi.org/10.1063/1.4977387
• Baird, Weldon R. 1964. Summary of the Aerothermoelastic Development Program for the X-20A (Dyna-Soar). Defense Technical Information Center. https://doi.org/10.21236/ad0450460
• Baird, Bradley W. 2021. “Overload Detection/Health Monitoring Landing Gear Sensor System Proposal.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14658024
• Baker, C. 2006. “Passive Radar Tracking.” In IET Seminar on the Future of Civil Radar, vol. 2006. IEE. https://doi.org/10.1049/ic:20060150
• Baker, D. C., and L. L. Galigher. 1960. Investigation of Static Stability and Aerodynamic Effects of Control Jets on a 1/3-SCALE Pye Wacket Missile at Transonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ad0320438
• Baklanov, Fedor, and Johann Dambeck. 2017. “Observability Analysis and Concept of Usage of Air Data Attitude and Heading Reference Systems (AD-AHRS): Observability and Concept of Usage of AD-AHRS.” Navigation 64 (4): 427–46. https://doi.org/10.1002/navi.206
• Bakulin, V. N., S. V. Borzykh, and V. V. Voronin. 2016. “Space Vehicle Landing Dynamics at Failure of Landing Gear.” Russian Aeronautics (Iz VUZ) 59 (1): 23–28. https://doi.org/10.3103/s1068799816010049
• Bakunowicz, Jerzy, and Paweł Rzucidło. 2016. 2.2: Coupling of MEMS Gyroscope Application with Wavelet Analysis for Detection of Airframe Oscillations in Flight Conditions. https://doi.org/10.5162/etc2016/2.2
• Balakrishnan, A. V. n.d. “On the Application of Kalman Filtering to Correct Errors Due to Vertical Deflections in Inertial Navigation.” In Lecture Notes in Control and Information Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/bfb0044271
• Balakrishnan, S., and Jie Shen. 1996. “Hamiltonian Based Adaptive Critics for Missile Guidance.” In Guidance, Navigation, and Control Conference. AIAA 1996-3836. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3836
• Balasubramani, Prajwal, Qian Shi, and Daniel DeLaurentis. 2024. “Explainable Machine Learning for Turbojet Engine Prognostic Health Management.” In AIAA SCITECH 2024 Forum. AIAA 2024-0762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0762
• Balbirnie, E., L. Sheporaitis, and C. Merriam. 1975. “Merging Conventional and Optimal Control Techniques for Practical Missile Terminal Guidance.” In Guidance and Control Conference. AIAA 1975-1127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1127
• Balepin, V., P. Czysz, and R. Moszee. 2001a. “Combined Engine for a Reusable Launch Vehicle (KLIN Cycle).” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1911
• Ball, L. H., and W. G. Smith. 1956. Static Lateral-Directional Stability Characteristics of Five Contemporary Airplane Models from Wind-Tunnel Tests at High Subsonic and Supersonic Speeds. NACA-RM-A55J03. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19660010446
• Ball, W., J. Syberg, and L. Surber. 1981. “Experimental Investigation of a High-Aspect-Ratio Supersonic Inlet.” In 17th Joint Propulsion Conference. AIAA 1981-1397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1397
• “BALLISTIC MISSILE and AEROSPACE TECHNOLOGY.” 1961. In Propulsion Space Science and Space Exploration. Elsevier. https://doi.org/10.1016/b978-0-12-395682-8.50001-7
• “BALLISTIC MISSILE and SPACE TECHNOLOGY.” 1960. In Bioastronautics and Electronics and Invited Addresses. Elsevier. https://doi.org/10.1016/b978-1-4832-2884-6.50001-4
• “Ballistic Missile Defence: ‘Technology, Working for You Now’.” 2009. In Justifying Ballistic Missile Defence. Cambridge University Press. https://doi.org/10.1017/cbo9780511691874.008
• Ballistic Missile Defense (BMD). 2017. https://doi.org/10.5040/9798216026273.ch-003
• Ballistic Missile Fundamentals: How Ballistic Missiles Work. 2006. https://doi.org/10.5040/9798216025856.0003
• Balov, Anatoly V., and Sergey P. Zarubin. 2016. Radio Systems for Long-Range Navigation. Wiley. https://doi.org/10.1002/9781119163060.ch3
• Ban, Jingxuan, Gang Chen, Yue Meng, and Junfeng Shu. 2022a. “Calibration Method for Misalignment Angles of a Fiber Optic Gyroscope in Single-Axis Rotational Inertial Navigation Systems.” Optics Express 30 (5): 6487. https://doi.org/10.1364/oe.449629
• Ban, Jingxuan, Lei Wang, and Gang Chen. 2022b. “A Platform Control Algorithm for Long-Endurance Hybrid Inertial Navigation System with Fiber Optic Gyroscope.” Instruments and Experimental Techniques 65 (4): 645–52. https://doi.org/10.1134/s0020441222040194
• Ban, Jingxuan, Lei Wang, Gang Chen, and Zengjun Liu. 2021. “An Improved Platform Control Algorithm for Tri-Axis Hybrid Inertial Navigation System with Fiber Optic Gyroscope.” Optics Express. https://doi.org/10.1364/oe.419092
• Bandyopadhyay, G. 1989. “Low Speed Aerodynamics of Canard Configurations.” Aeronautical Journal 93 (921): 22–28. https://doi.org/10.1017/s0001924000016651
• Banga, Julio R., and Eva Balsa-Canto. 2008. “Parameter Estimation and Optimal Experimental Design.” Essays in Biochemistry 45: 195–210. https://doi.org/10.1042/bse0450195
• Banichuk, Nikolay, Svetlana Ivanova, and Juha Jeronen. 2020. “Moving Web and Dynamic Problem of Aerothermoelastic Vibrations and Instability.” In Lecture Notes in Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-030-49882-5_7
• Bank, Thomas. 1997. “Characterizing a Star Tracker with Built-in Attitude Estimation Algorithms under the Night Sky.” In SPIE Proceedings, vol. 3086, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.277200
• Banks, Martin S. 1999. Visual Guided Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada380934
• Banks, H. T., and K. Kunisch. 1989. “Identifiability and Stability.” In Estimation Techniques for Distributed Parameter Systems. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-3700-6_4
• Banks, Daniel W., and John W. Paulson Jr. 1987. Low-Speed Aerodynamic Characteristics of a Wing-Canard Configuration with Underwing Spanwise Blowing on the Trailing-Edge Flap System. NASA-TM-89020. NASA. https://ntrs.nasa.gov/citations/19870005747
• Banner, R. D., and M. R. Kinsler. 1961. Status of X-15 Aerodynamic-Heating Studies. ARS PAPER-1629-61. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19630005436
• Banner, R. D., A. E. Kuhl, and R. D. Quinn. 1962. Preliminary Results of Aerodynamic Heating Studies on the X-15 Airplane. NASA-TM-X-638. NASA. https://ntrs.nasa.gov/citations/19660020178
• Banyasz, Cs., and L. Keviczky. n.d. “Optimal Input Design for Identification in Closed-Loop.” In Proceedings of the 5th Biannual World Automation Congress. TSI Press. https://doi.org/10.1109/wac.2002.1049436
• Bar-Itzhack, I. 1981. “Doppler Aided Low Accuracy Strapdown Inertial Navigation System.” In Guidance and Control Conference. AIAA 1981-1798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1798
• Bar-Itzhack, I. 1988. “Observability Analysis of Inertial Navigation Systems during in-Flight Alignment.” In Guidance, Navigation and Control Conference. AIAA 1988-4125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4125
• Bar-Itzhack, I. 1989. “Observability Studies of Inertial Navigation Systems.” In Guidance, Navigation and Control Conference. AIAA 1989-3580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3580
• Bar-Itzhack, Itzhack Y. 1990a. “In – Flight Alignment of Inertial Navigation Systems.” In Control and Dynamic Systems. Elsevier. https://doi.org/10.1016/b978-0-12-012738-2.50013-0
• Bar-Itzhack, Itzhack. 1990b. “A Unified Approach to Inertial Navigation System Error Modeling.” In Guidance, Navigation and Control Conference. AIAA 1990-3367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3367
• Bar-Itzhack, Itzhack. 1993. “On Two Misconceptions in the Theory of Inertial Navigation Systems.” In Guidance, Navigation and Control Conference. AIAA 1993-3819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3819
• Bar-Itzhack, I., and N. Berman. 1987. “Control Theoretic Approach to Inertial Navigation Systems.” In Guidance, Navigation and Control Conference. AIAA 1987-2591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2591
• Bar-Itzhack, I. Y., and D. Goshen-Meskin. 1988. “In-Flight Inertial Guidance Alignment.” In ICAS. https://ntrs.nasa.gov/citations/19890026186
• Barantsev, G. O., A. A. Golovan, and P. Yu. Kuznetsov. 2021b. “Initial Alignment Method for a Strapdown Inertial Navigation System on a Swing Base.” Moscow University Mechanics Bulletin 76 (5): 136–41. https://doi.org/10.3103/s0027133021050022
• Bardina, J., C. Lombard, and R. Luh. 1988. “CSCM Three Dimensional Navier-Stokes Computational Aerodynamics for a Projectile Configuration at Transonic Velocities.” In 6th Applied Aerodynamics Conference. AIAA 1988-2585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2585
• Barker, Jeffrey, and Gary Balas. 1999. “Flight Control of a Tailless Aircraft via Linear Parameter-Varying Techniques.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4133
• Barnes, John, Jerri McMichael, Jared Walker, Robert Olliffee, and B. Baker. 2007. “Nose Landing Gear Door Re-Design.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-2077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2077
• Barnett, Bruce. 1962. Trajectory Equations for a Six-Degree-of-Freedom Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0615569
• Barnhart, Paul. 1989. “A Supersonic through-Flow Fan Engine Airframe Integration Study.” In Aircraft Design and Operations Meeting. AIAA 1989-2140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2140
• Barnwell, R. W. 1974. “Transonic Flow about Lifting Wing-Body Combinations.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19740036062
• Barnwell, R. W. 1976. Approximate Method for Calculating Transonic Flow about Lifting Wing-Body Configurations. NASA-TR-R-452. NASA. https://ntrs.nasa.gov/citations/19760014063
• “Baro-Inertial Vertical Channel.” 2022. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch23
• Barr, Stephen M., Roger Birkbeck, Praveen Panickar, and Neeraj Sinha. 2022. “Wind Tunnel Test of a Highly-Compact Serpentine Supersonic Inlet.” In AIAA AVIATION 2022 Forum. AIAA 2022-3865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3865
• Barr, Eric J., Pablo A. Figueroa, and Semih M. Olcmen. 2026. “Hypersonic Glide Vehicle Trajectory Forecasting via Transformer and Physics-Informed GBDT Models.” In AIAA SCITECH 2026 Forum. AIAA 2026-1691. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1691
• Barr, Stephen M., Michael O’Gara, and Neeraj Sinha. 2018. “Highly Compact Supersonic Inlet Design Optimization.” In 2018 Joint Propulsion Conference. AIAA 2018-4842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4842
• Barry, Karen, Mark Hindman, and Russell Yates. 1993. Application of Flight Data to Space Shuttle CCD Star Tracker Catalog Design. ISSN: 0065-3438. Rockwell International, Downey, CA. https://ntrs.nasa.gov/citations/19950048795
• Bartlett, D. W., and C. D. Harris. 1972. Aerodynamic Characteristics of an NASA Supercritical-Wing Research Airplane Model with and without Fuselage Area-Rule Additions at Mach 0.25 to 1.00. NASA-TM-X-2633. NASA. https://ntrs.nasa.gov/citations/19780016137
• Bartnicki, A. 2014. “Teleoperation in Remote Steering System Built in Unmanned Land Vehicles.” In Diffusion and defect data, solid state data. Part B, Solid state phenomena/Solid state phenomena, vol. 223. Scientific.net. https://doi.org/10.4028/www.scientific.net/ssp.223.333
• Bartone, Chris, Rembert N. Schofield, and Ron Ostroff. 2001. Challenges in the Acceptance/Licensing of a Mobile Ballistic Missile Range Safety Technology (BMRST) System. Defense Technical Information Center. https://doi.org/10.21236/ada410647
• Bartone, Chris, Rembert N. Schofield, and Ron Ostroff. 2002. Challenges in the Acceptance/Licensing of a Mobile Ballistic Missile Range Safety Technology (BMRST) System. Defense Technical Information Center. https://doi.org/10.21236/ada417610
• Barz, Fynn. 2026. “Multifidelity Fluid-Structure Coupled Shape Optimization of a Hypersonic Glide Vehicle.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5022
• Bashir, Uzair, Shafaat Ahmed Bazaz, Muhammad Mubasher Saleem, Rana Iqtidar Shakoor, Muhammad Owais Tariq, and Pirbhat Kumar. 2024. “Design and Analysis of Mode-Matched Decoupled Mass MEMS Gyroscope with Improved Thermal Stability.” Measurement Science and Technology 35 (8): 086319. https://doi.org/10.1088/1361-6501/ad4bfd
• Bashkirov, Strelets D. Yu. Lavrischeva L. S. Staroverov N. N. Novoselov V. N. Fevralskih A. V. I. G. 2024. “Methodic for Three-Dimensional Parametric Optimization of the Aerodynamic Layout of a Supersonic Passenger Aircraft Based on Flypoint Parametrica.” Vestnik Mashinostroeniya: 672–78. https://doi.org/10.36652/0042-4633-2024-103-8-672-678
• “Basic Principles of Strapdown Inertial Navigation Systems.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch3
• “Basics of Missile Guidance.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-4
• Basil, Daniel D., Lawrence Hart, Kurotamuno P. Jackson, and Tamunobelema Oba. 2021. “Determination of Deflection of the Vertical Components: Implications on Terrestrial Geodetic Measurement.” Trends Journal of Sciences Research 1 (1): 36–49. https://doi.org/10.31586/wjgg.2021.104
• Bassett, George Z., Jing Pei, Adam Milne Slagle, and Bandu Pamadi. 2017. “Application of an Optimal Control Allocation Scheme with Structural Load and Aero Heating Feedback for a Morphing Inflatable Aerodynamic Decelerator.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20190000714
• Batill, Stephen M. 1982. A Study of Analytic Modeling Techniques for Landing Gear Dynamics. Defense Technical Information Center. https://doi.org/10.21236/ada122312
• Batill, S., and J. Bacarro. 1988. “Modeling and Identification of Nonlinear Dynamic Systems with Application to Aircraft Landing Gear.” In 29th Structures, Structural Dynamics and Materials Conference. AIAA 1988-2315. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2315
• Batt, J., and R. Gallagher. 1963. “Laboratory Simulation of Nonlinear Static Aerothermoelastic Behavior.” In Heterogeneous Combustion Conference. AIAA 1963-1034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1034
• Battersby, A., and Mary Blewitt. 1965. “Celestial Navigation for Yachtsmen.” OR 16 (4): 495. https://doi.org/10.2307/3006726
• Batterson, James G., and E. A. Morelli. 1996. Parameter Identification Flight Test Maneuvers for Closed Loop Modeling of the F-18 High Alpha Research Vehicle (HARV). NASA-CR-198269. NASA. https://ntrs.nasa.gov/citations/20040110721
• Baucom, Donald R. 1995. US Missile Defense Program, 1944-1994: A Protracted Revolution,. Defense Technical Information Center. https://doi.org/10.21236/ada338560
• Bauer, F., P. Garabedian, and I. C. Chang. 2026. “Wave Drag and the Entropy Inequality in Transonic Flow.” In Computational Fluid Dynamics Techniques. CRC Press. https://doi.org/10.1201/9781003760528-2
• Bauer, Steven, and S. McMillin. 1988. “Experimental and Theoretical Study of the Effects of Wing Geometry on a Supersonic Multibody Configuration.” In 6th Applied Aerodynamics Conference. AIAA 1988-2510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2510
• Bauer, R. C., W. W. Muse, and C. R. Tinsley. 1974. Simulation of Flow Approaching the Chin Inlet of a Ramjet Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0783244
• Bauermeister, W., and H. Ip. 1968. “727 Airplane Engine Inlet Development.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-595
• Baumgartner, Robert I. 1997. “Venturestar™ Single Stage to Orbit Reusable Launch Vehicle Program Overview.” In Space technology and applications international forum (STAIF - 97). ASCE. https://doi.org/10.1063/1.51920
• Baxa, E. G., Jr. 1978. Investigation of New Techniques for Aircraft Navigation Using the Omega Navigation. NASA-CR-145303. NASA. https://ntrs.nasa.gov/citations/19780009094
• Baye-Wallace, Lily, and Charles R. Krouse. 2022. “Simulation of Inlet Unstart in a Supersonic Engine Model Running on a Raspberry Pi.” In AIAA SCITECH 2022 Forum. AIAA 2022-0402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0402
• Bazarko, V. O., R. P. Cochran, and R. W. Cubbison. 1965. Aerodynamic Heating Tests of Several Variations of Insulation System. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19650010309
• Beale, D., and M. S. Collier. 1989. “Validation of a Free-Jet Technique for Evaluating Inlet-Engine Compatibility.” In 25th Joint Propulsion Conference. AIAA 1989-2325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2325
• Beale, David, Kevin Cramer, and Peter King. 2002. “Development of Improved Methods for Simulating Aircraft Inlet Distortion in Turbine Engine Ground Tests (Invited).” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3045
• Beale, Dave, Milt Davis, and Jim Sirbaugh. 2006. “Requirements and Advances in Simulating Aircraft Inlet Total Pressure Distortion in Turbine Engine Ground Tests.” In Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs. ASMEDC. https://doi.org/10.1115/gt2006-90038
• Beale, Dave, Scott Wieland, Jim Reed, and Larry Wilhite. 2007. “Demonstration of a Transient Total Pressure Distortion Generator for Simulating Aircraft Inlet Distortion in Turbine Engine Ground Tests.” In Volume 1: Turbo Expo 2007. ASMEDC. https://doi.org/10.1115/gt2007-27222
• Beale, D., and M. Zelenak. 1992. “Development and Validation of a Freejet Technique for Inlet-Engine Compatibility Testing.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3921
• Becka, Steve, Mitchell Novack, Sandra Slivinsky, and Chris Paul. 2008. “A High Reliability Solid State Accelerometer for Ballistic Missile Inertial Guidance.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7300. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7300
• Becker, S. 1973. “New Missile Guidance Concepts as Applied to Command Guidance Controlsystem.” In Guidance and Control Conference. AIAA 1973-835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-835
• Becker, Jonathan, and Mathieu Joerger. 2024. “Uncertainty Quantification for Radar/Inertial Pose Estimation in GNSS-Denied Areas.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2024.19708
• Bedke, Andrew, and Steven Gorrell. 2021. “The Effects of Various Inlet Distortion Patterns on Distortion Transfer and Generation in a Transonic Fan at Various Operating Points.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3465
• Bednarz, B., J. A. Dankowych, G. Joslin, K. Jew, D. H. Lewis, and W. A. Young. 1987. “Optomechanical Systems for a Closed Loop Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937539
• Beh, H., G. Hofinger, and P. Huber. 2018. “Control Law Design and Flight Test Results of the Experimental Aircraft X-31A.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-15
• Beheim, Milton A., and Gerald W. Englert. 1956. Effects of a J34 Turbojet Engine on Supersonic Diffuser Performance. NACA-RM-E55I21. NASA. https://ntrs.nasa.gov/citations/19930088936
• Behrouz, H., I. Mohammadzaman, and A. Mohammadai. 2021. “Gain-Scheduled H_2/H_∞ Autopilot Design with Regional Pole Placement Constraints: An LMI-Based Approach.” Scientia Iranica 28 (2): 757–72. https://doi.org/10.24200/sci.2020.53269.3154
• Bein, T., P. Friedmann, X. Zhong, and I. Nydick. 1993. “Hypersonic Flutter of a Curved Shallow Panel with Aerodynamic Heating.” In AIAA. https://ntrs.nasa.gov/citations/19930053431
• Beisner, Henry M. 1969. “Arbitrary Path Magnetic Navigation by Recursive Nonlinear Estimation.” Navigation 16 (3): 271–78. https://doi.org/10.1002/j.2161-4296.1969.tb01665.x
• Beissner, F. L., Jr., W. A. Lovell, A. W. Robins, and E. E. Swanson. 1986. Effect of Emerging Technology on a Convertible, Business/interceptor, Supersonic-Cruise Jet. NASA-CR-178097. NASA. https://ntrs.nasa.gov/citations/19860017806
• Beiter, S. 1970. “Integral Dynamic Self-Test of an Inertial Measurement Unit.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1013
• Beke, Andrew, Gerald Englert, and Milton Beheim. 1956. Effect of an Adjustable Supersonic Inlet on the Performance up to Mach Number 2.0 of a J34 Turbojet Engine. NACA-RM-E55I27. NASA. https://ntrs.nasa.gov/citations/19930088913
• Belcastro, C. M., and A. J. Ostroff. 1984. Total Energy-Rate Feedback for Automatic Glide-Slope Tracking during Wind-Shear Penetration. NASA-TP-2412. NASA. https://ntrs.nasa.gov/citations/19850015490
• Bell, Frank Coffman. 1967. “Newtonian Inertial Navigation.” Journal of Navigation 20 (2): 206–8. https://doi.org/10.1017/s0373463300028861
• Bell, C. C. 1971. Gravity Gradient Study. NASA-CR-123489. NASA. https://ntrs.nasa.gov/citations/19720010678
• Bell, Steven A., John A. Bangert, and George H. Kaplan. 2020. “Evolution of the Nautical Almanac & Celestial Navigation Today.” In Historical & Cultural Astronomy. Springer International Publishing. https://doi.org/10.1007/978-3-030-43631-5_9
• Bell, C. C., R. L. Forward, and H. P. Williams. 1970. “Simulated Terrain Mapping with the Rotating Gravity Gradiometer.” In ADVANCES IN DYNAMIC GRAVIMETRY, SYMPOSIUM ON DYNAMIC GRAVIMETRY. https://ntrs.nasa.gov/citations/19700067552
• Belyanin, L. N., V. S. Dmitriev, and D. K. Vu. 2018. “Computational Algorithms for Analytic Gyrocompassing System with Rotating Angular Rate Sensor.” Современные наукоемкие технологии (Modern High Technologies), no. №6 2018: 25–33. https://doi.org/10.17513/snt.37028
• Belzer, M. R., and Y. M. Cho. 1988. Micro-Computer Network Architecture for Range Instrumentation Applications. Defense Technical Information Center. https://doi.org/10.21236/ada196971
• Ben-Arosh, Rachel, Benveniste Natan, Elyeser Spiegler, et al. 1997. “The Reacting Flowfield within a Supersonic Combustion Solid Fuel Ramjet.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3119
• Ben-Ishai, A., J. Reiner, and H. Rotstein. 2001. “Kalman Filter Mechanization in INS/seeker Fusion and Observability Analysis.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4402
• Benavoli, Alessio, Luigi Chisci, Alfonso Farina, Sandro Immediata, and Luca Timmoneri. 2007. Knowledge-Based Radar Tracking. Wiley. https://doi.org/10.1002/9780470283158.ch8
• Benbassat, Danny. 2005. “Perceived Importance of the Visual Cues to the Timing of the Landing Flare.” Journal of Aviation/Aerospace Education & Research. https://doi.org/10.15394/jaaer.2005.1512
• Benbassat, Danny, and Charles Abramson. 2002. “General Aviation Landing Flare Instructions.” Journal of Aviation/Aerospace Education & Research. https://doi.org/10.15394/jaaer.2002.1298
• Benbow, R. 1971. “Principles of Performance Monitoring, with Application to Automatic Landing.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-958. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-958
• Bendot, Joseph G., Wallace G. Harkins, and Thomas G. Piercy. 1975. Low Cost Hypermixing Ejector Ramjet Program. Defense Technical Information Center. https://doi.org/10.21236/ada016430
• Bénet, Pierre, and Alexis Guinamard. 2026. “Gyrocompassing: From Gravity Rotation Analysis to Inertial Trajectory Fitting.” NAVIGATION: Journal of the Institute of Navigation 73 (1): navi.751. https://doi.org/10.33012/navi.751
• Bennett, G. G. 1979. “General Conventions and Solutions-Their Use in Celestial Navigation.” Navigation 26 (4): 275–80. https://doi.org/10.1002/j.2161-4296.1979.tb01386.x
• Benson, T. J., and B. H. Anderson. 1983. “Validation of a Three Dimensional Viscous Analysis of Axisymmetric Supersonic Inlet Flow Fields.” In 21st Aerospace Sciences Meeting. AIAA 1983-540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-540
• Benson, Rusty, and D. McRae. 1993. “Numerical Simulations of the Unstart Phenomenon in a Supersonic Inlet/diffuser.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2239
• Benyo, Theresa L. 2010a. The Effect of Magnetohydrodynamic (MHD) Energy Bypass on Specific Thrust for a Supersonic Turbojet Engine. NASA/TM-2010-216734. NASA. https://ntrs.nasa.gov/citations/20110002743
• Benyo, Theresa. 2010b. “The Effect of MHD Energy Bypass on Specific Thrust for Supersonic Turbojet Engine.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-232. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-232
• Benyo, Theresa. 2010c. “Initial Flow Matching Results of MHD Energy Bypass on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (NPSS) Environment.” In 41st Plasmadynamics and Lasers Conference. AIAA 2010-4301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4301
• Benyo, Theresa. 2011. “Flow Matching Results of an MHD Energy Bypass System on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (NPSS) Environment.” In 42nd AIAA Plasmadynamics and Lasers Conference. AIAA 2011-3591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3591
• Benzo, Sankofa. 2024. Resilient Star Tracker Algorithms. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/2586143
• Berezovsky, Уе. K. 2018. “Improvement of Wide-Chord Rotor Blade Fan Performance in Bypass Turbojet Engine.” Herald of Aeroenginebuilding 0 (1). https://doi.org/10.15588/1727-0219-2018-1-6
• Berg, Ralph. 1965. “Inertial Test Slab Stability Study.” In Guidance Control Conference. AIAA 1965-1230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1230
• Berger, John, and Roland Meyer. 1974. “Multi-Axis Pilot Models for Prediction of Weapon Delivery Accuracy.” In Mechanics and Control of Flight Conference. AIAA 1974-920. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-920
• Bergeron, H. P., A. T. Haynie, and J. B. McDede. 1980. Development of a Computer Program Data Base of a Navigation Aid Environment for Simulated IFR Flight and Landing Studies. NASA-TM-80064. NASA. https://ntrs.nasa.gov/citations/19810005448
• Bergh, R. A. 1990. “Dual-Ramp Closed-Loop Fiber-Optic Gyroscope.” In SPIE Proceedings, vol. 1169, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.963062
• Bergh, Ralph A., Melissa D. Lane, and Jonathan A. Bergh. 2026. “Aspects of the Fibernetics Navigation-Grade Inertial Measurement Unit (IMU).” In Fiber Optic Gyros: 50th Anniversary Conference, edited by Eric Udd, Herve C. Lefevre, Glen A. Sanders. SPIE. https://doi.org/10.1117/12.3095033
• Bergh, R. A., H. C. Lefèvre, and H. J. Shaw. 1982. “All Single Mode Fiber Optic Gyroscope.” In Springer Series in Optical Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-39490-7_28
• Bernard, A. 1989. “The GRADIO Spaceborne Gravity Gradiometer: Development and Accommodation.” In Ohio State Univ., Progress in the Determination of the Earth’s Gravity Field. https://ntrs.nasa.gov/citations/19900011244
• Berry, D., and G. Gilyard. 1973. “Airframe/propulsion System Interactions: An Important Factor in Supersonic Aircraft Flight Control.” In Guidance and Control Conference. AIAA 1973-831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-831
• Bertaska, Ivan Rodrigues. 2025. Temperature Variation Analysis of the STIM300 Inertial Measurement Unit. Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20250000898
• Berthelot, Alexander, Grace Craft, and Aaron Matheny. 2026. “Material Selection and Structural Analysis of an Undergraduate-Designed Unpowered Hypersonic Glide Vehicle.” In 2026 Regional Student Conferences. AIAA 2026-112174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-112174
• Bessaad, Nassim, Qilian Bao, Zhao Jiangkang, and Karam Eliker. 2021. “On SINS\star Tracker Geo-Localization.” Engineering Research Express 3 (4): 045040. https://doi.org/10.1088/2631-8695/ac3e12
• Besserer, C. W. 1952. Ramjet Technology. Chapter 14. Materials for Ramjet Engines and Components. Defense Technical Information Center. https://doi.org/10.21236/ad0036272
• Bessonov, R. V., A. N. Kurkina, and V. V. Sazonov. 2018. “Estimating the Accuracy in Determining Orientation Parameters by the BOKZ-M60 Star Tracker.” Mathematical Models and Computer Simulations 10 (3): 341–56. https://doi.org/10.1134/s2070048218030043
• Bettis, Benjamin, and Serhat Hosder. 2010. “Quantification of Uncertainty in Aerodynamic Heating of a Reentry Vehicle Due to Uncertain Wall and Freestream Conditions.” In 10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. AIAA 2010-4642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4642
• Bettwy, T. S., E. A. Goldberg, and H. A. Irwin. 1971. “Strapdown or Gimballed IMU’s for the Space Shuttle.” Navigation 18 (3): 331–43. https://doi.org/10.1002/j.2161-4296.1971.tb00104.x
• Beukers, J. M. 1973. “Accuracy Limitations of the OMEGA Navigation System Employed in the Differential Mode.” Navigation 20 (1): 81–92. https://doi.org/10.1002/j.2161-4296.1973.tb01156.x
• “Beyond GNSS: Advancing Autonomous Navigation Technologies.” 2025. In GNSS-Enabled Autonomous Navigation. SciTech Publishing Inc. https://doi.org/10.1049/sbra572e_ch6
• Bezick, Scott Michael. n.d. “Feedback Linearizing Control for the Guidance of a Homing Missile.” PhD diss., Drexel University. https://doi.org/10.17918/00008477
• Bhanu, Bir, and Barry A. Roberts. 1992. Inertial Navigation Sensor Integrated Obstacle Detection System. Patent Number: US-PATENT-5,128,874. Ames Research Center. https://ntrs.nasa.gov/citations/20080004326
• Bharadwaj, Raj Mohan, Vibhor L. Bageshwar, and Kyusung Kim. 2017. Systems and Methods for Determining Inertial Navigation System Faults. Patent Number: US-Patent-9,568,321. Ames Research Center. https://ntrs.nasa.gov/citations/20170001979
• Bhatia, Rachit, and David Geller. 2020. “Sensitivity Analysis of Precision Inertial Sensor-Based Navigation System (SAPIENS).” NAVIGATION 67 (4): 795–822. https://doi.org/10.1002/navi.397
• Bheemaiah, Anil Kumar. 2019. “BEAM Autopilot.” Preprint, . https://doi.org/10.35543/osf.io/st2xa
• Bhutta, Bilal, and Clark Lewis. 1992. “PNS Predictions for Supersonic/hypersonic Flows over Finned Missile Configurations.” In 10th Applied Aerodynamics Conference. AIAA 1992-2695. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2695
• Bi, Ran, Xuan She, Xiaowu Shu, and Cheng Liu. 2018. “Influence of the Modulation Phase Error on Bias Error in Interferometric Fiber Optic Gyroscope.” Optical Engineering 57 (08): 1–5. https://doi.org/10.1117/1.oe.57.8.087104
• Bibel, John, and Harold Stalford. 1991. “Mu-Synthesis Autopilot Design for a Flexible Missile.” In 29th Aerospace Sciences Meeting. AIAA 1991-586. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-586
• Biber, Kasim. 2015. “Flight Dynamics Modeling of a Supersonic Aircraft Concept.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0031
• Biblarz, O., B. Pomerantz, and S. Lindsey. 1998. “Transonic Missile Drag Area-Rule and Afterbody-Role Verification with CFD.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-527
• Bielas, M. S., T. F. El-Wailly, and R. Y. Liu. 1989. “Test Results of a Prototype Serrodyne Closed-Loop Interferometric Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 0985, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.948866
• Biesiadny, Thomas J., and Bruce J. Wendt. 2004. The Performance of a Subsonic Diffuser Designed for High Speed Turbojet-Propelled Flight. NASA/CR-2004-213410. NASA. https://ntrs.nasa.gov/citations/20050040781
• Billec, W. 1967. The Effect of Deck Span upon Arresting-Gear Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0813761
• Billig, Frederick. 1993. “SCRAM: A Supersonic Combustion Ramjet Missile.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2329
• Billig, F. S., and S. E. Grenleski. 1968. Investigation of an Actively Cooled Leading Edge for Hypersonic Ramjet Engines. NASA. https://ntrs.nasa.gov/citations/19680053411
• Billings, Deborah R., and Paula J. Durlach. 2008. Effects of Input Device and Latency on Performance While Training to Pilot a Simulated Micro-Unmanned Aerial Vehicle. Defense Technical Information Center. https://doi.org/10.21236/ada493588
• Bimal Raj, K., and Ashok Joshi. 2015. “In-Motion Alignment of Inertial Navigation System with Doppler Speed Measurements.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0096
• Biot, M. A. 1949. “Transonic Drag of an Accelerated Body.” Quarterly of Applied Mathematics 7 (1): 101–5. https://doi.org/10.1090/qam/28157
• Birch, Trevor, Jerry Allen, and Floyd Wilcox Jr. 2000. “Force, Surface Pressure and Flowfield Measurements on Slender Missile Configurations at Supersonic Speeds.” In 18th Applied Aerodynamics Conference. AIAA 2000-4207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4207
• Birch, Trevor, and John Cleminson. 2004. “Aerodynamic Characteristics of a Square Cross-Section Missile Configuration at Supersonic Speeds.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5197
• Birch, T., and K. Petterson. 2004. “CFD Predictions of Square and Elliptic Cross-Section Missile Configurations at Supersonic Speeds.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5453. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5453
• Birkmire, Brian, and John Gallagher. 2012. “Air-to-Air Missile Maximum Launch Range Modeling Using a Multilayer Perceptron.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2012-4942. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4942
• Birnbaum, M., and P. Salomon. 1967. “A Strapdown Star Tracker for Space Vehicle Attitude Control.” In Control and Flight Dynamics Conference. AIAA 1967-551. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-551
• Bischof, Wallace F. 1959. “Atlantic Missile Range Cine Processing Laboratory.” Journal of the SMPTE 68 (10): 683–86. https://doi.org/10.5594/j16966
• Bistrovs, Vadims, and Ansis Klūga. 2012. “Adaptive Extended Kalman Filter for Aided Inertial Navigation System.” Elektronika ir Elektrotechnika 122 (6): 37–40. https://doi.org/10.5755/j01.eee.122.6.1818
• Bjorkman, William S. 1987. NAVSIM 2: A Computer Program for Simulating Aided-Inertial Navigation for Aircraft. NASA-CR-177438. NASA. https://ntrs.nasa.gov/citations/19880003096
• Black, R. 1968. “Experimental Determination of Tire Parameters for Aircraft Landing Gear Shimmy Stability Studies.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-311
• Black, Raymond J. 1976. “Realistic Evaluation of Landing Gear Shimmy Stabilization by Test and Analysis.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/760496
• Black, David, Dragan Andjelic, and Septimiu Salcudean. 2022. “Evaluation of Communication and Human Response Latency for (Human) Teleoperation.” Preprint, TechRxiv. https://doi.org/10.36227/techrxiv.21432009
• Blackaby, James R., E. Gene Lyman, and John A. Altermann III. 1959. Inlet Performance Characteristics from Wind-Tunnel Tests of a 0.10-Scale Air-Induction System Model of the YF-108A Airplane at Mach Numbers of 2.50, 2.76, and 3.00. NASA-MEMO-7-18-59A. NASA. https://ntrs.nasa.gov/citations/19980228132
• Blair, A. B. 1990a. “Supersonic Aerodynamic Characteristics of a Maneuvering Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/901993
• Blair, J., and R. McCorkle. 1979. “Dual Digital Flight Control Redundancy Management System Development Program.” In Guidance and Control Conference. AIAA 1979-1701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1701
• Blair, A. B., and G. H. Rapp. 1980. “Experimental and Analytical Comparison of Aerodynamic Characteristics of a Forward-Control Missile.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19800038834
• Blair, A. B., Jr. 1978a. An Experimental Wind-Tunnel Investigation of a Ram-Air-Spoiler Roll-Control Device on a Forward-Control Missile at Supersonic Speeds. NASA-TP-1353. NASA. https://ntrs.nasa.gov/citations/19790009638
• Blair, A. B., Jr. 1978b. Wind-Tunnel Investigation at Supersonic Speeds of a Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins. NASA-TP-1316. NASA. https://ntrs.nasa.gov/citations/19780024124
• Blair, A. B., Jr. 1985. Wind-Tunnel Investigation at Supersonic Speeds of a Remote-Controlled Canard Missile with a Free-Rolling-Tail Brake Torque System. NASA-TP-2401. NASA. https://ntrs.nasa.gov/citations/19870008235
• Blair, A. B., Jr. 1990b. Supersonic Aerodynamic Characteristics of Conformal Carriage Monoplanar Circular Missile Configurations with Low-Profile Quadriform Tail Fins. AIAA PAPER 90-0620. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19900032895
• Blair, A. B., Jr., J. M. Allen, and G. Hernandez. 1983. Effect of Tail-Fin Span on Stability and Control Characteristics of a Canard-Controlled Missile at Supersonic Mach Numbers. NASA-TP-2157. NASA. https://ntrs.nasa.gov/citations/19830019688
• Blair, A., Jr., James Dillon, and Carolyn Watson. 1992. “Experimental Study of Tail-Span Effects on a Generic Canard-Controlled Missile.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-79. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-79
• Blair, A. B., Jr., and J. Grow. 1973. Aerodynamic Characteristics of a 55 Deg Clipped-Delta-Wing Orbiter Model at Mach Numbers from 1.60 to 4.63. NASA-TM-X-2748. NASA. https://ntrs.nasa.gov/citations/19730015331
• Blair, A. B., Jr., W. C. Sawyer, and C. M. Jackson Jr. 1978. “A Ram-Air-Spoiler Roll Stabilization Device for Forward Control Cruciform Missiles.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780036729
• Blake, Lamont V. 1968. Radio Ray (Radar) Range-Height-Angle Charts. Defense Technical Information Center. https://doi.org/10.21236/ad0665018
• Blake, William, and James Simon. 1998. “Tools for Rapid Analysis of Aircraft and Missile Aerodynamics.” In 16th AIAA Applied Aerodynamics Conference. AIAA 1998-2793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2793
• Blakely, Brandon, Aaron Nielsen, and Patrick Duff. 2025. “Comparative Analysis of Different Magnetic Anomaly Datasets Using Navigation Performance with Flight Test Data.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2025.20278
• Blanchard, Willard S. 1953. Drag and Longitudinal Trim at Low Lift of the North American YF-100A Airplane at Mach Numbers from 0.76 to 1.77 as Determined from the Flight Test of a 0.11-Scale Rocket Model. NACA-RM-SL53E11a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023638
• Blanchard, Ulysse J. 1963. Characteristics of a Lunar Landing Configuration Having Various Multiple-Leg Landing-Gear Arrangements. L-803. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20070030982
• Blanchard, Ulysse J. 1964. Characteristics of a Lunar Landing Configuration Having Various Multiple-Leg Landing-Gear Arrangements. NASA-TN-D-2027. NASA. https://ntrs.nasa.gov/citations/19640005067
• Blanchard, R. 1978. “High Accuracy Calibration of Electrostatic Gyro Strapdown Navigationsystems.” In Guidance and Control Conference. AIAA 1978-1255. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1255
• Bland, William M., Jr., and Katherine A. Collie. 1961. Free-Flight Aerodynamic-Heating Data to Mach Number 10.4 for a Modified Von Karman Nose Shape. NASA-TN-D-889. NASA. https://ntrs.nasa.gov/citations/19980228066
• Bland, William M., Jr., and Ronald Kolenkiewicz. 1958. Free-Flight Pressure Measurements over a Flare-Stabilized Rocket Model with a Modified Von Karman Nose for Mach Numbers up to 4.3. NACA-RM-L57J24. NASA. https://ntrs.nasa.gov/citations/19930089954
• Bland, W. M., Jr., R. Kolenkiewicz, and A. G. Swanson. 1958. Free-Flight Aerodynamic-Heating Data at Mach Numbers up to 10.9 on a Flat-Faced Cylinder. NACA-RM-L57K29. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19630003999
• Blank, S. 1995. “Passive Techniques for Controlling Flow in Supersonic Wing/body Junctions.” In 13th Applied Aerodynamics Conference. AIAA 1995-1816. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1816
• Blanton, Jeffrey N. 1980. A New Collapsing Technique for Star Identification Using Sensors with Nonsimultaneous Acquisition Times. Defense Technical Information Center. https://doi.org/10.21236/ada096242
• Blom, G., D. Ball, J. Bussoletti, and N. Yu. 1991. “Computations of the Supersonic Flow over an HSCT Type Configuration and Comparison with Wind Tunnel Data.” In 9th Applied Aerodynamics Conference. AIAA 1991-3290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3290
• Blosser, Max L. 1997. “Development of Metallic Thermal Protection Systems for the Reusable Launch Vehicle.” In Space technology and applications international forum (STAIF - 97). ASCE. https://doi.org/10.1063/1.51930
• Blumenthal, S., and J. Denton. 1962. Estimating Missile Reliability. Defense Technical Information Center. https://doi.org/10.21236/ad0291603
• Blutreich, J. N., E. F. Hitt, and F. G. Rhea. 1969. Development of an Evaluation Technique for Strapdown Guidance Systems Interim Report, 1 Feb. 1968: 1 Feb. 1969. NASA-CR-86286. NASA. https://ntrs.nasa.gov/citations/19700004988
• Bo, Yuan, and Yang Jun. 2014. “Design Method Research on Autopilot of Rolling Missile.” In Advances in Social Science, Education and Humanities Research. Atlantis Press. https://doi.org/10.2991/acta-14.2014.25
• Bobbili, Prasada Rao, Jagannath Nayak, Prerana Dabral Pinnoji, and D. V. Rama Koti Reddy. 2014. “Minimization of Reciprocal Noises in Resonator Fiber Optic Gyroscope by Localized Thermal Tuning of Fiber Ring Resonator.” In 12th International Conference on Fiber Optics and Photonics. OSA. https://doi.org/10.1364/photonics.2014.m3c.5
• Bobick, J. C., and A. E. Bryson Jr. 1972a. Improved Navigation by Combining VOR/DME Information with Air or Inertial Data. NASA-CR-124826. NASA. https://ntrs.nasa.gov/citations/19720022936
• Bobick, J. C., and A. E. Bryson Jr. 1972b. “Updating Inertial Navigation Systems with VOR/DME Information.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19720055417
• Bodson, Marc, William Pohlchuck, Marc Bodson, and William Pohlchuck. 1997. “Command Limiting in Reconfigurable Flight Control.” In Guidance, Navigation, and Control Conference. AIAA 1997-3604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3604
• Bogar, T., M. Sajben, and J. Kroutil. 1983. “Response of a Supersonic Inlet to Downstream Perturbations.” In 19th Joint Propulsion Conference. AIAA 1983-2017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2017
• Bogdanov, O. N., and A. V. Fomichev. 2018. “Effect of Delays in Rate Sensor Channels on the Accuracy of Navigation Solution of Strapdown Inertial Navigation System.” Gyroscopy and Navigation 9 (3): 199–206. https://doi.org/10.1134/s2075108718030033
• Bogdanov, A. V., S. V. Macksimovich, S. G. Petrov, and G.А. Yurin. 2024. “Dynamic Model of Doppler Frequency Separations of a Flight of Different Type of Aircraft Pair with Turbojet Engine.” Achievements of Modern Radioelectronics. https://doi.org/10.18127/j20700784-202403-04
• Bogomolov, Yaroslav, and Vladimir Malinin. 2017. “Determination Area of Parameters Ramjet Engine on Powdery Aluminum Fuel on the Basis of Characteristics Rocket-Ramjet Engine of the Missile “Meteor”.” Perm National Research Polytechnic University Aerospace Engineering Bulletin, no. 50: 58–67. https://doi.org/10.15593/2224-9982/2017.50.06
• Bogue, Rodney K., Harold R. Bagley, David C. Soreide, and David A. Bowdle. 1995. “Coherent Lidar Solution for the HSCT Supersonic Engine Inlet Unstart Problem.” In SPIE Proceedings, vol. 2464, edited by Robert G. Otto, James Lenz. SPIE. https://doi.org/10.1117/12.211479
• Bohm, K., and K. Perermann. 1987. “‘Signal Processing Schemes for the Fiber-Optic Gyroscope’.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937536
• Boithias, L. 1979. “Multipath Propagation in Line-of-Sight Links.” Electronics Letters 15 (7): 209–10. https://doi.org/10.1049/el:19790147
• Boland, J. S., III. 1970. On Error Bounds in the Digital Computation of the Four Parameters for Strapdown Inertial Systems. NASA-CR-103050. NASA. https://ntrs.nasa.gov/citations/19710009569
• Bolender, Michael, and David Doman. 2005. “A Non-Linear Model for the Longitudinal Dynamics of a Hypersonic Air-Breathing Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6255. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6255
• Boles, John, and Ryan Milligan. 2013. Technology for Sustained Supersonic Combustion Task Order 0006: Scramjet Research with Flight-Like Inflow Conditions. Defense Technical Information Center. https://doi.org/10.21236/ada586382
• Bollino, Kevin, Michael Oppenheimer, and David Doman. 2006. “Optimal Guidance Command Generation and Tracking for Reusable Launch Vehicle Reentry.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6691. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6691
• Bollner, M. 1987. “Star Identification Techniques Used for Attitude Determination and Control of the X-Ray Satellite Rosat.” In Guidance, Navigation and Control Conference. AIAA 1987-2531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2531
• Bolotnov, A. S. 2019. “The Use of a Laser Gyroscope in Strapdown Inertial Systems.” Politechnical student journal, no. 39. https://doi.org/10.18698/2541-8009-2019-10-533
• Bolt, M. 1981. “Flight Test Data Processing for Fleet Ballistic Missile Programs.” In 1st Flight Test Conference. AIAA 1981-2394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2394
• Bona, B. E., and C. E. Hutchinson. 1965. “An Optimum Stellar-Inertial Navigation System.” Navigation 12 (2): 171–78. https://doi.org/10.1002/j.2161-4296.1965.tb02129.x
• Bond, Ryan, and Jack Edwards. 2003. “CFD Analysis of an Independently Fueled Ramjet Stream in an RBCC Engine.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-17. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-17
• Bond, Evan H., and Nicole L. Key. 2025. “A Flow Physics Approach to Determining Critical Angle of Inlet Total Pressure Distortion for a Centrifugal Compressor.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2025-151711
• Bond, Aleck C., and Charles B. Rumsey. 1957. Free-Flight Skin Temperature and Pressure Measurements on a Slightly Blunted 25 Deg Cone-Cylinder-Flare Configuration to a Mach Number of 9.89. NACA-RM-L57B18. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19690093231
• Bond, Aleck C., and Andrew G. Swanson. 1953. Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance Characteristics of the North American MX-770 (X-10) Missile at Mach Numbers from 0.80 to 1.70. NACA-RM-SL53D10A. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050029470
• Bondarenko, Oleksandr, Anna Isenko, Evgen Sosulyaka, and Yuriy Yuryev. 2025. “Mathematical Model of a Gyroscope with a Hemispherical Quartz Resonator.” Mechanics of Gyroscopic Systems, no. 49: 85–97. https://doi.org/10.20535/0203-3771492025334111
• Bondre, Ahyaan. 2026. “Theoretical Analysis of a Combined-Cycle (Turbojet + Ramjet) Propulsion System.” International Journal of Innovative Science and Research Technology (IJISRT): 2597. https://doi.org/10.38124/ijisrt/26jan1332
• Bonner, E., M. H. Roe, R. M. Tyson, and R. Y. Mairs. 1974. Influence of Propulsion System Size, Shape, and Location on Supersonic Aircraft Design. NASA-CR-132544. NASA. https://ntrs.nasa.gov/citations/19750006675
• Boozer, Drayton D., and J. Richard Fellerhoff. 1988. “Terrain-Aided Navigation Test Results in the AFTI/F-16 Aircraft.” Navigation 35 (2): 161–75. https://doi.org/10.1002/j.2161-4296.1988.tb00949.x
• Boppart, J., and US Atomic Energy Commission (AEC). 1957. Preliminary Analysis of Supercharged Nuclear Ramjet Propulsion System. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1063980
• Boppe, C. W., and P. V. Aidala. 1980. “Complex Configuration Analysis at Transonic Speeds.” In AGARD Subsonic(Transonic Configuration Aerodyn.. https://ntrs.nasa.gov/citations/19810007501
• Borden, Brett. 1993. What Is the Radar Tracking ‘Glint’ Problem and Can It Be Solved. Defense Technical Information Center. https://doi.org/10.21236/ada266509
• Borodacz, Krystian, and Cezary Szczepański. 2023a. “GNSS Denied Navigation System for the Manoeuvring Flying Objects.” Aircraft Engineering and Aerospace Technology 96 (1): 63–72. https://doi.org/10.1108/aeat-05-2023-0124
• Borowski, Jerzy, and Slawomir Michalak. 2024. “Selected Error Compensation Problems of the Ahrs/ins Cardanless Inertial Navigation System.” Aviation and Security Issues 5 (1): 29–39. https://doi.org/10.55676/asi.v5i1.59
• Borror, Sean L. 1995. “Star Calibration of the Pallet Inertial Sensor Assembly for the High-Altitude Balloon Experiment.” In SPIE Proceedings, vol. 2468, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.210433
• Bortolami, Simone B., Helen Webb, Michael Richman, and Peter Norton. 2020. “Evaluation of a ‘Black-Box’ State-of-the-Art Vision-Based Navigation Algorithm for GPS-Denied Navigation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2020.17765
• Bortz, J. E., Sr. 1970. A New Concept in Strapdown Inertial Navigation. NASA-TR-R-329. NASA. https://ntrs.nasa.gov/citations/19700013316
• Bosch, J. A., and W. J. Kuehl. 1976. Reconfigurable Redundancy Management for Aircraft Flight Control. AIAA PAPER 76-1932. General Electric Co. https://ntrs.nasa.gov/citations/19760058477
• Bose, S. 1979. “Radar Updated Strapdown Inertial Midcourse Guidance Performance Analysis for Missiles.” In Guidance and Control Conference. AIAA 1979-1726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1726
• Bostock, Craig W. 1993. “Space Station Freedom Attitude Determination System Utilization of Star Tracker Capabilities.” In SPIE Proceedings, vol. 1949, edited by George E. Sevaston, Richard H. Stanton. SPIE. https://doi.org/10.1117/12.157072
• Bouazza, Tarek. n.d. “Contributions to Geometric Observer Design for Visual-Inertial Navigation.” PhD diss., Université Côte d’Azur. https://doi.org/10.70675/3f6d92c1zb960z4374z823bz61d974615240
• Bovens, N. L. A. 1994. “Position Accuracy of Celestial Fixes.” Journal of Navigation 47 (2): 214–20. https://doi.org/10.1017/s0373463300012133
• Bowcutt, Kevin, Richard Burrows, and Jeffery Weir. 1999. “Test Techniques to Determine Fasthawk Missile Aerodynamics Including Inlet Effects.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-432. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-432
• Bowditch, D., and R. Coltrin. 1983. “A Survey of Inlet/engine Distortion Compatibility.” In 19th Joint Propulsion Conference. AIAA 1983-1166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1166
• Bowers, J., D. Debra, J. Rodden, and E. Scott. 1967. “Orbital Gyrocompassing Heading Reference.” In Control and Flight Dynamics Conference. AIAA 1967-587. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-587
• Bowers, E. J., Jr. 1967. Calibration of Star-Tracker Bias Errors on OAO.. NASA. https://ntrs.nasa.gov/citations/19670053750
• Bowman, James S., Jr., and Frederick M. Healy. 1959. Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the North American T2J-1 Airplane. NASA-TM-SX-245. NASA. https://ntrs.nasa.gov/citations/19980227178
• Boxer, G. 1979. “Turbo Jet Engine, Ramjet and Rocket.” In Applications of Engineering Thermodynamics. Macmillan Education UK. https://doi.org/10.1007/978-1-349-04041-4_8
• Boyarsky, M. N. 1989. “Attitude Determination Using Star Tracker Data.” In Data Analysis in Astronomy III. Springer US. https://doi.org/10.1007/978-1-4684-5646-2_21
• Boyd, J. 1965. “Optimal Utilization of Supersonic Favorable Interference to Obtain High Lift-Drag Ratios.” In Aircraft Design and Technology Meeting. AIAA 1965-752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-752
• Boyd, John W., and Gene P. Menees. 1959. Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-Edge-Flap Control or a Cambered Forebody. NASA-MEMO-4-21-59A. NASA. https://ntrs.nasa.gov/citations/19980232086
• Boykov, Alexey, V. A. Mikhalskiy, and V. N. Ivantsov. 2017. “Evaluation of Navigation System Accuracy Indexes for Deviation Reading from Average Range.” TransNav, the International Journal on Marine Navigation and Safety of Sea Transportation 11 (4): 641–44. https://doi.org/10.12716/1001.11.04.10
• Braasch, Michael S. 2016. Inertial Navigation Systems. Wiley. https://doi.org/10.1002/9781119163060.ch1
• Brady, Tye M., Anthony S. Kourepenis, and William F. Wyman Jr. 2007. Integrated Inertial Stellar Attitude Sensor. Patent Application Number: US-Patent-Appl-SN-10/621,097. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20080009483
• Brady, Kevin, and Tzyh-Jong Tarn. 2001. “Handling Latency in Internet-Based Teleoperation.” In Beyond Webcams. The MIT Press. https://doi.org/10.7551/mitpress/1588.003.0016
• Braff, Ronald, and Nathaniel Braverman. 1965. “VLF Range-Range Navigation Error Contours.” Navigation 12 (1): 36–48. https://doi.org/10.1002/j.2161-4296.1965.tb01803.x
• Bralove, A. 1978. “Hand Held Calculators-An Evaluation of Their Use for Celestial Navigation.” Navigation 25 (4): 434–46. https://doi.org/10.1002/j.2161-4296.1978.tb01347.x
• Brammer, R. F. 1979. Estimation of the Ocean Geoid near the Blake Escarpment Using GEOS-3 Satellite Altimetry. NASA-CR-156857. NASA. https://ntrs.nasa.gov/citations/19790022697
• Brandon, Jay, C. Lan, Jilu Li, and Zhongjun Wang. 2001. “Estimation of Unsteady Aerodynamic Models from Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4017
• Braun, James, and Steve Podleski. 2019. “Propulsion Aerodynamics Workshop Special Topics: Supersonic Channeled Centerbody Inlet.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4021
• Brazzel, Charles E. 1963. The Effects of Base Bleed and Sustainer Rocket Nozzle Diameter and Location on the Base Drag of a Body of Revolution with Concentric Boost and Sustainer Rocket Nozzles. Defense Technical Information Center. https://doi.org/10.21236/ad0423963
• Breadboard Stellar Tracker System Test Report, Volume 2. 1981. NASA-CR-161954. NASA. https://ntrs.nasa.gov/citations/19820008298
• Breakwell, J. V. 1969. “Slightly Non-Linear Estimation with Noisy Data.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19690061381
• Brenner, Mats. 1996. “Integrated GPS/Inertial Fault Detection Availability.” Navigation 43 (2): 111–30. https://doi.org/10.1002/j.2161-4296.1996.tb01920.x
• Brereton, Peter, Holly Leopardi, Anand Mylapore, et al. n.d. Atom Interferometer Gravity Gradiometer (AIGG): Testbed for the Next-Generation Gravity Recovery Mission. Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20230007844
• Bresnahan, D. L. 1968. Experimental Investigation of a 10 Deg Conical Turbojet Plug Nozzle with Iris Primary and Translating Shroud at Mach Numbers from 0 to 2.0. NASA-TM-X-1709. NASA. https://ntrs.nasa.gov/citations/19690004981
• Bresnahan, D. L., and A. L. Johns. 1968. Cold Flow Investigation of a Low Angle Turbojet Plug Nozzle with Fixed Throat and Translating Shroud at Mach Numbers from 0 to 2.0. NASA-TM-X-1619. NASA. https://ntrs.nasa.gov/citations/19680020481
• Brewer, H. 1974. “Parameters Affecting Aircraft Tire Control Forces.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-966
• Brieger, Oliver, Daniel Ossmann, Markus Rüdinger, and Matthias Heller. 2008. “A New Flight Test Technique for Pilot Model Identification.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6556
• Briggs, M. 1986. “The Wavethruster Configuration Concept for High Lift/low Drag Supersonic Missiles.” In 24th Aerospace Sciences Meeting. AIAA 1986-571. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-571
• Bright, L. G., and V. L. Peterson. 1960. Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5. NASA-TM-X-392. NASA. https://ntrs.nasa.gov/citations/19650018341
• Brink, Kevin, John Hurtado, Andrey Soloviev, Adam Rutkowski, and Timothy Klausutis. 2010. “Integrated Estimation and Control Approach for Vision Aided Inertial Navigation.” In AIAA Infotech@Aerospace 2010. AIAA 2010-3403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-3403
• Briones, Alejandro M., and Brent A. Rankin. 2024. “Large Eddy Simulation with Sliding Mesh Method of a Small-Scale Turbojet Engine.” In Volume 1: Aircraft Engine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2024-121649
• Britting, K. R. 1968. Analysis of Space Stabilized Inertial Navigation Systems. NASA-CR-94735. NASA. https://ntrs.nasa.gov/citations/19680015237
• Britting, K. R. 1969a. Error Analysis of Strapdown and Local Level Inertial Systems Which Compute in Geographic Coordinates. NASA-CR-107741. NASA. https://ntrs.nasa.gov/citations/19700007517
• Britting, K. R. 1969b. State Transition Matrix for Inertial Navigation Systems. NASA-CR-107878. NASA. https://ntrs.nasa.gov/citations/19700008298
• Britting, K. R. 1969c. Strapdown Navigation Equations for Geographic and Tangent Coordinate Frames. NASA-CR-103296. NASA. https://ntrs.nasa.gov/citations/19690021973
• Britting, K. 1971c. “Unified Error Analysis of Terrestrial Inertial Navigation Systems.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-901
• Britting, K., S. Madden Jr., and R. Hildebrant. 1972. “The Impact of Gradiometer Techniques on the Performance of Inertial Navigation Systems.” In Guidance and Control Conference. AIAA 1972-850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-850
• Britting, K. R., and T. Palsson. 1968. Self Alignment Techniques for Strapdown Inertial Navigation Systems with Aircraft Application. NASA-CR-98671. NASA. https://ntrs.nasa.gov/citations/19690004931
• Brock, Marc, and Milton Franke. 2004. “Two-Stage-to-Orbit Reusable Launch Vehicle Propulsion Performance Study.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3903. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3903
• Brock, Larry, and George Schmidt. 1966. “Statistical Estimation in Inertial Navigation Systems.” In Guidance and Control Conference. AIAA 1966-1849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1849
• Brockmann, Kolja, and Dmitry Stefanovich. 2022. Hypersonic Boost-Glide Systems and Hypersonic Cruise Missiles: Challenges for the Missile Technology Control Regime. https://doi.org/10.55163/bdyx5243
• Broden, S. 1997. “Radar Tracking of Seaskimmers. Report from Field Trials with the CHASE Algorithm.” In Radar Systems (RADAR 97), vol. 1997. IEE. https://doi.org/10.1049/cp:19971775
• Brodersen, R. 1970. “Fluidic Inertial Platform.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1009. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1009
• Brodovsky, James, and Philip Dames. 2026. “Navigation in GNSS-Denied Environments Using MEMS-Grade Sensors and Geophysical Anomalies: A UKF Approach.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20508
• Brodzik, Łukasz. 2024a. “Gas temperature distribution in the evaporator of GTM400 turbojet engine.” Archives of Thermodynamics: 185–96. https://doi.org/10.24425/ather.2023.149731
• Brodzik, Lukasz. 2024b. “Stand Characteristics of the GTM 400 MOD Turbojet Engine.” Technical Sciences. https://doi.org/10.31648/ts.10159
• Broglio, Luigi. 1961. On Guidance and Landing Accuracy Requirements in Re-Entry Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ad0294976
• Bromberg, Joan Lisa. 1992. “Inventing Accuracy: A Historical Sociology of Nuclear Missile Guidance. Donald MacKenzie.” Isis 83 (3): 523–24. https://doi.org/10.1086/356271
• Brooks, J. E. 1961. Analysis of Ballistic Missile Performance. Part i. Basic Theory. Defense Technical Information Center. https://doi.org/10.21236/ad0607411
• Brooks, C. W., Jr., and C. D. Cone Jr. 1966. Hypersonic Aerodynamic Characteristics of Aircraft Configurations with Canard Controls. NASA-TN-D-3374. NASA. https://ntrs.nasa.gov/citations/19660012984
• Brooks, E., Jr., and F. Dejarnette. 1970. “Supersonic Flow of Nonuniform Free-Streams past Aerodynamic Decelerators.” In 3rd Aerodynamic Deceleration Systems Conference. AIAA 1970-1176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1176
• Brophy, Christopher M., and Clark W. Hawk. 1990. Flow Visualization of Four-Inlet Ducted Rocket Engine Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada378098
• Brouwer, Kirk, Abhijit Gogulapati, and Jack J. McNamara. 2016. “Efficient Treatment of Structural Deformation for Aerothermoelastic Loads Prediction in High-Speed Flows.” In 15th Dynamics Specialists Conference. AIAA 2016-1089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1089
• Brouwer, Kirk R., and Jack J. McNamara. 2019. “Refinement of CFD Surrogates for Aerothermoelastic Loads Prediction in High-Speed Flows.” In AIAA Scitech 2019 Forum. AIAA 2019-1121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1121
• Brower, W., Jr. 1989. “Theoretical Study of Passive Drag-Reduction on Transonic Airfoils.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3382. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3382
• Brown, Clarence A. 1955. Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of the Sidewinder Missile at Mach Numbers from 1.2 to 2.1. NACA-RM-SL55K16. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026358
• Brown, Robert. 1961. “Supersonic Trim Drag.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/610096
• Brown, R. D. 1975. Power Spectra of Geoid Undulations. NASA-TM-X-71028. NASA. https://ntrs.nasa.gov/citations/19760008467
• Brown, Richard D. 1983. Inversion of Moving-Base Gravity-Gradiometer Data for Geophysical Information. Defense Technical Information Center. https://doi.org/10.21236/ada126725
• Brown, Philip W. 1987. Flight Test Results for Several Light, Canard-Configured Airplanes. SAE PAPER 871801. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880043560
• Brown, Todd S. 2013. “In-Flight Performance of the Cassini Hemispherical Quartz Resonator Gyro Inertial Reference Units.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4630
• Brown, H. E., R. W. Dove, and R. A. McKern. 1973. “Failure Detection and Isolation of Redundant Inertial Systems for Space Shuttle.” In Symposium on Automatic Control in Space. https://ntrs.nasa.gov/citations/19740056742
• Brown, R. G., and L. L. Hagerman. 1969. “An Optimum Inertial/Doppler-Satellite Navigation System.” Navigation 16 (3): 260–70. https://doi.org/10.1002/j.2161-4296.1969.tb01664.x
• Brown, Glen, Roy Haggard, and Richard Benney. 2000. “Parachute Retraction Soft-Landing Systems Using Pneumatic Muscle Actuators.” In Modeling and Simulation Technologies Conference. AIAA 2000-4308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4308
• Brown, G., G. Harris, and G. Seemann. 1978. “A Subsonic Ramjet Engine for Expendable Drones.” In 14th Joint Propulsion Conference. AIAA 1978-962. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-962
• Brown, Nichols, and John Olds. 2005. “Evaluation of Multidisciplinary Optimazation (MDO) Techniques Applied to a Reusable Launch Vehicle.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-707. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-707
• Brown, W. W., and D. A. Redwine. 1948. Stess Analysis of Landing Gear XB-36,. Defense Technical Information Center. https://doi.org/10.21236/adb812167
• Brown, C. A., Jr. 1957. Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low-Aspect-Ratio Wing and Blunt Nose at Mach Numbers from 1.2 to 2.1. NACA-RM-L55K16. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710066230
• Broxmeyer, Charles. 1962. “Damping an Inertial Navigation System.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395586-9.50018-0
• Broxmeyer, C., D. MacKinnon, and P. Madden. 1968. Applications of Inertial Navigation and Modern Control Theory to the All Weather Landing Problem. NASA-CR-86096. NASA. https://ntrs.nasa.gov/citations/19680024688
• Brudnak, Mark J. 2016. “Predictive Displays for High Latency Teleoperation.” In SAE Technical Paper Series, vol. 1. National Defense Industrial Association. https://doi.org/10.4271/2024-01-3607
• Brudnak, Mark. 2020. “Predictive Diplays for High Latency Teleoperation: Extensions and Experiments.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2024-01-3842
• Brulle, R. 1977. “Dive Bombing Simulation Results Using Direct Side Force Control Modes.” In Guidance and Control Conference. AIAA 1977-1118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1118
• Brummund, U., and F. Scheel. 2002. “Imaging of Mixing and Combustion Processes in a Supersonic Combustion Ramjet Chamber.” International Journal of Energetic Materials and Chemical Propulsion 5 (1–6): 762–72. https://doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.790
• Brunner, T., and R. Nerem. 1970. “Initial Results on Theoretical Prediction of Drag for a Trailing Decelerator at Supersonic Speeds.” In 3rd Aerodynamic Deceleration Systems Conference. AIAA 1970-1177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1177
• Bryant, W. H., and F. R. Morrell. 1981. “Description of a Dual Fail-Operational Redundant Strapdown Inertial Measurement Unit for Integrated Avionics Systems Research.” In ROLM Computer Users Group Meeting. https://ntrs.nasa.gov/citations/19810042530
• Bryant, W., F. Morrell, and M. Bailey. 1984. “Flight Test Configuration for Verifying Inertial Sensor Redundancy Management Techniques.” In Aircraft Design Systems and Operations Meeting. AIAA 1984-2496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2496
• Bryant, L., M. Tigges, and D. Ives. 1998. “Analytic Drag Control for Precision Landing and Aerocapture.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4572
• Bryson, Joshua, Ilmars Celmins, and Frank Fresconi. 2019. “Aerodynamics and Aeroelasticity for Canard Control Actuation Technology on a Subsonic, Gun-Launched Munition.” In AIAA Scitech 2019 Forum. AIAA 2019-1593. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1593
• Bryson, Joshua, and Benjamin Gruenwald. 2022. Automated Gain-Scheduling Approach for Three-Loop Autopilot. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1181622
• Bryson, A., Jr. 1971a. “Three-Dimensional, Minimum Fuel Turns for a Supersonic Aircraft.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-913. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-913
• Bryson, A., Jr. 1971b. “Three-Dimensional, Minimum-Time Turns for a Supersonic Aircraft.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-796
• Bryson, A., Jr., and M. Desai. 1968. “The Energy-State Approximation in Performance Optimization of Supersonic Aircraft.” In Control and Flight Dynamics Conference. AIAA 1968-877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-877
• Bryson, A. E., Jr., and R. K. Mehra. 1968. “Linear Smoothing Using Measurements Containing Correlated Noise with an Application to Inertial Navigation.” In JOINT AUTOMATIC CONTROL CONFERENCE. https://ntrs.nasa.gov/citations/19680055593
• Brzezowski, S., D. Gleason, J. Goldstein, W. Heller, Christopher Jekeli, and J. White. 1989. “Synopsis of Early Field Test Results from the Gravity Gradiometer Survey System.” In Ohio State Univ., Progress in the Determination of the Earth’s Gravity Field. https://ntrs.nasa.gov/citations/19900011209
• Brzezowski, Steven J., and Robert C. Merenyi. 1986. Aided-Airborne Gravity Gradiometer Survey System (GGSS) Study. Defense Technical Information Center. https://doi.org/10.21236/ada170749
• Bu, Feng, Shuwen Guo, Mengmeng Cheng, Fen Zheng, Dacheng Xu, and Heming Zhao. 2019. “Effect of Circuit Phase Delay on Bias Stability of MEMS Gyroscope under Force Rebalance Detection and Self-Compensation Method.” Journal of Micromechanics and Microengineering 29 (9): 095002. https://doi.org/10.1088/1361-6439/ab27e8
• Bu, Suwan, Liang Yan, Nannan Du, and Xinghua He. 2025. “High Stability and Precision Sliding Mode Robust Control of Two-Axis Inertial Stabilization Platform.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2232-0_51
• Bucy, Richard S. 1979. New Methods for Analysis of the Performance of Guidance and Control Systems. Defense Technical Information Center. https://doi.org/10.21236/ada078534
• Buell, Heinz. 1964. “Doppler, Inertial, and Doppler-Inertial Techniques.” Navigation 11 (3): 250–59. https://doi.org/10.1002/j.2161-4296.1964.tb02099.x
• Buell, Heinz, and William C. Reed. 1967. “U. T. M. Grid Navigation by Doppler-Inertial Airborne Gyrocompassing.” Journal of the American Helicopter Society 12 (2): 14–25. https://doi.org/10.4050/jahs.12.14
• Buell, Donald A., and Bruce E. Tinling. 1959. The Static Longitudinal Stability and Control Characteristics in the Presence of the Ground of a Model Having a Triangular Wing and Canard. NASA-MEMO-3-4-59A. NASA. https://ntrs.nasa.gov/citations/19980228228
• Bullard, John W. 1963. History of the Field Army Ballistic Missile Defense System Project, 1959-1962. Defense Technical Information Center. https://doi.org/10.21236/ada434111
• Bullard, John W. 1965. History of the Redstone Missile System. Defense Technical Information Center. https://doi.org/10.21236/ada434109
• Bullock, T. E., and S. L. Fields. 1998. Application of Robust Control and Gain Scheduling to Missile Autopilot Design. Defense Technical Information Center. https://doi.org/10.21236/ada357847
• Bumer, C. T. 1946. Range and Tracking Accuracy of AN/APG-15B. Defense Technical Information Center. https://doi.org/10.21236/ada801531
• Bunge, Roberto, Felipe Munera Savino, and Ilan Kroo. 2015. “Stall/Spin Flight Test Techniques with COTS Model Aircraft and Flight Data Systems.” In AIAA Flight Testing Conference. AIAA 2015-3225. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3225
• Burchett, Bradley, Justin Paul, Joseph Vasile, and Joshua Bryson. 2021. A High Fidelity Roll Dependent Aerodynamic Model for a Long Range High Speed Missile. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1141614
• Burdess, J. S. 1983. “The Vibro-Mass Gyroscope.” Journal of Dynamic Systems, Measurement, and Control 105 (1): 18–23. https://doi.org/10.1115/1.3139722
• Burgan, Elmer T., and Fletcher C. Paddison. 1974. Surface Effect Takeoff and Landing System (SETOLS). Defense Technical Information Center. https://doi.org/10.21236/ada000101
• Burkardt, Leo A., and Leo C. Franciscus. 1990. “RAMSCRAM: A Flexible RAMJET/SCRAMJET Engine Simulation Program.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/90-gt-323
• Burke, Brian J., and Jonathan Poggie. 2023. “URANS Simulations of Inlet-Isolator Unstart at Mach 4.9.” In AIAA SCITECH 2023 Forum. AIAA 2023-1467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1467
• Burley, R. R., and A. H. Mansour. 1970. Static Performance of an Auxiliary Inlet Ejector Nozzle Using an Afterburning Turbojet Gas Generator. NASA-TM-X-1999. NASA. https://ntrs.nasa.gov/citations/19700015497
• Burns, William. 2006. “The Impact of Component Development on the Evolution of the Fiber Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.2006.ma2
• Burns, Michael. 2020. “Progress at Sandia for the DoD Common Hypersonic Boost Glide Vehicle and Autonomy for Hypersonics.” In Proposed for presentation at the Autonomous & Hypersonic Weapons Systems And Advanced Capability Enablers held November 4-6, 2020.. US DOE. https://doi.org/10.2172/1829235
• Burns, W. K., R. P. Moeller, C. A. Villarruel, and M. Abebe. 1983. “Fiber Optic Gyroscope with Polarization Holding Fiber.” In Optical Fiber Communication. OSA. https://doi.org/10.1364/ofc.1983.pd2
• Burr, R. 1968. “A Control System Concept for an Axisymmetric Supersonic Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-581
• Burris, P. 1966. “Dynamic Test Method for Supersonic Inlet/engine Development.” In 2nd Aerodynamic Testing Conference. AIAA 1966-741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-741
• Burrows, R. 1967. “Description of an Inertial Test Facility Located 1,100 Feet below the Surface of the Earth.” In Control and Flight Dynamics Conference. AIAA 1967-538. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-538
• Burrows, Travis J., Bojan Vukasinovic, and Ari Glezer. 2017. “Fluidic Control of an Aggressive Offset Diffuser for a Supersonic Inlet.” In 47th AIAA Fluid Dynamics Conference. AIAA 2017-4304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4304
• Burstadt, P. L., and J. E. Calogeras. 1974. Instantaneous Distortion in a Mach 2.5, 40-Percent-Internal-Contraction Inlet and Its Effect on Turbojet Stall Margin. NASA-TM-X-3002. NASA. https://ntrs.nasa.gov/citations/19740022130
• Burstadt, P. L., J. E. Calogeras, and R. E. Coltrin. 1971. “Instantaneous and Dynamic Analysis of Supersonic Inlet-Engine Compatibility.” In AIAA. https://ntrs.nasa.gov/citations/19710050036
• Burton, Philip R. 1959. “Celestial Navigation without a Vertical Reference.” Navigation 6 (5): 317–20. https://doi.org/10.1002/j.2161-4296.1959.tb01960.x
• Burton, Thomas D. 1981. Air Cushion Landing System Stability Study. Defense Technical Information Center. https://doi.org/10.21236/ada097744
• Buschek, Harald, and Harald Buschek. 1997. “Robust Autopilot Design for Future Missile Systems.” In Guidance, Navigation, and Control Conference. AIAA 1997-3763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3763
• Bush, R. W., and G. C. Newton Jr. 1964. Reduction of Errors in Vibratory Gyroscopes by Double Modulation. NASA. https://ntrs.nasa.gov/citations/19650035159
• Bushnell, D. 1990. “Supersonic Aircraft Drag Reduction.” In 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1990-1596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1596
• Bushnell, Dennis M. 2004. “Shock Wave Drag Reduction.” Annual Review of Fluid Mechanics 36 (1): 81–96. https://doi.org/10.1146/annurev.fluid.36.050802.122110
• Busnardo, David, Matthew Aitken, Robert Tolson, Diego Pierrottet, and Farzin Amzajerdian. 2011. “LIDAR-Aided Inertial Navigation with Extended Kalman Filtering for Pinpoint Landing over Rough Terrain.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-428
• Bustard, Andrew, Benjamin L. Bemis, and Thomas J. Juliano. 2024. “Global Time-Resolved Measurements of Axisymmetric Inlet/Isolator Unstart Induced by Mass Injection.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3893
• Butler, Cassandra J., Elizabeth K. Benitez, Joseph S. Jewell, Christopher J. Ruscher, and Sivaram P. Gogineni. 2022. “Pre- and Post-Flight Hypersonic Glide Vehicle Surface Roughness Measurements.” In AIAA SCITECH 2022 Forum. AIAA 2022-1905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1905
• Butler, Cassandra J., Elizabeth K. Benitez, Joseph S. Jewell, Christopher J. Ruscher, and Sivaram Gogineni. 2023. “Pre- and Post-Flight Surface Roughness Measurements on the X-23 Hypersonic Glide Vehicle.” In AIAA SCITECH 2023 Forum. AIAA 2023-1539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1539
• Butsko, J. 1966. “Prediction of the Subsonic Base Drag of Hypersonic Re-Entry Vehicles.” In 3rd Annual Meeting. AIAA 1966-991. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-991
• Butze, H. F., H. M. Moyer, and A. M. Trout. 1969. Performance of Swirl-Can Turbojet Combustors at Simulated Supersonic Combustor-Inlet Conditions. NASA-TN-D-4996. NASA. https://ntrs.nasa.gov/citations/19690006822
• Bużantowicz, Witold. 2015. “Modeling of Ballistic Missile Flight Trajectory in a Central Gravitational Field.” Mechanik, no. 7: 557/73-557/82. https://doi.org/10.17814/mechanik.2015.7.216
• Buzantowicz, W. 2019. “A Linear-Quadratic Stabilization System for a Canard-Controlled Missile.” In Engineering Mechanics. Institute of Thermomechanics of the Czech Academy of Sciences, Prague. https://doi.org/10.21495/71-0-73
• Bychkov, V. L., L. P. Grachev, I. I. Esakov, and A. V. Semenov. 2020. “Base Drag Reduction and Generation of the Lifting Force Using a Microwave Discharge in a Supersonic Flow.” Technical Physics 65 (8): 1233–38. https://doi.org/10.1134/s1063784220080046
• Bynum, James A., and Garvin L. Holman. 1979. Tactical Night Terrain Flight Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada086458
• Byrdsong, T. A. 1973. Some Effects of Grooved Runway Configurations on Aircraft Tire Braking Traction under Flooded Runway Conditions. NASA-TN-D-7215. NASA. https://ntrs.nasa.gov/citations/19730012330
• Caglayan, A. K., and R. E. Lancraft. 1982. Fault Tolerant Navigation in a Microwave Landing System Environment. Bolt, Beranek, and Newman, Inc. https://ntrs.nasa.gov/citations/19840029646
• Cagle, Mary T. 1977. History of the TOW Missile System. Defense Technical Information Center. https://doi.org/10.21236/ada434477
• Cai, Gui Fang. 2014. “Design of a Virtual Automatic Test System of the Missile Autopilot.” Applied Mechanics and Materials 543-547: 1377–80. https://doi.org/10.4028/www.scientific.net/amm.543-547.1377
• Cai, Xiangqun, Xiaoyong Lei, Shuling Dai, and Weiqi Li. 2024. “Flight Test Design and Nonlinear Model Identification for Landing Gear Aerodynamics.” International Journal of Aeronautical and Space Sciences 26 (2): 800–814. https://doi.org/10.1007/s42405-024-00786-6
• Cai, Shaokun, Kaidong Zhang, Meiping Wu, Yangming Huang, and Yapeng Yang. 2015. “An Iterative Method for the Accurate Determination of Airborne Gravity Horizontal Components Using Strapdown Inertial Navigation System/global Navigation Satellite System.” Geophysics 80 (6): G119-G129. https://doi.org/10.1190/geo2014-0063.1
• Cairns, A. H. 1970. “Autopilot Compatibility of the Digital Inertial Guidance System Used in the Eldo ‘Europa’ Launch Vehicle.” In Astrophysics and Space Science Library. Springer Netherlands. https://doi.org/10.1007/978-94-011-7551-7_9
• Cake, W. 1965. “Monitoring for Engine Maintenance in the Supersonic Transport.” In Propulsion Joint Specialist Conference. AIAA 1965-578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-578
• Calarese, W., and R. Walterick. 1978. “Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1180
• Calder, P., and P. Gupta. 1978. “Engine Options for Supersonic Cruise Aircraft.” In 14th Joint Propulsion Conference. AIAA 1978-1054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1054
• Calhoun, Philip. 2000. “An Entry Flight Controls Analysis for a Reusable Launch Vehicle.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-1046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1046
• Callaway, Lawrence C. 1963. Pacific Missile Range Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ad0405121
• Callinan, Joseph, and Gary Hikiss. 2002. “Operating Experience with the Turbine Technologies Sr 30 Turbojet Engine Test System.” In 2002 Annual Conference Proceedings. ASEE Conferences. https://doi.org/10.18260/1-2–10481
• Calogeras, J. E. 1969a. Experimental Investigation of Dynamic Distortion in a Mach 2.50 Inlet with 60 Percent Internal Contraction and Its Effect on Turbojet Stall Margin. NASA-TM-X-1842. NASA. https://ntrs.nasa.gov/citations/19690029214
• Calogeras, J. 1969b. “Supersonic Wind Tunnel Investigation of Inlet- Engine Compatibility.” In 5th Propulsion Joint Specialist. AIAA 1969-487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-487
• Camacho, Juan G., Lawrence F. Guest, Belen M. Hernandez, et al. 2007. Open Architecture as an Enabler for FORCEnet Cruise Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada473090
• Campbell, M. 1964. “A Celestial Orientation System Based on Star Pattern Recognition.” In Astrodynamics Guidance and Control Conference. AIAA 1964-652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-652
• Campbell, Jacob, Maarten Uijt De Haag, and Frank Van Graas. 2005. “Terrain-Referenced Positioning Using Airborne Laser Scanner.” Navigation 52 (4): 189–97. https://doi.org/10.1002/j.2161-4296.2005.tb00362.x
• Campbell, Jacob, Maarten Uijt De Haag, and Frank Van Graas. 2007. “Terrain-Referenced Precision Approach Guidance: Proof-of-Concept Flight Test Results.” Navigation 54 (1): 21–29. https://doi.org/10.1002/j.2161-4296.2007.tb00392.x
• Campbell, J., and S. Ellis. 1970. “Inlet-Engine Compatibility Analysis.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-941
• Campbell, Stefan F., Nhan T. Nguyen, John Kaneshige, and Kalmanje Krishnakumar. 2009. “Parameter Estimation for a Hybrid Adaptive Flight Controller.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090035862
• Campbell Jones, L. 1995. “The Application of the MATLAB/SIMULINK Analysis Packages to the Design of a Discrete Linear Quadratic Optimal Missile Autopilot.” In IEE Colloquium on Applied Control Techniques Using MATLAB, vol. 1995. IEE. https://doi.org/10.1049/ic:19950054
• Canciani, Aaron, and Kevin Brink. 2017. “Improved Magnetic Anomaly Navigation Accuracy through Cooperative Navigation.” In ION Pacific PNT. Institute of Navigation. https://doi.org/10.33012/2017.15059
• Canciani, Aaron J., and John F. Raquet. 2016a. “Magnetic Anomaly Navigation Accuracy with Respect to Map Quality and Altitude.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2016.13415
• Canciani, Aaron J., and John F. Raquet. 2016b. “Validation of a Magnetic Anomaly Navigation Model with Flight Test Data.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2016.14852
• Candler, Graham V. 2001. Effect of Internal Energy Excitation on Supersonic Blunt-Body Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ada387503
• Candler, Graham, and J. Kelley. 1999. “Effect of Internal Energy Excitation on Supersonic Blunt-Body Drag.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-418
• Cangelosi, Jonathan, Matthias Heinkenschloss, Jacob T. Needels, and Juan J. Alonso. 2024. “Simultaneous Design and Trajectory Optimization for Boosted Hypersonic Glide Vehicles.” In AIAA SCITECH 2024 Forum. AIAA 2024-0375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0375
• Canniff, J. 1969. “Flight Test Report of Experiments in Inertial Navigation System Updating.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-842
• Cantó, Begoña, Carmen Coll, and Elena Sánchez. 2009. “Structural Identifiability of Linear Singular Dynamic Systems.” In Lecture Notes in Control and Information Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-02894-6_23
• Cao, Huiliang. 2023a. “Dual-Mass Linear Vibration Silicon Based MEMS Gyroscope Monitoring Circuit Design and Test Technology.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_7
• Cao, Huiliang. 2023c. “Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope Quadrature Error Correction Technology and Optimization.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_4
• Cao, Huiliang. 2023d. “Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope Sensing Closed Loop and Frequency Tuning Technology.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_5
• Cao, Huiliang. 2023e. “Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope Structure Noise Analysis and System Model.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_3
• Cao, Huiliang. 2023f. “Silicon Based MEMS Gyroscope Structure and Working Principle.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_2
• Cao, Huiliang. 2023g. “Temperature Influence on Silicon-Based MEMS Gyroscope and Suppression Method.” In Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6_6
• Cao, Huiliang. 2026. “High-Precision MEMS Ring Vibration Gyroscope.” In Handbook of Wireless Positioning. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-1650-4_54-1
• Cao, Huiliang, Rang Cui, Wei Liu, et al. 2021a. “Dual Mass MEMS Gyroscope Temperature Drift Compensation Based on TFPF-MEA-BP Algorithm.” Sensor Review 41 (2): 162–75. https://doi.org/10.1108/sr-09-2020-0205
• Cao, Huiliang, and Li Jian-hua. 2018. “Dual-Mass MEMS Gyroscope Structure, Design, and Electrostatic Compensation.” In InTech eBooks. https://doi.org/10.5772/intechopen.74364
• Capey, E. C. 1961. “Transient Temperature Distributions in an Insulated Multi-Spar Wing: An Approximate Method of Solution for a Structure Subjected to Aerodynamic Heating Based on a System of Regions Having Similar Rates of Temperature Rise.” Aircraft Engineering and Aerospace Technology 33 (10): 282–88. https://doi.org/10.1108/eb033463
• Capone, Francis, Scott Asbury, and Karen Deere. 1996. “Experimental and Computational Induced Aerodynamics from Missile Jet Reaction Controls at Angles of Attack to 75 Deg.” In 14th Applied Aerodynamics Conference. AIAA 1996-2479. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2479
• Caraway, Willie D., and Randy R. 2001. An Analysis of Multi-Role Survivable Radar Tracking Performance Using the KTP-2 Group’s Real Track Metrics. Defense Technical Information Center. https://doi.org/10.21236/ada394832
• Cardoso Navarro, Lucas, and Luiz Carlos Sandoval. 2019. “Aircraft Braking Dynamics and Brake System Modeling for Fault Detection and Isolation.” In DINAME2019. ABCM. https://doi.org/10.26678/abcm.diname2019.din2019-0181
• Carek, David A. 1993. Structural Analysis of High-Rpm Composite Propfan Blades for a Cruise Missile Wind Tunnel Model. NASA-TM-105267. NASA. https://ntrs.nasa.gov/citations/19930013826
• Carestia, R. A., R. J. Hruby, and W. S. Bjorkman. 1983. Flight Test Results of the Strapdown Ring Laser Gyro Tetrad Inertial Navigation System. NASA-TM-84358. NASA. https://ntrs.nasa.gov/citations/19840003089
• Carey, Kevin, Benjamin Abruzzo, David P. Harvie, and Christopher Korpela. 2019. “Performance Comparison of Inertial Measurement Units Fused with Odometry in Extended Kalman Filter for Dead-Reckoning Navigation.” In Volume 5A: 43rd Mechanisms and Robotics Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/detc2019-98184
• Carlin, C. M., I. Frisch, J. J. Kolden, et al. 2003. Supersonic Test of the 10-Inch Bifurcated Two-Stage Supersonic Inlet (BTSSI). NASA/CR-2003-212313. NASA. https://ntrs.nasa.gov/citations/20030065839
• Carlsen, Wayne. 1994. “Development of Transonic Area-Rule Methodology.” In 12th Applied Aerodynamics Conference. AIAA 1994-1841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1841
• Carlson, Harry W. 1953. Preliminary Investigation of the Effects of Body Contouring as Specified by the Transonic Area Rule on the Aerodynamic Characteristics of a Delta Wing-Body Combination at Mach Numbers of 1.41 and 2.01. NACA-RM-L53G03. NASA. https://ntrs.nasa.gov/citations/19930087841
• Carlson, E. 1974. “Direct Sideforce Control for Improved Weapon Delivery Accuracy.” In 12th Aerospace Sciences Meeting. AIAA 1974-70. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-70
• Carlson, C. H. 1983. Preliminary Scramjet Design for Hypersonic Airbreathing Missile Application. NASA-CR-3742. NASA. https://ntrs.nasa.gov/citations/19840005127
• Carlson, Jeffrey, and Joel Beer. 2021. Performance Comparison of Circular and Spherical Error Probable Estimators. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1777092
• Carmel, M. M., D. T. Gregory, and T. C. Kelly. 1958. Aerodynamic Characteristics at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight. NACA-RM-L58G16. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19680068704
• Carpenter, Russell J., and Itzhack Y. Bar-Itzhack. 2004. Schuler Period in LEO Satellites. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20040040118
• Carrara, S. L. A., B. Y. Kim, and H. J. Shaw. 1987a. “Bias Drift Reduction in Polarization-Maintaining Fiber Gyroscope.” Optics Letters 12 (3): 214. https://doi.org/10.1364/ol.12.000214
• Carrara, S. L. A., B. Y. Kim, and H. J. Shaw. 1987b. “Fiber Gyroscope with Birefringence Modulation.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937537
• Carrier, Gerald G., Jérémy Cadillon, Franck Morel, et al. 2021. “Combined Conceptual and Preliminary Aerodynamic Design of a Low-Boom Supersonic Civil Transport Aircraft for Holistic Evaluation of Its Environmental Impact.” In AIAA Aviation 2021 Forum. AIAA 2021-2568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2568
• Carrington, W. A. 1970. “A Comparison of Inertial Sensor Digitizing Techniques.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19710031756
• Carroll, Jason D., and Aaron J. Canciani. 2021. “Terrain-Referenced Navigation Using a Steerable-Laser Measurement Sensor.” NAVIGATION 68 (1): 115–34. https://doi.org/10.1002/navi.406
• Carroll, J. E., R. L. Lillestrand, and J. S. Newcomb. 1966. Automatic Celestial Guidance. II: New Challenge to Designers’ Ingenuity. NASA. https://ntrs.nasa.gov/citations/19660046353
• Carter, J. 1972. “Space Shuttle Terminal Navigation with Conventional Navigation Aids.” In Guidance and Control Conference. AIAA 1972-832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-832
• Carter, Campbell D. 2012. Supersonic Combustion Ramjet Research. Defense Technical Information Center. https://doi.org/10.21236/ada563331
• Carter, John F., and Christopher J. Nagy. 1995. The NASA Landing Gear Test Airplane. NASA-TM-4703. NASA. https://ntrs.nasa.gov/citations/19960012281
• Carter, Roy L., and Robert M. Springfield. 2002. Lightweight Ablating Insulation for Ramjet Combustion. Defense Technical Information Center. https://doi.org/10.21236/ada413060
• Caruso, David. n.d. “Improving Visual-Inertial Navigation Using Stationary Environmental Magnetic Disturbances.” PhD diss., Université Paris-Saclay (ComUE). https://doi.org/10.70675/5f69e2d2z8552z4b7aza5b6z53a102612282
• Caruso, P. S., Jr., and C. R. Naegeli. 1976. Theoretical and Empirical Low Perigee Aerodynamic Heating during Orbital Flight of an Atmosphere Explorer. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/19760052458
• Caruy Povoa, Pedro H., Rodrigo M. Granzoto, Gilberto G. Becker, and Mauro R. Lopez. 2018. “Landing Gear Drag Reduction Using Lattice Boltzmann Method.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1556
• Casasent, David. 1979. Optical Pattern Recognition for Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada082134
• Casasent, D. 1984. Optical Data Processing for Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada149346
• “Case Study: Base Drag and Base Aeroheating for Space Vehicles.” 2001. In Design Methodologies for Space Transportation Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861734.0821.0843
• Casey, Mark. n.d. “The Integration of Global Positioning System (GPS) Data and Inertial Navigation System (INS) Data to Determine the Navigation State.” PhD diss., The University of Queensland. https://doi.org/10.14264/311857
• Cassel, Louis A., Norbert A. Durando, Clark W. Bullard, and James M. Kelso. 1969. Jet Interaction Control Effectiveness for Subsonic and Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0862483
• Cassidy, Lawrence W. 1994. “Miniature Star Tracker for Precise Attitude Reference in Space.” In SPIE Proceedings, vol. 2210, edited by Thierry M. Dewandre, Joachim J. Schulte-in-den-Baeumen, Emmanuel Sein. SPIE. https://doi.org/10.1117/12.188075
• Castro, Mario, and Rob J. de Boer. 2020. “Testing Structural Identifiability by a Simple Scaling Method.” Preprint, bioRxiv. https://doi.org/10.1101/2020.02.04.933630
• Catalano, George, and Walter Sturek. 2000. “A Numerical Investigation of Supersonic Flow past an Aft Body.” In 18th Applied Aerodynamics Conference. AIAA 2000-4520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4520
• Catalano, George D., and Walter B. Sturek. 2001. A Numerical Investigation of Supersonic Flow around Aft Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada395936
• Cavacece, Massimo. 2024. “Error Analysis of Inertial Navigation Based on Quaternion Approach.” Journal of Machine Design and Automation Intelligence 2 (1): 20230005. https://doi.org/10.1515/jmdai-2023-0005
• Cavalleri, R., and S. Posey. 1988. “Effect of Injection Configuration on Base Drag Reduction.” In 26th Aerospace Sciences Meeting. AIAA 1988-213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-213
• Cechowicz, Radosław. 2017. “Bias Drift Estimation for MEMS Gyroscope Used in Inertial Navigation.” Acta Mechanica et Automatica 11 (2): 104–10. https://doi.org/10.1515/ama-2017-0016
• Celestial Navigation. 2025. Wiley. https://doi.org/10.1002/9781394267743.ch09
• “Celestial Navigation for the People.” 2020. In The Ocean Reader. Duke University Press. https://doi.org/10.1215/9781478007456-098
• Çelikel, Oğuz, and Ferhat Sametoğlu. 2012. “Assessment of Magneto-Optic Faraday Effect-Based Drift on Interferometric Single-Mode Fiber Optic Gyroscope (IFOG) as a Function of Variable Degree of Polarization (DOP).” Measurement Science and Technology 23 (2): 025104. https://doi.org/10.1088/0957-0233/23/2/025104
• Çeliktaş, Erhan, Ahmet Topuz, and Zafer Kazancı. 2012. “Friction and Wear Behaviors of Aircraft Brake Linings Material.” Aircraft Engineering and Aerospace Technology 84 (5): 279–86. https://doi.org/10.1108/00022661211255458
• Celmins, Ilmars. 1990. Projectile Supersonic Drag Characteristics. Defense Technical Information Center. https://doi.org/10.21236/ada224217
• Cenko, A. 1979. “Advances in Supersonic Configuration Design Methods.” In 17th Aerospace Sciences Meeting. AIAA 1979-233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-233
• Centaur in Retrospect: A Technical Survey of the Centaur Inertial Guidance System Evolution from 1959 to 1967. 1968. NASA-CR-86040. NASA. https://ntrs.nasa.gov/citations/19680009695
• Cerre, N., E. Taufflieb, T. Gaiffe, N. Faussot, P. Simonpiétri, and H. C. Lefèvre. 1997. “Fiber Bragg Grating for Use within High-Accuracy Fiber Optic Gyroscope.” In 12th International Conference on Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1997.owb7
• Cesaro, R. S., and C. L. Walker. 1955. Application of Non-Afterburning Turbojets to Supersonic Flight. NACA-RM-55K16. NASA. https://ntrs.nasa.gov/citations/19670022705
• Çetiner, Abdullah E., Bedri Yagiz, Goktan Guzel, Onur Özgür, and Ilteris Koc. 2016. “CFD Based Response Surface Modeling with an Application in Missile Aerodynamics.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-4336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4336
• Chakraborty, I. 1996. Analysis of Drift Errors in the JPL/UCLA Micromachined Gyroscope. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20060036406
• Chaloff, D., R. Hiyama, and C. Martindale. 1974. A Structural Weight Estimation Program (SWEEP) for Aircraft. Volume V: Air Induction System and Landing Gear Modules. Part 2: Landing Gear Module. Defense Technical Information Center. https://doi.org/10.21236/ada002858
• Chamberlin, R., and B. Blaha. 1973. “Flight and Wind Tunnel Investigation of the Effects of Reynolds Number on Installed Boattail Drag at Subsonic Speeds.” In 11th Aerospace Sciences Meeting. AIAA 1973-139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-139
• Chambers, J., and L. Yip. 1984. “Aerodynamic Characteristics of Two General Aviation Canard Configurations at High Angles of Attack.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2198. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2198
• Chambers, J. R., L. P. Yip, and T. M. Moul. 1984. Wind-Tunnel Investigation of an Advanced General Aviation Canard Configuration. NASA-TM-85760. NASA. https://ntrs.nasa.gov/citations/19840013471
• Champine, R. A. 1976. Crosswind Landing-Gear Position Indicator. LAR-11941. NASA. https://ntrs.nasa.gov/citations/19760000120
• Chan, David T., Gregory S. Jones, William E. Milholen, and Scott L. Goodliff. 2017. “Transonic Drag Reduction through Trailing-Edge Blowing on the FAST-MAC Circulation Control Model.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3246
• Chandak, Prof. Ashok. S., and Dr. Anil J. Patil. 2014. “Rotation Measurement and Signal Processing for Navigation Control System Using Fiber Optic Gyroscope.” International Journal of Advanced Research in Electrical, Electronics and Instrumentation Engineering 3 (11): 12969–76. https://doi.org/10.15662/ijareeie.2014.0311047
• Chandler, Frank O., and Ricardo Montes. 2019. “A CFD Investigation of a Diverterless Supersonic Inlet of Ellipsoidal Entrance Shape.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4274
• Chang, Z. S. 1962. Supersonic Drag of Slender Bodies in a Simple Diatomic Dissociating Gas. Defense Technical Information Center. https://doi.org/10.21236/ad0274359
• Chang, Sun Hyok. 1999. “Suppression of Bias Fluctuation in Direction Switched Fiber Laser Gyroscope.” In 13th International Conference on Optical Fiber Sensors. SPIE. https://doi.org/10.1117/12.2302109
• Chang, Lubin, Baiqing Hu, An Li, and Fangjun Qin. 2013. “Strapdown Inertial Navigation System Alignment Based on Marginalised Unscented Kalman Filter.” IET Science, Measurement & Technology 7 (2): 128–38. https://doi.org/10.1049/iet-smt.2012.0071
• Chang, Ing, and Louis G. Hunter. 1996a. CFD Study of Turbo-Ramjet Interactions in Hypersonic Airbreathing Propulsion System. NASA-CR-202418. NASA. https://ntrs.nasa.gov/citations/19970001125
• Chang, Ing, and Louis Hunter. 1996b. A CFD Study of Turbojet and Single-Throat Ramjet Ejector Interaction. Paper-28. Prairie View Agricultural and Mechanical Coll. https://ntrs.nasa.gov/citations/19960052324
• Chang, Juntao, Nan Li, Kejing Xu, Wen Bao, and Daren Yu. 2017c. “Recent Research Progress on Unstart Mechanism, Detection and Control of Hypersonic Inlet.” Progress in Aerospace Sciences 89: 1–22. https://doi.org/10.1016/j.paerosci.2016.12.001
• Chang, Juntao, Lei Wang, Daren Yu, and Wen Bao. 2012. “Real-Time Unstart Prediction and Detection of Hypersonic Inlet Based on Recursive Fourier Transform.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-4150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4150
• Chang, J., D. Yu, W. Bao, Z. Xie, and Y. Fan. 2009a. “A CFD Assessment of Classifications for Hypersonic Inlet Start/unstart Phenomena.” Aeronautical Journal 113 (1142): 263–71. https://doi.org/10.1017/s0001924000002931
• Chaowanapreecha, Puwit. n.d. “Aerodynamic Performance and Circular Error Probable Modeling of Grid Fins for Drone-Deployed Payloads in Low-Subsonic Flight.” PhD diss., Chulalongkorn University. https://doi.org/10.58837/chula.the.2024.964
• Chaowanapreecha, Puwit, Pitaakphong Rattanagraikanakorn, and Joshua Staubs. 2025. “Evaluating the Impact of Grid-Fin Stabilizers on Munition Trajectory and Accuracy: A Circular Error Probable Approach.” In AIAA SCITECH 2025 Forum. AIAA 2025-0478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0478
• Chapman, G., and D. Kirk. 1974. “Nonlinear Parameter Identification: Ballistic Range Experience Applicable to Flight Testing.” In Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017467
• Chapman, Gary, Robert Mitcheltree, and Wayne Hathaway. 1999. “Transonic and Low Supersonic Static and Dynamic Aerodynamic Characteristics of the Stardust Sample Return Capsule.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-1021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1021
• Chapman, Rowe, Jr. 1955. Aerodynamic Characteristics at Mach Numbers from 0.7 to 1.75 of a Four-Engine Swept-Wing Airplane Configuration as Obtained from a Rocket-Propelled Model Test. NACA-RM-L55F23. NASA. https://ntrs.nasa.gov/citations/19930089136
• “Chapter 1: Asymptotically Simplified Gas-Dynamic Models of Supersonic and Hypersonic Aerodynamics and Heat Transfer.” 2013. In Hypersonic Aerodynamics and Heat Transfer. Begell House Inc. https://doi.org/10.1615/978-1-56700-309-3.78
• “Chapter 6. Piloting and Inertial Navigation.” 2012. In Nature’s Compass. Princeton University Press. https://doi.org/10.1515/9781400841660.155
• “Chapter 7: Parameter Identifiability and Influence.” 2024. In Uncertainty Quantification: Theory, Implementation, and Applications, Second Edition. Society for Industrial and Applied Mathematics. https://doi.org/10.1137/1.9781611977844.ch7
• Chasan, Chasan, and Ahmet Bingul. 2026. “Visible and Short-Wave Infrared Star Tracker Objective Designs for UAV Navigation.” Journal of the Optical Society of America A 43 (9): 1472. https://doi.org/10.1364/josaa.600241
• Chase, R. 1979. “A Comparative Assessment of Reusable Launch-Vehicle Candidates.” In Conference on Advanced Technology for Future Space Systems. AIAA 1979-894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-894
• Chase, Ramon, and Leon McKinney. 2005. “A Least Cost Reusable Operationally Responsive Space Launch Vehicle Demonstrator.” In Space 2005. AIAA 2005-6745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6745
• Chashnikova, Valentina. 2015. “Identifiability and Controllability of a Dynamic System under Restriction on Measuring Errors.” In AIP Conference Proceedings, vol. 1648. AIP Publishing LLC. https://doi.org/10.1063/1.4912663
• Chasoglou, A. C., P. Tsirikoglou, A. I. Kalfas, and R. S. Abhari. 2021. “Uncertainty Quantification for Aerodynamic Pressure Probes, Using Adaptive Quasi-Monte Carlo.” Measurement Science and Technology 33 (3): 035003. https://doi.org/10.1088/1361-6501/ac3f84
• Chatzis, M. N., E. N. Chatzi, and A. W. Smyth. 2014. “Observability and Identifiability Methods for Structural Dynamic Systems.” In Vulnerability, Uncertainty, and Risk. American Society of Civil Engineers. https://doi.org/10.1061/9780784413609.154
• Chaudhari, Bhargav N., and Timothy T. Takahashi. 2022. “Inlet Diffusor Buoyancy – Its Historical Use in Supersonic Transport Design.” In AIAA SCITECH 2022 Forum. AIAA 2022-2566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2566
• Chavent, G. 1987. “Identifiability of Parameters in the Output Least Square Formulation.” In Identifiability of Parametric Models. Elsevier. https://doi.org/10.1016/b978-0-08-034929-9.50010-8
• Chaves Barbosa, Guilherme, and Flávio José Silvestre. 2025. “Output Feedback Fuzzy Gain-Scheduling for MIMO Systems Applied to Flexible Aircraft Control.” Preprint, . https://doi.org/10.20944/preprints202505.1504.v1
• Che, Jun. n.d. “Automatic Landing Control Using H[infinity] Control and Stable Inversion.” PhD diss., Iowa State University. https://doi.org/10.31274/rtd-20201118-91
• Che, Lufeng, Baoyin Hou, Ye Zhu, et al. 2023. “A 3D-Printed Micro-Hemispherical Shell Resonator with Electrostatic Tuning for Coriolis Vibratory Gyroscope.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3309122/v1
• Cheadle, Christopher, and Nicholas DiZinno. 2026. “The Effect of off-Design Conditions on Inlet Buzz.” In Proceeding of 11th Thermal and Fluids Engineering Conference (TFEC). Begellhouse. https://doi.org/10.1615/tfec2026.fna.061757
• Chekanov, K. A. 2025. “Algorithms of Runway Detection in Video Images in Neural Network Based UAV Landing.” Gyroscopy and Navigation 16 (1): 21–33. https://doi.org/10.1134/s2075108725700099
• Chelnokov, Yu. N. 2019a. “Inertial Navigation in Space Using the Regular Quaternion Equations of Astrodynamics.” Mechanics of Solids 54 (2): 157–68. https://doi.org/10.3103/s0025654419030063
• Chen, Shih-Yuan. 1958. “Transient Temperature and Thermal Stresses in Skin of Hypersonic Vehicle with Variable Boundary Conditions.” Journal of Fluids Engineering 80 (7): 1389–94. https://doi.org/10.1115/1.4012730
• Chen, Chung-Jen. 2008. “Interferometric Fiber Optic Gyroscope Dead Band Suppression.” Applied Physics Express 1: 072501. https://doi.org/10.1143/apex.1.072501
• Chen, Kai. 2017. “Strapdown Inertial Navigation Algorithm for Hypersonic Boost-Glide Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2174
• Chen, Chengbin. 2020. “Obtaining World Coordinate Information of UAV in GNSS Denied Environments.” Preprint, . https://doi.org/10.32545/encyclopedia202005.0005.v1
• Chen, Wen-Chiao. 2024. “Validating a Star Tracker Algorithm and Measuring Its Accuracy through Suburban Night Sky Observations.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2024.19937
• Chen, Yanjun, Yuwen Cao, Lanxin Zhu, et al. 2023b. “A Bias-Instability-Enhanced Dual-Polarization Fiber-Optic Gyroscope for Precision Measurement.” In CLEO 2023. Optica Publishing Group. https://doi.org/10.1364/cleo_at.2023.jtu2a.30
• Chen, Tao, Guihong Chen, Yanshuang Zhao, Chaoqing Li, and Zhisheng Zheng. 2023e. “The Influence of Pigtail Bending Radius of Optical Devices on the Performance of Fiber Optic Gyroscope.” In AOPC 2023: Optic Fiber Gyro, edited by Shangran Xie, Qi Wang, Benli Yu. SPIE. https://doi.org/10.1117/12.3007855
• Chen, Yi, Rongyao Cui, Rongbo Ju, and Qingbo Dou. 2018e. “Simulation of Nose Landing Gear Shimmy with Flexible Airframe Considered.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 36 (2): 388–95. https://doi.org/10.1051/jnwpu/20183620388
• Chen, Yongchao, Xinbao Gao, Min Gao, and Dan Fang. 2018c. “An Optimal Missile Autopilot Design Model.” International Journal of Enterprise Information Systems 14 (1): 104–10. https://doi.org/10.4018/ijeis.2018010106
• Chen, Linzhouting, Hongjian Gao, Zhanchao Liu, and Jiancheng Fang. 2026d. “High-Dimensional System Error Model and Real-Time Estimation Scheme for GNSS/INS Integrated System.” Journal of Navigation: 1–18. https://doi.org/10.1017/s0373463326101660
• Chen, Lin, Peitong He, Biqiang Jiang, and Jianlin Zhao. 2024d. “Suppression of Modulation-Induced Polarization Error in Spliceless Open-Loop Fiber Optic Gyroscope [Invited].” Chinese Optics Letters 22 (7): 070601. https://doi.org/10.3788/col202422.070601
• Chen, Xin, Guangyuan Huang, Ankit Sharma, Atif Riaz, and Sergio Jimeno. 2026f. “Multi-Fidelity Gaussian Process for Uncertainty Quantification in Aerodynamic Analysis.” In AIAA SCITECH 2026 Forum. AIAA 2026-0297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0297
• Chen, C., J. C. Hung, and J. S. Miller. 1970. “Sensitivity Analyses for Several Celestial and Satellite Navigation Schemes.” In NATIONAL ELECTRONICS CONFERENCE. https://ntrs.nasa.gov/citations/19710039717
• Chen, Wen-Chiao, and Shau-Shiun Jan. 2019. “A Star Tracker for Cubesats: Implementation and Analysis.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2019.16720
• Chen, Gang, Kui Li, Wei Wang, and Peng Li. 2016b. “A Novel Redundant INS Based on Triple Rotary Inertial Measurement Units.” Measurement Science and Technology 27 (10): 105102. https://doi.org/10.1088/0957-0233/27/10/105102
• Chen, ZhaoFeng, LongHua Ma, and Zebin Feng. 2014b. “Parallel Design for Initial Alignment Algorithm of Strapdown Inertial Navigation System.” In WIT Transactions on Information and Communication Technologies, vol. 1. WIT Press. https://doi.org/10.2495/icie130842
• Chen, Robert K., Lisa A. Martinez, and David P. Wilson. 2025c. Computational Fluid Dynamics Analysis of Supersonic Inlet Design. National Aeronautics and Space Administration. https://doi.org/10.64631/abcd8901
• Chen, Jiaye, Rongjun Mu, Xin Zhang, and Yanpeng Deng. 2018d. “Reusable Launch Vehicle Model Uncertainties Impact Analysis.” In Young Scientists Forum 2017, edited by Songlin Zhuang, Junhao Chu, Jian-Wei Pan. SPIE. https://doi.org/10.1117/12.2317531
• Chen, Xiying, Zhe Pan, Shutong Zhao, Bo Gao, and Zeng Wang. 2025e. “Multidisciplinary Modeling and Analysis of Nose Landing Gear Shimmy.” IET Conference Proceedings 2024 (13): 462–67. https://doi.org/10.1049/icp.2024.2934
• Chen, XiaoLong, ShiQiao Qin, jiaxing Zheng, Shaolei Lu, and Zhisheng Wang. 2022c. “Periodic Change Error Tracking Calibration of Strapdown Inertial Navigation System.” In 2022 International Conference on Optoelectronic Information and Functional Materials (OIFM 2022), edited by Chao Zuo. SPIE. https://doi.org/10.1117/12.2639192
• Chen, Wen-Chiao, and Shau-Shiun Shau-Shiun. 2021. “Low-Cost Star Tracker Development with a Laboratory Simulation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2021.17917
• Chen, Dechao, Chentong Shi, Xiaofeng Pan, Jie Jin, and Shuai Li. 2025h. “VSDRL: A Robust and Accurate Unmanned Aerial Vehicle Autonomous Landing Scheme.” IET Control Theory & Applications 19 (1): e70002. https://doi.org/10.1049/cth2.70002
• Chen, Robert, Jason Speyer, and Dimitrios Lianos. 2010c. “Optimal Intercept Missile Guidance Strategies with Autopilot Lag.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7875
• Chen, Jian, Yuan Tian, Hugh Ht Liu, and Zhang Ren. 2010b. “Autopilot Design for a Side-Jet Missile Based on MRVSS Technique and GA Optimization.” In Earth and Space 2010. American Society of Civil Engineers. https://doi.org/10.1061/41096(366)164
• Chen, Wei, and John Valasek. 1999. “Observer/Kalman Filter Identification for on-Line System Identification of Aircraft.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4173
• Chen, W. H., and P. J. Wang. 1988. “Phase-Conjugate Fiber-Optic Gyroscope with Multimode Fibers.” In SPIE Proceedings, vol. 0838, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.942499
• Chen, Pengxin, Zhiwen Wu, Yuntao Guo, and Tianyu Lu. 2026e. “Mechanisms of Pressure-Wave Feedback and Shock Evolution during Transient Opening of a Supersonic Inlet.” Physics of Fluids 38 (9): 095119. https://doi.org/10.1063/5.0348275
• Chen, Jingjing, Yadong Wu, Zhonglin Wang, and Anjenq Wang. 2015. “Nacelle Aerodynamic Optimization and Inlet Compatibility.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-42346
• Chen, Nan, Fei Xing, and Zheng You. 2013. “A New Approach to Determine the Centroid of Star Spot for Star Tracker Based on MEMS-Gyro.” In Key engineering materials, vol. 562-565. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.562-565.350
• Chen, Xian, Jianhua Yang, Yilan Zhou, and Xiaowu Shu. 2017b. “An Improved Temperature Compensation Circuit for SLD Light Source of Fiber-Optic Gyroscope.” Journal of Physics: Conference Series 916: 012027. https://doi.org/10.1088/1742-6596/916/1/012027
• Chen, Qing, Baoqiang Zhang, Jing Yang, and Guoqiang Su. 2017c. “Model Updating and Uncertainty Propagation in Aerothermoelastic Analysis for C/SiC Panel of Ceramic Matrix Composite.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2359
• Chen, Rui, Qieqie Zhang, and Long Zhao. 2021b. “Real Time Airborne Terrain Aided Inertial Navigation System in Multi-Resolution Terrain.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-6324-6_43
• Chen, L., Y. X. Zhao, M. F. Yang, D. W. Zhang, X. W. Shu, and C. Liu. 2019a. “Cross-Coupling Drift between Magnetic Field and Temperature in Depolarized Interferometric Fiber Optic Gyroscope.” Optics Express 27 (5): 6003. https://doi.org/10.1364/oe.27.006003
• Chen, Yun Fang, Ruo Fei Zhong, and Bo Qiang Shi. 2011. “Integration Matching Algorithm on Gravity Aided Underwater Navigation.” Applied Mechanics and Materials 137: 128–33. https://doi.org/10.4028/www.scientific.net/amm.137.128
• Chen, Chu Xin, and De Yun Zhou. 2014. “Study on a New Algorithm for Tracking Ballistic Missile in Free Flight Phase.” Advanced materials research 981: 743–53. https://doi.org/10.4028/www.scientific.net/amr.981.743
• Chen, Manlin, Zhijie Zhou, Xiaoxia Han, Zhichao Feng, and You Cao. 2023f. “An Interpretable Method for Inertial Platform Fault Diagnosis Based on Combination Belief Rule Base.” Preprint, . https://doi.org/10.2139/ssrn.4374262
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020b. “Linear Pseudospectral Guidance Method for Eliminating General Nominal Effort Miss Distance.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_15
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020c. “Linear Pseudospectral Reentry Guidance with Adaptive Flight Phase Segmentation and Eliminating General Nominal Effort Miss Distance.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_16
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020d. “Mathematical Modeling for Hypersonic Glide Problem.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_3
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020e. “Singular Perturbation Guidance of Hypersonic Glide Reentry.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_11
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020f. “Trajectory Damping Control Technique for Hypersonic Glide Reentry.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_9
• Chen, Yongjie, and Weibao Zou. 2026. “On the Way to Intelligence: Geomagnetic Navigation for Aircrafts in GNSS-Denied Environments–a Review.” Measurement Science and Technology 37 (25): 252001. https://doi.org/10.1088/1361-6501/ae7997
• Cheng, R. K. 1966. “Surveyor Terminal Guidance.” In Peaceful Uses of Automation in Outer Space. Springer US. https://doi.org/10.1007/978-1-4899-6411-3_38
• Cheng, R. K., and I. Pfeffer. 1962. “Terminal Guidance System for Soft Lunar Landing.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395586-9.50014-3
• Cheng, Benny N., and Lap S. Tam. 2014. Bayesian Missile System Reliability from Point Estimates. Defense Technical Information Center. https://doi.org/10.21236/ada611099
• Cheng, Jian, Bing Yu Wang, and Daidai Chen. 2013b. “Error Analyzing Method for Rotation Inertial Navigation System Based on Fourier Transform.” Applied Mechanics and Materials 336-338: 982–87. https://doi.org/10.4028/www.scientific.net/amm.336-338.982
• Cheng, Yunpeng, Xiaodong Yan, and Feng Cheng. 2019. “Trajectory Estimation of Hypersonic Glide Vehicle Based on Analysis of Aerodynamic Performance.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37 (6): 1102–10. https://doi.org/10.1051/jnwpu/20193761102
• Cheng, T., D. Q. Zou, and Z. S. He. 2013a. “Adaptive Waveform and Sampling Interval Tracking Based on Estimation Accuracy for Doppler Radar.” In IET International Radar Conference 2013. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2013.0265
• Chengbin Lian, Zhang Ren, and Xinyue Shao. 2012. “Reference Command Tracking and Simulation Research of Hypersonic Cruise Vehicle.” In International Conference on Automatic Control and Artificial Intelligence (ACAI 2012). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2012.1300
• Chenoweth, C. C., and D. R. Ryder. 1976. “Redundancy of Hydraulic Flight Control Actuators.” In NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft. https://ntrs.nasa.gov/citations/19760024089
• Cheol Jeon, Hyun, and Chan Gook Park. 2018. “Comparative Study of Sequential Processing Terrain Referenced Navigation.” Proceedings of International Conference on Artificial Life and Robotics 23: 767–70. https://doi.org/10.5954/icarob.2018.os22-1
• Cheremisinoff, Nicholas P. 2020. “Experimental Design and Parameter Estimation.” In Practical Statistics for Engineers and Scientists. CRC Press. https://doi.org/10.1201/9781003070238-7
• Cheriet, Mohammed El-Amine. 2024. Optimizing Star Tracker Placement on Agile Satellites: Mitigating Glare for Enhanced Performance. https://doi.org/10.52202/078362-0128
• Chernenko, Serhii, and Vitalyi Burnashev. 2022. “Synthesis and Analysis of the Laws of Automatic Landing Control of an Unmanned Aircraft on a Landing Gear.” Mechanics of Gyroscopic Systems, no. 42: 20–32. https://doi.org/10.20535/0203-3771422021268461
• Chernyak, Mykola, and Evgen Burym. 2022. “Experimental Strapdown Inertial Navigation System for the Autonomous Guidance System of a Short-Range Uav.” Mechanics of Gyroscopic Systems, no. 43: 34–45. https://doi.org/10.20535/0203-3771432022275280
• Chernyak, Mykola, and Vadym Kolesnyk. 2023. “Improving Strapdown Inertial Navigation System Performance by Self-Compensation of Inertial Sensor Errors.” Transactions on Aerospace Research 2023 (4): 41–51. https://doi.org/10.2478/tar-2023-0022
• Chernyak, Mykola, and Vitaliy Romanchenko. 2025. “Reducing the Impact of Rapid Aircraft Rotation on the Measurement Range and Accuracy of Inertial Navigation System Sensors.” Mechanics of Gyroscopic Systems, no. 49: 97–108. https://doi.org/10.20535/0203-3771492025334112
• Chernyak, Mukola, and Heorhii Tarash. 2026. “Comparative Assessment of Azimuth Determination Accuracy Using the Gyro-Compassing Method with Modern Inertial Measuring Units.” Mechanics of Gyroscopic Systems, no. 51: 99–111. https://doi.org/10.20535/0203-3771512026371069
• Chhajer, Harsh, and Rahul Roy. 2023. “Rationalised Experiment Design for Parameter Estimation with Sensitivity Clustering.” Preprint, bioRxiv. https://doi.org/10.1101/2023.10.11.561860
• Chiang, Richard Y. 2013. “Star Tracker Rate Estimation with Kalman Filter Enhancement.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5024. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5024
• Chichka, David, Uday Shankar, Eugene Cliff, and Henry Kelley. 1987. “Cruise-Dash-Climb Analysis of an Airbreathing Missile.” In Guidance, Navigation and Control Conference. AIAA 1987-2512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2512
• Chicone, Carmen, and Jürgen Gerlach. 1987. “Identifiability of Distributed Parameters.” In Inverse and Ill-Posed Problems. Elsevier. https://doi.org/10.1016/b978-0-12-239040-1.50038-7
• Chief Engineer Star Sensors, Jena, Germany, Uwe Schmidt, Richard Würl, et al. 2023. High-Accuracy Star Tracker ASTRO XP. https://doi.org/10.5270/esa-gnc-icatt-2023-056
• Chiesa, Sergio, Michele Grassi, Gennaro Russo, and Paolo Teofilatto. 2005. “A Small-Scale Low-Cost Technology Demonstrator of a Reusable Launch Vehicle.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3346
• Chikovani, V. V. 2012. “Influence of Shock on the Vibration Amplitude Stabilization System of Coriolis Vibratory Gyroscope Resonator.” Electronics and Control Systems 4 (34). https://doi.org/10.18372/1990-5548.34.5717
• Chikovani, V. V. 2013. “Secondary Wave Control System of the Coriolis Vibratory Gyroscope Resonator.” Electronics and Control Systems 1 (35). https://doi.org/10.18372/1990-5548.35.5805
• Chikovani, Valerii. 2022. “The Sensitive Element of the Vibrating Gyroscope Is Based on a Quartz Hemispherical Resonator without a Leg.” Mechanics of Gyroscopic Systems, no. 43: 79–89. https://doi.org/10.20535/0203-3771432022275286
• Chikovani, Valeri, and Serhii Golovach. 2021. “Vibratory Gyroscope Scale Factor and Bias on-Run Self-Calibration.” Electronics and Control Systems 3 (69): 16–27. https://doi.org/10.18372/1990-5548.69.16423
• Chikovani, V. V., and H. V. Tsiruk. 2014. “Shock Resistance of Differential Type Ring-like Resonator Vibratory Gyroscope.” Electronics and Control Systems 4 (42). https://doi.org/10.18372/1990-5548.42.8816
• Child, R. D., and W. P. Henderson. 1978. “Canard Configured Aircraft with 2-D Nozzle.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780063995
• Chilton, E. A., and G. V. Zito. 1969. Design and Development of a Multipurpose, Boresighted Star Tracker. NASA-CR-976. NASA. https://ntrs.nasa.gov/citations/19690012140
• Chima, Rodrick. 2011a. “Computational Analysis of a Low Boom Supersonic Inlet (Invited).” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3801
• Chima, ROdrick V. 2011b. “Computational Analysis of the Large Scale Low-Boom Supersonic Inlet.” In 2011 Fundamental Aeronautics Program Technical Conference. https://ntrs.nasa.gov/citations/20110011335
• Chima, Rodrick V., Stefanie M. Hirt, and Robert Reger. 2011. Axisymmetric Calculations of a Low-Boom Inlet in a Supersonic Wind Tunnel. NASA/TM-2011-217224. NASA. https://ntrs.nasa.gov/citations/20110023762
• Chin, H. 1985. “Distributed Kalman Filter in an Integrated SAHRS/GPS Navigation System.” In Guidance, Navigation and Control Conference. AIAA 1985-1878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1878
• Chitrakaran, Vilas K., Darren M. Dawson, Jian Chen, and Mathew Feemster. 2005. Vision Assisted Landing of an Unmanned Aerial Vehicle. Defense Technical Information Center. https://doi.org/10.21236/ada465706
• Chmielowski, M., and D. Wynne. 1992. A Low-Cost, CCD Solid State Star Tracker. NASA-CR-192722. NASA. https://ntrs.nasa.gov/citations/19940027911
• Cho, Sung-Jin. 2023. “A Study on the Estimating Launch Location Based on Detection Information of Ballistic Missile Flight.” Journal of the KNST 6 (3): 331–35. https://doi.org/10.31818/jknst.2023.09.6.3.331
• Choe, Yohan, and Chongam Kim. 2016. “Numerical Investigation of Bleed Effects on Supersonic Inlet under Various Bleed and Inlet Conditions.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-3564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3564
• Choi, Seung Hyuk. 2016. “Flight Environment Simulation Test for Reliability Improvement of Precise Guided Missile.” Journal of the Korean Society for Precision Engineering 33 (10): 781–87. https://doi.org/10.7736/kspe.2016.33.10.781
• Choi, JeongYeol, and Vigor Yang. 2014. “High Resolution Numerical Study on the Supersonic Turbulent Flame Structures and Dynamics in Dual Combustion Ramjet.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3744. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3744
• Choi, Minseog, 좌성훈, Jong-Seok Kim, Hee-Moon Jeong, Inseob Song, and Yong-Chul Cho. 2004. “Reliability Assessment of MEMS Gyroscope Sensor.” Transactions of the Korean Society of Mechanical Engineers A 28 (9): 1297–1305. https://doi.org/10.3795/ksme-a.2004.28.9.1297
• Choo, Kyoseung, Hokyun Mun, Seunghoon Nam, Jihyoung Cha, and Sangho Ko. 2018. “A Survey on Recovery Technology for Reusable Space Launch Vehicle.” Journal of the Korean Society of Propulsion Engineers 22 (2): 138. https://doi.org/10.6108/kspe.2018.22.2.138
• Chopde, Rahul, Prasad Parkhi, and Ganapati Joshi. 2025. “Effect of Micro-Vortex Generator Geometry on Separation Characteristics of Supersonic Inlet.” In Ballistics 2025. Destech Publications, Inc. https://doi.org/10.12783/ballistics25/37185
• Chou, David C., and Theodore F. Smith. 1974. Aerodynamic Heating of Supersonic Blunt Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada001135
• Chou, D., and T. Smith. 1978. “A Simple Similarity Solution of Supersonic Blunt Body Boundary Layerflows with Heat Transfer.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1359. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1359
• Christensen, E. Lintz, and Gregers Mogensen. 1979. “Experimental Investigation of Line-of-Sight Propagation at 13.5–15.0 GHz.” Radio and Electronic Engineer 49 (3): 127. https://doi.org/10.1049/ree.1979.0025
• Christian, William R., Mark J. Rosker, and Ian McMichael. 1991. “Picosecond Pulsed Diode Ring Laser Gyroscope.” In Optical Society of America Annual Meeting. Optica Publishing Group. https://doi.org/10.1364/oam.1991.tup5
• Christian, William R., Mark J. Rosker, and Ian C. McMichael. 1992. “Pulsed Diode Ring Laser Gyroscope.” In SPIE Proceedings, vol. 1694, edited by Sharon S. Welch. SPIE. https://doi.org/10.1117/12.138138
• Chu, Peter Yaohwa, and Arthur E. Bryson Jr. 1987. Control of Aircraft Landing Approach in Wind Shear. AIAA PAPER 87-0632. Ford Aerospace and Communication Corp. https://ntrs.nasa.gov/citations/19870037720
• Chu, Trong Su, and Phi Minh Nguyen. 2026. “Observability Analysis of Navigation Systems: Lie Derivative Approach.” Open Engineering 16 (1): 20250185. https://doi.org/10.1515/eng-2025-0185
• Chub, V. F. 2014a. “Exact Geodesic Precession Related Solutions of the Inertial Navigation Equations.” Mechanics of Solids 49 (3): 237–52. https://doi.org/10.3103/s0025654414030017
• Chub, V. F. 2014b. “Exact Thomas Precession Related Solutions of the Inertial Navigation Equations.” Mechanics of Solids 49 (2): 113–26. https://doi.org/10.3103/s0025654414020010
• Chuban, Vitalii Dmitrievich. 2017. “Shimmy Analysis of Light Airplane Main Landing Gear.” TsAGI Science Journal 48 (7): 665–72. https://doi.org/10.1615/tsagiscij.2018026284
• Chuban, Vitalii Dmitrievich. 2019. “Shimmy Analysis of Aircraft Multi-Wheel Landing Gear.” TsAGI Science Journal 50 (2): 195–209. https://doi.org/10.1615/tsagiscij.2019030563
• Chudoba, B., E. Haney, L. Gonzalez, A. Omoragbon, and A. Oza. 2015. “Strategic Forecasting in Uncertain Environments: Hypersonic Cruise Vehicle Research and Development Case Study.” Aeronautical Journal 119 (1211): 45–65. https://doi.org/10.1017/s0001924000010241
• Chumankin, E. A. 2014. “Angular Rate Sensor Based on Hemispherical Resonator Gyro: Development and Test Results.” Gyroscopy and Navigation 5 (4): 219–23. https://doi.org/10.1134/s2075108714040129
• Chun, K., and D. Swanson. 1964. “Dynamic Simulation of Supersonic Inlet and Engine.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-598
• Chung, Joongkee. 1994. “Numerical Simulation of a Mixed-Compression Supersonic Inlet Flow.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-583
• Chung, P. M., and G. Goodwin. 1962. Effects of Nonequilibrium Flows on Aerodynamic Heating during Entry into the Earth’s Atmosphere from Parabolic Orbits. NASA. https://ntrs.nasa.gov/citations/19630026626
• Chunmei, Liu, Miao Lingjuan, and Dai Tian. 2017. “A Fuzzy Pattern Based ICCP Matching Algorithm in Gravity-Aided Navigation.” In Proceedings of the 2017 VI International Conference on Network, Communication and Computing. ACM. https://doi.org/10.1145/3171592.3171626
• Church, James D., and Nancy L. Taylor. 1959. An Investigation of a 0.05-Scale Model of the XSM-64A Navaho Missile and Booster: Force Study at Mach Numbers from 1.77 to 3.51: Part 1. NASA-MEMO-5-30-59L. NASA. https://ntrs.nasa.gov/citations/19980228032
• Chyba, Thomas H. 1991. “Deterministic and Noise-Induced Phase Jumps in the Ring Laser Gyroscope.” In SPIE Proceedings, vol. 1376, edited by Rajarshi Roy. SPIE. https://doi.org/10.1117/12.24993
• Cigada, Alfredo, Elisabetta Leo, and Marcello Vanali. 2005. “Optical and Electrical Methods to Measure the Dynamic Behavior of a MEMS Gyroscope Sensor.” In Microelectromechanical Systems. ASMEDC. https://doi.org/10.1115/imece2005-81022
• Circular Probable Error. 2014. Wiley. https://doi.org/10.1002/9781118445112.stat00938
• Clark, S. 1974a. “High Friction Interactive Aircraft Tire-Runway Systems.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-967. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-967
• Clark, L. 1974b. “Statistical Averages of Subsonic Inlet Distortion.” In 10th Propulsion Conference. AIAA 1974-1197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1197
• Clark, Larry. 1995. “Dynamic Response Characteristics of a Mixed Compression Supersonic Inlet as Part of a Larger System.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-36. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-36
• Clark, M. E. 1999. “High Range Resolution Techniques for Ballistic Missile Targets.” In IEE Colloquium on High Resolution Radar and Sonar, vol. 1999. IEE. https://doi.org/10.1049/ic:19990268
• Clayton, J. Louie. 2001. “Reusable Solid Rocket Motor Nozzle Joint-4 Thermal Analysis.” In The Tenth Thermal and Fluids Analysis Workshop. https://ntrs.nasa.gov/citations/20020050391
• Cleary, Mark C. 1991. “The NAVAHO Program.” In The 6555th: Missile and Space Launches Through 1970. https://spp.fas.org/military/program/6555th/6555c2-4.htm
• Clements, T. R. 1972. Development of a Short Length Combustor for a Supersonic Cruise Turbofan Engine Using a 90 Deg Sector of a Full Annulus. NASA-CR-120908. NASA. https://ntrs.nasa.gov/citations/19720015142
• Clemow, Brigadier J. 1957. “Guided Weapon Engineering: An Introduction to Guided Missile Design and Development.” Aircraft Engineering and Aerospace Technology 29 (9): 258–67. https://doi.org/10.1108/eb032867
• “Climbing Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0259.0292
• Cline, T. 1982. “A Time-Invariant Error Model for a Space-Stable Inertial Navigation System.” In Guidance and Control Conference. AIAA 1982-1545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1545
• Coakley, Janet M. n.d. “Dynamic Inversion and Backstepping Controller Robustness Analysis for a Reusable Launch Vehicle.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2011.26
• Cochran, R. P., and R. W. Cubbison. 1966. Supersonic Aerodynamic Heating Tests on a Lightweight External Insulation System for Liquid-Hydrogen Tanks of Boost Vehicles. NASA-TN-D-3300. NASA. https://ntrs.nasa.gov/citations/19660009748
• Cockayne, W., and W. Rusnak. 1971. Study of Automatic Flare and Decrab Guidance and Control System for the Space Shuttle. NASA-CR-114436. NASA. https://ntrs.nasa.gov/citations/19720017949
• Cockburn, J. 1965. “Automatic Landing Aids for Aircraft.” Students Quarterly Journal 36 (141): 47. https://doi.org/10.1049/sqj.1965.0062
• Cockrell, D. J., and K. F. Doherr. 1981. “Preliminary Consideration of Parameter Identification Analysis from Parachute Aerodynamic Flight Test Data.” In 7th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1981-1940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1940
• Coder, James G., and Sven Schmitz. 2019. “Thermodynamic Decomposition of Compressible Wave Drag in the Euler Equations.” In AIAA Aviation 2019 Forum. AIAA 2019-2958. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2958
• Coe, P. L., Jr. 1976. Propulsive-Lift Concepts for Improved Low-Speed Performance of Supersonic Cruise Arrow-Wing Configurations. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19760053942
• Coe, P. L., Jr., and A. B. Graham. 1976. “Results of Recent NASA Research on Low-Speed Aerodynamic Characteristics of Supersonic Cruise Aircraft.” In Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011059
• Coe, P. L., Jr., H. C. McLemore, and J. P. Shivers. 1976. Effects of Upper-Surface Blowing and Thrust Vectoring on Low Speed Aerodynamic Characteristics of a Large-Scale Supersonic Transport Model. NASA-TN-D-8296. NASA. https://ntrs.nasa.gov/citations/19770005122
• Coe, P. L., Jr., P. M. Smith, and L. P. Parlett. 1977. Low-Speed Wind Tunnel Investigation of an Advanced Supersonic Cruise Arrow-Wing Configuration. NASA-TM-74043. NASA. https://ntrs.nasa.gov/citations/19770022152
• Coelho Martins, Marcelo. n.d. “Desenvolvimento De Um Aferidor De Imu (Inertial Measurement Unit).” PhD diss., PONTIFÍCIA UNIVERSIDADE CATÓLICA DO RIO DE JANEIRO. https://doi.org/10.17771/pucrio.acad.33104
• Coetsee, Josef, Armando Montalvo, and Alison Brown. 1995. “A TIDGET/inertial Missile Sensor Fusion System.” In Guidance, Navigation, and Control Conference. AIAA 1995-3236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3236
• Coffee, John R., and Prasad Maganty. 1996. “An Integrated DGPS/INS Navigation System for a Ballistic Missile: Design and Flight Test Results.” Navigation 43 (3): 273–93. https://doi.org/10.1002/j.2161-4296.1996.tb02577.x
• Cohen, Abraham, Benveniste Natan, Abraham Cohen, and Benveniste Natan. 1997. “Experimental Investigation of a Supersonic Combustion Solid Fuel Ramjet.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3237
• Coirier, William J., James Stutts, and Christopher C. Rosema. 2014. “Development of a Transonic Fin Aerodynamic Database for Incorporation into Missile Datcom.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-2987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2987
• Cojuhari, Irina. 2024. “A PID Tuning Approach for Inertial Systems Performance Optimization.” Applied Mathematics 15 (01): 96–107. https://doi.org/10.4236/am.2024.151008
• Cole, Diana J. 2020a. “Bayesian Identifiability.” In Parameter Redundancy and Identifiability. Chapman and Hall/CRC. https://doi.org/10.1201/9781315120003-6
• Cole, Diana J. 2020b. “Identifiability in Continuous State-Space Models.” In Parameter Redundancy and Identifiability. Chapman and Hall/CRC. https://doi.org/10.1201/9781315120003-7
• Cole, Diana J. 2020c. “Identifiability in Discrete State-Space Models.” In Parameter Redundancy and Identifiability. Chapman and Hall/CRC. https://doi.org/10.1201/9781315120003-8
• Cole, S. R., and E. W. Glossbrenner. 1974. Long-Duration Life Tests of Slip Ring Capsule Assemblies for Inertial Guidance Platforms. NASA-CR-138948. NASA. https://ntrs.nasa.gov/citations/19740021004
• Cole, Henry, A., Jr., and Marvin Abramovitz. 1952. Theoretical Investigation of the Stability at Negative Static Margins of a Supersonic Missile with an Autopilot Sensitive to Pitch Angle and Pitching Velocity. NACA-RM-A52A14. NASA. https://ntrs.nasa.gov/citations/19930087033
• Coleman, J. L., J. L. Lundry, and W. D. Middleton. 1978. Design and Analysis of Supersonic Aircraft. LAR-12237. Boeing Co. https://ntrs.nasa.gov/citations/19770000422
• Colin, Kévin. n.d. “Data Informativity for the Prediction Error Identification of MIMO Systems: Identification of a MEMS Gyroscope.” PhD diss., Lyon. https://doi.org/10.70675/6630d4b7z100fz4c59z8fb8za09d42b31ea6
• Collins, J. J. 1968. A High-Voltage Problem Encountered in the Design of the Star Tracker Used on the Orbiting Astronomical Observatory. Kollsman Instrument Corp. https://ntrs.nasa.gov/citations/19680017438
• Collins, T. 1970. “Inlet Data for Engine Analysis.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-1214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1214
• Collins, Trevor, Kevin Kochersberger, and Virginia Tech. 2025. “Constrained Layer Damping Test Results for Aircraft Landing Gear.” In Structural Dynamics, Volume 3. River Publishers. https://doi.org/10.1007/978-1-4419-9834-7-28
• Collinson, R. P. G. 1973. “Strapped down Inertial Navigation Systems.” Journal of Navigation 26 (3): 341–51. https://doi.org/10.1017/s0373463300029957
• Collyer, Stanley C., Gilbert L. Ricard, Michael Anderson, Daniel P. Westra, and Ricky A. Perry. 1980. Field of View Requirements for Carrier Landing Training. Defense Technical Information Center. https://doi.org/10.21236/ada087012
• Colombo, G. 1979. System Noise Analysis of the Dumbbell Tethered Satellite for Gravity-Gradient Measurements. NASA-CR-162333. NASA. https://ntrs.nasa.gov/citations/19790025062
• Colombo, G., E. M. Gaposchkin, M. D. Grossi, and G. C. Weiffenbach. 1976. “Gravity-Gradient Measurements down to Approximately 100-Km Height by Means of Long-Tethered Satellites.” In International Astronautical Federation. https://ntrs.nasa.gov/citations/19760063076
• Colwell, A. R. 1966. “Flight Control for Automatic Landing: A Philosophy of the Duplicate Monitored System Used in the VC10 and Its Extension to Further Applications.” Aircraft Engineering and Aerospace Technology 38 (9): 49–54. https://doi.org/10.1108/eb034185
• “Component Analysis and Synthesis for Fully Separated Flows with Special Consideration of Base Drag Reduction by Combustion.” 1976. In Aerodynamics of Base Combustion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865145.0211.0254
• “Conclusion: The Future of Ballistic Missile Defense.” 2020. In Regional Missile Defense from a Global Perspective. Stanford University Press. https://doi.org/10.1515/9780804796569-018
• Condomines, Jean-Philippe. 2018. “Inertial Navigation Models.” In Nonlinear Kalman Filtering for Multi-Sensor Navigation of Unmanned Aerial Vehicles. Elsevier. https://doi.org/10.1016/b978-1-78548-285-4.50003-5
• Cone, Bruce E. 1976. The United States Air Force Eastern Test Range. Range Instrumentation Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada029237
• Conner, W. S., and W. S. Thompson. 1963. An Appraisal for Use in Reliability Analysis of the Test and Data Collection Procedures in the Manufacture of an Inertial Guidance System. NASA-CR-82979. NASA. https://ntrs.nasa.gov/citations/19670010653
• Connolly, Joseph W., and George Kopasakis. 2010. “Loop Shaping Control Design for a Supersonic Propulsion System Model Using Quantitative Feedback Theory (QFT) Specifications and Bounds.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100040421
• Connors, J. F. 1962. Telescoping-Spike Supersonic Inlet for Aircraft Engines Patent. Patent Number: US-PATENT-3,067,573. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19700030583
• Connors, James F., and John L. Allen. 1958. Survey of Supersonic Inlets for High Mach Number Applications. NACA-RM-E58A20. Lewis Research Center. https://ntrs.nasa.gov/citations/19710065526
• Conroy, Bartley F. 1964. Analysis of the Application of Imageforming Photosensors to Wide Field- of-View Daylight Star Trackers. Defense Technical Information Center. https://doi.org/10.21236/ad0604589
• Contreras, Alberto Mañero, and Chingiz Hajiyev. 2017. “Integration of Baro-Inertial-GPS Altimeter via Complementary Kalman Filter.” In Advances in Sustainable Aviation. Springer International Publishing. https://doi.org/10.1007/978-3-319-67134-5_18
• Cook, W. 1985. “In-Service Landing Gear Actuation System Problems: The Solution.” In Aircraft Design Systems and Operations Meeting. AIAA 1985-4019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4019
• Cook, Stephen. 1995. “The Reusable Launch Vehicle Technology Program.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6153
• Cook, Stephen. 1996. “X-33 Reusable Launch Vehicle Structural Technologies.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4563
• Cook, Brant. 2013. “Low Density Supersonic Decelerator Flight Dynamics Test Vehicle Design.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1353
• Cook, Francis J., and Joseph N. Craig. 1980. “Adaptive Learning Networks and Image Processing for Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959158
• Cook, Stephen, Terence Ghee, Hugo Gonzalez, Alexander Kokolios, Henrik Pettersson, and D. Owens. 2004. “Correlation of the Continuous Beta Sweep Test and Analysis Technique to Transonic Free-to-Roll and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5052
• Cooper, J. R. 1965. A Statistical Analysis of Gyro Drift Test Data, Volume I. NASA-CR-75226. NASA. https://ntrs.nasa.gov/citations/19660017591
• Cooper, R. J. 1970. “Fluid Effects in Floated Inertial Instruments.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19710031765
• Corban, J., Eric Johnson, and Anthony Calise. 2001. “Reusable Launch Vehicle Adaptive Guidance and Control Using Neural Networks.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4381
• Cordova, Amado, Ralph A. Patterson, Eric L. Goldner, and David M. Rozelle. 1994. “Interferometric Fiber Optic Gyroscope with Inertial Navigation Performance over Extended Dynamic Environments.” In SPIE Proceedings, vol. 2070, edited by Ramon P. DePaula. SPIE. https://doi.org/10.1117/12.169940
• Corson, R. W. 1979. Star Tracker Error Analysis: Roll-to-Pitch Nonorthogonality. NASA-TM-80835. NASA. https://ntrs.nasa.gov/citations/19800004879
• Corson, R. W. 1980. Onorbit IMU Alignment Error Budget. NASA-TM-80794. NASA. https://ntrs.nasa.gov/citations/19800013893
• Cortancioglu, Arda, Görkem Essiz, and Haydar T. Avcioglu. 2025. “Range Estimation Using Detector Image Size Measurements on IR Seeking Cruise Missile Systems.” In AIAA SCITECH 2025 Forum. AIAA 2025-2434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2434
• Cortright, Edgar M., Jr. 1951. Preliminary Investigation of a Translating Cowl Technique for Improving Take-off Performance of a Sharp-Lip Supersonic Diffuser. NACA-RM-E51I24. NASA. https://ntrs.nasa.gov/citations/19930086879
• Costa Canas, António, and Teresa Sousa. 2026. “Gauss’ Method of Celestial Navigation.” Journal of Navigation 79 (3–4): 131–41. https://doi.org/10.1017/s037346332610157x
• Cotter, C. H. 1963. “The Sextant and Precision Celestial Navigation.” Journal of Navigation 16 (2): 246–48. https://doi.org/10.1017/s0373463300019688
• Cottrill, Stanley D. 1992. Tracking Radar Advanced Signal Processing and Computing for Kwajalein Atoll (KA) Application. Defense Technical Information Center. https://doi.org/10.21236/ada259066
• Couch, L. M. 1975. Drag and Stability Characteristics of a Variety of Reefed and Unreefed Parachute Configurations at Mach 1.80 with an Empirical Correlation for Supersonic Mach Numbers. NASA-TR-R-429. NASA. https://ntrs.nasa.gov/citations/19750007612
• Coulibaly, Mamadou, Boris Chevrier, and Sylvain Philippon. 2026. “Semi-Analytical Modeling of Single Blade/casing Contact within Turbojet Engine.” Preprint, . https://doi.org/10.2139/ssrn.7541517
• Courdesses, M. 1983. “Comments on “Identifiability of Spatially Varying and Constant Parameters in Distributed Systems of Parabolic Type”.” SIAM Journal on Control and Optimization 21 (3): 410–12. https://doi.org/10.1137/0321023
• Courdesses, M., and M. Amouroux. 1983. “Identifiability and Identification in Distributed Systems.” In Control of Distributed Parameter Systems. Elsevier. https://doi.org/10.1016/b978-0-08-029361-5.50085-9
• Covell, P. F. 1985. Supersonic Aerodynamic Characteristics of Canard, Tailless, and Aft-Tail Configurations for 2 Wing Planforms. NASA-TP-2434. NASA. https://ntrs.nasa.gov/citations/19850019510
• Covell, Peter, Gloria Hernandez, Jeffrey Flamm, and Ollie Rose. 1990. “Supersonic Aerodynamic Characteristics of a Mach 3 High-Speed Civil Transport Configuration.” In Aircraft Design, Systems and Operations Conference. AIAA 1990-3210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3210
• Covell, Peter, Richard Wood, and David Miller. 1987. “Investigation of the Vortex Flap Concept on a 75-Deg Sweep Delta Wing at Supersonic Speeds.” In 5th Applied Aerodynamics Conference. AIAA 1987-2475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2475
• Cowling, Adam. 2011. “Orbiter Trajectory Analysis for a Two-Stage Reusable Launch Vehicle.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2370
• Cox, D. B. 1978. “Integration of GPS with Inertial Navigation Systems.” Navigation 25 (2): 236–45. https://doi.org/10.1002/j.2161-4296.1978.tb01335.x
• Cox, Jeremy, and Kc Wong. 2019. “Predictive Feedback Augmentation for Manual Control of an Unmanned Aerial Vehicle with Latency.” International Journal of Micro Air Vehicles 11: 1756829319869645. https://doi.org/10.1177/1756829319869645
• Craig, R. J., and J. Russell. 1978. Failure Modes and Redundancy Analysis for the Multifunction Inertial Reference Assembly (MIRA). Defense Technical Information Center. https://doi.org/10.21236/ada061449
• Craig, Joseph N., Michael F. Whalen, and Francis J. Cook. 1980. “Target Recognition for Missile Guidance Using Adaptive Learning Networks.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959160
• Crain, Timothy, Tye Brady, and Robert H. Bishop. 2010. Shifting the Inertial Navigation Paradigm with MEMS Technology. JSC-CN-18818. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/20090033139
• Cramer, E., and T. Lee. 1992. “Test Flight of LQR Missile Guidance.” In Astrodynamics Conference. AIAA 1992-4532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4532
• Crane, Harold L., and James J. Adams. 1950. Wing-Flow Measurements of Longitudinal Stability and Control Characteristics of a Canard Airplane Configuration with a 45 Degree Sweptback Wing and a Triangular All-Movable Control Surface. NACA-RM-L50A31. NASA. https://ntrs.nasa.gov/citations/19930086327
• Crane, H. L., and J. P. Reeder. 1945. Flight Measurements of Lateral and Directional Stability and Control Characteristics of the Grumman F8F-1 Airplane. NACA-RM-SL7L31. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028615
• Crassidis, John. 2005. “Sigma-Point Kalman Filtering for Integrated GPS and Inertial Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6052
• Crassidis, John, and D. Mook. 1991. “An Automatic Carrier Landing System Utilizing Aircraft Sensors.” In Navigation and Control Conference. AIAA 1991-2666. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2666
• Crassidis, John, and D. Mook. 1992. “Robust Control Design of an Automatic Carrier Landing System.” In Astrodynamics Conference. AIAA 1992-4619. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4619
• Crawford, B. S. 1970. Analysis of Strapdown Sensor Testing. NASA-CR-124126. NASA. https://ntrs.nasa.gov/citations/19730010914
• Crawford, D. J. 1975. Automatic Guidance and Control of a Transport Aircraft during a Helical Landing Approach. NASA-TN-D-7980. NASA. https://ntrs.nasa.gov/citations/19750023043
• Crawley, J., and L. Maunder. 1966. “Drift of a vibrating gyroscope supported in gimbals.” In Applied Mechanics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-29364-5_60
• Creagh, Michael, Peter Beasley, Igor Dimitrijevic, Melrose Brown, and Sandy Tirtey. 2012. “A Kalman-Filter Based Inertial Navigation System Processor for the SCRAMSPACE 1 Hypersonic Flight Experiment.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5894
• Creamer, Glenn. 1996. “Spacecraft Attitude Determination Using Gyros and Wide Field-of-View Star Cameras.” In Guidance, Navigation, and Control Conference. AIAA 1996-3752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3752
• Creamer, Paul M., Radha R. Gupta, and Peter B. Morris. 1984. “OMEGA Navigation System Position-Fix Accuracy Assessment.” Navigation 31 (4): 257–74. https://doi.org/10.1002/j.2161-4296.1984.tb00878.x
• Creed, R., and J. B. Hughes. 1971. “AN/ASN-86 Inertial Navigation Set.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f27-019
• Creel, T. R., Jr., and R. Miserentino. 1971. Aerodynamic Heating at Mach 8 of Attached Inflatable Decelerator Configurations. NASA-TM-X-2355. NASA. https://ntrs.nasa.gov/citations/19710029282
• Creese, Aaron, Rohit K. S. S. Vuppala, Scout D. Hernandez, and Kurt P. Rouser. 2023. “Engine Cycle Design and Integration of Component Interfaces of a Micro Turbojet Engine for Additive Manufacturing.” In AIAA SCITECH 2023 Forum. AIAA 2023-1465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1465
• Criss, Thomas, Melvin White, and Dewey Adams. 2010. “APLNav Terrain Relative Navigation Airplane Field Test.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8027. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8027
• Crocoll, Philipp, Lorenz Görcke, Gert F. Trommer, and Florian Holzapfel. 2013. “Unified Model Technique for Inertial Navigation Aided by Vehicle Dynamics Model: Unified Model Technique for Model-Aided Navigation.” Navigation 60 (3): 179–93. https://doi.org/10.1002/navi.39
• Crogan, Leonard E. 1961. Drag and Stability Data for Several SAMOS Configurations Obtained from Free-Flight Model Firings. Defense Technical Information Center. https://doi.org/10.21236/ad0323887
• Cronvich, L. L., and H. P. Liepman. 1979. Advanced Missile Technology. a Review of Technology Improvement Areas for Cruise Missiles. NASA-CR-3187. NASA. https://ntrs.nasa.gov/citations/19800001864
• Crose, D. 1965. “A Development and Demonstration Program on Low Cost Inertial Guidance for Tactical Weapon System Applications.” In Guidance Control Conference. AIAA 1965-1202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1202
• Crowley, F., R. Gray, and H. Ossing. 1971. “On Motion Error in Inertial Component Tests.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-923. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-923
• “Cruise Missile.” 2009. In Planet Austria, edited by Österreichische Akademie der Wissenschaften. Verlag der Österreichischen Akademie der Wissenschaften. https://doi.org/10.1553/planetaustrias164
• Cruise Missile Engines. 1982. NASA. https://ntrs.nasa.gov/citations/20030002808
• “Cruise Missiles.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_7
• Cruise Missiles. 2015. https://doi.org/10.5040/9798216523628.ch-vii
• “Cruising Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0215.0236
• Cruz, Rogério Luiz Verissimo, Carlos Alberto Gurgel Veras, and Olexiy Shynkarenko. 2024. “Cross-Domain Innovation: Developing a Supersonic Ramjet Antiship Missile Using Space Standards and Rocket Technology.” In Espaço exterior: um olhar multidisciplinar sobre o futuro da humanidade. Agência Espacial Brasileira. https://doi.org/10.70689/978-65-89535-19-5.116-128
• Cruzen, L. 1983. “Cruise Missile Propulsion versus Commercial Airliner Propulsion: Different Challenges Can Produce Similar Engine Cycles.” In 19th Joint Propulsion Conference. AIAA 1983-1176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1176
• Csavina, Frank L., and Russell K. Denney. 1991. “A Global Approach in Evaluating Inlet/Engine Compatibility.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-402
• Cubbison, R., and D. Smeltzer. 1968. “Study of a Family of Supersonic Inlet Systems.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-580
• Cui, Xiang-xiang, Hong-li Wang, Jing-hui Lu, and Cong Chen. 2014. “Star Covering Region Evaluation with Application to Star Tracker Design.” Journal of Aerospace Engineering 27 (2): 291–96. https://doi.org/10.1061/(asce)as.1943-5525.0000259
• Cui, Lei, Kang Zhang, Xijing Hu, Zhe Li, Jianying Yang, and Nan Jin. 2023b. “Improved Fixed-Time Convergence Guidance Scheme Design and Its Application to Missile.” Guidance, Navigation and Control 03 (04): 2350022. https://doi.org/10.1142/s273748072350022x
• Cui, Jian, and Qiancheng Zhao. 2020. “Bias Thermal Stability Improvement of MEMS Gyroscope with Quadrature Motion Correction and Temperature Self-Sensing Compensation.” Micro & Nano Letters 15 (4): 234–38. https://doi.org/10.1049/mnl.2019.0479
• Culick, F. 1984. “Numerical Calculations of Pressure Oscillations in a Side-Dump Ramjet Engine.” In 22nd Aerospace Sciences Meeting. AIAA 1984-365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-365
• Culick, F. E. C., F. E. Marble, and E. E. Zukoski. 1982. Mechanisms of Exciting Pressure Oscillations in Ramjet Engines. Defense Technical Information Center. https://doi.org/10.21236/ada133977
• Culick, F. E. C., F. E. Marble, and E. E. Zukoski. 1983. Mechanisms of Exciting Pressure Oscillations in Ramjet Engines. Defense Technical Information Center. https://doi.org/10.21236/ada147818
• Culick, F. E., F. E. Marble, and E. E. Zukoski. 1985. Mechanisms of Exciting Pressure Oscillations in Ramjet Engines. Defense Technical Information Center. https://doi.org/10.21236/ada172546
• Cullen, Francis P. 1969. Propagation Measurements for over-Water Low-Angle and over-Horizon Communications with Buoys. Defense Technical Information Center. https://doi.org/10.21236/ad0861695
• Culp, Robert D., and George Bickley. 1993. Guidance and Control, 1993; Annual Rocky Mountain Guidance and Control Conference, 16th, Keystone, CO, Feb. 6-10, 1993. ISSN: 0065-3438. Colorado Univ. https://ntrs.nasa.gov/citations/19950048790
• Cumming, Stephen B., Mark S. Smith, Aliyah N. Ali, Trong T. Bui, Joel C. Ellsworth, and Christian A. Garcia. 2016. “Aerodynamic Flight-Test Results for the Adaptive Compliant Trailing Edge.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160007775
• Curran, Edward T., and Roger R. Craig. 1973. The Use of Stream Thrust Concepts for the Approximate Evaluation of Hypersonic Ramjet Engine Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0769481
• Curry, T. Bradley, Jr., and Norman L. Crabill. 1961. Rocket-Model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-Engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37. NASA-TN-D-638. NASA. https://ntrs.nasa.gov/citations/20040006383
• Cusick, Andrew, and Konstantinos Kontis. 2019. “Creation of Design and Analysis Tools for Large Design Space Reusable Launch Vehicle Shape Optimization.” In AIAA Aviation 2019 Forum. AIAA 2019-2929. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2929
• D’Aiutolo, Charles T., and Allen B. Henning. 1955. Lateral Stability Characteristics at Low Lift between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-Arc Sections and 40 Degrees Sweepback. NACA-RM-L55A31. NASA. https://ntrs.nasa.gov/citations/19930088583
• D’Aiutolo, Charles T., and Allen B. Henning. 1956. Lateral Stability Characteristics between Mach Numbers of 0.80 and 1.57 and Simulation of Coupled Motion at Mach Number of 1.30 of a Rocket-Propelled Model of an Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces. NACA-RM-L56A17. NASA. https://ntrs.nasa.gov/citations/19930090203
• D’Aiutolo, Charles T., William W. Willoughby, and Lucille C. Coltrane. 1957. Free-Flight Experience of the Lateral Stability Characteristics at Low Lift of a 45 Degree Swept-Wing Rocket-Propelled Model Equipped with a Nonlinear Yaw-Rate Damper System at Mach Numbers from 0.76 to 1.73. NACA-RM-L56L18. NASA. https://ntrs.nasa.gov/citations/19930090110
• D’Amato, Anthony, and Dennis Bernstein. 2012. “Adaptive Control of a Seeker-Guided 2D Missile with Unmodeled Aerodynamics.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4617
• Da, Ren. 1993. “Failure Detection in Hybrid Strapdown-INS/GPS.” In Guidance, Navigation and Control Conference. AIAA 1993-3821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3821
• Dai, Xiao, Lin Zhao, and Zhen Shi. 2013b. “Optimal Sensor Fusion in Redundant Inertial Measurement Unit.” Applied Mechanics and Materials 433-435: 250–53. https://doi.org/10.4028/www.scientific.net/amm.433-435.250
• Dalton, Jeffrey, and S. Balakrishnan. 1993. “Neural on-Line Learning in Missile Guidance.” In Guidance, Navigation and Control Conference. AIAA 1993-3872. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3872
• DaMing, Zhu, Zhu Zhili, Tang Long, and Zhang Jin. 2009. “Overall Performance Design of Ramjet for Combined Engine.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-1426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-1426
• Damrongsak, B., and M. Kraft. 2006. “Design and Simulation of a Micromachined Electrostatically Suspended Gyroscope.” In IET Seminar on MEMS Sensors and Actuators, vol. 2006. IEE. https://doi.org/10.1049/ic:20060468
• Danai, Kourosh, James R. McCusker, and C. V. Hollot. 2008. “Mutual Identifiability Analysis for Parameter Signature Isolation in the Time-Scale Plane.” In ASME 2008 Dynamic Systems and Control Conference, Parts A and B. ASMEDC. https://doi.org/10.1115/dscc2008-2208
• Dangui, Vinayak, Michel J. F. Digonnet, and Gordon S. Kino. 2009. “Laser-Driven Photonic-Bandgap Fiber Optic Gyroscope with Negligible Kerr-Induced Drift.” Optics Letters 34 (7): 875. https://doi.org/10.1364/ol.34.000875
• Daniel, Donald B. 1965. “Radio Augmented and Calibrated Inertial Navigation Equipment.” Navigation 12 (4): 348–54. https://doi.org/10.1002/j.2161-4296.1965.tb02153.x
• Daniel, Walter K., Thomas E. Correll, and Mark O. Anderson. 1995. “Development of a Direct Match Technique for Star Identification on the SWAS Mission.” In Flight Mechanics(Estimation Theory Symposium 1995. https://ntrs.nasa.gov/citations/19950021350
• Daniel, F. P., G. B. Doane III, and R. R. Kissel. 1968. Strapdown Inertial Navigation at the Marshall Space Flight Center a Study. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19690027477
• Daniel, Leo, Giorgio Tumino, Torben Henriksen, and Christian Dujarric. 2004. “Advanced Composite Technology in Reusable Launch Vehicle (RLV).” In Space 2004 Conference and Exhibit. AIAA 2004-5825. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5825
• Danik, B. 1973. “Hybrid-Inertial Navigation with Range Updates in a Relative Grid.” In Guidance and Control Conference. AIAA 1973-873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-873
• Dankowych, J. A., B. Bednarz, G. Joslin, K. Jew, D. H. Lewis, and W. A. Young. 1986. “Closed Loop Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 0566. SPIE. https://doi.org/10.1117/12.949766
• Dann, Andrew. n.d. “Inlet Design for a Mach 2 Pulse Detonation Engine.” PhD diss., The University of Queensland. https://doi.org/10.14264/345514
• Danowsky, Brian P., David K. Schmidt, and Harald Pfifer. 2017. “Control-Oriented System and Parameter Identification of a Small Flexible Flying-Wing Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-1394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1394
• Dao, H. N., V. V. Klimakov, A. V. Molchanov, and M. V. Chirkin. 2017. “Gas Dynamics in Active Medium and Bias Instability of Laser Gyroscope.” Vestnik of Ryazan State Radio Engineering University 59 (1): 136–44. https://doi.org/10.21667/1995-4565-2017-59-1-136-144
• Daoudi, Amina. n.d. “A Method for Field Calibration of a Gyroscope in an Airborne Gravimetry Inertial Stable Platform.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2001-04972
• Darling, Jacob, Nathan Houtz, Carolin Frueh, and Kyle J. DeMars. 2016. “Recursive Filtering of Star Tracker Data.” In AIAA/AAS Astrodynamics Specialist Conference. AIAA 2016-5672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5672
• Daryabeigi, Kamran. 2001. Thermal Analysis and Design of Multi-Layer Insulation for Re-Entry Aerodynamic Heating. AIAA Paper 2001-2834. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010066880
• Das, Priya, Charu Chawla, and Radhakant Padhi. 2009. “Robust Partial Integrated Guidance and Control of Interceptors in Terminal Phase.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6275
• Dasari, Sathvik. 2026. “Autonomous Navigation for Hypersonic Aircraft Using Inertial Navigation Sensors Systems and Machine Learning.” In The Precise Time and Time Interval Systems and Applications Meeting. Institute of Navigation. https://doi.org/10.33012/2026.20487
• Dasaro, Joseph A. 1970. Rapid Initialization of Inertial Navigation Systems through Parameter Estimation. Defense Technical Information Center. https://doi.org/10.21236/ad0706219
• Dasgupta, Sagar, Minhaj Uddin Ahmad, Muhammad Sami Irfan, Mizanur Rahman, and Jordan D. Larson. 2026. “Resilient Urban Vehicle Navigation in GNSS-Denied Environments via Tightly Integrated Inertial Propagation, Deep Motion Inference, GIS Route Constraints, and Opportunistic Visual Landmark Corrections.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20799
• Daub, C. T. 1979. “A Completely Programmable Method of Celestial Navigation.” Navigation 26 (1): 59–62. https://doi.org/10.1002/j.2161-4296.1979.tb01356.x
• Daughetee, C. 1974. “Drop Testing Naval Aircraft and the VSD Landing Gear Dynamic Test Facility.” In 15th Structural Dynamics and Materials Conference. AIAA 1974-343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-343
• Davidson, G. Westly. 2015. “Improved Landing Gear Shimmy Model.” SAE International Journal of Aerospace 08 (1): 150–54. https://doi.org/10.4271/2015-01-9003
• Davidson Jr., H. D. Frank, and Lawrence A. 1972. Surface Effect Take-Off and Landing System (SETOLS) Subsonic Static Stability out of Ground Effect. Defense Technical Information Center. https://doi.org/10.21236/ad0763365
• Davies, Rose G. 2020. “Introduction of Supersonic Flight.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9780429261152-11
• Davies, Rose G. 2025. “Introduction of Supersonic Flight.” In Aerodynamics Principles for Air Transport Pilots. CRC Press. https://doi.org/10.1201/9781032692883-12
• Davis, Larry. 1986. Vision-Based Navigation for Autonomous Ground Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada171618
• Davis, Steve. 1988a. Electrical Load and Power Source Capacity Report for the C-130 Aircraft Microwave Landing System (MLS) SLIASC Model 6216. Defense Technical Information Center. https://doi.org/10.21236/ada196721
• Davis, Larry S. 1988b. Vision-Based Navigation for Autonomous Ground Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada203712
• Davis, Ian L. 1995. Sensor Fusion for Autonomous Outdoor Navigation Using Neural Networks. Defense Technical Information Center. https://doi.org/10.21236/ada293563
• Davis, R. A., S. D. Elrod, and D. T. Lovell. 1972. “Titanium Honeycomb Structure.” In NASA. Langley Res. Center Proc. of the Symp. on Welding, Bonding, and Fastening. https://ntrs.nasa.gov/citations/19740022813
• Davis, Milt, Alan Hale, and Dave Beale. 2001. “An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/2001-gt-0507
• Davis, Bradford S., Michael B. Hamilton, and David J. Hepner. 2002. Shock Experiment Results of the DFuze 8-Channel Inertial Sensor Suite That Contains Commercial Magnetometers and Accelerometers. Defense Technical Information Center. https://doi.org/10.21236/ada402987
• Davis, Milt W., and David S. Kidman. 2010. “Prediction and Analysis of Inlet Pressure and Temperature Distortion on Engine Operability from a Recent T-38 Flight Test Program.” In Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Education; Electric Power; Manufacturing Materials and Metallurgy. ASMEDC. https://doi.org/10.1115/gt2010-22047
• Davis, Pamela A., and Mercedes C. Lopez. 1987. Static Mechanical Properties of 30 x 11.5-14.5, Type VII, Aircraft Tires of Bias-Ply and Radial-Belted Design. SAE PAPER 871868. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880043595
• Davis, G. W., P. P. Plank, C. C. Richie, and I. F. Sakata. 1970a. Hypersonic Cruise Vehicle Wing Structure Evaluation. NASA-CR-1568. NASA. https://ntrs.nasa.gov/citations/19700018708
• Davis, G. W., P. P. Plank, C. C. Richie, and I. F. Sakata. 1970b. Hypersonic Cruise Vehicle Wing Structure Evaluation: Volume 2, Sections 11-22. NASA-CR-66897-2. NASA. https://ntrs.nasa.gov/citations/19700017939
• Davis, G. W., P. P. Plank, C. C. Richie, and I. F. Sakata. 1970c. Hypersonic Cruise Vehicle Wing Structure Evaluation: Volume 3, Sections 23-27. NASA-CR-66897-3. NASA. https://ntrs.nasa.gov/citations/19700017940
• Davis, G. W., P. P. Plank, C. C. Richie, and I. F. Sakata. 1970d. Substantiation Data for Hypersonic Cruise Vehicle Wing Structure Evaluation: Volume 1, Sections 1-10. NASA-CR-66897-1. NASA. https://ntrs.nasa.gov/citations/19700017938
• de Alvear Cárdenas, José Ignacio, and Gertjan Looye. 2021. “Automatic Landing Design for Overweight Transport Aircraft with Explicit Flare Controller and Incremental Backstepping.” In AIAA Scitech 2021 Forum. AIAA 2021-0781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0781
• de Aquino, F. Radler. 1951. “A New Wrinkle in Astro-Navigation.” Journal of Navigation 4 (04): 371–76. https://doi.org/10.1017/s0373463300034238
• De Groot, Loren E. 1965. “Loran-Inertial Navigation Systems for Long-Range Use.” Journal of Navigation 18 (3): 319–29. https://doi.org/10.1017/s0373463300019214
• De Groot, L. E., and J. Larsen. 1965. Three Dimension Celestial Navigation. Rockwell Polar Expedition. https://ntrs.nasa.gov/citations/19690067308
• de Nicola, C., R. Tognaccini, P. Visingardi, and L. Paparone. 1994. “Progress in the Aerodynamic Analysis of Inviscid Supersonic Flow Fields around Complex Aircraft Configurations.” In 12th Applied Aerodynamics Conference. AIAA 1994-1821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1821
• de Oliveira, Élcio Jeronimo, Waldemar de Castro Leite Filho, and Ijar Milagre da Fonseca. 2012b. “Inertial Measurement Unit Calibration Procedure for a Redundant Tetrahedral Gyro Configuration with Wavelet Denoising.” Journal of Aerospace Technology and Management 4 (2): 163–68. https://doi.org/10.5028/jatm.2012.04026111
• de Oliveira, Élcio, Hélio Koiti Kuga, and Ijar de Fonseca. 2012a. “Fault Detection and Isolation in Inertial Measurement Units Based on ?2-CUSUM and Wavelet Packet.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4753
• De VAULT, R. T. 1957. “The Ramjet-Turbojet Propulsion System for Supersonic Flight.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/570206
• de Vries, Pieter Simke, Jim Rojer, and Floris E. Kalff. 2023. “Quantum-Based Relative Inertial Navigation with Velocity-Aided Alignment and Initialization.” In ENC 2023. MDPI. https://doi.org/10.3390/enc2023-15437
• De-You, Yan. 1985. “Modelling the Axial-Flow Compressors for Calculating Starting of Turbojet Engines.” In Volume 1: Aircraft Engine; Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/85-igt-97
• DeAntonio, Luisa, Gabriel Udomkesmalee, James W. Alexander, et al. 1993. “Star-Tracker-Based, All-Sky, Autonomous Attitude Determination.” In SPIE Proceedings, vol. 1949, edited by George E. Sevaston, Richard H. Stanton. SPIE. https://doi.org/10.1117/12.157083
• Debiasi, Marco, Zeng Yan, and Tat Loon Chng. 2010. “Swept-Back Grid Fins for Transonic Drag Reduction.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4244
• DeBra, Daniel, and John Breakwell. 1986. Study to Develop Use of Gravity Gradiometers in Gravity Mapping. Defense Technical Information Center. https://doi.org/10.21236/ada179611
• DeBra, Daniel B., John V. Breakwell, and Eugene Wells. 1981. Gravity Gradiometer Survey and Real Time Techniques for Improving Inertial Navigation System Accuracy. Defense Technical Information Center. https://doi.org/10.21236/ada114636
• Decker, Robert K. 2002. Viscous Drag Measurement and Its Application to Base Drag Reduction. Defense Technical Information Center. https://doi.org/10.21236/ada403228
• Deep, R. A., J. H. Henderson, and C. E. Brazzel. 1971. Thrust Effects on Missile Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ad0728155
• Dees, Ray A., and Cheng M. Moua. 2010. “Challenges and Lessons Learned from Resurrecting a Legacy Research Flight Controller.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100001731
• DeGROOT, Loren E., and John Larsen. 1966. “Three Dimension Celestial Navigation.” Navigation 13 (4): 320–26. https://doi.org/10.1002/j.2161-4296.1966.tb02176.x
• Dehghani, Mehdi, Hamed Kharrati, Hadi Seyedarabi, and Mahdi Baradarannia. 2019. “The Correcting Approach of Gyroscope-Free Inertial Navigation Based on the Applicable Topological Map.” Journal of Computing and Information Science in Engineering 19 (2): 021001. https://doi.org/10.1115/1.4041969
• Deiler, Christoph, and Nicolas Fezans. 2025. “Modeling of the A320 Landing Gear Drag during Their Extension and Retraction.” In AIAA SCITECH 2025 Forum. AIAA 2025-1250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1250
• Deitering, J. S., and E. E. Hilliard. 1965. Wind Tunnel Investigation of Flexible Aerodynamic Decelerator Characteristics at Mach Numbers 1.5 to 6. Defense Technical Information Center. https://doi.org/10.21236/ad0464786
• Dejarnette, F. R. 1979. Aerodynamic Heating on Complex Configurations. AIAA PAPER 79-0891. North Carolina State University. https://ntrs.nasa.gov/citations/19790050710
• Dejarnette, F. R., and H. H. Hamilton. 1974. “Aerodynamic Heating on 3-D Bodies Including the Effects of Entropy-Layer Swallowing.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19740050428
• Dejarnette, F. R., H. H. Hamilton, K. J. Weilmuenster, and F. M. Cheatwood. 1985. A Review of Some Approximate Methods Used in Aerodynamic Heating Analyses. AIAA PAPER 85-0906. North Carolina State University. https://ntrs.nasa.gov/citations/19850055429
• Dejarnette, F. R., L. A. Kania, and A. Chitty. 1983. “Aerodynamic Heating and Surface Temperatures on Vehicles for Computer-Aided Design Studies.” In American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19830035481
• Delabie, Tjorven. 2013. “Robust and Efficient Star Tracker Attitude Estimation Using the AIM Algorithm.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4561. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4561
• Delabie, Tjorven. 2015. “Star Position Estimation Improvements for Accurate Star Tracker Attitude Estimation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-1332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1332
• Delaye, Philippe. 2000. “Double Phase Conjugate Multimode Fiber Optic Gyroscope.” In Fourteenth International Conference on Optical Fiber Sensors, edited by A. G. Mignani, H. C. Lefèvre. SPIE. https://doi.org/10.1117/12.2302252
• Delforge, J., L. d’Angio, and S. Audoly. 1987. “Results and Conjectures on the Identifiability of Linear Systems.” In Identifiability of Parametric Models. Elsevier. https://doi.org/10.1016/b978-0-08-034929-9.50006-6
• Delmundo, A. R., F. T. McQuilkin, and R. R. Rivas. 1981. SPF/DB Primary Structure for Supersonic Aircraft (T-38 Horizontal Stabilizer). NASA-CR-163114. NASA. https://ntrs.nasa.gov/citations/19840019791
• Delurgio, P., B. Engstrom, and W. Buhler. 1981. “The Mid-Air Recovery System for the Air Launched Cruise Missile.” In 7th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1981-1915. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1915
• DeMars, Kyle J., Jacob E. Darling, Michael A. Waltemate, and Samuel J. Haberberger. 2014. Performance Evaluation Criteria and Analysis of Navigation Systems Using Inertial Measurement Unit Technology. Defense Technical Information Center. https://doi.org/10.21236/ada605594
• Demichele, D. J., R. L. George, R. M. Mains, and N. H. Wood. 1965. Instrumentation Design Study for Testing a Hypersonic Ramjet Engine on the x-15 a-2. Volume 2- Preliminary Design of in-Flight Thrust/drag Measuring Device. NASA-CR-62183. NASA. https://ntrs.nasa.gov/citations/19650011863
• Demidov, O. V. 2009. “Estimation of Instrumental Errors for an Inertial Navigation System Using the Schuler Period.” Moscow University Mechanics Bulletin 64 (4): 97–100. https://doi.org/10.3103/s0027133009040050
• Demkowicz, Jerzy. 2024. “MEMS Modelling in the Context of Inertial Navigation.” International Journal of Electronics and Telecommunications: 887–93. https://doi.org/10.24425/ijet.2024.152074
• Denaci, D. E., W. P. Killalea, and C. T. Pesek. 1968. Clamping Assembly for Inertial Components Patent. Patent Number: US-PATENT-3,361,400. Honeywell, Inc. https://ntrs.nasa.gov/citations/19710011338
• Dendy, Jackson, Jackson Hayes, and Jacob Ramsey. 2026. “Design and Performance Analysis of Tachyon: A Low-Altitude Hypersonic Glide Vehicle.” In 2026 Regional Student Conferences. AIAA 2026-112635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-112635
• Deng, Jiahong. 2026. “Hypersonic Glide Trajectory Planning with Sequential Convex Optimization and Hp Pseudospectral Discretization.” Journal of Physics: Conference Series 3240 (1): 012025. https://doi.org/10.1088/1742-6596/3240/1/012025
• Deng, Zhiyun, and Luis Sentis. 2026. “The Kidnapped UAV Problem: Self-Supervised Detection and Recovery of Localization Failures for GNSS-Denied Navigation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20744
• Deng, Zhihong, Lei Shi, Tong Liu, and Bo Wang. 2019c. “Switching Method for Long-Term Inertial Navigation System Based on Switched Control.” Journal of Navigation 72 (5): 1315–30. https://doi.org/10.1017/s0373463319000122
• Deng, Zhi-Liang, Jin Sun, Fei Ding, and Mohamed Wahab Mohamed Ismail. 2024. “A Novel Damping Method for Strapdown Inertial Navigation System.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/27625377
• Deng, Jia, Sentang Wu, Hongbo Zhao, and Da Cai. 2019a. “Measurement Model and Observability Analysis for Optical Flow-Aided Inertial Navigation.” Optical Engineering 58 (08): 1–14. https://doi.org/10.1117/1.oe.58.8.083102
• Deng, Jiuqiang, Wenchao Xue, Xi Zhou, and Yao Mao. 2020. “On Disturbance Rejection Control for Inertial Stabilization of Long-Distance Laser Positioning with Movable Platform.” Measurement and Control 53 (7–8): 1203–17. https://doi.org/10.1177/0020294020935492
• Deng, Jiahong, and Jisong Zhao. 2026. “High-Precision Trajectory Planning Method for Hypersonic Glide Vehicles Based on Sequential Convex Optimization.” Journal of Physics: Conference Series 3207 (1): 012079. https://doi.org/10.1088/1742-6596/3207/1/012079
• Deng, Xinyun, Zhaomingyue Zheng, Yixin Huo, Yan Zhang, Yumeng Dan, and Pingping Zhang. 2025. “Reliability Assessment of Rocket Flight Test Based on Fuzzy Comprehensive Judgment Method.” IET Conference Proceedings 2025 (35): 1635–40. https://doi.org/10.1049/icp.2025.3751
• Dennison, Edwin W., James W. Alexander, and Richard H. Stanton. 1993. CCD Star Tracker Experience – Key Results from Astro 1 Flight. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210004494
• Denver, Troelz, John L. Jørgensen, Peter S. Jørgensen, Mathias Benn, Per Bodin, and Robin Courson. 2025. “The Comet Interceptor Mission Navigation Camera and Star Tracker System.” In Small Satellites Systems and Services Symposium (4S 2024), edited by Max Petrozzi-Ilstad. SPIE. https://doi.org/10.1117/12.3062622
• Derbel, Khaoula, and Károly Beneda. 2025. “Investigation of Turbojet Engine Performance in Subsonic Flight Conditions with Turbofan Power Ratio as Thrust Parameter.” Periodica Polytechnica Transportation Engineering 53 (2): 194–205. https://doi.org/10.3311/pptr.37560
• Derby, R. M., W. D. Foley, W. D. Gates, and J. J. Wilczynski. 1964. Optical Inertial Space Sextant for an Advanced Space Navigation System. NASA-CR-133. NASA. https://ntrs.nasa.gov/citations/19650002700
• Dermer, Dan. n.d. “Auto-Landing System for Fixed-Wing Unmanned Aerial Vehicle.” PhD diss., San Jose State University. https://doi.org/10.31979/etd.wtda-f4gc
• Derose, C. E., and W. K. Lockman. 1971. Aerodynamic Heating of a Space Shuttle Delta-Wing Booster at Free Stream Mach 7.4. NASA-TM-X-62058. NASA. https://ntrs.nasa.gov/citations/19710026878
• Derose, C. E., W. K. Lockman, J. G. Marvin, G. G. Mateer, C. C. Pappas, and H. L. Seegmiller. 1971. “Surface Flow Patterns and Aerodynamic Heating on Space Shuttle Vehicles.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19710050842
• Des Jardins, R. 1969. In-Orbit Star Tracker Misalignment Estimation on the OAO. NASA-TM-X-63681. NASA. https://ntrs.nasa.gov/citations/19690028314
• Deshpande, Sameet. 2021. “TerraPoiNT: An Advanced Terrestrial Technology to Enhance Navigation in a GNSS-Denied Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2021.18074
• “Design of Missile with Two-Loop and Autopilot Yaw Using Root Locus.” 2016. International Journal of Science and Research (IJSR) 5 (5): 2018–20. https://doi.org/10.21275/v5i5.nov163844
• DeSpirito, James. 2008. “CFD Prediction of Magnus Effect in Subsonic to Supersonic Flight.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-427
• DeSpirito, James. 2009. CFD Prediction of Magnus Effect in Subsonic to Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada508090
• DeSpirito, James, and Jubaraj Sahu. 2001. “Viscous CFD Calculations of Grid Fin Missile Aerodynamics in the Supersonic Flow Regime.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-257. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-257
• DeSpirito, James, Milton Vaughn, and William Washington. 2002. “CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins in Supersonic Flow.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4509
• DeSpirito, James, Milton Vaughn, and William Washington. 2003. “Subsonic Flow CFD Investigation of Canard-Controlled Missile with Planar and Grid Fins.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-27. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-27
• Dessornes, O., D. Scherrer, and P. Novelli. 2001. “Tests of the JAPHAR Dual Mode Ramjet Engine.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1886
• Deters, R. A., D. F. Eisenhut, and R. F. Gates. 1966. The Fine Guidance Sensor: An Electronic Scanning Star Tracker. NASA. https://ntrs.nasa.gov/citations/19660049162
• Deters, R., and R. Gutshall. 1984. “Charge Injection Device Star Tracker Applications.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1851. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1851
• Devaud, E., J. Harcaut, and H. Siguerdidjane. 1999. “Various Strategies to Design a Three-Axes Missile Autopilot.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-3976. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3976
• Deveikis, W. D., R. Rosecrans, and R. W. Walker. 1965. Flutter Investigation of Streamwise-Oriented Arrays of Curved Panels under Compressive Loading and Aerodynamic Heating. NASA-TN-D-2910. NASA. https://ntrs.nasa.gov/citations/19650018216
• “Development of Criterion of Degree of Identifiability of Parameters of Dynamic Systems.” 2015. In 2015 The 5th International Workshop on Computer Science and Engineering-Information Processing and Control Engineering. WCSE. https://doi.org/10.18178/wcse.2015.04.011
• DeVorkin, David. 1992. “Inventing Accuracy: A Historical Sociology of Nuclear Missile Guidance by Donald MacKenzie.” Technology and Culture 33 (3): 649–52. https://doi.org/10.1353/tech.1992.0099
• Devote, Basil Daniel, and Lawrence Hart. 2025. “Hybrid Model for Vertical Deflection Component Determination.” South African Journal of Geomatics 14 (2): 297–316. https://doi.org/10.4314/sajg.v14i2.8
• Dewar, Patrick, Joseph Gido, and Joseph Carroll. 1993. “D2 Inertial Measurement Unit.” In Annual Interceptor Technology Conference. AIAA 1993-2694. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2694
• Deweese, J., and R. McCarty. 1973. “Parachute Design and Performance Data Bank.” In 4th Aerodynamic Deceleration Systems Conference. AIAA 1973-484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-484
• Dewell, Larry, Jason Speyer, Michael Dinkelmann, et al. 1997. “Fuel-Optimal Periodic Solutions to Hypersonic Cruise with Active Engine Cooling.” In Guidance, Navigation, and Control Conference. AIAA 1997-3478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3478
• Dey, Saugato, Thazhe Kunnath Sunil Kumar, Sankar Ashok, and Saikat Kumar Shome. 2023. “Robust Cascade Control Strategy for Trajectory Tracking to Decouple Disturbances Using 3-Degree-of-Freedom Inertial Stabilized Platform and Its Experimental Validation.” Transactions of the Institute of Measurement and Control 47 (12): 2475–97. https://doi.org/10.1177/01423312221150290
• Deyle, Travis. 2005. Low-Cost Inertial Measurement Unit. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/922761
• Dhayalan, R., Subrahmanyam Saderla, and Ajoy Kanti Ghosh. 2018. “Parameter Estimation of UAV from Flight Data Using Neural Network.” Aircraft Engineering and Aerospace Technology 90 (2): 302–11. https://doi.org/10.1108/aeat-03-2016-0050
• Di Corato, Francesco, Mario Innocenti, and Lorenzo Pollini. 2013a. “Experimental Evaluation of a Visual-Inertial Navigation System with Guaranteed Convergence.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5038. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5038
• Di Corato, F., M. Innocenti, and L. Pollini. 2013b. “Robust Vision-Aided Inertial Navigation Algorithm via Entropy-like Relative Pose Estimation.” Gyroscopy and Navigation 4 (1): 1–13. https://doi.org/10.1134/s2075108713010033
• Dianetti, Andrew D., Ryan M. Weisman, and John L. Crassidis. 2017. “Application of Observability Analysis to Space Object Tracking.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1258
• Diaz, Jorge E., and Scott J. Pierce. 2016. “Satellite Ephemeris Correction via Remote Site Observation for Star Tracker Navigation Performance Improvement.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2016.13492
• Dickeson, Jeffrey, Armando Rodriguez, Srikanth Sridharan, Jose Benavides, and Don Soloway. 2009. “Decentralized Control of an Airbreathing Scramjet-Powered Hypersonic Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6281
• Dickey, Robert R. 1958. The Effect of Moment-of-Area-Rule Modifications on the Zero-Lift Drag of Three Wing-Body Combinations. NACA-RM-A58A31. NASA. https://ntrs.nasa.gov/citations/19930090067
• Dickey, Robert R. 1959. The Effect of Moment of Area Rule Modifications on the Drag, Lift and Pitching Moment Characteristics of an Unswept Aspect Ratio 6 Wing and Body Combination. NASA-MEMO-2-24-59A. NASA. https://ntrs.nasa.gov/citations/19980231999
• Dickman, Christopher A., and Timothy T. Takahashi. 2016. “Engine/Inlet Matching for Supersonic Aircraft Design.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0771
• DiDonato, Armido. 2007. Computation of the Circular Error Probable (CEP) and Confidence Intervals in Bombing Tests. Defense Technical Information Center. https://doi.org/10.21236/ada476333
• Dietrich, R. G., B. A. Hall, and K. E. Tiernan. 1963. A Minimum Fuel Vertical Touchdown Lunar Landing Guidance Technique. AIAA PAPER 63-345. NASA. https://ntrs.nasa.gov/citations/19630024609
• Dieudonne, J. E., R. D. Grove, and G. G. Steinmetz. 1976. A Simulation Study of Curved, Descending, Decelerating, Landing Approaches for Transport Aircraft. NASA-TN-D-8190. NASA. https://ntrs.nasa.gov/citations/19760014128
• “Differential Game-Based Interceptor Missile Guidance.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-17
• “Differential Geometry Applied to Missile Guidance.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-16
• Digges, Kennerly H. 1971. Theory of an Air Cushion Landing System for Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0728647
• Diggins, J. L. 1951. Diffuser Investigations in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0895227
• “A Digital Diagnostic System for a Small Turbojet Engine.” 2013. Acta Polytechnica Hungarica 10 (4). https://doi.org/10.12700/aph.10.04.2013.4.3
• Digonnet, Michel J. F. 2014. “The Fiber Optic Gyroscope: Past and Present.” In Frontiers in Optics 2014. OSA. https://doi.org/10.1364/fio.2014.ftu5b.1
• Digonnet, M. J. F., H. K. Kim, S. Blin, V. Dangui, and G. S. Kino. 2006. “Sensitivity and Stability of an Air-Core Fiber-Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.2006.me1
• Dill, Evan T., Steven D. Young, and Maarten Uijt De Haag. 2017. “GPS/Optical/Inertial Integration for 3D Navigation Using Multi-Copter Platforms.” In Institute of Navigation. https://ntrs.nasa.gov/citations/20170005464
• Dillenius, Marnix F. E. 1985. Program LRCDM2: Improved Aerodynamic Prediction Program for Supersonic Canard-Tail Missiles with Axisymmetric Bodies. NASA-CR-3883. NASA. https://ntrs.nasa.gov/citations/19870019092
• Dillenius, M. F. 1986. Aerodynamic Prediction for Supersonic Canard-Tail Missiles. ISSN: 0145-319X. Nielsen Engineering and Research, Inc. https://ntrs.nasa.gov/citations/19860000529
• Dillenius, M., M. Hemsch, W. Sawyer, J. Allen, and A. Blair Jr. 1982. “Comprehensive Missile Aerodynamics Programs for Preliminary Design.” In 20th Aerospace Sciences Meeting. AIAA 1982-375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-375
• Dillenius, M., D. Lesieutre, and J. Gjestvang. 2002. “Application of MISDL/KDA Aerodynamics Prediction Method to Penguin Missile.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-277
• Dillenius, M. F. E., and J. N. Nielsen. 1979. Computer Programs for Calculating Pressure Distributions Including Vortex Effects on Supersonic Monoplane or Cruciform Wing-Body-Tail Combinations with Round or Elliptical Bodies. NASA-CR-3122. NASA. https://ntrs.nasa.gov/citations/19810018506
• DİNÇ, Ali. 2021. “Metering Pin Diameter Optimization of an Aircraft Landing Gear Shock Absorber.” Eskişehir Teknik Üniversitesi Bilim ve Teknoloji Dergisi B - Teorik Bilimler 9 (2): 37–46. https://doi.org/10.20290/estubtdb.900786
• Ding, Hengzhi. 2015. “Design of Automatic Carrier Landing System Based on Dynamic Inverse and PID Control.” In Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015. Atlantis Press. https://doi.org/10.2991/icmmcce-15.2015.441
• Ding, Kun, Xuan Cui, Zhimei Wang, Zepeng Qiu, Yubao Hu, and Haiyan Zhang. 2024. “Research on Interception Model of Surface-to-Air Missile Anti-Cruise Missile Weapon System.” Journal of Physics: Conference Series 2890 (1): 012006. https://doi.org/10.1088/1742-6596/2890/1/012006
• Ding, Jianbin, Guang Feng, Panglun Liu, Li Yuan, Yiyao Jiang, and Bingyan Jiang. 2023. “Influence of Structural Torsional Degree of Freedom on Nose Landing Gear Shimmy.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3464356/v1
• Ding, F., C.-B. Shen, W. Huang, and J. Liu. 2015. “Numerical Validation and Back-Pressure Effect on Internal Compression Flows of Typical Supersonic Inlet.” Aeronautical Journal 119 (1215): 631–45. https://doi.org/10.1017/s0001924000010721
• Diop, S., and S. Kribs. 1993. “On the Identifiability of Deterministic Nonlinear Model Parameters.” In Nonlinear Control Systems Design 1992. Elsevier. https://doi.org/10.1016/b978-0-08-041901-5.50042-7
• Disher, John H., Robert C. Kohl, and Merle L. Jones. 1953. Free-Flight Performance of a Rocket-Boosted, Air-Launched 16-Inch-Diameter Ram-Jet Engine at Mach Numbers up to 2.20. NACA-RM-E52L02. NASA. https://ntrs.nasa.gov/citations/19930087445
• Dishman, B. H., and F. H. Shigemoto. 1965. Image Dissector Aperture Geometries and Scan Patterns for Use in Star Tracker Systems. NASA-TN-D-2990. NASA. https://ntrs.nasa.gov/citations/19650022798
• Dissel, Adam, Ajay Kothari, and Mark Lewis. 2005. “Weight Growth Study of Reusable Launch Vehicle Systems.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4369. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4369
• Divakaruni, Sudhakar, Gregg Keith, Chellappan Narayanan, and Joshua Keener. 2008. “Strategic Interferometric Fiber-Optic Gyroscope for Ballistic Missile Inertial Guidance.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7301
• Dixon, W. C., Jr., D. E. Hinton, J. A. Holland, and T. M. Walsh. 1968. A Celestial Attitude Measurement Instrument for Project Scanner. NASA-TN-D-4742. NASA. https://ntrs.nasa.gov/citations/19680022466
• Do, Hyungrok, Seong-kyun Im, Mark Mungal, and Mark Cappelli. 2011b. “The Influence of Boundary Layers on Supersonic Inlet Unstart.” In 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2011-2349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2349
• Do, Hyungrok, Seong-kyun Im, M. Godfrey Mungal, and Mark A. Cappelli. 2011c. “Supersonic Inlet Duct Unstart Induced by Fuel Jet Injection.” In Proceeding of Seventh International Symposium on Turbulence and Shear Flow Phenomena. Begellhouse. https://doi.org/10.1615/tsfp7.1670
• Do, Hyungrok, Seong-kyun Im, Mark Mungal, and Mark Cappelli. 2011d. “Unstart of a Supersonic Model Inlet/Isolator Flow Induced by Mass Injection.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-68. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-68
• Do, H., A. Passaro, and D. Baccarella. 2012. “Inlet Unstart of an Ethylene-Fueled Model Scramjet with a Mach 4.5 Freestream Flow.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5929. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5929
• Doan, Van Minh, Van Thinh Nguyen, Quoc Dat Dang, and Dinh Dung Nguyen. 2026. “Tetrahedral Redundant Accelerometer Block with Geometry-Consistent Fault Detection and Isolation for Strapdown Inertial Navigation Systems.” International Journal of Sustainable Aviation 12 (3): 10079473. https://doi.org/10.1504/ijsa.2026.10079473
• Dobrowolski, A. 1966. Analysis of Nonconstant Area Combustion and Mixing in Ramjet and Rocket-Ramjet Hybrid Engines. NASA-TN-D-3626. NASA. https://ntrs.nasa.gov/citations/19660030241
• DoD Office of Inspector General. 2012. Joint Land Attack Cruise Missile Defense Elevated Netted Sensor System Not Ready for Production Decision (REDACTED). Defense Technical Information Center. https://doi.org/10.21236/ad1016443
• Doherty, David. n.d. “Electropermanent Free-Flight Model Release System for the Hypersonic X3/R Impulse Facility.” PhD diss., The University of Queensland. https://doi.org/10.14264/30640a6
• Doherty, John J., Handing Wang, and Yaochu Jin. 2018. “Use of Global Drag Rise Boundaries to Investigate Ill-Posed Transonic Airfoil Optimization.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3953
• Dol, Sharul Sham. 2021. “Aerodynamics Analysis of Grid Fins Inner Lattice Structure in Cruise Missile.” WSEAS TRANSACTIONS ON FLUID MECHANICS 16: 92–101. https://doi.org/10.37394/232013.2021.16.9
• Dollevedo, Giácomo Antonio. 2023. “Design and Construction of an Improved Closed-Loop Interferometric Fiber Optic Gyroscope.” PhD diss.. https://doi.org/10.47749/t/unicamp.2023.1394045
• Domack, Christopher. 1991. “A Preliminary Investigation of Inlet Unstart Effects on a High-Speedcivil Transport Concept.” In 9th Applied Aerodynamics Conference. AIAA 1991-3327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3327
• Domaratzky, Bernard, Kevin Killian, Bernard Domaratzky, and Kevin Killian. 1997. “Development of a Strategic Grade Fiber Optic Gyro.” In Guidance, Navigation, and Control Conference. AIAA 1997-3549. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3549
• Donatelli-DuLong, D. E. 1979. Development and Evaluation of Adaptive Techniques for Reducing Ionospheric-Induced Radar Tracking Errors in Real Time. Defense Technical Information Center. https://doi.org/10.21236/ada081460
• Dong, Y. 2013. “MEMS Inertial Navigation Systems for Aircraft.” In MEMS for Automotive and Aerospace Applications. Elsevier. https://doi.org/10.1533/9780857096487.2.177
• Dong, Chunyun, and Yuanli Cai. 2017. “Reentry Trajectory Optimization for Hypersonic Glide Vehicle with Flexible Initial Conditions.” Journal of Aerospace Engineering 30 (5): 04017033. https://doi.org/10.1061/(asce)as.1943-5525.0000727
• Dong, Chao Yang, Yu Chen, and Qing Wang. 2009. “Reaction-Jet Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5644. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5644
• Dong, Yizhang, Zhiwei Shi, Kun Chen, and Jie Chen. 2019. “Experimental Investigation of the Effects of Sideslip on Canard-Configuration Aircraft at High Angle of Attack.” AIP Advances 9 (5): 055114. https://doi.org/10.1063/1.5093559
• Dong, C., F. Wu, Y. Liu, Z. Huang, and Y. Cai. 2023. “Fast Trajectory Planning and Guidance for Vertical Landing Reusable Launch Vehicle.” IET Conference Proceedings 2023 (21): 129–34. https://doi.org/10.1049/icp.2023.3008
• Doniger, J. 1967. “Some Automatic Landing System Design Considerations for Scheduled Operations.” In Commercial Aircraft Design and Operation Meeting. AIAA 1967-406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-406
• Doolin, B. F., and R. D. Showman. 1967. Attitude Stabilization of Satellites with Gimbaled Star Trackers. NASA. https://ntrs.nasa.gov/citations/19670060441
• Doolin, B. F., R. D. Showman, and G. M. Sullivan. 1968. Simple Processors of Star Tracker Commands for Stabilizing an Inertially Oriented Satellite. NASA-TN-D-4490. NASA. https://ntrs.nasa.gov/citations/19680009767
• Doronin, V. V. 2019. “Analysis of Experience in Assessing the Extent of Full-Scale Testing of Anti-Aircraft Missile Products during Development and Modernization.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 3: 58–68. https://doi.org/10.38013/2542-0542-2019-3-58-68
• Doronzo, Ruggero. 2026. “Trajectory Optimisation and Manoeuvrability Trade-Offs for Hypersonic Glide Vehicles in Contested Atmospheric Re-Entry.” Advances in Aerospace Science and Technology 11 (03): 77–95. https://doi.org/10.4236/aast.2026.113005
• Dorres, D. 1972. “Missile Launch: A Design Case History.” In Guidance and Control Conference. AIAA 1972-828. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-828
• Dorsey, John, David Myers, and Carl Martin. 2000. “Reusable Launch Vehicle Tank/intertank Sizing Trade Study.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-1043. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1043
• Dorsey, John T., Chauncey Wu, Kevin Rivers, Carl Martin, and Russell Smith. 1999. “Airframe Integration Trade Studies for a Reusable Launch Vehicle.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57503
• Douglas Aircraft Co Long Beach Ca. 1962. An Investigation of the Landing Loads Experienced by the A4D-2 Airplane during Flight Tests and Drop Tests and a Comparison with Theory. Defense Technical Information Center. https://doi.org/10.21236/ad0404510
• Douglas Aircraft Co Long Beach Ca. 1963. Simulator Study of Direct Lift Control during Carrier Landing Approaches. Defense Technical Information Center. https://doi.org/10.21236/ad0406168
• Douglass, M. E. 1963. Turbojet Engine Analyzer Design Study. Defense Technical Information Center. https://doi.org/10.21236/ad0406348
• Dragone, Thomas. 2000. “Structural Innovations in Design, Manufacturing, and Testing on the X-34 Reusable Launch Vehicle.” In Space 2000 Conference and Exposition. AIAA 2000-5309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5309
• Drakin, I. I. 1963. Aerodynamic and Radiation Heating during Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0295828
• Dranitsyna, E. V., and A. I. Sokolov. 2023. “Strapdown Inertial Navigation System Accuracy Improvement Methods Based on Inertial Measuring Unit Rotation: Analytical Review.” Gyroscopy and Navigation 14 (4): 290–304. https://doi.org/10.1134/s2075108724700020
• Draper, Charles S. 1963. “Mechanization of Inertial Guidance Systems.” In Kreiselprobleme / Gyrodynamics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-12200-6_7
• Draper, L. T. 1965. An Approach to Standardizing Star Tracker Calibration. NASA. https://ntrs.nasa.gov/citations/19660040211
• Draper, L. T. 1968. Star Tracker Calibration. NASA-TN-D-4594. NASA. https://ntrs.nasa.gov/citations/19680015083
• Draper, C. S., W. Wrigley, D. G. Hoag, et al. 1965. Space Navigation Guidance and Control, Volume 2. NASA-CR-75798. NASA. https://ntrs.nasa.gov/citations/19660019469
• Dreher, R. C., and W. B. Horne. 1966. Ground-Run Tests with a Bogie Landing Gear in Water and Slush. NASA-TN-D-3515. NASA. https://ntrs.nasa.gov/citations/19660021919
• Driver, Cornelius. 1957. Longitudinal and Lateral Stability and Control Characteristics of Two Canard Airplane Configurations at Mach Numbers of 1.41 and 2.01. NACA-RM-L56L19. NASA. https://ntrs.nasa.gov/citations/19930089678
• Driver, Cornelius. 1958. Longitudinal and Lateral Stability and Control Characteristics of Various Combinations of the Component Parts of Two Canard Airplane Configurations at Mach Numbers of 1.41 and 2.01. NASA-MEMO-10-1-58L. NASA. https://ntrs.nasa.gov/citations/19980232000
• Driver, C. 1960. Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing. NASA-TM-X-328. NASA. https://ntrs.nasa.gov/citations/19650003199
• Driver, C. 1974. “Advanced Supersonic Transport Design Developments.” In 6th Aircraft Design,Flight Test and Operations Meeting. AIAA 1974-987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-987
• Drummond, J. P. 1983. “Numerical Study of a Ramjet Dump Combustor Flow Field.” In American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19830035486
• Dryer, Murray, and Andrew Beke. 1952. Performance Characteristics of a Normal-Shock Side Inlet Located Downstream of a Canard Control Surface at Mach Numbers of 1.5 and 1.8/. NACA-RM-E52F09. NASA. https://ntrs.nasa.gov/citations/19930087106
• Du, Juan, Jian Bai, Jiantao Zhou, and Li Wang. 2018. “Optical Design and Accuracy Analysis of Interferometric Star Tracker.” In Optical Design and Testing VIII, edited by Yongtian Wang, Kimio Tatsuno, Tina E. Kidger. SPIE. https://doi.org/10.1117/12.2501653
• Du, Binhan, Zhifei Ke, Mingkuan Ding, Jinlong Song, and Zhiyong Shi. 2022. “A Configuration Design Method for the Redundant Inertial Measurement Unit Based on the Distributed Salp Swarm Algorithm.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-9492-9_112
• Du, Yijiang, Wei Li, Li Xu, and Qinchen Xu. 2026. “Trajectory Prediction of Hypersonic Glide Vehicles Based on Dual-Branch Attention-TCN-GRU Network.” Journal of Physics: Conference Series 3207 (1): 012059. https://doi.org/10.1088/1742-6596/3207/1/012059
• du Plessis, Francois, Friedl Swanepoel, and Andre Nel. 2009. “An Alternative Methodology for Fiber Optic Gyroscope Calibration.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5662. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5662
• Dual Reticle Star Tracker Final Project Report. 1969. NASA-CR-109722. NASA. https://ntrs.nasa.gov/citations/19700026841
• Duck, K. I. 1973. “Delta Launch Vehicle Inertial Guidance System (DIGS).” In Significant Accomplishments in Technol.. https://ntrs.nasa.gov/citations/19730019087
• Dudush, Anatolii, and Roman Snovydovych. 2026. “Comprehensive Mathematical Model of the Ballistic Trajectory of an Operational-Tactical Missile.” Міжнародний науковий журнал «Military Science» 3 (4): 257–66. https://doi.org/10.62524/msj.2025.3.4.20
• Due, H. 1987. “Development of the Model 373 Turbojet Engine.” In 23rd Joint Propulsion Conference. AIAA 1987-1908. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1908
• Dugan, Duane W. 1959. Estimation of Static Longitudinal Stability of Aircraft Configurations at High Mach Numbers and at Angles of Attack between 0 Deg and +/-180 Deg. NASA-MEMO-1-17-59A. NASA. https://ntrs.nasa.gov/citations/19980228238
• Dugan, J. F., Jr. 1973. Preliminary Study of Turbojets with Rotary Flow Inductors for a Low-Noise Supersonic Transport. NASA-TM-X-68233. NASA. https://ntrs.nasa.gov/citations/19730021077
• Dugger, P. H. 1982. Range Instrumentation Development. Defense Technical Information Center. https://doi.org/10.21236/ada118436
• Duggleby, Andrew, Sibylle Walter, Ben Saletta, Josh Camp, Bill Ross, and Joel Darin. 2025. “Rocket Based Combined Cycle Using a Rotating Detonation Rocket Engine and Ramjet.” In AIAA SCITECH 2025 Forum. AIAA 2025-1141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1141
• Dugundji, John, and John M. Calligeros. 1961. Proposed Test Program on Aerothermoelastic Similarity Laws. Defense Technical Information Center. https://doi.org/10.21236/ad0261532
• Dumbacher, Dan. 2002. “NASA’s Second Generation Reusable Launch Vehicle Program Introduction, Status and Future Plans.” In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2002-3613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3613
• Dumbacher, Dan, and Paul Klevatt. 1994. “DC-XA: First Step Top a Reusable Launch Vehicle.” In Space Programs and Technologies Conference and Exhibit. AIAA 1994-4682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-4682
• Dunbar, W. R., C. E. Hart, and G. Vasu. 1956. Preliminary Report on Experimental Investigation of Engine Dynamics and Controls for a 48-Inch Ramjet Engine. NACA-RM-E55J12. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19670022216
• Duncan, Donald B. 1958b. “Inertial Guidance and Space Navigation.” Navigation 6 (1): 30–33. https://doi.org/10.1002/j.2161-4296.1958.tb01031.x
• Duncan, Donald B. 1959. “Combined Doppler Radar and Inertial Navigation Systems.” Navigation 6 (5): 321–27. https://doi.org/10.1002/j.2161-4296.1959.tb01961.x
• Duncan, R. C. 1965. Technology Report: Guidance and Control Engineering. NASA. https://ntrs.nasa.gov/citations/19650052366
• Duncan, R. C. 1966. Guidance and Control Engineering. NASA. https://ntrs.nasa.gov/citations/19670051921
• Duncan, Robert C. 1968. “Inertial Navigation.” Navigation 15 (1): 39–52. https://doi.org/10.1002/j.2161-4296.1968.tb01584.x
• Duncan, R. 1980. Combinations of 148 Navigation Stars and the Star Tracker. NASA-TM-82203. NASA. https://ntrs.nasa.gov/citations/19800023856
• Duncan, Beverly. 1991. “CFD Analysis of a Hydrogen Fueled Ramjet Engine at Mach 3.44.” In 27th Joint Propulsion Conference. AIAA 1991-1919. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1919
• Duncan, Frank, and Ronald Huisken. 1982. “The Origin of the Strategic Cruise Missile.” Military Affairs 46 (4): 218. https://doi.org/10.2307/1987640
• Duncan, Beverly, and Scott Thomas. 1992. “Computational Analysis of Ramjet Engine Inlet Interaction.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3102
• Dunham, J., A. Long, P. Gural, K. Preiss, and H. Sielski. 1980. “Analysis of Estimation Algorithms for Autonomous Navigation with TDRSS Data.” In NASA. Goddard Space Flight Center Fifth Ann. Flight Mech.(Estimation Theory Symp.. https://ntrs.nasa.gov/citations/19810002568
• Dunmire, G., and L. Lopresti. 1963. “Tv Missile Target Acquisition Simulation and Terminal Guidance Simulation.” In Heterogeneous Combustion Conference. AIAA 1963-1024. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1024
• Dunn, Michael G. 1980. Nuclear Blast Response of Airbreathing Propulsion Systems. Laboratory Measurements with an Operational J-85-5 Turbojet Engine. Defense Technical Information Center. https://doi.org/10.21236/ada092229
• Dunn, K. P. 1984. Atmospheric Refraction Error and Its Compensation for Passive Optical Sensors. Defense Technical Information Center. https://doi.org/10.21236/ada144377
• Dunsworth, L., and G. Reed. 1978. “Ramjet Engine Testing and Simulation Techniques.” In 14th Joint Propulsion Conference. AIAA 1978-935. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-935
• Dupuis, Alain. 1988. “Aeroballistic Range Tests of a Dart Model at Supersonic Speeds.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4378
• Duran, Huseyin, and Ugur Murat Leloglu. 2026. “Maximum-Likelihood Aerial-to-Ground Landmark Matching for Drift Suppression in Lunar Visual–Inertial Navigation.” NAVIGATION: Journal of the Institute of Navigation 73 (1): navi.782. https://doi.org/10.33012/navi.782
• Durand, Tulvio S., and Gary L. Teper. 1964. An Analysis of Terminal Flight Path Control in Carrier Landing. Defense Technical Information Center. https://doi.org/10.21236/ad0606040
• Dusek, H. 1963. “Theory of Error Compensation in Astro-Inertial Guidance Systems for Low-Thrust Space Missions.” In Guidance and Control Conference. AIAA 1963-337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-337
• Dusek, Hermann M. 1964b. “Theory of Error Compensation in Astro-Inertial Guidance Systems for Low-Thrust Space Missions.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395587-6.50031-4
• Dutt, J. C. 1980. Fundamental Modelling of Reacting Flow in Ramjet Dump Combustors. Defense Technical Information Center. https://doi.org/10.21236/ada102554
• Dwyer, Jim. 1994. “Learjet Model 60 Flight Test Program.” In Biennial Flight Test Conference. AIAA 1994-2158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2158
• Dynamic Errors in Strapdown Inertial Navigation Systems. 1971. NASA-CR-1962. NASA. https://ntrs.nasa.gov/citations/19720011006
• Dynnikov, Alexey A. 2020. “The Evaluation of the Flight Incident Probability at the Aircraft Automatic Landing.” In Aviation Safety. CRC Press. https://doi.org/10.1201/9780429070372-59
• Earl, T. Desmond. 1967. Air Cushion Landing Gear Feasibility Study. Defense Technical Information Center. https://doi.org/10.21236/ad0817527
• Eastman, D. 1983. “Aerodynamics Characteristics of a Canard Controlled High Fineness Ratio Missile.” In Applied Aerodynamics Conference. AIAA 1983-1839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1839
• Eastman, Donald, and Donna Wenndt. 1988. “Base Drag of Highly Maneuvering Non-Thrusting Missiles.” In 6th Applied Aerodynamics Conference. AIAA 1988-2544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2544
• Eastwood, C. W., Jr. 1968. Centaur/Surveyor Nose Fairing Aerodynamic Heating Investigation. NASA-TM-X-1605. NASA. https://ntrs.nasa.gov/citations/19680018684
• Ebner, R. E. 1977. Flight-Control/navigation Inertial Reference System. Litton Systems, Inc. https://ntrs.nasa.gov/citations/19780031733
• Ebner, R. E., and W. E. Howell. 1979. “Design and Testing of a Redundant Skewed Inertial Sensor Complex for Integrated Navigation and Flight Control.” In AGARD The Guidance and Control of Helicopters and V(STOL Aircraft at Night and in Poor Visibility. https://ntrs.nasa.gov/citations/19790022031
• Ebner, R., and J. Mark. 1977. “Redundant Integrated Flight Control/navigation Inertial Sensor Complex.” In Guidance and Control Conference. AIAA 1977-1109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1109
• Eckstrom, C. 1975. “Evaluation of All-Parachute and Hybrid /Parachute-Retrorocket/ Recovery Systems for a One-Million-Pound Booster.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1392
• Edwards, Andrew. 1971. “The State of Strapdown Inertial Guidance and Navigation.” Navigation 18 (4): 386–401. https://doi.org/10.1002/j.2161-4296.1971.tb00110.x
• Edwards, A. A. 1975. “The Cost-Effectiveness of Inertial Navigation for Civil Aircraft.” Journal of Navigation 28 (3): 274–85. https://doi.org/10.1017/s0373463300041187
• Edwards, R. 1980. “Gravity Model Evaluation for Precise Terrestrial Inertial Navigation- a System Accuracy Approach.” In Guidance and Control Conference. AIAA 1980-1726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1726
• Edwards, F. G., and J. D. Foster. 1973. Flight Test Results from the CV990 Simulated Space Shuttle during Unpowered Automatic Approaches and Landings. NASA-TM-X-62285. NASA. https://ntrs.nasa.gov/citations/19730019021
• Edwards, F. G., J. D. Foster, D. M. Hegarty, D. W. Smith, F. J. Drinkwater III, and R. C. Wingrove. 1975. Flight Performance of a Navigation, Guidance, and Control System Concept for Automatic Approach and Landing of Space Shuttle Orbiter. NASA-TN-D-7899. NASA. https://ntrs.nasa.gov/citations/19750008540
• Effects of Array Error on SIAR Tracking Accuracy. 2014. Wiley. https://doi.org/10.1002/9781118609576.ch9
• “The Effects of Canard-Wing Flow-Field Interactions on Longitudinal Stability, Effective Dihedral and Potential Deep-Stall Trim.” 1988. In 6th Applied Aerodynamics Conference. AIAA 1988-2514. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2514
• Eftekhari, Malihe, Ali Siroueinejad, Mohammad Amin Nematollahi, and Mohammad Hosseini. 2025. “Unsteady Aerodynamic Heating and Nonlinear Panel Behavior in Supersonic Airflow.” Mechanics of Solids 60 (6): 5385–5400. https://doi.org/10.1134/s0025654425602496
• Egorov, D. A., and R. L. Novikov. 2023. “Studying the Temperature Dependency of h-Parameter of the Fiber-Optic Gyroscope Coil.” Gyroscopy and Navigation 14 (4): 411–16. https://doi.org/10.1134/s2075108724700123
• Eguchi, Hirofumi, Kazumitu Obana, and Masatoshi Kiso. 1999. “Standard Airframe Model for Missile Autopilot Design and Evaluation.” In Modeling and Simulation Technologies Conference and Exhibit. AIAA 1999-4322. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4322
• Eidell, Michael, Robert Nance, Gregory McGowan, James Carpenter, and Frankie Moore. 2012. “Computational Investigation of Roll Damping for Missile Configurations.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2904
• Einwoegerer, Walter, Hélio Koiti Kuga, and Paulo Giácomo Milani. 2010. “Navigation Using Low Cost Inertial Unit (IMU-MEMS) and GPS Receiver with Application of Sigma-Point Kalman Filter.” Journal of Aerospace Engineering, Sciences and Applications 2 (3): 20–28. https://doi.org/10.7446/jaesa.0203.03
• Eisenhut, D., R. Gates, and J. Kalley. 1971. “Ultra-High Accuracy Gimballed Star Tracker.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-963
• Eisenman, Allan Read, Carl Christian Liebe, John Lief Joergensen, and Gunnar Bent Jensen. 1997. (Abstract) Realization of a Faster, Cheaper, Better Mission and Its New Paradigm Star Tracker, the Advanced Stellar Compass. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20060036802
• Eisman, Mel. 1999. “Life Cycle Cost Impacts of Reusable Vehicles and Their Role in Space.” In Space Technology Conference and Exposition. AIAA 1999-4410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4410
• Ekaterinaris, John. 1994. “Computation of Flowfields over Missile Configurations.” In 12th Applied Aerodynamics Conference. AIAA 1994-1915. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1915
• Eklund, D. 2004. “Quicksat: A Two Stage to Orbit Reusable Launch Vehicle Utilizing Air Breathing Propulsion for Responsive Space Access.” In Space 2004 Conference and Exhibit. AIAA 2004-5950. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5950
• Eklund, Folke, and Sture Wickerts. 1968. “Wavelength Dependence of Microwave Propagation Far beyond the Radio Horizon.” Radio Science 3 (11): 1066–74. https://doi.org/10.1002/rds19683111066
• Ekvall, J., R. Rainen, D. Chellman, R. Flores, and M. Gersbach. 1989. “Elevated Temperature Aluminum Alloys for Advanced Fighter Aircraft.” In 30th Structures, Structural Dynamics and Materials Conference. AIAA 1989-1407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1407
• El Habiby, M. M., and M. G. Sideris. 2007. “A Wavelet Thresholding Technique for Local Geoid and Deflection of the Vertical Determination Using a Planar Approximation.” Geophysical Journal International 170 (2): 492–502. https://doi.org/10.1111/j.1365-246x.2007.03384.x
• El-Diasty, Mohammed, Ahmed El-Rabbany, and Spiros Pagiatakis. 2007. “An Accurate Nonlinear Stochastic Model for MEMS-Based Inertial Sensor Error with Wavelet Networks.” Journal of Applied Geodesy 1 (4). https://doi.org/10.1515/jag.2007.022
• El-Diasty, Mohammed, and Spiros D. Pagiatakis. 2008. “Calibration and Stochastic Modelling of Inertial Navigation Sensor Erros.” Journal of Global Positioning Systems 7 (2): 170–82. https://doi.org/10.5081/jgps.7.2.170
• El-gabri , A. N Ouda, A. R. 2018. “Command Guidance Missile Tracking Algorithms Evaluation Based on Visual Simulation.” International Journal of Engineering Research and V7 (08). https://doi.org/10.17577/ijertv7is080043
• El-Sayed, Ahmed F. 2026. “Turbojet Engine.” In Aircraft and Rocket Propulsion and Gas Turbine Engines. CRC Press. https://doi.org/10.1201/9781003561538-5
• El-Sheikh, Gamal. 1998. “Autopilot Design for a Beam Rider Guided Missile System.” International Conference on Electrical Engineering 1 (1): 401–9. https://doi.org/10.21608/iceeng.1998.61097
• Elahian, samaneh, M. A. Amiri Atashgah, and Bahram Tarverdizadeh. 2024. “Enhancing Autonomous Navigation in GNSS-Denied Environments: Integrating Collision Avoidance with Observability-Based Motion Planning.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4407556/v1
• Electrical Engineering, NIT, Agartala, India) and Manish Debnath. 2016. “Protection of Inter-Continental Ballistic Missile (ICBM) from Anti-Ballistic Missile (ABM) by Using Anti-Anti-Ballistic Missile (AABM).” International Journal Of Engineering And Computer Science. https://doi.org/10.18535/ijecs/v5i8.40
• Elgin, Stephen D., and Thomas J. Sutliff. 1993. Structural Dynamic Testing of Composite Propfan Blades for a Cruise Missile Wind Tunnel Model. NASA-TM-105272. NASA. https://ntrs.nasa.gov/citations/19930009686
• Elias, Antonio L., and Martin A. Knutson. 1995. “Pegasus Air-Launched Space Booster Flight Test Program.” In AGARD, Space Systems Design and Development Testing. https://ntrs.nasa.gov/citations/19960003894
• Elliott, G. L., and R. Weller. 1954. “Some Navigation Problems at a Guided Missile Range.” Navigation 4 (4): 145–51. https://doi.org/10.1002/j.2161-4296.1954.tb00148.x
• Ellison, J. C. 1977. Supersonic Longitudinal Aerodynamic Characteristics of Two Space Shuttle Orbiter Configurations. NASA-TM-74074. NASA. https://ntrs.nasa.gov/citations/19780004088
• Elmelhi, Ali Mohamed. 2013. “Neural Networks Autopilot Design for Ballistic Missile.” Journal of Engineering Research (Libya) 18: 1–16. https://doi.org/10.66411/jer.v18i.256
• Elrod, W., and J. Durniak. 1981. “Hydrogen Fueled Catalytic Combustion for Low Thrust Expendable Turbojet Engine.” In Aircraft Systems and Technology Conference. AIAA 1981-1715. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1715
• Elvin, John D. 1996. “Lockheed Martin Approach to a Reusable Launch Vehicle (RLV).” In AIP Conference Proceedings, vol. 361. AIP. https://doi.org/10.1063/1.49950
• Elwell, John. 1991. “Progress on Micromechanical Inertial Instruments.” In Navigation and Control Conference. AIAA 1991-2765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2765
• Emadzadeh, Amir Abbas, and Jason Lee Speyer. 2011. “Celestial-Based Navigation: An Overview.” In Navigation in Space by X-ray Pulsars. Springer New York. https://doi.org/10.1007/978-1-4419-8017-5_2
• Emel’yantsev, G. I., B. A. Blazhnov, and A. P. Stepanov. 2015. “Vertical Deflection Determination in High Latitudes Using Precision IMU and Two-Antenna GNSS System.” Gyroscopy and Navigation 6 (4): 305–9. https://doi.org/10.1134/s2075108715040057
• Eminton, E., and W. T. Lord. 1956. “Note on the Numerical Evaluation of the Wave Drag of Smooth Slender Bodies Using Optimum Area Distributions for Minimum Wave Drag.” Journal of the Royal Aeronautical Society 60 (541): 61–63. https://doi.org/10.1017/s0368393100132407
• Emmons, H. T., D. L. Norwood, J. E. Rasmusen, and H. E. Reynolds. 1977. Ramjet Cost Estimating Handbook. DTIC_ADA054856. Vought Corp. https://ntrs.nasa.gov/citations/19790021017
• Engel, C. D., and J. K. Lapointe. 1979. Aerodynamic Heating to Representative SRB and ET Protuberances. NASA-CR-161198. NASA. https://ntrs.nasa.gov/citations/19790012833
• Engel, C. D., J. E. Reardon, and C. E. Fuller. 1974. Booster Aerodynamic Heating: Test Support. NASA-CR-120234. NASA. https://ntrs.nasa.gov/citations/19740017428
• Engelbrecht, E. Geoffrey, Vasilis G. Gkoutzamanis, Christos P. Nasoulis, and Anestis I. Kalfas. 2022. “Inlet Flow Distortion Dependencies for Tail Mounted Ducted Fans on Hybrid-Electric Commuter Aircraft.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2022-80894
• Engelstad, Sean P., Brian J. Burke, Rohan N. Patel, Sejal Sahu, and Graeme J. Kennedy. 2023. “High-Fidelity Aerothermoelastic Optimization with Differentiable CAD Geometry.” In AIAA SCITECH 2023 Forum. AIAA 2023-0329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0329
• Engine Inlet, Exhaust, and Nacelle Systems. 2011. Wiley. https://doi.org/10.1002/9781119975489.ch6
• Englert, Gerald W., Donald J. Vargo, and Robert W. Cubbison. 1954. Effect of Jet-Nozzle-Expansion Ratio on Drag of Parabolic Afterbodies. NACA-RM-E54B12. NASA. https://ntrs.nasa.gov/citations/19930088172
• English, Robert E., and Richard H. Cavicchi. 1954. Analysis of off-Design Operation of High Mach Number Supersonic Turbojet Engines. NACA-RM-E53J01. NASA. https://ntrs.nasa.gov/citations/19930088030
• Enright, John J. 1985. “Laboratory Simulation of Landing Gear Pitch-Plane Dynamics.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/851937
• Enright, John. 2000. “Reducing Aircraft Brake Squeal with a Damped Brake-Rod.” In 2000 World Aviation Conference. AIAA 2000-5599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5599
• “Equations of Motion with General Gravity Model.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0153.0178
• Equipment to Simulate Aerodynamic Heating and Acoustical Environments on Space Shuttle Thermal Protection System Specimens, Instruction Manual. 1971. NASA-CR-103017. NASA. https://ntrs.nasa.gov/citations/19710007976
• Er-El, J. 1983. “The Leading-Edge Vortex Trajectories of Close-Coupled Wing-Canard Configurations and Their Breakdown Characteristics.” In Applied Aerodynamics Conference. AIAA 1983-1817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1817
• Eremenko, Paul, Christopher Mouton, and Hans Hornung. 2003. “The Wave Drag of Blunted Cones in Axisymmetric Supersonic Flow.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1269
• Erickson, Gary, John Schreiner, and Lawrence Rogers. 1990. “Canard-Wing Vortex Interactions at Subsonic through Supersonic Speeds.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2814
• Ericsson, L. 1980. “Viscous Effects on Missile Aerodynamics at Low Angles of Attack.” In 13th Fluid and PlasmaDynamics Conference. AIAA 1980-1378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1378
• Ericsson, L., B. Almroth, and J. Bailie. 1978. “Hypersonic Aerothermoelastic Characteristics of a Finned Missile.” In 16th Aerospace Sciences Meeting. AIAA 1978-231. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-231
• Ericsson, L., and J. Reding. 1974. “High Attitude Delta Wing Unsteady Aerodynamics.” In Mechanics and Control of Flight Conference. AIAA 1974-817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-817
• Eriksson, L. 1984. “Development of a Supersonic Turbine Stage for the HM60 Engine.” In 20th Joint Propulsion Conference. AIAA 1984-1464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1464
• Ermakov, Pavel, and Alexander Gogolev. 2021. “Comparative Analysis of Information Integration Architectures of Strapdown Inertial Navigation Systems for Unmanned Aerial Vehicles.” Trudy MAI, no. 117. https://doi.org/10.34759/trd-2021-117-11
• Ermakov, P., and A. Gogolev. 2022. “Comparative Analysis of Information Integration Schemes Sterile Inertial Navigation Systems for Unmanned Vehicles Aircraft.” East European Scientific Journal 3 (12(76)): 25–36. https://doi.org/10.31618/essa.2782-1994.2021.3.76.213
• Erzberger, H. 1967. Application of Kalman Filtering to Error Correction of Inertial Navigators. NASA-TN-D-3874. NASA. https://ntrs.nasa.gov/citations/19670008470
• “ESDU Data Item Estimates Fin Effect on Base Drag at Supersonic Speeds.” 1998. Aircraft Engineering and Aerospace Technology 70 (6). https://doi.org/10.1108/aeat.1998.12770fab.033
• Esenwein, Fred T. 1952. Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane III: Normal Wedge Inlet with Semicircular Cowl. NACA-RM-E52H20. NASA. https://ntrs.nasa.gov/citations/19930087252
• Esenwein, Fred T., and Carl F. Schueller. 1952. Analytical and Experimental Investigation of Inlet-Engine Matching for Turbojet-Powered Aircraft at Mach Numbers up to 2.0. NACA-RM-E51K20. NASA. https://ntrs.nasa.gov/citations/19930087893
• Esmaeilkhah, Ahmad, and Rene Jr Landry. 2025. “Estimation of the Effect of Single Source of RF Interference on an Airborne Global Navigation Satellite System Receiver: A Theoretical Study and Parametric Simulation.” In European Navigation Conference 2024. MDPI. https://doi.org/10.3390/engproc2025088053
• Est, Brian, and H. Nelson. 1991. “Fin Dihedral Effects on Aerodynamics of Supersonic Missiles with Square and Triangular Fuselage Cross Sections.” In 9th Applied Aerodynamics Conference. AIAA 1991-3256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3256
• Ettl, Josef, Dong Kim, Alexander P. Schmidt, and John Turner. 2016. “Using Data Fusion of DMARS-R-IMU and GPS Data for Improving Attitude Determination Accuracy.” In SpaceOps 2016 Conference. AIAA 2016-2637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2637
• Etzkorn, Letha. 2001. CORBA Support for Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada401028
• Eubank, H. A., C. C. Ross, and R. C. Stiff. 1955. “Some Aspects of Guided Missile Power-Plant Reliability Requirements.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/550065
• “Evaluation of Gravity Model Error Effects.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0291.0304
• Evans, Albert J. 1954. The Zero-Lift Drag of a Slender Body of Revolution (NACA RM-10 Research Model) as Determined from Tests in Several Wind Tunnels and in Flight at Supersonic Speeds. NACA-TR-1160. NASA. https://ntrs.nasa.gov/citations/19930092188
• Evans, G. C. 1966. “Influence of Ground Reflections on Radar Target-Tracking Accuracy.” Proceedings of the Institution of Electrical Engineers 113 (8): 1281. https://doi.org/10.1049/piee.1966.0216
• Evans, Parker, Mark Carpenter, and Roy Hartfield. 2026. “Unsupervised Clustering of Solid Propellant Missile Systems Using Performance Parameters and Telemetry Data.” In AIAA SCITECH 2026 Forum. AIAA 2026-0753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0753
• Evans, M., Z. Govindarajulu, and J. Barthoulot. 1985. Estimates of Circular Error Probabilities. Defense Technical Information Center. https://doi.org/10.21236/ada163257
• Evans, F., and J. Wilcox. 1969. “Experimental Strapdown Redundant Sensor Inertial Navigation System.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-851. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-851
• Evans, F. A., and J. C. Wilcox. 1970. Experimental Strapdown Redundant Sensor Inertial Navigation System. AIAA PAPER 69-851. NASA. https://ntrs.nasa.gov/citations/19700065742
• Evduzen, Rasit. 2026. “Gimballed Stable-Platform Seeker: Line-of-Sight Rate Estimation via Pixel-Plane Kalman Filtering and Gimbal-Mounted Gyro Fusion.” Preprint, . https://doi.org/10.31224/7653
• Eves, Kameron J., and John Valasek. 2024. “Inlet Unstart Prevention by Adaptive Regulation Using a Nonlinear Longitudinal Timescale Model.” In AIAA SCITECH 2024 Forum. AIAA 2024-2874. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2874
• “An Experimental Study on Air Intake Performance for a Rocket/ramjet Engine.” 1981. In 17th Joint Propulsion Conference. AIAA 1981-1488. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1488
• “Extension of a Portable Tactical Instrument Approach and Landing System.” 1972. Aircraft Engineering and Aerospace Technology 44 (11): 26–29. https://doi.org/10.1108/eb034962
• “External Autoignition Test for Simulating Flight Aeroheating of Staging Rocket Motor.” 1986. In 22nd Joint Propulsion Conference. AIAA 1986-1578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1578
• Ezekiel, Shaoul. 1980. Passive Ring Resonator Laser Gyroscope. Defense Technical Information Center. https://doi.org/10.21236/ada081649
• Ezekiel, S., and S. R. Balsamo. 1977. “Passive Ring Resonator Laser Gyroscope.” Applied Physics Letters 30 (9): 478–80. https://doi.org/10.1063/1.89455
• Ezrokhi, Yury, Daniil Fokin, and Pavel Nyagin. 2020. “Mathematical Modelling Application for Characteristics Estimation of Bypass Turbojet with Common Afterburner.” Vestnik Moskovskogo aviatsionnogo instituta 27 (2): 99–111. https://doi.org/10.34759/vst-2020-2-99-111
• Facinelli, William, and Oran Nicks. 1995. “Tests of Reaction Jets on a Scale Model of a Subsonic Missile.” In 13th Applied Aerodynamics Conference. AIAA 1995-1867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1867
• Fadaki, Mohammad Saber, Hamid Reza Koofigar, Mohsen Ekramian, and Mahdi Mortazavi. 2023. “A Switched Adaptive Strategy for State Estimation in MEMS-Based Inertial Navigation Systems with Application for a Flight Test.” Journal of Navigation 76 (6): 709–30. https://doi.org/10.1017/s0373463324000079
• Fairbairn, G. 1964. “Structural Materials for Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-628. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-628
• Fairbank, William M. 1983. Background Information on the He(3) Nuclear Gyroscope. Defense Technical Information Center. https://doi.org/10.21236/ada130755
• Fairfax, Luisa, Frank Fresconi, and Mark Costello. 2011. “Affordable State Estimation Using Inertial Navigation Sensor Arrays.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6267
• Falkiewicz, Nathan, and Carlos Cesnik. 2010. “Proper Orthogonal Decomposition for Reduced-Order Thermal Solution in Hypersonic Aerothermoelastic Simulations.” In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th. AIAA 2010-2798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-2798
• Falkiewicz, Nathan, and Carlos Cesnik. 2011a. “Enhanced Modal Solutions for Structural Dynamics in Aerothermoelastic Analysis.” In 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2011-1963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1963
• Falkiewicz, Nathan, Carlos Cesnik, Andrew Crowell, and Jack McNamara. 2010. “Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7928
• Fallon, William, and Lester Lyles. 2011. Science and Technology Issues of Early Intercept Ballistic Missile Defense Feasibility. Defense Technical Information Center. https://doi.org/10.21236/ada552472
• Fallon, Edward, II, Anthony Taylor, and Robert Meyerson. 1999. “Landing System Design Summary of the K-1 Reusable Launch Vehicle.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1720. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1720
• Falunin, M. P., and G. S. Ul’yanov. 1967. “Delta Wing in Supersonic Flow.” Fluid Dynamics 2 (6): 94–99. https://doi.org/10.1007/bf01013724
• Fan, Wuyang, Song Fu, and Shisheng Zhong. 2024. “Gyroscope in-Assembly Drift Anomaly Detection Based on Decision Re-Optimized Deep Auto-Encoder.” Measurement Science and Technology 36 (1): 016136. https://doi.org/10.1088/1361-6501/ad86de
• Fan, Wenfeng, Wei Quan, Feng Liu, Lihong Duan, and Gang Liu. 2019b. “Low Drift Nuclear Spin Gyroscope with Probe Light Intensity Error Suppression.” Chinese Physics B 28 (11): 110701. https://doi.org/10.1088/1674-1056/ab44a5
• Fan, Huiying, Kaiwen Tian, Guangxin Cheng, Zhuangzhuang Dong, and Xudong Yu. 2022. “Error Characteristic Analysis of Tri-Axis Rotating Optical Gyro Inertial Navigation System Based on Inertial Frame.” In Springer Proceedings in Physics. Springer Nature Singapore. https://doi.org/10.1007/978-981-16-7258-3_39
• Fan, Yue, and Wei Wang. 2016. “Experimental Study of Resonance Fiber Optic Gyroscope Employing a Dual-Ring Resonator.” In SPIE Proceedings, vol. 9684, edited by Yudong Zhang, Fan Wu, Ming Xu, Sandy To. SPIE. https://doi.org/10.1117/12.2243252
• Fan, Yonghua, Xiaofei Wu, Hongyang Xu, and Fan Wang. 2017a. “Design of Lateral Control System for a Hypersonic Cruise Missile.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2111
• Fang, Aiqing. 1995. Passive Terrain Following (TF) Systems Composed of Digital Mapping and GPS,. Defense Technical Information Center. https://doi.org/10.21236/ada300498
• Fang, Boyang, and Xiaoqing Qiang. 2022. “Design of Aircraft Engine Inlet Radial Distortion Generator.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-16-8154-7_14
• Farahmandi, Alireza, and Brian Reitz. 2024. “Predictive Cost Adaptive Control of a Planar Missile with Unmodeled Aerodynamics.” In AIAA SCITECH 2024 Forum. AIAA 2024-2218. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2218
• Farazian, John, Rob McEwen, and Rick Todd. 1996. “MSTI3 Star Tracker Attitude Determination and Estimation Algorithm.” In Guidance, Navigation, and Control Conference. AIAA 1996-3749. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3749
• Farr, A. 1973. “Evaluation of F-15 Inlet Dynamic Distortion.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-784
• Farrar, R. 1968. “High Density Fuel to Extend Range of Ramjet Missile.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-632
• Farrell, James. 1966. “Performance of Strapdown Inertial Attitude Reference Systems.” In Guidance and Control Conference. AIAA 1966-1802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1802
• Farrell, E. 1968. “Alignment Processing Techniques for Strapdown Inertial Guidance Systems.” In Control and Flight Dynamics Conference. AIAA 1968-829. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-829
• Farrell, James L. 2007. “Inertial Instrument Error Characterization.” Navigation 54 (3): 169–76. https://doi.org/10.1002/j.2161-4296.2007.tb00402.x
• Farrior, J. S. 1962. Inertial Guidance, Its Evolution and Future Potential. Lockheed Missiles and Space Co. https://ntrs.nasa.gov/citations/19630006118
• Faruqi, Farhan. 2012. “Intelligent 3-Party Game Theoretic Approach to Missile Guidance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4911
• Fashuyi, M. O., and T. J. Afullo. 2007. “Rain Attenuation Prediction and Modeling for Line-of-Sight Links on Terrestrial Paths in South Africa.” Radio Science 42 (5): 2007RS003618. https://doi.org/10.1029/2007rs003618
• Faulders, C., E. Lekawa, and R. McNary. 1967. “Aerodynamic Requirements for Flare and Landing of Low-L/D Glide Vehicles.” In Control and Flight Dynamics Conference. AIAA 1967-575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-575
• Faulkner, Frank D. 1961. Optimum Interception of a Ballistic Missile at Intermediate Range. Defense Technical Information Center. https://doi.org/10.21236/ad0265426
• Faulkner, Frank D., and Edward N. Ward. 1961. Optimum Interception of a Ballistic Missile at Moderate Range. Defense Technical Information Center. https://doi.org/10.21236/ad0266582
• Faulstich, Raymond, and Eugene Law. 2006. Test Methods for Telemetry Systems and Subsystems. Volume 1. Test Methods for Vehicle Telemetry Systems. Defense Technical Information Center. https://doi.org/10.21236/ada619554
• Fawcett, P., R. Funk, and N. Komerath. 1992. “Quantification of Canard and Wing Interactions Using Spatial Correlation Velocimetry.” In 10th Applied Aerodynamics Conference. AIAA 1992-2687. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2687
• Fearnside, K. 1959. “Instrumental and Automatic Control for Approach and Landing.” Journal of Navigation 12 (1): 66–83. https://doi.org/10.1017/s0373463300045859
• Feasibility Study of Scanning Celestial Attitude System (SCADS) for Earth Resources Technology Satellite (ERTS). 1971. NASA-CR-122361. NASA. https://ntrs.nasa.gov/citations/19720011007
• Feasibility Study of the Superconducting Gravity Gradiometer (SGG) Flight Test on the European Retrievable Carrier (EURECA). 1991. NASA-CR-184157. NASA. https://ntrs.nasa.gov/citations/19910013916
• Feather, J. B., and B. K. Craven. 1991. Microwave Landing System Autoland System Analysis. NASA-CR-189551. NASA. https://ntrs.nasa.gov/citations/19920005842
• “Feature Selection Criterion for Gravity Matching Navigation.” 2016. International Journal of Science and Research (IJSR) 5 (2): 1643–47. https://doi.org/10.21275/v5i2.nov161554
• Fedorov, Volodymyr, Vladislav Kikot, and Nataliya Shtefan. 2020. “On Using the Rotor Acceleration Mode to Increase the Accuracy of a Two-Stage Gyrocompass.” Mechanics of Gyroscopic Systems, no. 39: 5–13. https://doi.org/10.20535/0203-3771392020229091
• Fegley, K. A. 1965. Gimballess Inertial Navigation Systems. Semi- Annual Progress Report, 1 Nov. 1964: 30 Apr. 1965. NASA-CR-63474. NASA. https://ntrs.nasa.gov/citations/19650018044
• Fegley, K. A. 1967. Gimballess Inertial Navigation Systems Final Report, Nov. 1, 1966: Apr. 30, 1967. NASA-CR-90222. NASA. https://ntrs.nasa.gov/citations/19680001596
• Fehr, T., D. Fosth, and R. McDonald. 1972. “High Accuracy Approach Guidance System for Outer Planet Exploration.” In Guidance and Control Conference. AIAA 1972-867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-867
• Feifel, Winfried, and Benjamin Kerkam. 1992. “Propulsion/airframe Requirements and Optimization for a Joint Service Cruise Missile Concept.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-82. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-82
• Feistel, T. W. 1985. Interdependence of Parameters Important to the Design of Subsonic Canard-Configured Aircraft. SAE PAPER 850865. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19860053768
• Feld, Denis J. 1990. “An Analytical Investigation of Damping of Landing Gear Shimmy.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/902015
• Feldman, J. 1974. Standardized Strapdown Inertial Component Modularity Study, Volume 2. NASA-CR-120428. NASA. https://ntrs.nasa.gov/citations/19740023987
• Felikson, Denis, Matthew Ekinci, Joseph Hashmall, and Melissa Vess. 2011. “On-Orbit Solar Dynamics Observatory (SDO) Star Tracker Warm Pixel Analysis.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6728. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6728
• Fell, C. P. 2006. “Development of a Second Generation Low Cost MEMS Gyroscope: Design for Manufacture.” In IET Seminar on MEMS Sensors and Actuators, vol. 2006. IEE. https://doi.org/10.1049/ic:20060448
• Fellerhoff, J. R. 1988. AFTI/SITAN (Advanced Fighter Technology Integration/Sandia Inertial Terrain-Aided Navigation) Final Report. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/6873200
• Feng, Z. C. 2000. “A Nonlinear Dynamics Model of a Microelectromechanical Vibrating Wheel Gyroscope.” In Micro-Electro-Mechanical Systems (MEMS). American Society of Mechanical Engineers. https://doi.org/10.1115/imece2000-1113
• Feng, Peide, and James C. Hung. 1985. “Gyrocompassing on a Moving Land Vehicle.” SIMULATION 44 (3): 144–47. https://doi.org/10.1177/003754978504400305
• Feng, Shaoxin, and Yasheng Zhang. 2016. “Analysis of near Space Hypersonic Glide Vehicle Trajectory Characteristics and Defense Difficulties.” In Proceedings of the 2016 5th International Conference on Advanced Materials and Computer Science. Atlantis Press. https://doi.org/10.2991/icamcs-16.2016.138
• Feng, Changkun, Yonggui Zhang, Honghao Ma, Hui Li, and Lishuang Feng. 2022. “Improving Long-Term Temperature Bias Stability of an Integrated Optical Gyroscope Employing a Si3N4 Resonator.” Photonics Research 10 (7): 1661. https://doi.org/10.1364/prj.456321
• Fenwick, E. B. 1966. XV5A Aircraft Flight Tests Landing Strip Evaluations. Defense Technical Information Center. https://doi.org/10.21236/ad0737274
• Fenwick, William B. 1967. XC-142A Aircraft Flight Tests Landing Strip Evaluations. Defense Technical Information Center. https://doi.org/10.21236/ad0738376
• Fernandes Pereira de Lima, Sâmela, and Carlos Souto. 2021. “Transverse Vibrations of a Turbojet Rotor Subjected to Cruise Missile Flight Maneuvers.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-0757
• Fernandez, Rene, Charles J. Trefny, Scott R. Thomas, and Mel J. Bulman. 2001. Parametric Data from a Wind Tunnel Test on a Rocket-Based Combined-Cycle Engine Inlet. NASA/TM-2001-107181. NASA. https://ntrs.nasa.gov/citations/20020006304
• “Ferranti’s Lightweight Inertial Platform: A Description of the Lightweight Inertial Platform Produced by Ferranti Ltd. for Use with the Ferranti Lightweight Inertial Navigation System and as a Reference System for Aircraft, Space Vehicles and Ships.” 1964. Aircraft Engineering and Aerospace Technology 36 (11): 356–58. https://doi.org/10.1108/eb033945
• Ferreres, G., and M. M’Saad. 1995. “H∞ Design of a Multivariable Missile Autopilot Using Coprime Factors.” In Automatic Control in Aerospace 1994 (Aerospace Control ‘94). Elsevier. https://doi.org/10.1016/b978-0-08-042238-1.50024-0
• Ferri, Antonio, and Louis M. Nucci. 1951. Preliminary Investigation of a New Type of Supersonic Inlet. NACA-TN-2286. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930083137
• Ferrier, Bernard, Robert Ernst, and Ajay Sehgal. 2015. “Instrumented Deck Landing Cueing in Unmanned Aircraft Systems.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0071-2015-10296
• Fesenko, O., V. Ostapchuk, and R. Bieliakov. 2023. “Analysis of Navigation System Accuracy Characteristics for Micro UAVs.” Communication, informatization and cybersecurity systems and technologies 3 (3). https://doi.org/10.58254/viti.3.2023.15.128
• Fetahi, Kaleab, Sharanabasaweshwara Asundi, Arthur Taylor, Syed F. Ali, and Adem Ibrahim. 2020. “Parametric Study of a Turbojet Engine with Auxiliary Bypass Combustion – the TurboAux Engine.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3709. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3709
• Ficarrotta, Mike. 2001. “Integration of the GPS-Based Ballistic Missile Range Tracking System.” In AIAA Space 2001 Conference and Exposition. AIAA 2001-4547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4547
• Fields, Travis, Jeffrey LaCombe, and Eric Wang. 2011. “One Degree of Freedom Approach for an Autonomous Descent Vehicle Using a Variable Drag Parachute.” In 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2011-2518. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2518
• Filinov, Evgeny, and Kristina Bezborodova. 2021. “Double Bypass Turbojet Engine Structure Analysis.” Vestnik Moskovskogo aviatsionnogo instituta 28 (3): 159–70. https://doi.org/10.34759/vst-2021-2-159-170
• Filipovic, Z., and G. Dikic. 2011. “Design and Implementation of PCM/FM Telemetry Systems for Aircraft and Missile Testing during Flight Test Procedure.” International Conference on Aerospace Sciences and Aviation Technology 14 (AEROSPACE SCIENCES): 1–15. https://doi.org/10.21608/asat.2011.23257
• Finch, Robert Bruce. n.d. “Smoothing for Delayed State Model with Applications to Aided Inertial Navigation Systems.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180815-3743
• Fink, M., and W. Anderson. 1982. “Axisymmetric Nose Inlet Effects on Supersonic Missile Airloads.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1302. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1302
• Finneran, W., and J. Stanely. 1969. LASL RADIO COMMAND SYSTEM, TYPE SY-199. Technical Manual Number B-4041. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4721502
• Finney, Greg, Stephen Fox, Bijan Nemati, and Patrick Reardon. 2023. “Extremely Accurate Star Tracker for Celestial Navigation.” In AMOS 2023 Technical Papers. AMOS Conference. https://doi.org/10.64861/shkj5077
• Fischenberg, D. 1995. “Identification of an Unsteady Aerodynamic Stall Model from Flight Test Data.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3438
• Fischer, D. 1981. “Comparison of Model Testing with Computer Simulations of an Air Landing System.” In Aircraft Systems and Technology Conference. AIAA 1981-1663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1663
• Fischer, Sylvain, Patrick Meyrueis, and Werner W. Schroeder. 1995. “Brillouin Backscattering in Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 2510, edited by Ramon P. DePaula, John W. Berthold III. SPIE. https://doi.org/10.1117/12.221717
• Fischer, W. W., and R. H. Norris. 1949a. “Closure to “Discussion of ‘Supersonic Convective Heat-Transfer Correlation from Skin-Temperature Measurements on a V-2 Rocket in Flight’” (1949, Trans. ASME, 71, p. 467).” Journal of Fluids Engineering 71 (5): 467–69. https://doi.org/10.1115/1.4017112
• Fischer, W. W., and R. H. Norris. 1949b. “Supersonic Convective Heat-Transfer Correlation from Skin-Temperature Measurements on a V-2 Rocket in Flight.” Journal of Fluids Engineering 71 (5): 457–67. https://doi.org/10.1115/1.4017110
• Fischetti, T. L., and R. T. Whitcomb. 1953. Development of a Supersonic Area Rule and an Application to the Design of a Wing-Body Combination Having High Lift-to-Drag Ratios. NACA-RM-L53H31A. NASA. https://ntrs.nasa.gov/citations/19650077235
• Fischler, J. E. 1981. “Opportunities for Structural Improvements for an Advanced Supersonic Transport Vehicle.” In NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2. https://ntrs.nasa.gov/citations/19810009484
• Fisher, Franklin M. 1961. “Identifiability Criteria in Nonlinear Systems.” Econometrica 29 (4): 574. https://doi.org/10.2307/1911805
• Fisher, Jeff. 1996. “Orbital Gyrocompassing with Yaw Maneuvers.” In Guidance, Navigation, and Control Conference. AIAA 1996-3750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3750
• Fisher, B. D., P. L. Deal, R. A. Champine, and J. M. Patton Jr. 1979. Flight Investigation of Piloting Techniques and Crosswind Limitations Using a Research Type Crosswind Landing Gear. NASA-TP-1423. NASA. https://ntrs.nasa.gov/citations/19790014841
• Fisher, B. D., R. K. Sleeper, and S. M. Stubbs. 1978. Summary of NASA Landing-Gear Research. NASA-TM-78679. NASA. https://ntrs.nasa.gov/citations/19780018105
• Fite, E. Brian. 1993. Fabrication of Composite Propfan Blades for a Cruise Missile Wind Tunnel Model. NASA-TM-105270. NASA. https://ntrs.nasa.gov/citations/19930017013
• Fitzgerald, W., and M. Shapanka. 1979. “An Azimuth Verification Technique for an Advanced Inertial Reference Sphere.” In Guidance and Control Conference. AIAA 1979-1890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1890
• Fitzsimmons, Jeff. 1996. “Cost Analysis of a DC-X Reusable Launch Vehicle: Is It Affordable?” In Space Programs and Technologies Conference. AIAA 1996-4414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4414
• Flaherty, J. 1977. “Experimental and Analytical Investigations of High Angle of Attack Missile Aerodynamics.” In Guidance and Control Conference. AIAA 1977-1156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1156
• Flaherty, J. 1979. “An Analysis of High Angle of Attack Missile Aerodynamics at Subsonic Flow Mach Numbers.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1648
• Flanagan, M. J., Jr. 1993. “Aerodynamic Heating in the Vicinity of Hypersonic, Axisymmetric, Shock-Wave Boundary-Layer Interactions.” In AIAA. https://ntrs.nasa.gov/citations/19930062515
• Flanders, T. 1970. “The Inlet/engine Control Vector.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-696
• Flayac, Emilien. n.d. “Coupled Methods of Nonlinear Estimation and Control Applicable to Terrain-Aided Navigation.” PhD diss., Université Paris-Saclay (ComUE). https://doi.org/10.70675/ef4a7d4az117bz4e1ezab44z35a5bae960e7
• Fleck, T. 1983. “Interactive Real-Time Data Displays for Flying the Cruise Missile.” In 2nd Flight Testing Conference. AIAA 1983-2731. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2731
• Fleeter, S., R. McClure, G. Sinnet, and R. Holtman. 1974. “A Unique Supersonic Inlet Unsteady Aerodynamic Cascade Experiment.” In 8th Aerodynamic Testing Conference. AIAA 1974-622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-622
• Fleming, William A. 1953. Internal Performance of Several Types of Jet-Exit Configurations for Supersonic Turbojet Aircraft. NACA-RM-E52K04. NASA. https://ntrs.nasa.gov/citations/19930087367
• Fleming, W. A., D. S. Gabriel, and B. T. Lundin. 1956. Effect of Operating Conditions and Design on Afterburner Performance. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19670095388
• “Flight Engine Performance Evaluation for the Air-Launched Cruise Missile.” 1977. In Aircraft Systems and Technology Meeting. AIAA 1977-1201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1201
• “Flight Test Programme.” 1970. Aircraft Engineering and Aerospace Technology 42 (4): 25–32. https://doi.org/10.1108/eb034622
• Florio, Brendan James, Robert McKibbin, Calum Braham, John Ockendon, and Colin Please. 2019. “Estimating Transonic Drag.” ANZIAM Journal 59: 1. https://doi.org/10.21914/anziamj.v59i0.13408
• “Flying Controls and Automatic Landing: Details of the Primary Control Surfaces Which Are Aerodynamically Similar to Those of the Bristol Britannia, and a Description of the Smiths Automatic Flight Control System Mark 29.” 1963. Aircraft Engineering and Aerospace Technology 35 (9): 275–78. https://doi.org/10.1108/eb033786
• Follé, M. I. 1983. “Wave Drag of Slender Star-Shaped Bodies at Moderate Supersonic Flight Velocities.” Fluid Dynamics 18 (5): 783–88. https://doi.org/10.1007/bf01091003
• Folta, David, Cheryl Gramling, Dominic Leung, Sheela Belur, and Anne Long. 1999. Autonomous Navigation Using Celestial Objects. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/19990103599
• Fomichev, A. V. 2025. “Estimation and Compensation of Strapdown Inertial Navigation System Errors Caused by Inertial Sensor Delays.” Gyroscopy and Navigation 16 (2): 115–25. https://doi.org/10.1134/s2075108725700166
• Fomichev, A. V., and E. K. Li. 2017. “Accuracy Analysis of the Analytical Solution for the Lunar Lander Terminal Guidance Problem.” Mehatronika, Avtomatizacia, Upravlenie 18 (7): 484–92. https://doi.org/10.17587/mau.18.484-492
• Fontan Moura, Augusto. n.d. “Investigation of Supersonic Turbulent Combustion in a Mach 10 Scramjet Engine.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2019.413
• Forkun, I., D. Medzatyi, D. Makaryshkin, and О. Chervonetskii. 2020. “Automatic Control System for an Unmanned Aircraft Based on a Kalman Filter.” Herald of Khmelnytskyi National University. Technical sciences 289 (5): 57–64. https://doi.org/10.31891/2307-5732-2020-289-5-57-64
• Forlifer, W. R., R. P. Gaston Jr., and R. L. Hopping. 1967. Landing Gear Patent. Patent Number: NASA-CASE-XMF-01174. Martin Marietta Corp. https://ntrs.nasa.gov/citations/19700032273
• Fornasier, Luciano, and Stefan Heiss. 1987. “Application of HISSS Panel Code to a Fighter-Type Aircraft Configuration at Subsonic and Supersonic Speeds.” In 5th Applied Aerodynamics Conference. AIAA 1987-2619. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2619
• Forner, J., and J. Manter. 1982. “Prediction of Cruise Missile Inlet Peak Instantaneous Distortion Patterns from Steady State and Turbulence Data Using a Statistical Technique.” In 18th Joint Propulsion Conference. AIAA 1982-1085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1085
• Forsberg, Rene. 1984. A Study of Terrain Reductions, Density Anomalies and Geophysical Inversion Methods in Gravity Field Modelling. Defense Technical Information Center. https://doi.org/10.21236/ada150788
• Fortenbaugh, R. 1972. “Practical Integration of Direct Lift Control into an Automatic Carrier Landing System.” In Guidance and Control Conference. AIAA 1972-873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-873
• Forward, R. L. 1976. Rotating Gravity Gradiometer Study. NASA-CR-149800. NASA. https://ntrs.nasa.gov/citations/19770012442
• Forward, R. L. 1982. Rotating Gravity Gradiometer Study. NASA-CR-169440. NASA. https://ntrs.nasa.gov/citations/19830002134
• Forward, R. L., C. C. Bell, P. M. Lahue, E. F. Mallove, and D. W. Rouse. 1973. Development of a Rotating Gravity Gradiometer for Earth Orbit Applications (AAFE). NASA-CR-112215. NASA. https://ntrs.nasa.gov/citations/19730023608
• Fosbury, Adam, and John Crassidis. 2006. “Kalman Filtering for Relative Inertial Navigation of Uninhabited Air Vehicles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6544
• Foster, G. V. 1959a. Effects of Wing Vertical Location on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a Trapezoidal ASPECT-RATIO-3 Wing. NASA-TM-X-44. NASA. https://ntrs.nasa.gov/citations/19630002675
• Foster, G. V. 1959b. Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01. NASA-TM-X-134. NASA. https://ntrs.nasa.gov/citations/19670022204
• Foster, J. 1972. “Microwave Landing System Effect on the Flight Guidance and Control System.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-755
• Foster, L. D., T. F. Greenwood, and D. B. Lee. 1985. “Shuttle System Ascent Aerodynamic and Plume Heating.” In NASA. Johnson Space Center Space Shuttle Tech. Conf., Pt. 2. https://ntrs.nasa.gov/citations/19850008666
• Foster, J. D., and F. Neuman. 1970. Investigation of a Digital Automatic Aircraft Landing System in Turbulence. NASA-TN-D-6066. NASA. https://ntrs.nasa.gov/citations/19700033830
• Fourati, Hassen, and Christophe A. Prieur. 2023. Navigation magnéto-inertielle: Filtrage de Kalman et intelligence artificielle. https://doi.org/10.51257/a-v1-s7809
• Fournier, Paul G. 1961. Aerodynamic Characteristics of a Canard and an Outboard-Tail Airplane Model at High Subsonic Speeds. NASA-TN-D-1002. NASA. https://ntrs.nasa.gov/citations/19980228000
• Fournis, Camille. 2022. “Wave Drag Prediction Using the Lamb Vector in Two-Dimensional Steady Transonic Flows.” In AIAA AVIATION 2022 Forum. AIAA 2022-3886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3886
• Fowler, Kenneth J. 1990. Inertial Navigation System Simulator Program: Top-Level Design. Defense Technical Information Center. https://doi.org/10.21236/ada223762
• Fowler, W., and B. Tapley. 1965. “An Optimal Terminal Guidance Method for Continuous Powered Space Vehicles.” In Thermophysics Specialist Conference. AIAA 1965-696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-696
• Fox, Stephen, Greg Finney, Aaron Mebane, Bijan Nemati, and Kevin Ludwick. 2024. “Completion and Test of a Compact, Extremely Accurate Star Tracker.” In AMOS 2024 Technical Papers. AMOS Conference. https://doi.org/10.64861/vuse2201
• Fraenkel, L. E. 1958a. “A Note on the Drag of Wing-Body Combinations in Linearised Supersonic Flow.” Aeronautical Quarterly 9 (3): 305–12. https://doi.org/10.1017/s000192590001074x
• Fraenkel, L. E. 1958b. “The Wave Drag of Wing-Quasi-Cylinder Combinations at Zero Incidence.” Aeronautical Quarterly 9 (1): 55–70. https://doi.org/10.1017/s000192590000130x
• Franciscus, L. 1981a. “The Supersonic Fan Engine: An Advanced Concept in Supersonic Cruise Propulsion.” In 17th Joint Propulsion Conference. AIAA 1981-1599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1599
• Franciscus, L. 1981b. “Turbine Bypass Engine: A New Supersonic Cruise Propulsion Concept.” In 17th Joint Propulsion Conference. AIAA 1981-1596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1596
• Franciscus, L. 1983. “Supersonic Fan Engines for Military Aircraft.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2541. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2541
• Franciscus, L. C., and E. A. Lezberg. 1963a. Effects of Exhaust Nozzle Recombination of Hypersonic Ramjet Performance. i. Experimental Investigation of Recombination in Exhaust Nozzles. AIAA PAPER-63-118. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19640013357
• Franciscus, L. C., and E. A. Lezberg. 1963b. Effects of Exhaust Nozzle Recombination on Hypersonic Ramjet Performance- 1. Experimental Measurements. NASA-RP-57. NASA. https://ntrs.nasa.gov/citations/19640000246
• Franciscus, L. C., and E. A. Lezberg. 1963c. Effects of Exhaust Nozzle Recombination on Hypersonic Ramjet Performance. II: Analytical Investigation of the Effects of Exhaust Nozzle Recombination on Hydrogen-Fueled Hypersonic Ramjet Performance. AIAA PAPER 63119. NASA. https://ntrs.nasa.gov/citations/19630021448
• Franciscus, Leo C., and Jaime J. Maldonado. 1989. “Supersonic through-Flow Fan Engine and Aircraft Mission Performance.” In AIAA. https://ntrs.nasa.gov/citations/19900011722
• Franklin, Fred. 1954. “Methods Used in Celestial Navigation.” Navigation 4 (1): 9–21. https://doi.org/10.1002/j.2161-4296.1954.tb00693.x
• Frasier, C. W., and R. A. Gardiner. 1965. Lunar Excursion Module Mission and Related Guidance and Control Functions. NASA. https://ntrs.nasa.gov/citations/19660030753
• Frayer, R. G. 1965. Atlas Base Drag Study. NASA-CR-54501. NASA. https://ntrs.nasa.gov/citations/19660009183
• “Free-Flight Models.” 1953. Aircraft Engineering and Aerospace Technology 25 (4): 95–95. https://doi.org/10.1108/eb032277
• Freeman, Delma C., Theodore A. Talay, and Robert E. Austin. 1996. “The NASA Reusable Launch Vehicle Technology Program.” In Engineering, Construction, and Operations in Space V. American Society of Civil Engineers. https://doi.org/10.1061/40177(207)52
• Freiesleben, H. C. 1977. “From Two-Star Instruments to Modern Star Trackers.” Journal of Navigation 30 (1): 27–34. https://doi.org/10.1017/s0373463300043605
• “Frequency Tracking and Mitigation Method Based on CPHD Filter and Adaptive Multiple Linear Kalman Notch Filter for Multiple GNSS Interference.” 2020. NAVIGATION 67 (1): 213–213. https://doi.org/10.1002/navi.351
• Fresconi, Frank, Ilmars Celmins, James Maley, and Bryant Nelson. 2018. “Experimental Flight Characterization of a Canard-Controlled, Subsonic Missile.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3154. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3154
• Frey, Ashley E. 2014. Inlet Engineering Toolbox. Defense Technical Information Center. https://doi.org/10.21236/ada622072
• Frey, M., S. Jamme, R. Gojon, M. Fiore, and J. Gressier. 2025. “Large Eddy Simulation of the Control of the Inlet Buzz Phenomenon in a Supersonic Air Inlet.” In Proceedings of the 34th International Symposium on Shock Waves, Volume 1: Fundamentals. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-4767-5_2
• Friang, J., G. Duc, and J. Bonnet. 1996. “Robust Autopilot for an Air to Ground Missile: Loop Shaping H-Infinity Design, Gap-Metric and Real Nu-Analysis.” In Guidance, Navigation, and Control Conference. AIAA 1996-3729. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3729
• Friedman, R., and J. Reed. 1964. “Ballistic-Missile Research with Athena.” In 1st Annual Meeting. AIAA 1964-275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-275
• Friedmann, Peretz, Nicolas Lamorte, Bryan Glaz, Jack McNamara, Andrew Crowell, and Adam Culler. 2010. “Uncertainty Propagation in Hypersonic Aerothermoelastic Analysis.” In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th. AIAA 2010-2964. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-2964
• Frierson, J., and R. Van Meter. 1977. “An Electrostatic Roll Sensor for Supersonic Vehicles. I: Feasibility and Flight Tests.” In Guidance and Control Conference. AIAA 1977-1067. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1067
• Friest, David Thomas. n.d. “Optimization of a Celestial-Inertial Navigation System Using Single-Body Tracking.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180815-3395
• Frigo, N. J. 1986. “An Amplitude Switched Fiber Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1986.82
• Frigo, N. J. 1987. “A Constant Accuracy, High Dynamic Range Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937552
• Frisby, V. 1960. Design, Fabrication, and Test of High-Flotation Tires and Related Valving Mechanism for Rough Terrain Landing Gear. Defense Technical Information Center. https://doi.org/10.21236/ad0244172
• Frohnapfel, Dustin J., K. Todd Lowe, and Walter F. O’Brien. 2020. “Development, Analysis, and Validation of a Simultaneous Inlet Total Pressure and Swirl Distortion Generator.” In Volume 1: Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2020-16125
• Frohnapfel, Dustin J., Walter F. O’Brien, and Kevin T. Lowe. 2017. “Fan Rotor Flow Measurements in a Turbofan Engine Operating with Inlet Swirl Distortion.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1623
• Froning, H., Jr., L. McKinney, and R. Chase. 1996. “Aerospace Plane Trajectory Optimization for Sub-Orbital Boost Glide Flight.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4519
• Frühling, Stephan. 2025. “Ballistic Missile Defence.” In The Oxford Handbook of NATO. Oxford University Press. https://doi.org/10.1093/oxfordhb/9780198851196.013.26
• Fry, C. M., and A. P. Sage. 1974. “Identification of Aircraft Stability and Control Parameters Using Multilevel, Hierarchical Estimation.” In NASA. Flight Res. Center Parameter Estimation Tech. and Appl. in Aircraft Flight Testing. https://ntrs.nasa.gov/citations/19740017468
• Fu, Jan-Kaung. 1995. “Computations of Aerodynamic Drag for Spinning Transonic Projectiles Using an Implicit TVD Scheme.” Engineering Computations 12 (6): 529–44. https://doi.org/10.1108/02644409510799758
• Fu, Jan-Kaung, and Shen-Min Liang. 1991. “A Numerical Study on Drag Reduction for Turbulent Transonic Flow over a Projectile.” In 27th Joint Propulsion Conference. AIAA 1991-2260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2260
• Fu, Jan-Kaung, and Shen-Min Liang. 1993. “Computations of Aerodynamic Drag for Turbulent Transonic Projectileswith and without Spin.” In 11th Applied Aerodynamics Conference. AIAA 1993-3416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3416
• Fu, Zhen Xian, Yu Rong Lin, Yang Liu, and Xing Lin Chen. 2014a. “Accumulative Drifting Model of Inertial Navigation Platform under Elliptic Vibration.” In Key engineering materials, vol. 613. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.613.269
• Fu, Qiangwen, Yang Liu, Zhenbo Liu, Sihai Li, and Bofan Guan. 2018. “Autonomous in-Motion Alignment for Land Vehicle Strapdown Inertial Navigation System without the Aid of External Sensors.” Journal of Navigation 71 (6): 1312–28. https://doi.org/10.1017/s0373463318000437
• Fu, Jingneng, Wen Luo, and Hui Zhang. 2024b. “Real-Time Analysis of Star Sensor Attitude Accuracy.” Journal of Physics: Conference Series 2724 (1): 012024. https://doi.org/10.1088/1742-6596/2724/1/012024
• Fu, Zhumu, Dongfeng Wan, Zhikai Wang, and Fazhan Tao. 2024a. “Adaptive Variable Structure Interacting Multiple Model Tracking Algorithm for Hypersonic Glide Vehicle.” Journal of Aerospace Technology and Management 16: e3524. https://doi.org/10.1590/jatm.v16.1355
• Fu, Wen Xing, Tong Zhang, and Zi Jun Ren. 2017. “A New Decoupling Matrix Construction Method for Fault Detection and Isolation of a Redundant Strapdown Inertial Measurement Unit.” Transactions of the Japan Society for Aeronautical and Space Sciences 60 (1): 60–63. https://doi.org/10.2322/tjsass.60.60
• Fu-jun, Wang, Su Rui, and Lin Shuang-quan. 2024. “Research on Low Temperature Drift Suppression of Micro-Machined Gyroscope Based on Self-Calibration Technology.” Journal of Nanoelectronics and Optoelectronics 19 (1): 22–28. https://doi.org/10.1166/jno.2024.3552
• Fuchs, Jared, Matthew Haskell, Benjamin Thompson, Tate Harriman, and William Hankins. 2018. “Concept Study of a Reusable Suborbital Launch Vehicle.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0084. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0084
• Fuhrmann, Henri. 1993. “Application of Natural Laminar Flow to a Supersonic Transport Concept.” In 11th Applied Aerodynamics Conference. AIAA 1993-3467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3467
• Fujimoto, Akira, and Nobuo Niwa. 1993. “Experimental and Numerical Investigation of Mach 2.5 Supersonic Mixed Compression Inlet.” In 31st Aerospace Sciences Meeting. AIAA 1993-289. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-289
• Fujimoto, Akira, Nobuo Niwa, and Keisuke Sawada. 1991. “Numerical Investigation of Supersonic Inlet with Realistic Bleed Andbypass Systems.” In 29th Aerospace Sciences Meeting. AIAA 1991-127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-127
• Fujino, Michimasa, and Y. Kawamura. 2003. “Wave-Drag Characteristics of an over-the-Wing Nacelle Business-Jet Configuration.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-933. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-933
• “Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method.” 2000. In Nonlinear Problems in Aviation and Aerospace. CRC Press. https://doi.org/10.1201/9781482296914-12
• “Fundamental Principles and Historical Developments of Inertial Navigation.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch2
• Fundamentals of Inertial Navigation. 2020. Wiley. https://doi.org/10.1002/9781119547860.ch3
• Fundamentals of Satellite and Inertial Navigation. 2000. Wiley. https://doi.org/10.1002/0471200719.ch2
• Fundamentals of Satellite and Inertial Navigation. 2006. Wiley. https://doi.org/10.1002/9780470099728.ch2
• Funk, James E. 1975. Terrain Following Control Based on an Optimized Spline Model of Aircraft Motion. Defense Technical Information Center. https://doi.org/10.21236/ada021328
• Fuqun, Chen, Li Wenlan, Wang Zongyuan, and Cong Mengzi. 1985. “An Experimental Investigation of Response of a Turbojet Engine to Inlet Distortion.” In Volume 1: Aircraft Engine; Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/85-igt-12
• Furnish, J. F., and D. E. Anders. 1971. “Analytical Simulation of Landing Gear Dynamics for Aircraft Design and Analysis.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/710401
• Furukawa, Takeshi, and Yoshikazu Makino. 2007. “Conceptual Design and Aerodynamic Optimization of Silent Supersonic Aircraft at JAXA.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4166
• “Fusion of Multi-Antenna Carrier Phase Differential GPS and Inertial Measurements for Performance Evaluation of High Accuracy Integrated Aircraft Navigation Systems.” 2012. In Infotech@Aerospace 2012. AIAA 2012-2480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2480
• Fye, Robert W. 1966. Ballistic Missile Defense – the Crux of the Matter. Defense Technical Information Center. https://doi.org/10.21236/ada522410
• Gabriel, David S., Richard P. Krebs, E. Clinton Wilcox, and Stanley L. Koutz. 1953. Analysis of the Turbojet Engine for Propulsion of Supersonic Fighter Airplanes / David S. Gabriel, Richard P. Krebs, E.Clinton Wilcox, Stanley L.Koutz. NACA-RM-E52F17. NASA. https://ntrs.nasa.gov/citations/19930087143
• Gad-El-Hak, M., and C.-M. Ho. 1986. “Aerodynamics of a Missile in Unsteady Flight.” In 24th Aerospace Sciences Meeting. AIAA 1986-572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-572
• Gadalla, S., M. EL-lithy, and A. Makarious. 1993. “Simulation of Ballistic Missile Motion in Free-Flight (Ballistic) Phase Using NAVSTAR (GPS) Navigation Model.” International Conference on Aerospace Sciences and Aviation Technology 5 (ASAT CONFERENCE): 1–10. https://doi.org/10.21608/asat.1993.25644
• Gadeberg, B. L., and K. C. White. 1970. Theory of the Correction of Celestial Observations Made for Space Navigation or Training. NASA-TN-D-5239. NASA. https://ntrs.nasa.gov/citations/19700008007
• Gage, Douglas W. 1998. An Evolutionary Strategy for Achieving Autonomous Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada422374
• Gage, Peter, and Jeremy Vander Kam. 2003. “A Data Model for Evaluating Reusable Launch Vehicle Concepts.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1330
• Gai, E. G., and R. E. Curry. 1975. “Failure Detection by Pilots during Automatic Landing: Models and Experiments.” In NASA. Ames Res. Center 11th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19750025607
• Gainer, T. G. 1961. Low-Speed Investigation of Effects of Vertical Tails on the Static Stability Characteristics of a Canard-Bomber Configuration Having a Very Thin Wing and a Slender Elliptical Fuselage. NASA-TM-X-436. NASA. https://ntrs.nasa.gov/citations/19660024046
• Gainer, T. G., M. J. Mann, and J. K. Huffman. 1984. Low-Speed Investigation of Effects of Wing Leading- and Trailing-Edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward-Swept Wing. NASA-TM-85795. NASA. https://ntrs.nasa.gov/citations/19840018599
• Gainor, Christopher. 2013. “The Atlas and the Air Force: Reassessing the Beginnings of America’s First Intercontinental Ballistic Missile.” Technology and Culture 54 (2): 346–70. https://doi.org/10.1353/tech.2013.0069
• Galante, Joseph, and Robert Sanner. 2012. “A Nonlinear Adaptive Filter for Gyro Thermal Bias Error Cancellation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4475
• Gallagher, James F. 1969. Some Remarks on Circular Probable Error and Other Statistics of Two- Dimensional Distributions. Defense Technical Information Center. https://doi.org/10.21236/ad0689780
• Gallo Olalla, Eduardo. n.d. “Autonomous Fixed Wing Unmanned Air Vehicle GNSS-Denied Navigation: Fusion of Extended Kalman Filter in SE(3) Manifold with Inertially Assisted Semi-Direct Visual Odometry.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.77163
• Gallon, John C., and Allen Witkowski. 2015. “Verification and Validation Testing of the Parachute Decelerator System Prior to the First Supersonic Flight Dynamics Test for the Low Density Supersonic Decelerator Program.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2162
• Galloway, L. M., and J. F. Barnaba. 1983. “Inertial Navigation/calibration/precise Time and Frequency Capabilities.” In NASA. Goddard Space Flight Center Proc. of the 14th Ann. Precise Time and Time Interval (PTTI) Appl. Planning Meeting. https://ntrs.nasa.gov/citations/19830027102
• Galyagin, K. S., M. A. Oshivalov, and M. A. Savin. 2017. “Numerical Modeling of the Drift of a Fiber-Optic Gyroscope with External Shock Exposure.” Izvestiâ vysših učebnyh zavedenij. Priborostroenie: 1169–76. https://doi.org/10.17586/0021-3454-2017-60-12-1169-1176
• Gan, XVDong, Shuang Du, and WenHui Yang. 2022. “A MM-Aided Inertial Navigation for Land Vehicle in GNSS-Denied Environment.” In 4th International Conference on Information Science, Electrical, and Automation Engineering (ISEAE 2022), edited by Mengyi (Milly) Cen, Lidan Wang. SPIE. https://doi.org/10.1117/12.2639548
• Ganeko, Y. 1976. Astrogeodetic Geoid of Japan. NASA-CR-146855. NASA. https://ntrs.nasa.gov/citations/19760014711
• Ganeko, Y. 1977. “An Astrogeodetic Geoid of Japan.” Journal of Geophysical Research 82. https://ntrs.nasa.gov/citations/19770054146
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021b. “Combined Test of the Flight Control Subsystem.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00005-x
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021c. “Flight Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00008-5
• Gao, Yakui, Gang An, and Chaoyou Zhi. 2021d. “Unit Test of the Flight Control System.” In Test Techniques for Flight Control Systems of Large Transport Aircraft. Elsevier. https://doi.org/10.1016/b978-0-12-822990-3.00002-4
• Gao, Jia-zhi, Xiao-qian Chen, and Jian-ying Song. 2018a. “Gauss Pseudospectral Method Based Trajectory Optimization for Hypersonic Glide Vehicles.” DEStech Transactions on Computer Science and Engineering, no. pcmm. https://doi.org/10.12783/dtcse/pcmm2018/23663
• Gao, Yang, Zhongyu Luo, Junhong Xiang, and Shuyuan Wen. 2024b. “Binocular Pose Measurement Method for Automatic Landing of Fixed-Wing Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.4923748
• Gao, Weiwei, Hongyun Wang, Dan Fang, Yi Wang, Hongyan Zhang, and Yang Li. 2019. “Research on Initial Precision Alignment Method of Strapdown Inertial Navigation System.” In AIP Conference Proceedings, vol. 2122. AIP Publishing. https://doi.org/10.1063/1.5116484
• Gao, Junfeng, Chao Wei, Jun Zhang, Yi Li, and Xu Yao. 2026. “Advanced Gyroscope Technologies for Autonomous Inertial Navigation: From Mechanical to Atomic Sensors.” In International Conference on Optoelectronics and Information Technology (ICOIT 2026), edited by Yonghang Tai, Robertas Damaševičius, Peng Geng. SPIE. https://doi.org/10.1117/12.3116148
• Gao, Yimeng, and Lan Yang. 2023. “An Autonomous Navigation Method Based on Artificial Celestial Observation Using Star Sensors.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_165
• Gao, Wei, and Bo Zhao. 2012. “The Influence of Gravity Inaccuracy in Underwater ESG Inertial Navigation System.” Advanced materials research 566: 231–34. https://doi.org/10.4028/www.scientific.net/amr.566.231
• Garcia-Velo, Juan, and Bruce Walker. 1995. “Aerodynamic Parameter Estimation for High-Performance Aircraft Using Extended Kalman Filtering.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3500. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3500
• Gardinier, Debra, and Anthony Taylor. 1999. “Design and Testing of the K-1 Reusable Launch Vehicle Landing System Airbags.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1757
• Gardner, William N. 1953. Aerodynamic Characteristics of a Canard-Balanced Free-Floating, All-Movable Stabilizer as Obtained from Rocket-Powered-Model Flight Tests and Low-Speed Wind-Tunnel Tests. NACA-RM-L53I28a. NASA. https://ntrs.nasa.gov/citations/19930090588
• Gardner, A. J. 1955. “An Introduction to the Thermal Problems of Turbojet Engines for Supersonic Propulsion.” Journal of Fluids Engineering 77 (5): 715–20. https://doi.org/10.1115/1.4014484
• Gardner, William N., and James L. Edmondson. 1950. Preliminary Results Obtained from Flight Test of a Rocket Model Having the Tail Only of the Grumman XF10F Airplane Configuration, TED No. NACA DE 354. NACA-RM-SL51E04. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019389
• Gardner, A., J. Steelant, A. Paull, and K. Hannemann. 2004. “Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3345
• Garon, Katherine, Gregg Abate, and W. Hathaway. 2003. “Free-Flight Testing of Generic Missile with MEMs Protuberances.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1242
• “Gas Generators for Base Drag Reduction (Fumers).” 1976. In Aerodynamics of Base Combustion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865145.0471.0486
• Gates, R. L. 1964. Preliminary Report on Precision Testing of Gyroscopes on a High g Centrifuge. General Precision, Inc. https://ntrs.nasa.gov/citations/19650008141
• Gates, Russell, Albion Bowers, and Richard Howard. 1996. “A Comparison of Flight Input Techniques for Parameter Estimation of Highly-Augmented Aircraft.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3363. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3363
• Gates, Clarence R., and Elliott Cutting. 1963. “Midcourse Guidance Using Radio Techniques.” In Technology of Lunar Exploration. Elsevier. https://doi.org/10.1016/b978-0-12-395707-8.50015-2
• Gates, R., and K. McAloon. 1976. “A Precision Star Tracker Utilizing Advanced Techniques and Materials.” In 14th Aerospace Sciences Meeting. AIAA 1976-113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-113
• Gates, Robert K., and Robert F. Shipp. 1977. Standardization Potential across Navigation Systems (SPANS). Defense Technical Information Center. https://doi.org/10.21236/ada047937
• Gates, Ordway B., Jr., and Albert A. Schy. 1952. A Theoretical Investigation of the Effect of a Target Seeker Sensitive to Pitch Attitude on the Dynamic Stability and Response Characteristics of a Supersonic Canard Missile Configuration. NACA-RM-L52E19. NASA. https://ntrs.nasa.gov/citations/19930087147
• Gatlin, Gregory M., Dan D. Vicroy, and Melissa B. Carter. 2012. “Experimental Investigation of the Low-Speed Aerodynamic Characteristics of a 5.8-Percent Scale Hybrid Wing Body Configuration.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20120011838
• Gaver, Donald P., and Patricia A. Jacobs. 1997. Testing or Fault-Finding for Reliability Growth: A Missile Destructive-Test Example. Defense Technical Information Center. https://doi.org/10.21236/ada326542
• Ge, Zheng-Ming, Ming-Yen Liu, and Sann-Chie Lee. 1995. “The Influence of Temperature on the Drift of Gyroscope.” Transactions of the Canadian Society for Mechanical Engineering 19 (4): 363–82. https://doi.org/10.1139/tcsme-1995-0019
• Ge, Yongyan, Hong-Sen Yan, and Lingchen Xia. 2018. “Multi-Dimensional Taylor Network Optimal Control of the Axisymmetric Cruise Missile Flight.” In International Conference on Electromechanical Control Technology and Transportation (ICECTT). https://doi.org/10.5220/0006966801560162
• Gee, S. W. 1978. Flight Tests of a Radio-Controlled Airplane Mode with a Free-Wing, Free-Canard Configuration. NASA-TM-72853. NASA. https://ntrs.nasa.gov/citations/19780010099
• Gee, S., G. E. Jenks, J. Roskam, and R. Stone. 1976. “Flight Test Evaluation of a Separate Surface Attitude Command Control System on a Beech 99 Airplane.” In Guidance and Control Conference. AIAA 1976-1991. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1991
• Gelb, Arthur, and Arthur A. Sutherland. 1970. “Software Advances in Aided Inertial Navigation Systems.” Navigation 17 (4): 358–69. https://doi.org/10.1002/j.2161-4296.1970.tb00058.x
• General Dynamics/Astronautics San Diego Ca. 1962. (WS 107A-1) Flight Test Working Group Flight Test Report Atlas Missile 11F. AMR Range Test Number 71. Defense Technical Information Center. https://doi.org/10.21236/ad0852659
• General Dynamics/Astronautics San Diegoca. 1961. WS 107-1 Flight Test Working Group, Flight Test Report, Atlas Missile 26E.. Defense Technical Information Center. https://doi.org/10.21236/ad0843112
• Geng, Jingtong, and Yuwei Li. 2024. “Higher-Order Anti-PT-Symmetric Self-Injection Locking Micro-Resonator Optical Gyroscope.” Physica Scripta 99 (7): 075502. https://doi.org/10.1088/1402-4896/ad4fc6
• Genova, James J. 2005. Coherent Seeker Guided Antiship Missile Performance Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada430023
• Gentric, A. 1956. On Landing Gear Stresses. NACA-TM-1422. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20030065915
• Geohagan, Kevin, Bill Bernard, T. Emerson Oliver, Jared Leggett, and Dennis Strickland. 2018. 6DOF Testing of the SLS Inertial Navigation Unit. M17-6251. Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA). https://ntrs.nasa.gov/citations/20180002019
• Georghiou, Luke, J. Stanley Metcalfe, Michael Gibbons, Tim Ray, and Janet Evans. 1986. “Smiths Industries: Aircraft Automatic Landing Equipment.” In Post-Innovation Performance. Palgrave Macmillan UK. https://doi.org/10.1007/978-1-349-07455-6_35
• Georgieva, Hristina. 2017. “Modeling of Shimmy Oscillations in Aircraft Landing Gear.” MATEC Web of Conferences 133: 01007. https://doi.org/10.1051/matecconf/201713301007
• Geragersian, Patrick, Ivan Petrunin, Weisi Guo, and Raphael Grech. 2022. “An INS/GNSS Fusion Architecture in GNSS Denied Environment Using Gated Recurrent Unit.” In AIAA SCITECH 2022 Forum. AIAA 2022-1759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1759
• Gerber, M. 1975. “Propagation of Gravity Gradiometer Errors in an Airborne Inertial Navigation System.” In Guidance and Control Conference. AIAA 1975-1089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1089
• Gersdorf, Bernd, and Udo Freese. 2013. “A Kalman Filter for Odometry Using a Wheel Mounted Inertial Sensor.” In International Conference on Informatics in Control, Automation and Robotics (ICINCO). https://doi.org/10.5220/0004457300000783
• Gevaert, G., and B. Feinreich. 1977. The Development of Advanced Automatic Flare and Decrab for Powered Lift Short Haul Aircraft Using a Microwave Landing System. NASA-CR-151948. NASA. https://ntrs.nasa.gov/citations/19770016149
• Gevertz, Jana L., and Irina Kareva. 2023. “Minimally Sufficient Experimental Design Using Identifiability Analysis.” Preprint, bioRxiv. https://doi.org/10.1101/2023.10.14.562348
• Ghanbarpourasl, Habib. 2020. “A New Robust Quaternion-Based Initial Alignment Algorithm for Stationary Strapdown Inertial Navigation Systems.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234 (12): 1913–25. https://doi.org/10.1177/0954410020920473
• Ghanizadegan, Khashayar. n.d. “Novel Quaternion-Based Nonlinear Kalman-Type Filters for GPS-Denied Visual-Inertial Navigation.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2025-17017
• Ghanizadegan, Khashayar, and Hashim A. Hashim. 2025c. “Unscented Particle Filter for Visual-Inertial Navigation Using IMU and Landmark Measurements.” Preprint, . https://doi.org/10.36227/techrxiv.174612877.77750997/v1
• Ghasemi, Abdollah, Ali Abedi, and Farshid Ghasemi. 2011. “Line of Sight Propagation.” In Propagation Engineering in Wireless Communications. Springer New York. https://doi.org/10.1007/978-1-4614-1077-5_7
• Ghasemi, Abdollah, Ali Abedi, and Farshid Ghasemi. 2016. “Line-of-Sight Propagation.” In Propagation Engineering in Wireless Communications. Springer International Publishing. https://doi.org/10.1007/978-3-319-32783-9_7
• Ghasrizadeh, Reza, and Amirali Nikkhah. 2020. “improve coarse alignment in inertial navigation system By the method of Identification the Kalman filter matrix.” Journal of Space Science and Technology 13 (4): 81–90. https://doi.org/10.30699/jsst.2021.1213
• Ghesmati, Mohammad, Jafar Heyrani Nobari, Mohammadreza Arvan, and Abdorreza Kashaninia. 2020. “Gyroscope Drift Error Analysis in the Position-Independent Navigation Algorithm of a stable platform Inertial System.” Journal of Control 14 (2): 1–15. https://doi.org/10.29252/joc.14.2.1
• Ghori, Abdullah, S. Narendar, and Yogita Dubey. 2023. “Thermo-Structural Response Prediction of UHTCC Control Surface for Hypersonic Cruise Vehicle.” Applied Mechanics and Materials 915: 81–94. https://doi.org/10.4028/p-oah3jt
• Ghosh, A., and S. Raisinghani. 2000. “Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4102
• Gibson, Philip T., Graham H. Alexander, and Hobart A. Cress. 1968. Validation of Design Theory for Aircraft Arresting-Gear Cable. Defense Technical Information Center. https://doi.org/10.21236/ad0665328
• Gido, J., R. Jaffe, and R. Wilson. 1974. “Merging Conventional and Modern Control Techniques for Practical Missile Autopilot Design.” In Mechanics and Control of Flight Conference. AIAA 1974-911. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-911
• Gilbert, R., and M. Kayton. 1964. “Effect of Component Orthogonality on Aircraft Inertial Navigation System Errors.” In 1st Annual Meeting. AIAA 1964-237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-237
• Gill, Waqas Amin, Ian Howard, Ilyas Mazhar, and Kristoffer McKee. 2022. “MEMS Vibrating Ring Gyroscope with Worm-Shaped Support Springs for Space Applications.” In ASEC 2022. MDPI. https://doi.org/10.3390/asec2022-13800
• Gill, Waqas Amin, Ian Howard, Ilyas Mazhar, and Kristoffer McKee. 2023a. “Dynamic Analysis of a MEMS Vibrating Ring Gyroscope.” Preprint, . https://doi.org/10.20944/preprints202311.0506.v1
• Gill, Waqas Amin, Ian Howard, Ilyas Mazhar, and Kristoffer McKee. 2023b. “Simulation-Based Design and Analysis for MEMS Vibrating Ring Gyroscope.” In ASEC 2023. MDPI. https://doi.org/10.3390/asec2023-15273
• Gillespie, Warren, Jr. 1960. Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20. NASA-TN-D-509. NASA. https://ntrs.nasa.gov/citations/20040046997
• Gillespie, Warren, Jr., and Richard G. Arbic. 1951. Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.87 to 1.39 of 1/10-Scale Models of the Northrop MX-775A Missile. NACA-RM-SL51K07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030052
• Gillis, Clarence L., and Rowe Chapman Jr. 1956. Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3. NACA-RM-L56E17. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019449
• Gillis, Clarence L., and Jesse L. Mitchell. 1957. Determination of Longitudinal Stability and Control Characteristics from Free-Flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations. NACA-TR-1337. NASA. https://ntrs.nasa.gov/citations/19930092326
• Gilmore, J. P. 1967. Conceptual Nonorthogonal Gyro Configuration for Guidance and Navigation. MSC-11363. NASA. https://ntrs.nasa.gov/citations/19670000433
• Gilmore, J. P. 1968. “A Non-Orthogonal Multi-Sensor Strapdown Inertial Reference Unit.” In IEEE. https://ntrs.nasa.gov/citations/19690035222
• Gilmore, J. P., and R. A. McKern. 1970. “A Redundant Strapdown Inertial Systems Mechanization-SIRU.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19700066199
• Giridharan, V., and S. Sivakumar. 2022. “Shimmy Analysis of Light Weight Aircraft Nose Wheel Landing Gear.” Vibroengineering Procedia 47: 8–15. https://doi.org/10.21595/vp.2022.22988
• Gitterman, Harry N., and Samuel N. Watkins. 1965. Line-of-Sight Propagation Experimentation and Modeling for Partially Illuminated Terrain. Defense Technical Information Center. https://doi.org/10.21236/ad0643318
• Giudici, M. 1991. “Identifiability of Distributed Physical Parameters in Diffusive-like Systems.” Inverse Problems 7 (2): 231–45. https://doi.org/10.1088/0266-5611/7/2/007
• “Gladkov I. a. Application of Trajectory Analysis to Design a System of Safe Take-off and Landing of Aircraft.” 2017. Исследования космоса 2 (2): 115–25. https://doi.org/10.7256/2453-8817.2017.2.23099
• Glavich, Thomas. 1987. Star-Tracker Computer Program. NPO-16862. Caltech. https://ntrs.nasa.gov/citations/19870000540
• Glessner, Paul T. 1999. “Power Effects on High Lift, Stability and Control Characteristics of the TCA Model Tested in the LaRC 14 x 22 Ft Wind Tunnel.” In 1998 NASA High-Speed Research Program Aeodynamic Performance Workshop. https://ntrs.nasa.gov/citations/20000036439
• Gloss, B. B. 1974a. The Effect of Canard Leading Edge Sweep and Dihedral Angle on the Longitudinal and Lateral Aerodynamic Characteristic of a Close-Coupled Canard-Wing Configuration. NASA-TN-D-7814. NASA. https://ntrs.nasa.gov/citations/19750004860
• Gloss, B. B. 1974b. Effect of Canard Location and Size on Canard-Wing Interference and Aerodynamic Center Shift Related to Maneuvering Aircraft at Transonic Speeds. NASA-TN-D-7505. NASA. https://ntrs.nasa.gov/citations/19740020361
• Gloss, B. B. 1975. Effect of Wing Planform and Canard Location and Geometry on the Longitudinal Aerodynamic Characteristics of a Close-Coupled Canard Wing Model at Subsonic Speeds. NASA-TN-D-7910. NASA. https://ntrs.nasa.gov/citations/19750015442
• Gloss, B. B. 1978. Effect of Camber on the Trimmed Lift Capability of a Close-Coupled Canard-Wing Configuration. NASA-TM-78686. NASA. https://ntrs.nasa.gov/citations/19780020109
• Gloss, B. B., W. P. Henderson, and J. K. Huffman. 1974. Effect of Canard Position and Wing Leading-Edge Flap Deflection on Wing Buffet at Transonic Speeds. NASA-TM-X-72681. NASA. https://ntrs.nasa.gov/citations/19750015487
• Gloss, B. B., E. J. Ray, and K. E. Washburn. 1978. Effect of Canard Vertical Location, Size, and Deflection on Canard-Wing Interference at Subsonic Speeds. NASA-TM-78790. NASA. https://ntrs.nasa.gov/citations/19790005842
• Gloss, B. B., and K. E. Washburn. 1977a. “Load Distribution on a Close-Coupled Wing Canard at Transonic Speeds.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19770060346
• Gloss, B. B., and K. E. Washburn. 1977b. Load Distribution on a Closed-Coupled Wing Canard at Transonic Speeds. NASA-TM-74053. NASA. https://ntrs.nasa.gov/citations/19770022153
• Gloss, B. B., and K. E. Washburn. 1979. A Study of Canard-Wing Interference Using Experimental Pressure Data at Transonic Speeds. NASA-TP-1355. NASA. https://ntrs.nasa.gov/citations/19790007731
• Gnadt, Albert. 2022. “Machine Learning-Enhanced Magnetic Calibration for Airborne Magnetic Anomaly Navigation.” In AIAA SCITECH 2022 Forum. AIAA 2022-1760. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1760
• “GNSS-Aided INS: Loose Coupling.” 2022a. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch20
• “GNSS-Aided INS: Tight Coupling.” 2022b. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch21
• Godfrey, K. R., and J. J. DiStefano. 1987. “Identifiability of Model Parameters.” In Identifiability of Parametric Models. Elsevier. https://doi.org/10.1016/b978-0-08-034929-9.50005-4
• Goertzen, L. L. 1972. Altitude-Aided Radar Tracking. Defense Technical Information Center. https://doi.org/10.21236/ad0756655
• Gogulapati, Abhijit, Kirk R. Brouwer, X. Q. Wang, Raghavendra Murthy, Jack J. McNamara, and Marc P. Mignolet. 2017. “Full and Reduced Order Aerothermoelastic Modeling of Built- up Aerospace Panels in High-Speed Flows.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0180
• Gold, Ronald, and Ronald Busan. 1994. “Design and Implementation of a Full-Scale Spinning Missile Model with Active Canard Control.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-721
• Golden, Joe P. 1980. “Terrain Contour Matching (TERCOM): A Cruise Missile Guidance Aid.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959127
• Goldhirsh, Julius, and G. Daniel Dockery. 1991. “Propagation Measurements and Modeling at C Band for over-the-Water, Line-of-Sight Propagation Links in the Mid-Atlantic Coast.” Radio Science 26 (3): 671–90. https://doi.org/10.1029/91rs00101
• Goldhirsh, Julius, G. Daniel Dockery, and Bert H. Musiani. 1992. “Fade Statistics and Propagation Events at C Band for Two Overwater, Line-of-Sight Propagation Paths over a 1-Year Period.” Radio Science 27 (6): 813–28. https://doi.org/10.1029/92rs01775
• Goldsmith, H. A. 1964. “Stability and Control of Supersonic Aircraft at Low Speeds.” In International Council of the Aeronautical Sciences. AIAA 1964-588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-588
• Golovan, A. A., and K. A. Kuznetsova. 2025. “Velocity Estimation Using Carrier Phase Measurements of a Global Navigation Satellite System in Autonomous Mode.” Gyroscopy and Navigation 16 (3): 209–19. https://doi.org/10.1134/s2075108725700282
• Golubek, O. 2024. “Correcting Measurements of Launch Vehicle’s Angular Motion Parameters of a Strapdown Inertial Navigation System with the Use of a Celestial Navigation System.” Science and Innovation 20 (1): 74–86. https://doi.org/10.15407/scine20.01.074
• Golyakov, Alexey D., Alexander M. Richnyak, and Ivan V. Fominov. 2022. “Investigation of the Accuracy Parameters of a Spacecraft with an Adaptive Autonomous Navigation System.” Trudy MAI, no. 126. https://doi.org/10.34759/trd-2022-126-23
• Gonzalez, Jesse M., and Arthur R. Denny. 1970. Theoretical Sensitivity Analysis and System Delivery Accuracy Computations for High and Low Drag Weapons at Several Subsonic and Supersonic Delivery Conditions. Defense Technical Information Center. https://doi.org/10.21236/ad0878792
• Goodall, William, and Donald Ewen. 1987. “Test Analysis and Evaluation Requirements for Second Source Missile Guidance Systems.” In Guidance, Navigation and Control Conference. AIAA 1987-2584. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2584
• Goodsell, Aga, Robert Kennelly Jr., and Scott Lawrence. 2000. “Accounting for Laminar Run and Trip Drag in Supersonic Cruise Performance Testing.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-265
• Goodstein, R., B. Tse, D. Winkel, and C. Halliday. 1984. “Flight Test Results of the Inertial Upper Stage Redundant Inertial Measurement Unit Redundancy Management Technique.” In 22nd Aerospace Sciences Meeting. AIAA 1984-568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-568
• Goodstein, R., B. Tse, D. Winkel, and P. Scott. 1982. “Failure Detection Technique for the Inertial Upper Stage Inertial Navigation System.” In Guidance and Control Conference. AIAA 1982-1622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1622
• Gopinath, N. K., V. Vignesh, and D. Roy Mahapatra. 2015. “Experimental Investigation on Metal Sandwich Panel for Hypersonic Cruise Vehicle Airframe with Active Cooling.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3558
• Gordan, Andrew L. 1987. Optical Alignment of Centaur’s Inertial Guidance System. NASA-TM-88844. NASA. https://ntrs.nasa.gov/citations/19880003133
• Gordon, Robert B. 1964. “The Attainment of Precision in Celestial Navigation.” Journal of Navigation 17 (2): 125–47. https://doi.org/10.1017/s0373463300048505
• Gordon, Rachel. 1990. “Numerical Simulation of Vortical Flows over a Strake-Delta Wing and a Close Coupled Delta-Canard Configuration.” In 8th Applied Aerodynamics Conference. AIAA 1990-3002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3002
• Goss, W. C. 1969. “The Mariner Spacecraft Star Tracker.” In INTERNATIONAL ASTRONAUTICAL FEDERATION. https://ntrs.nasa.gov/citations/19700063123
• Goss, W. C. 1972. “The Mariner Spacecraft Star Tracker.” In Proceedings of the XXth International Astronautical Congress. Elsevier. https://doi.org/10.1016/b978-0-08-016841-8.50045-6
• Goss, W. H., and Emory Cook. 1948. “THE RAMJET as a Supersonic Propulsion Plant.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/480228
• Goto, Keita, Yoshikazu Miyazawa, and Masakazu Sagisaka. 2001. “Development of Ground Taxiing Control Law for Automatic Landing Flight Experiment (ALFLEX).” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4242
• Gottlieb, Jonah R., John M. Mines, Daniel C. Garmendia, Jerold W. Emhoff, and Daniel E. Clemens. 2024. “Coupled Vehicle and Trajectory Design Optimization for Boost-Glide Hypersonic Systems.” In AIAA SCITECH 2024 Forum. AIAA 2024-0373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0373
• Gou, Wanxiang, Chonghui Li, Xinna Li, et al. 2025a. “Prediction-Selection-Extraction: Star Point Extraction from Daytime Star Maps Based on the Randomness of Stellar Imaging Energy.” Optics Express 33 (5): 10835. https://doi.org/10.1364/oe.549351
• “GPS Aided Inertial System.” 2007. In Introduction to Modern Navigation Systems. WORLD SCIENTIFIC. https://doi.org/10.1142/9789812708755_0012
• Graber, E., Jr., and W. Braithwaite. 1974. “Summary of Recent Investigations of Inlet Flow Distortion Effects Onengine Stability.” In 12th Aerospace Sciences Meeting. AIAA 1974-236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-236
• Grace, Josh, Luca Merlo Paula Soares, Trevor Loe, and John Bellardo. 2022. “A Low Cost Star Tracker for CubeSat Missions.” In AIAA SCITECH 2022 Forum. AIAA 2022-0520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0520
• Graf, Carl, and Joel Trimble. 1980. “Multisensor Image Processing Integration for Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959161
• Grammatikos, A. 1965. Gimballess Inertial Systems for Space Navigation. NASA-CR-71089. NASA. https://ntrs.nasa.gov/citations/19660010238
• Granot, R., and H. Mayorchik. 1983. “Evaluation of a Rocket Burnout Velocity from Ground and Free Flight Tests.” In 21st Aerospace Sciences Meeting. AIAA 1983-36. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-36
• Granot, R., and Y. Sylman. 1982. “Parameter Identification for Free Flight Rockets.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1377. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1377
• Grant, Matthew J., and Michel J. F. Digonnet. 2019. “Loss-Gain Coupled Ring Resonator Gyroscope.” In Optical, Opto-Atomic, and Entanglement-Enhanced Precision Metrology, edited by Selim M. Shahriar, Jacob Scheuer. SPIE. https://doi.org/10.1117/12.2515657
• Grant, Frederick C., and John R. Sevier Jr. 1960. Transonic and Supersonic Wind-Tunnel Tests of Wing-Body Combinations Designed for High Efficiency at a Mach Number of 1.41. NASA-TN-D-435. NASA. https://ntrs.nasa.gov/citations/19980230620
• Grashof, J. 1983. “Numerical Investigation of Three-Dimensional Transonic Flow through Air Intakes Disturbed by a Missile Plume.” In Applied Aerodynamics Conference. AIAA 1983-1854. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1854
• Gratt, Harvey, and Wayne McCowan. 1993. “Autopilot Design for the Advanced Kinetic Energy Missile (ADKEM) Boost Phase.” In Guidance, Navigation and Control Conference. AIAA 1993-3736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3736
• Grauer, Jared A. 2020a. “Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements.” In AIAA SciTech 2020. https://ntrs.nasa.gov/citations/20200002779
• Grauer, Jared A. 2020b. A Learn-to-Fly Approach for Adaptively Tuning Flight Control Systems. NF1676L-35663. Langley Research Center. https://ntrs.nasa.gov/citations/20200003217
• Grauer, Jared A. 2021. A Learn-to-Fly Approach for Adaptively Tuning Flight Control Systems. Langley Research Center. https://ntrs.nasa.gov/citations/20210021941
• Grauer, Jared A., and Matthew J. Boucher. n.d. “System Identification of Flexible Aircraft: Lessons Learned from the X-56A Phase 1 Flight Tests.” In AIAA SciTech 2020. https://ntrs.nasa.gov/citations/20200002775
• Grauer, Jared A., and Matthew J. Boucher. 2018. “Real-Time Parameter Estimation for Flexible Aircraft.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3155
• Grauer, Jared A., and Eugene A. Morelli. 2015. “A New Formulation of the Filter-Error Method for Aerodynamic Parameter Estimation in Turbulence.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2704
• Gravelle, Joseph. n.d. “A Computer Aided Turbojet Engine Trimming System.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1977-13015
• Graves, E. B. 1972. Supersonic Aerodynamic Characteristics of a Two-Staged Space-Shuttle Model Having a Delta-Wing Orbiter Mated atop a Winged Booster. NASA-TM-X-2569. NASA. https://ntrs.nasa.gov/citations/19720022345
• Graves, W. 1977. “Shimmy Analysis and Test of the Rockwell International -40 Model Sabreliner Corotating Dual Wheel Nose Gear.” In Dynamics Specialists Conference. AIAA 1977-440. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-440
• Gray, I. D. 1997. “Effects of the Earth’s Curvature on Radar Tracking Systems.” In Radar Systems (RADAR 97), vol. 1997. IEE. https://doi.org/10.1049/cp:19971746
• Greene, J. E. 1957. Static Stability and Magnus Characteristics of the U.s. Navy 1,000 Pound Low-Drag Bomb at Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0132012
• Greene, Joel. 1964. “A Daylight Astro Tracker for Supersonic Transport Navigation.” Navigation 11 (3): 228–36. https://doi.org/10.1002/j.2161-4296.1964.tb02097.x
• Greenland, Bradley James. 2021. “Resolution of Indeterminate Landing Gear Structure Design.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14657595
• Greenspan, Richard L. 1995. “Inertial Navigation Technology from 1970-1995.” Navigation 42 (1): 165–85. https://doi.org/10.1002/j.2161-4296.1995.tb02334.x
• Greenstein, J. 1968. “Postflight Guidance Accuracy Analysis of Atlas.” In Control and Flight Dynamics Conference. AIAA 1968-842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-842
• Greentree, Andrew D., Xuezhi Wang, Wenchao Li, et al. 2022. Quantum Diamond Magnetometry for Navigation in GNSS Denied Environments. https://doi.org/10.5194/iag-comm4-2022-32
• Gregoriou, G. 1989. “ADAM: An Advanced Design Code for Missile Aerodynamics.” In 7th Applied Aerodynamics Conference. AIAA 1989-2171. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2171
• Grenet, P., and F. Mansour. 2010. “Using Vicon System and Optical Method to Evaluate Inertial and Magnetic System Accuracy.” EPJ Web of Conferences 6: 12004. https://doi.org/10.1051/epjconf/20100612004
• Grenson, Pierre, and Samir Beneddine. 2018. “Analysis of Shock Oscillations of an External Compression Supersonic Inlet through Unsteady Numerical Simulations.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3011. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3011
• Gresham, James L., Jean-Michel W. Fahmi, Benjamin M. Simmons, Jeremy W. Hopwood, Wade Foster, and Craig A. Woolsey. 2022. “Flight Test Approach for Modeling and Control Law Validation for Unmanned Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-2406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2406
• Griffin, K., and F. Jonas. 1983. “Wake Characteristics and Interactions of the Canard/wing Lifting Surface Configuration of the X-29 Forward-Swept Wing Flight Demonstrator.” In Applied Aerodynamics Conference. AIAA 1983-1835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1835
• Griffin, Jack A., Timothy T. Takahashi, and Patrick E. Rodi. 2023. “Aerothermodynamic Assessment of Conceptual and Detail Configuration Changes to a Rocket Propelled Aircraft.” In AIAA SCITECH 2023 Forum. AIAA 2023-0216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0216
• Griffioen, J. W., and P. J. Oonincx. 2012. “Suitability of Low-Frequency Navigation Systems for Artillery Positioning in a GNSS Denied Environment.” Journal of Navigation 66 (1): 35–48. https://doi.org/10.1017/s0373463312000410
• Griggs, C. E., M. V. Moody, R. S. Norton, H. J. Paik, and K. Venkateswara. n.d. “Sensitive Superconducting Gravity Gradiometer Constructed with Levitated Test Masses.” Physical Review Applied 8 (6). https://ntrs.nasa.gov/citations/45640396838410
• Grigsby, Carl E. 1954. Investigation of a Canard Missile Configuration (NACA RM-4) in the Langley 9-Inch Supersonic Tunnel at Mach Numbers of 1.62 and 1.93. NACA-RM-L54E20. NASA. https://ntrs.nasa.gov/citations/19930088086
• Gringorten, Irving I. 1967. A Statistical Model of the Temperature Field at Supersonic Aircraft Altitudes. Defense Technical Information Center. https://doi.org/10.21236/ad0656309
• Gringorten, Irving I., and Paul Tattelman. 1970. Point and Route Temperatures for Supersonic Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0712017
• Gro¨nstedt, Tomas U. J. 2002. “Identifiability in Multi-Point Gas Turbine Parameter Estimation Problems.” In Volume 2: Turbo Expo 2002, Parts A and B. ASMEDC. https://doi.org/10.1115/gt2002-30020
• Grosch, C. B., D. F. Nickel, H. R. Paetznick, R. W. Peterson, and B. D. Vannelli. 1967. Feasibility Study for a Scanning Celestial Attitude Determination System SCADS on the IMP Spacecraft Final Report. NASA-CR-95808. NASA. https://ntrs.nasa.gov/citations/19680020235
• Gross, L. W. 1976. “Comparison of Vortex Lattice Predicted Forces with Wind Tunnel Experiments for the F-4E(CCV) Airplane with a Closely Coupled Canard.” In NASA. Langley Res. Center Vortex-Lattice Utilization. https://ntrs.nasa.gov/citations/19760021090
• Gross, Jason, Yu Gu, Srikanth Gururajan, Brad Seanor, and Marcello Napolitano. 2010a. “A Comparison of Extended Kalman Filter, Sigma-Point Kalman Filter, and Particle Filter in GPS/INS Sensor Fusion.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8332
• Gross, Jason, Yu Gu, and Marcello Napolitano. 2010b. “A Systematic Approach for Extended Kalman Filter Tuning and Low-Cost Inertial Sensor Calibration within a GPS/INS Application.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7759
• Grossman, Daniel T. 1980. “F-15 Nose Landing Gear Shimmy, Taxi Test and Correlative Analyses.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/801239
• Groten, Erwin, and Dieter Keller. 1987. “GPS-Aided Inertial Positioning in Irregular Ocean Gravity Fields.” In Proceedings International Symposium on Marine Positioning. Springer Netherlands. https://doi.org/10.1007/978-94-009-3885-4_15
• Groutage, F. D. 1980. High Torque-to-Inertia Servo System for Stabilizing Sensor Systems. Candidate Systems Include Missile Guidance, Surveillance, and Tracking. Defense Technical Information Center. https://doi.org/10.21236/ada086705
• Groves, Paul D., Robin J. Handley, and Andrew R. Runnalls. 2005. “Optimising the Integration of Terrain Referenced Navigation with INS and GPS.” Journal of Navigation 59 (1): 71–89. https://doi.org/10.1017/s0373463305003462
• Grubin, C. 1973. “Attitude Determination for a Strapdown Inertial System Using the Euler Axis/angle and Quaternion Parameters.” In Guidance and Control Conference. AIAA 1973-900. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-900
• Grubin, C. 1975. “Accuracy Improvement in a Gravity Gradiometer-Aided Cruise Inertial Navigator Subjected to Deflections of the Vertical.” In Guidance and Control Conference. AIAA 1975-1090. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1090
• Grubin, C. 1979. “A Three-Axis Gravity Gradiometer.” In Guidance and Control Conference. AIAA 1979-1756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1756
• Grunwald, Warren, and Eric D. Swenson. 2015. “Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2015-0402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0402
• Gstattenbauer, Gregory, Milton Franke, and John Livingston. 2006. “Cost Comparison of Expendable, Hybrid, and Reusable Launch Vehicles.” In Space 2006. AIAA 2006-7211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7211
• Gu, Weizao, Wenyan Liu, and Jianping Tu. 1998. “Investigation on the Enhanced Cooling of Ramjet Engine Combustor.” In Proceeding of International Heat Transfer Conference 11. Begellhouse. https://doi.org/10.1615/ihtc11.1790
• Guan, Xiang Yi. 2012. “Verification of FLUENT in the Computation of Supersonic Inlet.” Advanced materials research 591-593: 2064–67. https://doi.org/10.4028/www.scientific.net/amr.591-593.2064
• Guan, Xiaohui. 2013. “Supersonic Bi-Directional Flying Wing Wave Drag Optimization Based on Alternative Form of CST Method.” Applied Mechanics and Materials 477-478: 240–45. https://doi.org/10.4028/www.scientific.net/amm.477-478.240
• Guan, X. 2014. “Supersonic Wing-Body Wave Drag Co-Ordinated Optimisation Based on FCE Methodology.” Aeronautical Journal 118 (1209): 1359–72. https://doi.org/10.1017/s0001924000010010
• Guan, Y., and S. Yarng. 1984. “A Linear Multivariable Dynamical Model of Supersonic Inlet-Engine Combination.” In 20th Joint Propulsion Conference. AIAA 1984-1496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1496
• Guan, Yan-Shen, and Shin Yarng. 1987. “Large Amplitude Supersonic Inlet Dynamics.” In 23rd Joint Propulsion Conference. AIAA 1987-2053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2053
• Guanghua, Wu. 1991. “An Optimal Estimating Method for Celestial Navigation.” Journal of Navigation 44 (2): 266–69. https://doi.org/10.1017/s037346330000998x
• Guangyue, Dai, Lei Zeng, Hongyin Jia, Lei Liu, Bo Qiu, and Yewei Gui. 2017. “Preliminary Study on the Influence of Aerothermoelastic Deformation on 2-D Hypersonic Inlet Performance.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2403
• Gueho, Damien, Puneet Singla, and Daning Huang. 2021a. “Sparse Nonlinear System Identification for Hypersonic Aerothermoelastic Analysis with Stochastic Loads.” In AIAA Scitech 2021 Forum. AIAA 2021-1609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1609
• Gueho, Damien, Puneet Singla, and Daning Huang. 2021b. “Time-Varying Linear Reduced Order Model for Hypersonic Aerothermoelastic Analysis.” In AIAA Scitech 2021 Forum. AIAA 2021-1706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1706
• Guelman, Moshe. 2004. “Boost Phase Interception of Ballistic Missiles.” In Threat of Ballistic Missiles in the Middle East. Liverpool University Press. https://doi.org/10.2307/jj.18654776.18
• Guelman, M., and O. M. Golan. 1995. “Minimum Energy Guidance for Boost Phase Ballistic Missile Interception.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 6. American Autom Control Council. https://doi.org/10.1109/acc.1995.532709
• Guerrier, Stéphane, Roberto Molinari, and Jan Skaloud. 2015. “Automatic Identification and Calibration of Stochastic Parameters in Inertial Sensors.” Navigation 62 (4): 265–72. https://doi.org/10.1002/navi.119
• Guess, M. K., R. S. Kaneko, and G. G. Wald. 1981. “Advanced Materials and Fabrication Processes for Supersonic Cruise Aircraft.” In NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2. https://ntrs.nasa.gov/citations/19810009488
• Guimarães, Thiago A., Carlos E. S. Cesnik, and Ilya Kolmanovsky. 2021. “Low Speed Aerodynamic Modeling for Control-Related Considerations in Supersonic Aircraft Design.” In AIAA Aviation 2021 Forum. AIAA 2021-2531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2531
• Guimaraes, Tamara B., Kevin T. Lowe, Michael Nelson, Walter F. O’Brien, and Caroline Kirk. 2015. “Stereoscopic PIV Measurements in a Turbofan Engine Inlet with Tailored Swirl Distortion.” In 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2015-2866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2866
• Gulick, Joseph F., and James S. Miller. 1982. Missile Guidance: Interferometer Homing Using Body-Fixed Antennas. Defense Technical Information Center. https://doi.org/10.21236/ada119957
• Gully, S., and E. Skelley. 1975. “Observers for Cruise Missile Autopilots.” In Guidance and Control Conference. AIAA 1975-1113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1113
• Guo, xiangying, tian Nan, yao Chen, weixing Zhang, and Dongxing Cao. 2024a. “Aircraft Nose Landing Gear Shimmy with Nonlinear Tyre Models.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-5335614/v1
• Guo, Xiangying, Tian Nan, Yao Chen, Weixing Zhang, and Dongxing Cao. 2025a. “Aircraft Nose Landing Gear Shimmy with Nonlinear Tire Models.” International Journal of Bifurcation and Chaos 35 (16): 2550184. https://doi.org/10.1142/s0218127425501846
• Guo, xiangying, Tian Nan, Yao Chen, Wei-Xing Zhang, and Dongxing Cao. 2025b. “Aircraft Nose Landing Gear Shimmy with Nonlinear Tyre Models.” Preprint, . https://doi.org/10.2139/ssrn.5105230
• Guo, Hongli, Shaofeng Ren, Huaiqiang Yan, Hongtao Zhao, Chunshuang Wei, and Yun Gao. 2022. “Compensation Analysis of Subsidence Angle of Supersonic Low-Altitude Cruise Target Projectile Launch.” Journal of Physics: Conference Series 2336 (1): 012011. https://doi.org/10.1088/1742-6596/2336/1/012011
• Guo, Kechen, Yulie Wu, Yongmeng Zhang, Dingbang Xiao, and Xuezhong Wu. 2020. “Adaptive Compensation of Damping Asymmetry in Whole-Angle Hemispherical Resonator Gyroscope.” AIP Advances 10 (10): 105109. https://doi.org/10.1063/5.0026821
• Guo, Kuiyuan, Kexin Zhang, and Xiaoqin Zhou. 2026c. “Deep Neural Network-Enhanced Integrated Navigation Using Global Navigation Satellite System and Inertial Navigation System for Vehicle Safety Testing.” Computer Journal: bxag067. https://doi.org/10.1093/comjnl/bxag067
• Guoxiang Gu, J. R. Cloutier, and Gisoon Kim. 1995. “Gain Scheduled Missile Autopilot Design Using Observer-Based H/sub ∞/ Control.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 3. American Autom Control Council. https://doi.org/10.1109/acc.1995.531228
• Gupta, S. C. 2023. “Wing Aerodynamic Optimization in the Presence of Interacting Canard at Subsonic and Supersonic Speeds.” Journal of Aerospace Sciences and Technologies: 303–12. https://doi.org/10.61653/joast.v68i4.2016.368
• Gupta, Kajal, Sang Choi, and Adem Ibrahim. 2010. “Development of a Aerothermoelastic-Acoustics Simulation Capability of Flight Vehicles.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-50. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-50
• Gupta, Anurag, Stephen Ruffin, Anurag Gupta, and Stephen Ruffin. 1997. “Aerothermodynamic Design of Supersonic Channel Airfoils for Drag Reduction.” In 1997 World Aviation Congress. AIAA 1997-5572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-5572
• Gurfil, Pini. 2012. “Neoclassical Missile Guidance.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-8
• Gusev, V. N., and A. A. Puporevich. 2021. “Improving Accuracy of Navigation Using Gyroscopes with Regard to Gyro Drift and Azimuth Error.” Mining informational and analytical bulletin, no. 10: 134–45. https://doi.org/10.25018/0236_1493_2021_10_0_134
• Gutierrez, Samuel T., Cesar I. Fuentes, and Marcos A. Diaz. 2017. “Open Hardware and Software Star Tracker: An Opportunity for Collaboration in the Emerging Cubesat Community.” Preprint, . https://doi.org/10.20944/preprints201703.0111.v1
• Guy, Yair, Thomas McLaughlin, and Julie Morrow. 2000. “Effects of Canard Shape on the Center of Pressure of a Generic Missile Configuration.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-264
• Guy, Yair, Thomas McLaughlin, and Julie Morrow. 2001. “Blunt Body Wave Drag Reduction by Means of a Standoff Spike.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-888. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-888
• Guy, Yair, Julie Morrow, and Thomas McLaughlin. 1999. “The Effects of Canard Shape on the Aerodynamic Characteristics of a Generic Missile Configuration.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4256
• “Gyroscope Technology 1.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch4
• “Gyroscope Technology 2.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch5
• G�bel, Mario, Thomas Kr�ger, Stefan Nowak, Jan Meifarth, and Ulf Bestmann. 2017. “Multisensor Concept for Autonomous Navigation of Unmanned Systems in GNSS-Denied Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2017.15410
• Ha, Cheolkeun, and Sang-Won Ahn. 2004. “Longitudinal Automatic Landing in AdaptivePID Control Law under Wind Shear Turbulence.” International Journal of Aeronautical and Space Sciences 5 (1): 30–38. https://doi.org/10.5139/ijass.2004.5.1.030
• Ha, Cheolkeun, and Jong-kwon Kim. 2005. “Automatic Landing under Wind Shear Turbulence in Adaptive Gain Scheduled PID Control Optimized in Genetic Algorithm.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6346
• Ha, Jong-Soo, Han-Jin Lee, SooJi Lee, and Sung-Yong Hong. 2022. “Performance Analysis of Interferometric Radar Altimeter by Terrain Type for Estimating Reliability of Terrain Referenced Navigation.” Journal of the Korean Society for Aeronautical & Space Sciences 50 (2): 83–92. https://doi.org/10.5139/jksas.2022.50.2.83
• Haak, Jeffrey W. 1994. Verification of Robustified Kalman Filters for the Integration of Global Positioning System (GPS) and Inertial Navigation System (INS) Data,. Defense Technical Information Center. https://doi.org/10.21236/ada288609
• Haas, M., and A. Karanian. 1980. “Small-Scale Supersonic Inlet Test Facility.” In 16th Joint Propulsion Conference. AIAA 1980-1145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1145
• Hadaegh, F. Y., and G. A. Bekey. 1987. “Identifiability of Systems with Modeling Error — A New Formulation.” In Identifiability of Parametric Models. Elsevier. https://doi.org/10.1016/b978-0-08-034929-9.50013-3
• Haderlie, Jacob, and William Crossley. 2010. “Multiobjective Optimization of a Supersonic-Inlet Bypass-Duct Splitter via Surrogate Modeling.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9170
• Hadfield, M. 1980. “Field Test Results on the GEO-SPIN ESG Inertial Positioning System.” In Guidance and Control Conference. AIAA 1980-1756. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1756
• Hageman, Jacob, Mark Smith, and Susan Stachowiak. 2003. “Integration of Online Parameter Identification and Neural Network for in-Flight Adaptive Control.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20030112874
• Hagerman, Larry Leon. n.d. “An Optimum Doppler-Satellite Inertial Navigation System.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180817-1972
• Hagopian, Jeff. 2002. “2nd Generation Reusable Launch Vehicle-Concepts for Flight Operations.” In SpaceOps 2002 Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-t3-55
• Hahne, David E. 1989. Low-Speed Static and Dynamic Force Tests of a Generic Supersonic Cruise Fighter Configuration. NASA-TM-4138. NASA. https://ntrs.nasa.gov/citations/19890019115
• Hahne, David E. 1997. Evaluation of the Low-Speed Stability and Control Characteristics of a Mach 5.5 Waverider Concept. NASA-TM-4756. NASA. https://ntrs.nasa.gov/citations/19970022891
• Haitjema, Anne. 2026. “Drift Happens: Advancing Calibration-Free Kinematic Estimation with a Minimal Inertial Sensor Set.” PhD diss.. https://doi.org/10.3990/1.9789036574723
• Hajiyev, Chingiz. 2026. “Difference Kalman Filter Robust to Systematic Measurement Errors Related to Inertial Navigation.” Proceedings of the Technical University of Sofia 76 (3). https://doi.org/10.47978/tus.2026.76.03.002
• Halasey, R. L., and R. B. Noll. 1963. Theoretical Investigation of the Slideout Dynamics of a Vehicle Equipped with a Tricycle Skid-Type Landing-Gear System. NASA-TN-D-1828. NASA. https://ntrs.nasa.gov/citations/19630006422
• Hale, Alan, Milt Davis, and Jim Sirbaugh. 2004. “A Numerical Simulation Capability for Analysis of Aircraft Inlet-Engine Compatibility.” Journal of Engineering for Gas Turbines and Power 128 (3): 473–81. https://doi.org/10.1115/1.1925649
• Halim, Lenard J., Sejal Sahu, Graeme Kennedy, and Marilyn J. Smith. 2022. “Aerothermoelastic Analysis and Optimization of Stiffened Thin-Walled Structures.” In AIAA SCITECH 2022 Forum. AIAA 2022-1612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1612
• Hall, J. R. 1952a. Free-Flight Investigation of Longitudinal and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Inline Wings and Tails. NACA-RM-L51J17. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19680068636
• Hall, James R. 1952b. Free-Flight Investigation of Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Inline Wings and Tails. NACA-RM-L51J17. NASA. https://ntrs.nasa.gov/citations/19930086932
• Hall, James Rudyard. 1956a. Effect of Wing Size and Amount of Indentation on Applicability of Transonic Area Rule to Swept-Wing Configurations. NACA-RM-L55F03. NASA. https://ntrs.nasa.gov/citations/19930088762
• Hall, James Rudyard. 1956b. Two Experiments on Applications of the Transonic Area Rule to Asymmetric Configurations. NACA-RM-L56A25. NASA. https://ntrs.nasa.gov/citations/19930089202
• Hall, Les. 2002. “Chimera Moving Body Methodology for Rolling Airframe Missile Simulation with Dithering Canards.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2801
• Hall, Elyse G., Justin W. Foster, and William P. England. 2023. “Development of an Aerothermoelastic Framework for Resolving Hypersonic Flow around a Maneuverable Vehicle.” In AIAA AVIATION 2023 Forum. AIAA 2023-4133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4133
• Hall, J. R., and C. A. Sandahl. 1951. Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails. NACA-RM-L51B15. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19680068689
• Hall, Elyse G., Avery J. Schemmel, and Justin Foster. 2026. “Coupling Fidelity and Stability in a Trajectory-Resolved Aerothermoelastic Analysis of a Maneuvering Hypersonic Vehicle.” In AIAA AVIATION 2026 Forum. AIAA 2026-4402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4402
• Hall, Charles, and Yuri Shtessel. 2005. “Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6145
• Hall, John J., Robert L. Williams, and Frank van Graas. 2000. “Cartesian Control for the Inertial Measurement Unit Calibration Platform.” In Volume 7A: 26th Biennial Mechanisms and Robotics Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/detc2000/mech-14112
• Hallstaff, T. 1966. “Aerodynamics of Powerplant Installation on Supersonic Aircraft.” In 2nd Propulsion Joint Specialist Conference. AIAA 1966-665. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-665
• Halyo, N. 1977. Development of a Digital Automatic Control Law for Steep Glideslope Capture and Flare. NASA-CR-2834. NASA. https://ntrs.nasa.gov/citations/19770018205
• Halyo, N. 1979. Development of a Digital Guidance and Control Law for Steep Approach Automatic Landings Using Modern Control Techniques. NASA-CR-3074. NASA. https://ntrs.nasa.gov/citations/19790008653
• Halyo, N. 1984. Flight Tests of the Digital Integrated Automatic Landing System (DIALS). NASA-CR-3859. NASA. https://ntrs.nasa.gov/citations/19850004592
• Halyo, Nesim. 1987. A Combined Stochastic Feedforward and Feedback Control Design Methodology with Application to Autoland Design. NASA-CR-4078. NASA. https://ntrs.nasa.gov/citations/19870016373
• Halyo, N., and R. M. Hueschen. 1981. “Development of a Digital Integrated Automatic Landing System (DIALS) for Steep Approach and Landing.” In Joint Automatic Control Conference, University of Virginia. https://ntrs.nasa.gov/citations/19820036762
• Ham, Byoung S. 2022a. “Optical Quantum Sensing for Ring Laser Gyroscope.” In Optica Advanced Photonics Congress 2022. Optica Publishing Group. https://doi.org/10.1364/bgppm.2022.jtu2a.5
• Hamada, Tsubasa. 2020. “Uncertainty Quantification for Aerodynamic Characteristics in LES.” Wind Engineers JAWE 45 (2): 145–48. https://doi.org/10.5359/jawe.45.145
• Hamada, Tsubasa, and Tetsuro Tamura. 2019. “Uncertainty Quantification on Aerodynamic Characteristics of Flow around Square and Corner-Rounded Cylinder with Glancing Angle.” In Proceedings of the 3rd International Conference on Uncertainty Quantification in Computational Sciences and Engineering (UNCECOMP 2019). Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece. https://doi.org/10.7712/120219.6370.18497
• Hamed, Awatef, Keith Numbers, Awatef Hamed, and Keith Numbers. 1997. “Inlet Distortion Considerations for High Cycle Fatigue in Gas Turbine Engine.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3364
• Hammad, May, Menatallh Hammad, Atheel Redah, and Sérgio Montenegro. 2024. Innovative Artificial Intelligence-Based Star Tracker for Deep Space Exploration. https://doi.org/10.52202/078363-0020
• Hampton, D. E., and J. R. Mills. 1964. “The Long-Range Navigation of Civil Aircraft.” Journal of Navigation 17 (2): 167–82. https://doi.org/10.1017/s0373463300048530
• Han, Lit S. 1971. Air Cushion Pressure during Stiff-Operation for Air Cushion Landing System. Part 1. Theory. Defense Technical Information Center. https://doi.org/10.21236/ad0726606
• Han, Hongxiang, Jun Fu, and Duanyang Gao. 2018c. “Research on the Fast Calibration Method of MEMS Gyroscope.” In Global Intelligence Industry Conference (GIIC 2018), edited by Yueguang Lv. SPIE. https://doi.org/10.1117/12.2505175
• Han, Jiwoo, Woojin Kim, Eun Hye Jang, et al. 2026a. “Human Responses to Network Latency in Level 4 Autonomous Vehicle Teleoperation: From Perception–Control Breakdown to Trust Decay.” In Proceedings of the Extended Abstracts of the 2026 CHI Conference on Human Factors in Computing Systems. ACM. https://doi.org/10.1145/3772363.3798932
• Han, Kyung Jun, and Chan Gook Park. 2024. “Modified Interactive Multiple Model Particle Filter for Terrain Referenced Navigation with Classification Error Minimisation Strategy.” IET Radar, Sonar & Navigation 18 (8): 1247–59. https://doi.org/10.1049/rsn2.12564
• Han, Sangjin, and Paul Sabbagh. 2022. Integration of the ADIS16465 Tactical-Grade Inertial Sensor with the Open-Source Pixhawk Autopilot and PX4 Flight Stack. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1169845
• Hancock, B., C. Liebe, and B. Pain. 1997. Active Pixel Sensor (APS) Based Star Tracker. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210005218
• Hand, J. 1968. “Computer-Aided Inertial Platform Realignment in Manned Space Flight.” In Control and Flight Dynamics Conference. AIAA 1968-838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-838
• Hand, P. J. 1974. Temperature Compensated Digital Inertial Sensor. Patent Number: NASA-CASE-NPO-13044-1. NASA Pasadena Office. https://ntrs.nasa.gov/citations/19740006981
• Hanin, M. 1983. “Roll Divergence of a Canard-Controlled Missile with Freely Spinning Tail.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2080
• Hansen, O. M., Y. K. Pang, and J. S. White. 1963. Study of Inertial Navigation Errors during Reentry to the Earth’s Atmosphere. NASA-TN-D-1772. NASA. https://ntrs.nasa.gov/citations/19630005597
• Hao, Qiao, Sun Peng, and Li Xinguo. 2017. “United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2108
• Harcaut, J., D. Farret, and G. Duc. 2001. “Multirate H-Infinity Loop-Shaping Control Applied to Missile Autopilot Design.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4283. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4283
• Harder, Keith C., and E. B. Klunker. 1956. On Slender-Body Theory and the Area Rule at Transonic Speeds. NACA-TN-3815. NASA. https://ntrs.nasa.gov/citations/19930084626
• Harding, J. T. 1965. Drift Data for the Cryogenic Gyro. NASA. https://ntrs.nasa.gov/citations/19650051614
• Hardouin, Jean. 1961. “Navigation Equipment for Subsonic and Supersonic Long-Range Jet Transports.” Navigation 8 (2): 133–35. https://doi.org/10.1002/j.2161-4296.1961.tb02476.x
• Hardy, Jeremy. n.d. “Sensitivity Analysis of a Relative Navigation Solution for Unmanned Aerial Vehicles in a GNSS-Denied Environment.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.5763
• Hardy, S. 1978. “Nonlinear Rolling Motion of a Canard-Controlled Missile Configuration at Angles of Attack from 0 to 30 Degrees in Incompressible Flow.” In 16th Aerospace Sciences Meeting. AIAA 1978-61. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-61
• Hardy, R., L. Eldrenkamp, and D. Ruzicka. 1993. “A Reusable Two-Stage Launch Vehicle.” In Space Programs and Technologies Conference and Exhibit. AIAA 1993-4161. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4161
• Hariton, Eliot D., and Aaron Swank. 2015. “Tool for Optimizing Star Tracker and IMU Configuration.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0334. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0334
• Harl, Nathan. 2008. “Reentry Terminal Guidance through Sliding Mode Control.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6215
• Harl, Nathan, S. Balakrishnan, and Craig Phillips. 2010. “Sliding Mode Integrated Missile Guidance and Control.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7741
• Harloff, Gary, and Gregory Smith. 1995. “On Supersonic-Inlet Boundary-Layer Bleed Flow.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-38. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-38
• Haroldsen, David. 2000. “Navier-Stokes Computations of Finned Missiles at Supersonic Speeds.” In 18th Applied Aerodynamics Conference. AIAA 2000-4208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4208
• Harri, J. 1964. The Aerodynamic Heating of a Vehicle Traveling at Supersonic Velocities through a Compressible Fluid. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4597699
• Harriman, D., and J. Harrison. 1984. “A Statistical Analysis of Gravity-Induced Errors in Airborne Inertial Navigation.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1877
• Harris, C. W. 1959. “Quality Assurance for Missile Reliability.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/590172
• Harris, K. E. 1961. “Discussion on “Radio Guidance Elements of the B.L.E.U. Automatic Landing System for Aircraft”.” Journal of the British Institution of Radio Engineers 21 (1): 32–33. https://doi.org/10.1049/jbire.1961.0005
• Harris, White J. 1969. Turbojet Engine Analyzer System. Defense Technical Information Center. https://doi.org/10.21236/ad0856377
• Harris, C. D., and D. W. Bartlett. 1972. Tabulated Pressure Measurements of a NASA Supercritical-Wing Research Airplane Model with and without Fuselage Area-Rule Additions at Mach 0.25 to 1.00. NASA-TM-X-2634. NASA. https://ntrs.nasa.gov/citations/19780016134
• Harris, Paul, Rocco Farinaccio, and Robert Ripley. 2004b. “Multi-Tube Two-Dimensional Evaluation of a Pulse Detonation Engine as a Ramjet Replacement.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3745
• Harris, Paul, R. Ripley, and Stephen Guzik. 2004c. “Single-Tube Two-Dimensional Evaluation of a Pulse Detonation Engine as a Ramjet Replacement.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3744. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3744
• Harris, Paul, Robert Stowe, and S. Guzik. 2004a. “Design Methodology for a Pulse Detonation Engine as a Ramjet Replacement.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3400
• Harris, R., Jr. 1965. “Recent Research Results in the Aerodynamics of Supersonic Vehicles.” In Aircraft Design and Technology Meeting. AIAA 1965-717. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-717
• Harrison, D., and W. Lockman. 1968. “Heat-Transfer Telemetry from Free-Flight Models in Wind Tunnels. II.” In 3rd Aerodynamics Testing Conference. AIAA 1968-407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-407
• Harrison, R., and W. Marko. 1968. “Heat-Transfer Telemetry from Free-Flight Models in Wind Tunnels. I.” In 3rd Aerodynamics Testing Conference. AIAA 1968-406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-406
• Hart, K. G. 1956. Automatic Flight Control Systems for Piloted Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0108104
• Hart, Pierce, and Sven Schmitz. 2022a. “A Partial Pressure Field for Airfoil Wave Drag.” In AIAA SCITECH 2022 Forum. AIAA 2022-2482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2482
• Hart, Pierce, Anja Vogel, Freya Bradley, and Sven Schmitz. 2025. “A near-Field CFD Method for Wave Drag Decomposition.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3430. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3430
• Hartana, Pande. n.d. “Comparison of Linearized and Extended Kalman Filter in GPS Aided Inertial Navigation System.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2000-04613
• Hartl, Derek. n.d. “Alignment Determination and Error Characterisation of Inertial Components for Use in an Airborne Gravimeter.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1995-03003
• Hartl, Engelbert, Gert F. Trommer, R. Mueller, and Hans Poisel. 1992. “Low-Cost Passive Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 1585, edited by Shaoul Ezekiel, Eric Udd. SPIE. https://doi.org/10.1117/12.135073
• Hartman, Andrea, William Long, and Lisa Veitch. 2001. Quiet Supersonic Platform (QSP) Materials and Structures Focus Group Meeting, 26 June 2001. Defense Technical Information Center. https://doi.org/10.21236/ada408538
• Hartwell, T., H. A. Irwin, Y. Miyatake, and D. E. Wedekind. 1971. General Test Plan Redundant Sensor Strapdown IMU Evaluation Program. NASA-CR-130722. NASA. https://ntrs.nasa.gov/citations/19730008985
• Harvey, W. D. 1967. Instrumenting Models for Aerodynamic Heat- Transfer Studies Involving Transient Heating Rates. NASA. https://ntrs.nasa.gov/citations/19670046097
• Hashim, Hadzli. n.d. “Implementing the Extended Kalman Filter for Loran-C Navigation.” PhD diss., Drexel University. https://doi.org/10.17918/00009422
• Hashmall, Joseph A. 2003. Star Identification Using a Triplet Algorithm. Computer Sciences Corp. https://ntrs.nasa.gov/citations/20030053380
• Hashmall, Joseph A., Gregory Natanson, Jonathan Glickman, and Joseph Sedlak. 2004. Compensation for Time-Dependent Star Tracker Thermal Deformation on the Aqua Spacecraft. AI Solutions, Inc. https://ntrs.nasa.gov/citations/20040171520
• Haskins, Glenn. 2000. “Embedded Adaptive Optimally Guided Missile Controller.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4071
• Hassan, Jafar M., Laith K. Abbass, and Laith W. Ismail. 2010. “Investigation and Modification of Aerodynamic Characteristics of Supersonic Aircraft.” Journal of Engineering 16 (03): 5606–19. https://doi.org/10.31026/j.eng.2010.03.21
• Hattenberger, Gautier, Fabien Bonneval, Matheus Ladeira, Emmanuel Grolleau, and Yassine Ouhammou. 2023. “Design of Micro-Drone Autopilot Architecture with Static Scheduling Optimization.” Unmanned Systems 12 (03): 565–78. https://doi.org/10.1142/s2301385024430015
• Haussler, J. 1967. “Powered Flight Trajectory Determination Techniques as Applied to Saturn V Vehicles.” In Control and Flight Dynamics Conference. AIAA 1967-547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-547
• Hawkins, W., and E. Marquart. 1995. “Two-Dimensional Generic Inlet Unstart Detection at Mach 2.5-5.0.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6019
• Haydon, Tucker. 2025. Earth-Centered, Earth-Fixed Inertial Navigation System & Error-State Kalman Filter Reference Manual. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/2516824
• Haydon, Tucker, Andy Huang, and Todd E. Humphreys. 2025. “Analysis of the Trusted Inertial Terrain-Aided Navigation Measurement Function.” NAVIGATION: Journal of the Institute of Navigation 72 (3): navi.707. https://doi.org/10.33012/navi.707
• Haydon, Tucker, and Todd E. Humphreys. 2023. “Trusted Inertial Terrain-Aided Navigation (TITAN).” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2023.19409
• Hayes, R. J. 1968. Strapdown Guidance Component Research. NASA Electronics Research Center. https://ntrs.nasa.gov/citations/19690027493
• Hayslett, Charles R., Joe L. Rosson, and William H. Swantner. 1978. “Testing and Analysis of Optical Components and Systems at White Sands Missile Range.” In SPIE Proceedings, vol. 0134, edited by Walter J. Carrion, Jed E. Durrenberger, Richard K. Petersen, John Cornell. SPIE. https://doi.org/10.1117/12.956086
• Hayworth, Ken. 2003. Continuous Tuning and Calibration of Vibratory Gyroscopes. NPO-30449. California Inst. of Tech. https://ntrs.nasa.gov/citations/20110023987
• He, Xufei. 2018. “Shimmy Simulation and Virtual Verification for Civil Aircraft Landing Gear Airworthiness Certification.” Journal of Mechanical Engineering 54 (1): 179. https://doi.org/10.3901/jme.2018.14.179
• He, Xufei, Jianliang Ai, and Zhitao Song. 2018. “Shimmy Simulation and Virtual Verification for Amphibious Aircraft’s Landing Gear Airworthiness Certification.” In 2018 Modeling and Simulation Technologies Conference. AIAA 2018-3896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3896
• He, Shaoming, Chang-Hun Lee, Hyo-Sang Shin, and Antonios Tsourdos. 2020c. “Optimal Error Dynamics in Missile Guidance.” In Springer Aerospace Technology. Springer International Publishing. https://doi.org/10.1007/978-3-030-47348-8_2
• He, Shaoming, Defu Lin, and Jiang Wang. 2015a. “Compound Control Methodology for a Robust Missile Autopilot Design.” Journal of Aerospace Engineering 28 (6): 04014145. https://doi.org/10.1061/(asce)as.1943-5525.0000484
• He, Chenxin, Zuohong Liu, Zhongyi Wang, Lei Gao, and Guanglei Xu. 2023. “Effect of Insert Plate on the Inlet Pressure Distortion of the Aero-Engine.” Advances in Mechanical Engineering 15 (10): 16878132231200562. https://doi.org/10.1177/16878132231200562
• He, Zhikun, Guangbin Liu, Zhao Xijing, and Zhicheng Yao. 2013a. “A Novel Comprehensive Compensation Approach for Fiber Optic Gyroscope Temperature Drift by Gaussian Process Regression.” Journal of Convergence Information Technology 8 (1): 134–42. https://doi.org/10.4156/jcit.vol8.issue1.17
• He, Kunpeng, Yuping Shao, Xiaoxue Wang, and Chenyang Wang. 2015c. “A Novel Redundant Inertial Measurement Unit and Error Compensation Technology.” In Information Technology and Applications. CRC Press. https://doi.org/10.1201/b18284-28
• He, Fenghua, Long Wang, Yu Yao, Denggao Ji, and Weishan Chen. 2013b. “The Terminal Guidance System Performance Analysis: A Finite-Time Gain Measurement Approach.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4930
• He, Dinglong, and Zhonghui Wei. 2024. “A Multimodal Approach for Attitude Measurement of near-Earth Daytime Star Sensors.” Traitement du Signal 41 (1): 283–92. https://doi.org/10.18280/ts.410123
• Headrick, J. M., F. H. Utley, and C. B. Tesauro. 1967. Information on over-the-Horizon Radar. Part 14. HF Radar Performance at More than One Hop. Defense Technical Information Center. https://doi.org/10.21236/ada472348
• “Heat Recovery from Reciprocating Engine for Ramjet Power Augmentation.” 2021. In Applying Engineering Thermodynamics. WORLD SCIENTIFIC. https://doi.org/10.1142/9789811205248_0012
• Heathman, John, and Larry Kelly. 1966. “Hydrogen Tankage for Hypersonic Cruise Vehicles.” In 7th Structures and Materials Conference. AIAA 1966-1740. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1740
• Heatwole, Scott. n.d. “Star Trackers for Suborbital Applications.” In Star Tracker Working Group. https://ntrs.nasa.gov/citations/20260007210
• Heatwole, Scott. 2019. Low Cost Star Tracker for Suborbital Platforms Design and Flight. GSFC-E-DAA-TN75548. NASA Wallops Flight Facility. https://ntrs.nasa.gov/citations/20190033456
• Hebbar, Sheshagiri, Max Platzer, and Da-Ming Liu. 1993. “Effect of Canard Oscillations on the Vortical Flowfield of a X-31A-like Fighter Model in Dynamic Motion.” In 11th Applied Aerodynamics Conference. AIAA 1993-3427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3427
• Heck, M., J. Findlay, G. Kelly, and H. Compton. 1982. “The Adaptation of a Strap down Formulation for Processing Inertial Platform Data.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1332
• Heeg, Jennifer, Michael Gilbert, and Anthony Pototzky. 1990. “Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft.” In Guidance, Navigation and Control Conference. AIAA 1990-3337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3337
• Heeg, Jennifer, Thomas Zeiler, Anthony Pototzky, Charles Spain, and Walter Engelund. 1993b. “Aerothermoelastic Analysis of a NASP Demostrator Model.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1366
• Hefti, Larry D. 2012. “Elevated Temperature Forming of Titanium Aircraft Hardware.” In Materials science forum, vol. 735. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.735.338
• Heimerl, George J., and Herbert F. Hardrath. 1965. “An Assessment of a Titanium Alloy for Supersonic Transport Operations.” In NASA Conference on Aircraft Operating Problems: A Compilation of the Papers Presented. https://ntrs.nasa.gov/citations/20000011991
• Hein, GÜNTER W., Gerald Baustert, Bernd Eissfeller, and Herbert Landau. 1989. “High-Precision Kinematic GPS Differential Positioning and Integration of GPS with a Ring Laser Strapdown Inertial System.” Navigation 36 (1): 77–98. https://doi.org/10.1002/j.2161-4296.1989.tb00982.x
• Heineck, James T., Daniel Banks, Edward T. Schairer, Edward A. Haering, and Paul Bean. 2016. “Background Oriented Schlieren (BOS) of a Supersonic Aircraft in Flight.” In AIAA Flight Testing Conference. AIAA 2016-3356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3356
• Heiser, Melissa, and John Burkhalter. 2002. “Linear Aerodynamic Analysis of a Spinning Missile with Dithering Canards.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2800. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2800
• Heller, W., and S. Jordan. 1975. “Mechanization and Error Equations for Two New Gradiometer-Aided Inertial Navigation System Configurations.” In Guidance and Control Conference. AIAA 1975-1091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1091
• Hellings, Frazier J. 1973. Application of Extended Kalman Filtering to a Dynamic Laboratory Calibration of an Inertial Navigation System. Defense Technical Information Center. https://doi.org/10.21236/ad0763718
• Helliwell, J. B. 1952. “The Automatic Control of an Aeroplane in the Landing Approach onto an Aircraft Carrier.” Aeronautical Quarterly 3 (4): 241–62. https://doi.org/10.1017/s0001925900000688
• Hellman, H. 1962. “The Development of Inertial Navigation.” Navigation 9 (2): 83–94. https://doi.org/10.1002/j.2161-4296.1962.tb02557.x
• Hemsch, M. 1985. “Nonlinear Applications of Slender-Body Theory to Missile Aerodynamics.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1775. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1775
• Hemsch, Michael J., and Jack N. Nielsen. 1986. Tactical Missile Aerodynamics. PRC Kentron, Inc. https://ntrs.nasa.gov/citations/19870035652
• Henderson, W. P. 1974. The Effect of Canard and Vertical Tails on the Aerodynamic Characteristics of a Model with a 59 Deg Sweptback Wing at a Mach Number of 0.30. NASA-TM-X-3088. NASA. https://ntrs.nasa.gov/citations/19740024299
• Henderson, Dennis. 1999. “Impacts of Structural Dynamics on Inlet Flow Incidence Angle and Inlet Unstart.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-369. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-369
• Henning, Allen B. 1954. The Effects of Wing-Mounted External Stores on the Trim, Buffet, and Drag Characteristics of a Rocket-Propelled Model Having a 45 Degree Sweptback Wing. NACA-RM-L54B19. NASA. https://ntrs.nasa.gov/citations/19930090493
• Henning, Allen B. 1957. Effects of Wing Inboard Plan-Form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-Propelled Free-Flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3. NACA-RM-L57D29. NASA. https://ntrs.nasa.gov/citations/19930089916
• Henry, J., F. Guyon, and J. P. Yvon. 1990. “Optimal Weighting for Improving Practical Identifiability in DPS Parameter Estimation Problems.” In Control of Distributed Parameter Systems 1989. Elsevier. https://doi.org/10.1016/b978-0-08-037036-1.50067-7
• Hepburn-Dickins, Floyd. n.d. “Machine Learning Using Graph Neural Networks for Star Identification in Celestial Navigation.” PhD diss., Swansea University. https://doi.org/10.23889/suthesis.72245
• Hepler, A. K., H. Zeck, W. Walker, and W. Scharf. 1979. A Turbojet-Boosted Two-Stage-to-Orbit Space Transportation System Design Study. NASA-CR-159018. NASA. https://ntrs.nasa.gov/citations/19790015826
• Herges, Thomas, J. Dutton, and Gregory Elliott. 2012. “High-Speed Schlieren Analysis of Buzz in a Relaxed-Compression Supersonic Inlet.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-4146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4146
• Herling, W., F. Saheli, J. Holcomb, and R. Hanson. 1985. “Prediction of the Steady Three-Dimensional Aerodynamics of a Supersonic Ramjet Missile.” In 21st Joint Propulsion Conference. AIAA 1985-1121. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1121
• Hermann, Rudolf. 1950. Diffuser Efficiency and Flow Process of Supersonic Wind Tunnels with Free Jet Test Section. Defense Technical Information Center. https://doi.org/10.21236/ada377566
• Hermann, Rudolf. 1956. “Engine Inlet Air Diffuser Controls for Supersonic Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/560270
• Herrera, Linda M. 2010. “Space Shuttle Star Tracker Challenges.” In Department of Defense. https://ntrs.nasa.gov/citations/20110003998
• Herrick, Samuel. 1946. “Instrumental Solutions in Celestial Navigation.” Navigation 1 (2): 22–27. https://doi.org/10.1002/j.2161-4296.1946.tb01079.x
• Herrmann, Emily G., Adam Cox, and Dimitri Mavris. 2025. “Multidisciplinary Design and Analysis of a Hypersonic Glide Vehicle with Trimmed Aerodynamics.” In AIAA SCITECH 2025 Forum. AIAA 2025-1338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1338
• Herrmann, U., and M. Orlowski. 1997. “Numerical Aerodynamic Optimization Study for a Supersonic Aircraft.” In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-86573-1_24
• Herrmann, H., and H. Rick. 1991. “Propulsion Aspects of Hypersonic Turbo-Ramjet-Engines with Special Emphasis on Nozzle/Aftbody Integration.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-395
• Hertel, R., and I. Lowen. 1970. “Scanning Celestial Attitude Determination System for a Stabilized Satellite.” In ELECTRO-OPTICAL SYSTEMS DESIGN CONFERENCE. https://ntrs.nasa.gov/citations/19700057043
• Hervas, Jaime Rubio, Mahmut Reyhanoglu, and Hui Tang. 2014b. “Nonlinear Automatic Landing Control of Unmanned Aerial Vehicles on Moving Platforms via a 3D Laser Radar.” In AIP Conference Proceedings, vol. 1637. AIP Publishing LLC. https://doi.org/10.1063/1.4904663
• Heryana, Ana, Dikdik Krisnandi, Hilman Pardede, et al. 2022. “Realtime Video Latency Reduction for Autonomous Vehicle Teleoperation Using RTMP over UDP Protocols.” In Proceedings of the 2022 International Conference on Computer, Control, Informatics and Its Applications. ACM. https://doi.org/10.1145/3575882.3575891
• Herzog, J., Y. Yue, and R. Bickford. 1998. “Dynamics Sensor Validation for Reusable Launch Vehicle Propulsion.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3604
• Hess, R. 1989. “Self-Tuning Generalized Predictive Control Applied to Terrain Following Flight.” In Guidance, Navigation and Control Conference. AIAA 1989-3450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3450
• “Heterogeneous Engineering and the Origins of the Fleet Ballistic Missile.” 1994. In From Polaris to Trident. Cambridge University Press. https://doi.org/10.1017/cbo9780511559136.003
• Hetherington, Samuel, Dean Osgood, Joe McMann, Viki Roberts, James Gill, and Kyle McLean. 2013. “Optical Alignment of the Global Precipitation Measurement (GPM) Star Trackers.” In International Society for Optical Engineering. https://ntrs.nasa.gov/citations/20160000787
• High, D., and W. Bowman. 1995. “A Shock Tube Study of Aerodynamic Heating of Gaps in a Cylinder Subjected to Supersonic Cross Flow.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-157
• High-Speed Schlieren Movies of the Flow about Reefed Parachute Models Towed at Supersonic Speeds behind a Conical Body (4.875 Inches in Diameter). Drag Values Based on the Unreefed Diameter of 1.73 F. Porosity of Unreefed Parachute Is 28 Percent. 1960. L-556. Langley Research Center. https://ntrs.nasa.gov/citations/20070030948
• “Higher-Order Sliding Modes for Missile Guidance and Control.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-14
• Hildebrand, R. 1979. “The Air Launched Cruise Missile Flight Test Status.” In Aircraft Systems and Technology Meeting. AIAA 1979-1787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1787
• Hildebrand, Roland, and Michel Gevers. 2002. “Identification for Control: Optimal Input Design with Respect to a Worst-Case Nu-Gap Cost Function.” SIAM Journal on Control and Optimization 41 (5): 1586–1608. https://doi.org/10.1137/s0363012901399866
• Hilgemann, Evan, Hunter Ruch, and James W. Cutler. 2016. “Development of Rate Gyroscope Characterization Tools with Application to Helium Exposure Testing.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0143
• Hiller, K. W., and D. I. Drain. 1976. “Control of Propulsion Systems for Supersonic Cruise Aircraft.” In Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011072
• Himmel, Seymour C. 1952. Some Control Considerations for Ram-Jet Engines / c Seymour Himmel. NACA-RM-E52F10. NASA. https://ntrs.nasa.gov/citations/19930090440
• Himpler, H. P. 1975. Design-To-Cost Monitoring System for Cruise Missile Project. Defense Technical Information Center. https://doi.org/10.21236/ada051820
• Hinchey, J. 1968. “Some Basic Guidelines for Establishing Structural Design Parameters for the Landing Gear of Stable, Soft Landing Spacecraft.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-345
• Hinchliffe, Benjamin L., and Ning Qin. 2016. “Using Surface Sensitivity from Mesh Adjoint Solution for Transonic Wing Drag Reduction.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0560
• Hintz, J., and E. J. Saltzman. 1967. Flight Evaluation of Splitter-Plate Effectiveness in Reducing Base Drag at Mach Numbers from 0.65 to 0.90. NASA-TM-X-1376. NASA. https://ntrs.nasa.gov/citations/19670017229
• Hirokawa, Rui, Koichi Sato, and Shunji Manabe. 2001. “Autopilot Design for a Missile with Reaction-Jet Using Coefficient Diagram Method.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4162
• Hirsch, Markus, and Luigi del Re. 2009. “Sequential Identification of Engine Subsystems by Optimal Input Design.” SAE International Journal of Engines 02 (2): 562–69. https://doi.org/10.4271/2009-24-0132
• Hirshon, Sidney. 1964. “Inertial System Capabilities Applied to SST Operation.” Navigation 11 (3): 237–49. https://doi.org/10.1002/j.2161-4296.1964.tb02098.x
• History of Supersonic Transport Aircraft Development. 2020. Wiley. https://doi.org/10.1002/9781119667063.ch1
• Hledik, J. 1963. “Simulation Techniques to Investigate the Controllability of an Electro-Optically Guided Missile.” In Heterogeneous Combustion Conference. AIAA 1963-1033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1033
• Hodge, J., and D. Audley. 1983. “Aerothermodynamic Parameter Estimation from Space Shuttle Thermocouple Data during Transient Flight Test Maneuvers.” In 21st Aerospace Sciences Meeting. AIAA 1983-482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-482
• Hodgson, Jeremy, and David Lee. 2003. “Terminal Guidance Using a Doppler Beam Sharpening Radar.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5796. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5796
• Hoenk, Michael E. 1994. “Small Inertial Measurement Units: Sources of Error and Limitations on Accuracy.” In SPIE Proceedings, vol. 2220, edited by Jacques G. Verly, Sharon S. Welch. SPIE. https://doi.org/10.1117/12.179603
• Hoffman, Sherwood. 1953. An Investigation of the Transonic Area Rule by Flight Tests of a Sweptback Wing on a Cylindrical Body with and without Body Indentation between Mach Numbers 0.9 and 1.8. NACA-RM-L53J20a. NASA. https://ntrs.nasa.gov/citations/19930087956
• Hoffman, Sherwood. 1954. A Flight Investigation of the Transonic Area Rule for a 52.5 Degree Sweptback Wing-Body Configuration at Mach Numbers between 0.8 and 1.6. NACA-RM-L54H13a. NASA. https://ntrs.nasa.gov/citations/19930088324
• Hoffman, Sherwood. 1956. Supersonic-Area-Rule Design and Rocket-Propelled Flight Investigation of a Zero-Lift Straight-Wing–Body–Nacelle Configuration between Mach Numbers 0.8 and 1.53. NACA-RM-L56B27. NASA. https://ntrs.nasa.gov/citations/19930089180
• Hoffman, Donald, Kenneth W. Bauer, and Stephen P. Chambal. 2005. “Using Neural Networks for Estimating Cruise Missile Reliability.” Military Operations Research 10 (3): 5–24. https://doi.org/10.5711/morj.10.3.5
• Hoffman, Sherwood, Austin L. Wolff, and Maxime A. Faget. 1955. Flight Investigation of the Supersonic Area Rule for a Straight Wing-Body Configuration at Mach Numbers between 0.8 and 1.5. NACA-RM-L55C09. NASA. https://ntrs.nasa.gov/citations/19930088641
• Hofmann, W. 1977. “Optimal State Estimation and Its Application to Inertial Navigation System Control.” In Optimal Estimation in Approximation Theory. Springer US. https://doi.org/10.1007/978-1-4684-2388-4_14
• Hofmann-Wellenhof, Bernhard, Klaus Legat, and Manfred Wieser. 2003. “Celestial Navigation.” In Navigation. Springer Vienna. https://doi.org/10.1007/978-3-7091-6078-7_7
• Hohenkerk, Catherine, John Kemp, and Brian Nibbs. 2012. “Astro Navigation Remembered.” Journal of Navigation 65 (3): 381–95. https://doi.org/10.1017/s0373463312000033
• Hojnacki, John T. 1972. Ramjet Engine Fuel Injection Studies. Defense Technical Information Center. https://doi.org/10.21236/ad0754852
• Hoke, C., V. Burnley, and G. Schwabacher. 2004. “Aerodynamic Analysis of Complex Missile Configurations Using AVUS (Air Vehicles Unstructured Solver).” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5452
• Hokmabadi, Mohammad P., Alexander Schumer, Demetrios N. Christodouides, and Mercedeh Khajavikhan. 2020. “Exceptional Point Based He-Ne Ring Laser Gyroscope.” In Conference on Lasers and Electro-Optics. Optica Publishing Group. https://doi.org/10.1364/cleo_qels.2020.ftu3a.5
• Holberg, D., and J. Grabowsky. 1981. “Pave Mover Flight Test Program.” In 1st Flight Test Conference. AIAA 1981-2492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2492
• Holbrook, J. C. 2005. “Celestial Navigators and Navigation Stories.” Culture and Cosmos 09 (02): 69–78. https://doi.org/10.46472/cc.0209.0211
• Holifield, Laura, and Matthew W. Tufts. 2024. “Uncertainty Quantification of Hypersonic Aerodynamic Heating.” In AIAA SCITECH 2024 Forum. AIAA 2024-0672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0672
• Holland, Allan L. n.d. “A Cruise Inertial Guidance System.” PhD diss., Drexel University. https://doi.org/10.17918/00003284
• Holland, R. L. 1971. A First Order Theory for Rotating Gravity Gradiometers. NASA-TM-X-64605. NASA. https://ntrs.nasa.gov/citations/19710024896
• Holley, W., and A. Bryson Jr. 1975. “Wind Modeling and Lateral Control for Automatic Landing.” In Guidance and Control Conference. AIAA 1975-1077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1077
• Holley, M. D., W. L. Swingle, S. L. Bachman, C. J. Leblanc, H. T. Howard, and H. M. Biggs. 1976. Apollo Experience Report Guidance and Control Systems: Primary Guidance, Navigation, and Control System Development. NASA-TN-D-8227. NASA. https://ntrs.nasa.gov/citations/19760016247
• Hollinger, J. A. 1965. Separation Tests of Rocket-Propelled Models of a Pilot-Escape Capsule. NASA-TN-D-2901. NASA. https://ntrs.nasa.gov/citations/19650019254
• Holm, R. J. 1968. “Relation of Azimuth and Position Errors in a Long-Range Aircraft Inertial System.” Navigation 15 (3): 274–79. https://doi.org/10.1002/j.2161-4296.1968.tb01619.x
• Holway, H. 1966. “A Wind Tunnel Free Flight Testing Technique for Nonplanar Motion of Spinning Models.” In 2nd Aerodynamic Testing Conference. AIAA 1966-774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-774
• Hong, J. 1965. “Resolution of Speed Stability for Supersonic Aircraft.” In Propulsion Joint Specialist Conference. AIAA 1965-622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-622
• Hong, Wooneson, Kyung-Jun Han, Chulsoo Lee, and BokSoo Paik. 2010. “Three Stage in-Flight Alignment with Covariance Shaping Adaptive Filter for the Strap-Down Inertial Navigation System(SDINS).” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7854. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7854
• Hong, SeokJin, and SangHoon Jung. 2016. “A Study of Reliability of Guided Missile(OO) Using Probit Analysis.” Journal of Korean Society for Quality Management 44 (3): 553–64. https://doi.org/10.7469/jksqm.2016.44.3.553
• Hong, Wooram, and Chongam Kim. 2011. “Numerical Study on Supersonic Inlet Buzz under Various Throttling Conditions and Fluid-Structure Interaction.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3967. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3967
• Hong, WoonSeon, and Chan Gook Park. 2017. “A Multistage in-Flight Alignment with No Initial Attitude References for Strapdown Inertial Navigation Systems.” International Journal of Aeronautical and Space Sciences 18 (3): 565–73. https://doi.org/10.5139/ijass.2017.18.3.565
• Hong, Wei, Bin Ren, Yihua Wang, et al. 2026. “Study on Thermal Hysteresis Effects in Temperature Compensation for Fiber Optic Gyroscope.” In Fifth International Computational Imaging Conference (CITA 2025), edited by Fei Liu, Ping Su. SPIE. https://doi.org/10.1117/12.3093520
• Honkanen, Tomi, Tuomas Tuisku, and Antti Pankkonen. 2011. “CFD Simulations and Wind Tunnel Experiments of a Generic Split-Canard Air-to-Air Missile at High Angles of Attack in Turbulent Subsonic Flow.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6335
• Hood, R., R. Krieger, and J. Gregoire. 1980. “The Impact of Constraints on Advanced Supersonic Cruise and Maneuvering Missile Concepts.” In 18th Aerospace Sciences Meeting. AIAA 1980-257. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-257
• Hopkins, J. 1981. “The Global Positioning System versus Gravity Disturbance Modeling in an Inertial Navigation System.” In 19th Aerospace Sciences Meeting. AIAA 1981-87. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-87
• Hornbeck, Charles E. 1975. Can-Type Combustor Design for a Low Cost Subsonic Ramjet Engine. Defense Technical Information Center. https://doi.org/10.21236/ada023471
• Hornbuckle, Joseph Iii B. 2015. Joint Precision Approach and Landing System Increment 1A (JPALS Inc 1A). Defense Technical Information Center. https://doi.org/10.21236/ad1019476
• Horne, Walter B., and Trafford J. W. Leland. 1962. Influence of Tire Tread Pattern and Runway Surface Condition on Braking Friction and Rolling Resistance of a Modern Aircraft Tire. NASA-TN-D-1376. NASA. https://ntrs.nasa.gov/citations/19620005764
• Horneman, Kenneth, and Craig Kluever. 2004. “Terminal Area Energy Management Trajectory Planning for an Unpowered Reusable Launch Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-5183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5183
• Horta, Lucas G., Robert H. Daugherty, and Veloria J. Martinson. 1999. “Actively Controlled Landing Gear for Aircraft Vibration Reduction.” In CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999. https://ntrs.nasa.gov/citations/19990052695
• Horton, Amanda, and D. Landrum. 2006. “Aerodynamic Evaluation of an Offset Planar Wing Missile Configuration.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3313
• Horvath, Thomas, Scott Splinter, Kamran Daryabeigi, William Wood, Richard Schwartz, and Martin Ross. 2008. “Assessment and Mission Planning Capability for Quantitative Aerothermodynamic Flight Measurements Using Remote Imaging.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080023462
• Hossein, Mohammad, and Hamidreza R. Amindavar. 2012. “Doppler Radar Tracking Using Moments.” In InTech eBooks. https://doi.org/10.5772/37307
• Hosseini, Seyedbarzin, Nikolai Botkin, Johannes Diepolder, and Florian Holzapfel. 2020. “Robust Optimal Input Design for Flight Vehicle System Identification.” In AIAA Scitech 2020 Forum. AIAA 2020-0290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0290
• Hosseini, Seyedbarzin, Christoph Göttlicher, and Florian Holzapfel. 2019. “Optimal Input Design for Flight Vehicle System Identification via Dynamic Programming and the Direct Method for Optimal Control.” In AIAA Scitech 2019 Forum. AIAA 2019-1319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1319
• Hosseini, Seyedbarzin, Rodolfo Hofmann, Florian Holzapfel, and Juergen Rauleder. 2025. “Optimal Input Design for Aircraft Parameter Estimation: Flight Test Results.” In AIAA SCITECH 2025 Forum. AIAA 2025-2173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2173
• Hosseini, Seyedbarzin, and Florian Holzapfel. 2022. “Optimal Input Design for Flight Vehicle System Identification in Frequency Domain.” In AIAA SCITECH 2022 Forum. AIAA 2022-2297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2297
• Hosters, N., M. Klaus, G. Schieffer, M. Behr, and H.-G. Reimerdes. 2013. “Towards Aerothermoelastic Simulations of Supersonic Flow through Nozzles.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/201304637
• Hostetler, L. 1978. “Optimal Terrain-Aided Navigation Systems.” In Guidance and Control Conference. AIAA 1978-1243. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1243
• Hostetler, Jeffrey K. 2005. “Missile Control System Design and Specification for a Long-Range Supersonic Cruise Missile.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2005-01-3379
• Hotate, K., and K. Tabe. 1986a. “Drift of an Optical Fiber Gyroscope Caused by the Faraday Effect: Experiment.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1986.84
• Hou, Bowen, Dayi Wang, Tianshu Dong, and Juhui Wei. 2025. “Observability-Based Optical Autonomous Navigation Using Starlight Angular Distance for Deep Space Exploration Cruise Phase.” Guidance, Navigation and Control 05 (04): 459–76. https://doi.org/10.1142/s273748072550030x
• Hou, Lanhua, Xiaosu Xu, Yiqing Yao, Di Wang, and Jinwu Tong. 2020. “Improved Exponential Weighted Moving Average Based Measurement Noise Estimation for Strapdown Inertial Navigation System/doppler Velocity Log Integrated System.” Journal of Navigation 74 (2): 467–87. https://doi.org/10.1017/s0373463320000570
• Houchard, J. H., C. M. Carlin, and E. Tjonneland. 1983. “Inlet, Engine, Airframe Controls Integration Development for Supercruising Aircraft.” In International Symposium on Air Breathing Engines. https://ntrs.nasa.gov/citations/19830054624
• Houston, M. H., G. Lloyd, D. A. Rankin, and D. Thompson. 1969. Gravity Gradient Preliminary Investigations on Exhibit ‘‘A’’ Final Report. NASA-CR-101867. NASA. https://ntrs.nasa.gov/citations/19690026569
• Howard, J. L. 1980. LORAN Navigation System. Defense Technical Information Center. https://doi.org/10.21236/ada085646
• Howard, W. J., and N. Kaufman. 1964. Numerical Analysis of System Availability and of Parameter Estimation Methods. Defense Technical Information Center. https://doi.org/10.21236/ad0444364
• Howard, Richard, and John Kersh Jr. 1991. “Effect of Canard Deflection on Enhanced Lift for a Close-Coupled-Canard Configuration.” In 9th Applied Aerodynamics Conference. AIAA 1991-3222. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3222
• Howard, D. D., and B. L. Lewis. 1955. Tracking Radar External Range Noise Measurements and Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0072960
• Howard, Richard, and John O’Leary. 1993. “A Flowfield Study of a Close-Coupled Canard Configuration.” In 11th Applied Aerodynamics Conference. AIAA 1993-3499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3499
• Howcroft, Chris, Bernd Krauskopf, Mark H. Lowenberg, and Simon A. Neild. 2013. “Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear.” SIAM Journal on Applied Dynamical Systems 12 (3): 1181–1209. https://doi.org/10.1137/120887643
• Howcroft, C., M. Lowenberg, S. Neild, B. Krauskopf, and E. Coetzee. 2015. “Shimmy of an Aircraft Main Landing Gear with Geometric Coupling and Mechanical Freeplay.” Journal of Computational and Nonlinear Dynamics 10 (5): 051011. https://doi.org/10.1115/1.4028852
• Howell, Alvin H. 1980. Balloon-Supported Antenna for Loran C/D Navigation System,. Defense Technical Information Center. https://doi.org/10.21236/ada087488
• Howell, Jan. 1988. “Reliability and Maintainability Evaluation during Flight Test.” In 4th Flight Test Conference. AIAA 1988-2185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2185
• Howell, R. G. 2003. “Terrestrial Line-of-Sight Links: Recommendations ITU-R P.530.” In Propagation of Radiowaves. Institution of Engineering and Technology. https://doi.org/10.1049/pbew502e_ch19
• Howell, William E., John R. McCehee, Robert H. Daugherty, and William A. Vogler. 1990. “F-106B Airplane Active Control Landing Gear Drop Test Performance.” In AGARD, Landing Gear Design Loads. https://ntrs.nasa.gov/citations/19910018850
• Howlett, R. A. 1976. “Variable Stream Control Engine Concept for Advanced Supersonic Aircraft: Features and Benefits.” In NASA. Langley Res. Center Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011068
• Howlett, R. A., J. Johnson, J. Sabatella, and T. Sewall. 1976. Advanced Supersonic Propulsion Study, Phase 3. NASA-CR-135148. NASA. https://ntrs.nasa.gov/citations/19770008098
• Howlett, R. A., and H. Kozlowski. 1975. “Variable Cycle Engines for Advanced Supersonic Transports.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19760039339
• Hoy, W. W. 1963. A Method for Establishing Landing Design Criteria for Carrier-Based Airplanes. Defense Technical Information Center. https://doi.org/10.21236/ad0409438
• Hoy, W. 1989. “Long Range Subsonic Cruise Missile Propulsion Performance Comparison.” In 25th Joint Propulsion Conference. AIAA 1989-2474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2474
• Hruby, R. J., G. Xenakis, R. A. Carestia, W. S. Bjorkman, S. F. Schmit, and L. D. Corliss. 1986. Laser Inertial Navigation System. ARC-11473. University of Southern Colorado. https://ntrs.nasa.gov/citations/19860000215
• Hsieh, T., and A. Wardlaw Jr. 1994. “Unsteady Aerodynamics of a Transient Pitching Missile Body from 0 Deg to 25 Deg.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3500. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3500
• Hsieh, Shih-Yang, Vigor Yang, Shih-Yang Hsieh, and Vigor Yang. 1997. “A Unified Analysis of Unsteady Flow Structures in a Supersonic Ramjet Engine.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-396. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-396
• Hsu, T. Y., and V. J. Tekippe. 1984. “A Passive Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 0478, edited by Emery L. Moore, O. G. Ramer. SPIE. https://doi.org/10.1117/12.942679
• Hu, Zhouxiang, Wang Lei, Bi Ran, and Xiaowu Shu. 2026. “Calibration-Excitation Design for Fiber-Optic Gyroscope Bias Compensation under Sparse Temperature Sensing.” Measurement Science and Technology 37 (37): 375102. https://doi.org/10.1088/1361-6501/ae9da9
• Hu, Jian Bo, Bing Qi Liu, and Kai Qiu. 2020a. “Fibre Optic Angle Rate Gyroscope Performance Evaluation in Terms of Allan Variance.” International Journal of Data Analysis Techniques and Strategies 12 (2): 114. https://doi.org/10.1504/ijdats.2020.106640
• Hu, Junyi, Shuang Liu, Yuxin Wang, and Huilian Ma. 2023a. “Compact Resonant Fiber-Optic Gyroscope with a Broadband Light Source.” In 28th International Conference on Optical Fiber Sensors. Optica Publishing Group. https://doi.org/10.1364/ofs.2023.th6.48
• Hu, Lichen, Feiyu Long, Borui Xie, and Xuanzhou Zhuang. 2023b. “Four Variants of Turbofan, Turbojet, Turboprop and Ramjet Engines and Their Future Prospects.” Applied and Computational Engineering 11 (1): 137–42. https://doi.org/10.54254/2755-2721/11/20230222
• Hu, Wen, Zhili Zhang, Zhaofa Zhou, He Chen, and ZiHao Xu. 2017. “Initial Attitude Impact on Error Propagation of Single-Axis Rotation Inertial Navigation System.” In Proceedings of the 2nd International Conference on Mechatronics Engineering and Information Technology (ICMEIT 2017). Atlantis Press. https://doi.org/10.2991/icmeit-17.2017.129
• Huang, K. H., Ho-Pen Chang, and Eugene M. Wells. 1990. Navigation Systems Requirement Analysis for the Aeroassist Flight Experiment (AFE). AIAA PAPER 90-0476. Teledyne Brown Engineering. https://ntrs.nasa.gov/citations/19900032810
• Huang, Daning, and Peretz P. Friedmann. 2016. “An Integrated Aerothermoelastic Analysis Framework for Predicting the Response of Composite Panels.” In 15th Dynamics Specialists Conference. AIAA 2016-1090. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1090
• Huang, Daning, and Peretz P. Friedmann. 2019. “A Surrogate-Based Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws with Application to Skin Panels.” In AIAA Scitech 2019 Forum. AIAA 2019-1120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1120
• Huang, Jun Yan, Pei-yu He, Yong Ming Gao, and Ren-ke Li. 2011. “A Novel Algorithm for Improving Range-Tracking Accuracy of Short-Range Millimeter Wave Radar.” JOURNAL OF ELECTRONICS INFORMATION TECHNOLOGY 32 (12): 2854–60. https://doi.org/10.3724/sp.j.1146.2009.01584
• Huang, Yue-Qing, and Xin Ma. 2021. “Autonomous Celestial Navigation Method for a Deep-Space Probe Based on Angle-Constraint Aided Celestial Angle Measurement.” SCIENTIA SINICA Physica, Mechanica & Astronomica 52 (1): 214512. https://doi.org/10.1360/sspma-2020-0434
• Huang, Daning, Tomer Rokita, and Peretz P. Friedmann. 2017a. “An Aerothermoelastic Analysis Framework Enhanced by Model Order Reduction with Applications.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-1601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1601
• Huang, Daning, Tomer Rokita, and Peretz P. Friedmann. 2018b. “Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation.” In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2018-1684. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1684
• Huang, Chao, Guoxing Yi, and Qingshuang Zen. 2018a. “Accuracy Evaluation Method of Stable Platform Inertial Navigation System Based on Quantum Neural Network.” NeuroQuantology 16 (6). https://doi.org/10.14704/nq.2018.16.6.1569
• Huang, Chao, Guoxing Yi, Qingshuang Zen, Lei Hu, and Zeyuan Xu. 2019b. “A Navigation Accuracy Evaluation Method for Multi-Path Platform Inertial Navigation System.” Instrumentation Mesure Métrologie 18 (2): 115–21. https://doi.org/10.18280/i2m.180204
• Huang, Mingyang, and Mingkang Zhang. 2026. “Adaptive Control for Outward-Folding Landing Legs of Reusable Rockets: Achieving Synchronized Touchdown under Tilted Conditions.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01213-8
• Huang, Wenyi, Senyu Zhang, Jamal N. A. Hassan, et al. 2023a. “High-Precision Angular Rate Detection Based on an Optomechanical Micro Hemispherical Shell Resonator Gyroscope.” Optics Express 31 (8): 12433. https://doi.org/10.1364/oe.482859
• Huang, Ming, Kaiyuan Zhang, Zhigang Li, and Jun Li. 2022. “Efficient Uncertainty Quantification on the Aerodynamic Performance of the Transonic Multi-Cavity Squealer Tip.” Preprint, . https://doi.org/10.2139/ssrn.4246509
• Huang, Z. C., Y. S. Zhang, and Yao Liu. 2018d. “Research on State Estimation of Hypersonic Glide Vehicle.” Journal of Physics: Conference Series 1060: 012088. https://doi.org/10.1088/1742-6596/1060/1/012088
• Huang, Tianqi, Yibiao Zhou, and Bihui Zhang. 2024a. “Image Matching-Based Visual-Inertial Integrated Navigation for UAV in GNSS-Denied Environments.” Journal of Physics: Conference Series 2784 (1): 012014. https://doi.org/10.1088/1742-6596/2784/1/012014
• Hubble, J. D., and R. E. Smith. 1979. Evaluation of an Airjet Distortion Generator Used to Produce Steady- State, Total-Pressure Distortion at the Inlet of a General Electric F101-GE-100 Turbofan Engine. Defense Technical Information Center. https://doi.org/10.21236/ada072743
• Hube, Frederick K. 1968. Tests of One-Third-Scale NASA Hypersonic Research Engine Inlet at Mach Numbers 6 and 8. Defense Technical Information Center. https://doi.org/10.21236/ad0388036
• Huddle, James R. 1983. “Inertial Navigation System Error-Model Considerations in Kalman Filtering Applications.” In Control and Dynamic Systems. Elsevier. https://doi.org/10.1016/b978-0-12-012720-7.50012-7
• Hue, David, and Pascal Molton. 2020. “Turbulent Drag Induced by Low Surface Roughness at Transonic Speeds: Experimental/numerical Comparisons.” Physics of Fluids 32 (4): 045108. https://doi.org/10.1063/1.5143068
• Huebner, Lawrence D., and Kenneth E. Tatum. 1991. Computational and Experimental Aftbody Flow Fields for Hypersonic, Airbreathing Configurations with Scramjet Exhaust Flow Simulation. AIAA PAPER 91-1709. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910057938
• Huerta, Joseph. 1969. An Experimental Investigation at Supersonic Mach Numbers of Base Drag of Various Boattail Shapes with Simulated Base Rocket Exhaust. Defense Technical Information Center. https://doi.org/10.21236/ad0855156
• Hueschen, R. M. 1984. “Flight Test Results for the Digital Integrated Automatic Landing Systems (DIALS): A Modern Control Full-State Feedback Design.” In NASA Aircraft Controls Research, 1983. https://ntrs.nasa.gov/citations/19840012521
• Hueschen, R. M. 1986. Implementation and Flight Tests for the Digital Integrated Automatic Landing System (DIALS). Part 2: Complete Set of Flight Data. NASA-TM-87632-PT-2. NASA. https://ntrs.nasa.gov/citations/19860018621
• Huff, J., and E. Herbert. 1979. “Digital Guidance and Control for a Low Cost Medium Range Surface-to-Surface Missile System.” In Guidance and Control Conference. AIAA 1979-1753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1753
• Huffman, J. K. 1975. Effect of Vertical-Tail Location on the Aerodynamic Characteristics at Subsonic Speeds of a Close-Coupled Canard Configuration. NASA-TN-D-7947. NASA. https://ntrs.nasa.gov/citations/19750019955
• Huffman, J. K., and C. H. Fox Jr. 1977. Subsonic Longitudinal Aerodynamic Characteristics of a Vectored-Engine-over-Wing Configuration Having Spanwise Leading-Edge Vortex Enhancement. NASA-TM-X-73955. NASA. https://ntrs.nasa.gov/citations/19770020128
• Huffman, J. K., and C. H. Fox Jr. 1978. Subsonic Longitudinal and Lateral-Directional Static Aerodynamic Characteristics for a Close-Coupled Wing-Canard Model in Both Swept Back and Swept Forward Configurations. NASA-TM-74092. NASA. https://ntrs.nasa.gov/citations/19780013106
• Huffman, J. K., and C. H. Fox Jr. 1979. The Effect of Canard Relative Size and Vertical Location on the Subsonic Longitudinal and Lateral-Directional Static Aerodynamic Characteristics for a Model with a Swept Forward Wing. NASA-TM-78739. NASA. https://ntrs.nasa.gov/citations/19790019967
• Huffman, J. K., and C. H. Fox Jr. 1985. Subsonic Pressure Distributions near a Wing-Fin Juncture on a Supersonic Arrow-Wing Configuration with Wing-Mounted Vertical Fins. AIAA PAPER 85-0276. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19850037477
• Hughson, Montgomery, Eric Blades, and Gregg Abate. 2006. “Transonic Aerodynamic Analysis of Lattice Grid Tail Fin Missiles.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3651
• Hui, Yi, Siu-seong Law, Min Liu, and Shouying Li. 2019. “Parameter and Aerodynamic Force Identification of Single-Degree-of-Freedom System in Wind Tunnel Test.” Journal of Engineering Mechanics 145 (1): 04018120. https://doi.org/10.1061/(asce)em.1943-7889.0001542
• Hull, David, and Dinesh Muzumdar. 1993. “Optimal Guidance for a Short Range Attack Missile.” In Guidance, Navigation and Control Conference. AIAA 1993-3784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3784
• Hull, Donald L., and Kenneth L. Roger. 1975. B-52E CCV Flight Test Data Applicable to Parameter Estimation. Defense Technical Information Center. https://doi.org/10.21236/adb011143
• Hull, D., J. Speyer, and P. Kite. 1983. “New Target Models for Homing Missile Guidance.” In Guidance and Control Conference. AIAA 1983-2166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2166
• Hulshoff, S., J. Mulder, and H. Hoejmakers. 1996. “Estimation of Aircraft Dynamic Parameters Using Euler Computations and Comparison with Flight-Test Data.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3416
• Humble, Ronald D. 2024. “Ballistic Missile Defence.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781032675480-5
• Hummel, R., D. Panda, and R. Aggarwal. 1980. “Application of Relaxation Labeling to Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959152
• Humphrey, Ian. 1999. Inertial System Requirements for Deflection of the Vertical Compensations. Defense Technical Information Center. https://doi.org/10.21236/ada403448
• Humphrey, Ian, and Ian Humphrey. 1997. “Inertial Navigation System for a Micro Unmanned Air Vehicle.” In Guidance, Navigation, and Control Conference. AIAA 1997-3567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3567
• Hung, H., C. Laskoskie, T. El-Wailly, and C. L. Chang. 1988. “Ti-LiNbO3 Waveguide Serrodyne Modulator with Ultrahigh Sideband-Suppression for Fiber Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1988.thdd3
• Hung, J. C., and H. V. White. 1974. IMU Self-Alignment Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada002696
• Hunt, Dillon. n.d. “Supersonic Combustion in Inlet-Fuelled Busemann-like Axisymmetric Scramjet Flow Paths.” PhD diss., The University of Queensland. https://doi.org/10.14264/uql.2014.194
• Hunt, G. L. 1960. Investigation of the Static Longitudinal Stability Characteristics of an Air-To-Surface Canard Missile Configuration in the Transonic Mach Number Range. NASA-TM-X-305. NASA. https://ntrs.nasa.gov/citations/19630004026
• Hunt, R. L. 1974. Aerodynamic Heating and Loading within Large Open Cavities in Cone and Cone-Cylinder-Flare Models at Mach 6.7. NASA-TN-D-7403. NASA. https://ntrs.nasa.gov/citations/19740010445
• Hunt, L. R. 1977. Aerodynamic Heating in Large Cavities in an Array of RSI Tiles. NASA-TN-D-8400. NASA. https://ntrs.nasa.gov/citations/19770017483
• Hunt, J. L., P. J. Johnston, J. M. Cubbage, et al. 1982. “Hypersonic Airbreathing Missile Concepts under Study at NASA Langley Research Center.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820043566
• Hunt, J. L., and R. A. Jones. 1966. Comment on ‘‘Measurement of Aerodynamic Heating of Wind-Tunnel Models by Means of Temperature- Sensitive Paint.’‘. NASA. https://ntrs.nasa.gov/citations/19660051626
• Hunt, J. L., and R. A. Jones. 1968. Effects of Several Ramp-Fairing, Umbilical, and Pad Configurations on Aerodynamic Heating to Apollo Command Module at Mach 8. NASA-TM-X-1640. NASA. https://ntrs.nasa.gov/citations/19680025669
• Hunt, J. L., P. L. Lawing, D. C. Marcum, and J. M. Cubbage. 1978. “Conceptual Study of Hypersonic Airbreathing Missiles.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780036719
• Hunter, L., and J. Cawthon. 1984. “Improved Supersonic Performance Design for the F-16 Inlet Modified for the J-79 Engine.” In 20th Joint Propulsion Conference. AIAA 1984-1272. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1272
• Hunter, L., J. Tripp, and D. Howlett. 1985. “A Mach 2.0 Plus Supersonic Inlet Study Using the Navier-Stokes Equations.” In 21st Joint Propulsion Conference. AIAA 1985-1211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1211
• Huntington, D., and C. Lyrintzis. 1996. “Random Vibration in Aircraft Landing Gear.” In 37th Structure, Structural Dynamics and Materials Conference. AIAA 1996-1360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1360
• Huo, Ying, Majdedin Mirmirani, Petros Ioannou, and Mathew Kuipers. 2006. “Altitude and Velocity Tracking Control for an Airbreathing Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6695. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6695
• Hurley, W. V. 1951a. “Closure to “Discussion of ‘Turbojet-Engine Design for High-Speed Flight’” (1951, Trans. ASME, 73, p. 920).” Journal of Fluids Engineering 73 (7): 920–920. https://doi.org/10.1115/1.4016502
• Hurley, W. V. 1951b. “Turbojet-Engine Design for High-Speed Flight.” Journal of Fluids Engineering 73 (7): 915–20. https://doi.org/10.1115/1.4016500
• Hurrell, H. G. 1957. Simplified Theory for Dynamic Relation of Ramjet Pressures and Fuel Flow. NACA-RM-E57I13. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19630002651
• Hursh, John W. 1985. “Aerial Profiling of Terrain System (APTS), a Laser-Inertial Airborne Surveyor.” Navigation 32 (3): 282–99. https://doi.org/10.1002/j.2161-4296.1985.tb00910.x
• Hurwitz, Wayne, Kyle Whitcomb, Wayne Hurwitz, and Kyle Whitcomb. 1997. “Flight Test Validation of B-2 Inlet/engine Compatibility: A Risk Management Approach.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3157
• Hussein, Mennatallah M., Sara Hauptman, and Ahmed Ghoniem. 2026. “Performance Evaluation of a Conceptual Turbo-Ramjet Engine for a Two Stage to Orbit Launch System.” In AIAA SCITECH 2026 Forum. AIAA 2026-2741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2741
• Hutchin, Richard. 2008. “Operating Principles of a New Interferometric Star Tracker and Test Results.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6651
• Hutchins, Kelley, Maruthi Akella, Noel Clemens, and Jeffrey Donbar. 2012. “Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart.” In 6th AIAA Flow Control Conference. AIAA 2012-2808. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2808
• Hutchins, Robert G., and Philip E. Pace. 2006. “Studies in Trajectory Tracking and Launch Point Determination for Ballistic Missile Defense.” In SPIE Proceedings, vol. 6236, edited by Oliver E. Drummond. SPIE. https://doi.org/10.1117/12.666254
• Hutchinson, I., and P. Inglima. 1970. “An Improved Ring Laser Rate Sensor for Use in Strapdown Inertial Systems.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1025
• Hutchison, W. L. 1975. Star Tracker Axis-to-Sunlit Earth Horizon Angle Constraint Evaluations for Rendezvous Operations. NASA-CR-151023. NASA. https://ntrs.nasa.gov/citations/19760026191
• Hwang, Jin-Ah;Nam, Gi-Gun;Lee, Jang-Myung;. 2007. “Automatic Landing System Using a Trajectory of Laser Beam.” Journal of Control Automation and Systems Engineering 13 (1): 39–45. https://doi.org/10.5302/j.icros.2007.13.1.039
• Hyde, Rick, and John Cleminson. 2004. “Autopilot Design for a Square Cross-Section Missile.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5329
• Hyde, Eric, William Escher, and Jordan Roddy. 2000. “Marquardt’s Mach 4.5 Supercharged Ejector Ramjet High-Performance Aircraft Engine Project.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3109
• “Hypersonic Ramjet Engine with Balanced Variable Mechanisms.” 2004. In 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-04-s.5.05
• Hyzhnyak, E., and Mykola Chernyak. 2024. “Improving the Accuracy of a Platformless Inertial Navigation System for an Aircraft during Rapid Roll Rotation.” Mechanics of Gyroscopic Systems, no. 48: 98–107. https://doi.org/10.20535/0203-3771482024317967
• Iannelli, Joe. 2007a. “Supersonic-Inlet Start Amelioration and Unstart Mitigation via Mass and Heat Transfer.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-522
• Iannelli, Joe. 2007b. “Unstart Mitigation in Inlet and Isolator via Wall Mass Transfer: A Computational Study.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5071
• Identifiability of Initial Conditions and Bias Parameters. 2015. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624102790.0579.0582
• Ighodaro, Osarobo, E. I. Aburime, and Andrew Amagbor Erameh. 2022. “Off-Design Modelling of a Turbo Jet Engine with Operative Afterburner.” Open Journal of Energy Efficiency 11 (03): 88–107. https://doi.org/10.4236/ojee.2022.113007
• Iglesias, Pablo, and Thomas Urban. 1999. “Loop Shaping Design of a Missile Autopilot: Controller Configurations and Weighting Filter Selection.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-3973. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3973
• Ignagni, M. B. 1972. “An All-Earth Inertial Navigation Scheme.” Navigation 19 (3): 209–14. https://doi.org/10.1002/j.2161-4296.1972.tb01686.x
• Ikawa, Hideo. 1989. “Rapid Methodology for Design and Performance Prediction of Integrated Scramjet/hypersonic Vehicle.” In 25th Joint Propulsion Conference. AIAA 1989-2682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2682
• Iliff, K., and R. Maine. 1982. “NASA Dryden’s Experience in Parameter Estimation and Its Uses in Flight Test.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1373
• Im, Seong-kyun, and Hyungrok Do. 2018. “Unstart Phenomena Induced by Flow Choking in Scramjet Inlet-Isolators.” Progress in Aerospace Sciences 97: 1–21. https://doi.org/10.1016/j.paerosci.2017.12.001
• Imazu, Hayama, and Fumihiko Kawamoto. 1975. “Rectangular Navigation System and It’s Accuracy.” Journal of Japan Institute of Navigation 53 (0): 1–12. https://doi.org/10.9749/jin.53.1
• Imig, La. 1973. “Fatigue of Supersonic Transport Materials Using Simulated Flight-by-Flight Loading.” In Fatigue at Elevated Temperatures. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp38845s
• Inagaki, Luis, and Fábio de Oliveira Fialho. 2019. “Stellar Variability Modeling for Autonomous Star Tracker Simulator.” In Proceedings of the 25th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2019.cob2019-0759
• Indeitsev, D. A., P. P. Udalov, I. A. Popov, and A. V. Lukin. 2022. “Nonlinear Dynamics of the Hemispherical Resonator of a Rate-Integrating Gyroscope under Parametric Excitation of the Free Precession Mode.” Journal of Machinery Manufacture and Reliability 51 (5): 386–96. https://doi.org/10.3103/s1052618822040082
• “Inertial Guidance.” 1964. Aircraft Engineering and Aerospace Technology 36 (1): 1–1. https://doi.org/10.1108/eb033818
• “Inertial Guidance.” 1993. In Dynamics of Atmospheric Re-Entry. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861741.0477.0534
• “Inertial Instrumentation.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0059.0077
• Inertial Navigation and Kalman Filtering. 2018. Wiley. https://doi.org/10.1002/9781119262367.ch9
• Inertial Navigation Error Analysis. 2020. Wiley. https://doi.org/10.1002/9781119547860.ch11
• “Inertial Navigation Sensors and Systems.” 1999. In Integrated Navigation and Guidance Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861994.0039.0071
• “Inertial Navigation System Alignment.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch10
• “The Inertial Navigation System Equations.” 2007. In Introduction to Modern Navigation Systems. WORLD SCIENTIFIC. https://doi.org/10.1142/9789812708755_0006
• “Inertial Navigation System Ground Alignment.” 2007. In Applied Mathematics in Integrated Navigation Systems, Third Edition. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861598.0215.0228
• Inertial Navigation Systems. 2006. Wiley. https://doi.org/10.1002/9780470099728.ch9
• “Inertial Navigation with External Measurements.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0181.0209
• Inertial Sensors and Inertial Measurement Units. 2021. Wiley. https://doi.org/10.1002/9781119699910.ch2
• Inertial Sensors and Inertial Navigation Systems. 2025. Wiley. https://doi.org/10.1002/9781394155293.ch4
• “Influence of Back Pressure on the Flow in the Diffuser of a Supersonic Air Inlet.” 2017. Perm National Research Polytechnic University Aerospace Engineering Bulletin, no. 49. https://doi.org/10.15593/2224-9982/2017.49.02
• Ingenito, Antonella. 2021. “Design of Supersonic/Hypersonic Vehicles.” In SpringerBriefs in Applied Sciences and Technology. Springer International Publishing. https://doi.org/10.1007/978-3-030-66881-5_3
• Ingram, W., L. Yip, and E. Cook. 1986. “Wind-Tunnel Investigation of the OMAC Canard Configuration.” In General Aviation Technology Conference. AIAA 1986-2608. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2608
• “Initial Alignment of Large Azimuth Misalignment Angle in SINS Based on MEP-CKF.” 2018. In Information, Computer and Application Engineering. CRC Press. https://doi.org/10.1201/b18658-31
• INS, Initialization, and Alignment. 2001. “8 INS Initialization and Alignment.” In Inertial Navigation Systems with Geodetic Applications. DE GRUYTER. https://doi.org/10.1515/9783110800234.238
• INS, Initialization, and Alignment. 2023. “8 INS Initialization and Alignment.” In Inertial Navigation Systems with Geodetic Applications. De Gruyter. https://doi.org/10.1515/9783110784329-008
• “Instrumentation for in-Flight Determination of Steady-State and Dynamic Inlet Performance in Supersonic Aircraft.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0041.0058
• “Integrated Guidance and Control for Missiles.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-13
• “Integrated MEMS Inertial/GPS Navigation System.” 2002. Aircraft Engineering and Aerospace Technology 74 (6). https://doi.org/10.1108/aeat.2002.12774fad.009
• “Integrated Navigation Systems.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch13
• “Introduction and Overview of Inertial Navigation Systems.” 2022. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch1
• Iozan, L. I., M. Kirkko-Jaakkola, J. Collin, J. Takala, and C. Rusu. 2012. “Using a MEMS Gyroscope to Measure the Earth’s Rotation for Gyrocompassing Applications.” Measurement Science and Technology 23 (2): 025005. https://doi.org/10.1088/0957-0233/23/2/025005
• İpek, Begüm. 2025. “Quantum Computing for Aerothermal and Structural Optimization of Next-Generation Mobility Systems.” Next Generation Journal for The Young Researchers 9 (1): 99–102. https://doi.org/10.62802/qrgkjb97
• Irwin, D. C. 1966. Landing Dynamics Study for Lunar Landing Research Vehicle. NASA-CR-428. NASA. https://ntrs.nasa.gov/citations/19660014158
• Ishijima, Yoshiyuki, Shuichi Matsumoto, and Kentaro Hayashi. 1998. “Re-Entry and Terminal Guidance for Vertical-Landing TSTO (Two-Stage to Orbit).” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4120
• Ishimaru, Akira. 1978a. “Line-of-Sight Propagation of a Plane Wave through a Random Medium—Weak Fluctuation Case.” In Wave Propagation and Scattering in Random Media. Elsevier. https://doi.org/10.1016/b978-0-12-374702-0.50010-8
• Ishimaru, Akira. 1978b. “Line-of-Sight Propagation of Spherical and Beam Waves through a Random Medium—Weak Fluctuation Case.” In Wave Propagation and Scattering in Random Media. Elsevier. https://doi.org/10.1016/b978-0-12-374702-0.50011-x
• Ishimaru, Akira. 1978c. “Line-of-Sight Propagation through Tenuous Distribution of Particles.” In Wave Propagation and Scattering in Random Media. Elsevier. https://doi.org/10.1016/b978-0-12-374701-3.50012-0
• Ivanov, Yu. A. 2015. “Complexed Navigation System Based on a Strapdown Inertial Navigation System and Correlation Meter Speed and Drift.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 2: 74–81. https://doi.org/10.38013/2542-0542-2015-2-74-81
• Ivanov, Vadim Aleksandrovich. 2022. “Efficiency of the Introduction the Intermediate Heating in Cycle of Afterburning Turbofan for Supersonic the Aircraft.” Vestnik UGATU 26 (1): 59–68. https://doi.org/10.54708/19926502_2022_2619559
• Ivanov, Danil, Yaroslav Vladimirovich Mashtakov, and Uliana Vladimirovna Monakhova. 2024. Study of Attitude Determination Accuracy and Earth-Point Stabilization Performance Using Asynchronous Star Tracker and Angular Velocity Sensor Measurements. https://doi.org/10.52202/078368-0006
• Ivanov, O. A., and Y. A. Opanasiuk. 2018. “Inertial Navigation Accuracy and Accelerometers with Damping.” Electronics and Control Systems 3 (57). https://doi.org/10.18372/1990-5548.57.13229
• Iwakawa, Akira, Daiki Furukawa, Yuma Aoki, and Akihiro Sasoh. 2015. “Free Flight Measurement of Aircraft Model Using Aero Ballistic Range.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2584. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2584
• Iwatsuki, K. 1991. “Long-Term Bias Stability of All-PANDA Fibre Gyroscope with Er-Doped Superfluorescent Fibre Laser.” Electronics Letters 27 (12): 1092–93. https://doi.org/10.1049/el:19910678
• Iyer, N. R. 1995. “Recent Advances in Antitank Guided Missile Systems.” Defence Science Journal 45 (3): 187–97. https://doi.org/10.14429/dsj.45.4118
• Jackson, H. Herbert. 1955. Longitudinal Aerodynamic Characteristics and Effect of Rocket Jet on Drag of Models of the Hermes a-3A and a-3B Missiles in Free Flight at Mach Numbers from 0.6 to 2.0. NACA-RM-SL55F15. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20010057623
• Jackson, S. B. 1965. “Advantages of a Brake Parachute Compared with Thrust Reversal for Landing Civil Aircraft.” Journal of the Royal Aeronautical Society 69 (650): 80–84. https://doi.org/10.1017/s0001924000060334
• Jackson, A. 1973. “Continuous Calibration and Alignment Techniques for an All-Attitude Inertial Platform.” In Guidance and Control Conference. AIAA 1973-865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-865
• Jackson, Paul. 1992. “A Gradient Projection Algorithm for Missile Autopilot Stability Analysis.” In Astrodynamics Conference. AIAA 1992-4534. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4534
• Jackson, L. R., J. A. Martin, and W. J. Small. 1977. A Fully Reusable, Horizontal Takeoff Space Transport Concept with Two Small Turbojet Boosters. NASA-TM-74087. NASA. https://ntrs.nasa.gov/citations/19780003229
• Jackson, R. J., and T. T. Wang. 1974. Hypersonic Ramjet Experiment Project. Phase 1: Computer Program Description, Ramjet and Scramjet Cycle Performance. NASA-CR-132454. NASA. https://ntrs.nasa.gov/citations/19740021101
• Jacob, S., R. Chathhyan, M. R. Rajkumar, P. Balavino, and P. Arikrishnan. 2014. “Steam Fuel System in Ramjet Engine.” Advanced materials research 984-985: 967–69. https://doi.org/10.4028/www.scientific.net/amr.984-985.967
• Jacocks, J. L., and K. R. Kneile. 1975. Statistical Prediction of Maximum Time-Variant Inlet Distortion Levels. Defense Technical Information Center. https://doi.org/10.21236/ada004104
• Jacot, A., and D. Hellmers. 1982. “Control Dynamics of the Deployable Wing Cruise Ballistic Missile.” In 20th Aerospace Sciences Meeting. AIAA 1982-181. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-181
• Jaeger, Sam, and Maziar Hemati. 2025. “Hypersonic Glide Vehicle Trajectory Design Using Constrained Energy Maneuverability.” In 2025 Regional Student Conferences. AIAA 2025-97945. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-97945
• Jafari, Mahdi, and Jafar Roshanian. 2012. “Optimal Redundant Sensor Configuration for Accuracy and Reliability Increasing in Space Inertial Navigation Systems.” Journal of Navigation 66 (2): 199–208. https://doi.org/10.1017/s0373463312000434
• Jafarov, Elbrous M., and Ramazan Tasaltin. 2001. “Design of Robust Autopilot-Output Integral Sliding Mode Controllers for Guided Missile Systems with Parameter Perturbations.” Aircraft Engineering and Aerospace Technology 73 (1): 16–26. https://doi.org/10.1108/00022660110366854
• Jagannathan, Rangesh, and Craig T. Johansen. 2019. “Numerical Assessment of Intake Buzz with Nano-Particles across a Supersonic External Compression Intake.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4425. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4425
• Jaggers, R. 1977. “An Explicit Solution to the Exoatmospheric Powered Flight Guidance and Trajectory Optimization Problem for Rocket Propelled Vehicles.” In Guidance and Control Conference. AIAA 1977-1051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1051
• Jah, Moriba, Michael Lisano, and George Hockney. 2007. Inertial Measurements for Aero-Assisted Navigation (IMAN). NPO-43677. California Inst. of Tech. https://ntrs.nasa.gov/citations/20100010952
• Jahanshahi, M. H., and J. Y. Lai. 1983. Galileo Spacecraft Inertial Sensors in-Flight Calibration Design. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/19840035838
• Jahnen, Werner, Thomas Peters, and Leonhard Fottner. 1999. “Stall Inception in a 5-Stage HP-Compressor with Increased Load Due to Inlet Distortion.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/99-gt-440
• Jain, Anshul A. 2025. “Component Sizing and Design-Point Performance Evaluation of a Two-Spool Turbofan Engine with Mixed Exhaust and Afterburner.” International Journal of Science and Research (IJSR): 1945–48. https://doi.org/10.21275/sr251223120745
• Jameian, Hassan, and Behrouz Safarinejadian. 2021. “Overcoming the Settling Time Challenge of Initial Alignment of Strapdown Inertial Navigation System by a Novel Solution.” IET Radar, Sonar & Navigation 15 (4): 419–30. https://doi.org/10.1049/rsn2.12045
• James, Stuart. 1998. “Supersonic Flight: Revised Edition.” Reference Reviews 12 (1): 25–26. https://doi.org/10.1108/rr.1998.12.1.25.27
• Jameson, Antony, Sriram Shankaran, Luigi Martinelli, Susan Cliff, and Scott Thomas. 2005. “Aerodynamic Shape Optimization of Supersonic Aircraft Configurations.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-1013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1013
• Janes, H. B. 1959. An Analysis of Propagation Measurements Made at 418 Mc, Well beyond the Radio Horizon. National Bureau of Standards. https://doi.org/10.6028/nbs.tn.6
• Jang, Sukwon, and Hyochoong Bang. 2017. “Acquisition Method for Terrain Referenced Navigation Using Terrain Contour Intersections.” IET Radar, Sonar & Navigation 11 (9): 1444–50. https://doi.org/10.1049/iet-rsn.2017.0023
• Jang, Dongin, and Sungsu Park. 2026. “Maneuvering Trajectory Generation Technique for Prediction of Terminal Trajectory of Maneuverable Ballistic Missile.” Journal of the Korean Society for Aeronautical & Space Sciences 54 (1): 33–41. https://doi.org/10.5139/jksas.2026.54.1.33
• Janicijevic, Slobodan. 2004. “Determining Optimum Inertial Measurement Unit Architecture from the View-Point of Sensor Fault Detection.” Vojnotehnicki glasnik 52 (2): 147–61. https://doi.org/10.5937/vojtehg0402147j
• Jankiewicz, Jakub Antoni. 2026. “The Impact of Staggered Fins on Aerodynamic Drag of a Transonic Sounding Rocket.” In Materials Research Proceedings, vol. 69. Materials Research Forum LLC. https://doi.org/10.21741/9781644904251-46
• Jankowski, P. C. 1970. Hybrid Altimeter Using a Strapdown Inertial Navigation System. NASA-CR-109086. NASA. https://ntrs.nasa.gov/citations/19700011619
• Janus, J., David Whitfield, and Francis Mansfield. 1990. “Computation of the Unsteady Flowfield about a Counterrotating Prop-Fan Cruise Missile.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3093
• Jarmark, B. 1986. “Optimal Missile Range with Respect to Thrust and Altitude Profiles.” In Astrodynamics Conference. AIAA 1986-2081. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2081
• Jaroszewicz, J. L., and M. Szustakowski. 1995. “The Application of a Fiber Optic Gyroscope for Studies of Extinction Ratio of Fiber Optic Polarizer.” In Trends in Optical Fibre Metrology and Standards. Springer Netherlands. https://doi.org/10.1007/978-94-011-0035-9_53
• Jasani, Bhupendra. 2020. “Ballistic Missile Defence.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781003053798-7
• Jauberthie, Carine, Louise Travé-MassuyèEs, and Nathalie Verdière. 2016. “Set-Membership Identifiability of Nonlinear Models and Related Parameter Estimation Properties.” International Journal of Applied Mathematics and Computer Science 26 (4): 803–13. https://doi.org/10.1515/amcs-2016-0057
• Jayaraman, Pattam, Joerg Fischer, Alan Moorhouse, and Mathias Lauer. 2006. “Star Tracker Operational Usage in Different Phases of the Mars Express Mission.” In SpaceOps 2006 Conference. AIAA 2006-5930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-5930
• Jee, Craig, and Jason Etele. 2018. “Multi-Objective Optimization of a Supersonic Rocket Based Combined Cycle Inlet through Differential Evolution.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-0409. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0409
• Jeffrie, H., and D. Rolston. 1972. “Survivable Flight Control System Compatibility Test Program.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-761. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-761
• Jegarkandi Mohsen, Fathi, Salezadeh Nobari Ali, Sabzehparvar Mahdi, Haddadpour Hassan, and Tavakkoli Farhad. 2009. “Aeroelasticity Consideration of Supersonic Vehicle Using Closed Form Analytical Aerodynamic Model.” Aircraft Engineering and Aerospace Technology 81 (2): 128–36. https://doi.org/10.1108/00022660910941820
• Jekeli, Christopher. 1997. “Gravity on Precise, Short-Term, 3-D Free-Inertial Navigation.” Navigation 44 (3): 347–57. https://doi.org/10.1002/j.2161-4296.1997.tb02353.x
• Jekeli, Christopher. 2005. “Navigation Error Analysis of Atom Interferometer Inertial Sensor.” Navigation 52 (1): 1–14. https://doi.org/10.1002/j.2161-4296.2005.tb01726.x
• Jekeli, Christopher. 2021. The Deflection of the Vertical, from Bouguer to Vening-Meinesz, and beyond – the Unsung Hero of Geodesy and Geophysics. https://doi.org/10.5194/egusphere-egu21-596
• Jekeli, C., and R. H. Rapp. 1980. Accuracy of the Determination of Mean Anomalies and Mean Geoid Undulations from a Satellite Gravity Field Mapping Mission. REPT-307. Ohio State Univ. https://ntrs.nasa.gov/citations/19810004158
• Jenkins, M., and R. Meyer. 1975. “A Large-Scale Low-Speed Tunnel Test of a Canard Configuration with Spanwise Blowing.” In Aircraft Systems and Technology Meeting. AIAA 1975-994. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-994
• Jenn, A., and H. Nelson. 1988. “Effect of Wing Vertical Position on Lift for Supersonic Delta Wing Missile Configurations.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4381
• Jensen, Gunnar Bent, John Lief Jøergensen, Carl Christian Liebe, and Allen Read Eisenman. 1997. Realization of a Faster, Cheaper, Better Star Tracker for the New Millennium. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210003847
• Jeon, Koang-Kyu, Ki-Wook Jung, and Chang-Hun Lee. 2026. “A Two-Gain Acceleration-Feedback Three-Loop Autopilot for Mitigating Guidance-Control Loop Divergence.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01250-3
• Jeon, Hyun Cheol, Jong Nam Lim, and Chan Gook Park. 2018b. “Modified Sequential Processing Terrain Referenced Navigation Considering Slant Range Measurement.” IET Radar, Sonar & Navigation 12 (11): 1208–16. https://doi.org/10.1049/iet-rsn.2018.5170
• Jeon, Hyun Cheol, Woo Jeong Park, and Chan Gook Park. 2017. “Accurate and Efficient Terrain Referenced Navigation Using Multiple Measurements by Flash LiDAR.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2017.15130
• Jerome, Richard. n.d. “Performance Analysis of Space-Based Radar Tracking Techniques.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1990-01816
• Jeronymo, Daniel, and Felipe Stark. 2017. “Particle Swarm Optimization of Turbojet Engine Thrust.” In Procceedings of the 24th ABCM International Congress of Mechanicl Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2017.cob17-2836
• Jessell, A. H. 1949. “The Use of Astro-Navigation in Fast Aircraft.” Journal of Navigation 2 (4): 282–85. https://doi.org/10.1017/s0373463300034007
• Jetawatthana, Sarocha, and Thanakorn Khamvilai. 2026. “Extended Kalman Filtering with Censoring Statistics for Inertial-Only Navigation under GPS Denial.” In AIAA SCITECH 2026 Forum. AIAA 2026-1176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1176
• Jettmar, R. 1984. “Calculations of Viscous Supersonic Flow over Finned Bodies Using a ‘Thin-Fin’ Approximation.” In 11th Atmospheric Flight Mechanics Conference. AIAA 1984-2114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2114
• Ji, Xiu Ling, Haipeng Wang, Shi Ming Zeng, and Chen Yang Jia. 2011. “Lateral-Directional Aerodynamics of a Canard Guided Spin Stabilized Projectile at Supersonic Velocity.” Applied Mechanics and Materials 110-116: 4343–50. https://doi.org/10.4028/www.scientific.net/amm.110-116.4343
• Ji, Xiu Ling, Haipeng Wang, Shi Ming Zeng, and Chen Yang Jia. 2012. “Longitudinal Aerodynamics of a Canard Guided Spin Stabilized Projectile.” Advanced materials research 443-444: 719–23. https://doi.org/10.4028/www.scientific.net/amr.443-444.719
• Ji, Chunxiu, and Dan Xie. 2022. “Reduced Order Model Based on SPOD for Aerothermoelastic Analysis of a Hypersonic Panel.” International Conference on Computational & Experimental Engineering and Sciences 24 (1): 1–2. https://doi.org/10.32604/icces.2022.08737
• Jia-fan, Zhang, Yan Qing-hua, and Zhai Tong. 2011. “Numerical Approach to Identifiability Test of Parametric Models in Nonlinear Mechanical Systems.” Journal of Dynamic Systems, Measurement, and Control 133 (5): 051002. https://doi.org/10.1115/1.4004062
• Jialei, 李家垒 Li, 许化龙 Xu Hualong, and 何婧 He Jing. 2011. “Temperature Compensation of Start-up Drift for Fiber Optic Gyroscope Based on Wavelet Network.” Acta Optica Sinica 31 (5): 0506005. https://doi.org/10.3788/aos201131.0506005
• Jiang, Taofei, Liran Chen, Shuaiqi Liu, Meng Xia, Dexin Ba, and Yongkang Dong. 2025b. “Complete Characterization of Polarization-Maintaining Fibers in Fiber-Optic Gyroscope Coils Using Stimulated Brillouin Scattering.” Chinese Optics Letters 23 (10): 100602. https://doi.org/10.3788/col202523.100602
• Jiang, Yifu, and Sihai Li. 2023. “Gyro-Axis-Based Calibration Method for Rate-Bias Laser-Gyroscope Inertial Navigation System.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_41
• Jiang, Tao, and Defu Lin. 2016. “Tensor Product Model-Based Gain Scheduling of a Missile Autopilot.” Transactions of the Japan Society for Aeronautical and Space Sciences 59 (3): 142–49. https://doi.org/10.2322/tjsass.59.142
• Jianzhong, Wang. 2018. “Research on Initial Alignment of Vehicle Strapdown Inertial Navigation System.” Journal of Engineering 2018 (16): 1629–36. https://doi.org/10.1049/joe.2018.8323
• Jieyu, 刘洁瑜 Liu, 蔚国强 Yu Guoqiang, 杨建业 Yang Jianye, and 汪立新 Wang Lixin. 2012. “A New Method of Error Autocompensation for Ring Laser Gyroscope in Rotation-Modulated Strapdown Inertial Navigation System.” Acta Optica Sinica 32 (3): 0323002. https://doi.org/10.3788/aos201232.0323002
• Jimmerson, Gary T., and Hans J. Dall. 2000. Application of Low-Cost Turbo-Jet Powered Interceptors for Cruise Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada391408
• Jin, Sangwook, Hojin Choi, Jong-Ryul Byun, and Gisu Park. 2023a. “Combustion Characteristics of a Dual-Mode Ramjet Engine with a Supersonic Aerodynamic Ramp Injector.” Preprint, . https://doi.org/10.2139/ssrn.4459211
• Jin, Wei, and Brian Culshaw. 1992. “Laser Intensity Noise in a Fiber Optic Gyroscope System Due to Signal Feedback.” In SPIE Proceedings, vol. 1585, edited by Shaoul Ezekiel, Eric Udd. SPIE. https://doi.org/10.1117/12.135065
• Jin, Zhu, Jingwen Huang, Weiping Yang, Liu Gao, and Zhaozi Zu. 2025b. “A Precision Evaluation Method for Initial Alignment Algorithm of Rotating Inertial Navigation System.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2204-7_31
• Jin, Zhenlu, Xuezhi Wang, Bill Moran, Quan Pan, and Chunhui Zhao. 2016. “Multi-Region Scene Matching Based Localisation for Autonomous Vision Navigation of UAVs.” Journal of Navigation 69 (6): 1215–33. https://doi.org/10.1017/s0373463316000187
• Jin, Yi, Lu Zhang, and Ying Chen. 2026. “Flow Characteristics of the Hypersonic Inlet Unstart/restart Process Induced by Downstream Backpressure.” Journal of Physics: Conference Series 3170 (1): 012036. https://doi.org/10.1088/1742-6596/3170/1/012036
• Jin, Yi, Yue Zhang, Hui-jun Tan, and Hang Yu. 2023c. “Unstart/Restart Boundary Broadening Method for a Two-Dimensional Supersonic Variable Inlet Based on a Distributed Bleed System.” Journal of Aerospace Engineering 36 (1): 04022115. https://doi.org/10.1061/jaeeez.aseng-4615
• Jing, Tingting, Guoqiang He, Bin B. Lin, Wenqiang Li, Fei Qin, and Yang Liu. 2016b. “Thermal Analysis of RBCC Engine at Ejector, Ramjet and Scramjet Modes.” In 14th International Energy Conversion Engineering Conference. AIAA 2016-4913. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4913
• Jing, Cheng, and Tang Shuo. 2008. “Integrated Optimization Design of Hypersonic Cruise Vehicle.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-142
• Jing, Che, Tang Shuo, and Kang Bingnan. 2007. “Airframe/Scramjet Integrated Design of Hypersonic Cruise Vehicle.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-642
• Jing, Che, and Shao Yuan-pei. 2015. “Concurrent Subspace Optimization Design of Hypersonic Cruise Vehicle.” In 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2015-3242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3242
• Jischke, Martin C. 1978. Supersonic Flow past Conical Bodies with Nearly Circular Cross-Sections. Defense Technical Information Center. https://doi.org/10.21236/ada068004
• Jo, Min-Seon, Bu-Kyeng Sung, Seung-Min Jeong, and JeongYeol Choi. 2024. “Operation Mode Analysis of Dual Combustion Ramjet Engine from 3D Turbulent Combustion Simulation.” In AIAA SCITECH 2024 Forum. AIAA 2024-1249. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1249
• Jo, Min-Seon, Bu-Kyeng Sung, Seung-Min Jeong, JeongYeol Choi, Vigor Yang, and Umesh Unnikrishnan. 2025. “LES Investigation on the Supersonic Turbulent Combustion in Dual Combustion Ramjet Engine.” In AIAA SCITECH 2025 Forum. AIAA 2025-2487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2487
• Johansen, H. K. 1969. Uncertainty Estimation via Preflight Test Procedures for a Space Stabilized Inertial Navigation System. NASA-CR-107311. NASA. https://ntrs.nasa.gov/citations/19700004824
• Johns, Christopher. 2000. “Solution of an Engine Inlet Compatibility Problem during C-17 Low Cost N/EAT Nacelle Thrust Reverser Development.” In 2000 World Aviation Conference. AIAA 2000-5579. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5579
• Johnson, Cris William. n.d. “Design and Analysis of an Inertial Calibration Kalman Filter.” PhD diss., Iowa State University. https://doi.org/10.31274/td-20260408-59
• Johnson, H. A. 1949. “Discussion: “Supersonic Convective Heat-Transfer Correlation from Skin-Temperature Measurements on a V-2 Rocket in Flight” (Fischer, W. W., and Norris, R. H., 1949, Trans. ASME, 71, Pp. 457–467).” Journal of Fluids Engineering 71 (5): 467–467. https://doi.org/10.1115/1.4017111
• Johnson, L. M. 1985. “Integrated-Optic Fiber-Gyroscope Chip Components.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1985.wbb4
• Johnson, Andrew, Adnan Ansar, and Larry Matthies. 2007. Mapped Landmark Algorithm for Precision Landing. NPO-44463. California Inst. of Tech. https://ntrs.nasa.gov/citations/20100010934
• Johnson, Donald, Thomas Bogar, and James Hunt. 2001. “Configuration Development for a Hydrocarbon Fueled Hypersonic Cruise Vehicle.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1926
• Johnson, Andrew, and Tonislav Ivanov. 2011. “Analysis and Testing of a LIDAR-Based Approach to Terrain Relative Navigation for Precise Lunar Landing.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6578
• Johnson, Alan, Thomas Jacobs, Adam Stiegelmeier, John Pope, and Michael Martindale. 2006. “Simulating Reusable Military Launch Vehicle Regeneration Activities between Flights.” In Space 2006. AIAA 2006-7230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7230
• Johnson, Ethan, Chase Jenquin, and Venkateswaran Narayanaswamy. 2022. “Experimental Studies of Unstart Shock Dynamics within a Streamtraced Scramjet Inlet.” In AIAA AVIATION 2022 Forum. AIAA 2022-3478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3478
• Johnson, W., B. Johnson, and N. Swaminathan. 1989. Stellar Inertial Navigation Workstation. MSC-21093. Abacus Programming Corp. https://ntrs.nasa.gov/citations/19890000074
• Johnson, C., and J. W. Mosely. 1964. Preliminary Warhead Terminal Ballistic Handbook. Part 1. Terminal Ballistic Effects. Defense Technical Information Center. https://doi.org/10.21236/ad0350496
• Johnson, Alan, and Joseph Servidio. 2008. “Ground Support Process Time Refinement for Reusable Launch Vehicle Regeneration Modeling.” In AIAA SPACE 2008 Conference & Exposition. AIAA 2008-7647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7647
• Johnson, J. A., and B. J. C. Wu. 1975. “Pressure Recovery in Supersonic Diffusers.” Journal of Fluids Engineering 97 (3): 374–76. https://doi.org/10.1115/1.3447318
• Johnson, Joseph A., III, and Benjamin J. Wu. 1974. Pressure Recovery and Related Properties in Supersonic Diffusers: A Review. Defense Technical Information Center. https://doi.org/10.21236/ada017631
• Johnson-Groh, Mara. 2018. “Numerical Supersonic Flow Simulations Help Improve High-Speed Engine Design.” Scilight 2018 (40): 400004. https://doi.org/10.1063/1.5063584
• Johnston, P. J., and J. L. Hunt. 1984. Mach 6 Flow-Field and Boundary-Layer Surveys beneath the Forebody of an Airbreathing Missile. AIAA PAPER 84-0233. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840035176
• Jones, Robert. 1970a. Flight Test Results of a DAVI Isolated Platform. Defense Technical Information Center. https://doi.org/10.21236/ad0880948
• Jones, A. 1970b. “Spiral–A New Algorithm for Non-Linear Parameter Estimation Using Least Squares.” Computer Journal 13 (3): 301–8. https://doi.org/10.1093/comjnl/13.3.301
• Jones, Ruel Edwin. 1991. “An Autonomous Rendezvous and Docking System Using Cruise Missile Technologies.” In NASA, Washington, NASA Automated Rendezvous and Capture Review. A Compilation of the Abstracts. https://ntrs.nasa.gov/citations/19930013083
• Jones, Ruel. 1992a. “An Autonomous Rendezvous and Docking System Using Cruise Missile Technologies.” In Space Programs and Technologies Conference. AIAA 1992-1721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1721
• Jones, Ruel E. 1992b. “Autonomous Rendezvous, Docking, and Landing System Using Cruise Missile Technologies.” In SPIE Proceedings, vol. 1694, edited by Sharon S. Welch. SPIE. https://doi.org/10.1117/12.138134
• Jones, Michael, and Carlos Cesnik. 2025. “Aerothermoelastic Modeling Effects on the Simulation of Free-Flying Hypersonic Vehicles.” In AIAA SCITECH 2025 Forum. AIAA 2025-0414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0414
• Jones, R. A., and P. W. Huber. 1978. “Airframe-Integrated Propulsion System for Hypersonic Cruise Vehicles.” In Recent Advan. in Structures for Hypersonic Flight, Pt. 1. https://ntrs.nasa.gov/citations/19790013253
• Jones, P., E. Mickle, and G. Swetnam. 1970. “Homing Radar Tracking Accuracy Improvement with Frequency Diversity.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-992. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-992
• Jones, Ed, and Bruce Nicholson. 1991. “An Autonomous Rendezvous and Docking System Using Cruise Missile Technology.” In NASA, Washington, NASA Automated Rendezvous and Capture Review. Executive Summary. https://ntrs.nasa.gov/citations/19930012243
• Jones, E., and J. W. Parker. 1986. “Bias Reduction by Polarisation Dispersion in the Fibre-Optic Gyroscope.” Electronics Letters 22 (1): 54–56. https://doi.org/10.1049/el:19860037
• Joos, Alexander, Matthias Müller, Daniel Baumgärtner, Walter Fichter, and Frank Allgöwer. 2011. “Nonlinear Predictive Control Based on Time-Domain Simulation for Automatic Landing.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6298. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6298
• Jordan, Stanley K. 1986. “Establishing Requirements for Gravity Surveys for Very Accurate Inertial Navigation.” Navigation 33 (2): 90–108. https://doi.org/10.1002/j.2161-4296.1986.tb00930.x
• Jordan, F. L., Jr. 1972. Investigation at near-Sonic Speed of Some Effects of Humidity on the Longitudinal Aerodynamic Characteristics of an NASA Supercritical Wing Research Airplane Model. NASA-TM-X-2618. NASA. https://ntrs.nasa.gov/citations/19830002759
• Joscelyne, Robert, and Trevor Young. 2011. “An Approach to Formulate and Model Aerodynamic Drag on Aircraft Landing Gear.” In 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. AIAA 2011-7061. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-7061
• Jose, Ebi. n.d. “Automatic Feature Detection and Terrain Mapping Using Millimeter Wave Radar for Autonomous Land Vehicle Navigation.” PhD diss., Nanyang Technological University. https://doi.org/10.32657/10356/46991
• Joshi, Hemant, Peter Thomas, Hongwei Wu, and Christabel Tan. 2024. “Improved Drag Prediction Using Mach-Cone Influence in Vortex Lattice Method for Supersonic Aircraft.” In AIAA SCITECH 2024 Forum. AIAA 2024-1879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1879
• Joubert, Dominique, J. D. Stigter, and Jaap Molenaar. 2021. “Assessing the Role of Initial Conditions in the Local Structural Identifiability of Large Dynamic Models.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-209455/v1
• Jovanovic, Ilija, John P. Enright, and Kaamran Raahemifar. 2014. “Improved Star Tracker Calibration Observability.” In AIAA/AAS Astrodynamics Specialist Conference. AIAA 2014-4418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-4418
• Joyner, U. 1969. “Steerable Landing Gear for Vehicles with Main Gear Skids.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-790. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-790
• Joyner, U. T. 1970. A Steerable Landing Gear for Vehicles with Main Gear Skids. AIAA PAPER 69-790. NASA. https://ntrs.nasa.gov/citations/19700052398
• Ju, Gwanghyeok, Hye-Young Kim, Tom Pollock, and John Junkins. 1999. “DIGISTAR: A Low Cost Micro Star Tracker.” In Space Technology Conference and Exposition. AIAA 1999-4603. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4603
• Ju, Gwanghyoek, Hye-Young Kim, Tom Pollock, and John Junkins. 2000. “Micro Star Tracker and Attitude Determination System.” In Space Technology Proceedings. Springer Netherlands. https://doi.org/10.1007/978-94-015-9395-3_27
• Juang, Jeng-Nan, and R. Radharamanan. 2009. “Evaluation of Ring Laser and Fiber Optic Gyroscope Technology.” In 2009 Fall ASEE Middle Atlantic Section Conference Proceedings. ASEE Conferences. https://doi.org/10.18260/1-2-1153-50181
• Juang, Jyh-Ching, and Shang-Lin Yu. 2016. “Context-Dependent Scan Matching for Aided Navigation.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2016.13430
• Judd, Joseph H., and Ralph A. Falanga. 1956. Flight Investigation of the Effect of a Propulsive Jet Positioned According to the Transonic Area Rule on the Drag Coefficients of a Single-Engine Delta-Wing Configuration at Mach Numbers from 0.83 to 1.36. NACA-RM-L56A16. NASA. https://ntrs.nasa.gov/citations/19930089355
• Julian L. Center. 1975. Systematic Design of Modular Estimators for Aircraft Navigation. Defense Technical Information Center. https://doi.org/10.21236/adb006719
• Jump, Michael, and Gareth Padfield. 2005. “Tau Flare or Not Tau Flare: That Is the Question: Developing Guidelines for an Approach and Landing Sky Guide.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6404. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6404
• Junaid R, Mohammed, and Laila Beebi M. 2015. “Non-Linear Adaptive Control on Reusable Launch Vehicle Due to Actuator Stuck.” International Journal of Scientific Engineering and Research 3 (8): 45–48. https://doi.org/10.70729/ijser15399
• Jung, Suk. 2003. “Investigation of Plume Effects on Longitudinal Aerodynamics of Missile at M=1.2.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3938
• Jung, A-Mi, Hyun-Jin Kim, Hui-Jin Kim, and Seok-Bong Park. 2022. “A Study on the RAM-C Analysis for Optimization of Life Cycle Cost of Weapon System.” Journal of the Korea Academia-Industrial cooperation Society 23 (9): 185–92. https://doi.org/10.5762/kais.2022.23.9.185
• Jung, Ki-Wook, Hyeonjae Kim, Min-Jea Tahk, and Chang-Hun Lee. 2025a. “Feedback Landing Guidance for Reusable Launch Vehicle in Atmosphere Based on Homing Guidance.” In IAF Astrodynamics Symposium. International Astronautical Federation (IAF). https://doi.org/10.52202/083087-0113
• Jung, Jongho, Jaehyoung Park, Dabeen Jeong, and Shinkyu Jeong. 2025b. “Mission-Based Multidisciplinary Optimization of a Reusable Unmanned Space Vehicle.” International Journal of Aeronautical and Space Sciences 27 (2): 1189–1202. https://doi.org/10.1007/s42405-025-01031-4
• Jurado, Juan D., and John F. Raquet. 2017. “Keynote: A Common Framework for Inertial Sensor Error Modeling.” In ION Pacific PNT. Institute of Navigation. https://doi.org/10.33012/2017.15053
• K.А., Hu Ts. Selezneva M. S. Proletarskiy A. V. Neusypin. 2021. “Parametric Identification of the Error Model for the Aircraft Inertial Navigation System.” Automation Modern Techologies. https://doi.org/10.36652/0869-4931-2021-75-7-317-321
• Kaçar, Emin N., Altug Piskin, and Berrin Erbay. 2018. “Coupled Heat Transfer Investigation for Turbine Cavity of a Turbojet Engine.” In 2018 Joint Propulsion Conference. AIAA 2018-4433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4433
• Kada, B. 2015. “Two-Channel Pitch/yaw Missile Autopilot Design Using Arbitrary Order Sliding Modes Based Pole Placement.” Aeronautical Journal 119 (1216): 765–79. https://doi.org/10.1017/s0001924000010812
• Kadam, Mahesh, S. Sathish, Aditya Bujurke, Keertivardhan Joshi, and Balamurugan Gopalsamy. 2018. “Dynamics of Articulated Landing Gear in Tail-Down Landing Condition.” In Lecture Notes in Mechanical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-10-8597-0_17
• Kadiwar, R. K., and I. P. Giles. 1989. “Optical Fibre Brillouin Ring Laser Gyroscope.” Electronics Letters 25 (25): 1729–31. https://doi.org/10.1049/el:19891157
• Kaehr, Ronald, and Marvin Spector. 1980. “USAF Development of Optical Correlation Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959129
• Kaemming, Tom. 2001. “Integrated Vehicle Comparison of Turbo-Ramjet Engine and Pulsed Detonation Engine (PDE).” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/2001-gt-0451
• Kaemming, T. 2002. “Integrated Vehicle Comparison of Turbo-Ramjet Engine and Pulsed Detonation Engine.” Journal of Engineering for Gas Turbines and Power 125 (1): 257–62. https://doi.org/10.1115/1.1496116
• Kaertner, Franz X. 2006. Narrow Linewidth Tunable Solid-State Microchip Lasers for Precision Inertial Navigation Systems (PINS). Defense Technical Information Center. https://doi.org/10.21236/ada442348
• Kahn, W. D. 1984. Accuracy of Mapping the Earth’s Gravity Field Fine Structure with a Spaceborne Gravity Gradiometer Mission. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/19840022404
• Kahn, W. D., and T. S. Englar Jr. 1987. “Gravity Field Fine Structure Estimation Techniques for a Spaceborne Gravity Gradiometer.” In 1987 Annual Summer Computer Simulation Conference. https://ntrs.nasa.gov/citations/19880059732
• Kahn, W. D., and F. O. Von Bun. 1985. “Error Analyses for a Gravity Gradiometer Mission.” IEEE Transactions on Geoscience and Remote Sensing GE-23. https://ntrs.nasa.gov/citations/19850060321
• Kailasanath, K., J. Gardner, J. Boris, and Elaine Oran. 1986. Numerical Simulations of the Flowfield in a Central-Dump Ramjet Combustor. 1. Tests of the Model and Effects of Forcing. Defense Technical Information Center. https://doi.org/10.21236/ada170936
• Kain, J., C. Brown Jr., J. Lee, S. Pallas, and E. Sears. 1978. “Missile Aerodynamic Parameter and Structure Identification from Flight Test Data.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1341. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1341
• Kajioka, H., N. Ashizuka, T. Kumagai, and H. Nakai. 1992. “Experimental Investigation on Direction Sensor Using a Fiber Optic Gyroscope with High Resolution.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1992.w24
• Kaku, Ryoji. 1990. “Amplitude Variation Effects of Phase Modulators in a Serrodyne Fiber-Optic Gyroscope.” In SPIE Proceedings, vol. 1169, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.963049
• Kalaghan, P. M., and G. Colombo. 1978. “Gravity Gradient Determination with Tethered Systems.” In Alabama Univ. UAH(NASA Workshop on the Use of a Tethered Satellite System. https://ntrs.nasa.gov/citations/19810020943
• Kalantarov, Dmitriy, and Christopher P. Search. 2013. “The Role of Waveguide Coupling on the Sensitivity of a Coupled Resonator Optical Waveguide Gyroscope.” In Frontiers in Optics 2013. OSA. https://doi.org/10.1364/fio.2013.ftu3a.17
• Kalata, Paul R. 1984. An Information-Theoretic Approach to Target Estimation of a Laser Radar Tracking System. Defense Technical Information Center. https://doi.org/10.21236/ada142247
• Kalenova, N. V. 2009. “Influence of the Resonator Angular Displacements in a Hemispherical Resonator Gyro on the Coupling between the Working and Beam-Type Vibrations.” Mechanics of Solids 44 (5): 686–90. https://doi.org/10.3103/s0025654409050057
• Kaletka, Juergen, and Kuang-Hua Fu. 1993. “Frequency-Domain Identification of Unstable Systems Using X-31A Aircraft Flight Test Data.” In Flight Simulation and Technologies. AIAA 1993-3635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3635
• “Kalman Filter Inertial Navigation System Flight Applications.” 1999. In Integrated Navigation and Guidance Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861994.0095.0107
• Kamalvand, Ahmad, Paul MacDonald, and Thai-Duong Tran. 2004. Factored Sampling Tracking: Comparison of the Kalman and the Condensation Algorithms for Missile Tracking in a Defense Target Environment. Defense Technical Information Center. https://doi.org/10.21236/ada430271
• Kamel, Ahmed A., Donald E. Ekman, John Savides, and Gerald J. Zwirn. 1988. Star Sightings by Satellite for Image Navigation. Patent Number: US-PATENT-4,746,976. Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20080012403
• Kane, L. D., A. J. Mooers, D. F. Nickel, and R. D. Willey. 1966. Breadboard Design of a Scanning Celestial Attitude Determination System (SCADS) Final Report. NASA-CR-91532. NASA. https://ntrs.nasa.gov/citations/19680004046
• Kaneko, Kento, Akira Oyama, and Aiko Yakeno. 2024. “Viscous Drag Reduction Effect of Riblet at Cruising Speed of Transonic Aircraft.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3588
• Kang, Suktae, Kyung Jun Han, and Myeong-Jong Yu. 2020. “Robust Immune Particle Filter Design for Terrain-Referenced Navigation with Interferometric Radar Altimeter.” IET Radar, Sonar & Navigation 14 (9): 1402–9. https://doi.org/10.1049/iet-rsn.2020.0047
• Kang, Guo, Du Xiaojing, and Mao Xinyuan. 2011. “Research on Multi Update Rate Method of Precise Satellite Attitude Determination Based on Gyro and Star-Sensor.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6645
• Kansas Univ Lawrence. 1952a. Launching and Landing of Carrier Aircraft. Part 3. a Multi-Jet Driven Catapult (Hydrapult). Defense Technical Information Center. https://doi.org/10.21236/ad0009895
• Kansas Univ Lawrence. 1952b. The Launching and Landing of Carrier Aircraft. Part 4. Barricades. Defense Technical Information Center. https://doi.org/10.21236/ad0021570
• Kanter, J. I. 1966. Applications for Inertial Sensors in Space. NASA. https://ntrs.nasa.gov/citations/19670043667
• Kaplan, George H. 1996a. The Motion of the Observer in Celestial Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada423226
• Kaplan, George H. 1996b. A Navigation Solution Involving Changes to Course and Speed. Defense Technical Information Center. https://doi.org/10.21236/ada434100
• Kaplan, Marshall H. 2002. “Reusable Launch Vehicle Facts and Fantasies.” In AIP Conference Proceedings, vol. 608. AIP. https://doi.org/10.1063/1.1449851
• Kapoor, Kamlesh, Bernhard H. Anderson, and Robert J. Shaw. 1994. A Full Navier-Stokes Analysis of Subsonic Diffuser of a Bifurcated 70/30 Supersonic Inlet for High Speed Civil Transport Application. NASA-TM-106637. NASA. https://ntrs.nasa.gov/citations/19950004408
• Karabutov, Nikolay Nikolayevich. 2020. “Structural Identifiability of Nonlinear Dynamic Systems under Uncertainty.” International Journal of Intelligent Systems and Applications 12 (1): 12–22. https://doi.org/10.5815/ijisa.2020.01.02
• Karabutov, Nikolay. 2025a. “On Structural Identifiability of Decentralised Systems.” Preprint, . https://doi.org/10.20944/preprints202502.1380.v1
• Karabutov, Nikolay. 2025b. “Parametric Identifiability of Dynamic Systems Based on Adaptive Systems.” Preprint, . https://doi.org/10.20944/preprints202506.1561.v1
• Karel, G. 1967. “Near Term Reusable Rocket Launch Vehicle Concepts.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/670378
• Karimli, Toghrul. 2023. “Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices.” Herald of the Azerbaijan Engineering Academy 15 (2): 7–14. https://doi.org/10.52171/2076-0515_2023_15_02_07_14
• Karin, Omer, Uri Alon, and Eduardo Sontag. 2017. “A Note on Dynamical Compensation and Its Relation to Parameter Identifiability.” Preprint, bioRxiv. https://doi.org/10.1101/123489
• Karlgaard, Chris D., Prasad Kutty, and Mark Schoenenberger. 2015. “Coupled Inertial Navigation and Flush Air Data Sensing Algorithm for Atmosphere Estimation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-0526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0526
• Karmozdi, Ali, Mojtaba Hashemi, and Hassan Salarieh. 2018. “Design and Practical Implementation of Kinematic Constraints in Inertial Navigation System-Doppler Velocity Log (INS-DVL)-Based Navigation.” Navigation 65 (4): 629–42. https://doi.org/10.1002/navi.271
• Karp, K. A., V. V. Malyshev, A. Y. Mishin, and P. V. Pakshin. 2003. “Algorithms of a Complex Inertial and Satellite Navigation System for Aircraft.” In Space Studies. Springer Netherlands. https://doi.org/10.1007/978-94-017-0401-4_27
• Karwacki, Francis A., Martin A. Sanzari, and H. L. Cui. 1996. Superconducting Gyroscope,. Defense Technical Information Center. https://doi.org/10.21236/ada318927
• Kasahara, Mikihiro, and Katsuya Hasegawa. 2025. “Flying by the Sun: Solar-Based Celestial Navigation for UAVs.” Preprint, . https://doi.org/10.31219/osf.io/sdjbe_v1
• Kashima, Yasumasa, Akio Matoba, Masao Kobayashi, and Hiroshi Takano. 1991. “1.55-μm Superluminescent Diode for a Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 1365, edited by Paul M. Kopera. SPIE. https://doi.org/10.1117/12.24665
• Kashiwagi, Yasutada. 1968. Prediction of Ballistic Missile Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ad0728502
• Kashyap, Sudesh K. 2025. “Vision-Aided Inertial Navigation.” In Mathematical Modelling of Aerospace Dynamic Systems with Practical Applications. CRC Press. https://doi.org/10.1201/9781003429869-5
• Kassas, Zaher, and Todd Humphreys. 2012. “Observability Analysis of Opportunistic Navigation with Pseudorange Measurements.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4760. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4760
• Kassas, Zak M., Joe Khalife, Ali Abdallah, and Chiawei Lee. 2020. “I Am Not Afraid of the Jammer: Navigating with Signals of Opportunity in GPS-Denied Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2020.17737
• Kato, Akio, and Yoshiki Inagaki. 2007. “Control Law for Automatic Landing Using Fuzzy Logic Control.” Journal of the Japan Society for Aeronautical and Space Sciences 55 (636): 17–26. https://doi.org/10.2322/jjsass.55.17
• Kato, Akio, and Yoshiki Inagaki. 2008. “Control Law for Automatic Landing Using Fuzzy-Logic Control.” Transactions of the Japan Society for Aeronautical and Space Sciences 50 (170): 274–83. https://doi.org/10.2322/tjsass.50.274
• Kau, S., A. Morgan, R. Malzahn, and T. Nosek. 1983. “Laser Gyro for Instrumentation of Advanced Missile Guidance System Testing.” In Guidance and Control Conference. AIAA 1983-2271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2271
• Kauffman, H., R. Grandhi, W. Hankey, and P. Belcher. 1991. “Optimum Transitions in Climb/cruise/descent for Hypersonic Cruise Vehicles.” In 29th Aerospace Sciences Meeting. AIAA 1991-472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-472
• Kaufman, H. 1976. Research in Digital Adaptive Flight Controllers. NASA-CR-2684. NASA. https://ntrs.nasa.gov/citations/19760017143
• Kaufman, L. G., II, and C. B. Johnson. 1984. Aerodynamic Heating Rate Distributions Induced by Trailing Edge Controls on Hypersonic Aircraft Configurations at Mach 8. NASA-TM-87453. NASA. https://ntrs.nasa.gov/citations/19850014059
• Kaufmann, David N., and B. David McNally. 1995. Flight Test Evaluation of the E-Systems Differential GPS Category 3 Automatic Landing System. NASA-TM-110368. NASA. https://ntrs.nasa.gov/citations/19960002042
• Kaufmann, David N., and B. David Ncnally. 1995. Flight Test Evaluation of the Stanford University/United Airlines Differential GPS Category 3 Automatic Landing System. NASA-TM-110354. NASA. https://ntrs.nasa.gov/citations/19950024367
• Kawamura, T., W. Chyu, and D. Bencze. 1987. “Numerical Simulation of Three-Dimensional Supersonic Inlet Flow Fields.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-160
• Kay, Jennifer S., and C. Thorpe. 1995. “Operator Interface Design Issues in a Low-Bandwidth and High-Latency Vehicle Teleoperation System.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/951485
• Kayton, Myron. 1962. “Fundamental Limitations on Inertial Measurements.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395586-9.50020-9
• Kazarian, K., W. Koerner, and D. Stewart. 1973. “The P-Star Technique and Its Application to Inertial Guidance.” In Guidance and Control Conference. AIAA 1973-837. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-837
• Kaznevskiy, V. P. 1967. Firing of the World’s First Ramjet Rocket. Holman (John F.) and Co., Inc. https://ntrs.nasa.gov/citations/19680004102
• Keçeci, Murat, Yavuzer Karakuş, and Ramin Barzegar. 2025. “A Rapid Prediction Tool for Aerodynamic Heating in High-Speed Aircraft Design.” In ASME 2025 Heat Transfer Summer Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/ht2025-154242
• Keenan, J., and J. Kuhlman. 1991. “Winglet Effectiveness on Low Aspect Ratio Wings at Supersonic Mach Numbers.” In 9th Applied Aerodynamics Conference. AIAA 1991-3305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3305
• Kehrer, W. 1971. “The Performance Benefits Derived for the Supersonic Transport Througha New Approach to Stability Augmentation.” In 3rd Aircraft Design and Operations Meeting. AIAA 1971-785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-785
• Keijer, Wouter, and Martin Weiss. 2005. “Aerodynamic Missile Characteristics from Telemetry Measurements.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2005-6022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6022
• Kelly, R. J. 1977. “Guidance Accuracy Consideration for the Microwave Landing System.” Navigation 24 (3): 189–205. https://doi.org/10.1002/j.2161-4296.1977.tb01284.x
• Kelly, R. J. 1980. “Supersonic Cruise Vehicle Research/business Jet.” In NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2. https://ntrs.nasa.gov/citations/19810009499
• Kelly, Alonzo. 1994. A 3D State Space Formulation of a Navigation Kalman Filter for Autonomous Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada282853
• Kelly, Michael, A. C. Charania, John Olds, and Dominic DePasquale. 2009. “Discrete Event Simulation of Reusable Launch Vehicle Development, Acquisition, and Ground Operations.” In AIAA SPACE 2009 Conference & Exposition. AIAA 2009-6484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6484
• Kelly, R. J., and E. F. C. LaBERGE. 1980. “Guidance Accuracy Considerations for the Microwave Landing System Precision DME.” Navigation 27 (1): 1–22. https://doi.org/10.1002/j.2161-4296.1980.tb01395.x
• Kelly, Thomas C., and Robert S. Osborne. 1954. Effects of Fuselage Modifications on the Drag Characteristics of a 1/20-Scale Model of the Convair F-102 Airplane at Transonic Speeds. NACA-RM-SL54K18a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028506
• Kelly, Jonathan, and Gaurav S. Sukhatme. 2010. “Visual-Inertial Sensor Fusion: Localization, Mapping and Sensor-to-Sensor Self-Calibration.” International Journal of Robotics Research 30 (1): 56–79. https://doi.org/10.1177/0278364910382802
• Kelso, J. 1993. “Boresight Error Slope Predictions versus Flight Test Results in a Hypersonic Flow Field.” In Annual Interceptor Technology Conference. AIAA 1993-2688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2688
• Kennedy, Paul. 1995. “Ballistic Missile Defence Command, Control and Communications.” In Space Programs and Technologies Conference. AIAA 1995-4026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-4026
• Kennedy, J., and C. Lowry. 1995. “Space Shuttle Orbiter Drag Parachute System.” In 13th Aerodynamic Decelerator Systems Technology Conference. AIAA 1995-1595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1595
• Kennel, H. 1967. “Initial Alignment of a Strapdown Inertial Reference and Navigation System.” In Control and Flight Dynamics Conference. AIAA 1967-556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-556
• Kennon, Stephen. 1989. “Supersonic Inlet Calculations Using an Upwind Finite-Volume Method on Adaptive Unstructured Grids.” In 27th Aerospace Sciences Meeting. AIAA 1989-113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-113
• Kenny, Thomas, Albert Lee, Michael Donnelly, Michael Schroder, and Mark McNally. 2003. Performance of the Star Tracker Lightshades on the Earth Observing Satellite (EOS) Aqua. NASA Headquarters. https://ntrs.nasa.gov/citations/20030022762
• Kepler, C. Edward, and Frank W. Barry. 1965. “Engine Air Inlet Compatibility for the Supersonic Transport.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/650225
• Kepler, C., and G. Champagne. 1989. “Performance Potential of Air Turbo-Ramjet Employing Supersonic through-Flow Fan.” In 27th Aerospace Sciences Meeting. AIAA 1989-10. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-10
• Kerlick, G. 1985. “Adaptive Mesh Solution for Supersonic Conical Flow in a Rectilinear Inlet.” In 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. AIAA 1985-1626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1626
• Kersey, A. D., A. Dandridge, and W. K. Burns. 1989. “Fiber Optic Gyroscope Technology.” Optics News 15 (11): 12. https://doi.org/10.1364/on.15.11.000012
• Kerslake, W. R. 1958. Combustion of Gaseous Hydrogen at Low Pressures in a 35 Deg Sector of a 28-Inch-Diameter Ramjet Combustor. NACA-RM-E58A21A. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19660030240
• Kersten, P. R., and A. C. Kak. 1989. Tutorial on Using LISP Object-Oriented Programming for Blackboards: Solving the Radar Tracking Problem. Defense Technical Information Center. https://doi.org/10.21236/ada224272
• Keshmiri, Shahriar, Richard Colgren, Saeed Farokhi, and Maj Mirmirani. 2006. “Ramjet and Scramjet Engine Cycle Analysis for a Generic Hypersonic Vehicle.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8158
• Ketchum, Eleanor A., and Robert H. Tolson. 1993. “Lost in Space: Onboard Star Identification Using CCD Star Tracker Data without an a Priori Attitude.” In In: Spaceflight dynamics 1993; AAS(NASA International Symposium, 8th, Greenbelt, MD, Apr. 26-30, 1993, Parts 1 & 2 . A95-85716. https://ntrs.nasa.gov/citations/19950054194
• Ketterle, Wolfgang, Vladan Vuletic, and Mara Prentiss. 2008. Atom Interferometry on Atom Chips-A Novel Approach towards Precision Inertial Navigation Systems (PINS). Defense Technical Information Center. https://doi.org/10.21236/ada499671
• Keum, Seunghwan, and Alok Warey. 2026. “Bracketing Inference with Uncertainty Quantification: A Reliability Pipeline for Neural Aerodynamic Surrogates.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9775673/v1
• Keuper, Jerome P. 1960. “Estimates of Accuracy of Atlantic Missile Instrumentation.” In Bioastronautics and Electronics and Invited Addresses. Elsevier. https://doi.org/10.1016/b978-1-4832-2884-6.50027-0
• Khamlak, Maryna. 2026. “Methodology for Ensuring Safety and Operational Reliability of Reusable Launch Vehicle Composite Structures under High-Intensity Vibroacoustic Loads.” American Journal of Engineering and Technology 08 (06): 01–61. https://doi.org/10.37547/tajet/book-26-01
• Khan, Jan Amir, Lilja Gudmundsdottir, and Mansoor Alam. 2017. “Fiber Optic Gyroscope Coils: Performance Characterization.” In SPIE Proceedings, vol. 10208, edited by Christopher S. Baldwin, Gary Pickrell, Henry H. Du. SPIE. https://doi.org/10.1117/12.2261977
• Khan, Tauha I., Jehanzeb Masud, Zakria G. Toor, and Bilal Mufti. 2019. “Analysis of High Alpha Aerodynamic Characteristics of a Supersonic Aircraft.” In AIAA Scitech 2019 Forum. AIAA 2019-2307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2307
• Khan, Hassan N., Jehanzeb Masud, Usman Zia, and Muhammad Muneeb Safdar. 2025. “Investigation for Reduction of Wave Drag through Design and Analysis of Supersonic Fuel Tanks.” In AIAA SCITECH 2025 Forum. AIAA 2025-1051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1051
• Khan, Imran, Ahmad Rahbar Ranji, David S-K. Ting, and Mohammed Jalal Ahamed. 2023. “Design and Development of a Mems Ring Gyroscope with Ring-Shaped Spokes.” Preprint, . https://doi.org/10.2139/ssrn.4415765
• Khandelwal, Suresh C., Gary Cole, and Joongkee Chung. 1996. “Parallel Computation of Unsteady Supersonic-Inlet Flows.” In Parallel Computational Fluid Dynamics 1995. Elsevier. https://doi.org/10.1016/b978-044482322-9/50138-9
• Khankhasaeva, Ya. V. 2023. “Impact of Energy Input on the Aerodynamic Characteristics and Heat Flux Occurring in the 3D Supersonic Flow past a Model Aircraft.” Mathematical Models and Computer Simulations 15 (4): 765–79. https://doi.org/10.1134/s2070048223040063
• Khartovskii, V. E. 2005. “Controllability and Identifiability of Multi-Delay Dynamic Systems.” Automation and Remote Control 66 (9): 1396–1408. https://doi.org/10.1007/s10513-005-0180-4
• Khasawneh, Qais A., and C. Batur. 2003. “Adaptive Control of a Simulated MEMS Gyroscope.” In Microelectromechanical Systems. ASMEDC. https://doi.org/10.1115/imece2003-42140
• Khilnani, Aneesh V., Shida Ye, Yaakov Bar-Shalom, Ahmed Zaki, and Peter Willett. 2026. “Single-Axis Gyroscope Scale Factor Estimation for a First-Order Gauss–Markov Drift Model.” In AIAA SCITECH 2026 Forum. AIAA 2026-1253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1253
• Khlebnikov, V. S. 1990. “Aerodynamic Drag of a Pair of Bodies in Transonic and Supersonic Flow.” Fluid Dynamics 25 (3): 458–62. https://doi.org/10.1007/bf01049830
• Khodabakhshian, Shaghayegh, John Enright, Laila Kazemi, and Andrei Khramtsov. 2020. “Composite Magnitude: A Tool for Creating Better Star Tracker Catalogs.” In AIAA Scitech 2020 Forum. AIAA 2020-1595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1595
• Kholopov, I. S. 2015. “Development of Strapdown Inertial Navigation System with MEMS Sensors, Barometric Altimeter and Ultrasonic Range Meter.” IOP Conference Series: Materials Science and Engineering 93: 012060. https://doi.org/10.1088/1757-899x/93/1/012060
• Khorev, Andrey. n.d. “Hardware/Software Prototyping of a Miniaturized Star Tracker System for a Nanosatellite Platform.” PhD diss., Montpellier. https://doi.org/10.70675/548be7e2zc06bz4d9dz9149za281295b9d72
• Khot, Mantesh Basappa, Abhijit Prekash, Rahul Gopalakrishna, Karan Nanda, and Hriday Ghosh. 2025. “Modelling and Optimisation of Structural Parameters of Main Landing Gear during Touchdown and Taxing.” International Journal of Engineering Systems Modelling and Simulation 16 (5): 294–301. https://doi.org/10.1504/ijesms.2025.148256
• Khudher, Dhayaa. 2026. “LC-MSCKF: Hybrid Learned and Innovation-Feedback Covariance Calibration for Visual-Inertial Odometry.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-10806954/v1
• Kia, Tooraj, Walter J. Fowski, and David J. Flynn. 1993. Flight Performance of TOPEX/POSEIDON Star Tracker. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210004514
• Kidwell, John C. 1963. Takeoff and Landing Capabilities of the Caribou CV-2B Aircraft on Unprepared Surfaces. Defense Technical Information Center. https://doi.org/10.21236/ad0440406
• Killingsworth, W. R., Jr. 1968. Computation Frames for Strapdown Inertial Systems. NASA-CR-103295. NASA. https://ntrs.nasa.gov/citations/19690021976
• Kim, Sukyum. 2005. “Numerical Study on Thrust Performance Evaluation of Laser Propulsion during Supersonic/Hypersonic Flight.” In AIP Conference Proceedings, vol. 766. AIP. https://doi.org/10.1063/1.1925146
• Kim, Young-Taek. 2006. “Micro Supersonic Air-Breathing Laser- Spike Engine Propulsion.” In AIP Conference Proceedings, vol. 830. AIP. https://doi.org/10.1063/1.2203251
• Kim, Matteo. 2023a. “Artificial Runway Design for Shimmy Testing on Nose Landing Gear.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/24625116
• Kim, Kiduck. 2023b. “Design of Inertial Navigation System/Celestial Navigation System Navigation System for Horizontal Position Estimation and Performance Comparison between Loosely and Tightly Coupled Approach.” Journal of Space Technology and Applications 3 (1): 58–71. https://doi.org/10.52912/jsta.2023.3.1.58
• Kim, Eulgon, Hangju Cho, and Yongin Lee. 1996. “Terminal Guidance Algorithms of Missiles Maneuvering in the Vertical Plane.” In Guidance, Navigation, and Control Conference. AIAA 1996-3883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3883
• Kim, Hyun D., and Franco C. Frate. 2001. Experimental Evaluation of the Effect of Angle-of-Attack on the External Aerodynamics and Mass Capture of a Symmetric Three-Engine Air-Breathing Launch Vehicle Configuration at Supersonic Speeds. NASA/TM-2001-210565. NASA. https://ntrs.nasa.gov/citations/20010089702
• Kim, Sungjoong, Kyung Woo Hong, and Hyochoong Bang. 2022c. “Vision-Based Map-Referenced Navigation Using Terrain Classification of Aerial Images.” In AIAA SCITECH 2022 Forum. AIAA 2022-1223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1223
• Kim, Seungkeun, Insung Jung, Youdan Kim, and Changook Park. 2004a. “Hybrid Fault Detection and Isolation Techniques for Aircraft Inertial Measurement Sensors.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5419
• Kim, Y., and K. T. Kang. 2025. “Analysis of Aerodynamic Characteristics for Canard Controlled Missile with Free-Rotating Tail.” Journal of computational fluids engineering 30 (1): 82–94. https://doi.org/10.6112/kscfe.2025.30.1.082
• Kim, Heung-Seob, Ki-Tae Kim, and Geon-Wook Jeon. 2011a. “A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballistic Missile’s Flight Characteristics.” Journal of the Korea Institute of Military Science and Technology 14 (6): 1009–17. https://doi.org/10.9766/kimst.2011.14.6.1009
• Kim, WonGi, JaeYoul Ko, and Jaemyung Ahn. 2026b. “Design Space Exploration of a Reusable Launch Vehicle through Integrated Stage-Mission Optimization.” In AIAA SCITECH 2026 Forum. AIAA 2026-1707. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1707
• Kim, Youngjoo, Dongjin Lee, and Hyochoong Bang. 2013b. “Vision-Only Terrain Referenced Navigation and Uncertainty Analysis for Unmanned Aircraft.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4696. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4696
• Kim, Lawoo, Yudam Lee, and Hyung Keun Lee. 2021a. “Kalman–Hatch Dual-Filter Integrating Global Navigation Satellite System/inertial Navigation System/on-Board Diagnostics/altimeter for Precise Positioning in Urban Canyons.” IET Radar, Sonar & Navigation 16 (2): 379–97. https://doi.org/10.1049/rsn2.12190
• Kim, Cheonjoong, Kyungah Lim, and Seonah Kim. 2021b. “Self-Alignment/Navigation Performance Analysis in the Accelerometer Resonance State Generated by Dither Motion of Ring Laser Gyroscope in Laser Inertial Navigation System.” Journal of the Korea Institute of Military Science and Technology 24 (6): 577–90. https://doi.org/10.9766/kimst.2021.24.6.577
• Kim, Taeyun, Seongho Nam, Changky Sung, and Junpyo Park. 2024. “Vision-Based Terrain-Referenced Navigation with Iterative Closest Point Algorithm.” In ION Pacific PNT. Institute of Navigation. https://doi.org/10.33012/2024.19635
• Kim, Hwan–Seong, Duy Anh Nguyễn, and Heon-Hui Kim. 2004b. “Periodic Bias Compensation Algorithm for Inertial Navigation System.” Journal of Navigation and Port Research 28 (9): 803–8. https://doi.org/10.5394/kinpr.2004.28.9.803
• Kim, Heyone, Sang Heon Oh, Jae Hoon Son, and Dong-Hwan Hwang. 2023b. “Coarse Alignment of Gyro-Free Inertial Navigation System.” Preprint, . https://doi.org/10.20944/preprints202305.0099.v1
• Kim, E. C., and S. H. Park. 2026. “Flow Separation Suppression of Swept Shock Wave-Boundary Layer Interaction by Using Bleed Slots over Supersonic Inlet Sidewall.” Journal of computational fluids engineering 31 (2): 84–103. https://doi.org/10.6112/kscfe.2026.31.2.084
• Kim, Youngjoo, Junwoo Park, and Hyochoong Bang. 2018b. “Terrain-Referenced Navigation Using an Interferometric Radar Altimeter: IRA-Based TRN.” Navigation 65 (2): 157–67. https://doi.org/10.1002/navi.233
• Kim, Sungjoong, Junwoo Park, and HyoChoong Bang. 2025a. “Enhanced Terrain-Referenced Navigation through Adaptive Radar Altimeter Error Estimation with Monte Carlo Sampling.” International Journal of Aeronautical and Space Sciences 26 (4): 1954–74. https://doi.org/10.1007/s42405-024-00881-8
• Kim, Yong-Ho, Yongkyu Park, and Keeyoung Choi. 2023c. “Landing Guidance for Reusable Launch Vehicle Using Sequential Convex Programming with Deep Neural Network Based Initialization.” Journal of the Korean Society for Aeronautical & Space Sciences 51 (8): 507–16. https://doi.org/10.5139/jksas.2023.51.8.507
• Kim, Mark S., Scott J. Pierce, and Kevin M. Brink. 2017. “Celestial Aided Inertial Navigation by Tracking High Altitude Vehicles.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2017.14888
• Kim, Je-Nam, Mun-Ho Ryu, Ho-Rim Choi, and Yoon-Seok Yang. 2013a. “Anatomy Calibration of Inertial Measurement Unit Using a Principle Component Analysis.” International Journal of Bio-Science and Bio-Technology 5 (6): 181–90. https://doi.org/10.14257/ijbsbt.2013.5.6.19
• Kim, B. Y., and H. J. Shaw. 1984a. “All-Fiber-Optic Gyroscope with Linear Scale Factor Using Phase Detection.” In SPIE Proceedings, vol. 0478, edited by Emery L. Moore, O. G. Ramer. SPIE. https://doi.org/10.1117/12.942681
• Kim, B. Y., and H. J. Shaw. 1984b. “Phase-Reading, All-Fiber-Optic Gyroscope.” Optics Letters 9 (8): 378. https://doi.org/10.1364/ol.9.000378
• Kim, Cheon-Joong, Kyu-Min Shim, Heung-Won Park, and Joon Lyou. 2011b. “A Study on the Design Requirement of a Small Ring Laser Gyroscope for Medium-Grade Inertial Navigation.” Journal of the Korean Society for Aeronautical & Space Sciences 39 (8): 788–95. https://doi.org/10.5139/jksas.2011.39.8.788
• Kim, Jonghyuk, and Salah Sukkarieh. 2005. “6DoF SLAM Aided GNSS/INS Navigation in GNSS Denied and Unknown Environments.” Journal of Global Positioning Systems 4 (1&2): 120–28. https://doi.org/10.5081/jgps.4.1.120
• Kim, Cheon-Joong, Haesung Yu, Inseop Lee, Juhyun Oh, and Sang Jeong Lee. 2018a. “A Study on Error Analysis of Dual-Axis Rotational Inertial Navigation System Based on Ring Laser Gyroscope.” Journal of the Korean Society for Aeronautical & Space Sciences 46 (11): 921–33. https://doi.org/10.5139/jksas.2018.46.11.921
• Kimel, H., and D. Harnett. 1963. “Reliability of the Atlas Radio-Command Guidance and Re-Entry Vehicle Systems.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/630576
• Kimmel, Elliot, Daning Huang, Vansh Sharma, Jagmohan Singh, Venkatramanan Raman, and Peretz P. Friedmann. 2024. “Evaluation of Shock Wave-Boundary Layer Interaction Modeling Capabilities for Use in a Hypersonic Aerothermoelastic Framework.” In AIAA SCITECH 2024 Forum. AIAA 2024-2735. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2735
• Kimmel, R., and Y. Oh. 1988. “A Parametric Experimental Investigation of Large Flared Afterbodies on a Supersonic Cruciform Missile.” In 6th Applied Aerodynamics Conference. AIAA 1988-2542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2542
• King, G. E. 1971. “Guided Weapon Design to Meet Cost Requirements.” Aeronautical Journal 75 (730): 747–51. https://doi.org/10.1017/s0001924000046686
• King, I. R. 1983. Accuracy of Measurement of Star Images on a Pixel Array. California, University. https://ntrs.nasa.gov/citations/19830044370
• King, A. D. 1997. “Inertial Navigation: Past, Present, and Future.” In IEE Colloquium on Airborne Navigation Systems Workshop, vol. 1997. IEE. https://doi.org/10.1049/ic:19970908
• King, A. D. 1998. “Inertial Navigation: Past, Present, and Future.” In IEE Airborne Navigation Systems Workshop, vol. 1998. IEE. https://doi.org/10.1049/ic:19980388
• Kirkpatrick, Damon, Dylan Dooner, Andrew J. Neely, Charles Hoke, Timothy J. Beberniss, and David Buttsworth. 2026. “Mach 6 Aerothermoelastic Experiment for an Inclined, Compliant CFCF Panel with Buckling.” In AIAA SCITECH 2026 Forum. AIAA 2026-2045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2045
• Kirsch, Jared R., Nima Fathi, and William J. Rider. 2025. “Application of SciML-Adapted PCMM to Deep Neural Network Surrogate Model Used for Aerodynamic Coefficient Prediction.” Journal of Verification, Validation and Uncertainty Quantification 10 (4): 041001. https://doi.org/10.1115/1.4071802
• Kis, L., and B. Lantos. 2014. “Development of State Estimation System with INS, Magnetometer and Carrier Phase GPS for Vehicle Navigation.” Gyroscopy and Navigation 5 (3): 153–61. https://doi.org/10.1134/s2075108714030055
• Kishi, Yuki, Shinya Kitazaki, Atthaphon Ariyarit, Yoshikazu Makino, and Masahiro Kanazaki. 2017. “Planform Dependency of Optimum Supersonic Airfoil for Wing-Body-Nacelle Configuration Using Multi-Fidelity Design Optimization.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-4468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4468
• Kissel, Glen J., and Fred Y. Hadaegh. 1993. “Micro Guidance and Control Technology Overview.” In Proceedings of the Workshop on Microtechnologies and Applications to Space Systems. https://ntrs.nasa.gov/citations/19940025268
• Kitamura, S., and S. Nakagiri. 1977b. “Identifiability of Spatially-Varying and Constant Parameters in Distributed Systems of Parabolic Type.” SIAM Journal on Control and Optimization 15 (5): 785–802. https://doi.org/10.1137/0315050
• Kitamura, Shinzo, and Shin-ichi Nakagiri. 1978. “Identifiability of Internal and Boundary Parameters in Distributed Systems of Parabolic Type.” In Control of Distributed Parameter Systems. Elsevier. https://doi.org/10.1016/b978-0-08-022018-5.50042-2
• Klausmeyer, Steven. 2004. “Drag, Lift, and Moment Estimates of Transonic Aircraft Using the Navier-Stokes Equations.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-553
• Klein, V. 1983. A Review of System Identification Methods Applied to Aircraft. Joint Inst. for Acoustics and Flight Sciences. https://ntrs.nasa.gov/citations/19830025630
• Klein, Vladislav. 1989. “On Parameter Estimation of Highly Augmented Aircraft.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3356
• Klein, Vladislav. 1990. “Optimal Input Design for Aircraft Parameter Estimation Using Dynamicprogramming Principles.” In 17th Atmospheric Flight Mechanics Conference. AIAA 1990-2801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2801
• Klein, Vladislav, and Patrick C. Murphy. 1999. “Aerodynamic Parameters of High Performance Aircraft Estimated from Wind Tunnel and Flight Test Data.” In System Identification for Integrated Aircraft Development and Flight Testing. https://ntrs.nasa.gov/citations/19990032465
• Klenke, Robert. 2006. Development of a Novel, Two-Processor Architecture for a Small UAV Autopilot System,. Defense Technical Information Center. https://doi.org/10.21236/ada455450
• Klestadt, B. 1971. A Stellar Tracking Reference System. NASA-CR-126260. NASA. https://ntrs.nasa.gov/citations/19720012067
• Klinar, Walter J., and Henry A. Lee. 1955. Supplementary Investigation in the Langley Free-Spinning Tunnel of a 1/20-Scale Model of the Douglas XF4D-1 Airplane Including Spin-Recovery Parachute Tests of the Model Loaded to Simulate the Douglas F5D-1 Airplane. Rept-5269. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030045
• Kline, Paul, and Frank Vangraas. 1990. “Integrated Inertial/gps.” In NASA, Langley Research Center, Joint University Program for Air Transportation Research, 1989-1990. https://ntrs.nasa.gov/citations/19910009719
• Kling, Thomas. 1989. “Separation of Gravitational and Inertial Accelerations with a Combined Inertial Navigation and Gravity-Gradiometer System.” In High Precision Navigation. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-74585-0_39
• Klipa, A. M. 2012. “Estimation Procedure of Sensor Biases on the Basis of Flight Test Data.” Problems of Informatization and Management 3 (39). https://doi.org/10.18372/2073-4751.3.7189
• Klock, Ryan, and Carlos E. Cesnik. 2014. “Aerothermoelastic Simulation of Air-Breathing Hypersonic Vehicles.” In 55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2014-0149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0149
• Klock, Ryan, and Carlos E. Cesnik. 2015. “Aerothermoelastic Reduced-Order Model of a Hypersonic Vehicle.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-2711. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2711
• Klopfer, G. H. 1985. High Mach Number Predictive Methods for Missile Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada158358
• Kluever, Craig, and Kenneth Horneman. 2005. “Terminal Trajectory Planning and Optimization for an Unpowered Reusable Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6058
• Kluever, Craig, Kenneth Horneman, and John Schierman. 2009. “Rapid Terminal-Trajectory Planner for an Unpowered Reusable Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5766
• Kluge, Karl C., Alberto Lacaze, Zachary La Celle, Steven A. Legowik, Karl N. Murphy, and R. Thomson. 2013. “Toris: A System for Smooth Ground Vehicle Teleoperation in High Latency Conditions.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2024-01-3434
• Klumpp, Allan. 1966. “A Manually Retargeted Automatic Descent and Landing System for Lem.” In Guidance and Control Conference. AIAA 1966-1863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1863
• Klumpp, A. R. 1967. A Manually Retargeted Automatic Descent and Landing System for LM.. NASA. https://ntrs.nasa.gov/citations/19670060447
• Klumpp, A. R. 1968. A Manually Retargeted Automatic Landing System for Lunar Module (LM). NASA. https://ntrs.nasa.gov/citations/19680037529
• Klunker, E. Bernard, and H. Reese Ivey. 1949. An Analysis of Supersonic Aerodynamic Heating with Continuous Fluid Injection. NACA-TN-1987. NASA. https://ntrs.nasa.gov/citations/19930082730
• Klunker, E. G., and H. Reese Ivey. 1950. An Analysis of Supersonic Aerodynamic Heating with Continuous Fluid Injection. NACA-TR-990. NASA. https://ntrs.nasa.gov/citations/19930092049
• Knapp, Warren S. 1979. Summary of Communication and Navigation Systems Degradation in a Nuclear Environment. Defense Technical Information Center. https://doi.org/10.21236/ada196802
• Knapp, Matt. 1999. “Mission Optimization for a Reusable Launch Vehicle System.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4932
• Knickmeyer, Ernst H., and Elfriede T. Knickmeyer. 1991. “Basic Geometric Considerations for a Self-Calibration of Strapdown Inertial Sensor Blocks by Tumbles.” In International Association of Geodesy Symposia. Springer New York. https://doi.org/10.1007/978-1-4612-3102-8_10
• Knickmeyer, Elfriede, and Klaus-Peter Schwarz. 1989. “Error Characteristics of Inertial Systems from the Viewpoint of Oscillation Theory.” In High Precision Navigation. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-74585-0_7
• Knight, Jarrad M., Jordan Kildare, Fabian Zander, Yee Wei Law, and Michael J. Evans. 2026. “Characterisation of Wake-Region Optical Emissions from an Ablative Hypersonic Glide Vehicle.” In AIAA SCITECH 2026 Forum. AIAA 2026-2509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2509
• Knill, Duane, Anthony Giunta, Chuck Baker, et al. 1998. “HSCT Configuration Design Using Response Surface Approximations of Supersonic Euler Aerodynamics.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-905
• Kniskern, Marc W. 1990. “Analysis of a Six-Component, Flow-through, Strain-Gage, Force Balance Used for Hypersonic Wind Tunnel Models with Scramjet Exhaust Flow Simulation.” PhD diss., North Carolina State Univ.. https://ntrs.nasa.gov/citations/19900012459
• Knobbe, Edward J., and Gerald N. Haas. 1997. Celestial Navigation. Wiley. https://doi.org/10.1002/9780470172704.ch12
• Knoblach, J. 1974. Terminal Homing Engineering Flight Test T7 and MT7 Missile Launch Transients Data Reduction and Summary. Defense Technical Information Center. https://doi.org/10.21236/ada003241
• Knowles, S. H., K. J. Johnston, and E. O. Hulburt. 1973. “Applications of Radio Interferometry to Navigation.” In NASA. Goddard Space Flight Center Proc. of the 5th Ann. NASA and DOD Precise Time and Time Interval Planning Meeting. https://ntrs.nasa.gov/citations/19750003207
• Knudsen, Sverre, and Kjell Bløtekjær. 1995. “Interferometric Fiber-Optic Gyroscope Performance Owing to Temperature-Induced Index Fluctuations in the Fiber: Effect on Bias Modulation.” Optics Letters 20 (12): 1432. https://doi.org/10.1364/ol.20.001432
• Knuth, Taylor, and Paul Groves. 2025. “Terrain-Based Parameter Optimization for Zero Velocity Update Inertial Navigation Solutions.” In European Navigation Conference 2024. MDPI. https://doi.org/10.3390/engproc2025088067
• Kobayashi, Jun. 2026. “Active Inertial Self-Calibration beyond Identifiability: Task-Compatible Excitation and Terminal Feasibility.” Preprint, . https://doi.org/10.2139/ssrn.7507404
• Kobayashi, Hiroaki, Shujiro Sawai, Hideyuki Taguchi, et al. 2008. “Hypersonic Turbojet Engine Design of a Balloon-Based Flight Testing Vehicle.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2620
• Kochendorfer, Fred D. 1953. Investigation at a Mach Number of 1.90 of a Diverter-Type Boundary-Layer Removal System for a Scoop Inlet. NACA-RM-E53D07. NASA. https://ntrs.nasa.gov/citations/19930087800
• Koenig, R. W. 1967. Inlet Sensitivity Study for a Supersonic Transport. NASA-TN-D-3881. NASA. https://ntrs.nasa.gov/citations/19670010560
• Koh, Jun X., and Aditya A. Paranjape. 2020. “Comparative Study of Sensor Combinations for Autonomous Landing of Fixed-Wing Unmanned Aircraft.” In AIAA Scitech 2020 Forum. AIAA 2020-1086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1086
• Koh, YeonWan, HeungWon Park, and Byoung Yoon Kim. 2026. “Fiber-Optic Gyroscope Activities in Korea’s Defense and Civilian Applications: Insights from FIBERPRO.” In Fiber Optic Gyros: 50th Anniversary Conference, edited by Eric Udd, Herve C. Lefevre, Glen A. Sanders. SPIE. https://doi.org/10.1117/12.3094435
• Kohel, James M., Nan Yu, James R. Kellogg, Robert J. Thompson, David C. Aveline, and Lute Maleki. 2006. Quantum Gravity Gradiometer Development for Space. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/20060050289
• Kohrs, Richard, and Richard Petersen. 1998. “Development of the K-1 Two-Stage, Fully Reusable Launch Vehicle.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1540
• Koifman, M., I. Bar-Itzhack, and S. Merhav. 1995. “Dynamics-Aided Inertial Navigation System.” In Guidance, Navigation, and Control Conference. AIAA 1995-3195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3195
• Kolbas, Yu Yu, M. E. Grushin, and V. N. Gorshkov. 2018. “The Nonmagnetic Component of the Zero Bias of a Zeeman Laser Gyroscope.” Quantum Electronics 48 (3): 283–89. https://doi.org/10.1070/qel16509
• Kolbas, Yu. Yu., Ya. S. Pyatnitskii, M. I. Rodionov, and I. I. Saveliev. 2022. “Output Characteristic of Four-Frequency Zeeman Laser Gyroscope with an Alternating Frequency Bias.” Quantum Electronics 52 (2): 202–6. https://doi.org/10.1070/qel17991
• Kolbas, Yu Yu, I. I. Saveliev, and N. I. Khokhlov. 2015. “Effect of External and Internal Magnetic Fields on the Bias Stability in a Zeeman Laser Gyroscope.” Quantum Electronics 45 (6): 573–81. https://doi.org/10.1070/qe2015v045n06abeh015538
• Koller, Tom Lucas, Tim Laue, and Udo Frese. 2019. “State Observability through Prior Knowledge: A Conceptional Paradigm in Inertial Sensing.” In International Conference on Informatics in Control, Automation and Robotics (ICINCO). https://doi.org/10.5220/0007952307810788
• Kollodge, J. C., M. W. Hubbard, S. Jain, and C. A. Schons. 1981. Breadboard Stellar Tracker System Test Report, Volume 1. NASA-CR-161953. NASA. https://ntrs.nasa.gov/citations/19820008297
• Kollodge, J. C., and J. A. Sand. 1983. “An Advanced Star Tracker Design Using the Charge Injection Device.” In Automatic Control in Space 1982. Elsevier. https://doi.org/10.1016/b978-0-08-029328-8.50038-4
• Komar, D., and R. Christenson. 1996. “Reusable Launch Vehicle Engine Systems Operations Analysis.” In Space Programs and Technologies Conference. AIAA 1996-4246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4246
• Komarov, Bohdan, and Dmytro Zinchenko. 2023. “The Aerodynamic Behavioral Study of Canard Plane with Fan Wing Configuration.” Mechanics of Gyroscopic Systems, no. 45: 118–35. https://doi.org/10.20535/0203-3771452023290873
• Komatsu, Yutaka, Shinji Suzuki, and Kazuya Masui. 2003. “Development of Semi-Automatic Emergency Landing System for Aircraft.” Proceedings of the Transportation and Logistics Conference 2003.12 (0): 207–10. https://doi.org/10.1299/jsmetld.2003.12.207
• Kondrashkin, Georgy, Albert Bolotnov, and Mikhail Shkatov. 2025. “Algorithmic Method to Determine the Star Sensor Basis in Stellar-Inertial Navigation System Basis.” Telecommunications and Comunications, no. 5. https://doi.org/10.21681/3034-4050-2025-5-55-66
• Kong, Jeffrey. 1994. “The Accuracy of Parameter Estimation in System Identification of Noisy Aircraft Load Measurement.” PhD diss., California Univ.. https://ntrs.nasa.gov/citations/19950012715
• Kong, E. H., Jr., and W. H. Schuck. 1966. Analytical and Experimental Investigations into Problems Associated with Gyro-Stabilized Platform-Mounted Optical Sensing Elements Final Summary Report. NASA-CR-77502. NASA. https://ntrs.nasa.gov/citations/19660025948
• Konno, Akira, Kenji Kishimoto, and Masahiro Atsumi. 1998. “Investigation of Next Generation Engine for Reusable Launch Vehicle.” In AIP Conference Proceedings, vol. 420. AIP. https://doi.org/10.1063/1.54720
• Kopasakis, George, and Joseph Connolly. 2009. “Shock Positioning Controls Design for a Supersonic Inlet.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5117
• Kordes, E. E., and J. M. McKay. 1962. Landing Loads and Dynamics of the X-15 Airplane. NASA-TM-X-639. NASA. https://ntrs.nasa.gov/citations/19630002688
• Korger, Harold F. 1957. “Precision Celestial Navigation in High-Speed, High-Altitude Aircraft.” Navigation 5 (6): 311–22. https://doi.org/10.1002/j.2161-4296.1957.tb02430.x
• Korn, J. 1974. “The Effect of Inlet Distortion on the Performance and Stability of the Low-Speed Spool of a Turbofan Engine.” In 12th Aerospace Sciences Meeting. AIAA 1974-234. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-234
• Korst, H. H., and R. A. Deep. 1979. “Modeling of Plume Induced Interference Problems in Missile Aerodynamics.” In 17th Aerospace Sciences Meeting. AIAA 1979-362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-362
• Korsun, O. N., B. K. Poplavsky, A. V. Stulovskii, and Moung Htang Om. 2024. “Identification of Engine Thrust and Aerodynamic Drag Force According to Flight Test Data with Smoothing of Random Measurement Errors.” Teoriâ i sistemy upravleniâ, no. 3: 69–84. https://doi.org/10.31857/s0002338824030066
• Kortunov, V. I., I. Yu. Dybska, G. A. Proskura, and T. Trachsel. 2007. “Accuracy Analysis of Strapdown Inertial Navigation Systems.” Kosmìčna nauka ì tehnologìâ 13 (4): 40–48. https://doi.org/10.15407/knit2007.04.040
• Kostic, I., C. Mitrovic, D. Cvetkovic, and A. Bengin. 2002. “An Algorithm of Computation of Airfoil Drag in Lower Transonic Domain.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-545
• Kostyushin, Kirill, Anuar Kagenov, Ivan Eremin, Konstantin Zhiltsov, and Vladimir Shuvarikov. 2017. “Gas Flow Calculation Method of a Ramjet Engine.” In AIP Conference Proceedings, vol. 1899. Author(s). https://doi.org/10.1063/1.5009883
• Kothe, Hans-Henning, and Eberhard Hofer. 1988. “Analytical Techniques for Observability Analysis and Filter Design for Inertial Navigation Systems.” In Guidance, Navigation and Control Conference. AIAA 1988-4127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4127
• Kotob, S., and H. Kaufman. 1974. Digital System Identification and Its Application to Digital Flight Control. Rensselaer Polytechnic. https://ntrs.nasa.gov/citations/19740051018
• Kotob, S., and H. Kaufman. 1975. Minimum Variance System Identification with Application to Digital Adaptive Flight Control. Rensselaer Polytechnic Inst. https://ntrs.nasa.gov/citations/19760060695
• Kottas, Dimitrios, and Stergios Roumeliotis. 2013. “Exploiting Urban Scenes for Vision-Aided Inertial Navigation.” In Robotics: Science and Systems IX. Robotics: Science and Systems Foundation. https://doi.org/10.15607/rss.2013.ix.021
• Koubek, F. J. 1963. High Temperature Resistant Materials for Missile Propulsion Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0408362
• Kouyoumjian, W. L. 1957. Preliminary Wind-Tunnel Investigation of the Performance of Republic F-105 Wing-Root Inlet Configurations at Various Angles of Attack and a Mach Number of 2.01. NACA-RM-SL56L12. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19660082192
• Kowalczyk, Adam, and Rafał Chorzępa. 2020. “Processing Accuracy of Instantaneous Values of a Stochastic Signal in an Inertial Measurement System.” Measurement Science Review 20 (4): 157–61. https://doi.org/10.2478/msr-2020-0019
• Kowalski, Mirosław, and Ryszard Szczepanik. 2014. “Studies on Unsteady Operation of a Turbojet Engine and an Intake Channel of a Supersonic Aircraft.” Journal of KONES Powertrain and Transport 21 (2): 143–51. https://doi.org/10.5604/12314005.1133888
• Kozina, John S. 1976. C-141 All Weather Landing System Engineering Support. Defense Technical Information Center. https://doi.org/10.21236/ada029467
• Koziol, J. S., Jr., P. S. Rempfer, and L. E. Stevenson. 1971. An Evaluation of Low-Visibility Landing Systems by Simulation. NASA. https://ntrs.nasa.gov/citations/19710037726
• Krabacher, William E. 1993. “Aircraft Landing Gear Dynamics Present and Future.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/931400
• Krabacher, William E. 1996b. “The Experimental Measurement of the T-46 Nose Landing Gear Shimmy Parameters.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/961313
• Kraft, David C., Henry Luming, and J. R. Hoppenjans. 1971. Multiwheel Landing Gear-Soils Interaction and Flotation Criteria: Phase 3, Part 1. Defense Technical Information Center. https://doi.org/10.21236/ad0885275
• Kraiko, A. N. 2023. “On “New Methodologies of Processing” of Results Calculated for Rotating Detonation Engines and of Results of Force Measurements for Ramjet Models Tested in Supersonic Test Benches.” Thermophysics and Aeromechanics 29 (6): 809–14. https://doi.org/10.1134/s0869864322060014
• Kraiko, A. N., and D. E. Pudovikov. 1998. “Thin Airfoils of Minimum Wave Drag with Given Chord, Longitudinal Section Area, and Lift.” Fluid Dynamics 33 (4): 594–97. https://doi.org/10.1007/bf02698225
• Krainsk, W., and N. Rosato. 2001. “Demonstration of a 1,000-Pound Capacity Parachute Retraction Soft Landing System.” In 16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2001-2049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2049
• Krainski, W., Jr., S. Kunz, W. Krainski Jr., and S. Kunz. 1997. “The Dynamics of a Parachute Retraction Soft Landing System.” In 14th Aerodynamic Decelerator Systems Technology Conference. AIAA 1997-1540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1540
• Kramer, Manuel. 1964. “Apollo Command Module and LEM Guidance and Navigation Systems.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/640632
• Krebs, J. N. 1976. “Advanced Supersonic Technology Study: Engine Program Summary. Supersonic Propulsion: 1971 to 1976.” In NASA Proc. of the SCAR Conf., Part 1. https://ntrs.nasa.gov/citations/19770011069
• Krebs, Richard P., and E. Clinton Wilcox. 1954. Analysis of the Turbojet for Propulsion of Supersonic Bombers. NACA-RM-E54A21. NASA. https://ntrs.nasa.gov/citations/19930088157
• Kreeger, Richard, and D. Landrum. 2003. “Spinning Tail Aerodynamics of a Low Cost Precision Guided Missile.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3935. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3935
• Kremeyer, Kevin. 2004. “Lines of Pulsed Energy for Supersonic/Hypersonic Drag Reduction: Generation and Implementation.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-984. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-984
• Kremeyer, Kevin, and Andrew V. Pakhomov. 2008. “Lines of Energy Deposition for Supersonic∕Hypersonic Temperature∕Drag-Reduction and Vehicle Control.” In AIP Conference Proceedings, vol. 997. AIP. https://doi.org/10.1063/1.2931905
• Kretzschmar, Richard, Stephen Mallette, Raymond Deep, and Leslie Hall. 1995. “Aerodynamic Characteristics of Wrap around Fins on a Tube Launched Tactical Missile.” In 13th Applied Aerodynamics Conference. AIAA 1995-1897. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1897
• Krieger, R. 1979. “Aerodynamic Design Criteria for Supersonic Climb: Cruise Missiles.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1671. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1671
• Krieger, R. 1980. “A Technique for Developing Low Drag Nose Shapes for Advanced Supersonic Missile Concepts.” In 18th Aerospace Sciences Meeting. AIAA 1980-361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-361
• Krieger, R. 1982. “Supersonic Missile Aerodynamic and Performance Relationships for Lowobservables Mission Profiles.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1298. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1298
• Krieger, R., and J. Williams. 1981. “Accuracy Criteria for Evaluating Supersonic Missile Aerodynamic Coefficient Predictions.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1894
• Kriegsman, B. A. 1966. Radar-Updated Inertial Navigation of a Continuously-Powered Space Vehicle. NASA. https://ntrs.nasa.gov/citations/19660057931
• Kriegsman, Bernard A., William M. Stonestreet, and Duncan B. Cox Jr. 1977. Functional Requirements of the Interface between the NAVSTAR GPS Receiver Model X and the Advanced Inertial Reference Sphere. Volume II.. Defense Technical Information Center. https://doi.org/10.21236/ada057656
• Krishnan, G. L. Yadhu, and K. S. Sajikumar. 2023. “Modelling and Analysis of Vertical Landing Reusable Launch Vehicle with Spring Damper.” In AIP Conference Proceedings, vol. 2949. AIP Publishing. https://doi.org/10.1063/5.0157175
• Krivec, D. K., R. T. Ling, and J. Vadyak. 1984. “Investigation of Transonic Inlet Drag Characteristics.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/841539
• Krogmann, Uwe. 1988. “Optimal Integration of Inertial Sensor Functions for Flight-Control and Avionics.” In Digital Avionics Systems Conference. AIAA 1988-3878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-3878
• Kublanova, I. L., V. A. Shulepov, and A. V. Kulikov. 2021. “Study of an Interferometric Fiber-Optic Gyroscope with a Birefringence Modulator.” Gyroscopy and Navigation 12 (4): 363–69. https://doi.org/10.1134/s2075108721040052
• KÜChemann, D. 1962. “Aircraft Shapes and Their Aerodynamics for Flight at Supersonic Speeds.” In Advances in Aeronautical Sciences. Elsevier. https://doi.org/10.1016/b978-0-08-006550-2.50019-3
• Kudriashov, V. Ye., M. I. Rozhkov, A. Yu. Tkachenko, and Yu. P. Chervonyak. 2018. “Conditional Probability of Hitting Anti-Aircraft Missile System by Anti-Radar-Guided Missile.” Radiotekhnika, no. 192: 34–40. https://doi.org/10.30837/rt.2018.1.192.05
• Kudva, P., and A. Throckmorton. 1993. “EOS Attitude Determination and Next Generation Star Tracker Enhancements.” In AIAA. https://ntrs.nasa.gov/citations/19930046923
• Kügler, Martin E., Julian Rhein, and Florian Holzapfel. 2019. “Timely Flare Initiation during Automatic Landing – a Model Checking Application Example.” In AIAA Scitech 2019 Forum. AIAA 2019-0505. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0505
• Kuhar, Miran, Marta Okorn, and Bojan Stopar. 2010. “Determination of Deflection of the Vertical from Geoid Heights.” Geodetski vestnik 54 (04): 595–605. https://doi.org/10.15292/geodetski-vestnik.2010.04.595-605
• Kuhn, Richard E. 1959. Semiempirical Procedure for Estimating Lift and Drag Characteristics of Propeller-Wing-Flap Configurations for Vertical-and Short-Take-Off-and-Landing Airplanes. NASA-MEMO-1-16-59L. NASA. https://ntrs.nasa.gov/citations/19980232082
• Kuhn, Elizabeth, Connor Furlong, Tymoteusz Czerwiec, and Noah Reynolds. 2026. “Multi-Phase Fuel Injector for a Turbojet Engine.” In 2026 Regional Student Conferences. AIAA 2026-115638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-115638
• Kuipers, Matthew, Majdedin Mirmirani, Petros Ioannou, and Ying Huo. 2007. “Adaptive Control of an Aeroelastic Airbreathing Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6326
• Kulakova, V. I. 2018. “Method of Experimental Verification of Accuracy of UAV Antenna Phase Center Motion Parameters Determined by Navigation System.” Gyroscopy and Navigation 9 (4): 334–43. https://doi.org/10.1134/s2075108718040120
• Kulfan, R. 1978. “Application of Hypersonic Favorable Aerodynamic Interference Concepts to Supersonic Aircraft.” In Aircraft Systems and Technology Conference. AIAA 1978-1458. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1458
• Kulfan, Brenda. 2002. “Reynolds Numbers Considerations for Supersonic Flight.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2839
• Kulfan, Brenda. 2008. “New Supersonic Wing Far Far-Field Composite Element Wave Drag Optimization Method ‘FCE’.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-132
• Kulhánek, Robert. 2019. “Identification of a Degradation of Aerodynamic Characteristics of a Paraglider Due to Its Flexibility from Flight Test.” Aircraft Engineering and Aerospace Technology 91 (6): 873–79. https://doi.org/10.1108/aeat-06-2018-0162
• Kumar, Er. Arun. 2026a. “Adaptive AI-Based Scene-Aided Navigation for Robust Airborne Visual Localisation in GNSS-Denied Environments.” Preprint, . https://doi.org/10.2139/ssrn.7527864
• Kumar, Er. Arun. 2026b. “Detailed Architecture and Research Methodology for Terrain Aided Navigation Using Digital Elevation Maps and Machine Learning.” Preprint, . https://doi.org/10.2139/ssrn.7527841
• Kumar, R., and A. K. Ghosh. 2011. “Parameter Estimation Using Unsteady Downwash Model from Real Flight Data of Hansa-3 Aircraft.” Aeronautical Journal 115 (1171): 577–88. https://doi.org/10.1017/s0001924000006217
• Kumar, Ajit, and Ajoy K. Ghosh. 2018. “Data-Driven Method Based Aerodynamic Parameter Estimation from Flight Data.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0768
• Kumar, Ajit, and A. K. Ghosh. 2023. “Regularization Regression Methods for Aerodynamic Parameter Estimation from Flight Data.” Aircraft Engineering and Aerospace Technology 95 (5): 820–30. https://doi.org/10.1108/aeat-09-2019-0179
• Kumar, Rakesh, A. K. Ghosh, and Ajay Misra. 2013. “Parameter Estimation from Flight Data of Hansa-3 Aircraft Using Quasi-Steady Stall Modeling.” Journal of Aerospace Engineering 26 (3): 544–54. https://doi.org/10.1061/(asce)as.1943-5525.0000155
• Kumar, Kamlesh, Ch. Hima Gireesh, and V. Manohar. 2025. “Analysis of Aerodynamics of a Missile Using Ansys Fluent Software.” International Journal of Research Publication and Reviews 6 (8): 3441–51. https://doi.org/10.55248/gengpi.6.0825.3063
• Kumar, Neeraj, and Vinay Anand Yadav. 2022. “Preliminary Design of a Ramjet Engine: An Analytical Approach.” International Journal of Analytical, Experimental and Finite Element Analysis (IJAEFEA) 9 (3). https://doi.org/10.26706/jtfs.3.2.20220901
• Kumazaki, Taichi, and Kohei Shimamura. 2026. “Multi-Objective Aerodynamics Design of Supersonic Inlet for Laser Propulsion.” In AIAA SCITECH 2026 Forum. AIAA 2026-1104. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1104
• Kumm, E. L., and D. Bitondo. 1953. Preliminary Design Studies of a Turbo-Ramjet Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0025105
• Kuo, C.-Y., and Y.-C. Chiou. 2000. “Geometric Analysis of Missile Guidance Command.” IEE Proceedings - Control Theory and Applications 147 (2): 205–11. https://doi.org/10.1049/ip-cta:20000294
• Kurbatov, A. M., R. A. Kurbatov, and A. M. Goryachkin. 2019. “Fiber-Optic Gyroscope Accuracy Improvement by Suppressing the Parasitic Effects in Integrated Optic Phase Modulators.” Gyroscopy and Navigation 10 (4): 256–67. https://doi.org/10.1134/s2075108719040114
• Kurnaz, Sefer, Omer Cetin, and Okyay Kaynak. n.d. “Fuzzy Logic Based Approach to Design of Flight Control and Navigation Tasks for Autonomous Unmanned Aerial Vehicles.” In Unmanned Aircraft Systems. Springer Netherlands. https://doi.org/10.1007/978-1-4020-9137-7_13
• Kuroda, Shinichi. 1993. “Numerical Simulation of Supersonic Flow around Space Plane for Airframe-Engine Integration.” In 31st Aerospace Sciences Meeting. AIAA 1993-886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-886
• Kuroda, Shinichi, and Kozo Fujii. 1991. “Supersonic Inlet Flow Computations Using Fortified Navier-Stokes Approach.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1730
• Kuroda, Takeshi, and Fumiaki Imado. 1988. “Advanced Missile Guidance System against Very High Speed Target.” In Guidance, Navigation and Control Conference. AIAA 1988-4092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4092
• Kuroda, Takeshi, Fumiaki Imado, and Akira Ichikawa. 1993. “Active Missile Guidance against Very Low-Altitude Targets.” In Guidance, Navigation and Control Conference. AIAA 1993-3783. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3783
• Kurten, P. M. 1975. Apollo Experience Report Guidance and Control Systems: Lunar Module Abort Guidance System. NASA-TN-D-7990. NASA. https://ntrs.nasa.gov/citations/19750018954
• Kurth, Guido, and Christoph Bauer. 2015. “Air Intake Development for a Mach 5+ Throttleable Ducted Rocket Propelled Lower Tier Interceptor.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-4233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4233
• Kurzke, Joachim. 2006. “Effects of Inlet Flow Distortion on the Performance of Aircraft Gas Turbines.” In Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs. ASMEDC. https://doi.org/10.1115/gt2006-90419
• Kurzke, Joachim, and Ian Halliwell. 2018. “Inlet Flow Distortion.” In Propulsion and Power. Springer International Publishing. https://doi.org/10.1007/978-3-319-75979-1_6
• Kusunose, Kazuhiro, James Crowder, and Robert Watzlavick. 1999. “Wave Drag Extraction from Profile Drag Based on a Wake-Integral Method.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-275
• Kutluay, Umit, Gokmen Mahmutyazicioglu, and Bulent Platin. 2009. “An Application of Equation Error Method to Aerodynamic Model Identification and Parameter Estimation of a Gliding Flight Vehicle.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5724
• Kuzin, Anatoly, Sergey Lozin, Pavel Lechov, and Alexander Semenov. 2009. “Reusable Launch Vehicle Systems: Khrunichev Space Center’s Feasibility Studies.” In AIAA SPACE 2009 Conference & Exposition. AIAA 2009-6732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6732
• Kuznetsov, A. G., A. V. Molchanov, M. V. Chirkin, and E. A. Izmailov. 2015. “Precise Laser Gyroscope for Autonomous Inertial Navigation.” Quantum Electronics 45 (1): 78–88. https://doi.org/10.1070/qe2015v045n01abeh015420
• Kuznetsov, A. G., B. I. Portnov, and E. A. Izmailov. 2014. “Two Classes of Aircraft Strapdown Inertial Navigation Systems on Laser Gyros: Development and Test Results.” Gyroscopy and Navigation 5 (4): 187–94. https://doi.org/10.1134/s2075108714040087
• Kwak, JunYoung, Wooram Hong, Sang Joon Shin, Il Lee, JuSok Yi, and Chongam Kim. 2012. “Transient Time Aeroelastic Analysis for a Supersonic Flight Vehicle with a Ramjet Engine.” In 42nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2012-3271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3271
• Kwak, JunYoung, Wooram Hong, SangJoon Shin, Il Lee, JinWoo Yim, and Chongam Kim. 2010. “Static Aeroelastic Analysis of a Supersonic Flight Vehicle with a Ramjet Engine.” In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th. AIAA 2010-2636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-2636
• Kwak, Einkeun, and Seungsoo Lee. 2011. “Convergence Study of Inlet Buzz Frequency with Computational Parameters.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3362
• Kwak, Einkeun, and Seungsoo Lee. 2013a. “Numerical Study of the Effect of Exit Configurations on Supersonic Inlet Buzz.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3025. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3025
• Kwak, E., and S. Lee. 2013b. “Supersonic Inlet Buzz Control Using Corrected Bleed Model.” Journal of computational fluids engineering 18 (4): 82–89. https://doi.org/10.6112/kscfe.2013.18.4.082
• Kwak, E., N. Lee, H. Gong, and S. Lee. 2013b. “Numerical Simulations of Low- and High-Frequency Buzz around an Axisymmetric Supersonic Inlet.” Journal of computational fluids engineering 18 (2): 78–84. https://doi.org/10.6112/kscfe.2013.18.2.078
• Kwak, Dong-Youn, Keisuke Ohira, Michele Gaffuri, and Joel Brezillon. 2013a. “CFD Validation for the Supersonic Transport Configuration at Low-Speed and High Alpha Flight Condition.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-3030. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3030
• Kwiek, Agnieszka, Krzysztof Bogdański, Jarosław Hajduk, and Andrzej Tarnowski. 2022. “Technique Used to Perform Rocket-Plane Free-Flight Tests.” Transactions on Aerospace Research 2022 (3): 74–90. https://doi.org/10.2478/tar-2022-0018
• Kwon, Jay Hyoun, and Christopher Jekeli. 2005. “Gravity Requirements for Compensation of Ultra-Precise Inertial Navigation.” Journal of Navigation 58 (3): 479–92. https://doi.org/10.1017/s0373463305003395
• La, H. C., H. G. Bock, and J. P. Schlöder. 2017. “Structure of Optimal Samples in Continuous Nonlinear Experimental Design for Parameter Estimation.” In Modeling, Simulation and Optimization of Complex Processes HPSC 2015. Springer International Publishing. https://doi.org/10.1007/978-3-319-67168-0_7
• La Vaglia, A. 1969. Bendix OAO Star Tracker Program Final Report, 1962: 1969. NASA-CR-106095. NASA. https://ntrs.nasa.gov/citations/19690030373
• Lacerda Montes, Pedro, Vinicius Alves, and Guilherme Luis Takahashi de Carvalho. 2025. “Parametric Study of an Experimental Rocket’s Drag in Transonic Flow.” In Proceedings of the 27th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2023.cob2023-1895
• Lacey, David W. 1979. Aerodynamic Characteristics of the Close-Coupled Canard as Applied to Low-to-Moderate Swept Wings. Volume 3. Transonic-Supersonic Speed Regime. Defense Technical Information Center. https://doi.org/10.21236/ada085065
• Ladd, John, and William Norby. 1998. “Dynamic Inlet Distortion Predictions Using a CFD/distortion Synthesis Approach.” In 16th AIAA Applied Aerodynamics Conference. AIAA 1998-2735. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2735
• Ladeinde, Foluso. 2022. “The Theory of Supersonic Combustion Turbulence in the Rotating Detonation Engine.” In AIAA AVIATION 2022 Forum. AIAA 2022-4036. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4036
• Ladyzhenskij, M. D. 1963. The Hypersonic Area Rule. Defense Technical Information Center. https://doi.org/10.21236/ad0295787
• Lai, Yu Wang, De Feng Gu, Jun Hong Liu, Wen Ping Li, and Dong Yun Yi. 2014a. “Attitude Measurement Low Frequency Error Identification and Compensation for Star Tracker with Gyros.” Applied Mechanics and Materials 664: 298–303. https://doi.org/10.4028/www.scientific.net/amm.664.298
• Lai, Jizhou, Pin Lyu, Jianye Liu, and Bin Jiang. 2012. “Noncommutativity Error Analysis of Strapdown Inertial Navigation System under the Vibration in UAVs.” International Journal of Advanced Robotic Systems 9 (4). https://doi.org/10.5772/52758
• Lam, Vincent. 2005. “Time-to-Go Estimate for Missile Guidance.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6459. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6459
• Lam, Quang, Teresa Hunt, Paul Sanneman, and Stanley Underwood. 2003. “Analysis and Design of a Fifteen State Stellar Inertial Attitude Determination System.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5483. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5483
• Lamb, Mark. 1999. “Wind Tunnel Investigations of the AGM-130 Turbojet-Powered Configurations.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4257. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4257
• Lamb, Mark, and William Marx. 1999. “Development of the AGM-130 Turbojet-Powered Missile System.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4017
• Lamb, M., W. C. Sawyer, and J. L. Thomas. 1981. Experimental and Theoretical Supersonic Lateral-Directional Stability Characteristics of a Simplified Wing-Body Configuration with a Series of Vertical-Tail Arrangements. NASA-TP-1878. NASA. https://ntrs.nasa.gov/citations/19810020557
• Lambert, H. C., S. R. Vogel, A. S. Brewster, and K. Dunn. 2009. Validating the Modeling and Simulation of a Generic Tracking Radar. Defense Technical Information Center. https://doi.org/10.21236/ada502982
• Lambregts, A. 1982. “Avoiding the Pitfalls in Automatic Landing Control System Design.” In Guidance and Control Conference. AIAA 1982-1599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1599
• Lambregts, A., and J. Creedon. 1980. “Development and Flight Evaluation of Automatic Flare Laws with Improved Touchdown Dispersion.” In Guidance and Control Conference. AIAA 1980-1757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1757
• Lamont, G. 1973. “Digital Control of a Pneumatic Isolation System for Inertial Instrument Testing.” In Guidance and Control Conference. AIAA 1973-830. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-830
• Lamorte, Nicolas, and Peretz P. Friedmann. 2013. “Aerothermoelastic and Aeroelastic Studies of Hypersonic Vehicles Using CFD.” In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2013-1591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1591
• Lana, J. D. 1974. Apollo Telescope Mount (ATM) Gimballed Star Tracker. NASA-CR-120439. NASA. https://ntrs.nasa.gov/citations/19740024781
• Lance, G. N. 1954. “The Delta Wing in a Non-Uniform Supersonic Stream.” Aeronautical Quarterly 5 (1): 55–72. https://doi.org/10.1017/s0001925900001086
• Landau, Z., and M. Yeneriz. 1965. “Parametric Supersonic Combustion Ramjet Engine Optimization.” In 2nd Annual Meeting. AIAA 1965-446. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-446
• Landers, Michael, and Lamar Auman. 2001. “Experimental Investigation of Nose-Mounted Controls for a Hypersonic Missile.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-2433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2433
• Landers, Michael, Les Hall, and Lamar Auman. 2000. “Aerodynamic Predictions of Pitch and Roll Control for Canard-Controlled Missiles.” In 18th Applied Aerodynamics Conference. AIAA 2000-4516. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4516
• Landers, Michael, Les Hall, Lamar Auman, and Milton Vaughn. 2003. “Deflectable Nose and Canard Controls for a Fin-Stabilized Projectile at Supersonic and Hypersonic Speeds.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3805
• Landers, Michael, D. Landrum, Michael Landers, and D. Landrum. 1997. “Prediction of Hinge Moment Coefficients for Nose-Mounted Canard Controls at Supersonic Speeds.” In 15th Applied Aerodynamics Conference. AIAA 1997-2248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2248
• Landherr, Stefan F., and Mark H. Klein. 1987. Inertial Navigation System Simulator: Behavioral Specification. Defense Technical Information Center. https://doi.org/10.21236/ada200604
• Landherr, Stefan F., and Mark H. Klein. 1989. Inertial Navigation System Simulator: Behavioral Specification. Revision. Defense Technical Information Center. https://doi.org/10.21236/ada219294
• Landis. 2020b. “Navaho Missile Program, Part 2.” https://media.defense.gov/2020/May/18/2002302215/-1/-1/1/FLASHBACK_NAVAHO-PART%202.PDF
• Lange, William G. 1977. Development, Test, and Calibration of a Three-Axis Accelerometer System. Defense Technical Information Center. https://doi.org/10.21236/ada056711
• Lange, Gunter, Bernhard MoBbacher, and David Purll. 1986. “The ROSAT Star Tracker.” In SPIE Proceedings, vol. 0627, edited by David L. Crawford. SPIE. https://doi.org/10.1117/12.968097
• Lange, B., and B. Parkinson. 1965. “Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance.” In Thermophysics Specialist Conference. AIAA 1965-691. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-691
• Lange, Benjamin O., and Bradford W. Parkinson. 1966. “Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance.” In Progress in Astronautics and Rocketry. Elsevier. https://doi.org/10.1016/b978-1-4832-2729-0.50018-1
• Langford, R. C. 1965. Unconventional Inertial Sensors. AIAA PAPER 65-401. NASA. https://ntrs.nasa.gov/citations/19650046965
• Langford, R. C. 1966. Unconventional Inertial Sensors. NASA. https://ntrs.nasa.gov/citations/19670037788
• Langill, A., Jr. 1965. “Solid Rocket Motor Specific Impulse Correlation: Captive Test Data to Flight Test Results.” In Flight Testing Conference. AIAA 1965-205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-205
• Langley, Frank J., and John Demetrick. 1978. Modular Digital Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada072544
• Lanning, W. D., and F. T. Hung. 1971. Shuttle Ascent and Shock Impingement Aerodynamic Heating Studies. NASA-CR-123533. NASA. https://ntrs.nasa.gov/citations/19720011227
• Lardas, Mark N. 1989. “Shuttle Tethered Operations: The Effect on Orbital Trajectory and Inertial Navigation.” In NASA, Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1989. https://ntrs.nasa.gov/citations/19900004109
• Larin, V. B., and A. A. Tunik. 2012a. “Algorithms of Gyro-Free Accelerometer-Based Satellite-Inertial Navigation System.” Electronics and Control Systems 4 (34). https://doi.org/10.18372/1990-5548.34.5702
• Larsen, Charles. 2000. “Commercial Space Transportation Reusable Launch Vehicle Operations and Maintenance Considerations.” In Space 2000 Conference and Exposition. AIAA 2000-5114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5114
• Larsen, Charles. 2003. “Commercial Space Transportation Reusable Launch Vehicle Operations and Maintenance Developments.” In AIAA Space 2003 Conference & Exposition. AIAA 2003-6407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6407
• Larsen, Charles. 2005. “Development of Guide to Commercial Space Transportation Reusable Launch Vehicle Operations and Mainenance.” In Space 2005. AIAA 2005-6795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6795
• Larson, John W. 1959a. Advanced Nuclear Turbojet Powerplant Characteristics Summary for Supersonic Aircraft. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1245002
• Larson, John W. 1959b. Supplement 1: Advanced Nuclear Turbojet Powerplant Characteristics Summary for Supersonic Aircraft. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1245004
• Larson, P. 1965. “Titan Iii Inertial Guidance System.” In 2nd Annual Meeting. AIAA 1965-306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-306
• Larson, Gregory, and Bert Mount. 1986. “Eigenstructure Synthesis and Command Generator Tracking Applied to Oblique Wing. Flight Control.” In Guidance, Navigation and Control Conference. AIAA 1986-2245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2245
• “Laser-Driven Fiber-Optic Gyroscope.” 2025. Оптический журнал. https://doi.org/10.17586/1023-5086-2025-92-08-21-31
• Last, David. 1992. “The Accuracy and Coverage of Loran-C and of the Decca Navigator System — And the Fallacy of Fixed Errors.” Journal of Navigation 45 (1): 36–51. https://doi.org/10.1017/s0373463300010456
• Latham, R. W., and P. T. Richards. 1977. “A Multi-DME/Inertial System for Aircraft Positioning.” Navigation 24 (1): 72–83. https://doi.org/10.1002/j.2161-4296.1977.tb01268.x
• Laubendorfer, William, William Whitesell, and Charles Erast. 1965. “A Low-Cost Aircraft Inertial Navigation System: The Locating System 1.” In Guidance Control Conference. AIAA 1965-1210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1210
• Laumann, E. A. 1965. Comparisons of Experimental and Theoretical Aerodynamic Heating Results in Air-Carbon Dioxide Mixtures. NASA-CR-57215. NASA. https://ntrs.nasa.gov/citations/19650009669
• Lautier-Blisson, Jean. n.d. “Développement D’un Accéléromètre Atomique Compact Pour La Gravimétrie De Terrain Et La Navigation Inertielle.” PhD diss., Paris 6. https://doi.org/10.70675/cd486989z526dz43b4z9e3ez6ea4cb81ed75
• Lauziere, N., and D. Kump. 1958. Design and Test of Transpiration Air Cooled Turbine Blades in a Full Scale Turbojet Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0481394
• Lavan Kumar, Gundeti, Kiran Vunnam, Bruce Bouldin, and Yogi Sheoran. 2013. “Investigation of Plenum Inlet Distortion and Its Impact on Compressor Total Pressure and Swirl Distortion.” In Volume 2: Aircraft Engine; Coal, Biomass and Alternative Fuels; Cycle Innovations. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2013-94981
• Lawrence, R. 1991. “Advanced Missile Guidance.” In Navigation and Control Conference. AIAA 1991-2726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2726
• Lawrence, Anthony. 1993a. “The Dynamically Tuned Gyroscope.” In Modern Inertial Technology. Springer US. https://doi.org/10.1007/978-1-4684-0444-9_10
• Lawrence, Anthony. 1993b. “An Outline of Inertial Navigation.” In Modern Inertial Technology. Springer US. https://doi.org/10.1007/978-1-4684-0444-9_2
• Lawrence, Anthony. 1993c. “The Ring Laser Gyro.” In Modern Inertial Technology. Springer US. https://doi.org/10.1007/978-1-4684-0444-9_14
• Lawrence, Douglas, Joy Kelly, and Johnny Evers. 1998. “Gain Scheduled Missile Autopilot Design Using a Control Signal Interpolation Technique.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4418
• Lawton, John A., Robert J. Jesionowski, and Paul Zarchan. 1997. Comparison of Four Filtering Options for a Radar Tracking Problem,. Defense Technical Information Center. https://doi.org/10.21236/ada329021
• Le Ngoc, Luan, Clark Borst, Max Mulder, and Rene Van Paassen. 2010. “The Effect of Synthetic Vision Enhancements on Landing Flare Performance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8170
• Leavitt, L. D. 1979. Longitudinal Aerodynamic Characteristics of a Vectored-Engine-over-Wing Configuration at Subsonic Speeds. NASA-TP-1533. NASA. https://ntrs.nasa.gov/citations/19790024993
• Leavitt, L. D., P. D. Whitten, and S. C. Stumpfl. 1978. “Low Speed Aerodynamic Characteristics of a Vectored-Engine-over-Wing Configuration.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19780059678
• Lebsock, K., N. Gautier, P. Hacking, et al. 2000. Attitude Control System and Star Tracker Performance of the Wide-Field Infrared Explorer Spacecraft. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210003422
• Lecca, Paola. 2020. “Model Identifiability.” In SpringerBriefs in Statistics. Springer International Publishing. https://doi.org/10.1007/978-3-030-41255-5_3
• Lecca, Paola. 2024. “Model Identifiability.” In SpringerBriefs in Statistics. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-74748-9_3
• Leccadito, Matthew, Tim M. Bakker, Ruixin Niu, and Robert H. Klenke. 2015. “A Kalman Filter Based Attitude Heading Reference System Using a Low Cost Inertial Measurement Unit.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0604. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0604
• Lee, Chih-hsiao. n.d.-a. “Stochastic Control System Parameter Identifiability.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180816-4290
• Lee, Yongsik. n.d.-b. “A Study of Parametric Excitation Applied to a MEMS Tuning Fork Gyroscope.” PhD diss., University of Missouri–Columbia. https://doi.org/10.32469/10355/4697
• Lee, J. A. 1964a. “Aircraft Inertial Navigation: A Description of Gyroscopes and Accelerometers Suitable for Navigational Purposes, the Principles Involved in Inertial Navigation Round the Earth and the Combination of Doppler and Inertial Systems.” Aircraft Engineering and Aerospace Technology 36 (1): 2–9. https://doi.org/10.1108/eb033819
• Lee, Henry A. 1964b. Spin Tunnel Investigation of a 1/30 Scale Model of the North American a-5A Airplane. NASA-TM-SX-946. NASA. https://ntrs.nasa.gov/citations/19980236423
• Lee, C. E. 1969a. ATM Star Tracker Vehicle Structure Occultation Study. NASA-TM-X-53836. NASA. https://ntrs.nasa.gov/citations/19700031772
• Lee, R. W. 1969b. “A Review of Line-of-Sight Propagation Studies of the Small-Scale Structure of the Atmosphere.” Radio Science 4 (12): 1211–23. https://doi.org/10.1029/rs004i012p01211
• Lee, J. A. 1969c. “‘The Schuler Pendulum and Inertial Navigation‘.” Journal of Navigation 22 (2): 267–69. https://doi.org/10.1017/s0373463300025479
• Lee, C. E. 1971. Star Tracker for the Apollo Telescope Mount. NASA-TM-X-64622. NASA. https://ntrs.nasa.gov/citations/19720004930
• Lee, B. 1974. “An Integrated Inertial Reference: Inertial Navigation System.” In Mechanics and Control of Flight Conference. AIAA 1974-869. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-869
• Lee, B. 1976b. “Redundant Position Measurements from an Inertial Reference-Inertial Navigation System Mechanization.” In Guidance and Control Conference. AIAA 1976-1937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1937
• Lee, J. 1985. “Aerodynamic Parameter Identification of a Tactical Missile Utilizingpostflight Telemetry Data.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1768. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1768
• Lee, Abigail. 2025. “Star Tracker Algorithm Improvements to Restore Performance after Radiation Exposure.” In Small Satellites Systems and Services Symposium (4S 2024), edited by Max Petrozzi-Ilstad. SPIE. https://doi.org/10.1117/12.3061924
• Lee, Chang-Hyuck, Joongki Ahn, Hyo-Gil Bae, and Jang-Hyuk Kwon. 2010b. “Reliability Based Design Optimization for the Pressure Recovery of Supersonic Double-Wedge Inlet.” Journal of the Korean Society for Aeronautical & Space Sciences 38 (11): 1067–74. https://doi.org/10.5139/jksas.2010.38.11.1067
• Lee, Bongsul, and Juhyun Bae. 2023. “Numerical Study of an Integrated Combustor of Dual Mode Ramjet Equipped with an Ejector Rocket for Multiple Joined Combined Cycle.” Journal of the Korean Society of Propulsion Engineers 27 (4): 15. https://doi.org/10.6108/kspe.2023.27.4.015
• Lee, Jayden Dongwoo, Hyochoong Bang, Minseok Choi, et al. 2026b. “Federated Extended Kalman Filter Integrating Terrain-Referenced and Quantum Magnetometer–Aided Navigation for GNSS-Denied Environments.” In ION Pacific PNT. Institute of Navigation. https://doi.org/10.33012/2026.20639
• Lee, David G., and H. D. Davidson Jr. 1973. Low Speed Aerodynamic Characteristics of an a-4 Aircraft with an Air Cushion Landing System. Defense Technical Information Center. https://doi.org/10.21236/ad0761621
• Lee, H.-J., and I.-S. Jeung. 2009. “Experimental and Numerical Investigation on the Supersonic Inlet Buzz with Angle of Attack.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_51
• Lee, Younghwan, Hyeon Jin, Min-Gyu Kim, and Hyungrok Do. 2024b. “An Investigation of Internal Drag Correction Methodology for Wind Tunnel Test Data in a High-Speed Air-Breathing Vehicle Using Numerical Analysis.” International Journal of Aeronautical and Space Sciences 26 (3): 945–52. https://doi.org/10.1007/s42405-024-00836-z
• Lee, Jaewon, and Sang Hun Kang. 2019. “Numerical Study on the Start and Unstart Phenomena in a Scramjet Inlet-Isolator Model.” PLOS ONE 14 (11): e0224994. https://doi.org/10.1371/journal.pone.0224994
• Lee, Dong Eun, Young-Seok Kang, and Dong-Ho Rhee. 2025b. “Study on the Design and Performance Analysis of an Afterburner Diffuser for a Supersonic Micro Turbojet Engine.” KSFM Journal of Fluid Machinery 28 (1): 82–91. https://doi.org/10.5293/kfma.2025.28.1.082
• Lee, Dongjin, Youngjoo Kim, and Hyochoong Bang. 2014. “Vision-Aided Terrain Referenced Navigation for Unmanned Aerial Vehicles Using Ground Features.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228 (13): 2399–2413. https://doi.org/10.1177/0954410013517804
• Lee, Yu Dam, La Woo Kim, and Hyung Keun Lee. 2022. “A Tightly-Coupled Compressed-State Constraint Kalman Filter for Integrated Visual-Inertial-Global Navigation Satellite System Navigation in GNSS-Degraded Environments.” IET Radar, Sonar & Navigation 16 (8): 1344–63. https://doi.org/10.1049/rsn2.12265
• Lee, Seokwon, Youdan Kim, Gwanyoumg Moon, and Byung-Eul Jun. 2015a. “Missile Autopilot Design during Boost Phase Using Robust Backstepping Approach.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0860
• Lee, Ja Kyoung, Sang Boo Kim, Yun Gyu Park, and In Hwa Bae. 2024c. “Life Cycle Cost Estimation Method for Spare Parts Using Weapon System Hierarchy.” Journal of Korean Society for Quality Management 52 (2): 275–86. https://doi.org/10.7469/jksqm.2024.52.2.275
• Lee, Kyungjae, Bo-Hwa Lee, Sang-Hun Kang, et al. 2007b. “Development of Block Type Inlet Distortion Simulating Device for Gas Turbine Engine Inlet Distortion Test.” International Journal of Aeronautical and Space Sciences 8 (2): 121–25. https://doi.org/10.5139/ijass.2007.8.2.121
• Lee, Kyungjae, Bohwa Lee, Sanghun Kang, Sooseok Yang, and Daesung Lee. 2010a. “Inlet Distortion Test with Gas Turbine Engine in the Altitude Engine Test Facility.” In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2010-4337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4337
• Lee, Dong-Chan, and M. Nagati. 1999. “Improved Coupled Force and Moment Parameter Estimation for Aircraft.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4174. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4174
• Lee, Shinhak, Gerardo G. Ortiz, and James W. Alexander. 2005. “Pointing Knowledge Accuracy of the Star Tracker Based ATP System.” In SPIE Proceedings, vol. 5712, edited by G. Stephen Mecherle. SPIE. https://doi.org/10.1117/12.612037
• Lee, Man Hyung, Won Chul Park, Kil Soo Lee, et al. 2012a. “Observability Analysis Techniques on Inertial Navigation Systems.” Journal of System Design and Dynamics 6 (1): 28–44. https://doi.org/10.1299/jsdd.6.28
• Lee, Hohyeong, Junwoo Park, Hosun Lee, Seongheon Lee, Youngjae Kim, and Hyochoong Bang. 2026d. “Observability-Constrained Optical Flow-Inertial Navigation for Consistent State Estimation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20866
• Lee, Howard, Stephen Reiman, Charles Dillon, and Hussein Youssef. 2007c. “Robust Nonlinear Dynamic Inversion Control for a Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6685. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6685
• Lee, D. B., and C. B. Rumsey. 1959. Heat-Transfer Measurements on a Blunt Spherical-Segment Nose to a Mach Number of 15.1 and Flight Performance of the Rocket-Propelled Model to a Mach Number of 17.8. NASA-TM-X-77. NASA. https://ntrs.nasa.gov/citations/19650018847
• Lee, Tae–Gon, and Jee-Hwan Ryu. 2010. “A Study on the Teleoperation of the Unmanned Grounded Vehicle for Improving Telepresence.” Journal of Institute of Control Robotics and Systems 16 (6): 553–58. https://doi.org/10.5302/j.icros.2010.16.6.553
• Lee, Keum, and Sahjendra Singh. 2011. “Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6250
• Lee, Keum W., and Sahjendra N. Singh. 2026. “Nonlinear Longitudinal Autopilot Design for Robust Finite-Time Missile Control.” In AIAA SCITECH 2026 Forum. AIAA 2026-2163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2163
• Lee, H. C., and A. R. Swegle. 1963. Landing Gear Development. Defense Technical Information Center. https://doi.org/10.21236/ad0408930
• Lee Kingsley, Oliver. 1967. “Data Reduction Techniques and Missile Range Instrumentation.” In Advances in Space Science and Technology. Elsevier. https://doi.org/10.1016/b978-1-4831-9967-2.50010-3
• Lees, D. E. 1959. “Aerodynamic Influence Coefficients for Delta Wings in Steady Supersonic Flow: A Method of Numerical Integration Using Panels Bounded by Mach Lines.” Aircraft Engineering and Aerospace Technology 31 (1): 9–12. https://doi.org/10.1108/eb033067
• Lefevre, Hevré C. 1988. “The Fiber Optic Gyroscope: Another Optical Revolution in the Inertia Business.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1988.fbb1
• Léfèvre, H. C. 1989. “Evolution of the Fiber Optic Gyroscope.” In Springer Proceedings in Physics. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-75088-5_20
• Lefevre, Herve C. 1993. “Interferometric Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 10266. SPIE. https://doi.org/10.1117/12.145202
• Lefevre, Herve C. 1996. “Fundamentals of the Interferometric Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 2837, edited by Eric Udd, Herve C. Lefevre, Kazuo Hotate. SPIE. https://doi.org/10.1117/12.258167
• Lefèvre, Hérve C. 1996. “Fundamentals of the Interferometric Fiber-Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1996.tu3s1
• Lefèvre, H. C. 2012. “The Fiber-Optic Gyroscope: Achievement and Perspective.” Gyroscopy and Navigation 3 (4): 223–26. https://doi.org/10.1134/s2075108712040062
• Lefevre, Hervé C. 2012. “The Fiber-Optic Gyroscope: Actually Better than the Ring-Laser Gyroscope?” In SPIE Proceedings, vol. 8421, edited by Yanbiao Liao, Wei Jin, David D. Sampson, Ryozo Yamauchi, Youngjoo Chung, Kentaro Nakamura, Yunjiang Rao. SPIE. https://doi.org/10.1117/12.978920
• Lefevre, H. C., R. A. Bergh, and H. J. Shaw. 1982. “All-Fiber Gyroscope with Inertial-Navigation Short-Term Sensitivity.” Optics Letters 7 (9): 454. https://doi.org/10.1364/ol.7.000454
• Lefevre, H. C., S. Vatoux, M. Papuchon, and C. Puech. 1987. “Integrated Optics: A Practical Solution for the Fiber-Optic Gyroscope.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937545
• Lehman, August F. 1964. An Experimental Study of the Dynamic and Steady State Flow Disturbances Encountered by Aircraft during a Carrier Landing Approach. Defense Technical Information Center. https://doi.org/10.21236/ad0606886
• Lei, He, Xiaodong Yan, Yakun Shen, and Liu Liyang. 2017. “High-Altitude and Low-Speed Reentry Guidance for Suborbital Reusable Launch Vehicle Returning to Launch Site.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2256
• Leissler, L. A., and J. C. Nettles. 1954. Investigation of Adjustable Supersonic Inlet in Combination with J34 Engine up to Mach 2.0. NACA-RM-E54H11. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19630004111
• Lensi, Michael. 2000. “Estimating Open-Loop Stability and Control Derivatives for the Tu-144LL Supersonic Transport from Flight Data.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3901
• Lentsch, A., H. Taguchi, R. Shepperd, and M. Maita. 2001. “Vehicle Concepts for an Ejector Ramjet Combined Cycle Engine.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1793
• Leonard, P., and R. Rodier. 1966. “Design Integration Aspects of a Land Landing System for Apollo Applications.” In Aerodynamic Deceleration Systems Conference. AIAA 1966-1524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1524
• Leonov, S., D. Yarantsev, and F. Falempin. 2012. “Flow Control in a Supersonic Inlet Model by Electrical Discharge.” In Progress in Flight Physics. EDP Sciences. https://doi.org/10.1051/eucass/201203557
• Lesieutre, Daniel J. 2017. “Prediction of Sparrow Missile Aerodynamic Characteristics with a Nonlinear Engineering Level Missile Prediction Method.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3399
• Lesieutre, Daniel, John Love, and Marnix Dillenius. 1996. “High Angle of Attack Missile Aerodynamics Including Rotational Rates: Program M3HAX.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3392
• Lesnic, D. 2000. “Identifiability of Distributed Parameters in Beam-Type Systems.” jiip 8 (4): 379–97. https://doi.org/10.1515/jiip.2000.8.4.379
• Lestage, Richard. 2003. “Missile State Estimation from Telemetry Measurements.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5721
• Lestev, A. M., and M. V. Fedorov. 2012. “Vibration-Induced Error of a Pendulous MEMS Accelerometer.” Gyroscopy and Navigation 3 (1): 47–50. https://doi.org/10.1134/s2075108712010087
• Letchworth, Gary. 2011. “X-33 Reusable Launch Vehicle Demonstrator, Spaceport and Range.” In AIAA SPACE 2011 Conference & Exposition. AIAA 2011-7314. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-7314
• Letchworth, Janet, and Gary Letchworth. 2000. “Second Generation Reusable Launch Vehicle Servicing of the International Space Station.” In Space 2000 Conference and Exposition. AIAA 2000-5141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5141
• Leung, A. M. 2010. “Low-Cost Thermal Mems Gyroscope.” In 2010 Solid-State, Actuators, and Microsystems Workshop Technical Digest. Transducer Research Foundation. https://doi.org/10.31438/trf.hh2010.97
• Leve, R. M. 1974. “Psychological Effects in Celestial Navigation.” Navigation 21 (1): 83–87. https://doi.org/10.1002/j.2161-4296.1974.tb01201.x
• Levin, Jason, Petros Ioannou, and Maj Mirmirani. 2008. “Adaptive Mode Suppression Scheme for an Aeroelastic Airbreathing Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7137
• Levine, S., R. Dennis, and K. L. Bachman. 1990. “Strapdown Astro-Inertial Navigation Utilizing the Optical Wide-Angle Lens Startracker.” Navigation 37 (4): 347–62. https://doi.org/10.1002/j.2161-4296.1990.tb01561.x
• Levine, Paul, and Ronald E. Woods. 1981. North Pacific Omega Navigation System Validation. Defense Technical Information Center. https://doi.org/10.21236/ada121105
• Levinson, Sergei, Haim Weiss, and Joseph Z. Ben-Asher. 2002. “Trajectory Shaping and Terminal Guidance Using Linear Quadratic Differential Games.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4839
• Levitt, Larry J. 2001. Design of a Millimeter Wave Data Link for a Radar Guided Missile. Defense Technical Information Center. https://doi.org/10.21236/ada397366
• Levitt, B., R. McAdory, and G. Nearman. 1970. “Development and Evaluation of a Unique Low Cost Gimballed Inertial Guidance Platform.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1026
• Levy, L. L., and R. R. Dickey. 1955. “External-Store Drag Reduction at Transonic and Low Supersonic Mach Numbers by Application of Baldwin’s Moment-of-Area Rule.” In NACA Conf. on Aerodyn. of High Speed Aircraft. https://ntrs.nasa.gov/citations/19740075330
• Levy, Lionel L., Jr. 1959. Supersonic and Moment-of-Area Rules Combined for Rapid Zero-Lift Wave-Drag Calculations. NASA-MEMO-4-19-59A. NASA. https://ntrs.nasa.gov/citations/19980232076
• Levy, Lionel L., Jr., and Robert R. Dickey. 1956. External-Store Drag Reduction at Transonic and Low Supersonic Mach Numbers by Application of Baldwin’s Moment-of-Area Rule. NACA-RM-A55L14a. NASA. https://ntrs.nasa.gov/citations/19930089003
• Lewis, George N. 2017. “Ballistic Missile Defense Effectiveness.” In AIP Conference Proceedings. Author(s). https://doi.org/10.1063/1.5009222
• Lhachemi, Hugo, David Saussié, and Guchuan Zhu. 2016b. “Handling Hidden Coupling Terms in Gain-Scheduling Control Design: Application to a Pitch-Axis Missile Autopilot.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0365
• Li, Xiaopeng. 2010. “Interpolating Surface Gravity Data for Assessing the Accuracy of a Ground Inertial Navigation System/Global Positioning System Gravimetric System.” Journal of Surveying Engineering 136 (3): 139–46. https://doi.org/10.1061/(asce)su.1943-5428.0000025
• Li, Ying. 2013. “Mechanical Design on Finite Element Method for Ring Laser Gyroscope.” Applied Mechanics and Materials 421: 116–21. https://doi.org/10.4028/www.scientific.net/amm.421.116
• Li, Wu. 2015. “Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2581
• Li, Jia-xian. 2017. Design and Implementation of Automatic Landing Control System for UAV Based on GPS. https://doi.org/10.4108/eai.28-2-2017.152290
• Li, Jiafeng. 2026a. “Control-Theoretic Framework for Autonomous UAV Navigation in GNSS-Denied Environments via Adaptive Multi-Sensor Fusion.” Advances in Differential Equations and Control Processes. https://doi.org/10.59400/adecp4733
• Li, Anliang, Hong Cai, Shifeng Zhang, and Xibin Bai. 2013d. “Robust Stabilization Control for the Floated Sensor Inertial Platform.” Sensor Letters 11 (11): 2094–97. https://doi.org/10.1166/sl.2013.2970
• Li, Chan, Yuan Cao, and Shifeng Zhang. 2014d. “A Study on the Alignment of Platform INS Based on the Rotation around Azimuth Axis.” In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-44687-4_6
• Li, Tonghui, Heyu Chen, Hongmin Fu, et al. 2025e. “Integrated Optoelectronic Transceiver toward Navigation Grade Fiber Optic Gyroscope Using Silicon Photonics.” Optics Letters 50 (22): 7139. https://doi.org/10.1364/ol.576264
• Li, Changshu, Kaiting Chen, Wenyan Song, and Huijie Li. 2026h. “Reinforcement-Learning Enabled Speed Control for a Small Turbojet Engine.” Preprint, . https://doi.org/10.2139/ssrn.6631121
• Li, Chen, Jinbao Chen, Chen Wang, ZhiCheng Hu, Zihao Zhang, and Lihua Piao. 2026c. “Design and Aerodynamic Analysis of Multidimensional Combined Morphing for Supersonic Aircraft Forebody.” Aircraft Engineering and Aerospace Technology 98 (6–7): 863–75. https://doi.org/10.1108/aeat-09-2025-0332
• Li, Zhenwei, Yongmei Cheng, Huibin Wang, and Huaxia Wang. 2021d. “Fault Detection Approach Applied to Inertial Navigation System/air Data System Integrated Navigation System with Time-Offset.” IET Radar, Sonar & Navigation 15 (9): 945–56. https://doi.org/10.1049/rsn2.12092
• Li, Zhenwei, Yongmei Cheng, Xuhua Wu, Yachong Zhang, and Huaxia Wang. 2021a. “ALPF-GLRT Based Fault Detection Method for Small Faults Applied to Redundant IMUs.” Measurement Science and Technology 32 (12): 125101. https://doi.org/10.1088/1361-6501/ac1beb
• Li, Yu, Naigang Cui, and Siyuan Rong. 2009c. “Trajectory Optimization for Hypersonic Boost-Glide Missile Considering Aeroheating.” Aircraft Engineering and Aerospace Technology 81 (1): 3–13. https://doi.org/10.1108/00022660910926854
• Li, Bing, Jin Dong, Peng Xiao, and Qingtang Meng. 2021f. “Research on Locked Wheel Protection Function of Aircraft Brake System.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2021-01-1269
• Li, H. Y., and Q. T. Eri. 2007. “Numerical Simulation of Aerodynamic Heating Reduction Due to Opposing Jet in Supersonic Flow.” In New Trends in Fluid Mechanics Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-75995-9_90
• Li, E., and A. Fomichev. 2017. “Accuracy Analysis of Lunar Lander Terminal Guidance Algorithm.” Science and Education of the Bauman MSTU 17 (04): 113–28. https://doi.org/10.7463/0417.0000957
• Li, Zengke, Jingxiang Gao, and Jian Wang. 2016d. “Inertial Aided Cycle Slip Detection and Repair for PPP/INS Tightly Coupled Navigation.” Journal of Navigation 69 (6): 1357–78. https://doi.org/10.1017/s0373463316000023
• Li, Kui, Pengyu Gao, Xueyun Wang, and Lei Wang. 2016a. “Analysis and Experiment of Error Restraint Principle in an Inertial Navigation System with Inertial Sensors Rotation.” International Journal of Sensor Networks 21 (2): 127. https://doi.org/10.1504/ijsnet.2016.078188
• Li, Wenchao, Christopher Gilliam, Xuezhi Wang, Allison Kealy, Andrew D. Greentree, and Bill Moran. 2024d. “Gravity-Aided Navigation Using Viterbi Map Matching Algorithm.” Journal of Navigation 77 (3): 307–21. https://doi.org/10.1017/s0373463324000250
• Li, Zhen, Jinyun Guo, Cheinway Hwang, et al. 2025l. “Tailored Method for Optimizing Deflection of the Vertical Model Using Multidirectional Geoid Gradients from SWOT/KaRIn Observations.” Geophysical Journal International 244 (2): ggaf484. https://doi.org/10.1093/gji/ggaf484
• Li, Zhaoxiong, Shihao Han, Haodong Yan, et al. 2026l. “STARE: A Self-Calibrating Event-Based Star Tracker for Spacecraft Attitude Determination with Focal-Length Recovery.” Journal of Physics: Conference Series 3314 (1): 012006. https://doi.org/10.1088/1742-6596/3314/1/012006
• Li, Yuan, Jason Zheng Jiang, and Simon Neild. 2016f. “Optimisation of Shimmy Suppression Device in an Aircraft Main Landing Gear.” Journal of Physics: Conference Series 744: 012066. https://doi.org/10.1088/1742-6596/744/1/012066
• Li, Zhanke, Junfeng Jin, and Zheng Li. 2023d. “Modeling for Trajectory of Ballistic Missile Target Group.” Highlights in Science, Engineering and Technology 56: 527–34. https://doi.org/10.54097/hset.v56i.10789
• Li, Luo Gang, Wu Xing Jing, and Chang Gao. 2013a. “Design of Midcourse Trajectory for Tactical Ballistic Missile Intercept on the Basis of Zero Effort Miss.” Applied Mechanics and Materials 397-400: 536–45. https://doi.org/10.4028/www.scientific.net/amm.397-400.536
• Li, Ang, Zhenguo Jing, Qiang Liu, et al. 2021g. “Rhombic Optical Path Difference Bias White Light Interferometric Fiber-Optic Gyroscope.” Optics Letters 46 (7): 1502. https://doi.org/10.1364/ol.421012
• Li, Xuefeng, and Chaobing Li. 2018a. “Inertial Navigation and Initial Alignment Technology.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-10-6334-3_4
• Li, Xuefeng, and Chaobing Li. 2018b. “Redundant Fault Tolerance and Failure Reconfiguration Technology of Inertial Devices.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-10-6334-3_7
• Li, Jie, Yong Li, Qiao Jiang, and Jun Liu. 2012b. “The Initial Alignment Method for Low-Cost Strapdown Inertial Navigation System Based on Kalman Filter.” Applied Mechanics and Materials 220-223: 680–83. https://doi.org/10.4028/www.scientific.net/amm.220-223.680
• Li, Qihang, Kui Li, and Wenwei Liang. 2023l. “A Zero-Velocity Update Method Based on Neural Network and Kalman Filter for Vehicle-Mounted Inertial Navigation System.” Measurement Science and Technology 34 (4): 045110. https://doi.org/10.1088/1361-6501/acabde
• Li, Jianhua, Zhifeng Li, Zhenhong Niu, and Jiaqi Liu. 2017e. “Miniaturized Star Tracker for Micro Spacecraft with High Angular Rate.” In AOPC 2017: Space Optics and Earth Imaging and Space Navigation, edited by Carl Nardell, Suijian Xue, Huaidong Yang. SPIE. https://doi.org/10.1117/12.2283271
• Li, Bei, ZhuoNan Li, Xi Wang, ChengHao Huang, and Bo Yang. 2024a. “4.11-Million Q-Factor Whole-Angle MEMS Hemispherical Resonator Gyroscope with 0.013°/h Bias Instability.” Measurement Science and Technology 35 (11): 115116. https://doi.org/10.1088/1361-6501/ad6fc3
• Li, Jie, Jinguo Liu, and Zhihang Hao. 2006. “Active Pixel Sensor Geometrical Characteristic Effects on Star Image Subdivided Locating Accuracy for Star Tracker.” In SPIE Proceedings, edited by Jingshan Jiang, O. Y. Nosach, Jiaqi Wang. SPIE. https://doi.org/10.1117/12.667919
• Li, Jianli, Du Min, and Jiancheng Fang. 2011. “Fuzzy Modeling and Compensation of Scale Factor for Mems Gyroscope.” Mechanika 17 (4): 408–12. https://doi.org/10.5755/j01.mech.17.4.571
• Li, Mingyang, and Anastasios Mourikis. 2012. “Optimization-Based Estimator Design for Vision-Aided Inertial Navigation.” In Robotics: Science and Systems VIII. Robotics: Science and Systems Foundation. https://doi.org/10.15607/rss.2012.viii.031
• Li, Mingyang, and Anastasios I. Mourikis. 2013. “Optimization-Based Estimator Design for Vision-Aided Inertial Navigation.” In Robotics. The MIT Press. https://doi.org/10.7551/mitpress/9816.003.0036
• Li, Rongsheng (Ken), David Needelman, Richard Fowell, Tung-ching Tsao, and Yeong-Wei Wu. 2005. “Reusable Stellar Inertial Attitude Determination (SIAD) Design for Spacecraft Guidance, Navigation & Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-5928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5928
• Li, Hanzhou, Quan Pan, Xiaoxu Wang, Xiangjun Jiang, and Lin Deng. 2014b. “Kalman Filter Design for Initial Precision Alignment of a Strapdown Inertial Navigation System on a Rocking Base.” Journal of Navigation 68 (1): 184–95. https://doi.org/10.1017/s0373463314000575
• Li, Haitao, Zhenming Qu, Xinke Li, Feiteng Luo, and Wenjuan Chen. 2025k. “Research on Starting Characteristics of Two-Dimensional Supersonic Inlet by Using Unsteady Numerical Simulation.” Physics of Fluids 37 (7): 076102. https://doi.org/10.1063/5.0270314
• Li, Rui, and Y. J. Shi. 2010. “A Time-Fuel Optimal Control Problem of a Cruise Missile.” ANZIAM Journal 51. https://doi.org/10.21914/anziamj.v51i0.2680
• Li, Pei, Helmut Sobieczky, and Richard Seebass. 1995. “A Design Method for Supersonic Transport Wings.” In 13th Applied Aerodynamics Conference. AIAA 1995-1819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1819
• Li, Lin, Shiyan Sun, Yaqin Zeng, and Yusen Cheng. 2022h. “Reliability Evaluation Method of Guided Missile System Based on Multi-Source Information Fusion.” In 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022), edited by Xuexia Ye. SPIE. https://doi.org/10.1117/12.2635125
• Li, Wei, and Jinling Wang. 2013. “Magnetic Sensors for Navigation Applications: An Overview.” Journal of Navigation 67 (2): 263–75. https://doi.org/10.1017/s0373463313000544
• Li, Geng, Fei Wang, Guangzong Xiao, Guo Wei, Pengfei Zhang, and Xingwu Long. 2015e. “Temperature Compensation Method Using Readout Signals of Ring Laser Gyroscope.” Optics Express 23 (10): 13320. https://doi.org/10.1364/oe.23.013320
• Li, Rongsheng, Yeong-Wei Andy Wu, and Douglas H. Hein. 2004. System and Method for Calibrating Inter-Star-Tracker Misalignments in a Stellar Inertial Attitude Determination System. Patent Number: US-PATENT-6,691,033. Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20080005090
• Li, Xuefeng, Fan Xu, and Guoqiang Xu. 2022c. “Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs.” In Navigation: Science and Technology. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4637-0_2
• Li, Xuefeng, Fan Xu, and Guoqiang Xu. 2022f. “Redundant IMU Fault Detection.” In Navigation: Science and Technology. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4637-0_4
• Li, Xuefeng, Fan Xu, and Guoqiang Xu. 2022g. “Redundant IMU Reconfiguration.” In Navigation: Science and Technology. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4637-0_5
• Li, Shuai, Yuanhong Yang, and Liangya Du. 2023e. “Online Evaluation Technology for Fiber-Optic Coil Assembly in Depolarized Fiber-Optic Gyroscope.” In Advanced Sensor Systems and Applications XIII, edited by Minghong Yang, Xinyu Fan, Jianzhong Zhang, Chang-Seok Kim. SPIE. https://doi.org/10.1117/12.2687503
• Li, Fen, Hongtao Yang, and Linfeng Xu. 2017a. “A Design of Airborne Inertial Stabilized Platform Azimuth Shafting Structure.” In AIP Conference Proceedings, vol. 1864. Author(s). https://doi.org/10.1063/1.4993005
• Li, Zongxing, and Rui Zhang. 2021. “Two-Timescale Missile Autopilot Design Based on Suboptimal Control.” Journal of Physics: Conference Series 1828 (1): 012147. https://doi.org/10.1088/1742-6596/1828/1/012147
• Li, Kailun, Jiazhong Zhang, and Guanhua Mei. 2012a. “Aerothermoelastic Model of Panel Flutter with Consideration of the History Effects of Aerodynamic Heating.” International Journal of Applied Mechanics 04 (03): 1250034. https://doi.org/10.1142/s1758825112500342
• Li, Feifan, and Yanying Zhao. 2022. “Amplitude Reduction Optimization of Time Delay Semi-Active Control for Aircraft Landing Gear Shimmy.” Journal of Physics: Conference Series 2230 (1): 012009. https://doi.org/10.1088/1742-6596/2230/1/012009
• Li, Weiyi, Jisong Zhao, and Jiahong Deng. 2026k. “Sequential Convex Optimization for a Hypersonic Glide Vehicle Based on SOCP.” Journal of Physics: Conference Series 3207 (1): 012072. https://doi.org/10.1088/1742-6596/3207/1/012072
• Li, Pinghua, Xuye Zhuang, Xinpeng Zou, and Jianing Zhang. 2024e. “Improve the Performance of Mems Gyroscope by Combination of Virtual Gyroscope and Improved Sage-Husa Adaptive Filtering Algorithm.” Preprint, . https://doi.org/10.2139/ssrn.5009705
• Li-Xia and Luo Zhen-zhen. 2024. “Design and Implementation of Low Temperature Drift Suppression for Micro-Machined Gyroscope.” Journal of Nanoelectronics and Optoelectronics 19 (11): 1141–47. https://doi.org/10.1166/jno.2024.3673
• Lian, Cheng Bin, Bai Chen, Zhang Ren, and Xingyue Shao. 2013b. “Hypersonic Cruise Vehicle Attitude Control Based on NESO.” Applied Mechanics and Materials 427-429: 913–20. https://doi.org/10.4028/www.scientific.net/amm.427-429.913
• Lian, Chenglong, Bing Xiong, Xiaoqiang Fan, and Xiao Tang. 2025. “Impact of Aspect Ratio on Unstart Flow Characteristics in Hypersonic Inlet.” Journal of Physics: Conference Series 3085 (1): 012011. https://doi.org/10.1088/1742-6596/3085/1/012011
• Liang, D. 1978. “Application of Nonlinear Filter to Guided Missile Systems Involving Multistate Nonlinearities.” In Guidance and Control Conference. AIAA 1978-1305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1305
• Liang, Shen-Min, and Jan-Kaung Fu. 1991. “Passive Control Method for Drag Reduction for Transonic Projectiles.” In 9th Applied Aerodynamics Conference. AIAA 1991-3213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3213
• Liang, Xin Jian, and Shuai Gao. 2009. “A MEMS Capacitive Gyroscope with Improved Reliability.” In Materials science forum, vol. 628-629. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.628-629.341
• Liang, Yuxiao, and Dong Gao. 2025. “Geomagnetic/Inertial Fusion Navigation Method Based on Magnetic Anomaly Gradient Measurement.” Chinese Journal of Space Science 45 (1): 201. https://doi.org/10.11728/cjss2025.01.2024-0027
• Liang, Liyue, Daojie Yu, Jianping Du, Yijie Bai, Tao Li, and Jiale Zhou. 2026. “A Cooperative Adaptive Kalman Filter for Robust Terrain-Referenced Navigation in Complex Environments.” IET Radar, Sonar & Navigation 20 (1): e70101. https://doi.org/10.1049/rsn2.70101
• Liang, Dingwen, Lei Yuan, Zhihua Cai, and Qiong Gu. 2013. “Vehicle Navigation Algorithm Based on Unscented Kalman Filter Sensor Information Fusion.” Journal of Computer Applications 33 (12): 3444–48. https://doi.org/10.3724/sp.j.1087.2013.03444
• Liao, Hong Bo, Shi Xun Fan, Mo Hei, and Da Peng Fan. 2014. “Research on the Composite Control Scheme for the Stabilized Loop of Inertial Stabilized Platform.” In Key engineering materials, vol. 621. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.621.209
• Liao, Fang, Jian Wang, Eng Poh, and Dong Li. 2004. “Reliable Automatic Landing Control against Actuator Stuck Faults.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5233
• Licata, W. 1990. “Adaptive Learning Controller Applied to Tactical Missile Autopilot.” In 28th Aerospace Sciences Meeting. AIAA 1990-558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-558
• Lichtenstein, Bernard. 1965. “Design Philosophy Fora Low Cost Inertial Navigator.” In Guidance Control Conference. AIAA 1965-1212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1212
• Lichter, Michael. 2019. “Star Tracker Accuracy Improvement and Optimization for Attitude Measurement in Three-Axis.” In AMOS 2019 Technical Papers. AMOS Conference. https://doi.org/10.64861/jcvy3740
• Lichter, Nathan, and Gilbert Friedenreich. 1962. “Reliability Analysis of Redundancy Mechanisms.” In Seventh Military-Industry Missile and Space Reliability Symposium Proceedings. https://ntrs.nasa.gov/citations/19630007407
• Liebe, C., L. Callum, E. Dennison, L. Robeck, and P. Salomon. 2000. “APS Based Micro Star Tracker.” In International Society for Optical Engineering (SPIE), Aero Sense. https://ntrs.nasa.gov/citations/20060040869
• Liebe, Carl Christian, and Allen Eisenman. 1996. Operation and Performance of a Second Generation, Solid State, Star Tracker, the ASC. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210003826
• Lieberman, W. 1963. “Contributions of an Automatic Data System to Accomplishment of the Model 727 Certification Flight Test Program.” In Testing of Manned Flight Systems Conference. AIAA 1963-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1813
• “Light High-Temperature Aluminum Alloys for Supersonic and Hypersonic Vehicles.” 1992. In Thermal Structures and Materials for High-Speed Flight. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866128.0141.0160
• Lighthill, M. J. 1963. “The Automatic Landing of Aircraft Independently of the Weather.” Physics Bulletin 14 (3): 49–59. https://doi.org/10.1088/0031-9112/14/3/001
• Lijewski, Lawrence. 1980. Trajectory Prediction Theory of Supersonic High Fineness Ratio, Cruciform Fin Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada104989
• Lijewski, Lawrence. 1987. “Transonic Flow Solutions on a Blunt, Body-Wing-Canard Configuration Using the Euler Equations.” In 5th Applied Aerodynamics Conference. AIAA 1987-2273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2273
• Lill, Daniel, Jens Timmer, and Daniel Kaschek. 2019. “Local Riemannian Geometry of Model Manifolds and Its Implications for Practical Parameter Identifiability.” PLOS ONE 14 (6): e0217837. https://doi.org/10.1371/journal.pone.0217837
• Lim, Jaewook, Bum-Yong Park, and Dong-Hyun Cho. 2024. “Attitude Guidance for Constraining Star Tracker Elevation Angle during CubeSat-to-Ground Laser Pointing.” International Journal of Aeronautical and Space Sciences 26 (2): 760–72. https://doi.org/10.1007/s42405-024-00850-1
• Lim, K., A. Sreenatha, and M. Harrap. 2000. “Some Experiences with Preliminary Parameter Estimation of a Model Aircraft.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3904
• Lima Bezerra, Danielle, and Olexiy Shynkarenko. 2021. “Development of the 3D Printed Fuel Grain for a Solid-Fuel Ramjet Engine.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-0074
• Lin, Zhe. n.d. “Gain Scheduling of Aircraft Pitch Attitude and Control of Discrete, Affine, Linear Parametrically Varying Systems.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-11950
• Lin, Shih-Chun. 1978. “Sensitivity Limits of an Optical-Fiber Gyroscope.” In SPIE Proceedings, vol. 0157, edited by Shaoul Ezekiel, G. E. Knausenberger. SPIE. https://doi.org/10.1117/12.965480
• Lin, C.-F. 1982a. “Optimal Three-Dimensional Turning Performance of Supersonic Aircraft.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1326
• Lin, D.-F. 1982b. “Optimal Trajectories in Supersonic Flight.” In 20th Aerospace Sciences Meeting. AIAA 1982-366. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-366
• Lin, Huei Yung, and Li-Yu Chen. 2025. “Gnss-Denied Uav Localization with Satellite and Aerial Image Matching.” Preprint, . https://doi.org/10.2139/ssrn.5316247
• Lin, Yu Rong, Si Guo, and Guang Ying Zhang. 2011. “Fault Detection Method Applied to a Redundant Strapdown Inertial Navigation System.” Advanced materials research 179-180: 1242–47. https://doi.org/10.4028/www.scientific.net/amr.179-180.1242
• Lin, Chun-Liang, and Chai-Lin Hwang. 2003. “A Dynamically Fuzzy Gain – Scheduled Design for Missile Autopilot.” Aeronautical Journal 107 (1076): 599–606. https://doi.org/10.1017/s0001924000013816
• Lin, C.-F., and S.-P. Lee. 1984. “Robust Missile Autopilot Design Using Generalized Singular Optimal Control Technique.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1847
• Lin, Yusen, Lingjuan Miao, Zhiqiang Zhou, and Qi Ming. 2023. “System-Level Calibration Method Considering Nonorthogonal Angles in Dual-Axis Rotational Inertial Navigation System.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_416
• Lin, J. L., and C. S. Yang. 2005. “Heat Transfer Analysis of Charring Ablators under Aerodynamic Heating.” Aircraft Engineering and Aerospace Technology 77 (3): 214–21. https://doi.org/10.1108/00022660510597232
• Lin, Siying, Feng Yu, Zijun Zhou, and Chenyang Li. 2025. “UAV Swarm Cooperative Navigation Technology in Partial GNSS-Denied Environment.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2268-9_9
• Lina, Lindsay J., Robert A. Champine, and Garland J. Morris. 1959. Flight Investigation of an Automatic Throttle Control in Landing Approaches. NASA-MEMO-2-19-59L. NASA. https://ntrs.nasa.gov/citations/19980231089
• Lind, Rick. 1999. “Linear Parameter-Varying Modeling and Control of Structural Dynamics with Aerothermoelastic Effects.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1393
• Line of Sight Propagation. 2006. Wiley. https://doi.org/10.1002/9780470612095.ch4
• Ling, C. K. 1969. “Quasi-Optimum Design of an Aircraft Landing Control System.” In AMERICAN AUTOMATIC CONTROL COUNCIL, JOINT AUTOMATIC CONTROL CONFERENCE. https://ntrs.nasa.gov/citations/19690065291
• Liou, May-Fun, and Thomas Benson. 2010. “Optimization of Bleed for Supersonic Inlet.” In 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference. AIAA 2010-9172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-9172
• Liounis, Andrew, Sun Hur-Diaz, Chris Gnam, et al. n.d. “Celestial Navigation in Cislunar Space with autoNGC.” In Annual Cislunar Security Conference (CLSC). https://ntrs.nasa.gov/citations/20240014841
• Lipton, A. H. 1967. Alignment of Inertial Systems on a Moving Base. NASA-TN-D-4110. NASA. https://ntrs.nasa.gov/citations/19670026463
• Little, Joseph W. 1967. “An Engineering Approach to the Mathematics of Celestial Navigation.” Navigation 14 (3): 239–48. https://doi.org/10.1002/j.2161-4296.1967.tb02204.x
• Liu, Jun. n.d. “Eigenvector-Based Multidimensional Frequency Estimation: Identifiability, Performance, and Applications.” PhD diss., University of Louisville. https://doi.org/10.18297/etd/842
• Liu, Xiao. 2013. “Modeling and Analysis of Foldable Parallel Stabilized Platform in Non-Inertial System.” Journal of Mechanical Engineering 49 (17): 101. https://doi.org/10.3901/jme.2013.17.101
• Liu, Xipeng. 2018. “The Cruise Missile Guidance and Control System Design and Simulation Based on the Integral Sliding Mode Control.” In Proceedings of the 2018 7th International Conference on Energy and Environmental Protection (ICEEP 2018). Atlantis Press. https://doi.org/10.2991/iceep-18.2018.320
• Liu, Peiqing. 2022. “Aerodynamic Characteristics of Supersonic Thin Airfoil and Wing.” In Aerodynamics. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4586-1_12
• Liu, Zhao Hua, Jia Bin Chen, Yu Liang Mao, and Chun Lei Song. 2012c. “Research of Random Drift for MEMS Gyroscope Based on Gray System and ARMA Model.” Advanced materials research 546-547: 1526–31. https://doi.org/10.4028/www.scientific.net/amr.546-547.1526
• Liu, D. D., P. C. Chen, Lei Tang, K. T. Chang, and Adel Chemaly. 2002. Integrated Hypersonic Aerothermoelastic Methodology for Transatmospheric Vehicle (TAV)/Thermal Protection System (TPS) Structural Design and Optimization. Defense Technical Information Center. https://doi.org/10.21236/ada403577
• Liu, Hong Liang, Wei Yi Chen, and Zhong Sheng Xu. 2014a. “Application of Wavelet Analysis in Random Drift Signal Filtering of Fiber Optic Gyroscope.” Applied Mechanics and Materials 672-674: 2029–32. https://doi.org/10.4028/www.scientific.net/amm.672-674.2029
• Liu, Quanjun, Shicong Dai, Ying Wang, Yudong Wang, and Changwan Min. 2017f. “In-Flight Lateral Control Departure Parameter Estimation for Reusable Launch Vehicle Using Retrospective Cost Adaptive Control.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2284
• Liu, Ke, Xiaofeng He, Jun Mao, et al. 2023e. “Map Aided Visual-Inertial Integrated Navigation for Long Range UAVs.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_584
• Liu, Shuang, Junyi Hu, Yuxin Wang, Qingwen Liu, Huilian Ma, and Zuyuan He. 2023f. “Navigation-Grade Three-Axis Resonant Fiber-Optic Gyroscope Employing a Multiplexed Source.” Optics Letters 48 (10): 2639. https://doi.org/10.1364/ol.487077
• Liu, Shuang, Junyi Hu, Yuxin Wang, Hewei Wang, Lu Liu, and Huilian Ma. 2023h. “Optimizing the Broadband Source-Driven Resonant Fiber-Optic Gyroscope.” In 28th International Conference on Optical Fiber Sensors. Optica Publishing Group. https://doi.org/10.1364/ofs.2023.th6.47
• Liu, Hongwu, Shuling Hu, Gongliu Yang, and Yongfeng Zhang. 2023b. “Design of Nonlinear Integral Fuzzy Sliding Mode Control for Stability Loop of FOG Inertial Platform.” In Sixth International Conference on Intelligent Computing, Communication, and Devices (ICCD 2023), edited by Srikanta Patnaik. SPIE. https://doi.org/10.1117/12.2682983
• Liu, Jianhao, Dongzheng Kuang, Qinghua Zeng, and Liang Zhang. 2025k. “Predefined-Time Control with Disturbance Observer for Horizontal Take-off and Landing Reusable Launch Vehicle.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-3010-6_40
• Liu, Z., X. Li, X. Ding, and Z. Wang. 2021d. “Research on Soft Sensing of Aircraft Nose Landing Gear Shimmy Damp Based on Neural Network.” IET Conference Proceedings 2020 (3): 407–11. https://doi.org/10.1049/icp.2021.0418
• Liu, Mao Han, Chun Tao Li, and Yi Wang. 2011c. “UAV Automatic Landing Control Law.” Advanced materials research 383-390: 1452–57. https://doi.org/10.4028/www.scientific.net/amr.383-390.1452
• Liu, W. I., Zhixiong Li, and Zhichao Zhang. 2018a. “Error Modelling and Optimal Estimation of Laser Scanning Aided Inertial Navigation System in GNSS-Denied Environments.” Journal of Navigation 72 (3): 741–58. https://doi.org/10.1017/s037346331800084x
• Liu, Shijie, Weidong Liu, Yi Wang, and Zhiyong Lin. 2017e. “Free Jet Test of Continuous Rotating Detonation Ramjet Engine.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2282
• Liu, Zhenming, Yaoyao Long, Charlotte Wehner, Haoran Wen, and Farrokh Ayazi. 2023a. “4H Silicon Carbide Bulk Acoustic Wave MEMS Gyroscope with Ultra-High Q for on-Chip Inertial Navigation.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3197189/v1
• Liu, Rui, Pin Lyu, Jizhou Lai, Junqing Lu, and Huafeng Hu. 2025i. “Mechanism and Implementation of Error Suppression in MEMS Inertial Navigation System via Rotational Modulation and Array.” Measurement Science and Technology 36 (9): 095113. https://doi.org/10.1088/1361-6501/ae02ae
• Liu, Qili, Li Qiao, Kyungrae Kang, and Hyungrok Do. 2022f. “From Flow Choking to Inlet Buzz of Axisymmetric Scramjets in Mach 4.5 Flows.” In AIAA SCITECH 2022 Forum. AIAA 2022-0202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0202
• Liu, F., and W. Sirignano. 2000. “Turbojet and Turbofan Engine Performance Increases through Turbine Burners.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-741
• Liu, Yang, and Xuetao Tian. 2019. “Design and Implementation of UAV’s Flight Control System Test Platform.” IOP Conference Series: Materials Science and Engineering 677 (5): 052056. https://doi.org/10.1088/1757-899x/677/5/052056
• Liu, Jing, Long Wang, Xiao Li, et al. 2015. “Star Extraction Based on Clustering within a Star Tracker.” SCIENTIA SINICA Technologica 45 (3): 257–62. https://doi.org/10.1360/n092014-00480
• Liu, Yuanhua, Ziwei Wang, and Xinliang Niu. 2022j. “MEMS Gyroscope Temperature Compensation Based on SSA-RBF Neural Network.” In Proceedings of the 2022 5th International Conference on Artificial Intelligence and Pattern Recognition. ACM. https://doi.org/10.1145/3573942.3573959
• Liu, DongXu, ShaoXin Wang, KeQi Qi, Peng Dong, WeiChuan Guo, and JianJun Jia. 2024c. “Calibration Test Method of Capacitance Sensor for Multiple Degrees of Freedom Based on Inertial Sensor.” SCIENTIA SINICA Physica, Mechanica & Astronomica 54 (7): 270407. https://doi.org/10.1360/sspma-2024-0090
• Liu, Xiaolu, Linda Wanika, Michael Chappell, and Jürgen Branke. 2025c. “Efficiently Establishing Practical Identifiability via Active Learning.” Preprint, . https://doi.org/10.2139/ssrn.5125554
• Liu, Hui, Lin Wu, Lifeng Bao, Qianqian Li, Panpan Zhang, and Menghan Xi. 2022e. “A Fast Spatial Features Matching Method for Underwater Gravity Aided Navigation.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-2576-4_40
• Liu, Yong, Yeong-Wei Andy Wu, and Rongsheng Li. 2001. System for Star Catalog Equalization to Enhance Attitude Determination. Patent Application Number: US-PATENT-APPL-SN-628779. Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20080004162
• Liu, Feng, and Bo Yang. 2023. “An Initial Alignment Algorithm of Strapdown Inertial Navigation System Assisted by Doppler Radar Based on Adaptive Filtering.” In Fourth International Conference on Artificial Intelligence and Electromechanical Automation (AIEA 2023), edited by Fushuan Wen, chuanjun Zhao, Yanjiao Chen. SPIE. https://doi.org/10.1117/12.2684731
• Liu, Jun-Cheng, Jing-Juan Zhang, and Li-Fen Tan. 2012a. “Multi-Aircraft Inertial Navigation Data Fusion Method Aided by One Pseudolite.” In CICTP 2012. American Society of Civil Engineers. https://doi.org/10.1061/9780784412442.096
• Liu, Ming-Yi, Jing Juan Zhang, Xue Yun Wang, and Ran Li. 2014f. “A New Method for Platform Inertial Navigation Initial Alignment Based on Rotation Mode.” Applied Mechanics and Materials 543-547: 1344–50. https://doi.org/10.4028/www.scientific.net/amm.543-547.1344
• Liu, Qijia, Jiechao Zhang, Yao Zheng, and Yaolong Liu. 2025l. “Supersonic Aircraft Aerodynamic Performance Prediction Based on Machine Learning Approach.” AIP Advances 15 (8): 085111. https://doi.org/10.1063/5.0282257
• Liu, Qingwen, Shangxiang Zhao, Huilian Ma, and Zuyuan He. 2023k. “White-Light Multi-Beam Interferometry for Resonant Fiber Optic Gyroscope and Other Applications.” In 28th International Conference on Optical Fiber Sensors. Optica Publishing Group. https://doi.org/10.1364/ofs.2023.w2.1
• Liu, Xiao, Tieshi Zhao, Chang Wang, and Hui Bian. 2013a. “Kinematics Analysis and Simulation of Stabilizing Platform in Non-Inertial System.” ROBOT 35 (6): 723. https://doi.org/10.3724/sp.j.1218.2013.00723
• Liu, Hong, Yu-long Zhou, and Zhao-peng Gu. 2014e. “Inertial Measurement Unit-Camera Calibration Based on Incomplete Inertial Sensor Information.” Journal of Zhejiang University SCIENCE C 15 (11): 999–1008. https://doi.org/10.1631/jzus.c1400038
• Liu, Wenzhao, Yan Zhou, Haoyang Li, Longjie Tian, Chunxi Zhang, and Yanqiang Yang. 2025j. “A Novel Sequential Observability Analysis Method for a Multi-FOG Inertial Navigation System.” Measurement Science and Technology 36 (4): 046309. https://doi.org/10.1088/1361-6501/adbe92
• Liu, Zhenbo, Qifan Zhou, Yongyuan Qin, and Naser El-Sheimy. 2017g. “Vision-Aided Inertial Navigation System with Point and Vertical Line Observations for Land Vehicle Applications.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-10-4591-2_36
• Liu, Chun, Fagen Zhou, Yiwei Sun, Kaichang Di, and Zhaoqin Liu. 2012d. “Stereo-Image Matching Using a Speeded up Robust Feature Algorithm in an Integrated Vision Navigation System.” Journal of Navigation 65 (4): 671–92. https://doi.org/10.1017/s0373463312000264
• Livani, Mostafa, Keramat MalekzadehFard, and Saeed Shokrollahi. 2016. “Higher Order Flutter Analysis of Doubly Curved Sandwich Panels with Variable Thickness under Aerothermoelastic Loading.” Structural Engineering and Mechanics 60 (1): 1–19. https://doi.org/10.12989/sem.2016.60.1.001
• Lloyd, Seth W., Michel J. F. Digonnet, and Shanhui Fan. 2011. “Tactical-Grade Interferometric Fiber Optic Gyroscope Driven with a Narrow-Linewidth Laser.” In SPIE Proceedings, vol. 7753. SPIE. https://doi.org/10.1117/12.886025
• Lloyd, A. J. P., J. J. McAvoy, and V. K. Rajpaul. 1978. Integration of Air Cushion Landing System Technology into the JINDIVIK Remotely Piloted Vehicle. Defense Technical Information Center. https://doi.org/10.21236/ada058004
• Lo, James Ting-Ho. 1978. Optimal Estimation for the Satellite Attitude Using Star Tracker Measurements. Defense Technical Information Center. https://doi.org/10.21236/ada064779
• Lock, R. C. 1957. “A Note on the Application of the Supersonic Area Rule to the Determination of the Wave Drag of Rectangular Wings.” Journal of Fluid Mechanics 2 (6): 575–82. https://doi.org/10.1017/s0022112057000385
• Lock, R. C. 1963. “The Aerodynamic Design of Swept Winged Aircraft at Transonic and Supersonic Speeds.” Journal of the Royal Aeronautical Society 67 (630): 325–37. https://doi.org/10.1017/s0001924000062758
• Lock, R. C., and J. Bridgewater. 1967. “Theory of Aerodynamic Design for Swept-Winged Aircraft at Transonic and Supersonic Speeds.” Progress in Aerospace Sciences 8: 139–228. https://doi.org/10.1016/0376-0421(67)90004-8
• Lock, Andrew, Glen Oberman, Ingo H. Jahn, et al. 2025. “Hypersonic Glide Vehicle Shape and Trajectory Co-Design.” In AIAA SCITECH 2025 Forum. AIAA 2025-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1337
• Locke, W. 1981. “Cruise Missile System Design.” In 16th Annual Meeting and Technical Display. AIAA 1981-902. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-902
• Lockman, W. K., and C. E. Derose. 1971. Aerodynamic Heating of a Space Shuttle Delta-Wing Orbiter. NASA-TM-X-62057. NASA. https://ntrs.nasa.gov/citations/19710026868
• Loftin, L., Jr. 1967. “Research Relating to Long-Range Supersonic Cruising Aircraft.” In 10th Anglo-American Aeronautical Conference. AIAA 1967-748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-748
• Loftin, L. K., Jr. 1973. “Toward a Second-Generation Supersonic Transport.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730032806
• Lofts, Christopher S. 2015. Modular Missile Technologies (MMT): A Modular Open Architecture Approach for Guided Missiles. Defense Technical Information Center. https://doi.org/10.21236/ada622336
• Lombaerts, T. J. J., Q. P. Chu, J. A. Mulder, and D. A. Joosten. 2007. “Real Time Damaged Aircraft Model Identification for Reconfiguring Flight Control.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6717. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6717
• Lomov, A. A. 2011. “On Quantitative a Priori Measures of Identifiability of Coefficients of Linear Dynamic Systems.” Journal of Computer and Systems Sciences International 50 (1): 1–13. https://doi.org/10.1134/s106423071101014x
• Londono, Monica, and Bret Leonhardt. 2012. “Parameter Identification of an Executive Transport Aircraft: Simulation Update and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4734
• Long, G. A. 1950. “MISSILE GUIDANCE.” Navigation 2 (8): 290–94. https://doi.org/10.1002/j.2161-4296.1950.tb00580.x
• Longenbaker, W. 1982. “Terrain-Aided Navigation of an Unpowered Tactical Missile Using Autopilot-Grade Sensors.” In Guidance and Control Conference. AIAA 1982-1510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1510
• Longo, J., and A. Das. 1990. “Numerical Simulation of Vortical Flows over Close-Coupled Canard-Wing Configuration.” In 8th Applied Aerodynamics Conference. AIAA 1990-3003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3003
• Longstaff, I., S. Ellms, K. Goussak, and C. Christoff. 1992. “The Litton LN-100 Advanced Technology Medium Accuracy Lightweight Inertial Navigation System.” In Guidance, Navigation and Control Conference. AIAA 1992-4416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4416
• Longwell, J. P., and M. A. Weiss. 1952. Ramjet Technology. Chapter 7. Air-Fuel Mixture Preparation. Defense Technical Information Center. https://doi.org/10.21236/ad0041743
• Loomis, Bryant Daniel. n.d. Simulated Mass Change Recovery for Various Implementations of a Future Atomic Interferometer Gravity Gradiometer (AIGG). Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20230013435
• Lorenz, Roland, Robert Delaney, and John Custer. 1990. “Aerodynamic Analysis of a Stowed Cruise Missile Propfan Blade.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3092
• Lorenzini, D., and R. Neeland. 1971. “Analysis of a Pneumatic Isolation System for Inertial Instrument Testing.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-910. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-910
• Lory, C. B., J. Feldman, and J. S. Sinkiewicz Jr. 1971. Dynamic Testing of a Single-Degree-of-Freedom Strapdown Gyroscope. NASA-CR-123804. NASA. https://ntrs.nasa.gov/citations/19720022933
• Losik, Ph.D., Len. 2012. “Using the Prognostic Health Management Program on the Air Force Next Generation Reusable Launch Vehicle.” In AIAA SPACE 2012 Conference & Exposition. AIAA 2012-5197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5197
• Loth, Eric, Sean Candon, and Michael Rybalko. 2016. “Mass Flow Ratio Influence on Shock and Pressure Spectra for a Low-Boom Supersonic Inlet.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0532. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0532
• Lovell, D. 1999. “European Research to Reduce Drag for Supersonic Transport Aircraft.” In 17th Applied Aerodynamics Conference. AIAA 1999-3100. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3100
• Lovell, D. A. 2001. “European Research to Reduce Drag for Supersonic Transport Aircraft.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_14
• Lowell, Arthue L. 1953. “Guided Missiles and the Weapon System Concept.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/530070
• Lowen, I. B., and M. S. Maxwell. 1965. Scanning Celestial Attitude Determination System (SCADS). NASA. https://ntrs.nasa.gov/citations/19660040210
• Lowrance, John L., and Stephen R. Smith. 1996. ILARTS Imaging Sensor for Day/Night Aircraft Approach and Landing. Defense Technical Information Center. https://doi.org/10.21236/ada381746
• Lowry, J. L. 1966. An Introduction to Analytic Platforms for Inertial Guidance. NASA-CR-75074. NASA. https://ntrs.nasa.gov/citations/19660017409
• Lowry, Charles H. 2013. “Space Shuttle Orbiter Drag Chute Summary.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20130010383
• Lu, Ping, David B. Doman, and John D. Schierman. 2006. Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction. Defense Technical Information Center. https://doi.org/10.21236/ada445166
• Lu, Ping, David Doman, and John Shierman. 2005. “Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6059
• Lu, Jun, Wen-Gang Hu, and Jian-Ling Yin. 2017c. “Fiber Optic Gyroscope Miniaturization Technology.” In Mechatronics and Manufacturing Technologies. WORLD SCIENTIFIC. https://doi.org/10.1142/9789813222359_0015
• Lu, Chen, Rong-Bing Li, Jian-Ye Liu, and Ting-Wan Lei. 2018b. “Air Data Estimation by Fusing Navigation System and Flight Control System.” Journal of Navigation 71 (5): 1231–46. https://doi.org/10.1017/s037346331800022x
• Lu, Jiazhen, Shufang Liang, and Lie Yang. 2018c. “Analytic Coarse Alignment and Calibration for Inertial Navigation System on Swaying Base Assisted by Star Sensor.” IET Science, Measurement & Technology 12 (5): 673–77. https://doi.org/10.1049/iet-smt.2017.0535
• Lu, Peng, and Erik-Jan Van Kampen. 2015. “Aircraft Inertial Measurement Unit Fault Identification with Application to Real Flight Data.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0859. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0859
• Lu, Kewen, Jie Yang, Xinlong Wang, and Guanghao Nie. 2025. “An Innovative High-Precision Gyroscope-Free Strapdown Inertial Navigation Scheme.” Measurement Science and Technology 36 (10): 106309. https://doi.org/10.1088/1361-6501/ae131d
• Lu, Jiuli, Zhaohui Yuan, and Bo Liang. 2018a. “The Adaptive Control of Aircraft Brake Based on Asymmetric Barrier Lyapunov Function.” In International Conference on Electromechanical Control Technology and Transportation (ICECTT). https://doi.org/10.5220/0006965801020109
• Lucas, James R., Walter F. O’Brien, and Anthony M. Ferrar. 2014. “Effect of BLI–Type Inlet Distortion on Turbofan Engine Performance.” In Volume 1A: Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2014-26666
• Luce, Richard W., Jr. 1949. Deflections of a Supersonic Wing Due to Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ada278113
• Ludwig, Gary R. 1979. Tests of an Improved Rotating Stall Control System on a J-85 Turbojet Engine. Defense Technical Information Center. https://doi.org/10.21236/ada077704
• Lukacs, John, and Oleg Yakimenko. 2007. “Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles during the Boost Phase.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6538. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6538
• Lukens, David R., Alfred F. Schmitt, and George T. Broucek. 1961. Approximate Transfer Functions for Flexible-Booster-and Autopilot Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0269015
• Lukoyanov, Egor V., and Elena V. Dranitsyna. 2026. “Algorithms for Increasing the Fault Tolerance of Strapdown Redundant Inertial Navigation Systems.” Advanced Devices & Instrumentation 7: 0146. https://doi.org/10.34133/adi.0146
• Lukoyanov, E. V., D. A. Gontar, and E. V. Dranitsyna. 2025. “Comparative Analysis of Fault Detection and Isolation Algorithms for Redundant Strapdown Inertial Navigation Systems.” Izvestiâ vysših učebnyh zavedenij. Priborostroenie 68 (1): 79–88. https://doi.org/10.17586/0021-3454-2025-68-1-79-88
• Lukyanov, SHenzhen Zhao V. V. 2025. “Modeling of aircraft trajectories for studying strapdown inertial navigation systems.” Automation Modern Techologies: 450–55. https://doi.org/10.36652/0869-4931-2025-79-10-450-455
• Lunde, T. 1977. Real-Time Testing of Titanium Sheet and Extrusion Coupon Specimens Subjected to Mach 2.7 Supersonic Cruise Aircraft Wing Stresses and Temperatures. NASA-CR-2754. NASA. https://ntrs.nasa.gov/citations/19780005535
• Lungu, Mihai. 2017. “Automatic Control of Aircraft Landing by Using the H2/H∞ Control Technique.” In Modelling, Identification and Control. ACTAPRESS. https://doi.org/10.2316/p.2017.848-004
• Lungu, Romulus, and Mihai Lungu. 2015b. “Design of Automatic Landing Systems Using the H-Inf Control and the Dynamic Inversion.” Journal of Dynamic Systems, Measurement, and Control 138 (2): 024501. https://doi.org/10.1115/1.4032028
• Luo, Guo, and Bingling Chen. 2024. “Applying Adaptive Wavelet Neural Network and Sliding Mode Control for Tracking Control of MEMS Gyroscope.” Preprint, . https://doi.org/10.22541/au.172467436.66059147/v1
• Luo, Zhihuan, Dylan D. Dooner, and Andrew J. Neely. 2026. “Aerothermoelastic Deformation of an X-43 Inspired Hypersonic Scramjet Intake Flowpath.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5108
• Luo, Xuefeng, and Zhengbin Li. 2007. “Passive Ring Resonator Gyroscope Using High-Order Dispersion.” In SPIE Proceedings, vol. 6723, edited by Junhua Pan, James C. Wyant, Hexin Wang. SPIE. https://doi.org/10.1117/12.782904
• Luo, Qinghua, Boyuan Liu, Mutong Yu, Yuhao Su, Longxin Yang, and Lan Wang. 2025. “Inertial-Geomagnetic Integrated Navigation Method Based on Kalman Filter and Adaptive Search Area.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2236-8_45
• Luo, Shibin, Wencai Luo, Zhiyong Lin, and Zhengguo Wang. 2003. “Application of Taguchi Design Methods and Uniform Design Methods to Scramjet Propulsion System Optimization for Hypersonic Cruise Vehicle.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5193
• Luo, Cui Hua, Cai Wen Ma, and Yan Li. 2014. “Hybrid Adaptive Robust Controller on Inertial Gyro LOS Platform.” Applied Mechanics and Materials 513-517: 2910–13. https://doi.org/10.4028/www.scientific.net/amm.513-517.2910
• Luo, Wenguo, Yang Tao, Jianfeng Zhu, and Yancheng You. 2024. “Evolution Characteristics Analysis of Supersonic Inlet Buzz with High-Order Dynamic Mode Decomposition Method.” Journal of Aerospace Engineering 37 (3): 04024026. https://doi.org/10.1061/jaeeez.aseng-5388
• Luo, Zhicong, and Iryna Voronko. 2023. “Aircraft Landing Gear Test for Emerging Loads.” ГРААЛЬ НАУКИ, no. 24: 389–90. https://doi.org/10.36074/grail-of-science.17.02.2023.070
• Lušić, Zvonimir, Tony Pinčetić, and Paško Esko Krančević. 2024. “Role of Celestial Navigation in Modern Day and Future Navigation.” In Maritime Transport Conference. Universitat Politècnica de Catalunya. Iniciativa Digital Politècnica. https://doi.org/10.5821/mt.12734
• Lutgring, Stephen M., and Emil Tchilian. 2024. “Performance Testing the Advanced CT-2020 Domestic Star Tracker.” In Advances in the Astronautical Sciences. Springer International Publishing. https://doi.org/10.1007/978-3-031-51928-4_14
• Lv, Qiaochu, Xueying An, Dingjie Wang, and Jie Wu. 2021. “Research on Error Online Calibration Method of Inertial/Stellar Refraction Integrated Navigation System.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-3142-9_41
• Lv, Haiyin, Rui Li, Jinglei Xu, Zhencan Zhang, Yucheng Zhang, and Ziji Wang. 2026. “A One-Dimensional Model for an Air-Breathing Rotating Detonation Ramjet/scramjet Engine.” Preprint, . https://doi.org/10.2139/ssrn.6351266
• Lykken, L., and N. Shah. 1971. “Direct Lift Control for Improved Automatic Landing Safety and Performance for a Large Transport Aircraft.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-906
• Ma, Li. 2014. “Slope-Contact-Type Cavity Adjustment Method and Experiment Study for Ring Laser Gyroscope.” Journal of Mechanical Engineering 50 (1): 10. https://doi.org/10.3901/jme.2014.01.010
• Ma, Liheng, Franco Bernelli-Zazzera, Xingshu Wang, and Shiqiao Qin. 2016. “Attitude-Correlated Frames Algorithms to Improve the Attitude Accuracy of the Star Tracker under Highly Dynamic Conditions.” In AIAA/AAS Astrodynamics Specialist Conference. AIAA 2016-5670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5670
• Ma, Kwun Yeung, Cesare A. Hall, Tianhou Wang, and Tim S. Williams. 2024b. “Reverse Thrust Aerodynamics of Variable Pitch Fans with Inlet Distortion.” In Volume 1: Aircraft Engine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2024-121728
• Ma, Wenhui, Guoqiang He, Ya Jun Wang, Liu Zhilin, Shaohua Zhu, and Qin Fei. 2025b. Inlet-Engine Matching Control of Rocket Based Combined Cycle Engine under Rocket-Ramjet Mode. https://doi.org/10.52202/083090-0053
• Ma, Xinyu, Fuying Li, and Min Zhang. 1998. “Experimental Study of Polarization-Maintaining Fiber Ring Resonator in Resonator Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 3555, edited by Shanglian Huang, Kim D. Bennett, David A. Jackson. SPIE. https://doi.org/10.1117/12.318174
• Ma, Jun, Yi Lin, Hu Liang, and Maochun Li. 2021. “Temperature Modeling and Compensation Method of Fiber Optic Gyroscope Based on Multilayer Perceptron.” In AOPC 2021: Novel Technologies and Instruments for Astronomical Multi-Band Observations, edited by Suijian Xue, Yongtian Zhu. SPIE. https://doi.org/10.1117/12.2606390
• Ma, Huilian, Shuang Liu, Junyi Hu, Lu Liu, Yuxin Wang, and Hewei Wang. 2023c. “Navigation-Grade Resonant-Fiber Optic Gyroscope with a Broadband Source.” In CLEO 2023. Optica Publishing Group. https://doi.org/10.1364/cleo_si.2023.sf1h.1
• Ma, Xianglu, Xiaoshan Yao, Hao Meng, and Fan Yi. 2023b. “Evaluation of Initial Alignment Algorithm for Dynamic Base of Fiber Optic Gyro Inertial Navigation System.” In AOPC 2023: Optic Fiber Gyro, edited by Shangran Xie, Qi Wang, Benli Yu. SPIE. https://doi.org/10.1117/12.3005201
• Mabius, L., and H. Kaufman. 1976. An Adaptive Flight Controller for the F-8 without Explicit Parameter Identification. Analytic Sciences Corporation. https://ntrs.nasa.gov/citations/19770045952
• Macario, R. C. V. 1997. “Beyond the Line-of-Sight Propagation of VHF and UHF Radio Signals in the Middle East Arabian Gulf Areas.” In IEE Colloquium on Propagation Characteristics and Related System Techniques for Beyond Line-of Sight Radio, vol. 1997. IEE. https://doi.org/10.1049/ic:19971358
• Mace, J., and D. Sedlock. 1981. “A Perspective on Developing New Inlet Distortion Measurement and Predictive Methods.” In 17th Joint Propulsion Conference. AIAA 1981-1589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1589
• MacKinnon, D. 1969. Improving Automatic Landing System Performance Using Modern Control Theory and Inertial Measurements. NASA-CR-86186. NASA. https://ntrs.nasa.gov/citations/19690024058
• MacKinnon, D. 1970. Automatic Landing System Optimization Using Inertial Navigation Data and Modern Control Theory. NASA-CR-111575. NASA. https://ntrs.nasa.gov/citations/19710002956
• Mackinnon, D., and P. Madden. 1971. “Performance Limitation of a Simplified Radio- Inertial Lateral Control System for Automatic Landing.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-957. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-957
• MacLean, M., and H. Rodriguez. 1996. “A Low-Risk, Reliable, Operationally Efficient Auxiliary Propulsion System for the Reusable Launch Vehicle.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3228
• Macmillan, A. 1981. “Navstar Global Positioning System Flight Test Program Overview.” In 1st Flight Test Conference. AIAA 1981-2350. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2350
• MacPherson, Duncan. 1963. Self-Contained Explicit Guidance Equations for Ballistic Missiles. Defense Technical Information Center. https://doi.org/10.21236/ad0403872
• Macy, David F. 1995. “Single Ended Tuning Fork Inertial Sensor and Method.” Journal of the Acoustical Society of America 97 (2): 1363–1363. https://doi.org/10.1121/1.412147
• Madani, Irfan, and David Allerton. 2006. “An Optimized Routing Method for Terrain Referenced Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6601
• Madden, Michael. 2010. “Gravity Modeling Effects on Surface-Interacting Vehicles in Supersonic Flight.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2010-7919. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7919
• Madden, P., and M. Desai. 1973. “Nonlinear Trajectory Following in the Terminal Area: Guidance, Control and Flight Mechanics Concepts Using the Microwave Landing System.” In Guidance and Control Conference. AIAA 1973-903. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-903
• Madigan, R. J. 1969. “Flight Test Experiments to Evaluate Aided- Inertial System Performance for Terminal Guidance.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19700034187
• Madigan, Ronald J. 1970. “Flight Test Experiments to Evaluate Aided-Inertial System Performance for Terminal Guidance.” Navigation 17 (1): 83–91. https://doi.org/10.1002/j.2161-4296.1970.tb00025.x
• Madyastha, Venkatesh, Vishal Ravindra, Srinath Mallikarjunan, and Anup Goyal. 2011. “Extended Kalman Filter vs. Error State Kalman Filter for Aircraft Attitude Estimation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6615
• Magnani, M. 1993. “Very High Pointing Accuracy Star-Tracker Optics Trade-off Analysis.” In Lens and Optical Systems Design. SPIE. https://doi.org/10.1117/12.142870
• Magree, Daniel P., and Eric N. Johnson. 2013. “Performance of a Monocular Vision-Aided Inertial Navigation System for a Small UAV.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4699. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4699
• Magree, Daniel P., and Eric N. Johnson. 2015. “A Monocular Vision-Aided Inertial Navigation System with Improved Numerical Stability.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0097
• Mahajan, Aparajit J., John M. Lucero, Oral Mehmed, and George L. Stefko. 1992. Aeroelastic Stability Analyses of Two Counter Rotating Propfan Designs for a Cruise Missile Model. NASA-TM-105268. NASA. https://ntrs.nasa.gov/citations/19920013948
• Mahato, Mrinal, Srinivasa Raju Sarikonda, R. Balasubramanian, K. Anadhanarayanan, Ganesh T. K. Anavaradham, and Sandip Chattopadhayay. 2023. “Aerodynamic Characterization of Hypersonic Launch Vehicle Laden with Exposed Scramjet Based Cruise Vehicle.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3035
• Mahboub, Vahid, and Dorsa Mohammadi. 2018. “A Constrained Total Extended Kalman Filter for Integrated Navigation.” Journal of Navigation 71 (4): 971–88. https://doi.org/10.1017/s0373463318000012
• Mahi, Zoubida. 2025a. “Optical Noise Impact on Star-Tracker Centroid Calculation.” In International Conference on Space Optics — ICSO 2024, edited by Frédéric Bernard, Nikos Karafolas, Philippe Kubik, Kyriaki Minoglou. SPIE. https://doi.org/10.1117/12.3071281
• Mahlmeister, J. E., T. Ishimoto, and A. Ambrosio. 1955. Studies on Thermal Stresses for Aircraft Structures Exposed to Transient External Heating. Volume 1. Evaluation of the Thermal Response, Force and Moment in a Plate. Defense Technical Information Center. https://doi.org/10.21236/ad0093337
• Mahoney, J. J. 1962. “Inlet Diffuser Design Techniques.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/620299
• Mahudapathi, Sumathi, Anish Bekal, Harinder Singh, and Balaji Srinivasan. 2022. “Investigation of Bias Stability Enhancement Using Frequency Comb Source in Resonant Fiber Optic Gyroscope.” In Optical and Quantum Sensing and Precision Metrology II, edited by Selim M. Shahriar, Jacob Scheuer. SPIE. https://doi.org/10.1117/12.2610072
• Maiuzzo, M. 1970. Compatibility Factors Affecting Concept Develoment of Approach and Landing Guidance System. Defense Technical Information Center. https://doi.org/10.21236/ad0707129
• Majid Msallam, Mohammed, Farah Flayyeh Alkhalid, Seerwan Waleed Jirjees, et al. 2025. “Inertial Sensor Measurement Calibration Using Artificial Intelligence Techniques: A Comparative Study.” Engineering Research Express 7 (4): 045213. https://doi.org/10.1088/2631-8695/ae0f0a
• Majumdar, S. C. 1974. “Some Observations of Distance Dependence in Tropospheric Propagation beyond Radio Horizon.” Radio and Electronic Engineer 44 (2): 63. https://doi.org/10.1049/ree.1974.0016
• Makaron, V., and Yu. Fedyayev. 1996. “Organization of Working Process in Liquefied Air Cycle Rocket-Ramjet Engine.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4522. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4522
• Makeich, G. S., and I. A. Kryukov. 2018. “Aerodynamics and Flight Dynamics Simulation of Basic Finner Supersonic Flight in Aeroballistic Experiment.” Journal of Physics: Conference Series 1009: 012009. https://doi.org/10.1088/1742-6596/1009/1/012009
• Makowski, J. 1964. “In-Flight Recording as a Maintenance Tool for Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-635
• Malan, Pieter J., Jacobus A. Engelbrecht, and Herman A. Engelbrecht. 2016. “Angle of Attack Upset Detection for Passenger Airliners Using Classification of Anemometric and Inertial Sensor Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3847
• Malay, Benjamin P. 2001. Celestial Navigation on the Surface of Mars. Defense Technical Information Center. https://doi.org/10.21236/ada390109
• Malek, Albert. 1992. “H2 Fueled Flightweight Ramjet Construction and Test.” In NASA. Lewis Research Center, Rocket-Based Combined-Cycle (RBCC) Propulsion Technology Workshop. Tutorial Session. https://ntrs.nasa.gov/citations/19920012288
• Malfa, E., L. Guarino, and L. Visintini. 1991. “Application of Euler Equations to Computation of Vortex Flow on Wing-Body and Close-Coupled Wing-Body-Canard Configurations.” In 9th Applied Aerodynamics Conference. AIAA 1991-3306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3306
• Malik, Dennis F. 1976. Storage Reliability of Missile Materiel Program. Igniters and Safe and Arm Device Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada026938
• Malinovsky, I. M., V. G. Nesterenko, and I. G. Ivanov. 2021. “Research and Optimization of Axial Gas Forces in Turbines of Turbojet Bypass Engines with Afterburner Combustion Chamber.” Journal of Physics: Conference Series 1925 (1): 012057. https://doi.org/10.1088/1742-6596/1925/1/012057
• Malkin, Roy. 2013. “Understanding the Accuracy of Astro Navigation.” Journal of Navigation 67 (1): 63–81. https://doi.org/10.1017/s0373463313000520
• Malmuth, N., C. Wu, and J. Cole. 1986. “Transonic Wave Drag Estimation and Optimization Using the Nonlinear Area Rule.” In 4th Applied Aerodynamics Conference. AIAA 1986-1798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1798
• Mamich, Rachel, Daniel Kucharski, Renato Zanetti, et al. 2024. “Navigation Using Serendipitous Star-Tracker Observations and on-Board Data Processing.” In Advances in the Astronautical Sciences. Springer International Publishing. https://doi.org/10.1007/978-3-031-51928-4_36
• Mandal, Tanmay, and Yu Gu. 2016. “Online Pilot Model Parameter Estimation Using Sub-Scale Aircraft Flight Data.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0636
• Manerikar, Ninad. n.d. “Visual-Inertial Sensor Fusion and State Estimation for the Navigation of Autonomous Vehicles.” PhD diss., Université Côte d’Azur. https://doi.org/10.70675/2fb94a1cz8915z4e69z8953z6e3defef1de5
• Mangold, Ulrich. 1997. “Theory and Performance Prediction for Continuous Vector Gravimetry Based on a DGPS Augmented Rate Bias Inertial Navigation System and a Star Tracker.” Navigation 44 (3): 329–45. https://doi.org/10.1002/j.2161-4296.1997.tb02352.x
• Mani, Mori, Ben Rider, Anthony Sclafani, et al. 2010. “RANS Technology for Transonic Drag Prediction; a Boeing Perspective of the 4th Drag Prediction Workshop.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4221
• Mann, M. J., and C. E. Mercer. 1986. Forward-Swept Wing Configuration Designed for High Maneuverability by Use of a Transonic Computational Method. NASA-TP-2628. NASA. https://ntrs.nasa.gov/citations/19870002269
• Manning, Valerie, and Ilan Kroo. 1999. “Multidisciplinary Optimization of a Natural Laminar Flow Supersonic Aircraft.” In 17th Applied Aerodynamics Conference. AIAA 1999-3102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3102
• Manoj Prabakar, S., and T. M. Muruganandam. 2019. “Experimental Investigations of a Diffuser Start/Unstart Characteristics for Two Stream Supersonic Wind Tunnel.” In 31st International Symposium on Shock Waves 2. Springer International Publishing. https://doi.org/10.1007/978-3-319-91017-8_139
• Manoni, L., and G. Sonneman. 1966. Study of Celestial/inertial Test Facility Final Report. NASA-CR-80007. NASA. https://ntrs.nasa.gov/citations/19670009369
• Manoussakis, Gerassimos, and R. Korakitis. 2020. Local Determination of the Components of the Deflection of the Vertical Using Gravitational Potential Parameters at a Neighboring Point. https://doi.org/10.5194/egusphere-egu2020-20090
• Mao, Ning, An Li, Jiangning Xu, et al. 2024. “Adaptive Gravity-Aided Inertial Navigation Based on Characteristic Analysis of Marine Gravity Anomaly from Satellite Altimetry.” IEEE Transactions on Geoscience and Remote Sensing 62: 1–13. https://doi.org/10.1109/tgrs.2024.3428492
• Mao, Hui, Huilian Ma, and Zhonghe Jin. 2010. “Resonator Micro-Optic Gyroscope Based on the Double Phase Modulation Technique.” In Conference on Lasers and Electro-Optics 2010. OSA. https://doi.org/10.1364/cleo.2010.jwa52
• Maples, Dupree. 1979. Aerodynamic Heating of Conventional Weapons. Defense Technical Information Center. https://doi.org/10.21236/ada069807
• Marchetti Tavares, Yuri, and Jacques Waldmann. 2021. “Parameter-Dependent Surface-to-Air Missile Autopilot Design.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-1829
• Marcus, Jean. 1966. “The Guidance of Missiles by Radio Remote-Control.” In Radio Remote-Control and Telemetry and their Application to Missiles. Elsevier. https://doi.org/10.1016/b978-1-4832-0086-6.50010-2
• Mardoc, V. 1970. “Distortion and Turbulence Interaction: A Method for Evaluating Engine/inlet Compatibility.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-632
• Margolis, Kenneth, Frank S. Malvestuto Jr., and Peter J. Maxie Jr. 1958. Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement. NACA-TN-4120. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930084830
• Maria-Agneta, Balint, and Balint Stef. 2011. “Oscillation Susceptibility of an Unmanned Aircraft Whose Automatic Flight Control System Fails.” In Advances in Flight Control Systems. InTech. https://doi.org/10.5772/14936
• Mark, H., C. T. Norgren, and E. V. Zettle. 1954. Combustion Performance of Two Experimental Turbojet Annular Combustors at Conditions Simulating High-Altitude Supersonic Flight. NACA-RM-E54A15. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19630003987
• Markhotok, Anna. 2021. “Wave Drag Modification in the Presence of Discharges.” In Aerodynamics. IntechOpen. https://doi.org/10.5772/intechopen.86858
• Marlow, Michael. 2003. “Highly Operable Propulsion for Reusable Launch Vehicle Applications.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5281
• Marner, Gene R. 1959. “Automatic Radio-Celestial Navigation.” Journal of Navigation 12 (3–4): 249–59. https://doi.org/10.1017/s0373463300031076
• Marquet, L. C. 1986. “The Directed Energy Program for Ballistic Missile Defense.” In SPIE Proceedings, vol. 0551, edited by Jacques E. Ludman. SPIE. https://doi.org/10.1117/12.948983
• Marshall, J. G., L. Xu, J. Denton, and J. W. Chew. 2000. “Prediction of Low Engine Order Inlet Distortion Driven Resonance in a Low Aspect Ratio Fan.” In Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education. American Society of Mechanical Engineers. https://doi.org/10.1115/2000-gt-0374
• Martens, Mats, and Maarten Uijt de Haag. 2023. “Cooperative Swarm Geometry Optimization for Assured Navigation with Range Radios in GNSS-Denied Environments.” In ENC 2023. MDPI. https://doi.org/10.3390/enc2023-15418
• Martin, J. A. 1977. “Ramjet Propulsion for Single-Stage-to-Orbit Vehicles.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19780039934
• Martin, J. 1997. “Range and Doppler Accuracy Improvement for Pulse Doppler Radar.” In Radar Systems (RADAR 97), vol. 1997. IEE. https://doi.org/10.1049/cp:19971713
• Martin, Jorge M. 2004. Modeling an Interferometric Fiber Optic Gyroscope. Defense Technical Information Center. https://doi.org/10.21236/ada429120
• Martin, James. 2006. “The Triplet Reusable Launch Vehicle Concept.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4960
• Martin, Henry, Paul Groves, and Mark Newman. 2016. “The Limits of in-Run Calibration of MEMS Inertial Sensors and Sensor Arrays: In-Run Calibration Limits of Inertial Sensors.” Navigation 63 (2): 127–43. https://doi.org/10.1002/navi.135
• Martin, Ainsley, Gavin Stay, Abigail Lingel, and Douglas Fontes. 2024. “Image Analysis of the Dynamics of Reusable Launch Vehicle.” In Volume 7: Engineering Education. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2024-142760
• Martin, G. L., and K. B. Walkley. 1980. Aerodynamic Design and Analysis of the AST-204, AST-205, and AST-206 Blended Wing-Fuse Large Supersonic Transport Configuration Concepts. NASA-CR-159223. NASA. https://ntrs.nasa.gov/citations/19800011750
• Martine, J. E. 1983. Relating Geoid Anomalies, Gravity Anomalies and Ocean Topography. Defense Technical Information Center. https://doi.org/10.21236/ada140112
• Martos, Borja, Paul Kiszely, and John Foster. 2011. “Flight Test Results of a GPS-Based Pitot-Static Calibration Method Using Output-Error Optimization for a Light Twin-Engine Airplane.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6669. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6669
• Martynenko, Yu. G. 1970. Electrostatic Gyroscope Drift Caused by Rotor Asphericity. NASA-CR-112644. NASA. https://ntrs.nasa.gov/citations/19700026693
• Maruyama, Daigo, Kisa Matsushima, Kazuhiro Kusunose, and Kazuhiro Nakahashi. 2006. “Aerodynamic Design of Biplane Airfoils for Low Wave Drag Supersonic Flight.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3323. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3323
• Marvin, I. 1968. “Integrated Math Modeling for Turbofan and Supersonic Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-648
• Marwaha, Monika, John Valasek, and Puneet Singla. 2008. “GLOMAP Approach for Nonlinear System Identification of Aircraft Dynamics Using Flight Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6895. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6895
• Mascitti, V. R. 1977. A Preliminary Study of the Performance and Characteristics of a Supersonic Executive Aircraft. NASA-TM-74055. NASA. https://ntrs.nasa.gov/citations/19780005097
• Mascitti, V. R., and D. J. Maglieri. 1979. Noise and Performance Calibration Study of a Mach 2.2 Supersonic Cruise Aircraft. NASA-TM-80043. NASA. https://ntrs.nasa.gov/citations/19790013698
• Masek, R. V., D. Hender, and J. A. Forney. 1973. “Evaluation of Aerodynamic Heating Uncertainties for Space Shuttle.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730051552
• Maskell, Craig. n.d. “An Extended Kalman Filter Integrated Navigation System for the N.A.E. Convair 580 Research Aircraft.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1982-00664
• Mason, Homer P. 1953. Flight Test Results of Rocket-Propelled Buffet-Research Models Having 45 Degree Sweptback Wings and 45 Degree Sweptback Tails Located in the Wing Chord Plane. NACA-RM-L53I10. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050041783
• Mason, W. 1982. “Wing-Canard Aerodynamics at Transonic Speeds: Fundamental Considerations on Minimum Drag Spanloads.” In 20th Aerospace Sciences Meeting. AIAA 1982-97. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-97
• Mason, W. 1991. “A Three-Dimensional Inverse Method for Supersonic and Hypersonic Body Design.” In 9th Applied Aerodynamics Conference. AIAA 1991-3325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3325
• Mason, David M. 2009. Directed Energy Weapon System for Ballistic Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada540023
• Mason, Homer P., and William N. Gardner. 1952. An Application of the Rocket-Propelled-Model Technique to the Investigation of Low-Lift Buffeting and the Results of Preliminary Tests. NACA-RM-L52C27. NASA. https://ntrs.nasa.gov/citations/19930087249
• Mason, W., and Jaewoo Lee. 1990. “On Optimal Supersonic/hypersonic Bodies.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3072. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3072
• Mason, W., and D. Wedekind. 1970. “Prediction and Measurement of Strapdown Inertial Measurement Unit Performance on Lunar Missions.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1028
• Masson, Christian, Charles Veilleux, and Ion Paraschivoiu. 1999. “Drag Predictions Using Euler Solutions of 2D and 3D Transonic Flows.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-527
• Masters, George. 1986. Derivation of the Radar Range Equation for a Pulse-Doppler Radar with Range and Velocity Gating and Coherent and Noncoherent Pulse Integration. Defense Technical Information Center. https://doi.org/10.21236/ada170354
• Masud, Jehanzeb, I. Arif, and Zakria Toor. 2017. “Composite Analysis and Characterization of Exhaust Effects on Aerodynamic Behavior of a Supersonic Aircraft.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0269
• Masud, Jehanzeb, and Omar Khan. 2015. “Evaluating an Experimental Streamlined Fairing for a Diverter Less Supersonic Inlet (DSI) Equipped Aircraft.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0248
• Masud, Jehanzeb, and Omer Khan. 2016. “Evaluating an Experimental Streamlined Fairing for a Diverterless Supersonic Inlet (DSI) Equipped Aircraft.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1566
• Masud, Jehanzeb, Tauha I. Khan, and Zakria G. Toor. 2018. “Analysis of High Alpha Aerodynamic Characteristics of a Supersonic Aircraft.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-2057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2057
• Masuda, Y. 1999. “Low Cost Gyrocompass Using Fiber Optic Gyroscope.” In 13th International Conference on Optical Fiber Sensors. SPIE. https://doi.org/10.1117/12.2302022
• Mathavaraj, S., and Radhakant Padhi. 2020. “Optimally Allocated Nonlinear Robust Control of a Reusable Launch Vehicle during Re-Entry.” Unmanned Systems 08 (01): 33–48. https://doi.org/10.1142/s230138502050003x
• Matheny, Aaron, and Isaac Smith. 2026. “Aerothermodynamic Analysis and High-Speed Schlieren Imaging of an Undergraduate-Designed Hypersonic Glide Vehicle.” In 2026 Regional Student Conferences. AIAA 2026-112162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-112162
• Mathijssen, Tiemo, Willem Bannink, and Fulvio Scarano. 2009. “Investigation of a Sharp-Edged Delta Wing in a Supersonic Flow Using Stereo PIV.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-3896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3896
• Matsumoto, Shuichi, Yoshinori Kondoh, Takane Imada, Satoshi Kobayashi, and Noboru Motoyama. 2015. “IMU-DM Integrated Navigation and Terminal Reentry Guidance for Accurate Guided Reentry Flight.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-1772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1772
• Matthews, J., M. Gneses, and D. Pasik. 1981. “Azimuth Determination Using a Low Noise Ring Laser Gyro Inertial Measurement Unit.” In Guidance and Control Conference. AIAA 1981-1747. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1747
• Matthews, Nathanael P., Simon A. Prince, Romain Seppey, and Zeeshan A. Rana. 2025. “The Application of Rapid Aerodynamic Prediction Techniques to Supersonic Aircraft.” In AIAA SCITECH 2025 Forum. AIAA 2025-2831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2831
• Matthews, A., and H. Welter. 1989. “Cost-Effective, High-Accuracy Inertial Navigation.” Navigation 36 (2): 157–72. https://doi.org/10.1002/j.2161-4296.1989.tb00989.x
• Mattin, R. B. 1968. “Problems of Guidance, in Particular— Inertial Guidance.” Aeronautical Journal 72 (691): 587–95. https://doi.org/10.1017/s0001924000084621
• Mattson, A. T., and R. S. Osborne. 1955. “Application and Limitations of the Area Rule.” In NACA Conf. on Aerodyn. of High Speed Aircraft. https://ntrs.nasa.gov/citations/19740075322
• Matveev, S. S., A. Yu. Truschinsky, and V. T. Yankovsky. 2025. “Comprehensive Measurement Processing of a Strapback Inertial Navigation System and a Two-Channel Coherent Radio Altimeter Aircraft.” Science Intensive Technologies: 35–40. https://doi.org/10.18127/j19998465-202504-04
• Maunder, D. 1979. “AFFTC Parameter Identification Experiencefor Aircraft Flight Characteristics.” In Aircraft Systems and Technology Meeting. AIAA 1979-1803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1803
• Maurer, Ricky L. 1995. Near Real-Time Telemetry Utilizing Satellite Communications. Defense Technical Information Center. https://doi.org/10.21236/ada300638
• Mavriplis, D., and D. Levy. 2002. “Transonic Drag Prediction Using an Unstructured Multigrid Solver.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-838
• Maybeck, Peter S. 1973. Wander Azimuth Implementation Algorithm for a Strapdown Inertial System. Defense Technical Information Center. https://doi.org/10.21236/ad0784752
• Mayer, Lee S. 2000. “Simulation of Aircraft Landing Gear Dynamics Using CATIA, CATDADS, DADS and NASTRAN at Cessna Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2000-01-1699
• Mayer, David, and Gerald Paynter. 1994. “Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-580
• Maykapar, G. I. 1968. Aerodynamic Heating of the Lifting Bodies. NASA-CR-97576. NASA. https://ntrs.nasa.gov/citations/19690001128
• Maywald, P. V., and D. K. Beale. 1991. “Development of a Freejet Capability for Evaluating Inlet-Engine Compatibility.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-401
• Mazaheri, K., P. Akbari, and A. Ghafourian. 1999. “Experimental Investigation of Combustion Instability in an Axisymmetric Laboratory Ramjet Engine.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2103. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2103
• Mazzoni, Alex, Ryan Rudy, Ryan Knight, and Jeff Pulskamp. 2021. Investigation of Thermoelastic Damping in Microelectromechanical System (MEMS) Quadruple-Mass Gyroscope (QMG) Designs. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1144809
• McBurney, Paul William. n.d. “Analysis of a GPS Aided Inertial Navigation System Using the Delayed State Kalman Filter.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-8076
• McCabe, James S., and Kyle J. DeMars. 2018. “Robust, Terrain-Aided Landing Navigation through Decentralized Fusion and Random Finite Sets.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1332. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1332
• McCabe, James S., and Kyle J. DeMars. 2019a. “Terrain Relative Navigation with Anonymous Features.” In AIAA Scitech 2019 Forum. AIAA 2019-0923. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0923
• McCabe, James S., and Kyle J. DeMars. 2019b. “Vision-Based, Terrain-Aided Navigation with Decentralized Fusion and Finite Set Statistics.” NAVIGATION 66 (3): 537–57. https://doi.org/10.1002/navi.320
• McCall, G. 1998. Global Air Navigation Systems. Volume 2. Detailed Findings. Defense Technical Information Center. https://doi.org/10.21236/ada367419
• McCartney, Earl J. 1966. “The Ring Laser Inertial Sensor.” Navigation 13 (3): 260–69. https://doi.org/10.1002/j.2161-4296.1966.tb01831.x
• McCarty, J. L., T. J. Yager, and S. R. Riccitiello. 1979. Wear, Friction, and Temperature Characteristics of an Aircraft Tire Undergoing Braking and Cornering. NASA-TP-1569. NASA. https://ntrs.nasa.gov/citations/19800004758
• McClinton, C., A. Rondakov, V. Semenov, and V. Kopehenov. 1991. Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20040110897
• McClure, Wallace. 1998. “Decision Criteria for a Reusable Launch Vehicle Investment Decision.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5139
• McDaniel, Melissa, Christine Evans, and Dan Lesieutre. 2010. “The Effect of Tail Fin Parameters on the Induced Roll of a Canard-Controlled Missile.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4226. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4226
• McDevitt, J. B., and J. V. Rakich. 1966. The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50 Deg. NASA-TM-X-162. NASA. https://ntrs.nasa.gov/citations/19660024050
• McDonald, W. T. 1967. Gyrocompass Spacecraft Attitude Reference. Massachusetts Inst. of Tech. https://ntrs.nasa.gov/citations/19670017203
• McDonald, J. A. 1980. “Aircraft Automatic Landing.” Navigation 27 (1): 23–29. https://doi.org/10.1002/j.2161-4296.1980.tb01396.x
• McDonald, Robert, and Dimitri Mavris. 2000. “Formulation, Realization, and Demonstration of a Process to Generate Aerodynamic Metamodels for Hypersonic Cruise Vehicle Design.” In 2000 World Aviation Conference. AIAA 2000-5559. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5559
• McFall, John C., Jr. 1954. Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-Propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6.0. NACA-RM-L53G22a. NASA. https://ntrs.nasa.gov/citations/19930087765
• McFall, John C., Jr., and James A. Hollinger. 1953. Longitudinal Stability, Control Effectiveness, and Drag Characteristics at Transonic Speeds of a Rocket-Propelled Model of an Airplane Configuration Having an Unswept Tapered Wing of Aspect Ratio 3.0 and NACA 65A004.5 Airfoil Sections. NACA-RM-L52L04. NASA. https://ntrs.nasa.gov/citations/19930087467
• McFarland, Michael, and Anthony Calise. 1996. “Neural-Adaptive Nonlinear Autopilot Design for an Agile Anti-Air Missile.” In Guidance, Navigation, and Control Conference. AIAA 1996-3914. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3914
• McFARLAND, M. B., and C. N. D’Souza. 1995. “Robust Nonlinear Missile Autopilot Design.” In Automatic Control in Aerospace 1994 (Aerospace Control ‘94). Elsevier. https://doi.org/10.1016/b978-0-08-042238-1.50025-2
• McGee, Timothy G., and Uday J. Shankar. 2018. “Sensor Model and Filter Considerations for Terrain Relative Navigation.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1331. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1331
• McGee, L. A., G. L. Smith, D. M. Hegarty, R. B. Merrick, T. M. Carson, and S. F. Schmidt. 1970. Navigation for Space Shuttle Approach and Landing Using an Inertial Navigation System Augmented by Data from a Precision Ranging System or a Microwave Scan Beam Landing Guidance System. NASA-TM-X-62123. NASA. https://ntrs.nasa.gov/citations/19720018866
• McGehee, J. R. 1985. “Active Control Landing Gear for Ground Loads Alleviation.” In AGARD Tech. Evaluation Rept. on the Flight Mech. Symp. on Active Control Systems. https://ntrs.nasa.gov/citations/19850018438
• McGehee, J. R., and H. D. Carden. 1976. A Mathematical Model of an Active Control Landing Gear for Load Control during Impact and Roll-out. NASA-TN-D-8080. NASA. https://ntrs.nasa.gov/citations/19760010002
• McGehee, J., H. Carden, and R. Edson. 1978. “Improved Aircraft Dynamic Response and Fatigue Life during Ground Operations Using an Active Control Landing Gear System.” In Aircraft Systems and Technology Conference. AIAA 1978-1499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1499
• McGehee, J. R., and R. C. Dreher. 1982. Experimental Investigation of Active Loads Control for Aircraft Landing Gear. NASA-TP-2042. NASA. https://ntrs.nasa.gov/citations/19820023445
• McGrath, Brian. 2004. “Subsonic Aerodynamic Fin-Folding Moments for the Tactical Tomahawk Missile Configuration.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5193
• McHenry, Neil, Tanner Hunt, Gregory Chamitoff, and Daniele Mortari. 2019. “Virtual Reality as a Testbed for Star Tracker Algorithms.” In AIAA Scitech 2019 Forum. AIAA 2019-1713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1713
• McKavitt, Thomas P., Jr. 1990. “Parameter Identification Studies on the NASA/Ames Research Center Advanced Concepts Flight Simulator.” PhD diss., Naval Postgraduate School. https://ntrs.nasa.gov/citations/19920001806
• McKay, J. M., and R. B. Noll. 1967. Theoretical Dynamic Analysis of the Landing Loads on a Vehicle with a Tricycle Landing Gear. NASA-TN-D-4075. NASA. https://ntrs.nasa.gov/citations/19670023065
• McKay, J. M., and B. J. Scott. 1961. Landing-Gear Behavior during Touchdown and Runout for 17 Landings of the X-15 Research Airplane. NASA-TM-X-518. NASA. https://ntrs.nasa.gov/citations/19630002687
• McKern, R., and H. Musoff. 1973. “Redundancy Management of Inertial Systems.” In Guidance and Control Conference. AIAA 1973-852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-852
• McKinlay, W. H. 1975. “Advances in Inertial Navigation: Sensor Technology.” Journal of Navigation 28 (4): 407–15. https://doi.org/10.1017/s037346330004217x
• McLain, Timothy, and Randal Beard. 1998. “Nonlinear Optimal Control Design of a Missile Autopilot.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4321. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4321
• McLain, Timothy, and Randal Beard. 1999. “Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-3997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3997
• McLandrich, M. N., and H. E. Rast. 1978. “Fiber Interferometer Gyroscope.” In SPIE Proceedings, vol. 0157, edited by Shaoul Ezekiel, G. E. Knausenberger. SPIE. https://doi.org/10.1117/12.965476
• McLean, D. 1994. “Reconfigurable Flight Control of a Large Flexible Supersonic Aircraft.” In International Conference on Control ‘94, vol. 1994. IEE. https://doi.org/10.1049/cp:19940361
• McMaster, J., and F. Schenk. 1973. “The Development of the F-12 Series Aircraft Manual and Automatic Flight Control System.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-822
• McMichael, Robert D., and Sean M. Blakley. 2022. “Simplified Algorithms for Adaptive Experiment Design in Parameter Estimation.” Physical Review Applied 18 (5): 054001. https://doi.org/10.1103/physrevapplied.18.054001
• McMillin, S. N., and R. M. Wood. 1986. Planform Effects for Low-Fineness Ratio Multibody Configurations at Supersonic Speeds. AIAA PAPER 86-1799. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19860053087
• McNally, B. David, Russell A. Paielli, Ralph E. Bach Jr., and David N. Warner Jr. 1992. “Flight Evaluation of Differential GPS Aided Inertial Navigation Systems.” In AGARD, Integrated and Multi-Function Navigation. https://ntrs.nasa.gov/citations/19930013601
• McNamara, Jack, Adam Culler, and Andrew Crowell. 2009. “Aerothermoelastic Modeling Considerations for Hypersonic Vehicles.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7397
• McNamara, Jack, and Peretz Friedmann. 2006. “Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8058. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8058
• McNamara, Jack, and Peretz Friedmann. 2007. “Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-2013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2013
• McNamara, J., Peretz Friedmann, K. Powell, B. Thuruthimattam, and R. Bartels. 2005a. “Aeroelastic and Aerothermoelastic Vehicle Behavior in Hypersonic Flow.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3305. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3305
• McNamara, Jack, Peretz Friedmann, Kenneth Powell, Biju Thuruthimattam, and Robert Bartels. 2005b. “Three-Dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow.” In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. AIAA 2005-2175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-2175
• McNamara, Jack, Biju Thuruthimattam, Peretz Friedmann, Kenneth Powell, and Robert Bartels. 2004. “Hypersonic Aerothermoelastic Studies for Reusable Launch Vehicles.” In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. AIAA 2004-1590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1590
• McPherson, R. 1977. “YC-14 Flight Test Results.” In Aircraft Systems and Technology Meeting. AIAA 1977-1259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1259
• McPherson, B. W., B. F. Walls, and J. B. White. 1976. Redundant Strapdown Laser Gyro Navigation System. IBM Corp. https://ntrs.nasa.gov/citations/19760064262
• McTaggart, Lester E. 1973. Feasibility of Ramjet Engine Test Capability on the Holloman Sled Track. Defense Technical Information Center. https://doi.org/10.21236/ad0769043
• McVey, Francis D., John V. Rejeske, and Edward J. Phillips. 1969. Experimental Evaluation of Inlet Drag Characteristics in the Transonic Mach Number Regime. Defense Technical Information Center. https://doi.org/10.21236/ad0861763
• Meacham, Michael B., Andrew Kennett, Derik J. Townsend, and Benjamin Marti. 2013. “Rocket Sled Propelled Testing of a Supersonic Inflatable Aerodynamic Decelerator.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1351
• Mease, Kenneth, P. Teufel, H. Schoenenberger, D. Chen, and S. Bharadwaj. 1999. “Re-Entry Trajectory Planning for a Reusable Launch Vehicle.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4160
• Medina, Jose A., Harinkumar Patel, and Bernd Chudoba. 2021. “2D Mixed-Compression Inlet Sizing of Supersonic Vehicles.” In AIAA Aviation 2021 Forum. AIAA 2021-2780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2780
• Medzorian, John P. 1999. “An Investigation of Landing Gear Shimmy: Tire Models, Tire Test Methodologies, Analysis, and Parameter Studies.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/1999-01-5527
• Mehalic, Charles. 1988. “Effect of Spatial Inlet Temperature and Pressure Distortion on Turbofan Engine Stability.” In 24th Joint Propulsion Conference. AIAA 1988-3016. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-3016
• Meher-Hornji, Cyrus B. 1997. “The Development of the Whittle Turbojet.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/97-gt-528
• Mehra, R. K. 1968. Application of Statistical Smoothing Techniques to Inertial Navigation. NASA-CR-97104. NASA. https://ntrs.nasa.gov/citations/19680026912
• Mehra, R. K., and N. K. Eupta. 1975. “Status of Input Design for Aircraft Parameter Identification.” In AGARD Methods for Aircraft State and Parameter Identification. https://ntrs.nasa.gov/citations/19750021936
• Mei, Sun. 1996. The Use of GPS for Evaluating Inertial Measurement Unit Errors,. Defense Technical Information Center. https://doi.org/10.21236/ada306521
• Mei, Chuan Zhi, Lin Hua Piao, and Bao Li Zhang. 2013. “Study on Fluidic Gyroscope Zero Temperature Compensation Method.” Advanced materials research 756-759: 4225–28. https://doi.org/10.4028/www.scientific.net/amr.756-759.4225
• Meidunas, Eduardo. 2008. “Estimating Elliptical Error Probable Confidence Intervals for Weapon System Performance Evaluation.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1623
• Meisl, C. 1986. “Life Cycle Cost Considerations for Launch Vehicle Liquid Propellant Rocket Engines.” In 22nd Joint Propulsion Conference. AIAA 1986-1408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1408
• Meissinger, Hans. 1963. “Lunar Landing by Command Guidance in the Presence of of Transmissiontime-Delay.” In Guidance and Control Conference. AIAA 1963-346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-346
• Melick, H., Jr., and W. Simpkin. 1972. “A Unified Theory of Inlet/engine Compatibility.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1115
• “MEMS Inertial Sensors.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch7
• Meng, Lin, Yang Gao, Jiachao Zhang, and Liangbao Jiao. 2022a. “Automatic Longitudinal Landing Control of FanWing.” In 2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022), edited by Xuexia Ye. SPIE. https://doi.org/10.1117/12.2635153
• Menon, S. 1992. Active Control of Combustion Instability in a Ramjet Using Large-Eddy Simulations. Defense Technical Information Center. https://doi.org/10.21236/ada255226
• Menon, P., V. Iragavarapu, E. Ohlmeyer, P. Menon, V. Iragavarapu, and E. Ohlmeyer. 1997. “Nonlinear Missile Autopilot Design Using Time-Scale Separation.” In Guidance, Navigation, and Control Conference. AIAA 1997-3765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3765
• Menon, P. K., V. R. Iragavarapu, G. Sweriduk, and E. J. Ohlmeyer. 1999. Software Tools for Nonlinear Missile Autopilot Design. Defense Technical Information Center. https://doi.org/10.21236/ada436304
• Ménou, Hubert. n.d. “Hierarchical Emergency Guidance Optimization for Reusable Tossback Vehicle Landing.” PhD diss., Université Paris sciences et lettres. https://doi.org/10.70675/01a02ab5zdcb3z4b95zb05czfea1b906f3dc
• Mercado-Ravell, Diego Alberto. n.d. “Autonomous Navigation and Teleoperation of Unmanned Aerial Vehicles Using Monocular Vision.” PhD diss., Compiègne. https://doi.org/10.70675/458fa1dbz4811z44c3zaa6az8c415b592611
• Merchant, Ali, Umair Ashun, James Paduano, and Mark Drela. 2003. “Design of an Actively Stabilized, near-Isentropic Supersonic Inlet.” In 16th AIAA Computational Fluid Dynamics Conference. AIAA 2003-4096. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4096
• Merhav, S. 1979. Low-Cost Inertial Navigation for Moderate-g Missions. NASA-TM-78611. NASA. https://ntrs.nasa.gov/citations/19790024034
• Merhav, S. J. 1982. Less-Costly Inertial Guidance. ARC-11257. National Research Council. https://ntrs.nasa.gov/citations/19810000049
• Meriwether, H. D., and I. E. Harris. 1962. Landing Loads Investigation Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ad0404420
• Merkle, T. 1959. The Nuclear Ramjet Propulsion System. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4217328
• Merkli, Peter E. 1975. Pressure Recovery in Rectangular Adjustable Area Supersonic Diffusers. Defense Technical Information Center. https://doi.org/10.21236/ada033630
• Merkulov, I. A. 1967. The First Experimental Investigations of Ramjet Engines by ‘‘GIRD’‘. Holman (John F.) and Co., Inc. https://ntrs.nasa.gov/citations/19680004101
• Merkulov, Igor A. 1976. “Basic Stages in the Development of the Theory of Ramjet Engines (RJE).” In Essays on the History of Rocketry and Astronautics: Proceedings of the Third through the Sixth History Symposia of the International Academy of Astronautics, volume 1. https://ntrs.nasa.gov/citations/19770026103
• Mermagen, W. H. 1964. High ‘g’ Telemetry for Ballistic Range Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ad0444246
• Mermagen, William H., and Rao J. Yalamanchili. 1983. First Diagnostic Tests of a 75mm Solid-Fuel Ramjet Tubular Projectile. Defense Technical Information Center. https://doi.org/10.21236/ada130598
• Mertens, J., K. Klevenhusen, and H. Jakob. 1986. “Accurate Transonic Wave Drag Prediction Using Simple Physical Models.” In 24th Aerospace Sciences Meeting. AIAA 1986-512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-512
• Meshkovsky, I. K., V. Ye. Strigalev, G. B. Deineka, V. G. Peshekhonov, D. V. Volynsky, and A. A. Untilov. 2011. “Three-Axis Fiber-Optic Gyroscope: Development and Test Results.” Gyroscopy and Navigation 2 (4): 208–13. https://doi.org/10.1134/s2075108711040122
• Messinger, Martin, and Howard E. Parker. 1963. The Dynamics of Gyroscope Damping for Geocentric Attitude Control. Defense Technical Information Center. https://doi.org/10.21236/ad0419083
• Metha, Deval Samirbhai. n.d. “A Reliable and Fast Lost-in-Space Mode Star Tracker.” PhD diss., Nanyang Technological University. https://doi.org/10.32657/10220/47620
• “A Method for Determining the Performance of a Precision Inertial Guidance System.” 1979. In Guidance and Control Conference. AIAA 1979-1891. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1891
• “Methods for Reducing Data Uncertainty in Flight Test Data.” 2003. In Flight Testing of Fixed-Wing Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600861840.0019.0028
• Metodiev, Konstantin. 2024. “System Identification of Aircraft Longitudinal Motion by Means of Flight Simulator Data.” Aerospace Research in Bulgaria 36: 115–23. https://doi.org/10.3897/arb.v36.e10
• Metrikin, V. S., and M. A. Peisel’. 2009. “Investigation of Landing Gear Wheel Shimmy Taking into Account Damper Frequency Characteristics.” Russian Aeronautics (Iz VUZ) 52 (2): 240–44. https://doi.org/10.3103/s1068799809020172
• Mettler, Edward, and Fred Y. Hadaegh. 1992. “Space Micro-Guidance and Control: Applications and Architectures.” In In: Sensors and sensor systems for guidance and navigation II; Proceedings of the Meeting, Orlando, FL, Apr. 22, 23, 1992 (A93-28151 10-35). https://ntrs.nasa.gov/citations/19930044169
• Metzger, E. H. 1970. “Temperature Compensation versus Temperature Control of Inertial Instruments.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19710031763
• Metzger, E. 1977. “Recent Gravity Gradiometer Developments.” In Guidance and Control Conference. AIAA 1977-1081. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1081
• Metzger, E., and A. Jircitano. 1975. “Inertial Navigation Performance Improvement Using Gravity Gradient Matching Techniques.” In Guidance and Control Conference. AIAA 1975-1092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1092
• Metzger, E., A. Jircitano, and C. Affleck. 1976. Satellite Borne Gravity Gradiometer Study. NASA-CR-144822. NASA. https://ntrs.nasa.gov/citations/19770007712
• Metzger, Juergen, Jan Wendel, Gert Trommer, Franz Tumbraegel, and Bernd Taddiken. 2004. “Hybrid Terrain Referenced Navigation System Using Kalman Filters and Comparison Techniques.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5126
• Metzger, Juergen, Katrin Wisotzky, Jan Wendel, and Gert Trommer. 2005. “Sigma-Point Filter for Terrain Referenced Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6068
• Meyer, Rudolf X. 1938. Magnetohydrodynamics and Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0608024
• Meyer, C. A. 1947. “Characteristics of Turbojet Engines at High Flight Speeds.” Journal of Fluids Engineering 69 (3): 237–43. https://doi.org/10.1115/1.4017361
• Meyer, R. E. 1957. “On the Measurement of Supersonic Aerofoil Drag by Pressure Traverse.” Aeronautical Quarterly 8 (2): 123–44. https://doi.org/10.1017/s0001925900010441
• Meyer, George, and G. Allan Smith. 1992. Automatic Flight Controller with Model Inversion. ARC-12849. NASA Ames Research Center, Moffett Field, CA. https://ntrs.nasa.gov/citations/19920000400
• Meyers, B. C., and Nelson H. Weiderman. 1988. Functional Performance Specification for an Inertial Navigation System. Defense Technical Information Center. https://doi.org/10.21236/ada204850
• Meyerson, Robert E. 1998. “Development Status of the Kistler Aerospace K-1 Reusable Launch Vehicle.” In Space 98. American Society of Civil Engineers. https://doi.org/10.1061/40339(206)21
• Meyerson, Robert E. 2001a. “Space Shuttle Orbital Drag Parachute Design.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20110001620
• Meyerson, Robert. 2001b. “Space Shuttle Orbiter Drag Parachute Design.” In 16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2001-2051. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2051
• Miao Ling-juan, Liu Xiao-guang, Lan Chun-yun, and Dai Ya-ping. 2002. “Derivation of Nonlinear Error Equations of Strapdown Inertial Navigation System Using Quaternion.” In Proceedings of the 41st SICE Annual Conference. SICE 2002., vol. 1. Soc. Instrument & Control Eng. (SICE). https://doi.org/10.1109/sice.2002.1195483
• Michal, David H. 1950. Free-Flight Investigation of the Static and Dynamic Longitudinal Stability Characteristics of 1/3.7-Scale Rocket-Powered Models of the Bell MX-776A. NACA-RM-SL50B23. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050028504
• Michal, David H., and Grady L. Mitcham. 1949. Preliminary Results of a Free-Flight Investigation of the Static Stability and Aileron Control Characteristics of 1/6 Scale Models of the Bell MX-776. NACA-RM-SL9D21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20010062500
• Michalski, Sydney, and Alan Johnson. 2007. “Logistics Manpower Requirements for Ground Support of a Reusable Military Launch Vehicle.” In AIAA SPACE 2007 Conference & Exposition. AIAA 2007-6273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6273
• Mickle, M. C., and J. J. Zhu. n.d.-b. “Simulation Results for Missile Autopilot Design Based on Extended Mean Assignment.” In Proceedings of 28th Southeastern Symposium on System Theory. IEEE Comput. Soc. Press. https://doi.org/10.1109/ssst.1996.493483
• Mickola, Richard H. 1961. Performance Summary of the Supersonic Diffuser and Its Application to Altitude Testing of Captive Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ad0256347
• Middleton, W. D., and J. L. Lundry. 1975. Aerodynamic Design and Analysis System for Supersonic Aircraft. Part 1: General Description and Theoretical Development. NASA-CR-2520. NASA. https://ntrs.nasa.gov/citations/19750010113
• Middleton, W. D., and J. L. Lundry. 1976. A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 1: General Description and Theoretical Development. NASA-CR-2715. NASA. https://ntrs.nasa.gov/citations/19760021073
• Middleton, W. D., and J. L. Lundry. 1980a. A System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 1: General Description and Theoretical Development. NASA-CR-3351. NASA. https://ntrs.nasa.gov/citations/19810006455
• Middleton, W. D., and J. L. Lundry. 1980b. A System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 4: Test Cases. NASA-CR-3354. NASA. https://ntrs.nasa.gov/citations/19810007462
• Middleton, W. D., J. L. Lundry, and R. G. Coleman. 1975. Aerodynamic Design and Analysis System for Supersonic Aircraft. Part 3: Computer Program Description. NASA-CR-2522. NASA. https://ntrs.nasa.gov/citations/19750010114
• Middleton, W. D., J. L. Lundry, and R. G. Coleman. 1980. A System for Aerodynamic Design and Analysis of Supersonic Aircraft. Part 2: User’s Manual. NASA-CR-3352. NASA. https://ntrs.nasa.gov/citations/19810005409
• Middleton, W. D., J. L. Lundry, and R. G. Coleman. 1982. Aerodynamics of Supersonic Aircraft. LAR-12857. The Boeing Co. https://ntrs.nasa.gov/citations/19810000199
• Mihigo, Jean Paul, Donald J. Malloy, Charles R. Vining, et al. 2009. “The Need to Address Aeromechanical T&E Requirements during Engine Inlet Distortion Testing.” In Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Education; Electric Power; Awards and Honors. ASMEDC. https://doi.org/10.1115/gt2009-59009
• Mikhail, Ameer G. 1979. Numerical Solution of a Supersonic Nozzle Afterbody Flow with Jet Exhaust. Defense Technical Information Center. https://doi.org/10.21236/ada076116
• Mikhail, Ameer. 1989. “Spike-Nosed Projectiles: Computations and Dual Flow Modes in Supersonic Flight.” In 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1989-1820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1820
• Miki, Hajime, Masaharu Kameda, and Yasushi Watanabe. 2014. “Low Drag Design and Aerodynamic Performance Evaluation of Supersonic Air Inlet.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3798. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3798
• Miklus, Kenneth J., Frank Kissh, and David J. Flynn. 1993. “Star Tracker Operation in a High Density Proton Field.” In NASA. Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1992. https://ntrs.nasa.gov/citations/19930015510
• Milder, N. L. 1971. Potential Star Tracker Interference from Radiation Produced by Mercury Bombardment Thrusters. NASA-TM-X-67858. NASA. https://ntrs.nasa.gov/citations/19710019341
• Miles, Richard B., and Christopher Limbach. 2015. “Adjoint Optimization of the Spatial Profile of Steady Energy Deposition for Supersonic Drag Reduction.” In 45th AIAA Fluid Dynamics Conference. AIAA 2015-2466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2466
• Miley, Stan, Michael Fisher, Bianca Anderson, and Robert Geenen. 1992. “Measurement of Attachment-Line Location in a Wind-Tunnel and in Supersonic Flight.” In 6th AIAA Biennial Flight Test Conference. AIAA 1992-4089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4089
• Milgram, D. L., and C. M. Bjorklund. 1980. “3-D Model Matching for Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959151
• Milholen, William, and Lewis Owens. 2005. “On the Application of Contour Bumps for Transonic Drag Reduction (Invited).” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-462
• Millard, W., W. Barton, and P. Hoekstra. 1982. “Development Flight Test Results and Performance Capabilities for theMalemute II Rocket Motor.” In 6th Sounding Rocket Conference. AIAA 1982-1726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1726
• Miller, J. E. 1965. Inertial Measurement Units and Pulse Torquing. Massachusetts Inst. of Tech. https://ntrs.nasa.gov/citations/19660019470
• Miller, Christopher J. 1994. Holographic Testing of Composite Propfans for a Cruise Missile Wind Tunnel Model. NASA-TM-105271. NASA. https://ntrs.nasa.gov/citations/19940019072
• Miller, C. D., and I. I. Pinkel. 1973. Aluminum Runway Surface as Possible Aid to Aircraft Braking. NASA-TN-D-7186. NASA. https://ntrs.nasa.gov/citations/19730009313
• Miller, J. E., and J. L. Sitomer. 1968. “A Body-Mounted Inertial System for Extended Manned Space Missions.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19680048143
• Miller, Daniel N., and Brian R. Smith. 2003. “CFD-Based Simulation of Inlet Unstart Phenomena: Toward Supersonic Inlet Flow Control Techniques.” In Volume 2: Symposia, Parts A, B, and C. ASMEDC. https://doi.org/10.1115/fedsm2003-45471
• Miller, Scott, and Jae Son. 2001. “On-Orbit Resolution of Radiation Induced Loss-of-Track Anomalies for the CT601 Star Tracker.” In AIAA Space 2001 Conference and Exposition. AIAA 2001-4723. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4723
• Miller, G. K., Jr. 1979. Fixed-Base Simulation Study of Decoupled Longitudinal Controls during Approach and Landing of a Medium Jet Transport in the Presence of Wind Shear. NASA-TP-1519. NASA. https://ntrs.nasa.gov/citations/19790025047
• Milliken, S. 1963. “Feasibility of Large Launch Vehicle Recovery.” In Summer Meeting. AIAA 1963-247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-247
• Milne, Garrett, and Borja Martos. 2012. “Flight Test Results of Efficient Maneuver Development for a GPS-Based Pitot-Static Calibration Method Using Output-Error Optimization.” In 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference. AIAA 2012-2855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2855
• Milwitzky, Benjamin, and Francis E. Cook. 1953. Analysis of Landing-Gear Behavior. NACA-TR-1154. NASA. https://ntrs.nasa.gov/citations/19930092181
• Min, Zhu, Liu Hua-zhang, and Xi Xiao-liang. 2013. “Thermal Characteristic Analysis of Balloon Decoys in Flight Midcourse of Ballistic Missile.” Journal of Applied Sciences 13 (22): 5478–82. https://doi.org/10.3923/jas.2013.5478.5482
• Min, Ke, Zhenqi Sun, Zejun Cai, et al. 2026. “A Physics-Informed Generative Framework for Predicting Symmetry-Plane Unstart Flow Evolution in a Turbine-Based Combined-Cycle Inlet.” Preprint, . https://doi.org/10.2139/ssrn.7133946
• Minaretzis, Chrysostomos, Davide Antonio Cucci, Naser El-Sheimy, Michael G. Sideris, Stéphane Guerrier, and Maria-Pia Victoria-Feser. 2024. “Robust Multi-Signal Estimation Framework with Applications to Inertial Sensor Stochastic Calibration.” Preprint, . https://doi.org/10.36227/techrxiv.170629378.82042843/v1
• Minato, Ryojiro, Takakage Arai, Takehiro Himeno, Hiroaki Kobayashi, Kazuhide Mizobata, and Nobuhiro Tanatsugu. 2005. “Off-Design Performance of Turbojet Engine for Sub-Scale Supersonic Unmanned Plane.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3415
• Minato, Ryojiro, Kazuhide Mizobata, Kazuyuki Higashino, and Nobuhiro Tanatsugu. 2013. “Characteristics of Bio-Ethanol Fueled GG-Cycle Air Turbo Ramjet Engine for Supersonic UAV along Flight Trajectory.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3873
• Minato, Ryojiro, Toyohiko Oota, Kiyoshi Fukutomi, et al. 2007. “Development of Counter Rotating Axial Fan Turbojet Engine for Supersonic Unmanned Plane.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5023
• Minato, Ryojiro, Nobuhiro Tanatsugu, Kazuhide Mizobata, Takayuki Kojima, and Hiroaki Kobayashi. 2006. “Development of Turbojet Engine for Supersonic Unmanned Plane.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-8145. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-8145
• Miner, D. D., and B. B. Gloss. 1975. Flow Visualization Study of Close-Coupled Canard Wing and Strake Wing Configuration. NASA-TM-X-72668. NASA. https://ntrs.nasa.gov/citations/19750013175
• Minervino, Mauro, and Renato Tognaccini. 2023. “Wave Drag and Vorticity in Two-Dimensional Viscous and Inviscid Flows.” In AIAA SCITECH 2023 Forum. AIAA 2023-1032. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1032
• Minford, W. J., G. A. Bogert, and F. T. Stone. 1987. “Ti:LiNbO 3 Components for a Fiber Gyroscope.” In SPIE Proceedings, vol. 0719, edited by Eric Udd. SPIE. https://doi.org/10.1117/12.937550
• Minford, William J., Ramon DePaula, and Gail A. Bogert. 1988. “Interferometric Fiber Optic Gyroscope Using a Novel 3x3 Integrated Optic Polarizer/Splitter.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1988.fbb2
• Minford, W. J., F. T. Stone, B. R. Youmans, and R. K. Bartman. 1990. “Fiber Optic Gyroscope Using an Eight-Component LiNbO 3 Integrated Optic Circuit.” In SPIE Proceedings, vol. 1169, edited by Ramon P. DePaula, Eric Udd. SPIE. https://doi.org/10.1117/12.963047
• “Miniature Inertial Measurement Unit.” 2018. In Space Microsystems and Micro/nano Satellites. Elsevier. https://doi.org/10.1016/b978-0-12-812672-1.00007-2
• Minor, John. 1965. “Low-Cost Strapdown Inertial Systems.” In Guidance Control Conference. AIAA 1965-1215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1215
• Minuti, Rafael. 2026a. “Accounting for Shared Reusable Launch Capacity a Mission-Adjusted Cost Allocation Framework under IFRS and US GAAP July 2026.” Preprint, . https://doi.org/10.2139/ssrn.7192719
• Minuti, Rafael. 2026b. “Flight-Cycle Depreciation and Impairment of Reusable Launch Vehicles: A Mission-Cycle Accounting Framework under IFRS and US GAAP.” Preprint, . https://doi.org/10.2139/ssrn.7176838
• Mishra, R. K. 1989. “Laser Beam Command Guidance.” In SPIE Proceedings, vol. 1042, edited by James D. Evans, Edward V. Locke. SPIE. https://doi.org/10.1117/12.951266
• Mishra, Pankil N., and Abhijit Gogulapati. 2022. “Topology Optimization of a Coupled Aerothermoelastic System.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-3938-9_34
• Mishra, Pankil N., and Abhijit Gogulapati. 2023. “Topology Optimization of 2D Approximate Aerothermoelastic System with Internal Radiation.” In AIAA SCITECH 2023 Forum. AIAA 2023-1673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1673
• “Missile Autopilot Design Using Dynamic Fuzzy Gain-Scheduling Technique.” 2004. In Advances in Dynamics and Control. CRC Press. https://doi.org/10.1201/9780203298916-8
• “Missile Guidance Software.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-13
• Mitani, Shinji, Tadahito Mizutani, Yusaku Tottori, Haruyuki Endo, and Yuichi Takushima. 2021. “Analysis of Temperature-Induced Drift Rate Error in Interferometric Multi-Core Fiber Optic Gyroscope.” In International Conference on Space Optics — ICSO 2020, edited by Zoran Sodnik, Bruno Cugny, Nikos Karafolas. SPIE. https://doi.org/10.1117/12.2599545
• Mitchell, W. 1970. The Bendix OAO Star Tracker High-Voltage System and Its Design Considerations. Bendix Corp. https://ntrs.nasa.gov/citations/19700022982
• Mitchell, Joe C. 1976a. Storage Reliability of Missile Materiel Program. Missile Hydraulic and Pneumatic Systems Actuator Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada026353
• Mitchell, Joe C. 1976b. Storage Reliability of Missile Materiel Program. Storage Reliability Summary Report. Volume 3. Hydraulic and Pneumatic Devices. Defense Technical Information Center. https://doi.org/10.21236/ada026477
• Mitchell, Glenn A., and Robert C. Campbell. 1957. Performance of a Supersonic Ramp-Type Side Inlet with Ram-Scoop Throat Bleed and Varying Fuselage Boundary-Layer Removal: Mach Number Range 1.5 to 2.0 / Glenn a. Mitchell and Robert C. Campbell. NACA-RM-E56I26. NASA. https://ntrs.nasa.gov/citations/19930089448
• Mitchell, Jesse L., and Robert F. Peck. 1950a. An Investigation of the Longitudinal Characteristics of the MX-656 Configuration Using Rocket-Propelled Models Preliminary Results at Mach Numbers from 0.65 to 1.25. NACA-RM-SL50J03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023623
• Mitchell, Jesse L., and Robert F. Peck. 1950b. Results of the Flight Test of a Dummy of the MX-656 Rocket-Propelled Models. NACA-RM-SL50A07. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026497
• Mitchell, Jesse L., and Robert F. Peck. 1955. Investigation of the Lateral Stability Characteristics of the Douglas X-3 Configuration at Mach Numbers from 0.6 to 1.1 by Means of a Rocket-Propelled Model. NACA-RM-L54L20. NASA. https://ntrs.nasa.gov/citations/19930088585
• Mitrev, Petar. n.d. “Navigating the Unknown: Radar–Inertial Localization for All-Terrain Autonomous Vehicles in GNSS-Denied Environments.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2025-16643
• Mittal, Sanchit, Sanjay Mittal, and L. Venkatakrishnan. 2026. “Stability and Buzz Characteristics of a Y-Shaped Conventional and Diverterless Supersonic Inlet.” Physics of Fluids 38 (9): 096136. https://doi.org/10.1063/5.0346197
• Miura, Ryu. 2022. “Performance of Multi-Hop Command and Telemetry Communication System in 169 MHz Band for Operation of Drones beyond Line-of-Sight.” Advances in Robotics & Mechanical Engineering 3 (5). https://doi.org/10.32474/arme.2022.03.000175
• Miwa, S., and F. Imado. 1985. “Clutter Effect on the Guidance of a Semi-Active Radar Homing Missile.” In Guidance, Navigation and Control Conference. AIAA 1985-1871. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1871
• Miyajima, Hiroshi, Nobuo Chinzei, Tohru Mitani, Yoshio Wakamatsu, and Masataka Maita. 1992. “Development Status of the NAL Ramjet Engine Test Facility and Sub-Scale Scramjet Engine.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5094. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5094
• Miyazawa, Yoshikazu, Kazutoshi Ishikawa, and Kenji Fujii. 1993. “Guidance and Control Law for Automatic Landing Flight Experiment of Reentry Space Vehicle.” In Guidance, Navigation and Control Conference. AIAA 1993-3818. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3818
• Miyazawa, Yoshikazu, Kazutoshi Ishikawa, Toshikazu Motoda, et al. 1996. “Flight Control System for the Automatic Landing Flight Experiment.” In Guidance, Navigation, and Control Conference. AIAA 1996-3782. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3782
• Miyazawa, Yoshikazu, Toshikazu Motoda, Tatsushi Izumi, and Takashi Hata. 1998. “Longitudinal Flight Control for Space Vehicle’s Automatic Landing.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4428
• Mo, Ran, Wenting Li, and Shanwei Su. 2022. “UDE-Based Adaptive Dynamic Surface Control for Attitude-Constrained Reusable Launch Vehicle.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2061133/v1
• Mock, F. C. 1951. “Turbojet and Turboprop Engine Controls.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/510198
• “Modal Analysis of a Typical Landing Gear Oleo Strut.” 2018. International Journal of Recent Trends in Engineering and Research 4 (1): 1–6. https://doi.org/10.23883/ijrter.2018.4001.t6fhs
• “Model of a Radar Semi-Active Homing System for a Guided Missile.” 2024. Journal of Computational and Engineering Mathematics 11 (2). https://doi.org/10.14529/jcem240204
• “Modularized Instrument System for Turbojet Engine Test Facilities.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0205.0215
• Moeller, R. P., W. K. Burns, and N. J. Frigo. 1988. “Scale Factor Accuracy and Stability in an Open Loop Fiber Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1988.fbb3
• Moghtadaei Rad, Amir. 2014. “Optimal Attitude Determination Method in Presence of Noise and Bias on Different Star Sensors.” International Journal of Engineering and Technology 3 (2): 155–65. https://doi.org/10.14419/ijet.v3i2.2216
• Mohamed, Ahmed S. A., and Apostolos Mamatas. 2012. “Fundamentals of GNSS-Aided Inertial Navigation.” In InTech eBooks. https://doi.org/10.5772/31093
• Mohamed, Emad Mahrous, and Lin Yan. 2016. “Design and Comparison of Two-Loop with PI and Three-Loop Autopilot for Static Unstable Missile.” International Journal of Computer and Electrical Engineering 8 (1): 1–11. https://doi.org/10.17706/ijcee.2016.8.1.1-11
• Mohammadkarimi, Hamed, and Hadi Nobahari. 2018. “A Model Aided Inertial Navigation System for Automatic Landing of Unmanned Aerial Vehicles: A Model Aided INS for Automatic Landing of UAVs.” Navigation 65 (2): 183–204. https://doi.org/10.1002/navi.232
• Mohammed Shibah, Sami Rashid. 2026. “ARES-X: A Staged Aerodynamic-Decelerator Concept for Crash-Energy Reduction of a Transport-Category Airframe -A Reduced-Order Feasibility Study with Uncertainty Quantification and Sensitivity Analysis.” Preprint, . https://doi.org/10.2139/ssrn.7405458
• Moin, Parviz, and Sanjiva K. Lele. 1998. Large Eddy Simulation of Supersonic Inlet Flows. Defense Technical Information Center. https://doi.org/10.21236/ada343835
• Mok, Sung-Hoon, and Hyochoong Bang. 2013. “Terrain Slope Estimation Methods Using the Least Squares Approach for Terrain Referenced Navigation.” International Journal of Aeronautical and Space Sciences 14 (1): 85–90. https://doi.org/10.5139/ijass.2013.14.1.85
• Mok, Sung-Hoon, Hyochoong Bang, and Myeong-Jong Yu. 2012. “A Performance Comparison of Nonlinear Kalman Filtering Based Terrain Referenced Navigation.” Journal of the Korean Society for Aeronautical & Space Sciences 40 (2): 108–17. https://doi.org/10.5139/jksas.2012.40.2.108
• Mok, Sung-Hoon, Hyochoong Bang, and Myeongjong Yu. 2017a. “Performance Analysis of Vision-Based Terrain Referenced Navigation.” Journal of Institute of Control Robotics and Systems 23 (4): 294–99. https://doi.org/10.5302/j.icros.2017.16.0196
• Mok, Sung-Hoon, Youngjoo Kim, and Hyochoong Bang. 2017b. “Vision-Based Terrain Referenced Navigation of Aerial Vehicles Using an Adaptive Extended Kalman Filter.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232 (8): 1584–97. https://doi.org/10.1177/0954410017699431
• Mokole, Eric L. 1991. Contributions to Radar Tracking Errors for a Two-Point Target Caused by Geometric Approximations. Defense Technical Information Center. https://doi.org/10.21236/ada241635
• Molander, Arne B. 1997. “The Celestial Navigation of Christopher Columbus.” Navigation 44 (4): 401–10. https://doi.org/10.1002/j.2161-4296.1997.tb02356.x
• Molander, Arne B. 1999. “Author’s Reply to Comments on “the Celestial Navigation of Christopher Columbus”.” Navigation 46 (3): 231–34. https://doi.org/10.1002/j.2161-4296.1999.tb02410.x
• Moleski, Travis W., and Jay P. Wilhelm. 2026. “Online Camera-LiDAR Extrinsic Calibration Using Planar Landmark Detection for GNSS-Denied Navigation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20802
• Molina, Carlos, Alan Johnson, and August Roesener. 2009. “Reusable Launch Vehicle Design Implications for Regeneration Time.” In AIAA SPACE 2009 Conference & Exposition. AIAA 2009-6471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6471
• Mollett, William E. 1956. “Celestial Navigation in High Latitudes.” Navigation 5 (2): 105–7. https://doi.org/10.1002/j.2161-4296.1956.tb00282.x
• Mongush, D. S., S. V. Ippolitov, and D. V. Lopatkin. 2025. “Method of Initial Alignment of the Video-Inertial Navigation System for an Unmanned Aerial Vehicle.” Information-measuring and Control Systems: 75–82. https://doi.org/10.18127/j20700814-202503-08
• Monir Hossain, Mohammad, and Muhammad Syahiran Abdul Muthalib. 2025. “The Application of Optical Gyroscope in Developing Inertial Navigation System.” ALAM Journal of Maritime Studies 3 (1): 35–48. https://doi.org/10.66352/ajms.v3i1.12
• Moniruzzaman, Md, Alexander Rassau, Douglas Chai, and Syed Mohammad Shamsul Islam. 2022. “High Latency Unmanned Ground Vehicle Teleoperation Enhancement through Video Transformation.” Preprint, . https://doi.org/10.2139/ssrn.4082840
• Monroe, Alfred J. 1963. “Weapon System Capability: Availability Models and Parameter Estimation.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/630534
• Montero Yéboles, Daniel. n.d. “Analysis and Optimization of Trajectories for Ballistic Missiles Interception.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.39534
• Montgomery, R. C. 1975. “Failure Detection and Control-System Reconfiguration: Past, Present, and Future.” In Systems Reliability Issues for Future Aircraft. https://ntrs.nasa.gov/citations/19770015869
• Moody, Alton B. 1972. “Celestial Fix-Internal or External?” Navigation 19 (4): 338–43. https://doi.org/10.1002/j.2161-4296.1972.tb01704.x
• Mook, D., Douglas Swanson, and Michael Roemer. 1990. “Improved Noise Rejection in Automatic Carrier Landing Systems.” In Guidance, Navigation and Control Conference. AIAA 1990-3374. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3374
• Moon, Gwanyoung, Byungeul Jun, and Doyle Knight. 2012. “A 3-Loop Autopilot Design for a Missile Using an Automated MDO Environment.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2012-4719. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4719
• Moore, Robert B. 1967. Satellite Celestial Navigation. Defense Technical Information Center. https://doi.org/10.21236/ad0648714
• Moore, F. 1974. “Static Aerodynamics of Missile Configurations for Mach Number Zero to Three.” In 7th Fluid and PlasmaDynamics Conference. AIAA 1974-538. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-538
• Moore, F. 1985. “Stall Transients of Axial Compression Systems with Inlet Distortion.” In 21st Joint Propulsion Conference. AIAA 1985-1348. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1348
• Moore, Frank G. 1993. State-of-the-Art Engineering Aeroprediction Methods with Emphasis on New Semiempirical Techniques for Predicting Nonlinear Aerodynamics on Complete Missile Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada273680
• Moore, J. W., L. Barnett, B. T. Farmer, E. E. McBride, and B. I. Reynolds. 1979. Peripheral Jet Air Cushion Landing System Spanloader Aircraft. Volume I. Defense Technical Information Center. https://doi.org/10.21236/ada085203
• Moore, F., T. Hymer, and F. Wilcox. 1993. “Base Drag Prediction on Missile Configurations.” In Flight Simulation and Technologies. AIAA 1993-3629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3629
• Moore, M., and A. Jenn. 1990. “Preliminary Design Aerodynamics of Missile Inlets.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3091
• Moore, F., and J. White. 1967. “Application of Redundancy in the Saturn V Guidance and Control System.” In Control and Flight Dynamics Conference. AIAA 1967-553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-553
• Moran, Kenneth, and Philip Beran. 1995. “Fin-Interference Effects on the Aerodynamics of a Swept-Fin Missile.” In 13th Applied Aerodynamics Conference. AIAA 1995-1899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1899
• Morani, Gianfranco, Felice Fruncillo, Sara Di Benedetto, Marco Marini, Marta Albano, and Simone Pizzurro. 2026. “Guidance and Control Algorithms of a Hypersonic Launch Vehicle.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5046
• Morelli, Eugene A. 1995. F-18 High Alpha Research Vehicle (HARV) Parameter Identification Flight Test Maneuvers for Optimal Input Design Validation and Lateral Control Effectiveness. NASA-CR-198248. NASA. https://ntrs.nasa.gov/citations/19960012190
• Morelli, Eugene A. 1996. Piloted Parameter Identification Flight Test Maneuvers for Closed Loop Modeling of the F-18 High Alpha Research Vehicle (HARV). NASA-CR-198268. NASA. https://ntrs.nasa.gov/citations/19960023575
• Morelli, Eugene A. 2000a. Identification of Low Order Equivalent System Models from Flight Test Data. NASA/TM-2000-210117. NASA. https://ntrs.nasa.gov/citations/20000085030
• Morelli, Eugene. 2000b. “Low Order Equivalent System Identification for the Tu-144LL Supersonic Transport Aircraft.” In Atmospheric Flight Mechanics Conference. AIAA 2000-3902. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3902
• Morelli, Eugene. 2002. “System Identification Programs for AirCraft (SIDPAC).” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4704
• Morelli, Eugene A. 2021. “Practical Aspects of Multiple-Input Design for Aircraft System Identification Flight Tests.” In AIAA Aviation 2021 Forum. AIAA 2021-2795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2795
• Morelli, Eugene, and Vladislav Klein. 1995. “Determining the Accuracy of Aerodynamic Model Parameters Estimated from Flight Test Data.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3499
• Morgan, F. 1971. “Advanced Techniques in the Testing and Evaluation of Terminal Guidance Subsystems.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-969
• Morgan, James G., Fritz P. Kronberger, and James V. Strickland. 1974. “Accuracy of an Integrated Satellite Navigation System Obtained from Geophysical Survey Data.” In Offshore Technology Conference. https://doi.org/10.4043/2009-ms
• Morgan, Samuel H., and Ho Jung Paik. 1988. Superconducting Gravity Gradiometer Mission. Volume 2: Study Team Technical Report. NASA-TM-4091-VOL-2. NASA. https://ntrs.nasa.gov/citations/19890010378
• Morgan, Samuel H., and Ho Jung Paik. 1989. Superconducting Gravity Gradiometer Mission. Volume 1: Study Team Executive Summary. NASA-TM-4091-VOL-1. NASA. https://ntrs.nasa.gov/citations/19900006229
• Morito, Jack, and Kenneth Sidwell. 1967. “Evaluation of Unsteady Aerodynamic Forces and Dynamic Response of Flexible Aircraft Structure to Continous Turbulance in Supersonic Flight.” In 8th Structural Dynamics and Materials Conference. AIAA 1967-1140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-1140
• Morito, J., II, and W. Rowe. 1972. “Unsteady Aerodynamics of Non-Planar Wings and Wing-Tail Configurations of Elastic Flight Vehicles in Supersonic Flight.” In 13th Structures, Structural Dynamics, and Materials Conference. AIAA 1972-378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-378
• Morlang, Frank. 2019. “Supersonic and Hypersonic Flight Dynamics Realization for the Spaceliner Real-Time Human-In-the-Loop Space Flight Simulator.” International Journal of Recent Technology and Engineering (IJRTE) 8 (2S11): 4043–46. https://doi.org/10.35940/ijrte.b1590.0982s1119
• Morozova, Katerina, Ansis Zarins, Gunars Silabriedis, Janis Balodis, and Reiner Jäger. 2019. “Digital Zenith Camera for Vertical Deflection Determination: On the Way to 1 Cm Precise Quasi-Geoid Model for Latvia.” Preprint, . https://doi.org/10.1002/essoar.10501273.1
• Morrell, F., M. Bailey, and P. Motyka. 1988. “Flight Test Results of a Vector-Based Failure Detection and Isolation Algorithm for a Redundant Strapdown Inertial Measurement Unit.” In 4th Flight Test Conference. AIAA 1988-2172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2172
• Morrell, F. R., and P. Motyka. 1983. Unified Analysis Methods for a Fault Tolerant Redundant Strapdown Inertial Measurement Unit. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840027883
• Morrell, F. R., P. R. Motyka, and M. L. Bailey. 1990. “Flight Test Results of Failure Detection and Isolation Algorithms for a Redundant Strapdown Inertial Measurement Unit.” In AGARD, Fault Tolerant Design Concepts for Highly Integrated Flight Critical Guidance and Control Systems. https://ntrs.nasa.gov/citations/19910003388
• Morrell, F. R., and J. G. Russell. 1980. Design of a Developmental Dual Fail Operational Redundant Strapped down Inertial Measurement Unit. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19810045858
• Morris, J. 1986. MaRV (Maneuverable Reentry Vehicles) PoP (Probability of Penetration) vs CEP (Circular Error Probability) Analysis Concept Study (MaRV Penetration Study Project). Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/6423110
• Morris, R. E., and G. D. Brewer. 1979. Hypersonic Cruise Aircraft Propulsion Integration Study, Volume 1. NASA-CR-158926-VOL-1. NASA. https://ntrs.nasa.gov/citations/19800006815
• Morris, D. L., and J. R. McGehee. 1983. Experimental and Analytical Investigation of Active Loads Control for Aircraft Landing Gear. AFWAL. https://ntrs.nasa.gov/citations/19840011818
• Morris, S. J., Jr., W. E. Foss Jr., and M. J. Neubauer Jr. 1980. Conceptual Study of an Advanced Supersonic Technology Transport (AST-107) for Transpacific Range Using Low-Bypass-Ratio Turbofan Engines. NASA-TM-81872. NASA. https://ntrs.nasa.gov/citations/19800024834
• Morris, Shelby J., Jr., Karl A. Geiselhart, and Peter G. Coen. 1989. Performance Potential of an Advanced Technology Mach 3 Turbojet Engine Installed on a Conceptual High-Speed Civil Transport. NASA-TM-4144. NASA. https://ntrs.nasa.gov/citations/19900000718
• Morrison, R. B. 1980. Oblique Detonation Wave Ramjet. NASA-CR-159192. NASA. https://ntrs.nasa.gov/citations/19800005874
• Morrison, Melvin M. 1988. “Morrison’s QUBIK Inertial Measurement Unit.” Navigation 35 (2): 177–84. https://doi.org/10.1002/j.2161-4296.1988.tb00950.x
• Morton, Scott A. 2014. “Inlet/Engine Integration Examples Using Coupled Transient and Steady Engine Performance Models with Kestrel.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0753
• Morton, Wayne K., Glen R. Lazalier, C. Dennis Rose, and R. F. (Pete) Lauer. 1991. “On-Line Distortion Analysis System for Inlet-Engine Testing.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/91-gt-166
• Mosbarger, Neal, and Paul King. 1995. “Time-Dependent Supersonic Separation of Tangent Bodies.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3462
• Moskowitz, S. 1973. “The Development of the Artificial Horizon for Celestial Navigation.” Navigation 20 (1): 1–16. https://doi.org/10.1002/j.2161-4296.1973.tb01149.x
• Moskowitz, L., and P. Soltis. 1976. Influence of Wire Properties on the Fatigue Performance of Arresting Gear Purchase Cable. Defense Technical Information Center. https://doi.org/10.21236/ada026115
• Moss, Matthew A., Joseph D. Vasile, Luis G. Bravo, and Jack Edwards. 2026. “Computational Exploration of Hypersonic Inlet Stability and Unstart Thresholds under Uncertainty.” In AIAA AVIATION 2026 Forum. AIAA 2026-4177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4177
• Mostafa, M. M., A. M. Moussa, N. El-Sheimy, and Abu B. Sesay. 2018b. “A Smart Hybrid Vision Aided Inertial Navigation System Approach for UAVs in a GNSS Denied Environment.” Navigation 65 (4): 533–47. https://doi.org/10.1002/navi.270
• Motohara, Shinji, and Aritaka Ohno. 1992. “Fiber Optic Gyroscope with Single Mode Fiber Coil.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1992.w22
• Motyka, P. 1983. Reliability Analysis and Fault-Tolerant System Development for a Redundant Strapdown Inertial Measurement Unit. NASA-CR-166050. NASA. https://ntrs.nasa.gov/citations/19830012655
• Motyka, P., M. Landey, and R. McKern. 1981. Failure Detection and Isolation Analysis of a Redundant Strapdown Inertial Measurement Unit. NASA-CR-165658. NASA. https://ntrs.nasa.gov/citations/19810009511
• Motyka, Paul, Roy Nurse, and Kevin Daly. 1978. Multifunction Inertial Reference Assembly Technology (MIRAT) Simulation Development, Configuration Evaluation, and Test Plan Development. Defense Technical Information Center. https://doi.org/10.21236/ada057324
• Motyka, P., R. Ornedo, and R. Mangoubi. 1984. Fault-Tolerant System Considerations for a Redundant Strapdown Inertial Measurement Unit. NASA-CR-172426. NASA. https://ntrs.nasa.gov/citations/19840025325
• Moua, Cheng M., Shaun C. McWherter, Timothy H. Cox, and Joe Gera. 2012. Flight Test Results on the Stability and Control of the F-15 Quiet Spike(TradeMark) Aircraft. NASA/TM-2012-215978. NASA. https://ntrs.nasa.gov/citations/20120013435
• Mouch, T., T. McLaughlin, and J. Ashworth. 1989. “Unsteady Flows Produced by Small Amplitude Oscillations of the Canard of an X-29 Model.” In 7th Applied Aerodynamics Conference. AIAA 1989-2229. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2229
• Moul, Martin T. 1953. Flight Investigation of a Supersonic Canard Missile Equipped with an Auxiliary Damping-in-Pitch Control System. NACA-RM-L52K14b. NASA. https://ntrs.nasa.gov/citations/19930087453
• Moul, Martin T., and Andrew R. Wineman. 1952. Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-Canard Area Ratio of 16:1. NACA-RM-L52D24a. NASA. https://ntrs.nasa.gov/citations/19930086980
• Moulden, T., J. Wu, and D. Spring. 1974. “A Flow Field Model for, and Some Studies on the Drag of, an Engine Exhaust System at Transonic Flight Speeds.” In 10th Propulsion Conference. AIAA 1974-1175. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1175
• Moussa, M., A. Moussa, and N. El-Sheimy. 2019. “Ultrasonic Wheel Based Aiding for Land Vehicle Navigation in GNSS Denied Environment.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2019.16695
• Mousseau, Albert. 2013. AGM-88E Advanced Anti-Radiation Guided Missile (AGM-88E AARGM). Defense Technical Information Center. https://doi.org/10.21236/ada613519
• Mousseau, Albert. 2015. AGM-88E Advanced Anti-Radiation Guided Missile (AGM-88E AARGM). Defense Technical Information Center. https://doi.org/10.21236/ad1018961
• Moyer, R. 1963a. Scientific Passenger Pod, Addendum to Annex Flight Test Directive Missile N-24. Defense Technical Information Center. https://doi.org/10.21236/ad0408760
• Moyer, J. 1963b. Tory II-C Performance as a Function of Flight Mach Number and Inlet Pressure Recovery. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/435307
• Mozafari, Saeid, Hamed Mohammadkarimi, Mahsa Ghasemi, Mohammad Ali Parhizkar, and Mahdi Mobtaker. 2025. “Analysis of IMU Rotation Effects on Inertial Navigation System Errors.” NAVIGATION: Journal of the Institute of Navigation 72 (1): navi.680. https://doi.org/10.33012/navi.680
• Mracek, Curtis, James Cloutier, James Cloutier, and Curtis Mracek. 1997. “Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method.” In Guidance, Navigation, and Control Conference. AIAA 1997-3767. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3767
• Mu, Sida, Lingyun Wang, Chun Wang, Xing Yu, and Yidan Wang. 2025. “Accelerated Motion Star Spot Centroid Localization Method for Star Tracker under High Dynamic Conditions.” Optics Express 33 (25): 52000. https://doi.org/10.1364/oe.577531
• Muehlner, Joachim W. 1962. Trends in Missile and Space Radio Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ad0407379
• Muehter, Vincent. 1974. Landing and Takeoff Roll-Out Augmentation. Defense Technical Information Center. https://doi.org/10.21236/ada043526
• Mulac, Richard A., Jon C. Schneider, and John J. Adamczyk. 1989. Average-Passage Simulation of Counter-Rotating Propfan Propulsion Systems as Applied to Cruise Missiles. NASA-TM-102043. NASA. https://ntrs.nasa.gov/citations/19890014045
• Muller, John F. n.d. “Inertial Guidance System Design Requirements for Short Range Missile Applications.” PhD diss., Drexel University. https://doi.org/10.17918/00005958
• Müller, Peter Chr. 1972. “Self — Alignment of Inertial Platforms.” In Special Problems of Gyrodynamics. Springer Vienna. https://doi.org/10.1007/978-3-7091-2882-4_4
• Muller, Mark, and Terrence Wesshaar. 1994. “Maximizing Deflections Produced by Induced Strain Beam-like Actuators for Transonic Drag Reduction.” In Adaptive Structures Forum. AIAA 1994-1775. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1775
• Munk, David J., Gareth A. Vio, and Dries Verstraete. 2016. “A Hypersonic Aircraft Optimization Tool with Strong Aerothermoelastic Coupling.” Applied Mechanics and Materials 846: 494–99. https://doi.org/10.4028/www.scientific.net/amm.846.494
• Muppidi, Suman, Clara O’Farrell, Christopher Tanner, John W. Van Norman, and Ian G. Clark. 2018. “Modeling and Flight Performance of Supersonic Disk-Gap-Band Parachutes in Slender Body Wakes.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3623
• Murman, Scott, and Michael Aftosmis. 2003. “Cartesian-Grid Simulations of a Canard-Controlled Missile with a Spinning Tail.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3670
• Murman, Scott M., Michael J. Aftosmis, and Dochan Kwak. 2002. Cartesian-Grid Simulations of a Canard-Controlled Missile with a Free-Spinning Tail. Eloret Corp. https://ntrs.nasa.gov/citations/20030002767
• Murman, E., and J. Cole. 1974. “Inviscid Drag at Transonic Speeds.” In 7th Fluid and PlasmaDynamics Conference. AIAA 1974-540. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-540
• Murphy, Patrick, and Vladislav Klein. 2008. “Transport Aircraft System Identification from Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6202
• Murphy, Patrick, and Vladislav Klein. 2010. “Transport Aircraft System Identification Using Roll and Yaw Oscillatory Wind Tunnel Data.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8122
• Murphy, J. D., and M. W. Rubesin. 1965. An Evaluation of Free-Flight Test Data for Aerodynamic Heating from Laminar, Turbulent, and Transitional Boundary Layers. Part II: The X-17 Reentry Body. NASA-CR-70931. NASA. https://ntrs.nasa.gov/citations/19660010795
• Murphy, C. H., and L. E. Schmidt. 1953. The Effect of Length on the Aerodynamic Characteristics of Bodies of Revolution in Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0023468
• Murray, Neil, and Johan Steelant. 2009. “Methodologies Involved in the Design of LAPCAT-MR1: A Hypersonic Cruise Passenger Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7399
• Murray-Smith, D. J. 1995. “Case Study II — An Aircraft Automatic Landing System.” In Continuous System Simulation. Springer US. https://doi.org/10.1007/978-1-4615-2504-2_11
• Muruganandan, Vishnu Anand, Ji Hyun Park, Sangyoon Lee, In-seuck Jeung, Sangkyun Kim, and Gwanghyeok Ju. 2018. “Star Selection Algorithm for Arcsecond Pico Star Tracker.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-2199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2199
• Murzionak, Aliaksandr. n.d. “Rocket Based Combined Cycle Exchange Inlet Performance Estimation at Supersonic Speeds.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2013-06868
• Mushtaq, Noraiz, and Paolo Gaetani. 2023. “Understanding and Modeling Unstarting Phenomena in a Supersonic Inlet Cascade.” Physics of Fluids 35 (10): 106101. https://doi.org/10.1063/5.0160706
• Mustafa, Mustafa Abdulsalam, Atheer Raheem Abdullah, and Mohammed Mousa Al-azzawi. 2025. “Numerical Modeling of Supersonic Flow through a Ramjet Nozzle Using Ansys Fluent.” International Journal of Computational Methods and Experimental Measurements 13 (4): 993–1005. https://doi.org/10.56578/ijcmem130416
• Mutz, M., E. Pierce, and A. Sievers. 1964. “Supersonic Transport Engine Cycle Selection.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-601. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-601
• Muzumdar, Dinesh, and David Hull. 1995. “Midcourse Guidance for a Short Range Attack Missile Using Error Compensation.” In Guidance, Navigation, and Control Conference. AIAA 1995-3279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3279
• Myers, George H. 1966. “Experience with the Applications of Radio Command Guidance to Satellite Launch Vehicles.” In Peaceful Uses of Automation in Outer Space. Springer US. https://doi.org/10.1007/978-1-4899-6411-3_4
• Myrabo, L. N., M. V. Powers, and C. L. Zaretzky. 1986. Analysis of Beamed-Energy Ramjet/scramjet Performance. AIAA PAPER 86-1761. Rensselaer Polytechnic. https://ntrs.nasa.gov/citations/19870034251
• Møller-Skuldbøl, Signe, Kasper B. Lauritsen, Maria Moga, Omkar Korgaonkar, Peter; id_orcid 0000-0002-8685-0246 Leth, and Andreas Møgelmose. 2026. “Towards GNSS-Denied Geo-Positioning Using Search Area Refinement.” In International Conference on Computer Vision Theory and Applications. https://doi.org/10.5220/0014620800004084
• NACA Conference on the Turbojet Engine for Supersonic Aircraft Propulsion: A Compilation of the Papers Presented. 1951. NASA-TM-X-57165. NASA. https://ntrs.nasa.gov/citations/19660006991
• Naca Conference on Turbojet Engines for Supersonic Propulsion a Compilation of Technical Material Presented. 1953. NASA-TM-X-56788. NASA. https://ntrs.nasa.gov/citations/19650023938
• Nadim Melhem, George, Paul Richard Munroe, and Akshay Vithal. 2024. “Supersonic Aircraft.” In Supersonic Effects on Rivets. CRC Press. https://doi.org/10.1201/9781003516903-2
• Nadkarni, A. A. 1981. Comparative Study of Flare Control Laws. NASA-CR-164903. NASA. https://ntrs.nasa.gov/citations/19820002159
• Nagamatsu, H., T. Trilling, and J. Bossard. 1987. “Passive Drag Reduction on a Complete NACA 0012 Airfoil at Transonic Mach Numbers.” In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1987-1263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1263
• Nagao, Tsukasa, Hidekazu Yoshida, Masakazu Sano, Tetsuya Sato, and Atsushi Hashimoto. 2019. “Numerical Analysis on Supersonic Inlet Buzz.” Aerospace Technology Japan, the Japan Society for Aeronautical and Space Sciences 18 (0): 81–89. https://doi.org/10.2322/astj.jsass-d-18-00007
• Nagaoka, Sakae. 1984. “Study on the Height Estimation Accuracy of a Radar for Navigation Accuracy Measurement.” Journal of Japan Institute of Navigation 70 (0): 85–92. https://doi.org/10.9749/jin.70.85
• Nagaoka, Sakae. 1992. “Analyses of Position Error Distributions of Inertial Navigation Systems.” Journal of Japan Institute of Navigation 87 (0): 99–106. https://doi.org/10.9749/jin.87.99
• Nagata, Takayuki, Akito Noguchi, Taku Nonomura, Toshihiro Ogawa, Kiyonobu Ohtani, and Keisuke Asai. 2019. “Schlieren Visualization of Transonic and Supersonic Flow over a Sphere at Reynolds Number between 103and 105through Free-Flight Tests.” In AIAA Scitech 2019 Forum. AIAA 2019-2156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2156
• Nah, Jakyoung. 2005. “Star Detectability Analysis of Daytime Star Sensor.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (9): 89–96. https://doi.org/10.5139/jksas.2005.33.9.089
• Naidu, Sivasubramaniam Nambi, and Ramesh Kumar. 2022. “Transfer Alignment Technique for Shipboard Missile Strapdown Inertial Navigation System Using an Adaptive Kalman Filter.” Defence Science Journal 72 (3): 464–72. https://doi.org/10.14429/dsj.72.17636
• Nair, Pranay Prem, and Mayur Kukreja. 2025. “Reusable Launch Vehicle and Rocket Study.” Preprint, . https://doi.org/10.31224/4543
• Nakagawa, Ichiro, and Yusuke Ezawa. 2014. “Study on the Key Technologies of a Hybrid Rocket & Ramjet Combined Cycle Engine.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3952. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3952
• Nakagiri, S. n.d. “On the Identifiability of Parameters in Distributed Systems.” In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0043946
• Nakamura-Zimmerer, Tenavi, Mary T. Stringer, Brendon K. Colbert, and James B. Scoggins. 2023. “Structured Covariance Gaussian Networks for Orion Crew Module Aerodynamic Uncertainty Quantification.” In AIAA SCITECH 2023 Forum. AIAA 2023-1184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1184
• Nam, Keesung. n.d. “Application of Kalman Filtering in Inertial Navigation System (INS) Aided by Global Positioning System (GPS).” PhD diss., Drexel University. https://doi.org/10.17918/00008556
• Nam, Junyeop, Duk-Min Kim, Tae-Seong Roh, and Hyoung Jin Lee. 2022. “Characteristics of Base Drag and Flow with Nozzle Flow Conditions in Supersonic Flow.” International Journal of Aeronautical and Space Sciences 23 (5): 870–81. https://doi.org/10.1007/s42405-022-00513-z
• Namkoung, Hyuck-Joon, Wooram Hong, Jungmin Kim, Junsok Yi, and Chong-Am Kim. 2012. “Effects of Angles of Attack and Throttling Conditions on Supersonic Inlet Buzz.” International Journal of Aeronautical and Space Sciences 13 (3): 296–306. https://doi.org/10.5139/ijass.2012.13.3.296
• Naohiko, Ban, Wataru Yamazaki, and Kazuhiro Kusunose. 2016. “Low-Boom / Low-Drag Design Optimization of Innovative Supersonic Transport Configuration.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-2002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2002
• Napjus, G. A. 1974. “The Application of Microprocessors to Strapdown Inertial Navigation.” In International Conference on Microprocessors. https://ntrs.nasa.gov/citations/19750042593
• Napjus, G. A. 1975. Recent Advances in Strapdown Inertial Navigation. Teledyne Systems Co. https://ntrs.nasa.gov/citations/19760028874
• Napolitano, Fabien, Thomas Buret, and David Ramecourt. 2017. “From Space Qualified Fiber Optic Gyroscope to Generic Fiber Optic Solutions Available for Space Application.” In International Conference on Space Optics — ICSO 2008, edited by Josiane Costeraste, Errico Armandillo, Nikos Karafolas. SPIE. https://doi.org/10.1117/12.2308279
• Narasimhan, Sridharakumar, S. Arun Srikanth, J. V. N. Sreeram, and Raghunathan Rengaswamy. 2011. “Optimal Plant Friendly Input Design for System Identification.” Industrial & Engineering Chemistry Research 50 (23): 13045–55. https://doi.org/10.1021/ie200472s
• Narasimhappa, Mundla, Samrat L. Sabat, and Jagannath Nayak. 2015. “Adaptive Sampling Strong Tracking Scaled Unscented Kalman Filter for Denoising the Fibre Optic Gyroscope Drift Signal.” IET Science, Measurement & Technology 9 (3): 241–49. https://doi.org/10.1049/iet-smt.2014.0001
• Nardozzo, Paige K., Sarah Popkin, and Justin R. Smith. 2019. “Feasibility Study for Hypersonic Flight Test Using a Reusable Hybrid Rocket Motor.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-3838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3838
• Naruse, Hiroki, Tatsuya Ishii, Hideshi Oinuma, et al. 2022. “Effect of Inlet Distortion with Crosswind on Aircraft-Engine Intake Aerodynamic Performance.” Transactions of the JSME (in Japanese) 88 (910): 21-00357-21-00357. https://doi.org/10.1299/transjsme.21-00357
• Naser-Moghadasi, M., F. Setoudeh, and S. A. Olamaei. 2013. “Stability Analysis of MEMS Gyroscope Dynamic Systems.” Advanced Computational Techniques in Electromagnetics 2013: 1–6. https://doi.org/10.5899/2013/acte-00124
• Naseri, A., M. Boroomand, and A. M. Tousi. 2012a. “The Effect of Inlet Flow Distortion on Performance of a Micro-Jet Engine: Part 1 — Development of an Inlet Simulator.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2012-86865
• Naseri, A., M. Boroomand, A. M. Tousi, and A. R. Alihosseini. 2012b. “The Effect of Inlet Flow Distortion on Performance of a Micro-Jet Engine: Part 2 — Engine Tests.” In Volume 1: Advances in Aerospace Technology. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2012-86803
• Nash, R., Jr., J. D’Appolito, and K. Roy. 1972. “Error Analysis of Hybrid Aircraft Inertial Navigation Systems.” In Guidance and Control Conference. AIAA 1972-848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-848
• Nassirharand, Amir, and S. R. Mousavi Firdeh. 2009. “Single-Range Controller Design for a Cruise Missile.” Aircraft Engineering and Aerospace Technology 81 (4): 283–87. https://doi.org/10.1108/00022660910967264
• Naughton, Jonathan. 1999. Reduction of Base Drag on Launch Vehicles. UWAL-2000-01. Wyoming Univ. https://ntrs.nasa.gov/citations/20000031396
• Naughton, Jonathan W. 2002. Reduction of Base Drag on Launch Vehicles. UWAL-2002-02. Wyoming Univ. https://ntrs.nasa.gov/citations/20020070521
• Navigation Error Analysis in Strapdown Inertial Navigation. 2021. Wiley. https://doi.org/10.1002/9781119699910.ch4
• “Navigation-Grade Inertial Sensors.” 2022. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch8
• Navon, Dan, Ehud Rivlin, and Hector Rotstein. 2025. “A Robust Approach to Vision-Based Terrain-Aided Localization.” NAVIGATION: Journal of the Institute of Navigation 72 (1): navi.683. https://doi.org/10.33012/navi.683
• Nazan, Yi. 2023. “Gravity Data Reduction, Bouguer Anomaly, and Gravity Disturbance.” Geofizicheskiy Zhurnal 45 (6). https://doi.org/10.24028/gj.v45i6.293314
• Neaves, Michael D., and D. Scott McRae. 1995. “Numerical Investigation of the Unstart Phenomenon in an Axisymmetric Supersonic Inlet.” In Computational Fluid Dynamics in Aeropropulsion. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0407
• Neaves, Michael, D. McRae, and Jack Edwards. 2001. “High-Speed Inlet Unstart Calculations Using an Implicit Solution Adaptive Mesh Algorithm.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-825. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-825
• Nebot, E., and H. Durrant-Whyte. n.d. “Initial Calibration and Alignment of an Inertial Navigation.” In Proceedings Fourth Annual Conference on Mechatronics and Machine Vision in Practice. IEEE Comput. Soc. https://doi.org/10.1109/mmvip.1997.625318
• Nechiporuk, S. Yu., and D. Kh. Zaripov. 2022. “Numerical Simulation of Throttling Processes in the Ramjet Engine.” Engineering Journal: Science and Innovation, no. 9 (129). https://doi.org/10.18698/2308-6033-2022-9-2212
• Needham, Timothy, and Michael Braasch. 2022. “Gravity Modeling in GNSS-Aided Inertial Navigation System Safety Certification.” NAVIGATION: Journal of the Institute of Navigation 69 (2): navi.520. https://doi.org/10.33012/navi.520
• Neel, C. B. 1958. An Analog Study of the Influence of Internal Modifications to a Wing Leading Edge on Its Transient Temperature Rise during Highspeed Flight. NACA-RM-A57K21. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19630004001
• Neely, Amanda, Lamar Auman, and William Blake. 2003. “Missile DATCOM Transonic Drag Improvements for Hemispherical Nose Shapes.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3668. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3668
• Negre, Y. 1975. “All Weather Automatic Landing on Civil Aircraft: A Review of Aerospatiale’s Experience on Concepts and Operations.” In Aircraft Systems and Technology Meeting. AIAA 1975-1023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1023
• Neiner, G. H., G. L. Cole, and F. J. Paulovich. 1978. “Normal Shock and Restart Controls for a Supersonic Airbreathing Propulsion System.” In NASA, Washington Fourth Inter-Center Control Systems Conf.. https://ntrs.nasa.gov/citations/19780015080
• Neistat, Raymond. n.d. “Observability-Aware Path Planning for Autonomous Navigation.” PhD diss., University of Rhode Island. https://doi.org/10.23860/thesis-2530
• Nelson, Bernard. 1965. “Understanding an Inertial Platform.” Navigation 12 (2): 145–52. https://doi.org/10.1002/j.2161-4296.1965.tb02126.x
• Nelson, H. 1988a. “Effect of Sideslip on Fin-Fin Interference in Supersonic Missile Aerodynamics.” In 26th Aerospace Sciences Meeting. AIAA 1988-214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-214
• Nelson, William. 1988b. Use of Circular Error Probability in Target Detection. Defense Technical Information Center. https://doi.org/10.21236/ada199190
• Nelson, H. 1991. “Supersonic Aerodynamics of Noncircular Cross Section Missile Forebodies.” In 29th Aerospace Sciences Meeting. AIAA 1991-390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-390
• Nelson, Michael, Kevin T. Lowe, Walter F. O’Brien, and Kevin M. Hoopes. 2014. “Stereoscopic PIV Measurements of Swirl Distortion on a Full-Scale Turbofan Engine Inlet.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0533
• Nelson, Walter C., and Anthony L. Passera. 1950. A Theoretical Investigation of the Influence of Auxiliary Damping in Pitch on the Dynamic Characteristics of a Proportionally Controlled Supersonic Canard Missile Configuration. NACA-RM-L50F30. NASA. https://ntrs.nasa.gov/citations/19930086299
• Nelson, Robert L., and Clement J. Welsh. 1960. Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag. NASA-TN-D-446. NASA. https://ntrs.nasa.gov/citations/19980227964
• Nenarokomov, Aleksey V., Ashley F. Emery, and Tushar D. Fadale. 1998. “Parameter Estimation and Optimal Experiment Design with Uncertainties in a-Priori Known Parameters.” In Inverse Problems in Engineering Mechanics. Elsevier. https://doi.org/10.1016/b978-008043319-6/50008-x
• “Neoclassical Missile Guidance.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-15
• Nesline, F. 1978. “Missile Guidance for Low Altitude Air Defense.” In Guidance and Control Conference. AIAA 1978-1317. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1317
• Nesline, F., B. Wells, and P. Zarchan. 1979. “A Combined Optimal/classical Approach to Robust Missile Autopilot Design.” In Guidance and Control Conference. AIAA 1979-1731. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1731
• Nesline, F., and P. Zarchan. 1979. “A New Look at Classical versus Modern Homing Missile Guidance.” In Guidance and Control Conference. AIAA 1979-1727. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1727
• Nesline, F., and P. Zarchan. 1980. “Robust Instrumentation Configurations for Homing Missile Flight Control.” In Guidance and Control Conference. AIAA 1980-1749. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1749
• Nesline, F., and P. Zarchan. 1982a. “A Classical Look at Modern Control for Missile Autopilot Design.” In Guidance and Control Conference. AIAA 1982-1512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1512
• Nesline, F., and P. Zarchan. 1982b. “Missile Guidance Design Trade-Offs for High Altitude Air Defense.” In Guidance and Control Conference. AIAA 1982-1506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1506
• Neuhauser, Tobias, Talha Ince, and Thomas Telaar. 2026. “A Solution to GNSS-Denied Navigation for Aeronautics—Combining GNSS-Denied Navigation Means and Collaborative Navigation.” In European Navigation Conference 2025. MDPI. https://doi.org/10.3390/engproc2026126026
• Neumann, R., J. Patterson, and N. Sliski. 1978. “Aerodynamic Heating to the Hypersonic Research Aircraft, X-24C.” In 16th Aerospace Sciences Meeting. AIAA 1978-37. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-37
• Neumann, Nils, Malak Samaan, Michael Conradt, and Stephan Theil. 2009. “Attitude Determination for the SHEFEX-2 Mission Using a Low Cost Star Tracker.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6279
• “New Applications of Engineering Level Missile Aerodynamics and Store Separation Prediction Methods.” 1994. In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-28. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-28
• Newcomb, William A. 1991. “Magnetohydrodynamic Wave Drag.” Physics of Fluids B: Plasma Physics 3 (8): 1818–29. https://doi.org/10.1063/1.859651
• Newsham, H. O. 2020. “Ballistic Missile Defence as a Practicable Proposition.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781003098522-1
• Ngo, Anhtuan, and William Blake. 2003. “Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5738
• Nguyen, Phu, Stanley Mak, and Jose Panza. 2006. “Simulation of Landing Events for an Unconventional UAV Landing Gear System Using Transient Dynamics Approach.” In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th. AIAA 2006-1762. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-1762
• Nguyen, Trong Yen, Quoc Khanh Nguyen, and Van Khoi Nguyen. 2023a. “Random Noise Suppression Method for Inertial Sensors Based on Complexing an AR Model and Adaptive SRUKF Kalman Filter under the PINS Alignment on a Stationary Platform.” Journal of the Russian Universities. Radioelectronics 26 (2): 101–19. https://doi.org/10.32603/1993-8985-2023-26-2-101-119
• Nguyen, Le Thanh, Quoc Quan Nguyen, and Ha Hiep Nguyen. 2023b. “Research on Operating Characteristics of Single-Spool Turbojet Enginewith the Afterburner AL-21F.” Ministry of Science and Technology, Vietnam 65 (3): 39–45. https://doi.org/10.31276/vjst.65(3).39-45
• Nho, Kyungmoon, and Ramesh Agarwal. 1998. “Automatic Landing System Design Using Fuzzy Logic.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4484
• Ni, Yuanman, Dongkai Dai, Wenfeng Tan, Xingshu Wang, and Shiqiao Qin. 2019. “Attitude-Correlated Frames Adding Approach to Improve Signal-to-Noise Ratio of Star Image for Star Tracker.” Optics Express 27 (11): 15548. https://doi.org/10.1364/oe.27.015548
• Nicholas, Andrew. 2009. Digital Imaging Star Camera. Defense Technical Information Center. https://doi.org/10.21236/ada531850
• Nicholas, W. U., G. L. Naville, J. E. Hoffschwelle, J. K. Huffman, and P. F. Covell. 1984. An Evaluation of the Relative Merits of Wing-Canard, Wing-Tail, and Tailless Arrangements for Advanced Fighter Applications. General Dynamics Corp. https://ntrs.nasa.gov/citations/19840062226
• Nichols, J. O. 1977. Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis. NASA-CR-2835. NASA. https://ntrs.nasa.gov/citations/19770021140
• Nicolaides, John D., and John J. Brady. 1959. Magnus Moment on Pure Cones Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0219843
• Niederer, P. G., and D. J. Mihora. 1972. Ground and Flight Test Program of a Stokes-Flow Parachute: Packaging, Deployment, and Sounding Rocket Integration. NASA-CR-112251. NASA. https://ntrs.nasa.gov/citations/19730010289
• Niehus, Jacob, and Curtis Mracek. 2010. “Laser Guided Rocket Inertial Measurement Unit Performance Determination Using Trajectory Reconstruction.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8323. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8323
• Nielsen, J. 1978. “Nonlinearities in Missile Aerodynamics.” In 16th Aerospace Sciences Meeting. AIAA 1978-20. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-20
• Nielsen, J. 1979. “Missile Aerodynamics: Past, Present, Future.” In Aircraft Systems and Technology Meeting. AIAA 1979-1819. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1819
• Nielsen, Jack N. 1982. Problems Associated with the Aerodynamic Design of Missile Shapes. Defense Technical Information Center. https://doi.org/10.21236/adp001949
• Nielsen, J. 1985. “Arrays for Minimum Wave Drag of Bodies of Revolution.” In 23rd Aerospace Sciences Meeting. AIAA 1985-449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-449
• Nielsen, J. 1986. “Supersonic Wing-Body Inteference at High Angles of Attack with Emphasis on Low Aspect Ratios.” In 24th Aerospace Sciences Meeting. AIAA 1986-568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-568
• Niemela, John. 1982. “The Integrated Inertial Navigation System AN/ASN-132.” Navigation 29 (4): 279–88. https://doi.org/10.1002/j.2161-4296.1982.tb00813.x
• Niespodziany, Sławomir. 2018. “Inertial Navigation Static Calibration.” International Journal of Electronics and Telecommunications. https://doi.org/10.24425/119518
• Niessen, F. R. 1973. A Low-Cost Inertial Smoothing System for Landing Approach Guidance. NASA-TN-D-7271. NASA. https://ntrs.nasa.gov/citations/19730015926
• Nietubicz, Charles J. 1975. Some Aerodynamic Characteristics of Supersonic Lifting Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada009704
• Nietubicz, C., J. Sahu, D. Mylin, and R. Lafarge. 1984. “Aerodynamic Coefficient Predictions for a Projectile Configuration at Transonic Speeds.” In 22nd Aerospace Sciences Meeting. AIAA 1984-326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-326
• Nietubicz, C., and W. Sturek. 1988. “Navier-Stokes Code Verification for Projectile Configurations at Supersonic and Transonic Velocities.” In 15th Aerodynamic Testing Conference. AIAA 1988-1995. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-1995
• Niewald, Roy J., and Martin T. Moul. 1950. The Longitudinal Stability, Control Effectiveness, and Control Hinge Moment Characteristics Obtained from a Flight Investigation of a Canard Missile Configuration at Transonic and Supersonic Speeds. NACA-RM-L50I27. NASA. https://ntrs.nasa.gov/citations/19930086447
• Nikaido, Ben, and Garth V. Hobson. 2025. “RANS Predictions of Inlet/Isolator Unstart at Mach 4.” In AIAA SCITECH 2025 Forum. AIAA 2025-0335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0335
• Nikfetrat, K., C. Van Dam, P. Vijgen, and I. Chang. 1992. “Prediction of Drag at Subsonic and Transonic Speeds Using Euler Methods.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-169
• Nikiforovskii, D. A., I. G. Deineka, I. A. Sharkov, and I. K. Meshkovskii. 2022. “A Method for Fiber Optic Gyroscope Temperature Drift Compensation Using Correlations between the Readings of the Gyroscope and Several Temperature Sensors.” Gyroscopy and Navigation 13 (2): 105–9. https://doi.org/10.1134/s2075108722020055
• Nikitaev, Dennis. 2019. “Air and Space Thermal Rocket Engine with Turbojet (ASTRET).” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4393. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4393
• Niknamian, Sorush. 2019. “‘The Optimization of a Jet Turbojet Engine by PSO and Searching Algorithms’.” Preprint, . https://doi.org/10.31219/osf.io/xh7s9
• Nikolic, Vojin, and Eric Jumper. 2004. “Zero-Lift Wave Drag Calculation Using Supersonic Area Rule and Its Modifications.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-217
• Ning, Xiaolin, Yuqing Yang, Xiaoyu Liang, and Jie Zhang. 2022a. “Accelerometer Bias and Star Sensor Installation Error Joint Calibration for the SINS/CNS Integrated Navigation System Using Attitude Maneuver.” Guidance, Navigation and Control 02 (02): 2250006. https://doi.org/10.1142/s2737480722500066
• Nishino, Hitoshi, Kazusuke Maenaka, and Takahito Ono. 2025. “Proposal for an Ultra-High Accuracy, High-Speed, and Miniaturized Ring-Laser Gyroscope by Optical Frequency Combs.” Preprint, Optica Open. https://doi.org/10.1364/opticaopen.28374407
• Nishiura, Yozo, Mitsuru Nishikawa, Kimizo Ono, and Yuji Kohsaka. 1986. “Phase Modulated Fiber-Optic Gyroscope with Linear Scale Factor.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1986.p9
• Nishiura, Yozo, Kimizo Ono, and Susumu Hiraoka. 1985. “Development of Compact Phase-Modulated Fiber-Optic Gyroscope with Stabilized Scale Factor.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1985.pds6
• Nitin, N. 2024. “Terminal Guidance for Fpv Drones in Kami Kaze Mission Using Computer Vision.” Preprint, . https://doi.org/10.2139/ssrn.5022844
• Niu, Xiaoji, You Li, Quan Zhang, Yahao Cheng, and Chuang Shi. 2012b. “Observability Analysis of Non-Holonomic Constraints for Land-Vehicle Navigation Systems.” Journal of Global Positioning Systems 11 (1): 80–88. https://doi.org/10.5081/jgps.11.1.80
• Niu, Yaobin, Zhongwei Wang, Huixin Yang, and Xixiang Yang. 2012a. “Aerothermoelastic Response of Hypersonic 2-D Lifting Surface.” Fluctuation and Noise Letters 11 (02): 1250017. https://doi.org/10.1142/s0219477512500174
• Nix, W. L. 1959. Heating and Impact Tests on Insulated and Uninsulated Ballisticmissile Fuse Mechanisms Subjected to Simulated Reentry Aerodynamic Heating. NASA-MEMO-12-5-58L. NASA. https://ntrs.nasa.gov/citations/19630004882
• Nixon, David. 2003. “A Relationship between Wave Drag and Induced Drag.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/2003-01-3021
• Noack, Thomas Luther. n.d. “An Optimized Celestial-Inertial Navigation System.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-17380
• Nobahari, Hadi, and Hamed Mohammadkarimi. 2017. “Accuracy Analysis of an Integrated Inertial Navigation System in Slow Maneuvers: Accuracy Analysis of an Integrated INS.” Navigation 64 (2): 197–211. https://doi.org/10.1002/navi.195
• Noble, Edward. 1963. “Optical Research and Development at White Sands Missile Range.” In Space Flight Testing Conference. AIAA 1963-93. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-93
• Noftz, Mark E., and Joseph S. Jewell. 2025. “Unstart Modes of a Streamtraced Busemann Inlet in Mach 6 Quiet Flow.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3620
• Noguchi, Kazuhide, Koshi Sato, Ryouichi Kasikawa, et al. 1996. “CCD Star Tracker for Attitude Determination and Control of a Satellite for a Space VLBI Mission.” In SPIE Proceedings, vol. 2810, edited by E. Kane Casani, Mark A. Vander Does. SPIE. https://doi.org/10.1117/12.255141
• Noneman, S. 2002. “Operations Analysis of the 2nd Generation Reusable Launch Vehicle.” In SpaceOps 2002 Conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-t4-34
• North, B. 1983. “Ablative Material Development for Tomahawk Cruise Missile Launch Canister Application.” In 18th Thermophysics Conference. AIAA 1983-1559. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1559
• North American Aviation INC LOS Angeles CA. 1963. Evaluation of a Mechanical Flight Control Servo. Defense Technical Information Center. https://doi.org/10.21236/ad0410334
• Northam, G., and G. Anderson. 1986. “Survey of Supersonic Combustion Ramjet Research at Langley.” In 24th Aerospace Sciences Meeting. AIAA 1986-159. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-159
• Nosek, T. 1982. “Space Shuttle as a Dynamic Test Tool for High Accuracy Missile Guidance Systems.” In Guidance and Control Conference. AIAA 1982-1502. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1502
• Noureldin, Aboelmagd, Tashfeen B. Karamat, and Jacques Georgy. 2012a. “Inertial Navigation System.” In Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-30466-8_4
• Noureldin, Aboelmagd, Tashfeen B. Karamat, and Jacques Georgy. 2012b. “Inertial Navigation System Modeling.” In Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-30466-8_5
• Noureldin, Aboelmagd, Tashfeen B. Karamat, and Jacques Georgy. 2012c. “Modeling INS Errors by Linear State Equations.” In Fundamentals of Inertial Navigation, Satellite-based Positioning and their Integration. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-30466-8_6
• “A Novel Method Based on a High-Dynamic Hybrid Forecasting Model for Fiber Optic Gyroscope Drift.” 2017. Sensors and Materials: 1. https://doi.org/10.18494/sam.2017.1331
• Novik, David. 1956. An Analog Study of a Shock-Position Diffuser Control on a Supersonic Turbojet Engine. NACA-RM-E56E09a. NASA. https://ntrs.nasa.gov/citations/19930089429
• Nugroho, Larasmoyo, Rika Andiarti, Rini Akmeliawati, and Sastra Kusuma Wijaya. 2024. “Enhancing the Landing Guidance of a Reusable Launch Vehicle by Improving Genetic Algorithm-Based Deep Reinforcement Learning Using Hybrid Deterministic-Stochastic Algorithm.” PLOS ONE 19 (2): e0292539. https://doi.org/10.1371/journal.pone.0292539
• “Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime.” 2019. Tehnicki vjesnik - Technical Gazette 26 (3). https://doi.org/10.17559/tv-20180724143418
• “Numerical Optimization on Approach and Landing for Reusable Launch Vehicle.” 2016. International Journal of Science and Research (IJSR) 5 (6): 1279–83. https://doi.org/10.21275/v5i6.nov164465
• “Numerical Study on Rolling Characteristics of Canard-Controlled Missile with a Free-Spinning Tail.” 2014. In Computer, Intelligent Computing and Education Technology. CRC Press. https://doi.org/10.1201/9781315760827-155
• Nurse, Roy J., John T. Prohaska, and Darold G. Riegsecker. 1978a. A New Baseline for the Inertial Navigation Strapdown Simulator Program. Volume 3. Program and Description and Users Guide. Defense Technical Information Center. https://doi.org/10.21236/ada062809
• Nurse, Roy J., John T. Prohaska, and Darold G. Riegsecker. 1978b. A New Baseline for the Inertial Navigation Strapdown Simulator Program. Volume 4. Program Listings. Defense Technical Information Center. https://doi.org/10.21236/ada062810
• Nusbaum, Uriel, Ilan Rusnak, and Itzik Klein. 2019. “Angular Accelerometer-Based Inertial Navigation System.” Navigation 66 (4): 681–93. https://doi.org/10.1002/navi.336
• Nygaard, Tor, and Robert Meakin. 2002. “An Aerodynamic Analysis of a Spinning Missile with Dithering Canards.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2799
• O’brien, Walter, and Todd Lowe. 2015. Advanced Simulation and Control of Engine Inlet Distortion Using Virginia Tech StreamVane Technology. https://doi.org/10.4050/sm_prop_2015-1484
• O’Brien, Kevin P., and Timothy T. Takahashi. 2023. “Configuration and Control Strategies for Maneuvering Supersonic Flight.” In AIAA AVIATION 2023 Forum. AIAA 2023-3233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3233
• O’Connor, John J. 1975. Transformations Applicable to Missile and Satellite Trajectory Computations. Defense Technical Information Center. https://doi.org/10.21236/ada013969
• O’Connor, Molly, Hanna Millares, Portia Banerjee, George Gorospe, and Naomi Endres. 2020. “Vibration-Based Health Characterization of Multiple IMUs in UAV Applications.” In International Mechanical Engineering Congress & Exposition 2020. https://ntrs.nasa.gov/citations/20205000223
• O’Halloran, W., Jr., and R. Warren. 1972. “Design of a Reduced-State Suboptimal Filter for Self-Calibration of a Terrestrial Inertial Navigation System.” In Guidance and Control Conference. AIAA 1972-849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-849
• O’Kane, T., and J. V. Ringwood. 2013. “Vehicle Speed Estimation Using GPS/RISS (Reduced Inertial Sensor System).” In 24th IET Irish Signals and Systems Conference (ISSC 2013). Institution of Engineering and Technology. https://doi.org/10.1049/ic.2013.0046
• Obikane, Y. 1984. “Numerical Computation of the Reynolds Stress in Supersonic Inlet Flows.” In 20th Joint Propulsion Conference. AIAA 1984-1364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1364
• Obuchovski, Romuald, Petras Petroškevičius, and Darius Popovas. 2014. “Analysis of Vertical Deflection Periodic Variations.” In Environmental engineering. https://doi.org/10.3846/enviro.2014.231
• Oconnor, B. J. 1971. “The ST-224: A Redundant Inertial Measurement System.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19710054363
• Odalović, Oleg, Marko Stanković, Sanja Grekulović, Danilo Joksimović, and Miljana Todorović-Drakul. 2018. “Determination of Deflection of the Vertical Components by Using Global Geopotential Model EGM2008.” Tehnika 73 (3): 333–38. https://doi.org/10.5937/tehnika1803333o
• Ogawa, Hideaki, and Holger Babinsky. 2005. “Evaluation of Wave Drag Reduction by Flow Control.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-1415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1415
• Ogilvie, R. E. 1977. “A New Method of Celestial Navigation.” Navigation 24 (1): 67–71. https://doi.org/10.1002/j.2161-4296.1977.tb01267.x
• Oglesby, T. L. 1975. Space Shuttle Orbiter Approach and Landing Test. NASA Kennedy Space Center. https://ntrs.nasa.gov/citations/19750056555
• Ogletree, G., J. Coccoli, R. McKern, M. Smith, and R. White. 1972a. Apollo Guidance, Navigation, and Control: Candidate Configuration Trade Study, Stellar-Inertial Measurement System (SIMS) for an Earth Observation Satellite (EOS). NASA-CR-115441. NASA. https://ntrs.nasa.gov/citations/19720011004
• Ogletree, G., J. Coccoli, R. McKern, M. Smith, and R. White. 1972b. Candidate Configuration Trade Study, Stellar-Inertial Measurement Systems (SIMS) for an Earth Observation Satellite (EOS). NASA-CR-115709. NASA. https://ntrs.nasa.gov/citations/19720021014
• Ogut, Serdar, Berk Osunluk, and Ekmel Ozbay. 2017. “Modeling of Thermal Sensitivity of a Fiber Optic Gyroscope Coil with Practical Quadrupole Winding.” In SPIE Proceedings, vol. 10208, edited by Christopher S. Baldwin, Gary Pickrell, Henry H. Du. SPIE. https://doi.org/10.1117/12.2258030
• Oh, Youh. 1989. “Three Dimensional Interpolation Method for Missile Aerodynamics.” In 27th Aerospace Sciences Meeting. AIAA 1989-481. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-481
• Oh, Sung Hoon. 2014. “The Development of a Drop Test Device for the Performance Test of the Landing Gear of an Unmanned Aircraft.” Applied Mechanics and Materials 513-517: 4219–22. https://doi.org/10.4028/www.scientific.net/amm.513-517.4219
• Oh, Seung-Min, and Eric Johnson. 2006. “Development of UAV Navigation System Based on Unscented Kalman Filter.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6351
• Oh, Jong, and Vigor Yang. 1994. “Interactions between Shock and Acoustic Waves in a Supersonic Inlet Diffuser.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-2706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2706
• Ohira, Keisuke, and Dong-Youn Kwak. 2014. “Investigation of Turbulence Models for the Supersonic Transport Configuration at Low-Speed and High Alpha Flight Condition.” In 32nd AIAA Applied Aerodynamics Conference. AIAA 2014-3098. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3098
• Ohno, Aritaka, Yutaka Ishii, Suminori Kamimatsuse, Hiroyuki Honma, and Kohsuke Maezawa. 1992. “Miniature SLD Module for Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 1585, edited by Shaoul Ezekiel, Eric Udd. SPIE. https://doi.org/10.1117/12.135059
• Ohno, Aritaka, Shin Masuki, Yoshiki Ikeda, et al. 2026. “Development History and Latest Status of Fiber Optic Gyroscope at JAE.” In Fiber Optic Gyros: 50th Anniversary Conference, edited by Eric Udd, Herve C. Lefevre, Glen A. Sanders. SPIE. https://doi.org/10.1117/12.3094031
• Ohno, Aritaka, Ryuji Usui, Kazuo Suzuki, Kenichi Okada, and Kazuhiro Sakuma. 1994. “Intermediate and Moderate Grade Fiber Optic Gyroscope for Industrial Applications.” In SPIE Proceedings, vol. 2292, edited by Ramon P. DePaula. SPIE. https://doi.org/10.1117/12.191831
• Oishi, Meeko, Ian Mitchell, Alexandre Bayen, Claire Tomlin, Asaf Degani, and Dennis Kega. 2002. Hybrid Verification of an Interface for an Automatic Landing. Stanford Univ. https://ntrs.nasa.gov/citations/20020091923
• Okelah, M. 1985. “The Co-Turbojet Engine: A Novel Concept for Milti-Spool Turbojet Engines.” International Conference on Aerospace Sciences and Aviation Technology 1 (CONFERENCE): 1–10. https://doi.org/10.21608/asat.1985.26520
• Oktaviana, Aditya Tri, Mochammad Ibnu Alwan, Adhi Kusumadjati, and Mikael Syväjärvi. 2026. “Model-Prototype Based Flight Test: Bringing Flight Control Engineering to Life for a Reusable Rocket with Flightgear.” International Journal of Applied Mathematics, Sciences, and Technology for National Defense 4 (1): 57–70. https://doi.org/10.58524/app.sci.def.v4i1.1128
• Olds, B. 1998. Simulated Inertial GPS Navigation Laboratory (SIGNaL). Defense Technical Information Center. https://doi.org/10.21236/ada389224
• Olds, John, and Peter Bellini. 1998. “Argus, a Highly Reusable SSTO Rocket-Based Combined Cycle Launch Vehicle with Maglifter Launch Assist.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1557
• Oliveira, Hallysson, Stiven Dias, and Marcelo G. S. Bruno. 2023. “GNSS-Denied Joint Cooperative Terrain Navigation and Target Tracking Using Factor Graph Geometric Average Fusion.” Preprint, TechRxiv. https://doi.org/10.36227/techrxiv.22305952
• Oliver, James H. 2012. Virtual Teleoperation for Unmanned Aerial Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada561658
• Olsen, Susan R. 2011. Mission Assurance Analysis of Theater Ballistic Missile Defense Systems. Defense Technical Information Center. https://doi.org/10.21236/ada547967
• Ombrello, Timothy, Scott Peltier, and Campbell D. Carter. 2015. “Effects of Inlet Distortion on Cavity Ignition in Supersonic Flow.” In 53rd AIAA Aerospace Sciences Meeting. AIAA 2015-0882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0882
• ONeal, Robert L. 1960. Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and from 2.50 to 4.05. NASA-TM-X-208. NASA. https://ntrs.nasa.gov/citations/19980227361
• Oosthuizen, Pierre. 2006. “Development and on-Orbit Results of the SSTL Low Cost Commercial Star Tracker.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6045
• “Optimal Input Design.” n.d. In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0009026
• Optimization and Simulation of Flight Control Laws under Parameter Uncertainty and External Disturbances. 1979. NASA-CR-163292. NASA. https://ntrs.nasa.gov/citations/19800017828
• “Optimization of Cruising Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0237.0258
• Optimum Digital Filter Study for Strapdown Inertial Navigation System Initial Alignment Final Report, 8 Jan. 1968: 8 Jul. 1968. 1968. NASA-CR-98101. NASA. https://ntrs.nasa.gov/citations/19690001548
• Ordaz, Irian, Sriram K. Rallabhandi, Eric J. Nielsen, and Boris Diskin. 2017. “Mitigation of Engine Inlet Distortion through Adjoint-Based Design.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3410
• Orlando, Robert J. 1994. Ramjet Bypass Duct and Preburner Configuration. Patent Application Number: US-PATENT-APPL-SN-058182. NASA. https://ntrs.nasa.gov/citations/20080003990
• Orme, John, and Glenn Gilyard. 1993. “Preliminary Supersonic Flight Test Evaluation of Performance Seeking Control.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1821
• Orme, Andrew, Steve Gorrell, and Addison Pulsiver. 2021. “Effects of Inlet Distortion Patterns on Induced Swirl in a Highly Loaded Fan Stage.” Preprint, . https://doi.org/10.1115/1.0002519v
• Ormsby, Charles C., and Harvey S. Long. 1980. “Potential Applications of Video Disc Technology to Missile Guidance.” In SPIE Proceedings, vol. 0238, edited by Thomas F. Wiener. SPIE. https://doi.org/10.1117/12.959146
• Ortiz, Gerardo G., and Shinhak Lee. 2006. “Star Tracker Based ATP System Conceptual Design and Pointing Accuracy Estimation.” In SPIE Proceedings, vol. 6105, edited by G. Stephen Mecherle. SPIE. https://doi.org/10.1117/12.660263
• Osder, S. S. 1970. Terminal Control and Automatic Landing of Unpowered Space Shuttle Vehicles. Sperry Phoenix Co. https://ntrs.nasa.gov/citations/19700031646
• Osipov, K. A. 2019. “The Influence of Features of Vortex Flow on Aerodynamic Characteristics of the Supersonic Maneuverable Aircraft Model.” Civil Aviation High TECHNOLOGIES 22 (1): 63–75. https://doi.org/10.26467/2079-0619-2019-22-1-63-75
• Ostgaard, M. A. 1962. “Flight Control System Design for Supersonic Transport.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/620343
• Ostner, Charles F. 1962. A Fortran Program to Calculate a Ballistic Missile Trajectory from Burn out to Impact. Defense Technical Information Center. https://doi.org/10.21236/ad0414825
• Ostoich, Chrisopher, Daniel J. Bodony, and Philippe Geubelle. 2013. “Aerothermoelastic Response of a Panel under a High Speed Turbulent Boundary Layer Using Direct Numerical Simulation.” In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2013-1662. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1662
• Ostowari, C., and D. Naik. 1986. An Experimental Study of the Lift, Drag and Static Longitudinal Stability for a Three Lifting Surface Configuration. AIAA PAPER 86-0398. Texas A&M Univ. https://ntrs.nasa.gov/citations/19860041891
• Ostrander, M., M. Thomas, and J. Clegern. 1995. “Inlet Analysis for ATR-Powered Supersonic Missile.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2805
• Oswatitsch, Klaus. 1980. “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (the Efficiency of Shock Diffusers).” In Contributions to the Development of Gasdynamics. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-91082-0_18
• Otsap, B., and G. Yankura. 1967. “A Fluidic Fuel Control System for an Advanced Ramjet Engine.” In 3rd Propulsion Joint Specialist Conference. AIAA 1967-497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-497
• Ott, Leo Edward. n.d. “Kalman Filter with Complementary Constraint and Integrated Navigation Systems Applications.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180815-307
• Ott, Lee, and Leo Edward Ott. 1979. “A New Integrated Radio Navigation System Describes New Lo-Cost, High-Accuracy Integrated Radio Navigation System.” In All Days. https://doi.org/10.4043/3552-ms
• Otten, D. D. 1966. A Look into Strap-down Guidance Design. I.. NASA. https://ntrs.nasa.gov/citations/19670031760
• Otter, Pieter W. 1985. “Parameter Identifiability, Prediction-Error Estimation and Model Check.” In Lecture Notes in Economics and Mathematical Systems. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-45593-3_5
• Otter, Pieter W. 1986. “Dynamic Structural Systems under Indirect Observation: Identifiability and Estimation Aspects from a System Theoretic Perspective.” Psychometrika 51 (3): 415–28. https://doi.org/10.1007/bf02294064
• Ouarti, Nawel, Gérard Lavergne, and Dominique Bissieres. 2003. “Modeling of the Spray Ignition for Turbojet Engine in-Flight Re-Light.” In 1st International Energy Conversion Engineering Conference (IECEC). AIAA 2003-6053. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-6053
• Ouellette, G. A., J. P. Gilmore, and G. S. Nurre. 1974. “Influence of Precision Inertial Systems on Astronomical Observations.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19740059061
• Outamazirt, Fariz, Muhammad Ushaq, Yan Lin, and Li Hua Fu. 2013. “Enhanced Accuracy Navigation Solutions Realized through SINS/GPS Integrated Navigation System.” Applied Mechanics and Materials 332: 79–85. https://doi.org/10.4028/www.scientific.net/amm.332.79
• Overall, B. W. 1976. Evaluation of an Airjet Distortion Generator Used to Produce Steady- State, Total-Pressure Distortion at the Inlet of Turbine Engines. Defense Technical Information Center. https://doi.org/10.21236/ada033883
• Owen, T., M. Meindl, and J. Fellerhoff. 1997. High Accuracy Integrated Global Positioning System/inertial Navigation System LDRD: Final Report. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/465885
• Owens, L. R., R. A. Wahls, M. B. Elzey, and M. P. Hamner. 2002. “Reynolds Number Effects on the Stability and Control Characteristics of a Supersonic Transport.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20020023445
• Oza, Utsav, Zhiwei Hu, and Xin Zhang. 2015. “Effect of Cavity Flow on Landing Gear Aerodynamic Loads.” In 22nd AIAA Computational Fluid Dynamics Conference. AIAA 2015-2288. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2288
• Ozcatalbas, Mustafa, Bulent Acar, and Sitki Uslu. 2020. “Effect of Free-Play and Initial Conditions on Aeroelastic Behavior of a Missile Canard in Supersonic Flow.” In AIAA Aviation 2020 Forum. AIAA 2020-2663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2663
• Özger, E. 2012. “Parameter Estimation of Highly Unstable Aircraft Assuming Linear Errors.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4511. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4511
• Ozger, Erol. 2013. “Parameter Estimation of Highly Unstable Aircraft Assuming Nonlinear Errors.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-4751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4751
• Pace, Charles, Allan Mense, and David King. 2008. “Air Launched Cruise Missile Reliability Assessment for Ground and Flight Test Data.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1617
• Paces, Pavel. 2014. “Navigation and Payload Sensors: Inertial Navigation System, Accelerometers, Gyroscopes, Global Navigation Satellite System. Electronics Associated with the Digital Measurement Chain. Analysis and Design of Instrumentation. Bus Systems Instrumentation.” Instrumentation viewpoint, no. 16: 27–27. https://doi.org/10.5821/iwp.2014.16.15180
• Padhi, Radhakant, S. Tiwari, Abhijit Bhattacharyya, and R. Padhi. 2010. “A ZEM Based Effective Integrated Estimation and Guidance of Interceptors in Terminal Phase.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8318
• Padro, Jorge, Jonathon Wright, and Eric Swenson. 2012. “Development of a Star Tracker-Based Reference System for Accurate Attitude Determination of a Simulated Satellite.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2012-4498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4498
• Pagan, D., O. Benoit, L. Serre, and D. Colliquet. 2001. “Chefren: Scale 1 Free Jet Testing of a Supersonic Ramjet Missile.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3293
• Page, William A. 1956a. Experimental Determination of the Range of Applicability of the Transonic Area Rule for Wings of Triangular Plan Form. NACA-TN-3872. NASA. https://ntrs.nasa.gov/citations/19930084647
• Page, William A. 1956b. Influence of the Body Flow Field on the Zero-Lift Wave Drag of Wing-Body Combinations Modified in Accordance with the Transonic Area Rule. NACA-RM-A55K10. NASA. https://ntrs.nasa.gov/citations/19930088967
• Page, Don, Fred Gloyna, and David Earls. 1992. “Environmental Mission Profile Facility for Reliability Testing of Multiple Cruise Missile Electronic Boxes.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3893
• Page, James H., Paul Hield, and Paul G. Tucker. 2017. “Effect of Inlet Distortion Features on Transonic Fan Rotor Stall.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2017-64612
• Paik, H. J. 1981a. A Spaceborne Superconducting Gravity Gradiometer for Mapping the Earth’s Gravity Field. Maryland, University. https://ntrs.nasa.gov/citations/19830028807
• Paik, H. J. 1981b. Superconducting Tensor Gravity Gradiometer. Maryland, University. https://ntrs.nasa.gov/citations/19820039510
• Paik, H. J. 1985. “Geodesy and Gravity Experiment in Earth Orbit Using a Superconducting Gravity Gradiometer.” IEEE Transactions on Geoscience and Remote Sensing GE-23. https://ntrs.nasa.gov/citations/19850060320
• Paik, Ho Jung. 1987. Three-Axis Superconducting Gravity Gradiometer. ISSN: 0145-319X. University of Maryland. https://ntrs.nasa.gov/citations/19870000559
• Paik, Ho Jung, Jurn-Sun Leung, Samuel H. Morgan, and Joseph Parker. 1988. “Global Gravity Survey by an Orbiting Gravity Gradiometer.” EOS 69. https://ntrs.nasa.gov/citations/19890052178
• Paik, H. J., and J. P. Richard. 1986. Development of a Sensitive Superconducting Gravity Gradiometer for Geological and Navigational Applications. NASA-CR-4011. NASA. https://ntrs.nasa.gov/citations/19870003588
• Painter, Chris C., and Andrei M. Shkel. 2001. “Structural and Thermal Analysis of a MEMS Angular Gyroscope.” In SPIE Proceedings, vol. 4334, edited by Vijay K. Varadan. SPIE. https://doi.org/10.1117/12.436630
• Pak, Jin Myong, Ji Myong Kim, Ryong Hun Paek, and Jin Su Pak. 2023. “Improving Multiple Mems Gyroscope Array Accuracy Based on Stkf.” Preprint, . https://doi.org/10.2139/ssrn.4564470
• Palchekovskaya, Natalia. 2019. “Aerodynamic Peculiarities of Flow over a Space Vehicle at Transonic and Supersonic Velocities.” International Journal of Fluid Mechanics Research 46 (3): 211–18. https://doi.org/10.1615/interjfluidmechres.2018025652
• Paletta, Nicola, Marika Belardo, and Luigi Di Palma. 2013. “An Automatic Procedure for the Landing Gear Conceptual Design of a Light Unmanned Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2013-01-2188
• Palko, R. 1972. “Full-Scale Inlet/engine Testing at High Maneuvering Angles at Transonic Velocities.” In 7th Aerodynamic Testing Conference. AIAA 1972-1026. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1026
• Palko, R. L. 1974. Experimental Verification of a Transonic Test Technique for Full-Scale Inlet/Engine Systems Simulating Maneuvering Attitudes. Defense Technical Information Center. https://doi.org/10.21236/ad0787659
• Palko, R. L. 1975. Aerodynamic Loads on Devices for Simulating Inlet/Engine Flow Conditions and Effects of Test Installation on Tunnel Operation. Defense Technical Information Center. https://doi.org/10.21236/ada012880
• Palmer, J. R. 1956. “Some Aspects of Turbojet Performance Calculation at High Flight Mach Numbers: Problems of Performance Prediction in Truly Supersonic Engines.” Aircraft Engineering and Aerospace Technology 28 (11): 376–80. https://doi.org/10.1108/eb032757
• Palmer, William E., Robert R. Howell, and Albert L. Braslow. 1956. Transonic Investigation at Lifting Conditions of Streamline Contouring in the Sweptback-Wing-Fuselage Juncture in Combination with the Transonic Area Rule. NACA-RM-L56D11a. NASA. https://ntrs.nasa.gov/citations/19930089285
• Palmer, Richard R., and Donald F. McAllister. 1962. “Multiple Inertial System Operation in Long Term Navigation.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395586-9.50019-2
• Palomino, Amparo, Stephania Romero, Juan Antonio Escareno Castro, and Sergio Vergara. 2026. “Bio-Inspired Signal Processing Framework for Uncertainty Estimation in Inertial Systems on a Two-Degree-of-Freedom UAV Platform.” Preprint, . https://doi.org/10.2139/ssrn.7099933
• Pampreen, Ron. 1986. Engine Studies for Future Subsonic Cruise Missiles. AIAA PAPER 86-1547. Williams International. https://ntrs.nasa.gov/citations/19870034239
• Pan, Jiaxing, Jiajia Ma, Junhua Huang, and Chong Sun. 2025b. “A Novel Attack Missile Guidance Method Considering the Terminal Angle Constraint of the Attack Missile-Target-Defense Missile Game.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2204-7_23
• Pan, Zhaolei, and Yangjun Pi. 2024. “Design of an Automatic Landing Strategy for Fixed-Wing Aircraft Based on Longitudinal and Lateral Collaborative Hierarchical Control.” Preprint, . https://doi.org/10.2139/ssrn.5047766
• Pan, Xudong, Fan Yang, and Yi Wu. 2025a. A GNSS-Aid Star Camera Fusion Approach towards Statistically Optimal Attitude Determination of Ll-SST Missions. https://doi.org/10.5194/egusphere-egu25-5406
• Panayotov, Hristian, Stanimir Penchev, and Dancho Kolibarov. 2017. “Experimental Study of Canard UAV Aerodynamics.” MATEC Web of Conferences 133: 01002. https://doi.org/10.1051/matecconf/201713301002
• Pang, Minjian. n.d. “Multi-State Constraint Kalman Filter Based Visual Inertial Navigation System for Monocular, Stereo and RGB-D Cameras.” PhD diss., The Hong Kong University of Science and Technology. https://doi.org/10.14711/thesis-991012636967903412
• Pang, Lu, Rui-chen Li, Bang-cai Huang, and Ding Ning. 2008. “Φ80μm Polarization-Maintaining Fiber Coupler for Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 7278, edited by Dieter S. Jäger, Deming Liu, Ping Shum. SPIE. https://doi.org/10.1117/12.822824
• Pankkonen, Antti. 2011. “Method for Rapid Modelling of Missile Aerodynamics.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6265
• Panneerselvam, S., C. Vasantharaj, M. Ramaswamy, and S. Santhakumar. 1996. “Aerodynamic Characteristics and Separation Dynamics of Nose Petal of a Missile.” In 14th Applied Aerodynamics Conference. AIAA 1996-2478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2478
• Pantaleoni, Mauro, Marcus Kirsch, Jim Martin, Alastair McDonald, and Mark Tuttlebee. 2010. “XMM-Newton Star Tracker Blemish Pixels: The New Treatment Strategy.” In SpaceOps 2010 Conference. AIAA 2010-1980. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1980
• Paoletti, F. 1996. “A Silicon Micromachined Tuning Fork Gyroscope.” In IEE Colloquium on Silicon Fabricated Inertial Instruments, vol. 1996. IEE. https://doi.org/10.1049/ic:19961215
• Papadopoulos, C. 1998. “The Development of a Total System Aircraft Landing Control Scheme.” In International Conference on Simulation (1998), vol. 1998. IEE. https://doi.org/10.1049/cp:19980634
• Papoutsis-Kiachagias, Evangelos, Varvara Asouti, and Kyriakos Giannakoglou. 2021. “Assessment of Variants of the Method of Moments and Polynomial Chaos Approaches to Aerodynamic Uncertainty Quantification.” In Proceedings of the 4th International Conference on Uncertainty Quantification in Computational Sciences and Engineering (UNCECOMP 2019). Institute of Research and Development for Computational Methods in Engineering Sciences (ICMES). https://doi.org/10.7712/120221.8043.19104
• Papp, Zoltan, and Andrea Rožnjik. 2022. “A Method for Approximating Circular Error Probable.” In NATO Science for Peace and Security Series C: Environmental Security. Springer Netherlands. https://doi.org/10.1007/978-94-024-2174-3_3
• Parellier, Colin. n.d. “Backpropagation Gradients through the Kalman Filter with Applications to Fault Detection and Navigation.” PhD diss., Université Paris sciences et lettres. https://doi.org/10.70675/9e54099fzd487z43d7zb444zb38e2812e945
• Paris, Alfonso, and Michael Bonner. 2003. “Nonlinear Model Development from Flight Test Data for the F/A-18E Super Hornet.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5535. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5535
• Parise, Keith. 1992. “Functional Ground Testing: Evaluating the Tomahawk Cruise Missile.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-202
• Park, Jaehun. 2025. “Statistical Adjustment Methods for Sample Size Reduction in Guided Missile Reliability Demonstration.” Journal of Applied Reliability 25 (4): 324–34. https://doi.org/10.33162/jar.2025.12.25.4.324
• Park, Haerhee, Jinsil Lee, and Jiyun Lee. 2022. “Error Modelling Method of Extended Kalman Filter-Based Terrain Referenced Navigation System for Integrity Assurance under Nominal Conditions.” IET Radar, Sonar & Navigation 16 (9): 1516–29. https://doi.org/10.1049/rsn2.12277
• Park, Jun-su, and Soon-Yong Park. 2021. “Visual Inertial Navigation System Optimization Using the Depth of Features with Stereo.” Journal of the Institute of Electronics and Information Engineers 58 (7): 77–87. https://doi.org/10.5573/ieie.2021.58.7.77
• Parker, J. B. 1956. “Acceleration Errors in Astro-Navigation.” Journal of Navigation 9 (1): 17–19. https://doi.org/10.1017/s0373463300046737
• Parker, R., and J. Templeman. 1967. “Automatic Landing System 727 Airplane.” In Control and Flight Dynamics Conference. AIAA 1967-573. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-573
• Parkhomey, Igor, Juliy Boiko, Irina Zeniv, and Taras Bondarenko. 2023. “Method for Measuring Voltages in Channels of a Hemispherical Resonator Gyroscope with an Arbitrary Orientation Axes.” Indonesian Journal of Electrical Engineering and Computer Science 29 (2): 715. https://doi.org/10.11591/ijeecs.v29.i2.pp715-724
• Parkinson, B. W., and K. T. Fitzgibbon. 1989. “Aircraft Automatic Landing Systems Using GPS.” Journal of Navigation 42 (1): 47–59. https://doi.org/10.1017/s0373463300015083
• Parkinson, Bradford W., Michael W. Wynne, and Leonard R. Kruczynski. 1973. Sight Line Autopilot: A New Concept in Air Weapons. Defense Technical Information Center. https://doi.org/10.21236/ada005402
• Parks, James H. 1954. Experimental Evidence of Sustained Coupled Longitudinal and Lateral Oscillations from a Rocket-Propelled Model of a 35 Degree Swept Wing Airplane Configuration. NACA-RM-L54D15. NASA. https://ntrs.nasa.gov/citations/19930088234
• Parks, James H., and Alan B. Kehlet. 1952. Longitudinal Stability, Trim, and Drag Characteristics of a Rocket-Propelled Model of an Airplane Configuration Having a 45 Degree Sweptback Wing and an Unswept Horizontal Tail. NACA-RM-L52F05. NASA. https://ntrs.nasa.gov/citations/19930087101
• Parlini, F. 1983. “Applications of Inertial Systems as Flight Test Sensors.” In 2nd Flight Testing Conference. AIAA 1983-2738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2738
• Parsons, Delbert. 1966. “Reliability Demonstration Shillelagh Missile Subsystem.” In Symposium on Deep Submergence Propulsion and Marine Systems. AIAA 1966-2592. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-2592
• “Part I Inertial Navigation.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0013.0013
• “Part Ii Inertial Navigation with Aids.” 1997. In Fundamentals Of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866463.0179.0179
• Paschal, N., C. Tournes, and P. Wilkerson. 2001. “Integrated Terminal Guidance and Automatic Pilot Using Subspace-Stabilization.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4275
• Pasik, D., M. Gneses, and G. Taylor. 1975. “A Ring Laser Gyro Strapdown Inertial Navigation System: Performanceanalysis and Test Results.” In Guidance and Control Conference. AIAA 1975-1095. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1095
• Passenheim, B. C., and C. E. Mallon. 1978. “Nuclear Radiation Vulnerability of Ring Laser Gyroscope.” In SPIE Proceedings, vol. 0157, edited by Shaoul Ezekiel, G. E. Knausenberger. SPIE. https://doi.org/10.1117/12.965486
• Passera, Anthony L. 1951. A Theoretical Investigation of the Influence of Autopilot Natural Frequency upon the Dynamic Performance Characteristics of a Supersonic Canard Missile Configuration with a Pitch-Attitude Control System. NACA-RM-L51H02. NASA. https://ntrs.nasa.gov/citations/19930086730
• Patel, Mehul, Jack DiCocco, Troy Prince, and Terry Ng. 2003. “Afterbody Flow Control for Low-Alpha Missile Maneuvering.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3673
• Patrick, A. M. 1972. “Automatic Landing and Microwave Guidance System Potential.” Aircraft Engineering and Aerospace Technology 44 (8): 19–22. https://doi.org/10.1108/eb034932
• Paull, A., R. J. Stalker, and D. J. Mee. 1995. “Experiments on Supersonic Combustion Ramjet Propulsion in a Shock Tunnel.” Journal of Fluid Mechanics 296: 159–83. https://doi.org/10.1017/s0022112095002096
• Paulsen, Thomas, and Luca Maresi. 2000. “Calibration and Verification of the TERMA Star Tracker for the NEMO Satellite.” In Space 2000 Conference and Exposition. AIAA 2000-5338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-5338
• Paulson, J. W., Jr., and J. L. Thomas. 1978. Effect of Twist and Camber on the Low-Speed Aerodynamic Characteristics of a Powered Close-Coupled Wing-Canard Configuration. NASA-TM-78722. NASA. https://ntrs.nasa.gov/citations/19780018153
• Paulson, J. W., Jr., J. L. Thomas, and M. M. Winston. 1979. “Transition Aerodynamics for Close-Coupled Wing-Canard Configuration.” In American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19790035660
• Pavlath, George. 1995. “Development of Inertial-Grade Fiber Gyros.” In Guidance, Navigation, and Control Conference. AIAA 1995-3231. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3231
• Pawlak, Rex. 1994. “Real Time Display of Flight Test Data.” In Biennial Flight Test Conference. AIAA 1994-2116. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2116
• Payne, J. 1968. “An Investigation of Optimization Criteria for the Aircraft Landing Flare Maneuver.” In 6th Aerospace Sciences Meeting. AIAA 1968-57. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-57
• Payne, David P., Robert B. Shoaf, and Hubert P. Koesters. 1975. Developmental Test of the Honeywell Laser Inertial Navigation System (LINS). Defense Technical Information Center. https://doi.org/10.21236/adb008929
• Paynter, Gerald. 1994. “CFD Status for Supersonic Inlet Design Support.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-465
• Paynter, G., and H. Chen. 1983. “Progress toward the Analysis of Supersonic Inlet Flows.” In 19th Joint Propulsion Conference. AIAA 1983-1371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1371
• Paynter, Gerald, David Mayer, and Elling Tjonneland. 1993. “Flow Stability Issues in Supersonic Inlet Flow Analyses.” In 31st Aerospace Sciences Meeting. AIAA 1993-290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-290
• Paynter, G. C., and E. Tjonneland. 1992. “Accuracy Issues in the Prediction of Supersonic Inlet Flows.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-400
• Paynter, Gerald, David Treiber, and W. Kneeling. 1992. “Modeling Supersonic Inlet Boundary Layer Bleed Roughness.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-269
• Pearson, Allan E. 1992. Parameter Identification for Nonlinear Aerodynamic Systems. NASA-CR-190264. NASA. https://ntrs.nasa.gov/citations/19920020086
• Pearson, A. E. 1995. Aerodynamic Parameter Estimation via Fourier Modulating Function Techniques. NASA-CR-4654. NASA. https://ntrs.nasa.gov/citations/19950018210
• Pearson, J. A., R. W. Bruce, Y. T. Chiu, W. A. Feess, and E. G. Fotou. 1973. The Low-G Accelerometer Calibration System Orbital Accelerometer Experiment. Volume 2. Experiment Analyses and Results. Defense Technical Information Center. https://doi.org/10.21236/ad0772718
• Pečinka, Jiří, Gabriel Thomas Bugajski, Petr Kmoch, and Adolf Jílek. 2017. “Jet Engine Inlet Distortion Screen and Descriptor Evaluation.” Acta Polytechnica 57 (1): 22–31. https://doi.org/10.14311/ap.2017.57.0022
• Peck, Robert F., and Lucille C. Coltrane. 1955. Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-Propelled Airplane Model Having a 60 Degree Delta Wing and Low Swept Horizontal Tail. NACA-RM-L55F27. NASA. https://ntrs.nasa.gov/citations/19930088863
• Pedrotty, Samuel M. n.d. COTS Camera and Computer-Based Open-Source Star Tracker. Johnson Space Center. https://ntrs.nasa.gov/citations/20210026330
• Pedrotty, Samuel, Ronney Lovelace, John Christian, Devin Renshaw, and Grace Quintero. 2020. “Design and Performance of an Open-Source Star Tracker Algorithm on Commercial off-The-Shelf Cameras and Computers.” In American Astronomical Society. https://ntrs.nasa.gov/citations/20200001376
• Peery, Steven D., and Randy C. Parsley. 1996. “Merits of Full Flow vs. Conventional Staged Combustion Cycles for Reusable Launch Vehicle Propulsion.” In AIP Conference Proceedings, vol. 361. AIP. https://doi.org/10.1063/1.49964
• Peijie, wu, zhu Zhanke, and Xizheng Ke. 2025. “Experimental Evaluation of a Vision-Aided Inertial Navigation System.” Preprint, . https://doi.org/10.2139/ssrn.5372497
• Pejsa, A. 1973. “Optimum Skewed Redundant Inertial Navigators.” In Guidance and Control Conference. AIAA 1973-850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-850
• Pella, Peter. 2018. “Ballistic Missile Threats.” In The Continuing Quest for Missile Defense. Morgan & Claypool Publishers. https://doi.org/10.1088/978-1-6817-4942-6ch4
• Pelosi, Michael, and Amie Honeycutt. 2017. “Cruise Missile Integrated Air Defense System Penetration: Modeling the S-400 System.” International Journal of Aviation, Aeronautics, and Aerospace. https://doi.org/10.15394/ijaaa.2017.1104
• Peng, Gangding, Shangyuan Huang, and Zongqi Lin. 1987. “New Heterodyne Fiber-Optic Gyroscope Using an Electrooptic Frequency Shifter.” In Optical Fiber Communication. OSA. https://doi.org/10.1364/ofc.1987.tuq13
• Pepitone, T., and I. Jacobson. 1977. “Resonant Behavior of a Symmetric Missile Having Roll Orientation-Dependent Aerodynamics.” In Guidance and Control Conference. AIAA 1977-1127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1127
• Pepper, David M., and Harry T. M. Wang. 1983. Nuclear Magnetic Resonance Gyroscope. Defense Technical Information Center. https://doi.org/10.21236/ada130102
• Percival, Jeffrey W., Kenneth H. Nordsieck, and Kurt P. Jaehnig. 2008. “The ST5000: A High-Precision Star Tracker and Attitude Determination System.” In SPIE Proceedings, edited by Jacobus M. Oschmann Jr., Mattheus W. M. de Graauw, Howard A. MacEwen. SPIE. https://doi.org/10.1117/12.787917
• Perez, D., and W. Benner. 1973. “Development of an Air Cushion Landing System.” In 5th Aircraft Design,Flight Test and Operations Meeting. AIAA 1973-812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-812
• Perkins, Adrien, Yu-Hsuan Chen, Sherman Lo, Chiawei Lee, and J. David Powell. 2019. “Real-Time Unmanned Aerial System (UAS) Based Interference Localization in a GNSS Denied Environment.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2019.16992
• Perkins, P. J., D. F. Schultz, and J. D. Wear. 1971. Full Scale Tests of a Short Length, Double Annular Ram Induction Turbojet Combustor for Supersonic Flight. NASA-TN-D-6254. NASA. https://ntrs.nasa.gov/citations/19710010816
• Perkins, Jared, Tyler Wills, Amy Underwood, and May Win Thein. 2012. “Dynamic Implementation of the Celestial Navigation (CelNav) Technique for Extraterrestrial Surface Navigation.” In AIAA/AAS Astrodynamics Specialist Conference. AIAA 2012-4663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4663
• Perrins, Erik. 2012. System Design for FEC in Aeronautical Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ada557598
• Perry, I. T. 1967. “Automating Long-Range Air Navigation Practices and Procedures.” Journal of Navigation 20 (4): 507–24. https://doi.org/10.1017/s0373463300030836
• Pertica, Alex, and Laura White. 2018. Monolithic Telescope-Based Star Tracker Final Report CRADA No. TC02205.0. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1435453
• Pertica, Alex, Laura White, and Dan Petrovich. 2021. Monolithic Telescope-Based Star Tracker. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1773589
• Peshekhonov, V. G. 2020. “Problem of the Vertical Deflection in High-Precision Inertial Navigation.” Gyroscopy and Navigation 11 (4): 255–62. https://doi.org/10.1134/s2075108720040094
• Peshkov, R. A., P. L. Loginova, and P. A. Tret’yakov. 2026. “Numerical Simulation of Resistance to Vibro-Acoustic Loads of Electronic Components of Reusable Launch Vehicles at the Launch and Landing Stage.” Russian Aeronautics 69 (2): 273–82. https://doi.org/10.3103/s1068799826020017
• Peter, Florian, Fabian Hellmundt, Florian Holzapfel, and Farhana Chew. 2013. “Anti-Windup Command Filtered Adaptive Backstepping Autopilot Design for a Tail-Controlled Air-Defense Missile.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5013
• Peters, R. 1978. “A Dynamic Angular Calibration System for Broadband Microradian Inertial Sensors.” In Guidance and Control Conference. AIAA 1978-1253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1253
• Peters, W. 1985. “A Simulation Technique for Jet Temperature Effects on Nozzle-Afterbody Drag at Transonic Mach Numbers.” In 21st Joint Propulsion Conference. AIAA 1985-1463. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1463
• Peters, Thomas, Thomas Bürgener, and Leonhard Fottner. 2001. “Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor.” In Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/2001-gt-0300
• Petersen, R. H. 1960. The Effects of Wing-Tip Droop on the Aerodynamic Characteristics of a Delta-Wing Aircraft at Supersonic Speeds. NASA-TM-X-363. NASA. https://ntrs.nasa.gov/citations/19660010439
• Petersen, K. 1981. “Flight Experience with a Remotely Augmented Vehicle Flight Test Technique.” In 1st Flight Test Conference. AIAA 1981-2417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2417
• Petersen, Christopher, Morgan Baldwin, and Ilya Kolmanovsky. 2013. “Model Predictive Control Guidance with Extended Command Governor Inner-Loop Flight Control for Hypersonic Vehicles.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5028
• Petersen, Ian R., Valery A. Ugrinovskii, and Andrey V. Savkin. 2000. “Missile Autopilot Design via Minimax Optimal Control of Stochastic Uncertain Systems.” In Communications and Control Engineering. Springer London. https://doi.org/10.1007/978-1-4471-0447-6_10
• Peterson, Victor L. 1961. Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22: Triangular Wing and Canard with Twin Vertical Tails. NASA-TN-D-1033. NASA. https://ntrs.nasa.gov/citations/19980227076
• Peterson, Victor L., and Gene P. Menees. 1961. Aerodynamic Loads at Mach Numbers from 0.70 to 2.22 on a Airplane Model Having a Wing and Canard of Triangular Plan Form and Either Single or Twin Vertical Tails. NASA-TN-D-690. NASA. https://ntrs.nasa.gov/citations/20040008213
• Petrenko, O. V. 2014. “Desing Analysis and Parameters Choice of Metallic Cylindrical Resonator Sensor for Coriolis Vibratory Gyroscope.” Electronics and Control Systems 2 (40). https://doi.org/10.18372/1990-5548.40.7444
• Petrishchev, V. F. 2018. “Energy-Saving Algorithm of Automatic Control of Compulsory Passenger Carrier Landing. Part 1.” Mekhatronika, Avtomatizatsiya, Upravlenie 19 (11): 725–33. https://doi.org/10.17587/mau.19.725-733
• Petrochenkov, Sergey. 2025. “A Project for a Wide-Range of Payload-Carrying Space Transport System Based on Returnable Cruise Missile Units.” Universum:Technical sciences 4 (133). https://doi.org/10.32743/unitech.2025.133.4.19719
• Petrov, B. N., E. I. Mitroshin, V. A. Glinskiy, and A. P. Sorokin. 1980. “Sequence-Algorithms of Descent and Pre-Landing Maneuvers Control in a Hypersonic Spacecraft.” In Automatic Control in Space. Elsevier. https://doi.org/10.1016/b978-0-08-024449-5.50022-9
• Pfaff, Larry J. 1965. Force and Pressure Tests on a Semi-Span Delta Wing at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0467448
• Pfaff, Larry J. 1968. Lift-to-Drag Ratios of Semispan Delta Wing Configurations at Supersonic and Hypersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ad0832104
• Pfeiffer, Neal. 1988a. “Flowfield Study at the Propeller Disks of a Twin Pusher, Canard Aircraft.” In 6th Applied Aerodynamics Conference. AIAA 1988-2511. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2511
• Pfeiffer, Neal. 1988b. “Wake Rake Studies behind a Swept Surface, Canard Aircraft.” In 6th Applied Aerodynamics Conference. AIAA 1988-2552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2552
• Pfenneberger, F. 1966. “Experimental Control-Wing Hinge Moments of a Transonic-Supersonic, Rolling, Maneuvering, Guided Missile.” In 2nd Aerodynamic Testing Conference. AIAA 1966-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-755
• Pfifer, Harald, Simon Hecker, and Gunther Michalka. 2009. “LFT-Based Stability Analysis of a Generic Guided Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6075
• Pfohl, Louis, Walter Rusnak, Albert Jircitano, and Andrew Grierson. 1988. Moving Base Gravity Gradiometer Survey (GGSS) Program. Defense Technical Information Center. https://doi.org/10.21236/ada198956
• Pfyl, F. A. 1952. Wind-Tunnel Investigation of the Aerodynamic Characteristics of a 0.07-Scale Model of the North American MX-770 Missile. NACA-RM-SA52E07. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19710073552
• Pfyl, Frank A. 1955. An Investigation of the Effects of Nose and Lip Shapes for an Underslung Scoop Inlet at Mach Numbers from 0 to 1.9. NACA-RM-A55G13. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/19650003100
• Phillips, Kerri B. n.d. “Aircraft Parameter Identification for Application within a Fault-Tolerant Flight Control System.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.3049
• Phillips, Norman S., Richard W. Carr, and Richard S. Scranton. 1973. Crashworthy Landing Gear Study. Defense Technical Information Center. https://doi.org/10.21236/ad0765489
• Phillips, Craig, and James Chisholm. 1995. “Missile Guidance and Control Challenges for Short Range Anti-Air Warfare.” In Guidance, Navigation, and Control Conference. AIAA 1995-3282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3282
• Phillips, W. P., H. R. Compton, and J. T. Findlay. 1983a. Base Drag Determination for STS Flights 1-5. AIAA PAPER 83-2719. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840029531
• Picard, Mary. 2002. F/A-18A/B/C/D Main Landing Gear Control Unit Hydraulic 2A Supply Line Pressure Spikes and Emergency Port Restrictor Ground and Flight Tests Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada409130
• Picard, Mary, and Scott Whitley. 2002. F/A-18A/B/C/D F404-GE-400/402 Engine Slotted Spraybar Inlet Flameholder Follow-On Flight Test Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada407860
• Piccirillo, Albert. 1998. “Heinkel and the Turbojet Engine: Origin of the First Jet Fighter.” In AIAA and SAE, 1998 World Aviation Conference. AIAA 1998-5598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5598
• Piccolo Serafim, Luisa, Kirk Brouwer, and Earl H. Dowell. 2025. “Correlation of Mathematical Model with AFRL RC-19 Aerothermoelastic Experiment Including an Impinging Shock.” In AIAA Aviation Forum and Ascend 2025. AIAA 2025-3381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-3381
• Pick, T. 1986. “The MULTISENSOR Inertial Measurement Unit (MIMU): A Low-Cost Technology for Tactical Applications.” In Astrodynamics Conference. AIAA 1986-2209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2209
• Pickering, Keith A. 1999. “Comments on “the Celestial Navigation of Christopher Columbus”.” Navigation 46 (3): 227–30. https://doi.org/10.1002/j.2161-4296.1999.tb02409.x
• Pidvysotskyi, Valentyn. 2021. “The Concept of an Inflatable Reusable Launch Vehicle.” Preprint, . https://doi.org/10.31224/osf.io/xbf8z
• Pienkowski, T. M. 1967. “Curves for Loran-Inertial Analysis.” Navigation 14 (4): 434–42. https://doi.org/10.1002/j.2161-4296.1967.tb02228.x
• Pierce, J. A., and R. H. Woodward. 1971. “The Development of Long-Range Hyperbolic Navigation in the United States.” Navigation 18 (1): 51–62. https://doi.org/10.1002/j.2161-4296.1971.tb00074.x
• Pierros, Frankiskos. 2018. “Stand-Alone Celestial Navigation Positioning Method.” Journal of Navigation 71 (6): 1344–62. https://doi.org/10.1017/s0373463318000401
• Piet-Lahanier, Helene, and Laurent Serre. 2017. “Trajectory and Guidance Scheme Design for Free Flight Test of Hypersonic Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2197. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2197
• Pileri, Luca, and Giacomo Langfelder. 2025. “Role of Feedthrough Capacitance in Mode-Split MEMS Gyroscope Bias-Instability.” In Lecture Notes in Electrical Engineering. Springer Nature Switzerland. https://doi.org/10.1007/978-3-031-71518-1_23
• Pilyugin, N. N., and V. S. Khlebnikov. 2005. “Study of the Effect of the Depth of the Cavity of a Braking Device on the Aerodynamic Drag of a Model in Transonic and Supersonic Flow.” Fluid Dynamics 40 (2): 332–37. https://doi.org/10.1007/s10697-005-0073-9
• Pines, S. 1982. Terminal Area Automatic Navigation, Guidance, and Control Research Using the Microwave Landing System (MLS). Part 4: Transition Path Reconstruction along a Straight Line Path Containing a Glideslope Change Waypoint. NASA-CR-3574. NASA. https://ntrs.nasa.gov/citations/19820020393
• Pines, S., and R. Hueschen. 1978. “Guidance and Navigation for Automatic Landing, Rollout, and Turnoff Using MLS and Magnetic Cable Sensors.” In Guidance and Control Conference. AIAA 1978-1296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1296
• Pintér, Marco, and Petr Marcoň. 2024. “Navigation of UAV in GNSS Denied Area.” In Proceedings II of the 30st Conference STUDENT EEICT 2024: Selected papers. Brno University of Technology, Faculty of Electrical Engineering and Communication. https://doi.org/10.13164/eeict.2024.96
• Pinto, Jonathan, Neil L. Whyman, Matthew A. Ritchie, and Hugh Griffiths. 2023. “Statistical Analysis of Hypersonic Glide Vehicle Radar Cross Section.” IET Radar, Sonar & Navigation 18 (1): 158–70. https://doi.org/10.1049/rsn2.12432
• Piovesan, Tommaso, Pavlos K. Zachos, David MacManus, et al. 2025. “Use of Non-Intrusive Flow Diagnostics for Aero-Engine Inlet Flow Distortion Measurements in an Industrial Wind-Tunnel.” In AIAA SCITECH 2025 Forum. AIAA 2025-2111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2111
• Pipko, I. D. 1966. Supersonic Passenger Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0646293
• Pishchela, Pavlo, Serhii Ponomarenko, Serhii Golovach, and Heorhii Strokach. 2023. “Thermal Compensation of the Drift of a Solid Vibrating Gyroscope Using the Spline Approximation.” Mechanics of Gyroscopic Systems, no. 46: 93–100. https://doi.org/10.20535/0203-3771462023302699
• Pismennyi, V. L. n.d. “Bypass Turbojet Engine of Pismennyi.” In Scientific research of the SCO countries: synergy and integration. Crossref. https://doi.org/10.34660/inf.2019.16.36674
• Pittman, J. L., D. S. Miller, and W. H. Mason. 1984. Body and Canard Effects on an Attached-Flow Maneuver Wing at Mach 1.62. NASA-TP-2249. NASA. https://ntrs.nasa.gov/citations/19840010095
• Plaetschke, E., and S. Weiss. 1988. “Aircraft System Identification — Determination of Flight Mechanics Parameters.” In Application of System Identification in Engineering. Springer Vienna. https://doi.org/10.1007/978-3-7091-2628-8_11
• Platzer, Max F. 2010. Missile Aerodynamics. Wiley. https://doi.org/10.1002/9780470686652.eae017
• Plinge, Walter R. 2003. “Automatic Approach and Landing Systems.” Measurement and Control 36 (6): 176–80. https://doi.org/10.1177/002029400303600603
• Poddar, Shashi, Vipan Kumar, and Amod Kumar. 2016. “A Comprehensive Overview of Inertial Sensor Calibration Techniques.” Journal of Dynamic Systems, Measurement, and Control 139 (1): 011006. https://doi.org/10.1115/1.4034419
• Pogosyan, Mikhail, and Alexander Vereikin. 2020. “Position and Motion Control of Aerial Vehicles in Automatic Landing Systems: Analytical Review.” Vestnik Moskovskogo aviatsionnogo instituta 27 (3): 7–22. https://doi.org/10.34759/vst-2020-3-7-22
• “Pointing and Tracking Accuracy. Recommended Standards.” 1969. In Structures Technology for Large Radio and Radar Telescope Systems. The MIT Press. https://doi.org/10.7551/mitpress/6523.003.0008
• Politis, E., and R. Kind. 1986. “Supersonic Aerodynamics of Spinning Tubular Bodies.” In 24th Aerospace Sciences Meeting. AIAA 1986-395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-395
• Pollack, Jonathan D. 2010. “Short-Range Ballistic Missile Capabilities.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780203087411-13
• Polli, Gian Mario, Franco Mastroddi, Liviu Librescu, and Claudia DiTrapani. 2006. “Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat Inputs.” In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th. AIAA 2006-1731. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-1731
• Pollin, Irvin. 1973. Precision Transonic Barometric Fuze System for the Laser Guided Honest John Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0779412
• Pollock, Luke, Jeremy Moran, and Andrew J. Neely. 2023. “Effects of Aerothermal Shape Distortion on Hypersonic Vehicle Performance in Cruise.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3033
• Polutchko, Robert J. 1973. Free-Flight Test Results of Scale Models Simulating Viking Parachute/Lander Staging. TR-3720386. Martin Marietta Corp. https://ntrs.nasa.gov/citations/20060047578
• Pond, J. E., P. O. McCormick, and S. D. Smith. 1971. Shuttle Reentry Aerodynamic Heating Test. NASA-CR-123580. NASA. https://ntrs.nasa.gov/citations/19720013278
• Pope, J. M., and W. N. Staehle. 1975. “Propeller Modulation Effects on a Scanning-Beam Microwave Landing System.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19750052589
• Popytalov, S. A., and V. V. Samsonov. 1978. “Computer Calculation of Aerodynamic Characteristics of Aircraft at Supersonic Velocities.” Fluid Dynamics 13 (3): 415–21. https://doi.org/10.1007/bf01050534
• Porat, B., and I. Bar-Itzhack. 1979. “Azimuth Observability Enhancement during INS in-Flight Alignment.” In Guidance and Control Conference. AIAA 1979-1706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1706
• Poritzky, S. 1970. “Seeking a New Precision Approach and Landing System: A Test of Maturity.” In 2nd Aircraft Design and Operations Meeting. AIAA 1970-937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-937
• Porter, J. M. 1965. “Some Problems and Uses of Fuel Flow Measurement in Supersonic Aircraft.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50011-7
• Porter, B., and A. Manganas. 1986. “Recursive Real-Time Identification of Step-Response Matrices of High-Performance Aircraft for Adaptive Digital Flight Control.” In 13th Atmospheric Flight Mechanics Conference. AIAA 1986-2017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2017
• Portnoy, H. 1959. “The Drag of Ducted Bodies with Annular or Side Intakes in Supersonic Flow.” Aeronautical Quarterly 10 (3): 283–95. https://doi.org/10.1017/s0001925900001505
• Position Error Propagation in the Simplex Strapdown Navigation System. 1976. NASA-CR-144220. NASA. https://ntrs.nasa.gov/citations/19760013094
• Poston, P. L. 1975. Star Tracker Constraint Violations Digital Capability Description and Analysis Results. Mission Planning, Mission Analysis, and Software Formulation. NASA-CR-147847. NASA. https://ntrs.nasa.gov/citations/19760022261
• Poth, Tim, and John Elwell. 1992. “Progress on Micromechanical Inertial Guidance System.” In Aerospace Design Conference. AIAA 1992-1119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1119
• Potter, Norman S. 1964. “Accuracy and Simplification in Doppler Navigation Satellite Systems.” Navigation 11 (4): 366–78. https://doi.org/10.1002/j.2161-4296.1964.tb02111.x
• Potter, J. E., and J. C. Deckert. 1972. Gyro and Accelerometer Failure Detection and Identification in Redundant Sensor Systems. MIT. https://ntrs.nasa.gov/citations/19720048522
• Poudel, Nishchal, and Sudip Bhattrai. 2026. “Numerical Investigation of Coupled Aerothermoelastic Effects on Hypersonic Intake Performance.” In AIAA SCITECH 2026 Forum. AIAA 2026-2046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2046
• Poudel, Nishchal, Sandip Gewali, and Sudip Bhattrai. 2026. “Numerical Investigation on the Aerothermoelastic Response of Compliant Panels under Hypersonic Shock Impingement.” In AIAA SCITECH 2026 Forum. AIAA 2026-0024. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0024
• Pourtakdoust, Seid, and C. Lan. 1990. “Thin-Layer Navier-Stokes Calculations of Supersonic Vortex Interaction on Missile Configurations.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3089
• Powell, F. D. 1960. “The AN/GSN-5 Automatic Landing System.” Navigation 7 (1): 48–56. https://doi.org/10.1002/j.2161-4296.1960.tb01992.x
• Powell, T., and M. Glickstein. 1988. “Precooled Turbojet Engine Cycle for High Mach Number Applications.” In 24th Joint Propulsion Conference. AIAA 1988-2946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2946
• Powell, A., H. Welge, and C. Trefny. 1985. “Low-Speed Aerodynamic Test of an Axisymmetric Supersonic Inlet with Variable Cowl Slot.” In 21st Joint Propulsion Conference. AIAA 1985-1210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1210
• Powers, C. S. 1960. “Precision Determination of Vacuum Specific Impulse from Trajectory Data.” In Ballistic Missile and Space Electronics. Elsevier. https://doi.org/10.1016/b978-0-12-395519-7.50008-2
• Powers, Sheryll. 1988. “Flight Tests of External Modifications Used to Reduce Blunt Base Drag.” In 6th Applied Aerodynamics Conference. AIAA 1988-2553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2553
• Pr, Ayswarya, S. S. Pournami, and Ravi Nambiar. 2015. “A Survey on Ring Laser Gyroscope Technology.” International Journal of Computer Applications 116 (2): 25–27. https://doi.org/10.5120/20310-2354
• Prabhakar, N., K. Chandra Sekhar, and V. Vaidiyanathan. 2013. “Target Hit Interceptor Mid-Course Guidance Scheme for Ballistic Missile Interception.” International Journal of Applied Research in Mechanical Engineering: 7–11. https://doi.org/10.47893/ijarme.2013.1105
• Prabhu, S., and G. Anitha. 2019. “An Innovative Analytic Redundancy Approach to Air Data Sensor Fault Detection.” Aeronautical Journal 124 (1273): 346–67. https://doi.org/10.1017/aer.2019.143
• Practical Issues for Radar Tracking. 1998. Wiley. https://doi.org/10.1002/0471224197.ch3
• Prado Pereira, Luis Eduardo, José Augusto Ignacio da Silva, and Flavio D. Marques. 2021. “A Robust Strategy to Stabilize Aircraft Landing Gear Shimmy under Structural Uncertainties.” In Proceedings of the 26th International Congress of Mechanical Engineering. ABCM. https://doi.org/10.26678/abcm.cobem2021.cob2021-0297
• Prahlada, Mr. 2002. “Quality and Reliability of Missile System.” Defence Science Journal 52 (1): 5–10. https://doi.org/10.14429/dsj.52.2142
• Prakash, Satya, Biju Uthup, and K. P. Singh. 2009. “A Computational Study of Onset of Pitch-Up on a Low Aspect Ratio Wing Fighter Aircraft Configuration.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3631. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3631
• Prasad, G. 2022. “Computational Fluid Dynamics Analysis on the Reusable Launch Vehicle.” Incas Bulletin 14 (1): 119–24. https://doi.org/10.13111/2066-8201.2022.14.1.10
• Pratt and Whitney Aircraft (United States), John Larson, and AEC. 1960e. P&WA Nuclear J58 Turbojet Engine Powerplant Characteristics Summaries. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12377065
• Pratt and Whitney Aircraft (United States), J. Larson, and DOE. 1958. Powerplant Performance for a Supersonic Nuclear Turbojet Powerplant. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12393299
• Pratt and Whitney Aircraft (United States), J. Larson, and DOE. 1960a. J-58 Turbojet Engine for NAA B-70 Airplane. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12393926
• Pratt and Whitney Aircraft (United States), J. Larson, and ERDA. 1960b. Nuclear JT11-20 Turbojet Engine Estimated Performance 1600F NaK Radiator. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12086919
• Pratt and Whitney Aircraft (United States), J. Larson, and ERDA. 1960c. Nuclear JT11D-20 Turbojet Engine Estimated Performance 1800F NaK Radiator. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12086918
• Pratt and Whitney Aircraft (United States), John Larson, and ERDA. 1960d. P&WA Nuclear J58 Turbojet Engine Performance Variation with Radiator Diameter. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/12086798
• Pratt and Whitney Aircraft, East Hartford, CT (United States), John Larson, and US Atomic Energy Commission (AEC). 1960. Pratt & Whitney Aircraft Nuclear J-8 Turbojet Engine Performance Variation with Radiator Diameter. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1245463
• Precision Attitude Determination System (PADS) Design and Analysis. Two-Axis Gimbal Star Tracker. 1973. NASA-CR-144704. NASA. https://ntrs.nasa.gov/citations/19760007064
• Precision Attitude Determination System (PADS) System Design and Analysis: Single-Axis Gimbal Star Tracker. 1974. NASA-CR-144726. NASA. https://ntrs.nasa.gov/citations/19760010102
• “Precision Landing of Aircraft Using Integrity Beacons.” 1996. In Global Positioning System: Theory and Applications, Volume II. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866395.0427.0459
• Precision Pointing Control System (PPCS) Star Tracker Test. 1972. NASA-CR-144727. NASA. https://ntrs.nasa.gov/citations/19760010101
• Prescott, Ford L. 1963. “Wave Drag of an Axisymmetric Body.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/630092
• Price, Charles F. 1970. Adaptive Control and Guidance for Tactical Missiles. Volume 2: Parts 3 and 4. Adaptive Control Applications and Guidance. Defense Technical Information Center. https://doi.org/10.21236/ad0879285
• Price, Earl A. 1978. A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/ada050891
• Price, E., Jr. 1981. “Interference Effects of Downstream Support Hardware on Throttle-Dependent Drag at Transonic Mach Numbers.” In 17th Joint Propulsion Conference. AIAA 1981-1493. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1493
• Priest, R., J. Kordas, and I. Lewis. 1995a. Clementine Star Tracker Stellar Compass: Final Report Part 1. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/114596
• Priest, R., J. Kordas, and I. Lewis. 1995b. Clementine Star Tracker Stellar Compass: Final Report Part 2. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/114597
• Priolo, F., A. Wardlaw Jr., and G. Kuhn. 1991. “High-Temperature Effects for Missile-Type Bodies Using the Euler Solver, ZEUS.” In 9th Applied Aerodynamics Conference. AIAA 1991-3259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3259
• Priyamvada, K. S., Yogendra Singh, Nimesh Thakor, K. D. Manoj Kumar, and Gopalan Jagadeesh. 2015. “Analytical Modeling and Design for an Air-Breathing Hypersonic Cruise Vehicle Using an Integrated Approach.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3678. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3678
• Prizevoits, Peteris. 1961. Inertial Platform Equations. Defense Technical Information Center. https://doi.org/10.21236/ad0273454
• Prochazka, Frederik. 2026. “Robust Two-Degree-of-Freedom Missile Autopilot Design via Scheduled μ-Synthesis and LPV Methods.” In AIAA SCITECH 2026 Forum. AIAA 2026-2162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2162
• “Properties and Design of Slender Aircraft for Supersonic Flight.” 2012. In The Aerodynamic Design of Aircraft. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781600869228.0338.0438
• Pruitt, D., and L. Bates. 1992. “Starting and Test Rhombus Characteristics of Two-Dimensional Supersonic Free-Jet Nozzle/generic Supersonic Aircraft Inlet Configurations.” In AlAA 4th International Aerospace Planes Conference. AIAA 1992-5091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-5091
• Pu, Yongbin, Guoping Huang, Zuo Fengyuan, and Chen Xia. 2017. “Numerical Investigation of Two-Dimensional Supersonic Variable-Geometry Inlet for Ramjet.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2415
• Puchalski, Walter J., and James F. Kowalick. 1976. Wake Region Perturbation for Base Drag Reduction. Defense Technical Information Center. https://doi.org/10.21236/ada026147
• Purcell, Madison V., Alexander M. Wicklund, and Nigam Vadecha. 2025. “Reusable Launch Vehicles: Designing Legs for Propulsive Rocket Landing.” In AIAA SCITECH 2025 Forum. AIAA 2025-0202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0202
• Qian, Kun, Jianguo Wang, and Hu G. Baoxin. 2015. “Novel Integration Strategy for GNSS-Aided Inertial Integrated Navigation.” GEOMATICA 69 (2): 217–30. https://doi.org/10.5623/cig2015-205
• Qifan, Zhang, Tan Huijun, and Bu Huanxian. 2014. “Investigation of a Movable Slot-Plate Control Method for Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3847. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3847
• Qin, Ning. 2012. “Drag Reduction for Transonic Wings Combining Reduced Wing Sweep with Shock Control.” In 28th International Symposium on Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-25688-2_7
• Qin, Fangjun, Jiangning Xu, An Li, and Baiqing Hu. 2011. “Strapdown Inertial Navigation System Attitude Algorithm with Gibbs Oscillation Removal in Gyro Signal Reconstruction.” Sensor Letters 9 (4): 1551–55. https://doi.org/10.1166/sl.2011.1667
• Qin, Feng, Xingqun Zhan, and Lei Zhan. 2014. “Performance Assessment of a Low-Cost Inertial Measurement Unit Based Ultra-Tight Global Navigation Satellite System/inertial Navigation System Integration for High Dynamic Applications.” IET Radar, Sonar & Navigation 8 (7): 828–36. https://doi.org/10.1049/iet-rsn.2013.0217
• Qu, Yaoyao, and Xiaoqing Qiang. 2023. “Design and Test of an Aero-Engine Inlet Distortion Screen Facility.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-0651-2_12
• Quadros, Jaimon D., Thalambeti Prashanth, and Sher A. Khan. 2022. “Base Drag Estimation in Suddenly Expanded Supersonic Flows Using Backpropagation Genetic and Recurrent Neural Networks.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 236 (14): 2991–3018. https://doi.org/10.1177/09544100211072594
• Quan, Wei, Xiaolin Gong, Jiancheng Fang, and Jianli Li. 2015a. “Error Modeling, Calibration, and Compensation of Inertial Measurement Unit (IMU).” In INS/CNS/GNSS Integrated Navigation Technology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-45159-5_4
• Quan, Wei, Xiaolin Gong, Jiancheng Fang, and Jianli Li. 2015b. “Star Map Processing Algorithm of Star Sensor and Autonomous Celestial Navigation.” In INS/CNS/GNSS Integrated Navigation Technology. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-45159-5_5
• Quang Lam, C. Woodruff, S. Ashton, and D. Martin. 2002. “Noise Estimation for Star Tracker Calibration and Enhanced Precision Attitude Determination.” In Proceedings of the Fifth International Conference on Information Fusion. FUSION 2002. (IEEE Cat.No.02EX5997), vol. 1. Int. Soc. Inf. Fusion. https://doi.org/10.1109/icif.2002.1021156
• Quigg, G. C., and D. G. Stewart. 1963. Similarity and Scale Effect in Ramjet Combustors. Aeronautical Research Labs. https://ntrs.nasa.gov/citations/19630008707
• Quinter, Rudolph F. 1970. Report on Modification of AIM-40 Falcon Missile Container to Accommodate Guidance and Control Section of AIM-7E/E2 Sparrow Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0720877
• Raab, Christian. 2014. “Rapid Aerodynamic Parameter Identification on a Large Transport Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-0730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0730
• Rabiee, Ramtin, Ian Bajaj, and Wee Peng Tay. 2019. “Vehicle Localization in GNSS-Denied Environments.” In Cooperative Localization and Navigation. CRC Press. https://doi.org/10.1201/9780429507229-11
• “Radar Tracking Algorithms.” 2010. In Principles of Modern Radar: Basic principles. Institution of Engineering and Technology. https://doi.org/10.1049/sbra021e_ch19
• Rademakers, Ruud, Thomas Kächele, Stefan Bindl, and Reinhard Niehuis. 2014. “Approach for an Optimized Evaluation of Pressure and Swirl Distortion in S-Shaped Engine Inlet Con[|#12#|]figurations.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3594. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3594
• Radio Optical/strap down Inertial Guidance Study for Advanced Kick Stage Applications. Volume 2: (Detailed Study Results) Final Report. 1967. NASA-CR-86012. NASA. https://ntrs.nasa.gov/citations/19680002782
• Radio/optical/strapdown Inertial Guidance Study for Advanced Kick Stage Applications: Launch Vehicle Data, Tasks 5 and 6. 1969. NASA-CR-86199. NASA. https://ntrs.nasa.gov/citations/19690024322
• “Radionavigation Kalman Filtering: Case Studies in Two Dimensions.” 2022. In Fundamentals of Inertial Navigation Systems and Aiding. SciTech Publishing Inc. https://doi.org/10.1049/sbra550e_ch15
• Radkey, R., H. Welge, and R. Roensch. 1976. “Aerodynamic Design of a Mach 2.2 Supersonic Cruise Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1976-955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-955
• Rae, W. M. 1961. “Engineering Aspects of Missile Telemetry Equipment—the Airborne Sender for 24-Channel Telemetry.” Journal of the British Institution of Radio Engineers 21 (1): 57–67. https://doi.org/10.1049/jbire.1961.0009
• Ragsdale, W. 2000. “A Generic Landing Gear Dynamics Model for LaSRS++.” In Modeling and Simulation Technologies Conference. AIAA 2000-4303. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4303
• Ragsdale, W. A., A. R. Osborne, and C. K. Seaman. 1974. Atmospheric Effects on the Space Shuttle Approach and Landing. Singer Co., Simulation Products Div., Houston. https://ntrs.nasa.gov/citations/19750051284
• Rahangdale, Shubham. 2025. “Adaptive Wavelet Selection for Enhanced Inertial Sensor Signal Processing.” Preprint, . https://doi.org/10.31224/6117
• Rahgoshay, Mohammad Ali, and Paknoosh Karimaghaie. 2020. “Robust in-Field Estimation and Calibration Approach for Strapdown Inertial Navigation Systems Accelerometers Bias Acting on the Vertical Channel.” IET Radar, Sonar & Navigation 14 (3): 407–14. https://doi.org/10.1049/iet-rsn.2019.0359
• Rahgoshay, Mohammad Ali, Paknoosh Karimaghaie, and Fereidoon Shabaninia. 2017. “Robust Inertial Frame-Based Alignment of Fiber-Optic Gyro Strapdown Inertial Navigation Systems Using a Generalized Proportional–integral–derivative Filter.” Optical Engineering 56 (09): 1–10. https://doi.org/10.1117/1.oe.56.9.095102
• Rahimi, Hossein, and Amir Ali Nikkhah. 2021. “Coarse Alignment of Marine Strapdown Inertial Navigation System Using the Location of Fitted Parametric Circle of Gravity Movement.” Journal of Navigation 74 (3): 574–93. https://doi.org/10.1017/s0373463321000151
• Rahmani, Mohsen, and Kamran Behdinan. 2018a. “Investigation on the Effect of Coulomb Friction on Nose Landing Gear Shimmy.” Journal of Vibration and Control 25 (2): 255–72. https://doi.org/10.1177/1077546318774440
• Rahmani, Mohsen, and Kamran Behdinan. 2018b. “Studying the Effect of Freeplay on Nose Landing Gear Shimmy Using a Fully Nonlinear Model.” In Volume 6: 14th International Conference on Multibody Systems, Nonlinear Dynamics, and Control. American Society of Mechanical Engineers. https://doi.org/10.1115/detc2018-85559
• Rahmani, Mohsen, and Kamran Behdinan. 2019b. “Performance Analysis and Parametric Studies of Nose Landing Gear Shimmy Dampers.” In Volume 4: Dynamics, Vibration, and Control. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2019-10167
• Raisinghani, S., G. Bhaskar Reddy, and A. Ghosh. 1999. “Parameter Estimation of an Augmented Aircraft Using Neural Networks.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4248
• Raisinghani, S., and Hemant Kumar. 1995. “Unsteady Aerodynamic Modeling for Parameter Estimation of a Canard Aircraft.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3435. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3435
• Rajabi, Mohammad Javad, S. M. M. Dehghan, and S. Mohammad-Hosseini. 2025. “Improving Inertial Navigation System Alignment Using a Proportional-Integral Left-Invariant Extended Kalman Filter: A Robust Approach against Inertial Sensors Errors.” Scientia Iranica 0 (0): 0–0. https://doi.org/10.24200/sci.2025.66968.10354
• Rajagopal, Karthikeyan, and S. Balakrishnan. 2012. “Adaptive Neural Network– Based Autopilot Design.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-5
• Rajagopalan, R., and S. Siddiqi. 1985. “Aircraft Turbojet Engine Modeling Using Artificial Intelligence Techniques.” In 23rd Aerospace Sciences Meeting. AIAA 1985-253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-253
• Rajchowski, Piotr, Krzysztof K. Cwalina, and Jarosław Sadowski. 2016. “Research and Analysis of Accuracy of Location Estimation in Inertial Navigation System.” Applied Mechanics and Materials 817: 308–16. https://doi.org/10.4028/www.scientific.net/amm.817.308
• Raju, Nandhini, Tonse Gokuldas Pai, S. B. Verma, and L. Venkatakrishnan. 2020. “An Experimental Investigation of Turbo-Ramjet Engine Intake at Mach 4.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3772
• Rakholia, A., A. Sugarbaker, A. Black, et al. 2017. “Development of an Atom Interferometer Gravity Gradiometer for Earth Sciences.” In American Physical Society. https://ntrs.nasa.gov/citations/20170005272
• Rakoczy, John, and Mark West. 1992. “Magnitude Calibration of a Fixed Head Star Tracker Using Astro-1 Flight Data.” In Space Programs and Technologies Conference. AIAA 1992-1467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1467
• Rallabhandi, Sriram, and Dimitri Mavris. 2003. “An Unstructured Wave Drag Code for Preliminary Design of Future Supersonic Aircraft.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3877
• Ramachandra, Lusitha S., Nicolas P. Avdelidis, and Ian K. Jennions. 2026a. “Emissivity-Corrected Thermography for Post Landing Aircraft Wheel and Brake Cooling.” In Thermosense: Thermal Infrared Applications XLVIII, edited by Marc Genest, Giovanni Ferrarini, Peter Spaeth. SPIE. https://doi.org/10.1117/12.3097420
• Ramalingam, R., G. Anitha, and J. Shanmugam. 2009. “Microelectromechnical Systems Inertial Measurement Unit Error Modelling and Error Analysis for Low-Cost Strapdown Inertial Navigation System.” Defence Science Journal 59 (6): 650–58. https://doi.org/10.14429/dsj.59.1571
• Ramanujachari, V. 2022. “Supersonic Combustion Ramjet Technology.” In Advances in Combustion Technology. CRC Press. https://doi.org/10.1201/9781003049005-8
• RAMJET Engine Controller Design Using Quantitative Feedback Theory (QFT). 2025. https://doi.org/10.37285/bsp.sacad2025.08
• Ramm, Heinrich J. 1990. “Lift Slope and Drag Rise at Sonic Speed.” In Fluid Dynamics for the Study of Transonic Flow. Oxford University PressNew York, NY. https://doi.org/10.1093/oso/9780195060973.003.0005
• Ran, Hongjun, and Dimitri Mavris. 2005. “Preliminary Design of a 2D Supersonic Inlet to Maximize Total Pressure Recovery.” In AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences. AIAA 2005-7357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-7357
• Rancourt, David, Mathieu Picard, Jean-Sébastien Plante, and Martin Brouillette. 2014. “High-g Field Combustor of a Rim-Rotor Rotary Ramjet Engine.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3450
• Rander, Peter W., and Brett Browning. 2009. Empirical Evaluation of the Virtual Autonomous Navigation Environment. Defense Technical Information Center. https://doi.org/10.21236/ada520805
• Range, D. W., and R. N. Southworth. 1967. “Use of a Small Computer as a Celestial Navigation Aid.” Navigation 14 (3): 270–79. https://doi.org/10.1002/j.2161-4296.1967.tb02209.x
• Rao, J. Srinivasa, D. Pullaiah, S. Padmasree, G. Nagendra Rao, and T. Alex. 2004. “Star Tracker Alignment Determination for Resourcesat-I.” In AIAA/AAS Astrodynamics Specialist Conference and Exhibit. AIAA 2004-5392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5392
• Rao, Venkatesh K. P., Shweta Rai, Tribhuvan Batish, and Anmol Gulati. 2022. “Coupled Field Analysis of Hemispherical Resonator Gyroscope.” International Journal of Vehicle Structures and Systems 14 (2). https://doi.org/10.4273/ijvss.14.2.06
• Raol, Jitendra R., and Jatinder Singh. 2023. “System Identification and Parameter Estimation for Aircraft.” In Flight Mechanics Modeling and Analysis. CRC Press. https://doi.org/10.1201/9781003293514-10
• Rashis, Bernard, and Aleck C. Bond. 1961. Free-Flight Skin-Temperature and Surface-Pressure Measurements on a Highly Polished Nose Having a 100 Deg Total-Angle Cone and a 10 Deg Half-Angle Conical Flare Section up to a Mach Number of 4.08. NASA-TN-D-807. NASA. https://ntrs.nasa.gov/citations/20040047118
• Rashleigh, S. C., and W. K. Burns. 1980. “Dual-Input Fiber-Optic Gyroscope.” Optics Letters 5 (11): 482. https://doi.org/10.1364/ol.5.000482
• Rashleigh, S. C., and W. K. Burns. 1981. “Alternating Current Operation of the Dual-Input Fiber-Optic Gyroscope.” In Integrated Optics and Optical Fiber Communication. OSA. https://doi.org/10.1364/ofc.1981.wi4
• Rasky, Daniel, R. Bruce Pittman, and Mark Newfield. 2006. “The Reusable Launch Vehicle Challenge.” In Space 2006. AIAA 2006-7208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7208
• Rasmussen, M. 1980. “Optimal Platform Skewing for Space Shuttle Inertial Measurement Unitredundancy Management.” In Guidance and Control Conference. AIAA 1980-1769. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1769
• Raspopov, V. Ya., R. V. Alaluev, A. V. Ladonkin, V. V. Likhosherst, S. I. Shepilov, and Michurinsk Plant «Progress», JSC, Michurinsk, Russia. 2020. “Tuning and Calibration of a Hemispherical Resonator Gyroscope with a Metal Resonator to Operate in Angular Rate Sensor Mode.” Giroskopiya i Navigatsiya 28 (1): 31–41. https://doi.org/10.17285/0869-7035.0019
• Rataczak, Jens A., Jay W. McMahon, and Iain D. Boyd. 2023. “Reachability Analysis of a Hypersonic Glide Vehicle Using Particle Swarm Optimization.” In AIAA SCITECH 2023 Forum. AIAA 2023-1172. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1172
• Rataichuk, I. A., and V. I. Kortunov. 2013. “Kalman Filter Stationarity Analysis in the Task of Inertial Navigation System Errors Estimation.” Electronics and Control Systems 2 (36). https://doi.org/10.18372/1990-5548.36.5855
• Ratchford, Jasmine, Jeremy Redding, and Luis Bravo. 2025. “Early Prediction of Inlet Unstart Using Upstream Flow Indicators.” Physics of Fluids 37 (11): 111701. https://doi.org/10.1063/5.0299691
• Ratekin, G., Allen Goldman, P. Ortwerth, S. Weisberg, and J. Craig McArthur. 2001. Rocket-Based Combined Cycle Engine Concept Development. Boeing Co. https://ntrs.nasa.gov/citations/20020016608
• Ratnayake, Nalin, Edwin Koshimoto, and Brian Taylor. 2011. “Multi-Axis Identifiability Using Single-Surface Parameter Estimation Maneuvers on the X-48B Blended Wing Body.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6273
• Raue, Andreas, and Jens Timmer. 2013. “Structural and Practical Identifiability Analysis.” In Encyclopedia of Systems Biology. Springer New York. https://doi.org/10.1007/978-1-4419-9863-7_1219
• Raut, Sakshaat, and Ninad Mehendale. 2025. “A Real-Time Aerodynamic Navigation System for Small Fixed-Wing Drones in GNSS-Denied Environments.” Preprint, . https://doi.org/10.2139/ssrn.5042078
• Ravanbod, Laleh, and Dominikus Noll. 2014. “Gain-Scheduled Two-Loop Autopilot for an Aircraft.” Journal of Dynamic Systems, Measurement, and Control 136 (4): 041021. https://doi.org/10.1115/1.4026832
• Raza, Ali, Hua Wang, and Hao Cheng. 2021. “SINS Integration with Baro-Inertial Vertical Channel Damping for Error Optimization.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_95
• Razgonyaev, Valery, and W. Mason. 1995. “Refined Lift and Side Force Wing-Body-Tail Interference Coefficients for Aircraft and Missile Aerodynamics.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3451
• Readshaw, D. 1961. “Predicting Temperature Rises, Due to Aerodynamic Heating: An Analogue Method Utilizing Trajectory Data to Calculate Temperature Distribution throughout a Missile Radome.” Aircraft Engineering and Aerospace Technology 33 (1): 8–11. https://doi.org/10.1108/eb033353
• “Real Time Spacecraft Attitude Determination by Star Pattern Recognition: Further Results.” 1979. In 17th Aerospace Sciences Meeting. AIAA 1979-254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-254
• Rector, Jack D., and Edwin R. Hattendorf. 1967. “All-Weather Landing Systems for Automatic and Manual Control.” Navigation 14 (2): 205–17. https://doi.org/10.1002/j.2161-4296.1967.tb02553.x
• Reda, Daniel C. 1977. Boundary-Layer Transition Experiments on Sharp, Slender Cones in Supersonic Freeflight. Defense Technical Information Center. https://doi.org/10.21236/ada054591
• Redding, Jeremy, Emma Cavanaugh, Luis Bravo, Muthuvel Murugan, and Venkat Narayanaswamy. 2025. “Investigation of Scramjet Inlet Unstart/restart Behavior Induced by High Angle of Attack and Dynamic Isolator Camber Motion.” Physics of Fluids 37 (6): 066112. https://doi.org/10.1063/5.0271076
• Reddy, C. Subba. 1993. “Aerodynamic Heating in Hypersonic Flows.” In Old Dominion Univ., The 1993 NASA-ODU American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program. https://ntrs.nasa.gov/citations/19940023416
• Reed, Wendell E. 1956. “A New Approach to Turbojet and Ramjet Engine Control.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/560042
• Reel, L. S. 1959. “Doppler-Inertial Navigation for High Performance Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/590297
• “Regularity and Strict Identifiability in MIMO Systems.” 2009. In Bayesian Bounds for Parameter Estimation and Nonlinear Filtering/Tracking. IEEE. https://doi.org/10.1109/9780470544198.ch38
• Reich, A., J. Connelly, and G. Calderone. 1976. “Coherent Optics for Missile Guidance.” In Guidance and Control Conference. AIAA 1976-1969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1969
• Reichert, R. 1989. “Application of H(infinity) Control to Missile Autopilot Design.” In Guidance, Navigation and Control Conference. AIAA 1989-3550. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3550
• Reilly, Richard H. W. 1994. “Air Alignment for the Base Inertial Navigation System: Lins 300.” In Vertical Flight Society Forum. https://doi.org/10.4050/vfs-f50-2009
• Reilly, D. H., and H. J. Welna. 1955. Preliminary Evaluation of Flight-Weight XRJ47-W-5 Ram-Jet Engine at a Mach Number of 2.75. NACA-RM-E55G22. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19660027126
• Rein, M., H. Rosemann, and E. Schülein. 2009. “Wave Drag Reduction by Means of Aerospikes on Transonic Wings.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_83
• Reitan, E. H., and S. H. Saib. 1976. “Computer Graphics in an Automatic Aircraft Landing System.” In Proceedings of the June 7-10, 1976, national computer conference and exposition on - AFIPS ‘76. ACM Press. https://doi.org/10.1145/1499799.1499894
• Reitbauer, Eva, Christoph Schmied, Fabian Theurl, and Manfred Wieser. 2023. “LIWO-SLAM: A LiDAR, IMU, and Wheel Odometry Simultaneous Localization and Mapping System for GNSS-Denied Environments Based on Factor Graph Optimization.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2023.19216
• Rekhy, Anuj, Mikhail Shneider, and Richard B. Miles. 2020. “LIDAR Requirements and Approaches for Transcontinental Supersonic Flight.” In AIAA Aviation 2020 Forum. AIAA 2020-3241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3241
• Ren, jiajing, chenghong Liu, hongke Jun, and Jianfeng Wang. 2024a. “The Influence of Vibration on Hemispherical Resonant Gyroscope.” In International Conference on Mechatronic Engineering and Artificial Intelligence (MEAI 2023), edited by Fengli Liu, Yonghe Wei. SPIE. https://doi.org/10.1117/12.3025570
• Ren, Hao, Yajie Ma, and Bin Jiang. 2024b. “Optimal Fault-Tolerant Control of Reusable Launch Vehicle with Actuator Faults Using Zero-Sum Differential Game Theory.” Preprint, . https://doi.org/10.2139/ssrn.4783505
• “Requirements of a Commercial Supersonic Aircraft on Its Engines.” 1967. In Commercial Aircraft Design and Operation Meeting. AIAA 1967-376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-376
• “Response Analysis of Landing Leg Deployment and Landing Transient Impact of Reusable Launch Vehicle.” 2026. Journal of Mechanical Engineering 62 (1): 159. https://doi.org/10.3901/jme.260010
• “Reusable Launch Vehicle Landing Gear Mechanism Technologies: A Review.” 2026. Journal of Mechanical Engineering 62 (1): 18. https://doi.org/10.3901/jme.260002
• Reuter, J. 1973. “Several Computerized Techniques to Aid in the Design and Optimization of Parachute Deceleration and Aerial-Delivery Systems.” In 4th Aerodynamic Deceleration Systems Conference. AIAA 1973-488. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-488
• Reuther, James. 2002. “Aerodynamic Shape Optimization for Supersonic Aircraft.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-2838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2838
• Reuther, J., M. Rimlinger, J. Alonso, and A. Jameson. 1996. “Aerodynamic Shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Distributed Memory Parallel Computers.” In 6th Symposium on Multidisciplinary Analysis and Optimization. AIAA 1996-4045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4045
• Rey, René J. 2000. “Deriving an Acceptable Level of Reusable Launch Vehicle Flightworthiness.” In AIP Conference Proceedings, vol. 504. AIP. https://doi.org/10.1063/1.1290921
• Reyhner, T., and T. Hickcox. 1972. “A Procedure for Combined Viscous-Inviscid Analysis of Supersonic Inlet Flow Fields.” In 10th Aerospace Sciences Meeting. AIAA 1972-44. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-44
• Reynolds, P. R. J. 1967. “An Accuracy Evaluation of a Civil Inertial Navigation System.” Journal of Navigation 20 (4): 449–63. https://doi.org/10.1017/s0373463300030770
• Reynolds, Homer E. 1977. Production/Cost Analysis of Ramjet Engines. Volume I.. Defense Technical Information Center. https://doi.org/10.21236/ada054856
• Rhoads, Donald W. 1967. In-Flight Simulation and Pilot Evaluation of Selected Landing Approach Handling Qualities of a Large Logistics Transport Airplane. Defense Technical Information Center. https://doi.org/10.21236/ad0820790
• Rhyne, R. H. 1980. Accuracy of Aircraft Velocities from Inertial Navigation Systems for Application to Airborne Wind Measurements. NASA-TM-81826. NASA. https://ntrs.nasa.gov/citations/19800019412
• Ri, Jong Chon, and Namchol Choe. 2023. “Improving the Accuracy of a Low-Cost Inertial Navigation System by Adaptive Zero Velocity Updating Using Machine Learning.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-3746855/v1
• Ribes, Mauricio A., Guenter Spahlinger, and Manfred W. Kemmler. 1996. “0.1-Deg/h DSP-Controlled Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 2837, edited by Eric Udd, Herve C. Lefevre, Kazuo Hotate. SPIE. https://doi.org/10.1117/12.258180
• Rice, Michael. 1999. A Comprehensive Investigation of Advanced Range Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ada375937
• Rice, Michael. 2013. The Challenges of C-Band Missile Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ada578383
• Rice, Robert, and Douglas Hazlwood. 1994. “Flight Test Program on the Cessna CitationJet.” In Biennial Flight Test Conference. AIAA 1994-2166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2166
• Rice, J., and R. McCorkle. 1979. “Digital Flight Control Reliability: Effects of Redundancy Level, Architecture and Redundancy Management Technique.” In Guidance and Control Conference. AIAA 1979-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1893
• Richeson, Justin, and Darryll Pines. 2007. “GPS Denied Inertial Navigation Using Gravity Gradiometry.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6791. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6791
• Rickard, J. 1963. “Collection and High-Speed Transmission of Radar Tracking Data at Theatlantic Missile Range.” In Space Flight Testing Conference. AIAA 1963-96. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-96
• Rickard, W. 1978. “Modeling and Parameter Uncertainties for Aircraft Flight Control System Design.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1371
• Rideau, Jean-Francois, Gilles Guyader, and Alain Cloarec. 2008. “MICROTURBO Families of Turbojet Engine for Missiles and Uav’s from the TR60 to the New Bypass Turbojet Engine Generation.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-4590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4590
• Ridha, R. 1968. “Minimum Weight Design of Aircraft Landing Gear Reinforcement Rings.” In 9th Structural Dynamics and Materials Conference. AIAA 1968-328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-328
• Riebe, G. D., W. J. Small, and O. A. Morris. 1981. Aerodynamic Tests and Analysis of a Turbojet-Boosted Launch Vehicle Concept (Spacejet) over a Mach Number Range of 1.50 to 2.86. NASA-TP-1888. NASA. https://ntrs.nasa.gov/citations/19810020560
• Ried, R. C., Jr. 1964. Aerodynamic Heating. NASA. https://ntrs.nasa.gov/citations/19650029832
• Riedel, F. 1976. “Design of a Control System Which Minimizes the Probability of Clobber for a Terrain Following Cruise Missile.” In Guidance and Control Conference. AIAA 1976-1941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1941
• Ries, Judy, and Sathvik Dasari. 2024. “Review of Autonomous Navigation Methods for Hypersonic Aircraft Using Inertial Navigation Sensors Systems and Machine Learning.” Preprint, . https://doi.org/10.2139/ssrn.4895146
• Riley, A. 1969. “Check out Procedures for the Computer Program Used in the ELDO Inertial Guidance System.” In Aerospace Computer Systems Conference. AIAA 1969-961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-961
• Riley, Christopher J., and Fred R. Dejarnette. 1992. An Engineering Aerodynamic Heating Method for Hypersonic Flow. AIAA PAPER 92-0499. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920043703
• Riley, Zachary A., Ricardo Perez, Timothy J. Beberniss, et al. 2026. “Aerothermoelastic Behavior of Thermally Buckled Panels at Mach 6.” Preprint, . https://doi.org/10.2139/ssrn.6509818
• Riley, Zachary B., Ricardo Perez, and Kirk R. Brouwer. 2023. “Design of Aerothermoelastic Experiments in the AFRL Mach 6 High Reynolds Number Facility.” In AIAA SCITECH 2023 Forum. AIAA 2023-0948. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0948
• Riley, Zachary B., and Benjamin Smarslok. 2017. “Investigation of Aerothermoelastic Model Sensitivity under Transitional Fluid Loading in High Speed Flow.” In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2017-3824. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3824
• Rimer, M., and H. Sperling. 1965. “Automatic Landing System for a Lunar Vehicle: Guidance & Cotrol -.” In Unmanned Spacecraft Meeting 1965. AIAA 1965-1437. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1437
• Rishel, R. 1967. “Optimal Terminal Guidance of an Air to Surface Missile.” In Control and Flight Dynamics Conference. AIAA 1967-580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-580
• Rithirun, Chart, and Pitikhate Sooraksa. 2013. “Automatic Landing Controller of Unmanned Aerial Vehicle.” Advanced materials research 677: 442–48. https://doi.org/10.4028/www.scientific.net/amr.677.442
• Ritland, John. 1989. “Survey of Aided-Inertial Navigation Systems for Missiles.” In Guidance, Navigation and Control Conference. AIAA 1989-3497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3497
• Ritland, John, and Kevin Spalding. 1987. “Impact of Inertial System Quality on GPS-Inertial Performance in a Jamming Environment.” In Guidance, Navigation and Control Conference. AIAA 1987-2594. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2594
• Rivers, S. M. B., and R. A. Wahls. 2003. “Turbulence Model Comparisons for Supersonic Transports at Transonic and Supersonic Conditions.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3418
• Rizvi, S. T. I., H. Linshu, X. Dajun, and S. I. A. Shah. 2017. “Trajectory Optimisation for a Rocket-Assisted Hypersonic Boost-Glide Vehicle.” Aeronautical Journal 121 (1238): 469–87. https://doi.org/10.1017/aer.2017.11
• Rizzetta, Donald. 1991. “Numerical Simulation of a Supersonic Inlet.” In 29th Aerospace Sciences Meeting. AIAA 1991-128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-128
• Rizzi, A., and W. Schmidt. 1978. “Study of Pitot-Type Supersonic Inlet-Flowfields Using the Finite-Volume Approach.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1115. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1115
• Roach, Robert, and H. Froning. 1996. “Drag Reduction of Transonic Airfoils by Freestream Perturbations and Heat Addition.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3413. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3413
• Robbins, J. W. 1985. Least Squares Collocation Applied to Local Gravimetric Solutions from Satellite Gravity Gradiometry Data. NASA-CR-176299. NASA. https://ntrs.nasa.gov/citations/19860002443
• Roberts, J. 1988. “F-15E Flight Test Program Overview: March 1988.” In 4th Flight Test Conference. AIAA 1988-2077. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2077
• Roberts, Simon. 2020. “CoDRIVE – Delivering High Accuracy, Ubiquitous Positioning through Combined Radio Navigation and Inertial Sensing Technologies.” Preprint, . https://doi.org/10.20944/preprints202009.0037.v1
• Robinette, G. Jeffrey, and Robert E. Witters. 1982. “A Multifunction Integrated Approach to Providing Aircraft Inertial Data.” Navigation 29 (4): 271–78. https://doi.org/10.1002/j.2161-4296.1982.tb00812.x
• Robinson, R. B. 1955. Effects of Free-Flight Rocket-Model Booster-Adapter Configurations on the Aerodynamic Characteristics in Pitch and Sideslip of a Swept-Wing Fighter Airplane Model at a Mach Number of 2.01. NACA-RM-L55B01. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710065524
• Robinson, R. B. 1958. Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Angles of Attack and Sideslip of Several Hypersonic Missile Configurations with Various Canard Controls. NACA-RM-L58A21. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19650014456
• Robinson, J., G. Culver, R. Bishop, and E. Bright. 2003. “Life Cycle Analysis of a Single Stage to Orbit (SSTO) Reusable Launch Vehicle.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5264
• Robinson, C., M. High, and L. Galigher. 1974. “Exhaust Plume Temperature and Reynolds Number Effects on Nozzle Afterbody Performance over the Transonic Mach Number Range.” In 10th Propulsion Conference. AIAA 1974-1148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1148
• “Robust Autopilot Design for Quasilinear Parameter-Varying Missile Model.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-9
• Rodgers, Colin. 1986. “A Jet Fuel Starter and Expendable Turbojet.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/86-gt-1
• Rodgers, John. 1992. “Aerothermoelastic Analysis of a NASP-like Vertical Fin.” In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2400
• Rodi, Patrick E. 2018. “Waverider Vehicle Optimization with Volumetric Constraints for Wave Drag Minimization.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1048
• Rodi, Patrick E., Henry Stoldt, Colin Hill, and Craig T. Johansen. 2019. “Design of a Sounding Rocket Flight Experiment to Validate Transonic Drag Minimized Waveriders.” In AIAA Aviation 2019 Forum. AIAA 2019-2812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2812
• Rodriguez, Armando A. 1999. Missile Guidance. Wiley. https://doi.org/10.1002/047134608x.w1122
• Rodriguez, David. 2004. “Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method.” In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2004-4492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4492
• Rodriguez, Armando A. 2007. Missile Guidance. Wiley. https://doi.org/10.1002/047134608x.w1122.pub2
• Rodríguez Martínez, Sebastián A. n.d. “Full Three-Axis Magnetometer and Gyroscope Bias Estimation Using Angular Rate Measurements.” PhD diss., Pontificia Universidad Católica de Chile. https://doi.org/10.7764/tesisuc/ing/66915
• Roeser, Mathias S., and Wulf Mönnich. 2024. “System Identification from Virtual Flight Test Data for a Flexible Transport Aircraft.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing. https://doi.org/10.1007/978-3-031-69425-7_5
• Rogalski, Tomasz. 2018. “Unmanned Aircraft Automatic Flight Control Algorithm in Loop Manoeuvre.” Aircraft Engineering and Aerospace Technology 90 (6): 877–84. https://doi.org/10.1108/aeat-02-2018-0088
• Rogalski, Tomasz, Paweł Rzucidło, Stanisław Noga, and Jacek Prusik. 2021. “Unmanned Aircraft Automatic Flight Control Algorithm in an Immelmann Manoeuvre.” Aircraft Engineering and Aerospace Technology 93 (9): 1460–69. https://doi.org/10.1108/aeat-11-2020-0269
• Rogalski, Tomasz, Paweł Rzucidło, and Jacek Prusik. 2020. “Unmanned Aircraft Automatic Flight Control Algorithm in a Spin Maneuver.” Aircraft Engineering and Aerospace Technology 92 (8): 1215–24. https://doi.org/10.1108/aeat-05-2019-0099
• Roger, Robert, Stephen Chan, and J. Smith. 2011. “Aerodynamic Effects of External Camera Pods and Launch Lugs on a Target Missile Configuration.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3664. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3664
• Rogers, W. F. 1972. “Apollo Lunar Module Landing Gear.” In The 7th Aerospace Mech. Symp.. https://ntrs.nasa.gov/citations/19730010151
• Rogers, John R. 1973. Two-Dimensional Air Cushion Landing System Peripheral Jet Confirmation Study. Defense Technical Information Center. https://doi.org/10.21236/ad0771616
• Rogers, Robert. 1994. “Kalman Filter Inertial Navigation System Error Model Based on Filter Stability Considerations.” In Guidance, Navigation, and Control Conference. AIAA 1994-3547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3547
• Rogers, Robert. 1995. “Velocity Error Representations in Inertial Navigation System Error Models.” In Guidance, Navigation, and Control Conference. AIAA 1995-3193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3193
• Rogers, Robert. 2002. “Correlation and Convergence of Inertial Navigation System Error Models.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4946. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4946
• Rogers, Steve. 2004. “Missile Guidance Comparison.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4882
• Rogers, Nancy, and Tom Dragone. 1996. “Modal Analysis and Separation Transient Dynamic Response of the X-34 Reusable Launch Vehicle.” In Dynamics Specialists Conference. AIAA 1996-1228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1228
• Rogers, Robert, and Robert Rogers. 1997. “Comparison of Inertial Navigation System Error Models in Application to IMU Transfer Alignment.” In Guidance, Navigation, and Control Conference. AIAA 1997-3599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3599
• Rogers, Jonathan, and Nathan Slegers. 2012. “Robust Parafoil Terminal Guidance Using Massively Parallel Processing.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4736
• Rogers Jr. and Walter K. 1955. Free Flight Tests of a Model of the ‘Redstone’, XSSM-A-14, Warhead. Defense Technical Information Center. https://doi.org/10.21236/ad0069214
• Roháč, J., M. Řeřábek, and R. Hudec. 2011. “Multi-Functional Star Tracker — Future Perspectives.” Acta Polytechnica 51 (6). https://doi.org/10.14311/1486
• Rohrschneider, Reuben. 2011. “Terrain Relative Navigation Using Crater Identification in Surface Topography Data.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6490. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6490
• Rollason, Malcolm, David Salmond, and Michael Evans. 2003. “Parameter Estimation for Terminal Guidance Using a Doppler Beam Sharpening Radar.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5447
• Rom, J., J. Er-El, and R. Gordon. 1989. “Measurements of the Aerodynamic Characteristics of Various Wing-Canard Configurations and Comparison with NLVLM Results.” In 7th Applied Aerodynamics Conference. AIAA 1989-2217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2217
• Rom, Josef, Arnan Seginer, and Michael Green. 1970. Investigation of Heat Transfer in Base Type Supersonic Laminar and Transitional Separated Flows. Defense Technical Information Center. https://doi.org/10.21236/ad0710347
• Romero, F. A. 2021. “Sensitivity Analysis for the Shimmy Dynamics of an Airplane Main Landing Gear.” Journal of Applied Nonlinear Dynamics 10 (3). https://doi.org/10.5890/jand.2021.09.011
• Rooney, Brendan. 2003. “Reusable Launch Vehicle Ground Operational Challenges.” In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. AIAA 2003-2953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2953
• Rose, Eugene J. 1986. Local Gravity Field Modeling. Defense Technical Information Center. https://doi.org/10.21236/ada202550
• Rose, Charlie. 1989. System Study: Radiation Hardened Autonomous Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada205604
• Rose, O., David Miller, James Pittman, P. Ashill, and J. Fulker. 1988. “A Full-Potential Theory Analysis of the Supersonic Aerodynamics of a60-Deg Delta Wing-Body Configuration.” In 26th Aerospace Sciences Meeting. AIAA 1988-480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-480
• Rosema, Christopher C. 2015. “A Comparison of Predictive Methodologies for Missile Configurations with Strakes.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2588
• Rosen, Marc A. 2001. “Exergy Analysis of a Turbojet Engine over a Complete Flight Cycle.” In Advanced Energy Systems. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2001/aes-23645
• Rosenberg, Paul. 1979. Position-Location/Navigation Systems Overview for Military Land Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada088070
• Rosenberg, R., and G. Schuch. 1983. “The M.C.A.-Method, a Flight Test Technique to Determine Thrust of Jet Aircraft in Flight.” In 2nd Flight Testing Conference. AIAA 1983-2749. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2749
• Rosenfeld, Azriel, and Lary S. Davis. 1986. Autonomous Vehicle Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada170379
• Rosenhead, L. 1956. “Springboard for Supersonic Flight.” Nature 177 (4505): 400–401. https://doi.org/10.1038/177400a0
• Rosevear, Jerry. 1992. “Supercharged Ejector Ramjet.” In NASA. Lewis Research Center, Rocket-Based Combined-Cycle (RBCC) Propulsion Technology Workshop. Turorial Session. https://ntrs.nasa.gov/citations/19920012284
• Rosner, D. E., and R. Cibrian. 1974. “Non-Equilibrium Stagnation Region Aerodynamic Heating of Hypersonic Glide Vehicles.” In American Society of Mechanical Engineers. https://ntrs.nasa.gov/citations/19740053212
• Rosner, Jakub, Damian Pęszor, Marcin Paszkuta, et al. 2018. “A System for Automatic Detection of Potential Landing Sites for Horizontally Landing Unmanned Aerial Vehicles.” In AIP Conference Proceedings, vol. 1978. Author(s). https://doi.org/10.1063/1.5043764
• Ross, A. Jean. 1979. “Application of Parameter Identification Techniques to Analysis of Flight Data.” Progress in Aerospace Sciences 18: 325–49. https://doi.org/10.1016/0376-0421(77)90011-2
• Ross, I. 1980. Flightworthy Active Control Landing Gear for a Supersonic Aircraft. NASA-CR-3298. NASA. https://ntrs.nasa.gov/citations/19800018849
• Ross, Paul F. 1994. “Minimizing Errors in Celestial Positioning.” Navigation 41 (3): 251–64. https://doi.org/10.1002/j.2161-4296.1994.tb01879.x
• Rothacker, Benjamin A. 2017. “On the Numerical Stability of the Eminton-Lord Wave Drag Method.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3576
• Rothman, Yaacov, Itzik Klein, and Sagi Filin. 2015. “Analytical Observability Analysis of INS with Vehicle Constraints.” Navigation 62 (3): 249–249. https://doi.org/10.1002/navi.116
• Rounds, Stephen. 1987. “Terminal Guidance with Low Update Rates.” In Guidance, Navigation and Control Conference. AIAA 1987-2592. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2592
• Rounds, S., and G. Marmar. 1983. “Stellar-Inertial Guidance Capabilities for Advanced ICBM.” In Guidance and Control Conference. AIAA 1983-2297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2297
• Roundy, James S. 1979. Demonstration Program for a Flexible Duct Valve for Ramjet Engine Fuel Controls. Defense Technical Information Center. https://doi.org/10.21236/ada078529
• Rowe, W. T., H. R. Welge, E. S. Johnson, and L. S. Rochte. 1981. “Advanced Supersonic Transport Propulsion and Configuration Technology Improvements.” In SAE. https://ntrs.nasa.gov/citations/19810056566
• Rowiński, Artur. 2016. “The Rig Stand for Testing Integrated Rocket Ramjet Engine.” Journal of KONES Powertrain and Transport 23 (4): 421–28. https://doi.org/10.5604/12314005.1217261
• Rowlandson, Lyall G., and John R. Herlihy. 1969. Analysis of Real-Time Refraction Correction Methods for Three Missile Flights from the Air Force Western Test Range. Defense Technical Information Center. https://doi.org/10.21236/ad0692785
• Roy-Aikins, Joseph. n.d. “Generation of the Turbine Characteristics of a Twin-Spool Turbojet and Its Application to Engine Health Monitoring.” PhD diss., Carleton University. https://doi.org/10.22215/etd/1983-00826
• Ruan, S., M. Zhang, Y. Hong, and H. Nie. 2023b. “Influence of Clearance and Structural Coupling Parameters on Shimmy Stability of Landing Gear.” Aeronautical Journal 127 (1315): 1591–1622. https://doi.org/10.1017/aer.2022.109
• Ruan, Shuang, Ming Zhang, Shaofei Yang, and Hong Nie. 2024a. “Dynamics Analysis of Nose Landing Gear Shimmy Performance Considering Aircraft Structural Flexibility.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 239 (8): 727–43. https://doi.org/10.1177/09544100241282717
• Rubin, Donald V. 1971. Rocket Plume Effects on Boattail and Flare Bodies of Revolution at Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0730669
• Ruffin, Paul. 2002. “Fiber Gyroscope Sensors.” In Optical Science and Engineering. CRC Press. https://doi.org/10.1201/9780824744571.ch8
• Ruffin, Paul. 2008. “Fiber Optic Gyroscope Sensors.” In Optical Science and Engineering. CRC Press. https://doi.org/10.1201/9781420053661.ch8
• Ruffin, Paul B. 2017. “Fiber Optic Gyroscope Sensors.” In Fiber Optic Sensors. CRC Press. https://doi.org/10.1201/9781420053661-8
• Ruffin, Stephen, Anurag Gupta, Stephen Ruffin, and Anurag Gupta. 1997. “Supersonic Channel-Airfoils for Reduced Drag.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-517. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-517
• Rummel, Reiner. 1980. Geoid Heights, Geoid Height Differences, and Mean Gravity Anomalies from ‘Low-Low’ Satellite-to-Satellite Tracking: An Error Analysis,. Defense Technical Information Center. https://doi.org/10.21236/ada092707
• Rumsey, Charles B., and Dorothy B. Lee. 1958. Heat-Transfer Measurements in Free Flight at Mach Numbers up to 14.6 on a Flat-Faced Conical Nose with a Total Angle of 29 Degrees. NACA-RM-L57L03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930089952
• Rumsey, Charles B., and Dorothy B. Lee. 1961a. Measurements of Aerodynamic Heat Transfer and Boundary-Layer Transition on a 10 Deg Cone in Free Flight at Supersonic Mach Numbers up to 5.9. NASA-TN-D-745. NASA. https://ntrs.nasa.gov/citations/20040047150
• Rumsey, Charles B., and Dorothy B. Lee. 1961b. Measurements of Aerodynamic Heat Transfer and Boundary-Layer Transition on a 15 Deg. Cone in Free Flight at Supersonic Mach Numbers up to 5.2. NASA-TN-D-888. NASA. https://ntrs.nasa.gov/citations/19980235513
• Runckel, J. F. 1958. Preliminary Transonic Performance Results for Solid and Slotted Turbojet Nacelle Afterbodies Incorporating Fixed Divergent Jet Nozzles Designed for Supersonic Operation. NASA-MEMO-10-24-58L. NASA. https://ntrs.nasa.gov/citations/19650003123
• Russell, W. 1964. “A Unified Concept of a Guidance and Flight Control System for a Ballistic Missile.” In 1st Annual Meeting. AIAA 1964-242. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-242
• Russo, Lorenzo, Renato Tognaccini, and Luciano Demasi. 2020. “Box Wing and Induced Drag: Compressibility Effect in Subsonic and Transonic Regimes.” In AIAA Scitech 2020 Forum. AIAA 2020-0447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0447
• Ruth, J. C. 1968. Analysis of Error Propagation in Aircraft Inertial Navigation Systems. NASA-CR-97074. NASA. https://ntrs.nasa.gov/citations/19680026286
• Ruth, Michael J. 1989. “Flexible Missile Autopilot Design Studies with PC-MATLAB/386.” In NASA. Langley Research Center, Proceedings of the Workshop on Computational Aspects in the Control of Flexible Systems, Part 1. https://ntrs.nasa.gov/citations/19900000772
• Rutishauser, David, Chirold Epp, and Edward Robertson. 2012. “Free-Flight Terrestrial Rocket Lander Demonstration for NASA’s Autonomous Landing and Hazard Avoidance Technology (ALHAT) System.” In AIAA SPACE 2012 Conference & Exposition. AIAA 2012-5239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5239
• Ryan, Jonathan G., and David M. Bevly. 2014. “On the Observability of Loosely Coupled Global Positioning System/Inertial Navigation System Integrations with Five Degree of Freedom and Four Degree of Freedom Inertial Measurement Units.” Journal of Dynamic Systems, Measurement, and Control 136 (2): 021023. https://doi.org/10.1115/1.4025985
• Ryu, Won-Hee, Hyeon-Ho Kim, and Jae-Sang Park. 2025. “Landing Simulations for Reusable Launch Vehicles Incorporating Landing Legs.” International Journal of Aeronautical and Space Sciences 27 (3): 2226–44. https://doi.org/10.1007/s42405-025-01081-8
• Sabatella, J. A. 1974. Advanced Supersonic Propulsion Study. NASA-CR-134633. NASA. https://ntrs.nasa.gov/citations/19740018137
• Sabri, L. M., Bambang Sudarsono, and Rina Dwi Indriana. 2019. “Determination of Vertical Deflection Based on Terestrial Gravity Disturbance Data (a Case Study in Semarang City).” KnE Engineering. https://doi.org/10.18502/keg.v4i3.5834
• Sabzevari, Sanaz, Ahmadreza Vali, Mohammad Hossein Ferdowsi, and Mohammad Reza Arvan. 2020. “Observability Analysis and Design of Two Nested Filters for the Satellite Attitude Estimation with Magnetometer-Only.” IET Radar, Sonar & Navigation 14 (4): 607–18. https://doi.org/10.1049/iet-rsn.2019.0351
• Sacher, Peter, and Bernhard Zellner. 1995. “Flight Testing Objectives for Small Hypersonic Flight Test Vehicles Featuring a Ramjet Engine.” In International Aerospace Planes and Hypersonics Technologies. AIAA 1995-6014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-6014
• Sachs, G., M. Heller, and L. Wahlberg. 1996. “Robust Control of a Hypersonic Experimental Vehicle with Ramjet Engines.” In Guidance, Navigation, and Control Conference. AIAA 1996-3728. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3728
• Sadagopan, Aravinth, Daning Huang, Umran Duzel, Martin E. Liza, and Kyle M. Hanquist. 2021. “Assessment of High-Temperature Effects on Hypersonic Aerothermoelastic Analysis Using Multi-Fidelity Multi-Variate Surrogates.” In AIAA Scitech 2021 Forum. AIAA 2021-1610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1610
• Sadagopan, Aravinth, Daning Huang, and Kyle M. Hanquist. 2020. “Impact of High-Temperature Effects on the Aerothermoelastic Behavior of Composite Skin Panels in Hypersonic Flow.” In AIAA Scitech 2020 Forum. AIAA 2020-0937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0937
• Saetta, Ettore, Renato Tognaccini, and Gianluca Iaccarino. 2023. “Uncertainty Quantification for Machine Learning Aerodynamic Predictions.” Preprint, . https://doi.org/10.2139/ssrn.4631464
• Sagan, Scott D. 1991. “Inventing Accuracy: A Historical Sociology of Nuclear Missile Guidance, by Donald MacKenzie.” Political Science Quarterly 106 (3): 534–36. https://doi.org/10.2307/2151759
• Sahoo, Niranjan, and Ravi Kumar Peetala. 2010. “Transient Temperature Data Analysis for a Supersonic Flight Test.” Journal of Heat Transfer 132 (8): 084503. https://doi.org/10.1115/1.4001128
• Sahu, J. 1985. “Computations of Supersonic Flow over a Missile Afterbody Containing an Exhaust Jet.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1815
• Sahu, Jubaraj. 1986a. Drag Predictions for Projectiles at Transonic and Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada171462
• Sahu, J. 1986b. “Supersonic Flow over Cylindrical Afterbodies with Base Bleed.” In 24th Aerospace Sciences Meeting. AIAA 1986-487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-487
• Sahu, Jubaraj. 2007. Unsteady Flow Computations of a Finned Body in Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ada471736
• Sahu, Jubaraj. 2011. “Unsteady Aerodynamic Simulations of a Canard-Controlled Projectile at Low Transonic Speeds.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6336
• Sahu, Jubaraj, and Frank Fresconi. 2017. “Computational and Experimental Free-Flight Motion of a Subsonic Canard-Controlled Body.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3400
• Sahu, Jubaraj, and Frank Fresconi. 2018. “Validation of Coupled Computations for Pitching Motions of a Canard-Controlled Body with Dynamic Wind Tunnel Data.” In 2018 Applied Aerodynamics Conference. AIAA 2018-4126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4126
• Sahu, Jubaraj, and Frank Fresconi. 2019. “Fast Generation of Aerodynamics Data for a Canard-Controlled Body with Thrust-Vector Control.” In AIAA Aviation 2019 Forum. AIAA 2019-3163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3163
• Sahu, Jubaraj, and Karen Heavey. 2009. “Computations of Supersonic Flow over a Complex Elliptical Missile Configuration.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5714
• Sahu, Jubaraj, and Karen Heavey. 2010. “Time-Accurate Computations for Rapid Generation of Missile Aerodynamics.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8248
• Saint-Mard, M., and P. Hendrick. 1999. “2D and 3D Supersonic Base Drag Reduction Calculation for a TSTO.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4840
• Saito, Toshihito, Fumiei Ono, Kan Kobayashi, Kenji Kudo, Masao Takegoshi, and Shu-ichi Ueda. 2005. “Firing Tests of a Liquid-Hydrogen-Cooling Scramjet Engine in the Ramjet Engine Test Facility 2nd.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-3821. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3821
• Sakai, Takeharu. 2009. “Supersonic Drag Performance of Truncated Cones with Repetitive Energy Depositions.” International Journal of Aerospace Innovations 1 (1): 31–43. https://doi.org/10.1260/175722509787549471
• Sakata, K. 2002. “Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology: Development and Flight Test Plan for the Unmanned Scaled Supersonic Glider.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-527
• Sakata, I. F., and G. W. Davis. 1977. Evaluation of Structural Design Concepts for an Arrow-Wing Supersonic Cruise Aircraft. NASA-CR-2667. NASA. https://ntrs.nasa.gov/citations/19770018637
• Sakata, I. F., G. W. Davis, J. C. Robinson, and E. C. Yates Jr. 1975. “Design Study of Structural Concepts for an Arrow-Wing Supersonic-Cruise Aircraft.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750055457
• Sakran, F. C. 1970. “Long Period Error Modes of a Doppler Radar/Free Directional Gyro Navigation System.” Navigation 17 (1): 39–46. https://doi.org/10.1002/j.2161-4296.1970.tb00019.x
• Sakran, F. C., Jr. 1967. Hybrid Doppler-Radar Inertial Navigation Techniques for the Supersonic Transport Aircraft. NASA-CR-92985. NASA. https://ntrs.nasa.gov/citations/19680007278
• Salomon, P., and W. Goss. 1976. “A Microprocessor-Controlled CCD Star Tracker.” In 14th Aerospace Sciences Meeting. AIAA 1976-116. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-116
• Salvadori, Simone. 2018. “Uncertainty Quantification in CFD: The Matrix of Knowledge.” In Uncertainty Quantification in Computational Fluid Dynamics and Aircraft Engines. Springer International Publishing. https://doi.org/10.1007/978-3-319-92943-9_2
• Salwen, Howard, and Henry Arbour. 1977. Perspective Navigation System. Defense Technical Information Center. https://doi.org/10.21236/ada049260
• Samaan, Malak, Ronney Lovelace, Riana Pecourt, and Greg Holt. n.d. “Optical Navigation Attitude Estimation and Calibration Performance Improvement Using Outlier Rejection.” In 44th Annual AAS Guidance, Navigation and Control Conference. https://ntrs.nasa.gov/citations/20210026612
• Samadzadegan, Farhad, and Sara Saeedi. 2008. “Vision Based Navigation of Aerial Vehicles Based on Geo-Referenced Imagery.” In Computational Intelligence in Decision and Control. WORLD SCIENTIFIC. https://doi.org/10.1142/9789812799470_0181
• Sametov, Dias, Inkar Zhalymbetova, and Toregali Seidegaliev. 2025. “Integration of GNSS and Inertial Navigation System: Correction Algorithms and Accuracy Improvement.” Universum:Technical sciences 4 (133). https://doi.org/10.32743/unitech.2025.133.4.19754
• Sammonds, R. 1970. “Transonic Static- and Dynamic-Stability Characteristics of Two Large-Angle Spherically Blunted High-Drag Cones.” In Propulsion and ASW Meeting. AIAA 1970-564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-564
• Samson, Mikel. 2024. On-Orbit Performance Verification of a Nanosat Star Tracker. https://doi.org/10.52202/078365-0061
• Samuelsson, Leif. 1999. “CUMFAT: A Tool for Life Prediction of Turbojet- and Rocket Engine Components.” In 40th Structures, Structural Dynamics, and Materials Conference and Exhibit. AIAA 1999-1326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1326
• San Martin, Emma, Nicholas Plewacki, Luis G. Bravo, and Muthuvel Murugan. 2025. “Numerical Study of Unstart Phenomena in a Scramjet Inlet-Isolator Model.” In AIAA SCITECH 2025 Forum. AIAA 2025-1464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1464
• San Martin, A. Miguel, Nikolas Trawny, and Dylan Conway. 2022. Vision-Based Velocimetry over Unknown Terrain with a Low-Noise IMU. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20230005717
• Sanchez, Richard D. 2004. Airborne Digital Sensor System and GPS-Aided Inertial Technology for Direct Geopositioning in Rough Terrain. US Geological Survey. https://doi.org/10.3133/ofr20041391
• Sandeep, Juluru. 2023. “Design and Performance of Hypersonic Intake for Scramjet Engine.” In Hypersonic and Supersonic Flight - Advances in Aerodynamics, Materials, and Vehicle Design. IntechOpen. https://doi.org/10.5772/intechopen.107840
• Sanders, Glen A. 1993. “Critical Review of Resonator Fiber Optic Gyroscope Technology.” In SPIE Proceedings, vol. 10266. SPIE. https://doi.org/10.1117/12.145203
• Sanfilippo, F. 1977. “Adaptive Static Margin Controller for Advanced Terminal Interceptors.” In Guidance and Control Conference. AIAA 1977-1064. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1064
• Sanketh, Ailneni. 2012. “Addressing Issues in Inertial Navigation of Micro Aerial Vehicles (MAV) via an Extended Kalman Filter with Biased Sensors.” International Journal of Applied Research in Mechanical Engineering: 17–23. https://doi.org/10.47893/ijarme.2012.1056
• Sanuki, Matao. 1965. “The Optimum Control of an Automatic Landing System of Aircraft.” Journal of the Society of Mechanical Engineers 68 (552): 99–106. https://doi.org/10.1299/jsmemag.68.552_99
• Sarathkumar Sebastin, J., S. Jeyakumar, and K. Karthik. 2021. “The Non-Reacting Flow Characteristics of Pylon and Wall Injections in a Dual Combustion Ramjet Engine.” International Journal of Engine Research 23 (9): 1495–1502. https://doi.org/10.1177/14680874211017856
• Saravanan, R., S. L. N. Desikan, and T. M. Muruganandam. 2017. “Effect of Back Pressure and Freestream Dynamic Pressure on a Typical Ramjet Engine Duct under Realistic Supersonic Inlet Condition.” Aeronautical Journal 122 (1247): 83–103. https://doi.org/10.1017/aer.2017.115
• Sarfaraz, Osama. 2015. “GPS Inertial Missile Guidance System.” Pakistan Journal of Engineering, Technology & Science 4 (2). https://doi.org/10.22555/pjets.v4i2.207
• Sargent, D. 1970. “The Modeling and Verification of the Critical Dynamic Errors of a Strapdown Inertial Guidance System.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-1029. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1029
• Sargent, Donald H., and Cedric Bielawski. 1970. Advanced Fuel Systems for Ramjet-Powered Vehicles. Material Selection for Fuel System Simulator. Defense Technical Information Center. https://doi.org/10.21236/ad0871448
• Sarigul-Klijn, Nesrin, and Jonathan Huber. 2006. “In-Flight Reconfigurable Autopilot for Unmanned Aircraft: Hardware Development and Flight Test Results.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6507
• Sarigul-Klijn, Marti, and Nesrin Sarigul-Klijn. 2003. “Flight Mechanics of Manned Sub-Orbital Reusable Launch Vehicles with Recommendations for Launch and Recovery.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-909. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-909
• Sarkar, A., M. Ananthasayanam, J. Umakant, T. Srinivasan, and P. Kar. 2009. “Flight Vehicle Aerodynamic Coefficients Estimation under Limited Measurements: New Flight-Test Results.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5940. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5940
• Sarkar, A., and S. Panneerselvam. 1998. “Aerodynamic Coefficients Estimation of a Tactical Flight Vehicle from Noisy Flight Test Data under Limited Measurements.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4260
• Sarwar, Md Gulam, Mushtaque Momin, Gulam Anwar, Petha Sethuraman Vignesh Ram, and Saista Tabssum. 2024. “Experimental and Numerical Investigation on Supersonic Intake Buzz: A Survey.” In Advances in Aerospace Technologies. River Publishers. https://doi.org/10.1201/9788770046299-8
• Sasaki, Daisuke, and Shigeru Obayashi. 2003. “Low-Boom Design Optimization for SST Canard-Wing-Fuselage Configuration.” In 16th AIAA Computational Fluid Dynamics Conference. AIAA 2003-3432. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3432
• Sasoh, Akihiro, Manabu Myokan, Henny Bottini, and Akira Iwakawa. 2018. “Mechanisms of Pressure Loss Recovery by Repetitive Energy Deposition in Supersonic Intake Model.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3179. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3179
• Sasoh, Akihiro, Takeharu Sakai, Yohei Sekiya, Atsushi Matsuda, and Jae Hyung Kim. 2009. “Supersonic Drag Reduction with Repetitive Laser Pulses through a Blunt Body.” In 40th AIAA Plasmadynamics and Lasers Conference. AIAA 2009-3585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3585
• Sasoh, Akihiro, Katsuya Shimizu, Kakuei Suzuki, and Atsushi Matsuda. 2010. “Supersonic Free Flight Experiments Using a Square-Bore Ballistic Range.” In 40th Fluid Dynamics Conference and Exhibit. AIAA 2010-4264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4264
• Sateesh, B., and D. K. Maiti. 2009. “The Analysis of Shimmy Instability of a Typical Nose Landing Gear Using Active Torsional Magneto-Rheological Damper.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 223 (3): 201–16. https://doi.org/10.1243/09544100jaero437
• Sato, Tetsuya, Hideyuki Taguchi, Hiroaki Kobayashi, et al. 2006. “Development Study of Precooled-Cycle Hypersonic Turbojet Engine for Flight Demonstration.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-c4.5.02
• Satran, D. R. 1986. Wind-Tunnel Investigation of the Flight Characteristics of a Canard General-Aviation Airplane Configuration. NASA-TP-2623. NASA. https://ntrs.nasa.gov/citations/19870000606
• Saunders, J., and T. Keith Jr. 1991. “Results from Computational Analysis of a Mixed Compression Supersonic Inlet.” In 27th Joint Propulsion Conference. AIAA 1991-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2581
• Saussié, David, Lahcen Saydy, and Ouassima Akhrif. 2008. “Gain Scheduling Control Design for a Pitch-Axis Missile Autopilot.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7000
• Savkin, A., D. Antonov, L. Kolganov, M. Ryabinkin, and E. Chekhov. 2021. “UAV Navigation Using Opto-Electronic and Inertial Means in GNSS-Denied Environment.” Journal of Physics: Conference Series 1925 (1): 012051. https://doi.org/10.1088/1742-6596/1925/1/012051
• Sawai, Shujiro, Kazuhisa Fujita, Hiroaki Kobayashi, et al. 2009. “Development of Supersonic Vehicle for Demonstration of a Precooled Turbojet Engine.” Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan 7 (ists26): Tg_27-Tg_34. https://doi.org/10.2322/tstj.7.tg_27
• Sawyer, James Wayne, and Harold Bush. 1998. “Experimental Investigation of a Graphite-Composite Intertank Section for a Reusable Launch Vehicle.” In AIP Conference Proceedings, vol. 420. AIP. https://doi.org/10.1063/1.54711
• Sawyer, James Wayne, Jefferson Hodge, Brad Moore, and Kevin Snyder. 1999. “Aerothermal Test of Thermal Protection Systems for X-33 Reusable Launch Vehicle.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57501
• Sawyer, W. C., W. J. Monta, W. V. Carter, and W. K. Alexander. 1981. “Control Characteristics for Wrap-around Fins on Cruise Missiles Configurations.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19810036129
• Sayles, Emily L. 2008. Preliminary Design of a Ramjet for Integration with Ground-Based Launch Assist. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20080047449
• Scala, S. M., and E. J. Nolan. 1960. “Aerothermodynamic Feasibility of Graphite for Hypersonic Glide Vehicles.” In Re-Entry and Vehicle Design. Elsevier. https://doi.org/10.1016/b978-1-4832-2885-3.50007-6
• Scandaroli, Glauco Garcia. n.d. “Visuo-Inertial Data Fusion for Pose Estimation and Self-Calibration.” PhD diss., Nice. https://doi.org/10.70675/f158581cz483az438ezb097zbb53e2f8215d
• Scattering Mechanism of over-Horizon UHF Propagation. 2004. Wiley. https://doi.org/10.1002/3527603816.ch6
• Schaechter, David, and James Ellis. 1991. “Direction Cosine Matrix Orthonormalization for Improved Inertial Navigation.” In Navigation and Control Conference. AIAA 1991-2704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2704
• Schaefer, John A., Andrew W. Cary, Earl P. Duque, and Seth Lawrence. 2019. “Application of a CFD Uncertainty Quantification Framework for Industrial-Scale Aerodynamic Analysis.” In AIAA Scitech 2019 Forum. AIAA 2019-1492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1492
• Schaff, Jeff, Matt Bille, Lamberth Blalock, and Stan Bailey. 2000. Future Ballistic Missile Requirements: A First Look. Defense Technical Information Center. https://doi.org/10.21236/ada386860
• Scharnhorst, Richard. 2012. “An Overview of Military Aircraft Supersonic Inlet Aerodynamics.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-13. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-13
• Schenkel, F. W. 1974. Star Tracker/Mapper: System Design Parameters. Defense Technical Information Center. https://doi.org/10.21236/ada008554
• Scher, S. H. 1965. Exploratory Investigations of the Recovery of a Large Booster by Means of Aerodynamic Decelerators and a Hot-Air Balloon. NASA-TM-X-56797. NASA. https://ntrs.nasa.gov/citations/19660020078
• Scher, Stanley, and James Dunavant. 1966. “Preliminary Analytical Study of Booster Recovery by Means of a Drag Balloon Which Converts to a Hot-Air Balloon for Final Recovery.” In Aerodynamic Deceleration Systems Conference. AIAA 1966-1519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1519
• Scherberg, M. G., and Theodore Rubin. 1953. Decelerations of Ballistic Type Missile on Reentry into Atmosphere. Defense Technical Information Center. https://doi.org/10.21236/ad0012619
• Schermerhorn, V. L. 1969. Static Stability and Axial Force Coefficients for the 0.125 Scale Model Mark 82 Low Drag Bomb with Closed Snakeye I Fins at Subsonic and Transonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0863422
• Schetz, J., F. Billig, and S. Favin. 1980. “Approximate Analysis of Base Drag Reduction by Base And/or External Burning for Axisymmetric, Supersonic Bodies.” In 16th Joint Propulsion Conference. AIAA 1980-1258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1258
• Schierman, John, Jason Hull, and David Ward. 2003. “On-Line Trajectory Command Reshaping for Reusable Launch Vehicles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5439
• Schindel, Leon. 1999. “Sensitivity of the Performance of an Integrated Scramjet-Powered Cruise Missile to Propulsion Parameters.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-883
• Schmidt, J. N. 1979. “Similarities between Classical Celestial Navigation and Electrostatic Gyro Navigation.” Navigation 26 (3): 203–18. https://doi.org/10.1002/j.2161-4296.1979.tb01375.x
• Schmidt, Uwe. 2005. “Astro APS: The Next Generation Hi-Rel Star Tracker Based on Active Pixel Sensor Technology.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-5925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5925
• Schmidt, U. 2017. “Autonomous Star Tracker Based on Active Pixel Sensors (APS).” In International Conference on Space Optics — ICSO 2004, edited by Josiane Costeraste, Errico Armandillo. SPIE. https://doi.org/10.1117/12.2307969
• Schmidt, S. F., W. S. Bjorkman, and B. Conrad. 1973. New Mechanization Equations for Aided Inertial Navigation Systems. NASA-CR-2352. NASA. https://ntrs.nasa.gov/citations/19740004245
• Schmidt, Uwe, Christian Elstner, and Klaus Michel. 2008. “ASTRO 15 Star Tracker Flight Experience and Further Improvements towards the ASTRO APS Star Tracker.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6649. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6649
• Schmidt, R., and B. Mann. 1996. “Reusable Launch Vehicle/X-33 Preliminary Structural Analysis for Dynamic Launch Environments.” In Dynamics Specialists Conference. AIAA 1996-1199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-1199
• Schmitt, Curtis, and Bradley Burchett. 2004. “Fuzzy IPPD Guidance for Approach and Landing of a Reusable Launch Vehicle.” In AIAA 1st Intelligent Systems Technical Conference. AIAA 2004-6254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-6254
• Schneider, Alan M. 1983. “Kalman Filter Formulations for Transfer Alignment of Strapdown Inertial Units.” Navigation 30 (1): 72–89. https://doi.org/10.1002/j.2161-4296.1983.tb00824.x
• Schnell, Samuel. 2023. “Development of an Aerodynamic Surrogate Model for Conceptual Supersonic Aircraft Design Based on DLR TAU Simulations.” In AIAA AVIATION 2023 Forum. AIAA 2023-3726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3726
• Schnepf, Christian, Erich Schuelein, and Josef Klevanski. 2017. “Experimental Und Numerical Investigation of the Aerodynamic Characteristic of a Generic Transonic Missile.” In 35th AIAA Applied Aerodynamics Conference. AIAA 2017-3401. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3401
• Schnerr, Guenter, and Ulrich Dohrmann. 1991. “Drag and Lift in Nonadiabatic Transonic Flow.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1716
• Schoch, K. F., and B. Darrel. 1967. “A Superconducting Gyroscope for Gimballed Platform Application.” In Advances in Cryogenic Engineering. Springer US. https://doi.org/10.1007/978-1-4757-0489-1_68
• Schoenman, R. L., and J. Doniger. 1965. “The Boeing/Bendix Automatic Landing System for the 707 Aircraft.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/650571
• Schoneman, Joe. 2019. “Aeroelastic Verification of a Dynamic Aerothermoelastic Analysis Framework.” In AIAA Scitech 2019 Forum. AIAA 2019-1119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1119
• Schouten, Gerrit, and Peter Bakker. 2000. “Supersonic Flight without Downward Shockwave.” In 6th Aeroacoustics Conference and Exhibit. AIAA 2000-2018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2018
• Schreiter, K., S. Müller, R. Luckner, and D. Manzey. 2017. “nxControl: Ground Mode for Manual Flight Control Laws with Longitudinal Load Factor Command.” In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing. https://doi.org/10.1007/978-3-319-65283-2_11
• Schuelein, Erich. 2008. “Wave Drag Reduction Approach for Blunt Bodies at High Angles of Attack: Proof-of-Concept Experiments.” In 4th Flow Control Conference. AIAA 2008-4000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4000
• Schuelein, Erich. 2015. “Simplified Model for Flow-Heating Effect on Wave Drag of Blunt Bodies and Its Validation.” In 45th AIAA Fluid Dynamics Conference. AIAA 2015-2778. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2778
• Schülein, E. 2009. “Wave Drag Reduction Concept for Blunt Bodies at High Angles of Attack.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_84
• Schülein, E., and E. Bornhöft. 2012. “Potential of Localized Flow Heating for Wave Drag Reduction.” In 28th International Symposium on Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-25688-2_93
• Schuler, Maximilian, and J. M. Slater. 1967. “The Disturbance of Pendulum and Gyroscopic Apparatus by the Acceleration of the Vehicle.” Navigation 14 (1): 26–32. https://doi.org/10.1002/j.2161-4296.1967.tb02190.x
• Schulte, Richard J., and Donald W. Dickinson. 1968. Four Methods of Solving for the Spherical Error Probable Associated with a Three-Dimensional Normal Distribution. Defense Technical Information Center. https://doi.org/10.21236/ad0666646
• Schutz, B. E. 1988. Advanced Simulation and Analysis of a Geopotential Research Mission. NASA-CR-182355. NASA. https://ntrs.nasa.gov/citations/19880004726
• Schwanz, R., and G. Grimes. 1980. “Parameter Identification of B-52E CCV Flight Test Data Including Aeroelastic Effects.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1635
• Schwartz, S. 2008. “Solid-State Ring Laser Gyroscope.” Annales de Physique 33 (1–2): 1–226. https://doi.org/10.1051/anphys:2008047
• Schwartz, Sylvain, Gilles Feugnet, Evguenii Lariontsev, and Jean-Paul Pocholle. 2007b. “Oscillation Regimes of a Solid-State Ring Laser with Active Beat-Note Stabilization: From a Chaotic Device to a Ring-Laser Gyroscope.” Physical Review A 76 (2): 023807. https://doi.org/10.1103/physreva.76.023807
• Schwartz, C. A., and H. Özbay. 1990. “Recursive Identification Algorithms as Nonlinear Systems: Parameter Identifiability and Controllability.” In Nonlinear Control Systems Design 1989. Elsevier. https://doi.org/10.1016/b978-0-08-037022-4.50024-7
• Schwarz, Harvey. 1954. “Dectra and Delrac Long Range Navigation Aids.” Navigation 4 (3): 129–36. https://doi.org/10.1002/j.2161-4296.1954.tb00139.x
• Schwarz, K. P. 1978. “Accuracy of Vertical Deflection Determination by Present-Day Inertial Instrumentation.” In Ohio State Univ. Appl. of Geodesy to Geodyn., an Intern. Symp.. https://ntrs.nasa.gov/citations/19790013329
• Schwarz, K. P. 1980. “Error Propagation in Inertial Positioning.” Canadian Surveyor 34 (3): 265–76. https://doi.org/10.1139/tcs-1980-0036
• Schwarz, Klaus-Peter. 1981. Gravity Induced Position Errors in Airborne Inertial Navigation,. Defense Technical Information Center. https://doi.org/10.21236/ada113823
• Schweppe, F. C. 1964. Algorithms for Estimating a Re-Entry Body’s Position, Velocity and Ballistic Coefficient in Real Time or for Post Flight Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0609524
• Sciegienny, Janusz, Roy Nurse, Peter Kampion, and John Wexler. 1978. Inertial Navigation System Standardized Software Development. Volume II. INS Survey and Analytical Development. Defense Technical Information Center. https://doi.org/10.21236/ada062803
• Scott, W. A. 1956. “A Course Computer for Long Range Polar Navigation.” Journal of Navigation 9 (3): 365–365. https://doi.org/10.1017/s0373463300036547
• Scott, R. B. 1963. Model Specification Liquid Propellant Rocket Engine Rocketdyne Model YLR105-NA-7, Sustainer. Defense Technical Information Center. https://doi.org/10.21236/ad0410255
• Scott, Francis P. 1964. “Limitations Imposed on Celestial Navigation Due to Inaccuracies of Star Positions.” Navigation 11 (1): 20–25. https://doi.org/10.1002/j.2161-4296.1964.tb02071.x
• Scott, J., W. Leslie, and D. Norausky. 1983. “Pacific Missile Test Center Range Capabilities.” In 2nd Flight Testing Conference. AIAA 1983-2790. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2790
• Scoville, Andrew, and Joseph Yamron. 1966. “The Mechanization of a Strapdown Inertial System Based on Time-Modulated Torquing.” In Guidance and Control Conference. AIAA 1966-1812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1812
• Seaberg, Ernest C. 1950. Theoretical Investigation of a Proportional-Plus-Flicker Automatic Pilot. NACA-RM-L50I19. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019266
• Seaberg, Ernest C. 1954. Three-Degree-of-Freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed. NACA-RM-L54C02. NASA. https://ntrs.nasa.gov/citations/19930088166
• Seaberg, Ernest C. 1957. Three-Degree-of Freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed. NACA-TN-4192. NASA. https://ntrs.nasa.gov/citations/19930085149
• Seaberg, Ernest C., and Earl F. Smith. 1951. Theoretical Investigation of an Automatic Control System with Primary Sensitivity to Normal Accelerations as Used to Control a Supersonic Canard Missile Configuration. NACA-RM-L51D23. NASA. https://ntrs.nasa.gov/citations/19930086720
• Seacord, Charles L., and John P. Campbell. 1945. Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel. NACA-ACR-L5A13. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930092552
• “Seal for a Turbojet Engine Pylon and Nacelle.” 2013. Sealing Technology 2013 (11): 12. https://doi.org/10.1016/s1350-4789(13)70412-4
• “Sealing Device for an Aircraft Turbojet Engine Nacelle.” 2020. Sealing Technology 2020 (1): 11–11. https://doi.org/10.1016/s1350-4789(20)30021-0
• Sears, William R. 1947. “On Projectiles of Minimum Wave Drag.” Quarterly of Applied Mathematics 4 (4): 361–66. https://doi.org/10.1090/qam/20394
• Sease, Brad, Ryan Koglin, and Brien Flewelling. 2013. “Long-Integration Star Tracker Image Processing for Combined Attitude-Attitude Rate Estimation.” In SPIE Proceedings, vol. 8739, edited by Khanh D. Pham, Joseph L. Cox, Richard T. Howard, Genshe Chen. SPIE. https://doi.org/10.1117/12.2020004
• Sedlock, Dennis. 1985. Improved Statistical Analysis Method for Prediction of Maximum Inlet Distortion. Defense Technical Information Center. https://doi.org/10.21236/ada153767
• Seeley, Richard B., and Roy Dale Cole. 1960. “Initial Alignment of a Moving Inertial Navigation System.” Journal of Navigation 13 (3): 301–15. https://doi.org/10.1017/s0373463300033622
• Seidelmann, P. K., R. Gaume, N. Zacharias, K. Johnston, and B. Dorland. 2007. Optical Reference Star Catalogs for Space Surveillance: Current Status and Future Plans. Defense Technical Information Center. https://doi.org/10.21236/ada480193
• Seider, G., and D. Haenel. 1991. “Numerical Influence of Upwind TVD Schemes on Transonic Airfoil Drag Prediction.” In 29th Aerospace Sciences Meeting. AIAA 1991-184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-184
• Seifert, L. I. 1970. Star-Tracker Systems. Kollsman Instrument Corp. https://ntrs.nasa.gov/citations/19700027415
• Seigler, T. Michael, Jae-Sung Bae, and Daniel J. Inman. 2004. “Flight Control of a Variable Span Cruise Missile.” In Dynamic Systems and Control, Parts A and B. ASMEDC. https://doi.org/10.1115/imece2004-61961
• Seiple, E. L. 1960. Production Engineering Test of Guided Missile XM5E3 Warhead. Defense Technical Information Center. https://doi.org/10.21236/ad0315737
• Sekar, Chandra, Ramraj Sundararaj, Rajat Arora, and Abhijit Kushari. 2021. “Analysis of Failed Startup Sequence of a Single Spool Turbojet Engine.” Preprint, . https://doi.org/10.1115/1.0002966v
• Selberg, B. P., and D. L. Cronin. 1985. Aerodynamic-Structural Study of Canard Wing, Dual Wing, and Conventional Wing Systems for General Aviation Applications. NASA-CR-172529. NASA. https://ntrs.nasa.gov/citations/19850008520
• Selberg, B., and K. Rokhsaz. 1985. “Aerodynamic Tradeoff Study of Conventional, Canard, and Tri-Surface Aircraft Systems.” In 3rd Applied Aerodynamics Conference. AIAA 1985-4071. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-4071
• Seldon, M. R., and D. W. Pertschuk. 1954. “The Experimental Determination of Guided Missile Reliability.” Journal of the Operations Research Society of America 2 (1): 31–40. https://doi.org/10.1287/opre.2.1.31
• Selected Ballistic Missile Programs. 2008. https://doi.org/10.5040/9798400686375.0018
• Selected Cruise Missile Programs. 2008. https://doi.org/10.5040/9798400686375.0017
• Selezneva, TSaotsu Hu Neusypin K.А. Kupriyanov A. O. Proletarskiy A. V. M. S. 2024. “Study of the Influence of the Parametric Identifiability Degree on the Estimation Accuracy of Navigation System Errors.” Automation Modern Techologies: 158–63. https://doi.org/10.36652/0869-4931-2024-78-4-158-163
• Sen, J. K. 1990a. Advanced Technology Landing Gear. Volume 1 Design. Defense Technical Information Center. https://doi.org/10.21236/ada227196
• Sen, J. K. 1990b. Advanced Technology Landing Gear. Volume 2. Test. Defense Technical Information Center. https://doi.org/10.21236/ada227197
• Sengupta, Prasenjit. 2025. “A Horizontal Accuracy Metric for Magnetic Navigation.” NAVIGATION: Journal of the Institute of Navigation 72 (4): navi.717. https://doi.org/10.33012/navi.717
• “Sensor Failure Detection, Identification and Accommodation Using on-Line Learning Neural Architectures.” 1994. In Guidance, Navigation, and Control Conference. AIAA 1994-3598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3598
• Seo, Min-Won, Hyuck-Hoon Kwon, and Han-Lim Choi. 2018b. “Sum-of-Squares-Based Region of Attraction Analysis for Gain-Scheduled Three-Loop Autopilot.” International Journal of Aeronautical and Space Sciences 19 (1): 196–207. https://doi.org/10.1007/s42405-018-0008-4
• Seo, Yangwoo, Kyeshin Lee, Younho Lee, and Jeyong Kim. 2018a. “Reliability Prediction Based on Field Failure Data of Guided Missile.” Journal of Applied Reliability 18 (3): 250–59. https://doi.org/10.33162/jar.2018.09.18.3.250
• Seo, Minseok, and Jongho Park. 2025. “Terminal Homing Guidance Algorithm for Ballistic Missile Interception Based on Deep Reinforcement Learning.” Journal of the Korean Society for Aeronautical & Space Sciences 53 (9): 975–84. https://doi.org/10.5139/jksas.2025.53.9.975
• Seraj, Sabet, and Joaquim R. Martins. 2023. “Minimum Trim Drag for a Three-Surface Supersonic Transport Aircraft.” In AIAA AVIATION 2023 Forum. AIAA 2023-3472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3472
• Serdarevic-Kadic, Sabina, and Jasmin Terzic. 2019. “Effects of Base Shape to Drag at Transonic and Supersonic Speeds by CFD.” In DAAAM International Scientific Book. DAAAM International Vienna. https://doi.org/10.2507/daaam.scibook.2019.06
• “A Series of Airfoils Designed by Transonic Drag Minimization for Gates Learjet Aircraft.” 1982. In Transonic Aerodynamics. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865558.0489.0509
• Serre, Laurent. 2009. “Development of S4 Free Jet Test Facility for the French LEA Flight Test Program.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7358
• Serre, Laurent, and Francois Falempin. 2008. “Development of S4 Free Jet Test Facility for the French LEA Flight Test Program.” In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2008-2651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-2651
• Servotte, Thomas. n.d. “Innovative Tools for Robust Statistics and Optimal Experiment Design.” PhD diss., University of Antwerp. https://doi.org/10.63028/10067/2128350151162165141
• Sethi, Kartikeya. 2024. “Reinforcement Learning in Missile Guidance: A New Era of Tactical Precision.” Preprint, ScienceOpen. https://doi.org/10.14293/pr2199.000691.v1
• Sethi, Kartikeya. 2025. “RL-Based Adaptive Control for Hypersonic Glide Vehicles under Uncertainty.” Preprint, ScienceOpen. https://doi.org/10.14293/pr2199.001888.v1
• Setiawan, Budi, Erlangga Galih Wisnu Wardhana, Nanang Firman Alamie, and Raden Parianom. 2025. “Life Cycle Cost Calculation Model Main Tools of the Weapon System Indonesian National Army.” Journal of Lifestyle and SDGs Review 5 (3): e03872. https://doi.org/10.47172/2965-730x.sdgsreview.v5.n03.pe03872
• Severance, Robert W. 1989. “Overdetermined Celestial Fix by Iteration.” Navigation 36 (4): 373–78. https://doi.org/10.1002/j.2161-4296.1989.tb01526.x
• Seywald, Hans, Eugene Cliff, and Klaus Well. 1991. “Range Optimization for a Supersonic Aircraft.” In Navigation and Control Conference. AIAA 1991-2712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2712
• Sforza, Pasquale. 2014. “Landing Gear Design.” In Commercial Airplane Design Principles. Elsevier. https://doi.org/10.1016/b978-0-12-419953-8.00007-3
• Shaferman, Vitaly, and Tal Shima. 2010. “Cooperative Multiple Model Adaptive Guidance for an Aircraft Defending Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8320. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8320
• Shaffer, Patrick, I. Ross, Michael Oppenheimer, and David Doman. 2005. “Optimal Trajectory Reconfiguration and Retargeting for a Reusable Launch Vehicle.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6148
• Shah, Syed Hassan R., and Anwar Ahmed. 2023. “An Investigation of the Canard Aspect Ratio and Spacing on the Aerodynamics of the Main Wing.” In AIAA SCITECH 2023 Forum. AIAA 2023-1982. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1982
• Shahoud, Ayham, Dmitriy Shashev, and Stanislav Shidlovskiy. 2021. “Detection of Good Matching Areas Using Convolutional Neural Networks in Scene Matching-Based Navigation Systems.” In Proceedings of the 31th International Conference on Computer Graphics and Vision. Volume 2. Keldysh Institute of Applied Mathematics. https://doi.org/10.20948/graphicon-2021-3027-443-452
• Shaikh, Aniba. 2025. “Astro-Quantum Navigation Array: Fusing Star Tracking, Quantum Sensing, and AI for GPS-Free Autonomous Navigation.” Preprint, . https://doi.org/10.2139/ssrn.5395070
• Shalom, E., J. W. Alexander, and R. H. Stanton. 1985. Acquisition and Track Algorithms for the Astros Star Tracker. AAS PAPER 85-050. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/19860047060
• Shan, Tiehua, Dan Wang, Wenlong Zuo, and Zheng Yang. 2025. “Compensation Method for Full Temperature Misalignment Angle of Fiber Optic Gyroscope Based on Rotation Testing.” In Tenth Symposium on Novel Optoelectronic Detection Technology and Applications, edited by Chen Ping. SPIE. https://doi.org/10.1117/12.3057062
• Shang, Changhong. 1990. “Linearity Analysis of Fiber-Optic Gyroscope.” In International Conference on Optoelectronic Science and Engineering ‘90. SPIE. https://doi.org/10.1117/12.2294818
• Shang, Song Tian, and Wen Shao Gao. 2012. “Application of Adaptive Kalman Filter Technique in Initial Alignment of Single-Axial Rotation Strap-Down Inertial Navigation System.” Advanced materials research 466-467: 617–21. https://doi.org/10.4028/www.scientific.net/amr.466-467.617
• Shang, Kejun, Ming Lei, Haowei Li, et al. 2022. “Ultra-Small Interferometric Fiber Optic Gyroscope with an Integrated Optical Chip.” Chinese Optics Letters 20 (4): 040601. https://doi.org/10.3788/col202220.040601
• Shang, Kejun, Ming Lei, Qiang Xiang, Yonglin Na, Lizhe Zhang, and Huaiyong Yu. 2020. “Near-Navigation-Grade Interferometric Fiber Optic Gyroscope with an Integrated Optical Chip.” Chinese Optics Letters 18 (12): 120601. https://doi.org/10.3788/col202018.120601
• Shanks, S., and J. Ahmad. 1991. “Aerodynamics of Powered Missile Separation from a Wing.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1663. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1663
• Shantz, I. 1953. Wind-Tunnel Investigation of the Cvac Supersonic Bomber (HUSTLER-MX-1964). Defense Technical Information Center. https://doi.org/10.21236/ad0037850
• Shapin, Steven. 1991. “Inventing Accuracy: A Historical Sociology of Nuclear Missile Guidance.Donald MacKenzie.” American Journal of Sociology 97 (2): 553–55. https://doi.org/10.1086/229798
• Sharifzadeh, Shayan, Patrick Hendrick, Shaun D’Mello, Dries Verstraete, and François Thirifay. 2014. “Structural Design Optimisation and Aerothermoelastic Analysis of LAPCAT A2 Mach 5 Cruise Vehicle.” In 14th AIAA Aviation Technology, Integration, and Operations Conference. AIAA 2014-2294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2294
• Sharma, Divyam. n.d. “Extrinsic Alignment of FMCW Radar with Inertial and Visual Sensors for Multisensor Systems.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2025-16784
• Sharma, Manu, and Nathan Richards. 2004. “Adaptive, Integrated Guidance and Control for Missile Interceptors.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4880. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4880
• Sharp, W. H. 1957. “Alloy Titanium in the J57 Turbojet Engine.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/570197
• Shaw, B. D. 1984. “The Annular Flow Electrothermal Ramjet.” PhD diss., Colorado State Univ.. https://ntrs.nasa.gov/citations/19840023205
• Shaw, L., I. Paul, and P. Henrikson. 1969. “Statistical Models for the Vertical Deflection from Gravity-Anomaly Models.” Journal of Geophysical Research 74 (17): 4259–65. https://doi.org/10.1029/jb074i017p04259
• Shaw, G. L., J. Rotge, and B. J. Simmons. 1986. “Progress on 58m2 Passive Resonant Ring Laser Gyroscope.” In SPIE Proceedings, vol. 0566. SPIE. https://doi.org/10.1117/12.949768
• Shayler, J. S. 1961. “Radio Guidance Elements of the B.L.E.U. Automatic Landing System for Aircraft.” Journal of the British Institution of Radio Engineers 21 (1): 17–32. https://doi.org/10.1049/jbire.1961.0004
• Sheem, Sang K. 1980. “Fiber-Optic Gyroscope with [3×3] Directional Coupler.” Applied Physics Letters 37 (10): 869–71. https://doi.org/10.1063/1.91867
• Shefer, M. 1990. “Optimal Missile Guidance with Feedback Pulse Motor Control.” In Guidance, Navigation and Control Conference. AIAA 1990-3376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3376
• Sheikhpour Kourabbaslou, Soroush. n.d. “Enhanced Design, Optimal Tuning, and Parallel Real-Time Implementation of Monocular Visual-Inertial-GNSS Navigation System.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2021-14772
• Sheldon, G. J. 1967. Re-Entry Module/Adapter Interconnect Fairing Aerodynamic Heating Wind Tunnel Tests AEDC Tunnel B. Defense Technical Information Center. https://doi.org/10.21236/ad0856658
• Sheldrick, J. H. 1967. “Inertial Navigation Systems for Subsonic and Supersonic Commercial Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/670329
• Shen, Chong. 2021a. “Noise Analysis and Processing Technology for Gyroscope.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-33-4516-4_3
• Shen, Chong. 2021b. “Synopsis of Typical Inertial Sensors and System.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-33-4516-4_2
• Shen, Chong. 2021c. “Temperature Drift Modeling and Compensation for Gyroscope.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-33-4516-4_4
• Shen, Sheng-Chih, Chia-Jung Chen, and Hsin-Jung Huang. 2010a. “A New Calibration Method for Low Cost Mems Inertial Sensor Module.” Journal of marine science and technology 18 (6). https://doi.org/10.51400/2709-6998.1939
• Shen, Shilei, and Linlong Ma. 2022. “Research on the Built-in Test Design of Civil Aircraft Flight Control System.” Journal of Physics: Conference Series 2252 (1): 012010. https://doi.org/10.1088/1742-6596/2252/1/012010
• Shen, Yufei, and Zia-ur Rahman. 2011. “An Automatic Computer-Aided Detection System for Aircraft Emergency Landing.” In Infotech@Aerospace 2011. AIAA 2011-1465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1465
• Shen, Kai, Yuanqing Xia, Meiling Wang, Konstantin A. Neusypin, and Andrey V. Proletarsky. 2018. “Quantifying Observability and Analysis in Integrated Navigation.” Navigation 65 (2): 169–81. https://doi.org/10.1002/navi.225
• Shen, Ying, and Hui Zhang. 2012. “Identifiability of Quantized Linear Systems.” In InTech eBooks. https://doi.org/10.5772/39274
• Shen, Jiahe, Xiaodong Zhang, Yazhou Yue, Qi Zhou, Nan Liu, and Shu Wang. 2025. “Vision-Inertial Fusion Navigation for Autonomous Landing Navigation of Large Aircraft.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2268-9_38
• Sheng, Chunhua, Xiao Wang, Montgomery Hughson, and David Marcum. 2008. “Unsteady Navier-Stokes Simulations of a Canard-Controlled Missile Configuration.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-7324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7324
• Sheporaitis, L., E. Balbirnie, and G. Liebner. 1976. “Practical Optimal Steering for Missile Terminal Guidance.” In Guidance and Control Conference. AIAA 1976-1917. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1917
• Shepperd, Stanley, and Andrew Staugler. 1999. “Autonomous on-Orbit Targeting and Guidance for a Reusable Launch Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4209
• Sher, Ibrahim, Adnan M. Maqsood, Jehanzeb Masud, Usman Zia, Muhammad Farhat Asim, and Uzair Yusuf. 2022. “Dynamic Analysis of High Alpha Coning Motion Aerodynamic Characteristics of a Supersonic Aircraft.” In AIAA SCITECH 2022 Forum. AIAA 2022-0433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0433
• Sherman, W. L. 1975. Effect of External Disturbances and Data Rate on the Response of an Automatic Landing System Capable of Curved Trajectories. NASA-TN-D-7971. NASA. https://ntrs.nasa.gov/citations/19750022975
• Sherman, W. L. 1976. Generalization and Refinement of an Automatic Landing System Capable of Curved Trajectories. NASA-TN-D-8336. NASA. https://ntrs.nasa.gov/citations/19770005089
• Sherman, W. L., and S. W. Winfrey. 1974. Preliminary Study of a Possible Automatic Landing System. NASA-TN-D-7611. NASA. https://ntrs.nasa.gov/citations/19740021006
• Shevchenko, S. A., I. A. Popov, and B. E. Melnikov. 2025. “Optical Method for Material Imperfections Identification in the Resonator Workpiece of Hemispherical Vibratory Gyroscope.” Advanced Engineering Research (Rostov-on-Don) 25 (4): 311–23. https://doi.org/10.23947/2687-1653-2025-25-4-2202
• Shi, X., J-T. Chang, W. Bao, D. Yu, and B. Li. 2010b. “Supersonic Inlet Buzz Margin Control of Ducted Rockets.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 224 (10): 1131–39. https://doi.org/10.1243/09544100jaero687
• Shi, Jiarui, Yugang Zhang, Yuchao He, and Yijia Wei. 2025. “Study on the Influence of Structural Clearance Evolution on Landing Gear Shimmy.” In Advances in Transdisciplinary Engineering. IOS Press. https://doi.org/10.3233/atde250101
• Shiau, Jaw Kuen, Der-Ming Ma, Chen Xuan Huang, and Ming Yu Chang. 2011. “MEMS Gyroscope Null Drift and Compensation Based on Neural Network.” Advanced materials research 255-260: 2077–81. https://doi.org/10.4028/www.scientific.net/amr.255-260.2077
• Shigematsu, Junji, Kazuomi Yamamoto, Kazuo Shiraishi, and Atsushige Tanaka. 1990. “A Numerical Investigation of Supersonic Inlet Using Implicit TVD Scheme.” In 26th Joint Propulsion Conference. AIAA 1990-2135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2135
• Shigematsu, Junji, Kazuomi Yamamoto, Kazuo Shiraishi, and Atsushige Tanaka. 1991. “A Numerical Investigation for Supersonic Inlet with Throat Cavity.” In 27th Joint Propulsion Conference. AIAA 1991-2477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2477
• Shillito, Thomas B., Donald P. Hearth, and Edgar M. Cortright. 1956. Exhaust Nozzles for Supersonic Flight with Turbojet Engines. NACA-RM-E56A18. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/20090024829
• Shim, David Hyunchul, Sungsik Huh, and Byung-mun Min. 2008. “A Vision-Based Automatic Landing System for Fixed-Wing UAVs Using an Inflated Airbag.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7450
• Shima, Tal, and Oded Golan. 2008. “Exo-Atmospheric Guidance of an Accelerating Interceptor Missile.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6494. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6494
• Shima, Tal, Yaakov Oshman, and Josef Shinar. 2000. “An Efficient Application of Multiple Model Adaptive Estimation in Ballistic Missile Interception Scenarios.” In 18th Applied Aerodynamics Conference. AIAA 2000-4274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4274
• Shimabukuro, K., H. Welge, and A. Lee. 1979. “Inlet Design Studies for a Mach 2.2 Advanced Supersonic Cruise Vehicle.” In Aircraft Systems and Technology Meeting. AIAA 1979-1814. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1814
• Shin, Phil-Kwon. 2005. “Buzz Suppression of Supersonic Air Inlet by Cowl Position Modification.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (3): 10–17. https://doi.org/10.5139/jksas.2005.33.3.010
• Shin, Eun-Hwan, and Naser El-Sheimy. 2007. “Unscented Kalman Filter and Attitude Errors of Low-Cost Inertial Navigation Systems.” Navigation 54 (1): 1–9. https://doi.org/10.1002/j.2161-4296.2007.tb00390.x
• Shinar, J., Y. Lipman, and M. Zarkh. 1995. “Mixed Strategies in Missile versus Missile Interception Scenarios.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 6. American Autom Control Council. https://doi.org/10.1109/acc.1995.532706
• Shindo, Shigemi, and Ryoji Yanagi. 1998. “Schlieren Photograph of Intake Throat in The Supersonic Ramjet Engine Test.” Journal of the Visualization Society of Japan 18 (Supplement1): 177–80. https://doi.org/10.3154/jvs.18.supplement1_177
• Shipplett, C. 1982. “Evaluation of AIRS Inertial Measurement Unit Accuracy from Rocket Sled Test Data.” In Guidance and Control Conference. AIAA 1982-1500. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1500
• Shipplett, C. 1983. “Use of Range Vernier Data in Missile Post-Flight Accuracy Evaluation.” In Guidance and Control Conference. AIAA 1983-2266. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2266
• Shiraishi, Yohei, and Takeshi Yamasaki. 2020. “Uncertain Autopilot Lag-Compensated Intercept Guidance for Integrated Guidance and Autopilot.” In AIAA Scitech 2020 Forum. AIAA 2020-1872. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1872
• Shirokov, M. V., D. Yu. Strelets, and I. G. Bashkirov. 2024. “Optimization of the Aerodynamic Configuration of the Isolated Wing for the Second-Generation Supersonic Passenger Aircraft.” Russian Aeronautics 67 (1): 70–79. https://doi.org/10.3103/s1068799824010082
• Shirron, Peter J., Michael J. DiPirro, Edgar R. Canavan, et al. 2010. Orbital Gravity Gradiometry beyond GOCE: Mission Concepts. LEGNEW-OLDGSFC-GSFC-LN-1010. NASA Goddard Space Flight Center. https://ntrs.nasa.gov/citations/20180000014
• Shiryaev, A. V., M. V. Maysak, V. V. Kremenchutsky, R. M. Safin, and V. V. Demidov. 2023. “On the Issue of Reducing the Temperature Heating of the Airframe Structure of a Supersonic Aircraft.” E3S Web of Conferences 383: 05009. https://doi.org/10.1051/e3sconf/202338305009
• Shistik, Eugene, and Asher Sigal. 2002. “The Interaction between Canards and Thick Bodies: Implementation in the Missile Datcom Code.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-3266. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3266
• Shkolnikov, I., Y. Shtessel, D. Lianos, and A. Thies. 2000. “Robust Missile Autopilot Design via High-Order Sliding Mode Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-3968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3968
• Short-Range Radio Navigation. 2018. Wiley. https://doi.org/10.1002/9781119262367.ch7
• Shortal, Joseph A. 1952. “Naca’s Role in Guided Missile Research.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/520145
• Shortal, Joseph A. 1953. “The N.A.C.A.’s Role in Guided Missile Research.” Aircraft Engineering and Aerospace Technology 25 (4): 96–100. https://doi.org/10.1108/eb032278
• Shro, D. J. 1968. Exploring in Aerospace Rocketry. 12: Inertial Guidance Systems. NASA-TM-X-52399. NASA. https://ntrs.nasa.gov/citations/19680011769
• Shrout, B. L., and R. H. Fournier. 1979. Aerodynamic Characteristics of a Supersonic Cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30. NASA-TM-78792. NASA. https://ntrs.nasa.gov/citations/19790005854
• Shtessel, Y. B. 1995. “Decentralized Sliding Mode Control in Inertial Navigation Systems.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 5. American Autom Control Council. https://doi.org/10.1109/acc.1995.533795
• Shtessel, Yuri B. 2001. Smooth Sliding Mode Controller Design for Robust Missile Autopilot. Defense Technical Information Center. https://doi.org/10.21236/ada396963
• Shtessel, Yuri, Charles Hall, and Mark Jackson. 2000. “Reusable Launch Vehicle Control in Multiple Time Scale Sliding Modes.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4155
• Shtessel, Y., and D. Krupp. n.d. “Sliding Mode Control of Reusable Launch Vehicle in Launch and Re-Entry Modes.” In Proceedings The Twenty-Ninth Southeastern Symposium on System Theory. IEEE Comput. Soc. Press. https://doi.org/10.1109/ssst.1997.581723
• Shtessel, Yuri, and Christian Tournes. 2012. “Higher- Order Sliding Modes for Missile Guidance and Control.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-7
• Shtessel, Yuri, Christian Tournes, Don Krupp, Yuri Shtessel, Christian Tournes, and Don Krupp. 1997. “Reusable Launch Vehicle Control in Sliding Modes.” In Guidance, Navigation, and Control Conference. AIAA 1997-3533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3533
• Shu, Julius. 1989. “Generalized KLE Algorithm for Real-Time Gravity Compensation.” In Guidance, Navigation and Control Conference. AIAA 1989-3437. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3437
• Shuang, Li, and Cui Pingyuan. 2006. “Vision-Aided Inertial Navigation for Pinpoint Lunar Landing.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-a3.6.07
• Shue, Shyh-Pyng, Ramesh Agarwal, and Yao-Huang Kuo. 1998. “Design of Automatic Landing Systems Using Mixed H2/H-Infinity Control.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-501
• Shue, Shyh-Pung, M. Sawan, and Kamran Rokhsaz. 1996. “Mixed H2/H-Infinity Gain Scheduling Control of Aircraft.” In Guidance, Navigation, and Control Conference. AIAA 1996-3779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3779
• Shufang Zhao, Yu Wang, and Hongtao Wang. 2012. “Study on Detection Sensitivity of Missile-Borne Star Tracker.” In International Conference on Automatic Control and Artificial Intelligence (ACAI 2012). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2012.1377
• Shufeldt, Henry H. 1961. Precision Celestial Navigation Experiments. Defense Technical Information Center. https://doi.org/10.21236/ad0259559
• Shulman, A., H. J. Parry, and N. Shapiro. 1966. “Study of Wall-Pressure Fluctuations in a Supersonic-Engine Inlet Duet.” Journal of the Acoustical Society of America 39 (6_Supplement): 1254–1254. https://doi.org/10.1121/1.1942873
• Shultz, Melvin E. 1963. Circular Error Probability of a Quantity Affected by a Bias. Defense Technical Information Center. https://doi.org/10.21236/ad0644106
• Shumaker, Justin L., and Ainsmar X. Brown. 2009. An Evaluation and Development Environment for an ARM7-Based Autopilot Using the Atmel SAM7S256 Microcontroller. Defense Technical Information Center. https://doi.org/10.21236/ada508133
• Shuo, Wang, Huang Xijun, Cui Jiya, and Luo Changtian. 1995. “A Method for Predicting Inlet Temperature Distortion Caused by Missile Plumes.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/95-gt-117
• “Shuttle Eleven Cove Aerodynamic Heating by Ingested Flow.” 1978. In Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865336.0027.0048
• Siddiqi, Shahid, and J. Abraham. 1988. “Integrated Aircraft Flight Test Approaches for Fault-Tolerant Avionics Systems.” In 4th Flight Test Conference. AIAA 1988-2170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2170
• Siddiqui, Md Shahriar Rahim, Arman Rahmim, and Eldad Haber. 2024. “Deep Optimal Experimental Design for Parameter Estimation Problems.” Physica Scripta 100 (1): 016005. https://doi.org/10.1088/1402-4896/ad88b1
• Siebenhaar, Adam, and T. Bogar. 2006. “The Impact of Round Combustors on TBCC Propulsion and Hypersonic Cruise Vehicles.” In 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7986. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7986
• Siewert, R., and V. Stewart. 1965. “Use of Boundary-Layer Control on a Supersonic Attack-Reconnaissance Aircraft.” In Aircraft Design and Technology Meeting. AIAA 1965-751. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-751
• Sigal, Asher. 1999. “The Interactions between a Canard and Thick Bodies. II: Analysis of the Interactions.” In 17th Applied Aerodynamics Conference. AIAA 1999-3146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3146
• Sigal, Asher. 2000. “The Interactions between a Canard and Thick Bodies. III: Applications.” In 18th Applied Aerodynamics Conference. AIAA 2000-4524. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4524
• Sigal, Erez, and Joseph Ben-Asher. 2010. “Near-Optimal Missile Guidance with Pulse-Motor Control Logic.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8055. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8055
• Sigal, Asher, Michael Victor, Asher Sigal, and Michael Victor. 1997. “The Interaction between a Canard and Thick Bodies. I: Characteristics of the Components.” In 15th Applied Aerodynamics Conference. AIAA 1997-2249. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2249
• Silton, Sidra I., and Craig J. Coyle. 2015. “Effect of Canard Deflection on Fin Performance of a Fin-Stabilized Projectile.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2586. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2586
• Silva, Bruno. 2011. “Data Gathering and Preliminary Results of the System Identification of a Flexible Aircraft Model.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6355. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6355
• Silva, Felipe O., Guillermo E. V. Hernandez, and Cristino de Souza. 2025. “Airspeed-Aided Inertial Navigation with Pseudovanes and Non-Optical Sensors for GNSS-and Vision-Denied UAV Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2025.20274
• Silva, Walter A., Mark D. Sanetrik, and Pawel Chwalowski. 2015. “Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2721
• Silver, Marvin, and Melvyn Greenberg. 1971. “Area Navigation-A Quantitative Evaluation of the Effectiveness of Inertial System Aiding.” Navigation 18 (4): 360–68. https://doi.org/10.1002/j.2161-4296.1971.tb00108.x
• Silverstein, Calvin C. 1986. Heat Pipe Cooling for Scramjet Engines. NASA-CR-4036. NASA. https://ntrs.nasa.gov/citations/19890005980
• Simon, J. M. 1965. Designing for Space: An Inertial Guidance Sensor for Lunar Orbiter. NASA. https://ntrs.nasa.gov/citations/19660040239
• Simon, Raymond, and Frank Montenes. 1966. “Inertial Platform Testing on a Moving Base.” In Guidance and Control Conference. AIAA 1966-1852. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1852
• Simon, J. M., and R. H. Sproull. 1965. The Objectives and Design of the Inertial Reference Unit for the Lunar Orbiter. NASA-TM-X-56776. NASA. https://ntrs.nasa.gov/citations/19660017783
• Simpson, W. 1972. “The Development of Dynamic Flight Test Techniques for the Extraction of Aircraft Performance.” In 4th Aircraft Design, Flight Test, and Operations Meeting. AIAA 1972-785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-785
• Simpson, Matthew J., and Ruth E. Baker. 2026. “Parameter Identifiability, Parameter Estimation, and Model Prediction for Differential Equation Models.” SIAM Review 68 (1): 153–71. https://doi.org/10.1137/24m1667968
• Simsek, Bugra, Bayindir Kuran, Mehmet Ali Ak, and Sitki Uslu. 2016. “Aerodynamic Heating Prediction Tool for a Supersonic Vehicle for Conceptual Design Phase.” In 46th AIAA Thermophysics Conference. AIAA 2016-4428. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4428
• Sineglazov, V. M., and F. M. Zakharin. 2012. “Peculiarities of Future Air Navigation System Based on Inertial Navigation Systems/global Positioning System.” Electronics and Control Systems 4 (34). https://doi.org/10.18372/1990-5548.34.5722
• Singelmann, Dietrich, and Heinz Mueller. 1948. BMW Rocket Engine Development. Defense Technical Information Center. https://doi.org/10.21236/ada402594
• Singh, Netra. 2016. “Sub-Optimal Autopilot Design Based on Dynamic Neural Unit Network for Tactical Missile.” Indian Journal of Science and Technology 9 (S1). https://doi.org/10.17485/ijst/2016/v9is1/107903
• Singh, Gurjit. 2022. “Magnetic Navigation Systems.” In Magnetic Materials and Technologies for Medical Applications. Elsevier. https://doi.org/10.1016/b978-0-12-822532-5.00016-9
• Singh, B., and E. H. Benstein. 1986. Year 2000 Small Engine Technology Payoffs in Cruise Missiles. AIAA PAPER 86-1546. Teledyne CAE. https://ntrs.nasa.gov/citations/19860057967
• Singh, Leena, and Sungyung Lim. 2008. “On Lunar on-Orbit Vision-Based Navigation: Terrain Mapping, Feature Tracking Driven EKF.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6834
• Singh, Sunayna, Briek Luyten, and Marco Sagliano. 2024. “Relative Navigation for the ‘in-Air Capturing’ of a Winged Reusable Launch Vehicle.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4674857/v1
• Singh, Vandana, D. Pullaiah, J. Sreenivasa Rao, et al. 2004. “Generation and Validation of on-Board Star Catalog for RESOURCESAT-I Star Tracker.” In AIAA/AAS Astrodynamics Specialist Conference and Exhibit. AIAA 2004-5391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5391
• Singh, Abhijeet, and Maarten Uijt de Haag. 2007. “Use of X-Band Weather Radar to Support the Terrain Database Integrity Monitoring and Terrain Referenced Navigation Function.” In SPIE Proceedings, vol. 6559, edited by Jacques G. Verly, Jeff J. Guell. SPIE. https://doi.org/10.1117/12.725075
• Sinha, Vikas Kumar, and Avinash Kumar Maurya. 2017. “Calibration of Inertial Sensor by Using Particle Swarm Optimization and Human Opinion Dynamics Algorithm.” International Journal of Instrumentation and Control Systems 7 (1): 1–13. https://doi.org/10.5121/ijics.2017.7101
• Sinkiewicz, J. S., J. Feldman, and C. B. Lory. 1974. Evaluation of Selected Strapdown Inertial Instruments and Pulse Torque Loops, Volume 1. NASA-CR-120427. NASA. https://ntrs.nasa.gov/citations/19740023986
• Sirbaugh, J. 1983. “An Assessment of PANDORA Using a Canard/Wing/Body Configuration.” In Applied Aerodynamics Conference. AIAA 1983-1850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1850
• Sireesha, T., and K. Sreenivasa Ravi. 2015. “Comparative Assessment on Ramp and Bias Voltage Variations of Closed Loop Interferometric Fiber Optic Gyroscope.” Indian Journal of Science and Technology 8 (18). https://doi.org/10.17485/ijst/2015/v8i18/67723
• Sirlin, S., J. Alexander, T. Vanelli, S. Joshi, and J. Hench. 2000. “MURKY ACS Software to Determine 3 Axis Attitude without the Star Tracker.” In M6F2 Flight Software Readiness Review. https://ntrs.nasa.gov/citations/20060032878
• Sisk, Thomas, and William Andrews. 1963. “Utilization of Existing Aircraft in Support of Supersonic-Transport Research Programs.” In Testing of Manned Flight Systems Conference. AIAA 1963-1808. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-1808
• Sitomer, James, Anthony Kourepenis, and James Connelly. 1999. “Micromechanical Inertial Guidance Navigation and Control Systems in Gun Launched Projectiles.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4074
• Siu, Marie-Michele, Borja Martos, and John Foster. 2013. “Flight Test Results of an Angle of Attack and Angle of Sideslip Calibration Method Using Output-Error Optimization.” In AIAA Atmospheric Flight Mechanics (AFM) Conference. AIAA 2013-5086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5086
• Sivakumaran, N. S., Paul A. Bigelman, Laura T. Lee, and Robert J. Jesionowski. 1998. The Probability of Negation of a Cruise Missile,. Defense Technical Information Center. https://doi.org/10.21236/ada357518
• Sivalingam, Baheerathan, and Ove Kent Hagen. 2023. “Experimentation of Monocular Visual-Aided Inertial Navigation on Fixed-Wing Unmanned Aerial Vehicle.” In ENC 2023. MDPI. https://doi.org/10.3390/enc2023-15476
• Sivalingam, Baheerathan, and Ove Kent Hagen. 2026. “Experimentation of an Integrated Vision-Aided Inertial Navigation System with Orthophoto Matching on a Fixed-Wing UAV.” In European Navigation Conference 2025. MDPI. https://doi.org/10.3390/engproc2026126003
• Sivan, K., and S. Pandian. 2018. “An Overview of Reusable Launch Vehicle Technology Demonstrator.” Current Science 114 (01): 38. https://doi.org/10.18520/cs/v114/i01/38-47
• Sivrioglu, Selim. 2023. “Modelling and Simulation of Vertical Landing Dynamics of an Aircraft Based on a Model System.” In Sustainable Aviation. Springer International Publishing. https://doi.org/10.1007/978-3-031-29933-9_8
• Sjoeberg, Lars. 1977. The Accuracy of Gravimetric Deflections of the Vertical as Derived from the Gem 7 Potential Coefficients and Terrestrial Gravity Data. Defense Technical Information Center. https://doi.org/10.21236/ada053234
• Skaloud, J., A. M. Bruton, and K. P. Schwarz. 1999. “Detection and Filtering of Short-Term (1 /Fγ) Noise in Inertial Sensors.” Navigation 46 (2): 97–107. https://doi.org/10.1002/j.2161-4296.1999.tb02398.x
• Skarman, B. 1978. “Estimation of Parameters in the Time Variable Dynamics of a Missile from Flight Test Data.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1330
• Skibina, N. P., and V. V. Faraponov. 2021. “Analysis of the Interaction of a Supersonic Gas Flow with a Solid Low Melting Polymer as a Ramjet Engine Propellant.” Computational Continuum Mechanics 14 (3): 278–88. https://doi.org/10.7242/1999-6691/2021.14.3.23
• Skin-Friction-Work Recovery by Aerodynamic Heating of Skin Coolants. 1963. NASA. https://ntrs.nasa.gov/citations/19630017704
• Sklar, Andrew, and Zvi Rusak. 2020. “Busemann-Sears-Haack Hybrid Geometries Applied toward Supersonic Commercial Vehicles for Improved Wave Drag Performance.” In AIAA Scitech 2020 Forum. AIAA 2020-0752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0752
• Slapnicar, Bor. n.d. “Flight Computer Design for Supersonic Unmanned Aerial Vehicle.” PhD diss., University of Queensland Library. https://doi.org/10.14264/69b8f75
• Slater, J. M. 1956a. “Choice of Coordinate Systems in Inertial Navigation.” Navigation 5 (2): 58–62. https://doi.org/10.1002/j.2161-4296.1956.tb00272.x
• Slater, J. M. 1956b. Measurement and Integration of Acceleration in Inertial Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada284483
• Slater, John. 2001. “Verification Assessment of Flow Boundary Conditions for CFD Analysis of Supersonic Inlet Flows.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3882
• Slater, John W. 2015. “Enhanced Performance of Streamline-Traced External-Compression Supersonic Inlets.” In NASA Glenn Research Center. https://ntrs.nasa.gov/citations/20150021040
• Slater, John W. 2016. “SUPIN: A Computational Tool for Supersonic Inlet Design.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0530
• Slater, John W. 2019. “Refinement of Vortex Generators in a Streamline-Traced, External-Compression Supersonic Inlet.” In AIAA Scitech 2019 Forum. AIAA 2019-1447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1447
• Sleeman, William C., Jr. 1957. Investigation at High Subsonic Speeds of the Static Longitudinal and Lateral Stability Characteristics of Two Canard Airplane Configurations. NACA-RM-L57J08. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019253
• Slivinsky, Charles, and Sudhiporn Patumtawapibal. 1980. Inherent Error in Asynchronous Digital Flight Controls. Defense Technical Information Center. https://doi.org/10.21236/ada082622
• Slocumb, Travis H., and Earl H. Andrews Jr. 1961. The Effect on Thrust Minus Base Drag of Exchanging Base Area for Nozzle Expansion in Supersonic Nozzles at Transonic Mach Numbers. NASA-TN-D-754. NASA. https://ntrs.nasa.gov/citations/20040006301
• Slomyanskiy, G. A. 1962. Calculation of Factors, Affecting the Accuracy in Determining the Drift of Floating Integrating Gyroscopes. Defense Technical Information Center. https://doi.org/10.21236/ad0292222
• Smeltzer, D., and N. Sorensen. 1972. “Performance Estimates for a Supersonic Axisymmetric Inlet System.” In 10th Aerospace Sciences Meeting. AIAA 1972-45. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-45
• Smiley, Robert F., and Walter B. Horne. 1957. Vertical Force-Deflection Characteristics of a Pair of 56-Inch-Diameter Aircraft Tires from Static and Drop Tests with and without Prerotation. NACA-TN-3909. NASA. https://ntrs.nasa.gov/citations/19930084807
• Smirnov, M. A. 2019. “Methodology for Evaluating Effectiveness of Air Defense Missile System (ADMS) Information Resources When Detecting a Hypersonic Cruise Missile, with Account for the Dynamic Target Scattering Crossover.” Journal of «Almaz – Antey» Air and Space Defence Corporation, no. 1: 18–23. https://doi.org/10.38013/2542-0542-2019-1-18-23
• Smith, G. L. 1973. Ames-Aided Inertial Navigation Work: The First Two Years of Progress. NASA-TM-X-62199. NASA. https://ntrs.nasa.gov/citations/19730013887
• Smith, R. A. 1974. Space Shuttle Orbiter Vehicle Star Tracker Test Program Plan. NASA-CR-140349. NASA. https://ntrs.nasa.gov/citations/19750003953
• Smith, S. G. 1986. “Developments in Inertial Navigation.” Journal of Navigation 39 (3): 401–15. https://doi.org/10.1017/s0373463300000874
• Smith, Stephen C. 1997. “Trefftz-Plane Drag Minimization at Transonic Speeds.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/971478
• Smith, Austin. 2011. “An Integrated Navigation System Model for Coupled GNSS-Inertial Navigation Research.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2011-6330. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6330
• Smith, F., M. Campbell, T. Blucker, C. Manry, and I. Saulietis. 1982. “Shuttle Orbiter Stellar-Inertial Reference System.” In Guidance and Control Conference. AIAA 1982-1560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1560
• Smith, I. W., and T. A. Dorschner. 1978. “Biassing the Raytheon Four-Frequency Ring Laser Gyroscope.” In SPIE Proceedings, vol. 0157, edited by Shaoul Ezekiel, G. E. Knausenberger. SPIE. https://doi.org/10.1117/12.965462
• Smith, D. W., F. G. Edwards, J. D. Foster, and F. J. Drinkwater III. 1974. “Flight Test of an Automatic Approach and Landing Concept for a Simulated Space Shuttle Represented by the NASA Convair 990 Aircraft.” In AGARD Advan. in Control Systems. https://ntrs.nasa.gov/citations/19740023344
• Smith, Liam J., Lenard J. Halim, Graeme Kennedy, and Marilyn J. Smith. 2021. “A High-Fidelity Coupling Framework for Aerothermoelastic Analysis and Adjoint-Based Gradient Evaluation.” In AIAA Scitech 2021 Forum. AIAA 2021-0407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0407
• Smith, Edmund, S. Hebbar, and M. Platzer. 1993. “Aerodynamic Characteristics of a Canard-Controlled Missile at High Angles of Attack.” In 31st Aerospace Sciences Meeting. AIAA 1993-763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-763
• Smith, G. A., and G. Meyer. 1980. Application of the Concept of Dynamic Trim Control to Automatic Landing of Carrier Aircraft. NASA-TP-1512. NASA. https://ntrs.nasa.gov/citations/19800010849
• Smith, G., and G. Meyer. 1981. “Application of the Concept of Dynamic Trim Control and Nonlinear System Inverses to Automatic Control of a Vertical Attitude Takeoff and Landing Aircraft.” In Digital Avionics Systems Conference. AIAA 1981-2238. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2238
• Smith, G. A., and George Meyer. 1990. Aircraft Automatic Flight Control System with Model Inversion. Yale University. https://ntrs.nasa.gov/citations/19910065996
• Smith, O. E., J. R. Redus, J. A. Forney, and M. J. Dash. 1972a. Effects of Atmospheric Models on Space Shuttle Trajectories and Aerodynamic Heating. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19720045147
• Smith, Theodore, Joseph Schetz, and Trong Bui. 2002. “Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests.” In 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2002-3134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3134
• Smith, C., Jr., and D. Biezad. 1986. “Performance Characteristics of Transponder-Aided versus GPS-Aided Inertial Navigation Systems.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9817. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9817
• Snodgrass, R. C. 1975. Recursive Navigation Algorithm for Electronic Grid Integration. Defense Technical Information Center. https://doi.org/10.21236/ada004477
• Sobieczky, H. 1991. “Generic Supersonic and Hypersonic Configurations.” In 9th Applied Aerodynamics Conference. AIAA 1991-3301. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3301
• Sokolov, S. V., and E. G. Chub. 2024. “Solving the Problem of Autonomous Navigation via the Integration of Inertial and Optical Navigation Systems.” Optoelectronics, Instrumentation and Data Processing 60 (6): 810–19. https://doi.org/10.3103/s8756699024700900
• Soler, Tomás, Jen-Yu Han, and Neil D. Weston. 2014. “On Deflection of the Vertical Components and Their Transformations.” Journal of Surveying Engineering 140 (2): 04014005. https://doi.org/10.1061/(asce)su.1943-5428.0000126
• Solmaz, Mehmet Burak, and Sıtkı Uslu. 2025. “Comparison of Reacting DDES and LES CFD Simulation Methodologies for a Dual Inlet Ramjet Engine Combustor.” Isı Bilimi ve Tekniği Dergisi 45 (1): 10–21. https://doi.org/10.47480/isibted.1490666
• Solov, E. G., and J. R. Thibodeau III. 1973. “Failure Detection and Isolation Methods for Redundant Gimballed Inertial Measurement Units.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730053988
• Soloviev, Andrey, Dustin Bates, and Frank Van Graas. 2007. “Tight Coupling of Laser Scanner and Inertial Measurements for a Fully Autonomous Relative Navigation Solution.” Navigation 54 (3): 189–205. https://doi.org/10.1002/j.2161-4296.2007.tb00404.x
• Soltani, Mohammad Reza, and Rasoul Askari. 2018. “Experimental Study on the Performance of a Body-Integrated Y-Shaped Supersonic Inlet.” In 2018 Joint Propulsion Conference. AIAA 2018-4456. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4456
• Soltani, M. R., M. Farahani, and M. H. Asgari Kaji. 2011. “An Experimental Study of Buzz Instability in an Axisymmetric Supersonic Inlet.” Scientia Iranica 18 (2): 241–49. https://doi.org/10.1016/j.scient.2011.03.019
• “Some Current Types of Landing Gear: A Survey of the Solutions Adopted in Landing Gear Design for a Range of Modern Aircraft.” 1968. Aircraft Engineering and Aerospace Technology 40 (1): 26–31. https://doi.org/10.1108/eb034335
• Somov, Yevgeny, Sergey Butyrin, and Viktor Fedosov. 2012. “Calibration and Alignment of Strapped-down Astro-Inertial System for Attitude Determination of Large-Scale Information Spacecraft.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.4765601
• Son, Jae-Hoon, Sang-Heon Oh, and Dong-Hwan Hwang. 2023. “Performance Improvement of Global Positioning System/Gyro-Free Inertial Navigation System Integrated Navigation Systems Using Gyroscopes.” Journal of Institute of Control Robotics and Systems 29 (6): 510–20. https://doi.org/10.5302/j.icros.2023.23.0010
• Song, Yongkyu, and Marcello Napolitano. 2002. “A Comparative Study of Real-Time Aircraft Parameter Identification Schemes Applied to NASA F/A-18 HARV Flight Data.” Transactions of the Japan Society for Aeronautical and Space Sciences 45 (149): 180–88. https://doi.org/10.2322/tjsass.45.180
• Song, Youshan, Shiqin Zhou, and Zheng Lu. 2001. “Fiber Optic Gyroscope for Strap-down Inertial Navigation Systems.” In SPIE Proceedings, vol. 4540, edited by Hiroyuki Fujisada, Joan B. Lurie, Konradin Weber. SPIE. https://doi.org/10.1117/12.450685
• Sontag, Eduardo. 2016. “Dynamic Compensation, Parameter Identifiability, and Equivariances.” Preprint, bioRxiv. https://doi.org/10.1101/095828
• Sontag, Eduardo D. 2017. “Dynamic Compensation, Parameter Identifiability, and Equivariances.” PLOS Computational Biology 13 (4): e1005447. https://doi.org/10.1371/journal.pcbi.1005447
• Sorensen, N., and D. Bencze. 1973. “Possibilities for Improved Supersonic Inlet Performance.” In 9th Propulsion Conference. AIAA 1973-1271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1271
• Sorensen, J., and J. Karmarkar. 1977. “Information Processing Requirements for on-Board Monitoring of Automatic Landing.” In Guidance and Control Conference. AIAA 1977-1093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1093
• Sorgenfrei, Matt, Matt Nehrenz, and Dayne Kemp. 2016. “Selection of an Inertial Measurement Unit for High Accuracy CubeSat Attitude Determination.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0961
• Sorgi, Lorenzo. 2009. “Estimation of Inertial Sensor to Camera Rotation from Single Axis Motion.” In International Conference on Computer Vision Theory and Applications. https://doi.org/10.5220/0001754500130019
• Soto, Hector, and Corey Hernandez. 2004. “Comparison of Engine/inlet Distortion Measurements with MEMS and ESP Pressure Sensors.” In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2004-2398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-2398
• Soumekh, M. n.d. “Automatic Aircraft Landing Using Interferometric Inverse Synthetic Aperture Radar Imaging.” In Proceedings., International Conference on Image Processing, vol. 1. IEEE Comput. Soc. Press. https://doi.org/10.1109/icip.1995.529056
• Sousa, Jorge, and Guillermo Paniagua. 2015. “One-Dimensional Assessment of Supersonic Inlet Turbines.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3930
• “Spaceborne Gravity Gradiometers. Part 1: Summary and Recommendations.” 1984a. In Spaceborne Gravity Gradiometers. https://ntrs.nasa.gov/citations/19840010649
• “Spaceborne Gravity Gradiometers. Part 2: Role of Gravity Gradiometers in NASA’s Programs.” 1984b. In Spaceborne Gravity Gradiometers. https://ntrs.nasa.gov/citations/19840010650
• “Spaceborne Gravity Gradiometers. Part 3: Instrument Status and Prospects.” 1984c. In Spaceborne Gravity Gradiometers. https://ntrs.nasa.gov/citations/19840010651
• “Spaceborne Gravity Gradiometers. Part 5: Development Plan.” 1984d. In Spaceborne Gravity Gradiometers. https://ntrs.nasa.gov/citations/19840010653
• Spalding, Kevin. 1989. “Advanced GPS-Inertial Integration Concepts.” In Guidance, Navigation and Control Conference. AIAA 1989-3501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3501
• Spammer, Stephanus J., and Pieter L. Swart. 1992. “Open-Loop Fiber Optic Gyroscope with Wide Dynamic Range and Source Variation Insensitivity.” In SPIE Proceedings, vol. 1585, edited by Shaoul Ezekiel, Eric Udd. SPIE. https://doi.org/10.1117/12.135050
• Spearman, M. Leroy. 1961. Aerodynamic Characteristics in Pitch of a Series of Cruciform-Wing Missiles with Canard Controls at a Mach Number of 2.01. NASA-TN-D-839. NASA. https://ntrs.nasa.gov/citations/20040047104
• Spearman, M. 1979a. “Historical Development of Worldwide Supersonic Aircraft.” In Aircraft Systems and Technology Meeting. AIAA 1979-1815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1815
• Spearman, M. L. 1979b. “Wind-Tunnel Studies of the Effects of Simulated Damage on the Aerodynamic Characteristics of Airplanes and Missiles.” In American Defense Preparedness Association, Vulnerability and Survivability Symposium, 4th, Tyndall AFB. https://ntrs.nasa.gov/citations/19790043411
• Spearman, M. L. 1983. An Aerodynamic Assessment of Various Supersonic Fighter Airplanes Based on Soviet Design Concepts. NASA-TM-84647. NASA. https://ntrs.nasa.gov/citations/19830013886
• Spearman, M. L. 1986. Some Effects of Interference Flow Fields on Supersonic Configurations. AIAA PAPER 86-2078. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19860062929
• Spearman, M. Leroy. 1989. “Historical Review of Missile Aerodynamic Developments.” In Nielsen Engineering and Research, Inc., Missile Aerodynamics: NEAR Conference on Missile Aerodynamics. https://ntrs.nasa.gov/citations/19900008226
• Spearman, M. L., and I. K. Collins. 1972. Aerodynamic Characteristic of a Swept-Wing Cruise Missile at Mach Numbers from 0.50 to 2.86. NASA-TN-D-7069. NASA. https://ntrs.nasa.gov/citations/19730001275
• Spearman, M. Leroy, and Cornelius Driver. 1959. Effects of Forebody Deflection on the Stability and Control Characteristics of a Canard Airplane Configuration with a High Trapezoidal Wing at a Mach Number of 2.01. NASA-MEMO-4-4-59L. NASA. https://ntrs.nasa.gov/citations/19980228222
• Spearman, Leroy M., Cornelius Driver, and Ross B. Robinson. 1955. Aerodynamic Characteristics of Various Configurations of a Model of a 45 Degree Swept-Wing Airplane at a Mach Number of 2.01. NACA-RM-L54J08. NASA. https://ntrs.nasa.gov/citations/19930090584
• Spearman, M. L., R. H. Fournier, and M. Lamb. 1977. Aerodynamic Characteristics of Supersonic Fighter Airplane Configurations Based on Soviet Design Concepts. AIAA PAPER 77-1162. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19770060336
• Spearman, M. Leroy, and Ross B. Robinson. 1958. Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-Wing Airplane Configuration with Canard Control Surfaces. NACA-RM-L58E20. NASA. https://ntrs.nasa.gov/citations/19930090148
• Spencer, Robert B. 1999. “The Reusable First Stage (RFS) Vehicle-an Enabler for Future Launch Systems.” In AIP Conference Proceedings. AIP. https://doi.org/10.1063/1.57511
• Spencer, Bernard, Jr. 1961. Effects of Canard Planform and Wing-Leading-Edge Modification on Low-Speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration. NASA-TN-D-958. NASA. https://ntrs.nasa.gov/citations/19980228059
• Sperry Gyroscope Co Great Neck Ny. 1963a. Development Program for an Inertial Sensor Technique. Defense Technical Information Center. https://doi.org/10.21236/ad0413922
• Sperry Gyroscope Co Great Neck Ny. 1963b. Dormant Missile Inertial Guidance and Control System. Phase I Study Program. Defense Technical Information Center. https://doi.org/10.21236/ad0430863
• Sperry Phoenix Co Az. 1962. Operational Analysis Report of the Microwave Command Guidance System. Defense Technical Information Center. https://doi.org/10.21236/ad0405722
• “Sperry’s SGN-10 Inertial System: Details of the Sperry Gyroscope Company’s SGN-10 Aircraft Inertial Navigation System Which Has Been Ordered in Quantity by Pan American World Airways.” 1964. Aircraft Engineering and Aerospace Technology 36 (11): 354–55. https://doi.org/10.1108/eb033944
• Spetzler, Max, and Anshu Narang-Siddarth. 2016. “Local Linear Controllability and Observability Analysis of Nonlinear Systems with Continuation Methods.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-0080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0080
• Speyer, Jason L. 1997. A Disturbance Attenuation Approach to Missile Guidance and Control. Defense Technical Information Center. https://doi.org/10.21236/ada329598
• Spieck, Martin. 2004. “Simulation of Aircraft Landing Impact under Consideration of Aerodynamic Forces on the Flexible Structure.” In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2004-4333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4333
• Spiridakos, Dimitrios P., Nicholas C. Markatos, and D. P. Karadimou. 2020. “Mathematical Modeling of Aerodynamic Heating and Pressure Distribution on a 5-Inch Hemispherical Concave Nose in Supersonic Flow.” In IntechOpen eBooks. IntechOpen. https://doi.org/10.5772/intechopen.91041
• Spreiter, John R. 1954. On the Range of Applicability of the Transonic Area Rule. NACA-RM-A54F28. NASA. https://ntrs.nasa.gov/citations/19930088332
• Spreiter, John R. 1956. On the Range of Applicability of the Transonic Area Rule. NACA-TN-3673. NASA. https://ntrs.nasa.gov/citations/19930084964
• Springer, Anthony. 1996. “Aerodynamic Characteristics of a Single-Stage-to-Orbit Wing Body Reusable Launch Vehicle Concept.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-196. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-196
• Squire, L. C. 1965. “The Use of Excess Engine Exit Area over Intake Area to Reduce Zero-Lift Drag at High Supersonic Speeds.” Aeronautical Quarterly 16 (3): 260–74. https://doi.org/10.1017/s0001925900003474
• Squire, L. C., and S. H. Nasser. 1993. “Cavity Drag at Transonic Speeds.” Aeronautical Journal 97 (967): 247–56. https://doi.org/10.1017/s000192400002635x
• Sreena, P. V., and Tessy Thomas. 2017. “Orbit Injection Error Mitigation by Time-Differenced GPS Carrier Phase Observables-Aided Inertial Navigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1517. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1517
• Sridharan, Srikanth, and Armando Rodriguez. 2013. “Impact of Control Specifications on Vehicle Design for Scramjet-Powered Hypersonic Vehicles.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5166. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5166
• Srivastava, B. 1998. “Computation and Validation of Asymmetric Force and Moment Coefficients for Lateral Jet Controlled Supersonic Missile.” In 16th AIAA Applied Aerodynamics Conference. AIAA 1998-2410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-2410
• Srivastava, B., and B. Srivastava. 1997. “Lateral Jet Control of a Supersonic Missile: Computational Studies with Forward, Rear Missile Body and Wing Tip Mounted Divert Jets.” In 15th Applied Aerodynamics Conference. AIAA 1997-2247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2247
• Sruthi, Beereddy, and P. Nagaraja. 2015. “Comparative Assessment of Ramp and Biasing Signal Amplitude Variations of Digital Closed-Loop Fiber Optic Gyroscope.” International Journal of Scientific Engineering and Research 3 (4): 18–20. https://doi.org/10.70729/ijser1561
• Staas Jr. and Philip C. 1963. Mechanization Equations for a Schuler-Tuned Inertial Navigation System Vertically Aligned to the Mass-Attraction Gravity Vector. Defense Technical Information Center. https://doi.org/10.21236/ad0406113
• Stachiw, Terrin. n.d. “Synthesis and Optimization of Mechanical Networks with Inerters in Landing Gear for Improved Landing Performance and Vibration Control at Touchdown Considering Airframe Flexibility.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2020-14047
• Stadler, Reinhold. 1998. “Results for a Fully Reusable TSTO-Launch Vehicle Concept.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1504. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1504
• Stafeev, D. V., and V. V. Tikhomirov. 2016. “Random Drift Estimation for Laser Gyroscopes Using Filters Based on the Error Equations of Inertial Navigation Systems.” Moscow University Mechanics Bulletin 71 (5): 103–7. https://doi.org/10.3103/s0027133016050010
• Stainback, P. C., and L. M. Weinstein. 1967. Aerodynamic Heating in the Vicinity of Corners at Hypersonic Speeds. NASA-TN-D-4130. NASA. https://ntrs.nasa.gov/citations/19670031239
• Stallard, D. 1979. “Optimal Missile Guidance for Low Miss and Perpendicular Impact.” In Guidance and Control Conference. AIAA 1979-1734. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1734
• Stallings, D. W., and A. S. Hartman. 1981. Wind Tunnel Testing of a Windshield Material for Supersonic Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ada103383
• Stallings, R., Jr. 1982. “Store Separation from Cavities at Supersonic Flight Speeds.” In 20th Aerospace Sciences Meeting. AIAA 1982-372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-372
• Stanhope, S., J. E. Rubin, and D. Swigon. 2014. “Identifiability of Linear and Linear-in-Parameters Dynamical Systems from a Single Trajectory.” SIAM Journal on Applied Dynamical Systems 13 (4): 1792–1815. https://doi.org/10.1137/130937913
• Staniszewski, Edgar. 1999. “Semi-Reusable Launch Vehicle: A Next Step for Europe?” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4826
• Stanley, Thomas Troy, Reginald Alexander, and Brian Landrum. 2000. A Collaborative Analysis Tool for Integrated Hypersonic Aerodynamics, Thermal Protection Systems, and RBCC Engine Performance for Single Stage to Orbit Vehicles. International Space Systems, Inc. https://ntrs.nasa.gov/citations/20000021504
• Stanton, R. H., J. W. Alexander, E. W. Dennison, T. A. Glavich, and P. M. Salomon. 1984. ASTROS: A Sub-Arcsec CCD Star Tracker. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/19860030592
• “Star Catalogues and Photographic Charts.” 2010. In Photographs of Stars, Star-Clusters and Nebulae. Cambridge University Press. https://doi.org/10.1017/cbo9780511659119.008
• “Star-Camera Algorithms.” 2023. In ADCS - Spacecraft Attitude Determination and Control. Elsevier. https://doi.org/10.1016/b978-0-32-399915-1.00050-4
• Starkey, Ryan, and Mark Lewis. 1999. “Aerodynamics of a Box Constrained Waverider Missile Using Multiple Scramjets.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2378
• Starkey, Ryan, Falcon Rankins, and Darryll Pines. 2006. “Effects of Hypersonic Cruise Trajectory Optimization Coupled with Airbreathing Vehicle Design.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-337
• Starks, G. T. 1974. Mariner Mars 1971 Inertial Reference Unit. NASA-CR-137356. NASA. https://ntrs.nasa.gov/citations/19740012117
• Starr, R., and M. Varner. 1976. “Experimental and Theoretical Observations on the Drag of Bodies of Revolution at Transonic Speeds.” In 14th Aerospace Sciences Meeting. AIAA 1976-90. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-90
• “Startup Tests Ramjet Engine.” 2023. Aerospace Testing International 2023 (3): 6–6. https://doi.org/10.12968/s1478-2774(23)50352-5
• Statsinger, J. 1959. “Theory and Instrumentation of Inertial Navigation Systems.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/590055
• Statz, Hermann, Terry A. Dorschner, Michael Holtz, and Irl W. Smith. 1985. “The Multioscillator Ring Laser Gyroscope.” In Laser Handbook. Elsevier. https://doi.org/10.1016/b978-0-444-86927-2.50007-3
• Stauffer, W. 1964. “Remarks on Structural Design Criteria for the Supersonic Transport.” In Transport Aircraft Design and Operations Meeting. AIAA 1964-627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-627
• Stebbins, R., P. Bender, and W. Folkner. 1998. Possible Use of a Narrow-Field Star Tracker on the New Millennium SSI Mission. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210003177
• Stechkin, B. 1967. “Ramjet Engines for Spacecraft.” In History of Aviation and Cosmonautics, Volume III. https://ntrs.nasa.gov/citations/19680004098
• Steenken, William. 2009. “Integrated Inlet-Engine Compatibility by Design.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5460. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5460
• Steer, A. 2000. “Integrated Control of a Second Generation Supersonic Commercial Transport Aircraft Using Thrust Vectoring.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4109
• Steer, Tony. 2003. “Handling Quality Design Criteria for Advanced Supersonic Aircraft Flight Control.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5308
• Steinberg, Marc. 1992. “A Fuzzy Logic Based F/A-18 Automatic Carrier Landing System.” In Guidance, Navigation and Control Conference. AIAA 1992-4392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4392
• Steinberg, Marc, and Anthony Page. 2001. A Comparison of Neural, Fuzzy, Evolutionary, and Adaptive Approaches for Carrier Landing. Defense Technical Information Center. https://doi.org/10.21236/ada390355
• Steinleitner, Andreas, Vincenz Frenzel, Ole Pfeifle, Jan Denzel, and Walter Fichter. 2022. “Automatic Take-Off and Landing of Tailwheel Aircraft with Incremental Nonlinear Dynamic Inversion.” In AIAA SCITECH 2022 Forum. AIAA 2022-1228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1228
• Steinmetz, Ronald, and Bob Hines. 1987. “Engine Variable Geometry Effects on Commercial Supersonic Transport Development.” In 23rd Joint Propulsion Conference. AIAA 1987-2101. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2101
• Stenberg, T. R. 1964. “The “Log” of Celestial Navigation.” Navigation 11 (1): 26–31. https://doi.org/10.1002/j.2161-4296.1964.tb02072.x
• Stengel, R. 1969. “Altitude Stability in Supersonic Cruising Flight.” In AIAA Aircraft Design and Operations Meeting. AIAA 1969-813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-813
• Stengel, R., J. Broussard, and P. Berry. 1977. “Command Augmentation Control Laws for Maneuvering Aircraft.” In Guidance and Control Conference. AIAA 1977-1044. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1044
• Stephens, Emily W. 1959. Free-Flight Investigation of a Rocket-Propelled Model to Determine the Aerodynamic Heating on a Thin, Unswept, Untapered, Multispar, Aluminum-Alloy Wing at Mach Numbers up to 2.22. NASA-MEMO-12-15-58L. NASA. https://ntrs.nasa.gov/citations/19980232232
• Stephens, Michael, and D. Ridgely. 1995. “Autopilot Design for a Tail-Controlled Missile Using Two-Degree-of-Freedom Controllers.” In Guidance, Navigation, and Control Conference. AIAA 1995-3264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3264
• Stephens, David, and Alexander A. Svetgoff. 2024. “Flow and Acoustics Simulations of a Supersonic Engine Inlet.” In 30th AIAA/CEAS Aeroacoustics Conference (2024). AIAA 2024-3390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3390
• Steppert, Michael, and Philipp Epple. 2017. “Numerical Investigation of the Drag of Rockets at Subsonic, Transonic and Supersonic Speeds.” In Volume 7: Fluids Engineering. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2017-71872
• Stevens, Joseph E. 1955. Qualitative Results from a Flight Investigation to Determine Aileron Effectiveness of Two Rocket-Propelled 1/20-Scale Models of the MX -76 Missile. Rept-5215. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050030038
• Stevens, Frederick. 1958. “Aiding the Inertial Navigation System.” Navigation 6 (3): 166–74. https://doi.org/10.1002/j.2161-4296.1958.tb02438.x
• Stevenson, Scott. 1991. “Parameter Identification Modeling for Simulation Aerodynamic Model Updates.” In 18th Atmospheric Flight Mechanics Conference. AIAA 1991-2878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2878
• Stewart, Robert J. 1958. “Elevated Temperature Strain-Gage Investigations at Grumman Aircraft Engineering Corporation.” In Symposium on Elevated Temperature Strain Gages. ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. https://doi.org/10.1520/stp45044s
• Stewart, V. R. 1986. Pretest Report for the Full Span Propulsive Wing/Canard Model Test in the NASA Langley 4 x 7 Meter Low Speed Wind Tunnel Second Series Test. NA-86-0015. Rockwell International Corp. https://ntrs.nasa.gov/citations/19990039611
• Stewart, V. R., and G. T. Kemmerly. 1987. “Effects of Ground Proximity on a Low Aspect Ratio Propulsive Wing/canard Configuration.” In NASA. Ames Research Center Proceedings of the 1985 NASA Ames Research Center’s Ground-Effects Workshop. https://ntrs.nasa.gov/citations/19870014989
• Stieglitz, M., J. Elston, and J. Bloodworth. 1979. “Minimizing Air Launched Cruise Missile Software Life Cycle Cost.” In 2nd Computers in Aerospace Conference. AIAA 1979-1907. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1907
• Stieler, B. 1971. Inertial Navigation System Using Three TDF Gyroscopic Sensors Not Jointly Mounted on a Stable Platform. NASA-CR-126358. NASA. https://ntrs.nasa.gov/citations/19720015004
• Stilley, G. 1988. “An Approach to Extraction of Initial Conditions from Projectile Free-Flight Test Data.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4350. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4350
• Stocker, Jeremy. 2004. “Ballistic Missile Early Warning.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780203309636-16
• Stocker, Jeremy. 2010. “Ballistic Missile Early Warning.” In Taylor & Francis eBooks. Taylor & Francis. https://doi.org/10.4324/9780203309636_chapter_5
• Stokes, Timothy M., and Ragini Acharya. 2023. “Identification of Scramjet Inlet Unstart Characteristics by Dynamic Mode Decomposition.” In 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2023-3075. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3075
• Stoldt, Henry, Craig T. Johansen, Artem Korobenko, and Paul Ziade. 2020. “Verification and Validation of a High-Fidelity Open-Source Simulation Tool for Supersonic Aircraft Aerodynamic Analysis.” In AIAA Aviation 2020 Forum. AIAA 2020-2758. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2758
• Stoldt, Henry H., Artem Korobenko, Paul Ziade, and Craig T. Johansen. 2021. “Verification and Validation of High-Fidelity Open-Source Simulation Tools for Supersonic Aircraft Aerodynamic Analysis.” Journal of Verification, Validation and Uncertainty Quantification 6 (4): 041005. https://doi.org/10.1115/1.4052150
• Stoltz, P. G., and J. H. Priedigkeit. 1975. Analysis of Army Operational Requirements for the Tactical Microwave Landing System. Defense Technical Information Center. https://doi.org/10.21236/adb010929
• Stone, H. W. 1969. The Leading-Edge Effects on the Laminar Flat- Plate Boundary Layer and the Aerodynamic Heating at Mach 10.4. NASA-TN-D-5160. NASA. https://ntrs.nasa.gov/citations/19690014093
• Stoner, E. 1972. “Spiral Descent Terminal Guidance.” In Guidance and Control Conference. AIAA 1972-834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-834
• Storer, N. Wyman. 1947. “Note on Dreisonstok’s Method in Celestial Navigation.” Navigation 1 (5): 98–100. https://doi.org/10.1002/j.2161-4296.1947.tb01109.x
• Stoven-Dubois, Alexis, Laurent Jospin, and Davide A. Cucci. 2018. “Cooperative Navigation for an UAV Tandem in GNSS Denied Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2018.15949
• Stowell, Elbridge Z., John C. Houbolt, and S. B. Batdord. 1948. An Evaluation of Some Approximate Methods of Computing Landing Stresses in Aircraft. NACA-TN-1584. NASA. https://ntrs.nasa.gov/citations/19930082235
• Stower, Geovian. 2024. A Preliminary Study on the Technical Feasibility of Launch Site Operations Utilizing a Two-Stage Reusable Launch Vehicle for Orbital Missions from the East Coast of Kenya. https://doi.org/10.52202/078377-0011
• Straight, D. M., and D. E. Harrington. 1973. Experimental Cold-Flow Evaluation of a Ram Air Cooled Plug Nozzle Concept for Afterburning Turbojet Engines. NASA-TM-X-2811. NASA. https://ntrs.nasa.gov/citations/19730017096
• Strandjord, Lee K., and Glen A. Sanders. 1993. “Performance Improvements of a Polarization-Rotating Resonator Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 1795, edited by Eric Udd, Ramon P. DePaula. SPIE. https://doi.org/10.1117/12.141234
• “Strap-Down Inertial Sensor Laboratory Calibration.” 2007. In Applied Mathematics in Integrated Navigation Systems, Third Edition. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861598.0171.0188
• Strapdown Inertial Navigation Mechanism. 2021. Wiley. https://doi.org/10.1002/9781119699910.ch3
• “Strapdown Navigation System Computation.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch11
• “Strapdown System Technology.” 2004. In Strapdown Inertial Navigation Technology. Institution of Engineering and Technology. https://doi.org/10.1049/pbra017e_ch9
• Strass, H. Kurt, and Emily W. Stephens. 1957. Aerodynamic Heating of a Thin, Unswept, Untapered, Multiweb, Aluminum-Alloy Wing at Mach Numbers up to 2.67 as Determined from a Free-Flight Investigation of a Rocket-Propelled Model. NACA-RM-L57F06. NASA. https://ntrs.nasa.gov/citations/19930089753
• “Strategic Missiles.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_6
• Stratton, A. 1963. “I—the Inertial Reference Platform in Civil Aviation.” Journal of Navigation 16 (3): 266–84. https://doi.org/10.1017/s0373463300020488
• Stratton, A. 1968. “The Schuler Pendulum and Inertial Navigation.” Journal of Navigation 21 (4): 507–10. https://doi.org/10.1017/s0373463300032409
• Strauss, Friedolin T., Nico Fischer, Samuel Michelfelder, Luca Bauer, and Christoph Kirchberger. 2026. “Ramjet Injection and Combustion Experiments on Sustainable Supersonic Flight.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5146
• Strauss, Friedolin T., Konstantin Manassis, Luca Bauer, and Christoph U. Kirchberger. 2025. “Ramjet Experiments on Sustainable Supersonic Flight.” In AIAA SCITECH 2025 Forum. AIAA 2025-1142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1142
• Stray, Ben, Xavier Bosch-Lluis, Robert Thompson, et al. 2025. Quantum Gravity Gradiometry for Future Mass Change Science. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20250011704
• Streiff, M. L. 1953. Ramjet Technology. Chapter 13. Exit-Nozzle Design. Defense Technical Information Center. https://doi.org/10.21236/ad0041742
• Stricker, Jeffrey. 1989. “Comparison Methodology for a Long Range Subsonic Cruise Missile Propulsion System.” In 25th Joint Propulsion Conference. AIAA 1989-2475. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2475
• Strohm, Luke S. 2011. A Terminal Guidance Model for Smart Projectiles Employing a Semi-Active Laser Seeker. Defense Technical Information Center. https://doi.org/10.21236/ada553607
• Stuart, Robin G. 2009. “Applications of Complex Analysis to Celestial Navigation.” Navigation 56 (4): 221–27. https://doi.org/10.1002/j.2161-4296.2009.tb01757.x
• Stuart, James, Thomasw. White, and Randall Coffey. 1987. “Space System Design and Tradeoffs of Ring-Laser Gyroscope Guidance and Control.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-400. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-400
• Stubbs, William. 1956. “Supersonic Air Inlet Controls.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/560075
• Stuchlik, Dave, and Scott Heatwole. 2016. “Celestial Attitude Reference and Determination System (CARDS) Daytime Star Tracker.” In The Scientific Ballooning Technologies Workshop. https://ntrs.nasa.gov/citations/20180007599
• Study of a Scanning Celestial Attitude Determination System (SCADS) for a Synchronous Satellite Final Report. 1968. NASA-CR-100149. NASA. https://ntrs.nasa.gov/citations/19690009988
• A Study of the Critical Computational Problems Associated with Strapdown Inertial Navigation Systems. 1968. NASA-CR-968. NASA. https://ntrs.nasa.gov/citations/19680012183
• Su, Chu Trong. 2024. “A New Coning, Sculling, and Scrolling Error Compensation Approach for Strapdown Inertial Navigation System.” International Review of Aerospace Engineering (IREASE) 17 (4): 132. https://doi.org/10.15866/irease.v17i4.25685
• Su, Yi Xiao. 2025. The Applications and Development Trend of Interferometric Fiber Optic Gyroscope in Space. https://doi.org/10.52202/083082-0128
• Su, Ya, Ying Dai, and Yi Liu. 2021. “A Hybrid Parallel Harris Hawks Optimization Algorithm for Reusable Launch Vehicle Reentry Trajectory Optimization with No-Fly Zones.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-554106/v1
• Su, Pei Ran, Qitai Eri, and Xi Xi Li. 2013b. “Numerical Simulation of Supersonic Aircraft Surface Aerodynamic Heating and Infrared Radiation Characteristics.” Applied Mechanics and Materials 0: 1234–38. https://doi.org/10.4028/www.scientific.net/amm.0.1234
• Su, Zili, Jisong Zhao, and Jiaolong Liu. 2024. “Reentry Trajectory Optimization of Hypersonic Glide Vehicle Based on Improved Particle Swarm Algorithm.” Journal of Physics: Conference Series 2764 (1): 012069. https://doi.org/10.1088/1742-6596/2764/1/012069
• Subedi, S., B. Hosseini, J. Diepolder, and F. Holzapfel. 2023. “Online Parameter Identification and Optimal Input Design Using Perturbed Nonlinear Programming.” Journal of Physics: Conference Series 2514 (1): 012020. https://doi.org/10.1088/1742-6596/2514/1/012020
• Subrahmanyam, M. Bala. 1995. “H ∞ Design of the F/A-18A Automatic Carrier Landing System.” In Finite Horizon H∞ and Related Control Problems. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-4272-7_6
• Suchocki, Tomasz, Piotr Lampart, and Piotr Klonowicz. 2015. “Numerical Investigation of a GTM-140 Turbojet Engine.” Open Engineering 5 (1). https://doi.org/10.1515/eng-2015-0053
• Suchov, Vitalii, Bogdan Kazmerchukh, and Petro Yukovenko. 2022. “Evaluation of the Aerodynamic Heating of the Aircraft Skin with Taking into Account Ablation.” Mechanics of Gyroscopic Systems, no. 44: 145–50. https://doi.org/10.20535/0203-3771442022284205
• Süelözgen, Özge. 2022. “A Novel Updating Algorithm for Linearized State-Space Models of an Unmanned Flexible Aircraft Using Flight Test Data.” In AIAA SCITECH 2022 Forum. AIAA 2022-0725. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0725
• Suetin, A. G., and B. V. Kartsev. 1993. “Fundamentals of Appearance Formation and Design Solutions for Supersonic Ramjet.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2483. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2483
• Suga, Yuki, and Wataru Yamazaki. 2015. “Aerodynamic Uncertainty Quantification of Supersonic Biplane Airfoil via Polynomial Chaos Approach.” In 17th AIAA Non-Deterministic Approaches Conference. AIAA 2015-1815. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1815
• Sukenik, Charles L. 2004. Application of Ultracold Molecules to Inertial Sensing for Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada421641
• Sukkarieh, Salah, Peter Gibbens, Ben Grocholsky, Keith Willis, and Hugh F. Durrant-Whyte. 2000. “A Low-Cost, Redundant Inertial Measurement Unit for Unmanned Air Vehicles.” International Journal of Robotics Research 19 (11): 1089–1103. https://doi.org/10.1177/02783640022067995
• Sullings, F., and P. Waller. 1967. “Automatic Landing Systems for All-Weather Operation by Civil Transport Aircraft.” In 10th Anglo-American Aeronautical Conference. AIAA 1967-757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-757
• Sullivan, Wendy I. 1994. “Performance Analysis of an Integrated GPS/inertial Attitude Determination System.” PhD diss., Draper (Charles Stark) Lab., Inc.. https://ntrs.nasa.gov/citations/19940028358
• Sumi, Takenori, Yasuhiro Yoshimura, and Toshiya Hanada. 2025. Observability Analysis of Satellites Perturbed by Solar Radiation Pressure in Angles-Only Navigation. https://doi.org/10.52202/083087-0027
• ŞUmnu, Ahmet, and İbrahim GÜZelbey. 2023. “The Effects of Different Wing Configurations on Missile Aerodynamics.” Journal of Thermal Engineering 9 (5): 1260–71. https://doi.org/10.18186/thermal.1377200
• Sun, Hongsheng. n.d. “Closed-Loop Endo-Atmospheric Ascent Guidance for Reusable Launch Vehicle.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-14281
• Sun, David F. 1979. Experimental Measurements of Ground Reflection Elevation Multipath Characteristics and Its Effects on a Small Aperture Elevation Tracking Radar. Defense Technical Information Center. https://doi.org/10.21236/ada077915
• Sun, Long. 2023. “An Attitude Determination Scheme for the Nano Star Tracker.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_93
• Sun, Yingbo, Xueming Dong, and Lishan Yuan. 2026a. “Online Identification and Compensation for Damping Non-Uniformity of Hemispherical Resonator Gyroscope.” International Journal of Structural Stability and Dynamics: S0219455427504876. https://doi.org/10.1142/s0219455427504876
• Sun, Peng, and Guotal Feng. 2006. “Unsteady Three-Dimensional Analysis of Inlet Distortion in a Transonic Fan.” In Fluids Engineering. ASMEDC. https://doi.org/10.1115/imece2006-13145
• Sun, Jing, Annette Grot, Charles Ih, and Mark Mentzer. 1987. “Fiber-Optic Gyroscope Using a SWAOM: A Progress Report.” In Annual Meeting Optical Society of America. Optica Publishing Group. https://doi.org/10.1364/oam.1987.wy5
• Sun, Jian, Pengbin Guo, Teng Wu, and Gang Chen. 2019b. “Pulsar/Star Tracker/INS Integrated Navigation Method Based on Asynchronous Observation Model.” Journal of Aerospace Engineering 32 (5): 04019075. https://doi.org/10.1061/(asce)as.1943-5525.0001045
• Sun, J., and S. Hansen. 1982. “Transonic Nose Wave Drag of Axisymmetric Bodies.” In 20th Aerospace Sciences Meeting. AIAA 1982-308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-308
• Sun, J., S. Hansen, R. Cummings, and H. August. 1984. “Missile Aerodynamics Prediction (MAP) Code.” In 22nd Aerospace Sciences Meeting. AIAA 1984-389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-389
• Sun, Zuoming, and Junwei Li. 2018. “Bias Thermal Stability of Interferometer Fiber Optic Gyroscope Using a Polarization-Maintaining Photonic Crystal Fiber.” In Fourth Seminar on Novel Optoelectronic Detection Technology and Application, edited by Weiqi Jin, Ye Li. SPIE. https://doi.org/10.1117/12.2310035
• Sun, Yicheng, Howard Smith, and Haixin Chen. 2020a. “Conceptual Design of Low-Boom Low-Drag Supersonic Transports.” In AIAA Aviation 2020 Forum. AIAA 2020-2635. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2635
• Sun, Ne-Zheng, and Alexander Sun. 2015. “Optimal Experimental Design.” In Model Calibration and Parameter Estimation. Springer New York. https://doi.org/10.1007/978-1-4939-2323-6_11
• Sun, Zhongzhou, Zheng Wu, and Fanbiao Li. 2024b. “Observer Based Fault Diagnosis of Aircraft Active Landing Gear System.” Journal of Physics: Conference Series 2708 (1): 012010. https://doi.org/10.1088/1742-6596/2708/1/012010
• Sun, Ting, Fei Xing, Zheng You, and Minsong Wei. 2013. “Motion-Blurred Star Acquisition Method of the Star Tracker under High Dynamic Conditions.” Optics Express 21 (17): 20096. https://doi.org/10.1364/oe.21.020096
• Sun, Jin, Dengyin Zhang, Xiaoye Shi, and Fei Ding. 2020b. “Fast Compass Alignment for Strapdown Inertial Navigation System.” Computers, Materials & Continua 65 (2): 1349–60. https://doi.org/10.32604/cmc.2020.011459
• Sun, Huajun, Heng Zhang, Ziyan Wei, and Jie Li. 2025a. “Aerodynamic Shape Design of Oblique Wing for Transonic/Supersonic Conditions: Integrating Coupled Drag and Lateral Performance Using the Adjoint Method.” Preprint, . https://doi.org/10.2139/ssrn.5251753
• Sundara, Ramesh Raju, and G. Raju. 2022. “Estimation of Indian Regional Navigation Satellite System Receiver’s Position Accuracy in Terms of Statistical Parameters.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2022-01-6000
• Sundvall, Paul, Patrie Jensfelt, and Bo Wahlberg. 2007. “Fault Detection Using Redundant Navigation Modules.” In Fault Detection, Supervision and Safety of Technical Processes 2006. Elsevier. https://doi.org/10.1016/b978-008044485-7/50088-9
• Sung, Hong-Gye, Shih-Yang Hsieh, and Vigor Yang. 2001a. “A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine. I: Transition from Rocket Booster to Ramjet Sustainerner.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3460. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3460
• Sung, Hong-Gye, Shih-Yang Hsieh, and Vigor Yang. 2001b. “A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine. II: Combustion Dynamics of Ramjet Engine.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3192
• Sung, Chang-Ky, Jungshin Lee, Juhyun Oh, and Sang Jeong Lee. 2019. “Probabilistic Batch Processing Algorithm for Terrain Referenced Navigation.” Journal of Institute of Control Robotics and Systems 25 (7): 657–64. https://doi.org/10.5302/j.icros.2019.19.0067
• Sung, Chang-Ky, Seong-Ho Nam, and Myeong-Jong Yu. 2017. “Terrain Referenced Navigation Based on Robust Point Mass Filter Using Variance Adjusted Discrete Normal PDF and Mean Valued Likelihood.” In ION Pacific PNT. Institute of Navigation. https://doi.org/10.33012/2017.15043
• Sung, Hong-Gye, and Vigor Yang. 2014a. “Unified Analysis of Internal Flowfield in an Integrated Rocket Ramjet Engine. I: Transition from Rocket Booster to Ramjet Sustainer.” Journal of Aerospace Engineering 27 (2): 390–97. https://doi.org/10.1061/(asce)as.1943-5525.0000255
• Sung, Hong-Gye, and Vigor Yang. 2014b. “Unified Analysis of Internal Flowfield in an Integrated Rocket Ramjet Engine. II: Ramjet Sustainer.” Journal of Aerospace Engineering 27 (2): 398–403. https://doi.org/10.1061/(asce)as.1943-5525.0000256
• Sununu, J. H. 1970. Study of the Thermal Design and Performance of Strapdown Guidance and Control Systems. NASA-CR-86373. NASA. https://ntrs.nasa.gov/citations/19700021745
• “Supersonic and Hypersonic Flight.” 1960. BMJ 2 (5203): 934–36. https://doi.org/10.1136/bmj.2.5203.934
• “Supersonic Cruise.” 1981. In Studies in Astronautics. Elsevier. https://doi.org/10.1016/b978-0-444-41961-3.50017-6
• “SUPERSONIC FLIGHT.” 2014. In Becoming a Spacewalker. Purdue University Press. https://doi.org/10.2307/j.ctv15wxpxz.9
• Supersonic Flight. 2025. Wiley. https://doi.org/10.1002/9781394309290.ch5
• “Supersonic Flows over Wings and Airplane Configurations.” 2021. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009105842.012
• “Supersonic Flows over Wings and Airplane Configurations.” 2025. In Aerodynamics for Engineers. Cambridge University Press. https://doi.org/10.1017/9781009501293.012
• “Supersonic Transport Wing Minimum Weight Design Integrating Aerodynamics and Structures.” 1992. In 33rd Structures, Structural Dynamics and Materials Conference. AIAA 1992-2372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2372
• Sura, Niranjan K., and S. Suryanarayan. 2023. “Shimmy Studies on Simplified Linear Nose-Wheel Landing Gears Models.” Journal of Aerospace Sciences and Technologies: 55–60. https://doi.org/10.61653/joast.v56i1.2004.835
• Surber, L. 1975. “Effect of Forebody Shape and Shielding Technique on 2-D Supersonic Inlet Performance.” In 11th Propulsion Conference. AIAA 1975-1183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1183
• Surber, L., and C. Robinson. 1983. “Survey of Inlet Development for Supersonic Aircraft.” In 19th Joint Propulsion Conference. AIAA 1983-1164. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1164
• Surber, L., and D. Sedlock. 1978. “Effects of Airframe-Inlet Integration on Half-Axisymmetric and Two-Dimensional Supersonic Inlet Performance.” In 14th Joint Propulsion Conference. AIAA 1978-960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-960
• Sushma, M. Indira Rani, and M. Madhavi. 2025. “Performance Evaluation of Ramjet Engines: Supersonic Combustion vs. Shock Induced Combustion.” International Journal of Vehicle Structures and Systems 17 (6). https://doi.org/10.4273/ijvss.17.6.11
• Sutherland Jr., Gelb Arthur A., and Arthur. 1968. The Kalman Filter in Transfer Alignment of Airborne Inertial Guidance Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0851067
• Suzuki, Karebu, Kenji Kobayashi, Shuji Nakashita, and Yukihisa Yoshida. 2019. “High-Accuracy MEMS Gyroscope for Inertial Measurement Unit.” IEEJ Transactions on Sensors and Micromachines 139 (7): 175–79. https://doi.org/10.1541/ieejsmas.139.175
• Swamy, M., S. Ahmed, and G. Sreenath. 1978. “Model Support System Interference on Zero-Lift Drag at Transonic Speeds.” In 10th Aerodynamic Testing Conference. AIAA 1978-809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-809
• Swank, Aaron J., Paul S. Greenberg, and Michael J. Lichter. 2025. Interferometric Star Tracker: Basic Sensitivity Analysis. National Aeronautics and Space Administration. https://doi.org/10.64631/loqm3130
• Swanson, A. G. 1958. Free-Flight Investigation of Aerodynamic Heat Transfer to a Simulated Glide-Rocket Shape at Mach Numbers up to 10. NACA-RM-L58G03. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19630010650
• Swanson, Clifford O. 1962. “The King Inertial Navigation Gyro.” In Guidance and Control. Elsevier. https://doi.org/10.1016/b978-0-12-395586-9.50021-0
• Swanson, E. R. 1963. Estimating the Accuracy of Navigation Systems. a Statistical Method of Determining Circular Error Probable. Defense Technical Information Center. https://doi.org/10.21236/ad0427269
• Swanson, Andrew G., and Charles B. Rumsey. 1956. Aerodynamic Heating of a Wing as Determined from a Free-Flight Rocket-Model Test to Mach Number 3.64. NACA-RM-L56F11a. NASA. https://ntrs.nasa.gov/citations/19930089374
• Swaszek, Peter F., Richard J. Hartnett, and Kelly C. Seals. 2019. “Rethinking Star Selection in Celestial Navigation.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2019.16678
• Sweeney, Kevin, Annis Nusseibeh, Tim Kukowski, and Sally Ann Keyes. 2021. “Honeywell Vision-Aided Navigation for GPS-Denied Environments.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2021.18124
• Swingle, W., and Y. Kang. 1982. “The Shuttle Inertial System.” In Guidance and Control Conference. AIAA 1982-1559. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1559
• Syarafina, I., P. Adnan, and F. Hartono. 2020. “Design of Single Stage Axial Turbine for Mini Turbojet Engine.” AVIA 2 (1). https://doi.org/10.47355/avia.v2i1.16
• Syberg, J., and J. Koncsek. 1975. “Experimental Evaluation of an Analytically Derived Bleed System for a Supersonic Inlet.” In 11th Propulsion Conference. AIAA 1975-1210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1210
• Syberg, J., G. Paynter, and C. Carlin. 1981. “Inlet Design Technology Development: Supersonic Cruise Research.” In 17th Joint Propulsion Conference. AIAA 1981-1598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1598
• Sykes, Harrison G. n.d. “Cold Flow Performance of a Ramjet Engine.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2014.182
• Syring, James D. 2015. Ballistic Missile Defense System (BMDS). Defense Technical Information Center. https://doi.org/10.21236/ad1018994
• “System for Evaluation of F-15 Inlet Dynamic Distortion.” 1974. In Instrumentation for Airbreathing Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865077.0059.0076
• Szeliga, R., and R. D. Allan. 1974. Advanced Supersonic Technology Propulsion System Study. NASA-CR-143634. NASA. https://ntrs.nasa.gov/citations/19740023161
• Szelmanowski, Andrzej. 2013. “Feasibility to Diagnose Inertial Navigation Systems through Analysis of Schuler Errors.” Research Works of Air Force Institute of Technology 33 (1): 173–86. https://doi.org/10.2478/afit-2013-0010
• Szelmanowski, Andrzej, Grzegorz Kowalczyk, Krzysztof Kubryński, and Piotr Rogala. 2019. “Identification of Measurement Chain Properties in the Inertial Navigation Gimbal Systems of Aircraft.” Journal of KONBiN 49 (4): 491–509. https://doi.org/10.2478/jok-2019-0098
• Szklarski, Adrian, and Robert Głębocki. 2025. “Aerodynamic control analysis in a canard configuration for a surface-to-surface missile.” Archive of Mechanical Engineering: 583–606. https://doi.org/10.24425/ame.2025.155873
• Szymanski, Maxime, Georges Ghazi, and Ruxandra M. Botez. 2025. “Enhanced Neural Network Model for Aircraft Flight Dynamics Prediction from Flight Test Data: Business Aircraft Application.” In AIAA SCITECH 2025 Forum. AIAA 2025-2228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2228
• SŁOwak, re-Paweł. 2025. “Factor Graph-Based Trajectory Estimation for Radar-Based Missile Tracking.” Przegląd Elektrotechniczny 1 (5): 219–23. https://doi.org/10.15199/48.2025.05.45
• “T-4 Inlet/engine Compatibility Flight Test Results.” 1989. In 25th Joint Propulsion Conference. AIAA 1989-2466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2466
• Tabassum, Tarafder Elmi, Sorin A. Negru, Ivan Petrunin, and Zeeshan Rana. 2026. “Error Correction Using Bayesian GRU Network in Hybrid Visual Inertial Navigation System.” In European Navigation Conference 2025. MDPI. https://doi.org/10.3390/engproc2026126052
• Tacina, Kathleen M., Derek P. Podboy, and Francisco J. Guzman. 2022. “Flametube Evaluation of a Lean-Lean Combustor Concept Developed for Supersonic Cruise Aircraft.” Journal of Engineering for Gas Turbines and Power 145 (5): 051008. https://doi.org/10.1115/1.4056100
• Taff, Laurence G. 1986. The Completion of a Star Catalog for the Optical Aircraft Measurements Program. Defense Technical Information Center. https://doi.org/10.21236/ada168017
• Taguchi, Hideyuki, Kenya Harada, Hiroaki Kobayashi, et al. 2009. “Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7311. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7311
• Taguchi, Hideyuki, Hiroaki Kobayashi, Takayuki Kojima, et al. 2012. “Hypersonic Flight Experiment Plan of Pre-Cooled Turbojet Engine.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5840
• Taguchi, Hideyuki, Tetsuya Sato, Hiroaki Kobayashi, et al. 2005. “Design Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments.” In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2005-3419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3419
• Tahani, M., M. Masdari, and M. Kazemi. 2017. “Aerodynamic Performance Improvement of a Canard Control Missile.” Aircraft Engineering and Aerospace Technology 89 (6): 871–78. https://doi.org/10.1108/aeat-01-2016-0019
• Taheri-Tehrani, P., T.-H. Su, A. Heidari, et al. 2014. “Micro-Scale Diamond Hemispherical Resonator Gyroscope.” In 2014 Solid-State, Actuators, and Microsystems Workshop Technical Digest. Transducer Research Foundation. https://doi.org/10.31438/trf.hh2014.77
• Taherian, Reza. 2026. “Design and Materials of Aircraft Brake Pads: Types, Formulations, and Case Studies.” In Brake Pads. Elsevier. https://doi.org/10.1016/b978-0-443-26645-4.00004-9
• Takahashi, Shinei, Kazuhide Mizobata, Keisuke Sawada, Shinei Takahashi, Kazuhide Mizobata, and Keisuke Sawada. 1997. “Conceptual Study of an Airbreathing Reusable Launch Vehicle.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-192
• Takahashi, Timothy, Raymond Spall, Damon Turner, and Mark Birney. 2005. “A Multi-Disciplinary Survey of Advanced Subsonic Tactical Cruise Missile Configurations.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-709. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-709
• Takanashi, Shinichiro, Etsuroh Sentoh, Akihiko Yoshida, et al. 1998. “Sidejet Aerodynamics Interaction Effect of the Missile. I: Estimation of Missile Sidejet Interaction Force by Modeling in Pressure Field.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4273
• Takasaki, Satoru, Akira Fujimoto, Brett Churchill, and Toru Takasu. 1998. “Inlet Unstart Influence on Aerodynamic Characteristics of Next Generation Supersonic Transport (SST).” In AIAA and SAE, 1998 World Aviation Conference. AIAA 1998-5546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5546
• Takehira, Tetsuya, Nguyen Vinh, Pierre Kabamba, Tetsuya Takehira, Nguyen Vinh, and Pierre Kabamba. 1997. “Analytical Solution of Missile Terminal Guidance.” In Guidance, Navigation, and Control Conference. AIAA 1997-3472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3472
• Takei, Nobuyuki, Martin Miranda, Yuki Miyazawa, and Mikio Kozuma. 2022. “Simultaneous Suppression of Thermal Phase Noise and Relative Intensity Noise in a Fiber Optic Gyroscope.” Preprint, TechRxiv. https://doi.org/10.36227/techrxiv.21776282
• Takovitskii, Sergey. 2020. “Axisymmetric Forebodies Having Minimum Drag in Supersonic Flow.” In AIAA Aviation 2020 Forum. AIAA 2020-3120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3120
• Takovitskii, S. A. 2023. “Direct Method of Aerodynamic Shape Optimization for Supersonic Aircraft Design.” Journal of Aerospace Sciences and Technologies: 201–8. https://doi.org/10.61653/joast.v61i1.2009.632
• Taletović, Jasmin, and Dževad Krdžalić. 2017. “Research on the Influence of Vertical Deflection to the Line Geodetic Network: Prism Method.” Geodetski glasnik, no. 48: 103–24. https://doi.org/10.58817/2233-1786.2017.51.48.103
• Talole, Sanjay, Vinay Upreti, and S. Phadke. 2004. “Predictive Estimation and Control Based Missile Autopilot Design.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5331. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5331
• Talwani, M. 1966. Gravity Anomaly Belts in the Caribbean. Natural Resources Canada/CMSS/Information Management. https://doi.org/10.4095/103302
• Tamada, Isao, Shigeru Aso, and Yasuhiro Tani. 2010. “Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-991. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-991
• Tanaka, Taku, Keiko Tanaka, Toshitaka Uneoka, et al. 2025. “CIMS (Celestial-Integrated Magnetic-Geophysical Navigation System): A Tightly-Coupled Multi-Physics GNSS-Denied Navigation Framework with Complementary Observability Analysis and Numerical Validation.” Preprint, . https://doi.org/10.36227/techrxiv.176472866.61761576/v1
• Tanck, Pamela A., and Kimberly B. Steadman. 1998. “Single Stage and Thrust Augmented Reusable Launch Vehicle Stability and Performance Study.” In AIP Conference Proceedings, vol. 420. AIP. https://doi.org/10.1063/1.54716
• Tang, Adrian J. 2013. Millimeter-Wave Localizers for Aircraft-to-Aircraft Approach Navigation. NPO-48868. California Inst. of Tech. https://ntrs.nasa.gov/citations/20140002265
• Tang, Jian-qiao, Ling Xiong, Kai-han Li, and Jie Ma. 2015b. “Research on Matching Area Selection Based on Multiple Features Fusion of Full Tensor Gravity Gradient.” In SPIE Proceedings, vol. 9812, edited by Nong Sang, Xinjian Chen. SPIE. https://doi.org/10.1117/12.2204828
• Tangirala, Venkat, Anthony Dean, Nobuyuki Tsuboi, and Koichi Hayashi. 2007. “Performance on a Pulse Detonation Engine under Subsonic and Supersonic Flight Conditions.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1245
• Tanner, W. 1972a. In-Flight Angular Alignment of Inertial Navigation Systems by Means of Radio Aids. NASA-CR-128806. NASA. https://ntrs.nasa.gov/citations/19730010912
• Tanner, J. A. 1972b. Performance of an Aircraft Tire under Cyclic Braking and of a Currently Operational Antiskid Braking System. NASA-TN-D-6755. NASA. https://ntrs.nasa.gov/citations/19720016364
• Tanner, J. A. 1973. “Fore and Aft Elastic Response Characteristics of Size 34x9.9, Type 7, 14 Ply-Rated Aircraft Tires of Bias Ply, Bias Belted, and Radial Belted Design.” PhD diss., NASA Langley Research Center. https://ntrs.nasa.gov/citations/19730020255
• Tanner, J. A. 1974. “Fore and Aft Elastic Response Characteristics of 34 x 9.9, Type 7, 14 Ply-Rating Aircraft Tires of Bias-Ply, Bias-Belted, and Radial-Belted Design.” PhD diss., NASA Langley Research Center. https://ntrs.nasa.gov/citations/19740011551
• Tanno, Hideyuki, Tomoyuki Komuro, Kazuo Sato, Katsuhiro Itoh, and Tetsuya Yamada. 2013. “Free-Flight Tests of Reentry Capsule Models in Free-Piston Shock Tunnel.” In 43rd Fluid Dynamics Conference. AIAA 2013-2979. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2979
• Tanriverdi, Gunes, and Mursel Emre Cavdaroglu. 2017. “Utilization of INS Measurements into Fixed-Point Smoothing Approach to Mitigate the Disturbance Effect of Missile Initial Heading Errors on Missile Terminal Guidance Performance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1033
• Tanzer, H. J. 1982. Fabrication and Development of Several Heat Pipe Honeycomb Sandwich Panel Concepts. NASA-CR-165962. NASA. https://ntrs.nasa.gov/citations/19830002109
• Tao, Xianlu, Chi Zhang, Shuguo Pan, Wang Gao, and Qiang Wang. 2026. “State-Aware Velocity Estimation for GNSS/INS Integration Using IMU Measurements in GNSS-Denied Environments.” Preprint, . https://doi.org/10.2139/ssrn.6849400
• Tartaruga, Irene, Mark H. Lowenberg, Jonathan E. Cooper, Pia Sartor, and Yves Lemmens. 2016. “Bifurcation Analysis of a Nose Landing Gear System.” In 15th Dynamics Specialists Conference. AIAA 2016-1572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1572
• Tashakkor, Scott B., Francisco Canabal, and Jason E. Mishtawy. 2011. CFD Modeling of Launch Vehicle Aerodynamic Heating. M11-0030. Jacobs Engineering Group, Inc. https://ntrs.nasa.gov/citations/20110014627
• Tatar, Erdinc. 2026. The Path to No-Drift MEMS Inertial Sensors with on-Chip Stress Calibration. https://doi.org/10.52843/cassyni.sxqcvq
• Tatum, G. R. 1949. “Some Problems in Guided-Missile Development.” Navigation 2 (1): 27–31. https://doi.org/10.1002/j.2161-4296.1949.tb00471.x
• Taur, Der-Ren. 2002. “Nonlinear Guidance and Navigation of a Tactical Missile with High Heading Error.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4773. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4773
• Taur, Der-ren. 2013. “Anti-Missile RF Homing Guidance and Navigation with Terminal Side Jet.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5245
• Taylor, J. 1968a. “Engine Compatibility Programs for the Supersonic Transport Propulsionsystem.” In 5th Annual Meeting and Technical Display. AIAA 1968-993. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-993
• Taylor, J. B. 1968b. “Inlet Duct-Engine Exhaust Nozzle Airflow Matching for the Supersonic Transport.” Aeronautical Journal 72 (690): 490–97. https://doi.org/10.1017/s0001924000084347
• Taylor, James H. 1975. Handbook for the Direct Statistical Analysis of Missile Guidance Systems via CADET (Trademark) (Covariance Analysis Describing Function Technique). Defense Technical Information Center. https://doi.org/10.21236/ada013397
• Taylor, Brian R. 2009. “X-48B Preliminary Flight Test Results.” In 2009 Annual Meeting, NASA Fundamenta Aeronautics Program, Subsonic Fixed Wing Project. https://ntrs.nasa.gov/citations/20090036791
• Taylor, Brian. 2012b. “A Full-Envelope Air Data Calibration and Three Dimensional Wind Estimation Method Using Global Output-Error Optimization and Flight-Test Techniques.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4410. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4410
• Taylor, R. E., T. R. Goerz, and J. V. Beck. 2021. “Automatic Non-Destructive Brake Tester for Thermal Diffusivity/Conductivity of Aircraft Brake Disks.” In Thermal Conductivity 23. CRC Press. https://doi.org/10.1201/9781003210719-5
• Taylor, James H., and Charles F. Price. 1974. Direct Statistical Analysis of Missile Guidance Systems via CADET (Covariance Analysis Describing Function Technique). Defense Technical Information Center. https://doi.org/10.21236/ad0783098
• Taylor, Brian, Nalin Ratnayake, and James Murray. 2010. “Simulation and Flight Evaluation of a Parameter Estimation Input Design Method for Hybrid-Wing-Body Aircraft.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7949
• Taylor, Fred, Jacob Spagnolli, Benon Gattis, and Dennis Akos. 2026. “Alternative PNT in GNSS-Denied Environments: A Flexible, COTS SDR System for Monitoring and Navigation.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20693
• Taylor, L., Jr., and B. Pamadi. 1983. “Estimation of Parameters Involved in High Angle-of-Attack Aerodynamic Theory Using Spin Flight Test Data.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2086. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2086
• “Technical Applications for an Experimental Supersonic Cruise Aircraft.” 1976. In Aircraft Systems and Technology Meeting. AIAA 1976-892. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-892
• “A Technology and Operations Assessment of Single Stage Rocket Technology Flight Test Program Results.” 1993. In Space Programs and Technologies Conference and Exhibit. AIAA 1993-4163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-4163
• Tekaslan, Huseyin E., Rumed Imrak, and Melike Nikbay. 2021. “Reliability Based Design Optimization of a Supersonic Engine Inlet.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3541. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3541
• Telen, Dries, Filip Logist, Eva Van Derlinden, and Jan F. Van Impe. 2012. “Parameter Accuracy vs. Decorrelation in Optimal Experiment Design.” In Computer Aided Chemical Engineering. Elsevier. https://doi.org/10.1016/b978-0-444-59520-1.50024-5
• Templier, Simon. n.d. “Three-Axis Hybridized Quantum Accelerometer for Inertial Navigation.” PhD diss., Bordeaux. https://doi.org/10.70675/bb7eef5az95b7z49c2za354zb359568b2de7
• Teng, Jian, Yancheng You, Yiqing Li, and Chengjian Pan. 2015a. “Flow Distortion Generation and Management of an Axisymmetric Ramjet Engine.” In 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2015-3630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3630
• “Terrain Aided Navigation System Combines with Moving Colour Maps.” 1986. Aircraft Engineering and Aerospace Technology 58 (5): 25–25. https://doi.org/10.1108/eb036289
• Terrain Referenced Navigation Technique Using Correlation Algorithms for Cruise Vehicle. 2023. https://doi.org/10.37285/bsp.sasat2023.11
• Terrain Relative Navigation. 2025. Wiley. https://doi.org/10.1002/9781394267743.ch10
• Teskey, W. F. 1982. “Determination of Deflection of the Vertical by the Astrogeodetic Difference Method.” Canadian Surveyor 36 (2): 183–90. https://doi.org/10.1139/tcs-1982-0020
• Tetlow, M., U. Schoettle, and G. Schneider. 2000. “Optimisation of a Reusable Launch Vehicle Concept.” In Modeling and Simulation Technologies Conference. AIAA 2000-4180. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4180
• Tewell, J. 1984. “An Unmanned Reentry/recovery Vehicle for a Reusable Launch System.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-781
• Thangadurai, G., B. Chandran, V. Babu, and T. Sundararajan. 2008. “Numerical Analysis of Integrated Liquid Ramjet Engine.” Defence Science Journal 58 (3): 327–37. https://doi.org/10.14429/dsj.58.1652
• Thapar, Gagandeep S., and Leonardo A. Torres. 2024. “Stochastic Modeling of the Star Tracker Measurement Process to Assess Accuracy and Precision from Perturbation Propagation.” In AIAA SCITECH 2024 Forum. AIAA 2024-1259. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1259
• Thawait, Amit Kumar, Parag Tandaiya, and Abhilash J. Chandy. 2024a. “Investigation of Nonlinear Aerothermoelastic Characteristics of the Deployable Control Fin Using Tightly Coupled Fluid-Thermal-Structural Interaction Analysis.” In Lecture Notes in Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-67241-5_36
• Thawait, Amit Kumar, Parag Tandaiya, Prakash C. Jain, and Abhilash J. Chandy. 2023a. “Delayed Detached Eddy Simulation-Based Aerothermoelastic Analysis of Deployable Control Fin in Supersonic and Hypersonic Flows.” Physics of Fluids 35 (9): 096110. https://doi.org/10.1063/5.0165168
• Thein, May-Win, David Quinn, and David Folta. 2008. “Celestial Navigation (CelNav): Lunar Surface Navigation.” In AIAA/AAS Astrodynamics Specialist Conference and Exhibit. AIAA 2008-6759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6759
• Theis, Julian, Harald Pfifer, Andreas Knoblach, Florian Saupe, and Herbert Werner. 2015. “Linear Parameter-Varying Feedforward Control: A Missile Autopilot Design.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-2001. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2001
• Theodoulis, Spilios, and Gilles Duc. 2008. “Gain Scheduled Autopilot Synthesis for an Atmosphere Re-Entry Vehicle.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7469. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7469
• “Theoretical Modeling of the Base Flow Region of Supersonic Bodies: A Steady-State Method.” 1976. In Aerodynamics of Base Combustion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865145.0255.0305
• “Theoretical Studies to Refine the Prediction of Unsteady Aerodynamics of Supersonic Elastic Aircraft.” 1970. In Guidance, Control and Flight Mechanics Conference. AIAA 1970-944. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-944
• Thibert, J. J., and D. Arnal. 2000. “A Review of ONERA Aerodynamic Research in Support of a Future Supersonic Transport Aircraft.” Progress in Aerospace Sciences 36 (8): 581–627. https://doi.org/10.1016/s0376-0421(00)00010-5
• Thibodeau, J. R., and S. R. Bauer. 1982. Redundancy Management of the Space Shuttle Inertial Measurement Units. AIAA PAPER 82-1561. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/19820055473
• Thomas, Paul D. 1965. Mathematical Models for Navigation Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0627893
• Thomas, Nathan R., Akhil Marayikkottu Vijayan, and Deborah A. Levin. 2022. “Heat Transfer Study of a Conically Shaped Hypersonic Vehicle in Glide.” In AIAA SCITECH 2022 Forum. AIAA 2022-1499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1499
• Thomas, J. L., J. W. Paulson Jr., and L. P. Yip. 1977. “Effects of Deflected Thrust on the Stability and Performance Characteristics of a Close-Coupled Canard Fighter Configuration.” In Society of Automotive Engineers. https://ntrs.nasa.gov/citations/19770055724
• Thomas, Scott R., H. Douglas Perkins, and Charles J. Trefny. 1997. “Evaluation of an Ejector Ramjet Based Propulsion System for Air-Breathing Hypersonic Flight.” In Future Aerospace Technology in the Service of the Alliance. https://ntrs.nasa.gov/citations/19980018678
• Thomas, Ronald D., and Gerald J. Shroyer. 1965. “Automatic Star-Trackers for Long-Range Navigation.” Journal of Navigation 18 (4): 482–97. https://doi.org/10.1017/s0373463300046403
• Thomas, Randy, and David Thomas. 2008. “Development of a Landing Drag Chute System for Very Light Jets.” In The 26th Congress of ICAS and 8th AIAA ATIO. AIAA 2008-8950. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-8950
• Thompson, J. S. 1951. “Lunar Parallax Method of Astro Navigation.” Navigation 3 (1–2): 50–57. https://doi.org/10.1002/j.2161-4296.1951.tb00604.x
• Thompson, David. 1965. “Automatic Vectoring and Landing of Carrier Based High Performance Aircraft.” In Guidance Control Conference. AIAA 1965-1209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1209
• Thompson, Andrew A. 2000. Calibration of Inertial Sensors. Defense Technical Information Center. https://doi.org/10.21236/ada384788
• Thompson, Peter, Benjamin Jan Andersson, Nicolas Sundqvist, and Gunnar Cedersund. 2022. “A New Method for a Priori Practical Identifiability.” Preprint, bioRxiv. https://doi.org/10.1101/2022.10.20.511900
• Thompson, Wilbur E., and Walter B. Horne. 1959. Low-Speed Yawed-Rolling Characteristics of a Pair of 56-Inch-Diameter, 32-Ply-Rating, Type 7 Aircraft Tires. NASA-MEMO-2-7-59L. NASA. https://ntrs.nasa.gov/citations/19980231043
• Thorp, Scott A., and Kevin M. Downey. 1992. Computer Aided Design and Manufacturing of Composite Propfan Blades for a Cruise Missile Wind Tunnel Model. NASA-TM-105269. NASA. https://ntrs.nasa.gov/citations/19930002834
• Thota, Phanikrishna, Bernd Krauskopf, and Mark Lowenberg. 2008b. “Modeling of Nose Landing Gear Shimmy with Lateral and Longitudinal Bending and a Non-Zero Rake Angle.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2008-7099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7099
• Thota, Phanikrishna, Bernd Krauskopf, Mark Lowenberg, and Etienne Coetzee. 2009. “Nonlinear Analysis of the Influence of Tire Inflation Pressure on Nose Landing Gear Shimmy.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2009-6230. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6230
• Thummala, Rajiv, and Gregory Falco. 2025. “Star Tracker Attacks and Defenses.” In AIAA SCITECH 2025 Forum. AIAA 2025-2721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2721
• Thurman, Sam W. 2004. Surveyor Spacecraft Automatic Landing System. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210001643
• Tian, Yuan, and Marc Compere. 2019. “Monocular Visual Inertial Odometry (VIO) Dataset Collection with a Self-Calibrating Platform for Inertial Measurement Unit (IMU).” In Volume 14: Design, Systems, and Complexity. American Society of Mechanical Engineers. https://doi.org/10.1115/imece2019-10595
• Tien, Khuat Quang. 2026. “Application of the Adaptive Kalman Filter in Sensor Drift Compensation and Accuracy Enhancement of the Inertial Navigation System.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0726002.2
• Ting, Kuang-Ying, Kenneth Wiersema, Reza Soltani, Chester Nelson, and Eli Livne. 2025. “Supersonic Configurations at Low Speeds (SCALOS) Lateral-Directional Aerodynamics: Configuration Variations and Control Surface Effects.” In AIAA SCITECH 2025 Forum. AIAA 2025-2361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2361
• Tischler, Mark B. 2018. “System Identification Methods for Aircraft Flight Control Development and Validation.” In Advances in Aircraft Flight Control. Routledge. https://doi.org/10.1201/9781315136820-2
• Tk, Khadeeja Nusrath, Ankur Sarmah, and Jatinder Singh. 2014. “Flight Path Reconstruction and Wind Estimation Using Flight Test Data from Crash Data Recorder (CDR).” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2014-01-2168
• Tkalenko, R. A. 1969. “Slender Bodies of Revolution with Minimum Wave Drag in Nonequilibrium Supersonic Flow.” Fluid Dynamics 4 (6): 47–49. https://doi.org/10.1007/bf01032473
• Todić, Ivana, and Vladimir Kuzmanović. 2018. “Code Optimization for Strapdown Inertial Navigation System Algorithm.” In InTech eBooks. https://doi.org/10.5772/intechopen.71732
• Tokugawa, Naoko, and Kenji Yoshida. 2006. “Transition Detection on Supersonic Natural Laminar Flow Wing in the Flight.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3165
• Tomaine, R. L., W. H. Bryant, and W. F. Hodge. 1978. “VALT Parameter Identification Flight Test.” In European Rotorcraft and Powered Lift Aircraft Forum. https://ntrs.nasa.gov/citations/19780061530
• Tomczak, Franciszek Dominik. 2026. “Numerical Investigation of the Applicability of a Single Ramp Supersonic Inlet for Ramjet Propulsion.” In Materials Research Proceedings, vol. 69. Materials Research Forum LLC. https://doi.org/10.21741/9781644904251-111
• Tomczyk, Andrzej, and Jan Gruszecki. 1999. “Preliminary Project of the Autonomous Landing System for Unmanned Aircraft.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/1999-01-5524
• Tomczyński, Jakub, Tomasz Mańkowski, and Piotr Kaczmarek. 2017. “Cross-Sensor Calibration Procedure for Magnetometer and Inertial Units.” In Advances in Intelligent Systems and Computing. Springer International Publishing. https://doi.org/10.1007/978-3-319-54042-9_43
• Tomioka, Sadatake, Kanenori Kato, Kouichiro Tani, Susumu Hasegawa, Masatoshi Kodera, and Shuichi Ueda. 2012. “Performance of a Rocket-Ramjet Combined-Cycle Engine Model under Ramjet-Mode Operations.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-3921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3921
• Tomioka, Sadatake, Shuuichi Ueda, Kohichiro Tani, and Takeshi Kanda. 2007. “Scramjet Engine Tests at Ramjet Engine Test Facility in JAXA-KSPC.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1040
• Tong, Yu-de, Shao-feng Bian, and Bing Ji. 2012. “A Real-Time Maximum Correlation Matching Based on Approximated Local Gravity Map.” In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-29187-6_49
• Tong, Shuai, Hui Li, and An Guo Wang. 2014. “Research on Accuracy of Multi-Channel Star Tracker.” Applied Mechanics and Materials 644-650: 4443–46. https://doi.org/10.4028/www.scientific.net/amm.644-650.4443
• Tong, Xindi, Jia Song, Wenling Li, and Yang Liu. 2026. “Learning-Based Artificial Potential Field Guidance for Hypersonic Glide Vehicle Penetration.” Aeronautical Journal: 1–25. https://doi.org/10.1017/aer.2026.10218
• Tong, Xiao-Tong, Lian-Jie Yue, Wan-Nan Wu, Qi-Fan Zhang, and Hao Chen. 2024. “Self-Similar Unstart Characteristics of Supersonic Contraction Duct with an Expansion Corner.” Physics of Fluids 36 (1): 016148. https://doi.org/10.1063/5.0180243
• Tooley, Mike, and David Wyatt. 2024a. “Aircraft Navigation.” In Aircraft Communications and Navigation Systems. Routledge. https://doi.org/10.1201/9781003411932-8
• Tooley, Mike, and David Wyatt. 2024b. “Inertial Navigation Systems.” In Aircraft Communications and Navigation Systems. Routledge. https://doi.org/10.1201/9781003411932-15
• Topal, Ahmet, Onder Turan, and Sıtkı Uslu. 2015. “Design, Manufacturing and Rig Test of a Small Turbojet Engine Combustor with Airblast Atomizer.” International Journal of Materials, Mechanics and Manufacturing 3 (2): 97–100. https://doi.org/10.7763/ijmmm.2015.v3.174
• Tournes, Christian, and C. Johnson. 1998a. “Ramjet-Powered Reusable Launch Vehicle Control by Subspace Stabilization.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4151. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4151
• Tournes, C., and C. Johnson. 1998b. “Reusable Launch Vehicle Guidance and Control Using Subspace Stabilization Control Techniques.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4119. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4119
• “Tracking Radar.” 1999. In Understanding Radar Systems. Institution of Engineering and Technology. https://doi.org/10.1049/sbra034e_ch3
• Trageser, M. 1975. “Feasibility Model Gravity Gradiometer Test Results.” In Guidance and Control Conference. AIAA 1975-1093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1093
• “Transonic Aircraft Configurations.” 2012. In Aerodynamic Principles of Flight Vehicles. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600869174.0171.0220
• “Transonic and Supersonic Flight.” 1992. In Aircraft Performance. Cambridge University Press. https://doi.org/10.1017/cbo9780511607134.012
• Traoré, Achmed, and Pascal Lemée. 2001. “Laminar Design for Supersonic Civil Transport.” In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_16
• Trapier, S., S. Deck, and P. Duveau. n.d. “Delayed Detached-Eddy Simulation of Supersonic Inlet Buzz.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-77815-8_25
• Trapier, Simon, Sébastien Deck, Philippe Duveau, and Philippe Guillen. 2007a. “Delayed Detached-Eddy Simulation of Supersonic Inlet Buzz.” In 37th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2007-4353. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4353
• Trawny, Nikolas, Corey L. Marcus, Po-Ting Chen, Robert A. Hewitt, and Timothy P. Setterfield. 2022. Real-World Testing of LiDAR-Inertial Based Navigation and Mapping for Precision Landing. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20230006930
• Trazzi, P. E. 2004. “Design and Development of a 70 n Thrust Class Turbojet Engine.” Revista de Engenharia Térmica 3 (1). https://doi.org/10.5380/ret.v3i1.3484
• Treder, Alfred, and Keith Meldahl. 1991. “Flight Results of Attitude Matching between Space Shuttle and Inertial Upper Stage (IUS) Navigation Systems.” In Navigation and Control Conference. AIAA 1991-2682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2682
• Trefny, Charles J. 2020. “CFD Simulation of an Inward-Turning Supersonic Inlet Unstart at Flight Mach Number 1.7.” In AIAA Propulsion and Energy 2020 Forum. AIAA 2020-3771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-3771
• Trefny, C. J., and T. J. Benson. 1995. “An Integration of the Turbojet and Single-Throat Ramjet.” In 1995 Airbreathing Propulsion Subcommittee Meeting. https://ntrs.nasa.gov/citations/19960016375
• Trefny, Charles, and Vance Dippold. 2010. “Supersonic Free-Jet Combustion in a Ramjet Burner.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6643
• Trifonov-Bogdanov, Peter, Anastasia Zhiravetska, Tatjana Trifonova-Bogdanova, and Vladimir Shestakov. 2012. “Mechanisms of Error Development in Inertial Navigation Systems.” Aviation 16 (2): 33–37. https://doi.org/10.3846/16487788.2012.701872
• Trifonova, E. S., and P. A. Ushakov. 2021. “Method for Measuring the Rotation Angles of Hemispherical Resonator Gyroscope Using the Frequency Division.” Intellekt. Sist. Proizv. 19 (1): 54. https://doi.org/10.22213/2410-9304-2021-1-54-58
• Trifonovs-Bogdanovs, Pjotrs, and Anvar Zabirov. 2018. “Analysis of the Strapdown Inertial Navigation System (SINS) Error Genesis.” Transport and Aerospace Engineering 6 (1): 44–54. https://doi.org/10.2478/tae-2018-0006
• Trifu, O., and G. Savu. 1993. “Optimum Axisymmetric Boattailing for Minimum Base Drag at Supersonic-Moderate Hypersonic Speeds.” In 5th International Aerospace Planes and Hypersonics Technologies Conference. AIAA 1993-5046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-5046
• Trimpi, R. 1980. “Modern Fluid Dynamics of Supersonic and Hypersonic Flight.” In International Meeting and Technical Display on Global Technology 2000. AIAA 1980-862. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-862
• Trinh, V. T., N. M. Nguyen, N. T. Dang, and K. A. Nguyen. 2018. “An Anthropocentric Approach for Solving the Problem of Optimal Automatic Landing Flare.” Russian Aeronautics 61 (2): 220–29. https://doi.org/10.3103/s1068799818020101
• Troiani, Chiara. n.d. “Vision-Aided Inertial Navigation: Low Computational Complexity Algorithms with Applications to Micro Aerial Vehicles.” PhD diss., Grenoble. https://doi.org/10.70675/1c7119d3z3240z4d06za5bezd2dce816f558
• Trotsyuk, A. V. 2021. “Detonation Structures in a Supersonic Annular Ramjet Chamber.” In Detonation: Latest accomplishments. TORUS PRESS. https://doi.org/10.30826/icpcd12b09
• Trotter, B. E. 1957. Navigation Systems. Defense Technical Information Center. https://doi.org/10.21236/ada459665
• Truesdale, Nicholas, Michael Skeen, Jedediah Diller, et al. 2013b. “DayStar: Modeling the Daytime Performance of a Star Tracker for High Altitude Balloons.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-139
• Truitt, R. W. 1968. Some Aspects of Aerodynamic Heating. North Carolina State Univ. https://ntrs.nasa.gov/citations/19700009384
• Trussell, Donald H., and Deene J. Weidman. 1960. A Radiant Heater to Simulate Aerodynamic Heating in a Wind Tunnel. NASA/TN-D-530. NASA. https://ntrs.nasa.gov/citations/20040047051
• Trutnev, G. A. 2015. “The Model of Hemispherical Resonator Gyroscope in Terms of Slow Variables.” Vestnik Udmurtskogo Universiteta. Matematika. Mekhanika. Komp’yuternye Nauki 25 (3): 421–29. https://doi.org/10.20537/vm150312
• Trutnev, G. A. 2019a. “Model of the Hemispherical Resonator Gyroscope Construction Damping.” Vestnik Udmurtskogo Universiteta. Matematika. Mekhanika. Komp’yuternye Nauki 29 (1): 84–91. https://doi.org/10.20537/vm190108
• Trutnev, G. A. 2019b. “Scale Factor Nonlinearity of Hemispherical Resonator Gyro.” Intellekt. Sist. Proizv. 16 (4): 138. https://doi.org/10.22213/2410-9304-2018-4-138-144
• Trutnev, G. A., K. K. Perevozchikov, and S. B. Nazarov. 2020. “Sensing System and Methods for Measuring Oscillations in the Resonator of a Hemispherical Resonator Gyroscope.” Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, no. 1 (130): 50–63. https://doi.org/10.18698/0236-3933-2020-1-50-63
• Trutnev, G. A., and A. V. Shchenyatskiy. 2022. “Computational Component in a Hemispherical Resonator Gyroscope with Its Measuring Component Utilising Alternating Voltage.” Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, no. 3 (140): 78–91. https://doi.org/10.18698/0236-3933-2022-3-78-91
• TRW Space Technology Labs Redondo Beach CA. 1963. Range Instrumentation Planning Study. Volume 5: Tracking, Telemetry, and Command (TTC). Defense Technical Information Center. https://doi.org/10.21236/ad0462795
• Tsai, Hsiu-Chi, and Chia-Tung Chung. 2026. “A Large-Scale Empirical Study of Deep Learning for MEMS Gyroscope Bias Estimation.” Preprint, . https://doi.org/10.31224/7144
• Tsai, Tsung-Ming, David Coombs, Billibon Yoshimi, and Ernest Kent. 2001. Visualizing Terrain and Navigation Data. National Institute of Standards and Technology. https://doi.org/10.6028/nist.ir.6720
• Tsai, Huan-Liang, and Jium-Ming Lin. 2006. “General Autopilot Design for BTT Missile by Generalized Linear Quadratic Gaussian / Loop Transfer Recovery Method.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6571. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6571
• Tsao, Shu-Hua. 2023. “Observability Analysis and Performance Evaluation for a Graph-Based GNSS–Visual–Inertial Odometry on Matrix Lie Groups.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2023.19401
• Tseng, Yi-Chen, and Shau-Shiun Jan. 2026. “Motion-Aware Restoration of Smeared Star Tracker Images for High-Performance Satellite Attitude Determination.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2026.20519
• Tsikalas, G., and D. Dyer. 1982. Shuttle Automatic Landing System. AAS 82-017. Sperry Corp. https://ntrs.nasa.gov/citations/19820062072
• Tsiopliakis, N. 2026. “Fast Block Kalman Filter for Visual-Inertial Navigation.” Gyroscopy and Navigation 17 (1): 43–58. https://doi.org/10.1134/s2075108726700112
• Tsoubanos, Christos M. 1979. Stabilized Terrain Optical Position Sensor (STOPS) Flight Test Report. Defense Technical Information Center. https://doi.org/10.21236/ada065018
• Tsourdos, A. 1998. “Autopilot Design of a Non-Linear Missile.” In UKACC International Conference on Control (CONTROL ‘98), vol. 1998. IEE. https://doi.org/10.1049/cp:19980346
• Tsourdos, Antonios, and Brian White. 2002. “Fuzzy Gain-Scheduling Flight Controller for a STT Missile.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4659. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4659
• Tsourdos, Antonios, and Brian White. 2012. “Robust Autopilot Design for Quasilinear Parameter- Varying Missile Model.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-2
• Tsukamoto, Takashiro, and Shuji Tanaka. 2018. “Virautlly Rotated High Bias Stability MEMS Whole Angle Gyroscope Using CW/CCW Mode Separation.” Proceedings of Mechanical Engineering Congress, Japan 2018 (0): J2240001. https://doi.org/10.1299/jsmemecj.2018.j2240001
• Tu, Eugene. 1991. “Navier-Stokes Simulation of a Close-Coupled Canard-Wing-Body Configuration.” In 29th Aerospace Sciences Meeting. AIAA 1991-70. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-70
• Tu, Eugene. 1992a. “Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics.” In 10th Applied Aerodynamics Conference. AIAA 1992-2602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2602
• Tu, Eugene. 1992b. “Effect of Canard Position on the Longitudinal Aerodynamic Characteristics of a Close-Coupled Canard-Wing-Body Configuration.” In Astrodynamics Conference. AIAA 1992-4632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4632
• Tu, Eugene. 1996. “Time-Accurate Navier-Stokes Simulation of a Canard-Wing-Body Configuration with Moving Canards.” In 14th Applied Aerodynamics Conference. AIAA 1996-2407. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2407
• Tu, Junyu, Lu Liu, Hanzhao Li, and Huilian Ma. 2020. “High-Performance Digital Signal Processor for Navigation Grade Resonant Fiber Optic Gyroscope.” In 14th Pacific Rim Conference on Lasers and Electro-Optics (CLEO PR 2020). Optica Publishing Group. https://doi.org/10.1364/cleopr.2020.c11g_5
• Tu, Eugene L., Shigeru Obayashi, and Guru P. Guruswamy. 1993. “Unsteady Navier-Stokes Simulation of the Canard-Wing-Body Ramp Motion.” In AIAA. https://ntrs.nasa.gov/citations/19930064238
• Tu, Eugene L., and William R. VanDalsem. 1996. Navier-Stokes Simulation of the Canard-Wing-Body Longitudinal Dynamic Stability Characteristics. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20020041911
• Tudosie, Alexandru Nicolae. 2017a. “Control Laws for an Aircraft Supersonic Inlet with Mobile Panel.” Scientific Research and Education in the AIR Force 19 (1): 231–42. https://doi.org/10.19062/2247-3173.2017.19.1.26
• Tudosie, Alexandru-Nicolae. 2017b. “Pneumo-Hydro-Mechanical Control System for an Aircraft Supersonic Inlet with Mobile Ramp.” Review of the Air Force Academy 15 (1): 123–30. https://doi.org/10.19062/1842-9238.2017.15.1.16
• Tudosie, Alexandru Nicolae. 2018. “Axisymmetric Frontal Supersonic Inlet for Trisonic Aircraft.” Scientific Research and Education in the AIR Force 20: 243–52. https://doi.org/10.19062/2247-3173.2018.20.33
• Tudosie, Alexandru Nicolae, and Mádálina Luciana PĂUnescu. 2017. “Automatic Control System for an Aircraft Plan Supersonic Inlet with Mobile Panel.” Scientific Research and Education in the AIR Force 19 (1): 243–52. https://doi.org/10.19062/2247-3173.2017.19.1.27
• Tudosie, Alexandru-Nicolae, and Vasile Prisacariu. 2022. “Supersonic Air Inlet for a High Velocity Propulsion System.” In Scientific Research and Education in the AIR Force. Publishing House of “Henri Coanda” Air Force Academy. https://doi.org/10.19062/2247-3173.2021.22.19
• Tuling, Sean, Laurent Dala, and Christine Toomer. 2013. “An Engineering Method for Very Low Aspect Ratio Cruciform Wing-Body Configurations.” In 31st AIAA Applied Aerodynamics Conference. AIAA 2013-2823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-2823
• Tuncer, I., and M. Platzer. 1996. “A Computational Study of a Close-Coupled Delta Canard-Wing-Body Configuration.” In 14th Applied Aerodynamics Conference. AIAA 1996-2440. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2440
• Tunik, Yu. V. 2020a. “Actual Schemes of Supersonic Ramjet on Detonation Combustion. Unsteady Detonation Waves.” Physical-Chemical Kinetics in Gas Dynamics 21 (1): 1–12. https://doi.org/10.33257/phchgd.21.1.871
• Tunik, Yu. V. 2020b. “Supersonic Ramjet behind the Aft of the Flying Vehicle.” Physical-Chemical Kinetics in Gas Dynamics 21 (1): 1–16. https://doi.org/10.33257/phchgd.21.1.899
• Tuohy, Seamus. 1998. “An Integrated Vehicle Simulation for the Development and Validation of a Commercial Reusable Launch Vehicle.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 1998-4177. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4177
• “Turbojet and Turbofan Engines for a Mach 3 Supersonic Transport.” 1964. In 1st Annual Meeting. AIAA 1964-244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-244
• “Turbojet Engines.” 2022. In Introduction to Aerospace Flight Vehicles. Embry-Riddle Aeronautical University. https://doi.org/10.15394/eaglepub.2022.1066.n32
• Turenko, Roman, and Sergii Pryhodko. 2024. “Compensation of Temperature Drift of a Ring Laser Gyroscope.” Mechanics of Gyroscopic Systems, no. 48: 91–98. https://doi.org/10.20535/0203-3771482024317966
• Turnbull, W. J., W. K. Boyd, C. R. Foster, J. M. Griffith, and O. B. Ray. 1952. Design of Flexible Airfield Pavements for Multiple-Wheel Landing Gear Assemblies. Report Number 1. Test Section with Lean Clay Subgrade. Defense Technical Information Center. https://doi.org/10.21236/ada319272
• Turner, K. J. 1965. “Free-Flight Model Techniques for Aerodynamic Research at Supersonic and Hypersonic Speeds.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50015-4
• “Turning Flights of Turbojet Aircraft.” 1995. In Flight Performance of Aircraft. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868535.0293.0312
• Tuten, Zacharia, Dylan D. Dooner, Andrew J. Neely, and David Buttsworth. 2025. “Aerothermoelastic Response of a Radiatively Heated Compliant Panel in Mach 6 Flow.” In AIAA SCITECH 2025 Forum. AIAA 2025-2454. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2454
• Tuzhanskyi, Stanislav, and Andrii Sakhno. 2015. “Fiber Optic Gyroscope Based on the Registration of the Spatial Interference Pattern.” In Frontiers in Optics 2015. OSA. https://doi.org/10.1364/fio.2015.jw2a.22
• Tuzlukov, Vyacheslav. 2026. “Guidance on Aircraft and Missile. Trajectory Control Algorithms.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-6
• Twigg, Shannon, Anthony Calise, and Eric Johnson. 2006. “3D Trajectory Optimization for Terrain Following and Terrain Masking.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6102. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6102
• Tyrén, Carl. 1982. “Magnetic Anomalies as a Reference for Ground-Speed and Map-Matching Navigation.” Journal of Navigation 35 (2): 242–54. https://doi.org/10.1017/s0373463300022025
• Udd, E., and R. F. Cahill. 1984. “Fiber-Optic Gyroscope Development.” In Seventh Topical Meeting on Integrated and Guided-Wave Optics. Optica Publishing Group. https://doi.org/10.1364/igwo.1984.wd1
• Udrescu, Radu, and Giuseppe Surace. 1999. “Dynamic Aerothermoelastic Behaviour of Panels under Transient Kinetic Heating Conditions.” In 33rd Thermophysics Conference. AIAA 1999-3562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3562
• Uemura, Masuji. 1960. “Structural Problems at Elevated Temperature in Supersonic Flight.” Transactions of the Japan Society of Mechanical Engineers 26 (170): 1317–19. https://doi.org/10.1299/kikai1938.26.1317
• Ueno, Makoto, Wataru Sarae, Takeshi Tsujimoto, Masaaki Yanagihara, Tomonari Hirotani, and Stephanie Venel. 2004. “Aerodynamic Characteristics Estimation of the High Speed Flight Demonstrator Phase II Using Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4943
• Uhde-Lacovara, J. A. 1986. “CSTAR Star Catalogue Development.” In NASA. Johnson Space Center NASA/American Society for Engineering Educati. https://ntrs.nasa.gov/citations/19860021962
• Uijt de Haag, Maarten, Jacob Campbell, and Frank van Graas. 2005. “Integration of a Synthetic Vision System with Airborne Laser Range Scanner-Based Terrain Referenced Navigation for Precision Approach Guidance.” In SPIE Proceedings, vol. 5802, edited by Jacques G. Verly. SPIE. https://doi.org/10.1117/12.611375
• ul Islam Rizvi, S. Tauqeer, He Linshu, and Xu Dajun. 2015. “Optimal Trajectory Analysis of Hypersonic Boost-Glide Waverider with Heat Load Constraint.” Aircraft Engineering and Aerospace Technology 87 (1): 67–78. https://doi.org/10.1108/aeat-04-2013-0079
• Ulrich, R. 1982. “Polarization and Depolarization in the Fiber-Optic Gyroscope.” In Springer Series in Optical Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-39490-7_4
• Underwood, G. W. 1964. “Transparencies for Supersonic and Hypersonic Flight.” Aircraft Engineering and Aerospace Technology 36 (12): 379–408. https://doi.org/10.1108/eb033956
• Underwood, Amy, and May Win L. Thein. 2013. “Celestial Navigation-Based Controller Design for Extraterrestrial Surface Navigation.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5248
• Unger, Robert. 1966. “THE ‘ASTRAL’ PARTS PROGRAM: A New Dimension for Testing High Reliability Parts for the Saturn V Inertial Guidance System.” In Symposium on Deep Submergence Propulsion and Marine Systems. AIAA 1966-2567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-2567
• Unlu, Halil Utku, Dimitris Chaikalis, Vinicius Gonçalves, and Anthony P. Tzes. 2023. “Control Barrier Functions and Lidar-Inertial Odometry for Safe Drone Navigation in GNSS-Denied Environments.” In IntechOpen eBooks. IntechOpen. https://doi.org/10.5772/intechopen.1002654
• “Unorthodox Landing Gears.” 1988. In Aircraft Landing Gear Design: Principles and Practices. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600861468.0305.0321
• “Unpublished Short-Method Astro-Navigational Tables.” 1994. Journal of Navigation 47 (2): 276–276. https://doi.org/10.1017/s0373463300012200
• Upadhyay, Triveni N., George J. Priovolos, and Harley Rhodehamel. 1990. Autonomous Integrated GPS/INS Navigation Experiment for OMV. Phase 1: Feasibility Study. NASA-CR-4267. NASA. https://ntrs.nasa.gov/citations/19900011653
• Urban, Rick. 1959. Specification for Airborne PCM/FM Telemetry System Components. Defense Technical Information Center. https://doi.org/10.21236/ad0405443
• Urban, Rick. 1963. Specification for Airborne FM/FM Telemetry Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0404648
• Urnes, J., and R. Hess. 1983. “Integrated Flight Control Systems Development: The F/A-18A Automatic Carrier Landing System.” In Guidance and Control Conference. AIAA 1983-2162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2162
• Urnes, J., R. Hess, R. Moomaw, and R. Huff. 1979. “Development of the Navy H-Dot Automatic Carrier Landing System Designed to Give Improved Approach Control in Air Turbulence.” In Guidance and Control Conference. AIAA 1979-1772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1772
• Urschel, Peter, and Timothy Cox. 2003. “Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2003-5544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5544
• Us, N. A., and A. A. Avershin. 2021. “High-Q Optical Design for a Laser-Diode-Based Packaged Ring Laser Gyroscope.” Journal of Optical Technology 88 (7): 372. https://doi.org/10.1364/jot.88.000372
• Uselton, Bob L. 1976. A Wind Tunnel Investigation of Impulse Effects on the Motion of an Impulse Correction Guidance Missile. Defense Technical Information Center. https://doi.org/10.21236/ada024210
• Uspenskyi, Valerii, Ivan Bagmut, and Mariia Nekrasova. 2018. “Development of Method and Algorithm of Dynamic Gyrocompassing for High­speed Systems of Navigation and Control of Movement.” Eastern-European Journal of Enterprise Technologies 1 (9 (91)): 72–29. https://doi.org/10.15587/1729-4061.2018.119735
• Usui, Ryuji. 1999. “Development of the Small Size 3-Axis Fiber Optic Gyroscope.” In 13th International Conference on Optical Fiber Sensors. SPIE. https://doi.org/10.1117/12.2302019
• Utomo, Muhammad Adnan, and Romie Oktavianus Bura. 2019. “Design of Inward-Turning External Compression Supersonic Inlet for Supersonic Transport Aircraft.” INSIST 2 (2): 104. https://doi.org/10.23960/ins.v2i2.90
• Vadillo, Jose, and Ramesh Agarwal. 2007. “Numerical Study of Transonic Drag Reduction for Flow past Airfoils Using Active Flow Control.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-712
• Vadillo, Jose, and Ramesh K. Agarwal. 2009. “Numerical Study of Transonic Drag Reduction for Flow past Airfoils Using Active Flow Control.” In Computational Fluid Dynamics 2006. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-92779-2_91
• Vaglio-Laurin, Roberto, and Reinald G. Finke. 1965. “Reusable Space Launch Vehicle Concepts: Outlook 1965.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/650801
• Vaispacher, Tomáš, Róbert Bréda, and František Adamčík. 2015. “Error Analysis of Inertial Navigation Systems Using Test Algorithms.” Naše more 62 (3): 204–8. https://doi.org/10.17818/nm/2015/si21
• Vaiuso, Andrea, Gabriele Immordino, Marcello Righi, and Andrea Da Ronch. 2025. “Multi-Fidelity Bayesian Neural Network for Uncertainty Quantification in Transonic Aerodynamic Loads.” Preprint, . https://doi.org/10.2139/ssrn.5084491
• Vajda, S. 1987. “Identifiability of Polynomial Systems: Structural and Numerical Aspects.” In Identifiability of Parametric Models. Elsevier. https://doi.org/10.1016/b978-0-08-034929-9.50008-x
• Vallot, Lawrence, Scott Snyder, Brian Schipper, Nigel Parker, and Cary Spitzer. 1991. “Design and Flight Test of a Differential GPS/inertial Navigation System for Approach/landing Guidance.” In National Technical Meeting. https://ntrs.nasa.gov/citations/19920034026
• Van Allen, James A. 1981. “An Analytical Solution of the Two Star Sight Problem of Celestial Navigation.” Navigation 28 (1): 40–43. https://doi.org/10.1002/j.2161-4296.1981.tb01441.x
• Van Bavel, Luc. 2014. “A Takeoff Rotation Model Including Pilot Technique Parameters for Flight Test Data Reduction and Expansion.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2059. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2059
• van Bezooijen, R. W. H. 1990. “A Star Pattern Recognition Algorithm for Autonomous Attitude Determination.” In Automatic Control in Aerospace 1989. Elsevier. https://doi.org/10.1016/b978-0-08-037027-9.50011-2
• van Bezooijen, R. W. H. 1993. “Autonomous Star Tracker Development.” In Automatic Control in Aerospace 1992. Elsevier. https://doi.org/10.1016/b978-0-08-041715-8.50075-4
• van Bezooijen, Roelof W. H. 2003. “SIRTF Autonomous Star Tracker.” In SPIE Proceedings, vol. 4850, edited by John C. Mather. SPIE. https://doi.org/10.1117/12.461606
• Van den Borre, Karel, Bayindir H. Saracoglu, and Axel Coussement. 2023. “Numerical Modelling of Hydrogen Combustion Phenomena in a Dual-Mode Ramjet Engine with Cavity Flameholder.” In AIAA SCITECH 2023 Forum. AIAA 2023-0499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0499
• van den Hout, Franklin, and Jo Koullen. 1996. “The Design, Manufacture and Successful Operation of a Very Small Turbojet Engine.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/96-gt-456
• van der Ploeg, Geart. 2026. “A Sub-Arcsecond, Ultra-Low-SWaP Star Tracker for Small Satellite Attitude Determination.” In Space Telescopes and Instrumentation 2026: Optical, Infrared, and Millimeter Wave, edited by Laura E. Coyle, Marshall D. Perrin, Shuji Matsuura. SPIE. https://doi.org/10.1117/12.3103583
• Van Der Vooren, J., and A. Van Der Wees. 1990. “Inviscid Drag Prediction for Transonic Transport Wings Using a Full-Potential Method.” In 28th Aerospace Sciences Meeting. AIAA 1990-576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-576
• van Dommelen, Dennis, Adam D’Silva, and Willem A. Anemaat. 2019. “Comparison of Methods to Predict Aerodynamic Center Shift Due to Bodies.” In AIAA Aviation 2019 Forum. AIAA 2019-3569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3569
• Van Eykeren, Laurens, and Q. Ping Chu. 2013. “Fault Detection and Isolation for Inertial Reference Units.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4697. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4697
• van Slagmaat, M. T. P. 2026. “Tire Models in Aircraft Landing Gear Simulation.” In Tyre Models for Vehicle Dynamics Analysis. CRC Press. https://doi.org/10.1201/9781003760634-9
• Vandenberghe, Alexander. 2024. Sagitta to Scorpio: Evolution of a New Space Star Tracker to Space-Qualified Component. https://doi.org/10.52202/078365-0181
• Vanderwerf, Kevin, and Knut Wefald. 1988. “Fault Tolerant Inertial Navigation System.” In Digital Avionics Systems Conference. AIAA 1988-4024. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4024
• VanderWyst, Anton. 2008. “Extracting Accurate Supersonic Flight Data for a Rotating Hemisphere with Offset Pitot Tubes.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6583
• Vargas Venegas, Carlos A., and Daning Huang. 2021. “Expedient Hypersonic Aerothermal Prediction for Aerothermoelastic Analysis via Field Inversion and Machine Learning.” In AIAA Scitech 2021 Forum. AIAA 2021-1707. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1707
• Vargas Venegas, Carlos A., and Daning Huang. 2022. “Physics-Infused Reduced Order Modeling of Hypersonic Aerothermal Loads for Aerothermoelastic Analysis.” In AIAA SCITECH 2022 Forum. AIAA 2022-0989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0989
• Vargas-Jimenez, Javier A., and Roelof Vos. 2016. “Development of a Wave Drag Prediction Method for the Conceptual Design Phase.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1279
• Vārna, Inese, Ansis Zariņš, and Augusts Rubāns. 2023. Digital Zenith Camera VESTA and Vertical Deflection Test Site Measurement Results. https://doi.org/10.5194/egusphere-egu23-1965
• Vasconcelos, J., P. Oliveira, and Carlos Silvestre. 2005. “Inertial Navigation System Aided by GPS and Selective Frequency Contents of Vector Measurements.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6057
• Vasconcelos, Jose, Carlos Silvestre, and Paulo Oliveira. 2006. “Embedded Vehicle Dynamics and LASER Aiding Techniques for Inertial Navigation Systems.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6581
• Vasilyuk, N. N. 2024. “Star Tracker Error Model Taking into Account the Calibration Errors of Intrinsic Parameters of the Digital Camera.” Gyroscopy and Navigation 15 (1): 37–49. https://doi.org/10.1134/s2075108724700160
• Vasyliev, V. M., V. O. Rogozhyn, and B. I. Dolintse. 2015. “Accuracy Analysis of Inertial-Satellite Navigation System Integrated with Using Corrective Circuits.” Electronics and Control Systems 4 (46). https://doi.org/10.18372/1990-5548.46.9930
• Vathsal, S. 1994. “Estimation of Circular Error Probability of Strapped down Inertial Navigation System by Propagation of Error Covariance Matrix.” Defence Science Journal 44 (1): 25–32. https://doi.org/10.14429/dsj.44.4148
• Vau, Bernard, Mehdi Bussutil, Joachin Honthaas, and Colin Stevens. 2021. “A Testbench with Increased Accuracy for the Calibration of Inertial Navigation Systems and Inertial Sensors.” In The International Technical Meeting of the The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2021.17865
• Vaughn, Ronald S. 1966. “Estimating Aircraft Inertial Navigator Performance.” Navigation 13 (4): 348–53. https://doi.org/10.1002/j.2161-4296.1966.tb02180.x
• Vaughn, Milton. 2002. “Practical Viscous Computations for a Spinning, Canard-Controlled Missile with the WIND Code.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2803
• Vaughn, Milton. 2006. “An Application of Vorticity Confinement to Missile Aerodynamic Design.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3866
• Vavdiya, Jay, and Vishal Kaushik. 2022. “A Critical Study on Missile and Missile Guidance.” Graduate Research in Engineering and Technology: 37–40. https://doi.org/10.47893/gret.2022.1131
• Vdoviak, J. W., and J. A. Ebacher. 1980. “VCE Test Bed Engine for Supersonic Cruise Research.” In NASA. Langley Research Center Supersonic Cruise Res. 1979, Pt. 1. https://ntrs.nasa.gov/citations/19810009472
• Veletas, Mihalis. 2026. “XB-1 Supersonic Demonstrator: Development and Flight Testing from a Flight Analysis Perspective.” In AIAA SCITECH 2026 Forum. AIAA 2026-2636. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2636
• Velikanova, E. P., A. A. Geltser, Zh. T. Erdyneev, and N. V. Panokin. 2017. “Analysis of Accuracy Requirements for an Inertial Navigation System in Synthetic Aperture Radars.” Gyroscopy and Navigation 8 (2): 129–35. https://doi.org/10.1134/s2075108717020110
• Vepa, Ranjan, and Amzari Zhahir. 2010. “High-Precision Kinematic Satellite and Doppler Aided Inertial Navigation System.” Journal of Navigation 64 (1): 91–108. https://doi.org/10.1017/s0373463310000329
• Verhoff, A., D. C. Stookesberry, B. M. Hopping, and T. R. Michal. 1990. “Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations.” In Numerical and Physical Aspects of Aerodynamic Flows IV. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-02643-4_12
• “The Verification of Inlet/engine Distortion Compatibility.” 1988. In 24th Joint Propulsion Conference. AIAA 1988-3267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-3267
• Verma, Hari O., and Nk Peyada. 2018. “Parameter Estimation of Stable and Unstable Aircraft Using Extreme Learning Machine.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0526. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0526
• Vidimlic, Najda, Alexandra Levin, Mohammad Loni, and Masoud Daneshtalab. 2021. “Image Synthesisation and Data Augmentation for Safe Object Detection in Aircraft Auto-Landing System.” In International Joint Conference on Computer Vision, Imaging and Computer Graphics Theory and Applications (VISIGRAPP). https://doi.org/10.5220/0010248801230135
• Vikas, Vishesh, and Carl D. Crane. 2014. “Gyroscope-Free Link Parameter Measurement Using Accelerometers and Magnetometer.” In Volume 5B: 38th Mechanisms and Robotics Conference. American Society of Mechanical Engineers. https://doi.org/10.1115/detc2014-35360
• Vimal, A., J. Sannut Nicholas, R. Navin, K. Prithiv Raj, and P. Kiruba. 2025. “Ring Laser Gyroscope Technology: A Review of Precision Navigation and Sensing Applications.” Journal of Physics: Conference Series 3045 (1): 012016. https://doi.org/10.1088/1742-6596/3045/1/012016
• Vinh, Nguyen, Pierre Kabamba, and Tetsuya Takehira. 1998. “Optimal Interception of a Maneuvering Long Range Missile.” In AIAA/AAS Astrodynamics Specialist Conference and Exhibit. AIAA 1998-4547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4547
• Vinícius M. G. B. Cavalcanti, Felipe O. Silva, Álvaro H. A. Maia, Danilo A. de Lima, Alexandre C. Leite, and Jay A. Farrell. 2023. “Evolutionary Optimization for Tuning Barometer-Aided Inertial Navigation System Vertical Channel Mechanization.” In Proceedings do Simpósio Brasileiro de Sistemas Elétricos. SBA Sociedade Brasileira de Automática. https://doi.org/10.20906/sbai-sbse-2023/3930
• Vinogradov, Viacheslav, and Vladimir Stepanov. 2008. “Scheme and Inlet Performance of Supersonic Business Aircraft.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-4585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4585
• Vinogradova, E. P., D. F. Vinogradov, A. V. Zhmurin, and O. I. Sauta. 2025. “Method for Correcting Barometric Altimeter Readings in Autonomous Navigation Systems.” Achievements of Modern Radioelectronics: 41–45. https://doi.org/10.18127/j20700784-202508-04
• “Visual Analysis of Strapdown Inertial Navigation Information Model.” 2023. International Journal of Science and Engineering Applications. https://doi.org/10.7753/ijsea1207.1045
• Viswanath, Anjitha, K. K. Santhakumari, Bindu John, and T. Sivasankar. 2022. “Self-Alignment Algorithm for Ring Laser Optical Sensor Based Strapdown Inertial Navigation Systems.” ECS Transactions 107 (1): 17085–92. https://doi.org/10.1149/10701.17085ecst
• Vitale, A. James. 1953. Effects of Wing Elasticity on the Aerodynamic Characteristics of an Airplane Configuration Having 45 Degrees Sweptback Wings as Obtained from Free-Flight Rocket-Model Tests at Transonic Speeds. NACA-RM-L52L30. NASA. https://ntrs.nasa.gov/citations/19930087446
• Vogel, K., H. Risken, and W. Schleich. 1989. “Noise in a Ring-Laser Gyroscope.” In Noise in Nonlinear Dynamical Systems. Cambridge University Press. https://doi.org/10.1017/cbo9780511897825.013
• Vogel, Anja, and Sven Schmitz. 2025. “Extraction of Induced and Wave Drag from CFD Solutions.” In 2025 Regional Student Conferences. AIAA 2025-97647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-97647
• Volkov, Konstantin. 2023a. “High-Temperature Effects on Supersonic Flow around a Wedge.” In IntechOpen eBooks. IntechOpen. https://doi.org/10.5772/intechopen.109268
• Volkov, D. Yu., and K. V. Galunova. 2018. “On Bifurcation in Dynamics of Hemispherical Resonator Gyroscope.” In AIP Conference Proceedings, vol. 1959. Author(s). https://doi.org/10.1063/1.5034603
• Volskii, V. A., G. N. Maltsev, and E. V. Chernyavskii. 2013. “On the Use of Error-Correction Coding in Radio Command Control Systems.” Telecommunications and Radio Engineering 72 (13): 1199–1207. https://doi.org/10.1615/telecomradeng.v72.i13.60
• von Huelsen, Leonardo. 2024. “Trajectory Reconstruction through Curvature Analysis from Inertial and Global Navigation Satellite System Measurements for Vehicle Navigation.” PhD diss.. https://doi.org/10.47749/t/unicamp.2024.1455904
• Vorchik, B. G. 1987. “Identifiability of Linear and Nonlinear Parametric Stochastic Systems.” In Stochastic Control. Elsevier. https://doi.org/10.1016/b978-0-08-033452-3.50022-3
• “Vortical Flow Topology on Windward and Leeward Side of Delta Wing at Supersonic Speed.” 2009. Journal of Applied Fluid Mechanics 2 (02). https://doi.org/10.36884/jafm.2.02.11860
• Vosteen, L. F. 1960. Aerodynamic Heating Tests of Missile Stabilizers in a Free Jet at Mach Number 2. NASA-TM-X-299. NASA. https://ntrs.nasa.gov/citations/19630004025
• Vovchenko, N. Ya. 1966. On the Calculation of an Inertial Navigation System. NASA-TM-X-59482. NASA. https://ntrs.nasa.gov/citations/19670014147
• Vu, Thuan Duc, Hiep Duc Nguyen, Chinh D. Hoang, and Ban D. Nguyen. 2019. “Developing a Control Architecture for Highly Accurate Multi-Axis Inertial Stabilized Platform.” In Electro-Optical and Infrared Systems: Technology and Applications XVI, edited by Duncan L. Hickman, Helge Bürsing. SPIE. https://doi.org/10.1117/12.2531943
• Vukmirica, Vladimir, Ivana Trajkovski, Nada Asanović, and Adrijana Jovanović. 2024. “Azimuth Angle Error Depending of the Inertial Navigation System Mounting Error.” In 11th International Scientific Conference on Defensive Technologies - OTEX 2024 - zbornik radova. Military Technical Institute, Belgrade. https://doi.org/10.5937/oteh24054v
• Vulfovich, Boris, and Vasily Fogilev. 2010. “New Ideas for Celestial Navigation in the Third Millennium.” Journal of Navigation 63 (2): 373–78. https://doi.org/10.1017/s0373463309990348
• Waddell, M. C. 1961. Surface-to-Air Guided Missile Systems Methods of Tactical Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0258634
• Waddington, Michael Jon. n.d. “Development of an Interactive Wave Drag Capability for the OpenVSP Parametric Geometry Tool.” PhD diss., California Polytechnic State University. https://doi.org/10.15368/theses.2015.126
• Wagdi, M. 1984. “An Active Control System for Aircraft during Landing Approach in Wind Shear.” In 22nd Aerospace Sciences Meeting. AIAA 1984-239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-239
• Wagner, Justin, Agustin Valdivia, Kemal Yuceil, Noel Clemens, and David Dolling. 2007. “An Experimental Investigation of Supersonic Inlet Unstart.” In 37th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2007-4352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4352
• Wagner, Justin, Kemal Yuceil, and Noel Clemens. 2009b. “PIV Measurements of Unstart of an Inlet-Isolator Model in a Mach 5 Flow.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-4209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-4209
• Wagner, Justin, Kemal Yuceil, Agustin Valdivia, Noel Clemens, and David Dolling. 2008. “PIV Measurements of the Unstart Process in a Supersonic Inlet/Isolator.” In 38th Fluid Dynamics Conference and Exhibit. AIAA 2008-3849. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-3849
• Waidmann, Winfried, Uwe Brummund, and Joachim Nuding. 2024. “Experimental Investigation of Supersonic Ramjet Combustion (Scramjet).” In Transport Phenomena In Combustion. Routledge. https://doi.org/10.1201/9780203735138-143
• Waldman, R. H. 1968. “Long Range Navigation Techniques for the Supersonic Transport.” Navigation 15 (2): 194–98. https://doi.org/10.1002/j.2161-4296.1968.tb01605.x
• Waldman, R. H. 1969. “Commercial Navigation Systems for Long-Range Subsonic Transports in the 1970’s.” Journal of Navigation 22 (4): 479–511. https://doi.org/10.1017/s0373463300042430
• Walker, J. H. 1949. “Rocket and Ramjet Supersonic Powerplants.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/490123
• Walker, James H. 1952. Ramjet Technology. Chapter 3. Engine Requirements for Supersonic Flight. Defense Technical Information Center. https://doi.org/10.21236/ad0041745
• Walker, J. M. 1960. “Fully Automatic Aircraft Landing Approach.” Students Quarterly Journal 31 (121): 11. https://doi.org/10.1049/sqj.1960.0043
• Walker, J. M. 1961. “Fully Automatic Aircraft-Landing Approach.” Journal of the Institution of Electrical Engineers 7 (74): 108–10. https://doi.org/10.1049/jiee-3.1961.0061
• Walker, Gary F. 1970. Counting Accelerometers (an Error Analysis). Defense Technical Information Center. https://doi.org/10.21236/ad0717151
• Walker, Darrell Winterton. 1973. “Navy Development of Low-Cost Supersonic Turbojet Engines.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/730362
• Walker, K., and W. Engelke. 1990. Engineering Support for Inertial Measurement Unit Development. Defense Technical Information Center. https://doi.org/10.21236/ada246805
• Walkley, K. 1986. “Wave Drag Analysis of Realistic Fighter Aircraft Using a Full Potential Method.” In Aircraft Systems, Design and Technology Meeting. AIAA 1986-2627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2627
• Walkley, K. B., and G. L. Martin. 1979. Aerodynamic Design and Analysis of the AST-200 Supersonic Transport Configuration Concept. NASA-CR-159051. NASA. https://ntrs.nasa.gov/citations/19790013875
• Wallace, J., J. Olds, A. Charania, and G. Woodcock. 2003. “A Study of ARTS: A Dual-Fuel Reusable Launch Vehicle (RLV) with Launch Assist.” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2003-5269. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5269
• Wallhagen, R. E., F. J. Paulovich, and L. C. Geyser. 1972. Dynamics of a Supersonic Inlet-Engine Combination Subjected to Disturbances in Fuel Flow and Inlet Overboard Bypass Airflow. NASA-TM-X-2558. NASA. https://ntrs.nasa.gov/citations/19720016187
• Wallskog, Harvey A. 1954a. Free-Flight Zero-Lift Drag Results from a 1/5-Scale Model and Several Small-Scale Equivalent Bodies of Revolution of the Convair F-102 Configuration at Mach Numbers up to 1.34. NACA-RM-SL54DO9b. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023601
• Wallskog, Harvey A. 1954b. Summary of Free-Flight Zero-Lift Drag Results from Tests of 1/5-Scale Models of the Convair YF-102 and F-102A Airplanes and Several Related Small Equivalent Bodies at Mach Numbers from 0.70 to 1.46. NACA-RM-SL54J25. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090022754
• Walsh, P. 1998. “The Use of Inertial Measurement Units as a Primary Sensor for a Flight Control System.” In IEE Airborne Navigation Systems Workshop, vol. 1998. IEE. https://doi.org/10.1049/ic:19980391
• Walsh, T., and R. Wartburg. 1978. “Ballistic Missile Sizing and Optimizing.” In 14th Joint Propulsion Conference. AIAA 1978-1019. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1019
• Walsh, T. M., and E. F. Weener. 1977. “Automatic Flight Performance of a Transport Airplane on Complex Microwave Landing System Paths.” In AGARD. https://ntrs.nasa.gov/citations/19780034890
• Walsh, T. M., and E. F. Weener. 1978. “Automatic Flight Performance of a Transport Airplane on Complex Microwave Landing System Paths.” In AGARD Guidance and Control Design Considerations for Low-Altitude and Terminal-Area Flight. https://ntrs.nasa.gov/citations/19780018123
• Walter, Leif, Gunther Schlöffel, and Florian Holzapfel. 2013. “Optimal Control Framework for Impulsive Missile Interception Guidance.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4787. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4787
• Walter, Sibylle F., and Ryan P. Starkey. 2016. “Interpolation Methods for Inlet Distortion Determination.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0531
• Walters, Richard E. 1954. Application of Transonic Area Rule to a Sharp-Lipped Ducted Nacelle. NACA-RM-L53J09b. NASA. https://ntrs.nasa.gov/citations/19930087981
• Walters, Brian D. 1959. Development of XM5E2 and XM10 Guided Missile Warheads. Defense Technical Information Center. https://doi.org/10.21236/ad0303146
• Walton, A. M. 1995. “Space Based Radar Tracking Filter.” In IEE Colloquium on `Algorithms for Target Tracking’, vol. 1995. IEE. https://doi.org/10.1049/ic:19950675
• Waltrup, P., F. Billig, and M. Evans. 1980. “Critical Considerations in the Design of Supersonic Combustion Ramjet /Scramjet/ Engines.” In 16th Joint Propulsion Conference. AIAA 1980-1284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1284
• Wan, Quan, Fang Chen, Dacheng Xu, Shuwen Guo, and Xinxin Li. 2019. “Enhancing the Closed-Loop Stability of a High-Q Polysilicon Micro-Hemispherical Resonating Gyroscope.” AIP Advances 9 (2): 025211. https://doi.org/10.1063/1.5045360
• Wan, Shuangai, Jian Cheng Fang, and Yao Chen. 2012. “Drift Error Analysis of Atomic Spin Gyroscope.” Applied Mechanics and Materials 241-244: 488–93. https://doi.org/10.4028/www.scientific.net/amm.241-244.488
• Wan, Xiaoyun, and Jinhai Yu. 2014. “Navigation Using Invariants of Gravity Vectors and Gravity Gradients.” In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-54740-9_42
• Wanchai, Jiajan. n.d. “Studies of Aerodynamics of Supersonic Generic Round Shaped Bodies.” PhD diss., Nanyang Technological University. https://doi.org/10.32657/10356/58905
• Wang, Teng. n.d. “Augmented UAS Navigation in GPS Denied Terrain Environments Using Synthetic Vision.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/etd-180810-5462
• Wang, Kai Yuen. 1979. Modeling and Error Analysis of a Superconducting Gravity Gradiometer. Defense Technical Information Center. https://doi.org/10.21236/ada082535
• Wang, Yan M. 1988. Determination of the Gravity Disturbance on the Earth’s Topographic Surface from Airborne Gravity Gradient Data. Defense Technical Information Center. https://doi.org/10.21236/ada214596
• Wang, Shih-Ho. 1998. Bandwidth Efficient Aeronautical Telemetry Modem and Transceiver Research. Defense Technical Information Center. https://doi.org/10.21236/ada387033
• Wang, Fenglin. 2019a. “Error Analysis for the Rate Azimuth Platform INS.” Journal of Physics: Conference Series 1311 (1): 012042. https://doi.org/10.1088/1742-6596/1311/1/012042
• Wang, Zhenbo. 2019b. “Maximum-Normal-Load Entry Trajectory Optimization for Hypersonic Glide Vehicles.” In AIAA Scitech 2019 Forum. AIAA 2019-0262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0262
• Wang, Junli. 2019c. “Transonic Static Aeroelastic and Longitudinal Aerodynamic Characteristics of a Low-Aspect-Ratio Swept Wing.” AIP Advances 9 (4): 045203. https://doi.org/10.1063/1.5087963
• Wang, Y. 2022. “Analysis of Emergency Landing Load of Civil Aircraft with Single Main Landing Gear Extended Landing.” IET Conference Proceedings 2022 (7): 336–39. https://doi.org/10.1049/icp.2022.1550
• Wang, Wei. 2025. “Adaptive Transformed Cubature Kalman Filter and Its Application in Initial Alignment of Strapdown Inertial Navigation System.” Physica Scripta 100 (6): 066001. https://doi.org/10.1088/1402-4896/add194
• Wang, Tianfu, and Samuel F. Asokanthan. 2005. “Dynamic Stability of a Single-Axis Vibratory MEMS Gyroscope.” In Volume 1: 20th Biennial Conference on Mechanical Vibration and Noise, Parts A, B, and C. ASMEDC. https://doi.org/10.1115/detc2005-85090
• Wang, Bo, and Tijing Cai. 2023. “Path Planning Method for Underwater Gravity-Aided Inertial Navigation Based on PCRB.” Preprint, . https://doi.org/10.20944/preprints202304.0076.v1
• Wang, Xinwang, and Huiliang Cao. 2020. “Temperature Drift Modeling and Compensation of Micro-Electro-Mechanical System Gyroscope Based on Improved Support Vector Machine Algorithms.” International Journal of Distributed Sensor Networks 16 (3): 155014772090819. https://doi.org/10.1177/1550147720908195
• Wang, Xingang, and Hongjun Cao. 2026. “Dynamics of the Aircraft Nose Landing Gear with Two Time Delays.” Journal of Applied Nonlinear Dynamics 16 (1): 187–210. https://doi.org/10.5890/jand.2027.03.010
• Wang, Xichen, Huiliang Cao, and Xiaomin Duan. 2021e. “Crow Search Algorithm for MEMS Gyroscope Temperature Drift Signal and Processing for Denoising.” Shock and Vibration 2021 (1): 9929966. https://doi.org/10.1155/2021/9929966
• Wang, Jiang, Chengyu Cao, Naira Hovakimyan, Richard Hindman, and D. Brett Ridgely. 2008. “L1 Adaptive Controller for a Missile Longitudinal Autopilot Design.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6282
• Wang, Ximing, and Udo Carl. 1999. “Fuzzy Control of Aircraft Semi-Active Landing Gear System.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-265
• Wang, Zhonglin, Jingjing Chen, and Yong Chen. 2017e. “Inlet Compatibility and Fan Aeromechanics of HBP Turbofan Engine.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2017-63427
• Wang, Yifan, Haoying Chen, Xuankai Liu, and Haibo Zhang. 2025h. “Mode Decision Control Method for Adaptive Cycle Engine Based on Inlet and Engine Matching.” International Journal of Aeronautical and Space Sciences 27 (3): 2028–53. https://doi.org/10.1007/s42405-025-01072-9
• Wang, Jiachen, Pu Chen, Zhiqiang Yao, Yi Zhang, and Fan Bai. 2026m. “Temperature Influence Analysis and Compensation Method of Hemisphere Resonator Gyroscope.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2026-99-0514
• Wang, Xinwang, Ying Cui, Xin Zhang, and Huiliang Cao. 2025m. “A Temperature Compensation Method for MEMS Disk Solid Wave Gyroscope Based on SSA-VMD and RF-GSO-GRU Algorithm.” Sensor Review 45 (5): 721–37. https://doi.org/10.1108/sr-03-2025-0166
• Wang, Cong, Chaolei Dang, Chan Ha, Jiang Qin, and Hongyan Huang. 2021l. “Thermodynamic Analysis for a Novel Steam Rankine Cycle Based Indirect Chemical Precooled Engine Used for Supersonic Flight.” Preprint, . https://doi.org/10.2139/ssrn.3980387
• Wang, Zhi Gang, and Yifan Deng. 2013. “High Accuracy Attitude Estimation for Spacecraft Using Quaternion Star Sensors and Gyros.” Applied Mechanics and Materials 427-429: 1544–47. https://doi.org/10.4028/www.scientific.net/amm.427-429.1544
• Wang, Yu, Zhihong Deng, and Wenzhe Zhang. 2025d. “A Gravity-Aided Navigation Matching Area Selection Algorithm Based on Triangulation.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2200-9_55
• Wang, Wen-jun, Xiao-jun Duan, and Ju-bo Zhu. 2013c. “Impact Analysis of Guidance Instrument Error Separation Accuracy on Sampling Rate of Inertial Navigation Equipment.” In Proceedings of the 2nd International Conference On Systems Engineering and Modeling. Atlantis Press. https://doi.org/10.2991/icsem.2013.22
• Wang, Xuezhi, Christopher Gilliam, Allison Kealy, John Close, and Bill Moran. 2023j. “Probabilistic Map Matching for Robust Inertial Navigation Aiding.” NAVIGATION: Journal of the Institute of Navigation 70 (2): navi.583. https://doi.org/10.33012/navi.583
• Wang, Haoning, Jie Guo, Baochao Zhang, Ziyao Wang, Xiang Li, and Shengjing Tang. 2025g. “Learning-Based Guidance Method of Avoiding Multiple Online-Detected No-Fly Zones for Hypersonic Cruise Vehicles.” Journal of Aerospace Engineering 38 (1): 04024107. https://doi.org/10.1061/jaeeez.aseng-5746
• Wang, Xiting, Ai He, Zhongzhi Hu, and Jincen Jiang. 2024a. “An Adaptive Modeling Method of Hydrogen-Fueled Turbojet Engine.” In AIAA SCITECH 2024 Forum. AIAA 2024-0521. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0521
• Wang, Kaiqiang, Yanze Hou, and Chong Chen. 2018d. “Influence of the Earth Rotation on Trajectory of a Returnable Hypersonic Cruise Vehicle.” IOP Conference Series: Materials Science and Engineering 449: 012006. https://doi.org/10.1088/1757-899x/449/1/012006
• Wang, Zhen, Jie Jiang, and Guangjun Zhang. 2019g. “Observation Angular Distance Error Modeling and Matching Threshold Optimization for Terrestrial Star Tracker.” Optics Express 27 (23): 33518. https://doi.org/10.1364/oe.27.033518
• Wang, Zhongjun, Edward Lan, and Jay Brandon. 2002. “Estimation of Lateral-Directional Unsteady Aerodynamic Models from Flight Test Data.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2002-4626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4626
• Wang, Lingcao, Kui Li, Yuanpei Chen, Juncheng Liu, and Yanchun Xu. 2017k. “Single-Axis Rotation/azimuth-Motion Insulation Inertial Navigation Control System with FOGs.” Optics Express 25 (25): 30956. https://doi.org/10.1364/oe.25.030956
• Wang, Dayi, Maodeng Li, Xiangyu Huang, and Xiaowen Zhang. 2020a. “Altimeter and Velocimeter-/Optical-Aided Inertial Navigation Technology.” In Space Science and Technologies. Springer Singapore. https://doi.org/10.1007/978-981-15-4879-6_10
• Wang, Hailiang, Guozhang Li, and Zhiyong Shi. 2017i. “Overview of Initial Alignment Method for Strap down Inertial Navigation System.” In Proceedings of the Advances in Materials, Machinery, Electrical Engineering (AMMEE 2017). Atlantis Press. https://doi.org/10.2991/ammee-17.2017.30
• Wang, Lingcao, Kui Li, Lei Wang, and Jiaxin Gao. 2017d. “Identifying Z-Axis Gyro Drift and Scale Factor Error Using Azimuth Measurement in Fiber Optic Gyroscope Single-Axis Rotation Inertial Navigation System.” Optical Engineering 56 (02): 1–10. https://doi.org/10.1117/1.oe.56.2.024102
• Wang, Zhipeng, Xin Li, Yanbo Zhu, Qiang Li, and Kun Fang. 2021i. “Integrity Monitoring of Global Navigation Satellite System/Inertial Navigation System Integrated Navigation System Based on Dynamic Fading Filter Optimisation.” IET Radar, Sonar & Navigation 16 (3): 515–30. https://doi.org/10.1049/rsn2.12199
• Wang, Hao Peng, and Ze Qian Liu. 2013. “Research on Searching Guidance of TV Guided Missile.” Applied Mechanics and Materials 404: 609–17. https://doi.org/10.4028/www.scientific.net/amm.404.609
• Wang, Zejin, Bohan Liu, Wei Luo, et al. 2021b. “Bias Instability of Additional Modulation from Interaxial Electromagnetic Interference in Multi-Axis Fiber Optical Gyroscope.” In AOPC 2021: Optical Sensing and Imaging Technology, edited by Yadong Jiang, Qunbo Lv, Bin Xue, Dengwei Zhang, Dong Liu. SPIE. https://doi.org/10.1117/12.2606930
• Wang, Yunshu, Jianye Liu, Jinling Wang, Qinghua Zeng, Xuesong Shen, and Yueyuan Zhang. 2019e. “Micro Aerial Vehicle Navigation with Visual-Inertial Integration Aided by Structured Light.” Journal of Navigation 73 (1): 16–36. https://doi.org/10.1017/s0373463319000511
• Wang, Yueze, Lin Ma, Hao Yu, Hongyu Gao, and Yujie Yuan. 2016d. “Modeling and Simulation on Temperature Performance in Fiber Optic Gyroscope Fiber Coil of Shipborne Strapdown Inertial Navigation System.” In SPIE Proceedings, vol. 10158. SPIE. https://doi.org/10.1117/12.2246797
• Wang, Liang, Ke Peng, Weihua Zhang, and Donghui Wang. 2018g. “Neural Extended State Observer Based Command Filtered Back-Stepping Hypersonic Vehicle Integrated Guidance and Autopilot.” Preprint, . https://doi.org/10.20944/preprints201805.0220.v1
• Wang, Xing, Lin Hua Piao, and Quan Gang Yu. 2012c. “Research on Nozzle Array Structure Fluidic Gyroscope Sensitivity-Temperature Compensation.” Advanced materials research 542-543: 806–9. https://doi.org/10.4028/www.scientific.net/amr.542-543.806
• Wang, Xing, Lin Hua Piao, and Quan Gang Yu. 2012d. “Research on Nozzle Array Structure Fluidic Gyroscope Zero Temperature Compensation.” Advanced materials research 542-543: 631–34. https://doi.org/10.4028/www.scientific.net/amr.542-543.631
• Wang, Lei, and Zai Kang Qi. 2013. “Design and Analysis of Nonlinear Autopilot for Tactical Missile.” Applied Mechanics and Materials 313-314: 1139–43. https://doi.org/10.4028/www.scientific.net/amm.313-314.1139
• Wang, Xiaogang, Wutao Qin, Yuliang Bai, and Naigang Cui. 2017l. “Trajectory Estimation for Ballistic Missile in Boost Stage Using Robust Filtering.” IET Radar, Sonar & Navigation 11 (3): 513–19. https://doi.org/10.1049/iet-rsn.2016.0335
• Wang, Cong, Jiang Qin, and Hongyan Huang. 2022o. “Thermodynamic Analysis for a Novel Chemical Precooling Turbojet Engine Based on a Multi-Stage Precooling-Compression Cycle.” Preprint, . https://doi.org/10.2139/ssrn.4102737
• Wang, Boning, Wei Shao, Hanxue Zhao, Lingfei Dou, and Wenlong Yao. 2020d. “A Celestial Navigation Approach Based on Star Pattern Recognition.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8458-9_36
• Wang, Chen, Ximing Sun, and Xian Du. 2023f. “Installed Performance Seeking Control Based on Supersonic Variable Inlet/engine Coupling Model.” International Journal of Turbo & Jet-Engines 41 (2): 189–200. https://doi.org/10.1515/tjj-2023-0030
• Wang, Lihui, Feng Rui Sun, Gang Wang, and Gang Liu. 2010b. “Study on the Drift of Modulated Phase in Interference Fiber Optic Gyroscope.” Journal of Computers 5 (3). https://doi.org/10.4304/jcp.5.3.394-400
• Wang, Hong, Chuangming Tong, and Jia Sun. 2013g. “Study on the Trajectory Simulation of the Ballistic Missile.” Applied Mechanics and Materials 416-417: 1845–50. https://doi.org/10.4028/www.scientific.net/amm.416-417.1845
• Wang, Bo, and Yu Wang. 2009. “Design of Missile Autopilot Considering Hardware Constraint.” In International Conference on Advanced Computer Theory and Engineering (ICACTE 2009). ASME Press. https://doi.org/10.1115/1.802977.paper40
• Wang, Wei, and Junlong Wang. 2010. “Study of Modulation Phase Drift in an Interferometric Fiber Optic Gyroscope.” Optical Engineering 49 (11): 1–5. https://doi.org/10.1117/1.3509360
• Wang, Dan, and Wei Wang. 2013a. “Airborne Integrated Vision/Inertial Navigation System for Landing on Aircraft Carrier.” Advanced materials research 748: 747–53. https://doi.org/10.4028/www.scientific.net/amr.748.747
• Wang, Hui, and Le Wang. 2013b. “Development of Landing and Taxiing Response Analysis System for Aircraft with Multi-Wheels and Multi-Landing Gears.” Applied Mechanics and Materials 459: 511–16. https://doi.org/10.4028/www.scientific.net/amm.459.511
• Wang, Meng, and Lei Wang. 2022. “Influence of Gyro Axis Sequence Configuration on the Accuracy of Alignment and Navigation in a Nested Rotation Inertial Navigation System.” Measurement Science and Technology 33 (11): 115119. https://doi.org/10.1088/1361-6501/ac804a
• Wang, Jinshun, Wei Wang, and Jingxuan Ban. 2026k. “A Self-Calibration Method for Azimuth Gyro Drift in Single-Axis Hybrid Inertial Navigation System.” Measurement Science and Technology 37 (31): 316306. https://doi.org/10.1088/1361-6501/ae8ff6
• Wang, Chenglong, Bo Wang, Zhihong Deng, and Mengyin Fu. 2021c. “A Co-Occurrence Matrix-Based Matching Area Selection Algorithm for Underwater Gravity-Aided Inertial Navigation.” IET Radar, Sonar & Navigation 15 (3): 250–60. https://doi.org/10.1049/rsn2.12021
• Wang, K., J. Y. Wang, H. X. Huang, L. R. Xie, Y. Liu, and H. J. Tan. 2023d. “Effects of Backpressure on Unstart and Restart Characteristics of a Supersonic Inlet.” Aeronautical Journal 127 (1316): 1774–92. https://doi.org/10.1017/aer.2023.19
• Wang, Lei, Wei Wang, Jian Liu, and Fang Liu. 2013e. “Research on Accelerometer Output Error for Rotational Inertial Navigation System.” Applied Mechanics and Materials 336-338: 995–98. https://doi.org/10.4028/www.scientific.net/amm.336-338.995
• Wang, Taojun, Ren Wang, Fanyi Meng, Ziyang Liu, and Gang Chen. 2024b. “A Deformation Decision-Making Method Based on Deep Reinforcement Learning for Morphing Reusable Launch Vehicle.” Preprint, . https://doi.org/10.2139/ssrn.4819076
• Wang, Jun, Xingshu Wang, Shuai Yang, and Jing Zhu. 2017c. “Gravity Compensation in a Strapdown Inertial Navigation System to Improve the Attitude Accuracy.” In AOPC 2017: Space Optics and Earth Imaging and Space Navigation, edited by Carl Nardell, Suijian Xue, Huaidong Yang. SPIE. https://doi.org/10.1117/12.2281217
• Wang, Xiaxiao, Xiang Wang, Jia Yu, and Yue Zheng. 2017b. “Eigenfrequency Detecting Method with Sawtooth Wave Modulation Theory for Navigation Grade Fiber Optic Gyroscopes.” Optical Engineering 56 (09): 1–6. https://doi.org/10.1117/1.oe.56.9.094109
• Wang, Ning, Zhennan Wei, Zeyuan Xu, et al. 2024c. “Energy Dissipation Mechanism and Enhancement Method for Quality Factor in Hemispherical Resonator Gyroscopes.” Preprint, . https://doi.org/10.2139/ssrn.4917343
• Wang, Feng Lin, Xiu Lan Wen, and Danghong Sheng. 2012a. “The Influence of Initial Error to the Rate Azimuth Platform Inertial System.” Advanced materials research 442: 430–35. https://doi.org/10.4028/www.scientific.net/amr.442.430
• Wang, Fenglin, Xiulan Wen, and Danghong Sheng. 2013d. “Observability Analysis and Simulation of Passive Gravity Navigation System.” Journal of Computers 8 (1). https://doi.org/10.4304/jcp.8.1.248-255
• Wang, Feng Lin, Xiu Lan Wen, and Dong Xia Wang. 2011b. “The Error Analysis Caused by Accelerometer Drifs to the Rate Azimuth Platform Inertial System.” Applied Mechanics and Materials 143-144: 595–600. https://doi.org/10.4028/www.scientific.net/amm.143-144.595
• Wang, Feng Lin, Xiu Lan Wen, and Dong Xia Wang. 2011d. “Observability Analysis and Simulation for RAPINS/Gravity Matching Integrated Navigation System.” Applied Mechanics and Materials 143-144: 707–11. https://doi.org/10.4028/www.scientific.net/amm.143-144.707
• Wang, Jian Qiang, and Hua Ling Wu. 2014. “The Impact of Vertical Deflection on the Ballistic Missiles for Direction and Positioning.” Applied Mechanics and Materials 568-570: 938–43. https://doi.org/10.4028/www.scientific.net/amm.568-570.938
• Wang, Hubiao, Lin Wu, Hua Chai, Houtse Hsu, and Yong Wang. 2016f. “Technology of Gravity Aided Inertial Navigation System and Its Trial in South China Sea.” IET Radar, Sonar & Navigation 10 (5): 862–69. https://doi.org/10.1049/iet-rsn.2014.0419
• Wang, Xueyun, Jie Wu, Tao Xu, and Wei Wang. 2013a. “Analysis and Verification of Rotation Modulation Effects on Inertial Navigation System Based on MEMS Sensors.” Journal of Navigation 66 (5): 751–72. https://doi.org/10.1017/s0373463313000246
• Wang, Geng, Fei Xing, Minsong Wei, Ting Sun, and Zheng You. 2017h. “Optimization Method for Star Tracker Orientation in the Sun-Pointing Mode.” Chinese Optics Letters 15 (8): 081201. https://doi.org/10.3788/col201715.081201
• Wang, Rong, Zhi Xiong, Jianye Liu, and Lina Zhong. 2014a. “Adaptive Huber-Based Filter for Hypersonic Cruise Vehicle Navigation.” Journal of Algorithms & Computational Technology 8 (3): 319–37. https://doi.org/10.1260/1748-3018.8.3.319
• Wang, Xueyun, Yefeng Xu, Jialin Wang, and Jialin Zhu. 2024m. “Optimal Guidance for Reusable Launch Vehicle in Reentry Phase Based on Adaptive Dynamic Programming with Experience Reply.” Preprint, . https://doi.org/10.22541/au.172114671.13104425/v1
• Wang, Yu, Yun Xu, and Xin Zhu. 2014d. “A Novel Filtering Method for the Random Drift of MEMS Gyroscope.” Advanced materials research 901: 73–79. https://doi.org/10.4028/www.scientific.net/amr.901.73
• Wang, Yue Gang, and Jia Sheng Yang. 2013. “Self-Alignment Algorithm for Strapdown Inertial Navigation System under Strong Flurry Interference.” Applied Mechanics and Materials 347-350: 3667–71. https://doi.org/10.4028/www.scientific.net/amm.347-350.3667
• Wang, Fenglin, YingHong Yang, and Dongxia Wang. 2015b. “Research on Gravity Interpolation Technology for RAPINS/Log/Gravity Matching Integrated Navigation System.” In Advances in Computer Science Research. Atlantis Press. https://doi.org/10.2991/isci-15.2015.81
• Wang, Qi, Chang-song Yang, and Shao-en Wu. 2020g. “Non-Exchangeable Error Compensation for Strapdown Inertial Navigation System in High Dynamic Environment.” Computers, Materials & Continua 64 (2): 973–86. https://doi.org/10.32604/cmc.2020.07575
• Wang, Qi, Chang Song Yang, Shao En Wu, and Yan Wang. 2020b. “Application of Gravity Passive Aided Strapdown Inertial Navigation in Underwater Vehicles.” International Journal of Sensor Networks 32 (4): 209. https://doi.org/10.1504/ijsnet.2020.106635
• Wang, Jiayu, Weiping Yang, Guoliang Yang, Yu Tian, and Xiaokun Ding. 2024i. “Navigation in GNSS-Denied Environment Based on Observation of RSOs and Stars.” Guidance, Navigation and Control 05 (01): 101–13. https://doi.org/10.1142/s2737480724500225
• Wang, He Nian, Guo Yi, Changhong Wang, and Yu Guan. 2011c. “Nonlinear Initial Alignment of Strapdown Inertial Navigation System Using CSVM.” Applied Mechanics and Materials 148-149: 616–20. https://doi.org/10.4028/www.scientific.net/amm.148-149.616
• Wang, Le Yi, G. George Yin, Ji-Feng Zhang, and Yanlong Zhao. 2010a. “Input Design for Identification in Connected Systems.” In Systems & Control: Foundations & Applications. Birkhäuser Boston. https://doi.org/10.1007/978-0-8176-4956-2_7
• Wang, C., V. Zakkay, and H. Parikh. 1980. “An Experimental and Analytical Investigation of a Hypersonic Cruise Vehicle at Mach 6.” In 18th Aerospace Sciences Meeting. AIAA 1980-4. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-4
• Wang, fang, Haitao Zhang, Jiangtao Cai, and Jie Jin. 2022h. “Influence of Fuel Properties on Atomization Characteristics of Turbojet Engine Wp11.” Preprint, . https://doi.org/10.2139/ssrn.4172052
• Wang, ShiXuan, Min Zhang, Juan Du, Dun Ba, ChaoQun Nie, and YangYang Wang. 2024k. “Numerical Simulation and Prediction Using Neural Network for Internal Flow Field and Outlet Distortion Contour of S-Shape Inlet Ducts.” In Volume 1: Aircraft Engine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2024-128513
• Wang, Yong, Tao Zhang, Xianyu Jin, and Yin Yin. 2023m. “Shimmy Suppression of an Aircraft Nose Landing Gear Using Torsional Nonlinear Energy Sink.” Journal of Computational and Nonlinear Dynamics 18 (10): 101002. https://doi.org/10.1115/1.4062909
• Wang, Lipeng, Zhi Zhang, Qidan Zhu, and Zixia Wen. 2021j. “Longitudinal automatic carrier-landing control law rejecting disturbances and coupling based on adaptive dynamic inversion.” Bulletin of the Polish Academy of Sciences Technical Sciences: 136217–136217. https://doi.org/10.24425/bpasts.2020.136217
• Wang, Dangwei, and Lei Zhou. 2015. “Experimental Investigation on CNS/SINS Integrated Navigation Using Star Tracker.” In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46632-2_40
• Wang, Kedong, Junjie Zhou, Wenhui Han, and Jinling Wang. 2025n. “Terrain Matching without Redundant 3D Zernike Moments.” Journal of Navigation 78 (2–3): 210–20. https://doi.org/10.1017/s0373463325101070
• Wang, Kedong, Tongqian Zhu, and Jinling Wang. 2018h. “Real-Time Terrain Matching Based on 3D Zernike Moments.” Journal of Navigation 71 (6): 1441–59. https://doi.org/10.1017/s0373463318000449
• Wang, Kedong, Tongqian Zhu, and Jinling Wang. 2019c. “Impact of Terrain Factors on the Matching Performance of Terrain-Aided Navigation.” Navigation 66 (2): 451–62. https://doi.org/10.1002/navi.306
• Wangu, Srimal, and William Mouyos. 1998. “Reusable Launch Vehicle System Health Management.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5239
• Ward, L. K., and A. W. Myers. 1967. Free-Flight Testing of Aerodynamic Decelerators in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0815090
• Ward, T. R., and James Neeley. 1959. Altitude Performance Evaluation of Two Afterburner Fuel Manifold Configurations in an Iroquois Series 2 Turbojet Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0221389
• Wardana, T. K., F. S. Pranoto, and G. Akhiri. 2021. “Performance Comparison of Unmanned Aircraft System (UAS) Flight Controller with Independent Flight Test Instrumentation (FTI) during Flight.” In AIP Conference Proceedings, vol. 2366. AIP Publishing. https://doi.org/10.1063/5.0060371
• Warner, D. F. 1951. “Discussion: “Turbojet-Engine Design for High-Speed Flight” (Hurley, W. V., 1951, Trans. ASME, 73, Pp. 915–920).” Journal of Fluids Engineering 73 (7): 920–920. https://doi.org/10.1115/1.4016501
• Washburn, K. E., and B. B. Gloss. 1978. Aerodynamic Load Distributions at Transonic Speeds for a Close-Coupled Wing-Canard Configuration: Tabulated Pressure Data. NASA-TM-78780. NASA. https://ntrs.nasa.gov/citations/19780025102
• Washington, W., and D. Spring. 1982. “An Experimental Investigation of Wing-Tail Interference for a Typical Supersonic Missile.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1339. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1339
• Wasilczuk, Filip, Marcin Kurowski, and Paweł Flaszyński. 2024. “Test Section Design for Measuring the Drag Coefficient of a Suborbital Rocket Model at Ma 2.45.” Transactions on Aerospace Research 2024 (3): 86–100. https://doi.org/10.2478/tar-2024-0018
• Wasserbauer, J. F. 1969. Dynamic Response of a Mach 2.5 Axisymmetric Inlet with Engine or Cold Pipe and Utilizing 60 Percent Supersonic Internal Area Contraction. NASA-TN-D-5338. NASA. https://ntrs.nasa.gov/citations/19690021958
• Wasserbauer, J., and W. Gerstenmaier. 1978. “Inlet-Engine Matching for SCAR Including Application of a Bicone Variable Geometry Inlet.” In 14th Joint Propulsion Conference. AIAA 1978-961. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-961
• Wasserbauer, J., and R. Willoh. 1968. “Experimental and Analytical Investigation of the Dynamic Response Ofa Supersonic Mixed- Compression Inlet.” In 4th Propulsion Joint Specialist Conference. AIAA 1968-651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-651
• Wasserman, Richard, and John F. Mitchell. 1973. In-Flight Simulation of Minimum Longitudinal Stability for Large Delta- Wing Transports in Landing Approach and Touchdown. Volume 1. Technical Results. Defense Technical Information Center. https://doi.org/10.21236/ad0761120
• Waters, Kristy L., Jose H. Ramos, and Kevin M. Brink. 2025. “Iterative Closest Point Batch Recursive Update for Magnetic Anomaly-Based Navigation.” In AIAA SCITECH 2025 Forum. AIAA 2025-2610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2610
• Watkinson, K., N. Smith, and D. Humphreys. 1986. “Simulation of the Launch Transient Dynamics of a Canard-Controlled Missile Launched from an Underwing Pod.” In Astrodynamics Conference. AIAA 1986-2080. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2080
• Watson, Earl C. 1953. An Analytical Study of the Comparative Performance of Six Air-Induction Systems for Turbojet-Powered Airplanes Designed to Operate at Mach Numbers up to 2.0. NACA-RM-A53H03. NASA. https://ntrs.nasa.gov/citations/19930087828
• Watson, D. M., G. H. Hardy, and D. N. Warner Jr. 1983. Flight-Test of the Glide-Slope Track and Flare-Control Laws for an Automatic Landing System for a Powered-Lift STOL Airplane. NASA-TP-2128. NASA. https://ntrs.nasa.gov/citations/19840005130
• Watson, Michael D., and Kurt Jackson. 2002. Tightly Coupled Inertial Navigation System/Global Positioning System (TCMIG). NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20020067401
• Wattenbarger, Zachary, and Kurt Rouser. 2025. “Development of a Micro-Turbojet Engine Control Unit for Component Level Efficiencies Monitoring.” In 2025 Regional Student Conferences. AIAA 2025-98963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-98963
• Waugh, Steve. 1998. Joint Composite Tracking Network (JCTN)-Benefits to Cruise Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada359394
• Way, Alexander S., Adrian Sescu, Edward Luke, and Ian D. Dettwiller. 2024. “Hypernetwork Based Surrogate Modeling of Hypersonic Glide Vehicle Aerothermodynamics.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4107
• Webb, William. 1979. Sources of Tracking Error in Millimeter Wavelength Missile Guidance Systems. Defense Technical Information Center. https://doi.org/10.21236/ada078226
• Webber, J. P. H., and D. S. Houghton. 1963. “Spar Web Buckling of a Supersonic Aircraft: An Analysis of a Simply-Supported Rectangular Plate under the Action of in-Plane Stresses Due to the Action of Aerodynamic and Inertia Forces and Kinetic Heating Effects.” Aircraft Engineering and Aerospace Technology 35 (12): 364–68. https://doi.org/10.1108/eb033812
• Weber, R. J. 1959. “A Survey of Hypersonic-Ramjet Concepts.” In American Rocket society Semi-Annual Meeting. https://ntrs.nasa.gov/citations/19630039050
• Weber, R. J. 1967. Liquefied Natural Gas as a Fuel for Supersonic Aircraft. NASA. https://ntrs.nasa.gov/citations/19670048710
• Webster, A. P. 1947. Free-Falls and Parachute Descents in the Standard Atmosphere. NACA-TN-1315. Bureau of Medicine and Surgery, Navy Department. https://ntrs.nasa.gov/citations/19930082042
• Weddig, Nicolai Ben, and Steffen Schön. 2024. “Observability and Estimability Analysis of an Error State Multi-Sensor Navigation Filter Using Numerical Observability Methods.” In ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation. Institute of Navigation. https://doi.org/10.33012/2024.19867
• Weeratunga, Sisira, and Suresh Menon. 1993. “Parallel Computations of Unsteady Combustion in a Ramjet Engine.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1914. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1914
• Wegener, Peter P. 1977. Supersonic Diffuser Research. Defense Technical Information Center. https://doi.org/10.21236/ada038280
• Wegener, Peter P. 1991. “Toward High Speed: Supersonic and Hypersonic Flight.” In What Makes Airplanes Fly?. Springer US. https://doi.org/10.1007/978-1-4684-0403-6_10
• Wegener, Peter P. 1997. “Toward High Speed: Supersonic and Hypersonic Flight.” In What Makes Airplanes Fly?. Springer New York. https://doi.org/10.1007/978-1-4612-2254-5_10
• Wei, Erhu, Cuijun Dong, Yali Yang, et al. 2017. “A Robust Solution of Integrated SITAN with TERCOM Algorithm: Weight-Reducing Iteration Technique for Underwater Vehicles’ Gravity-Aided Inertial Navigation System.” Navigation 64 (1): 111–22. https://doi.org/10.1002/navi.176
• Wei, Guo, Chunfeng Gao, Qi Wang, Qun Wang, Zhenyu Xiong, and Xingwu Long. 2016b. “A New Systematic Calibration Method of Ring Laser Gyroscope Inertial Navigation System.” In SPIE Proceedings, vol. 9987, edited by David A. Huckridge, Reinhard Ebert, Stephen T. Lee. SPIE. https://doi.org/10.1117/12.2241253
• Wei, Jian, Jipeng He, Jiahao Zhang, Shixing Zhu, Shuangbao Li, and Hengjia Zhu. 2026d. “Shimmy Dynamics Analysis of a Dual-Wheel Main Landing Gear Considering Side Stay Angular Coupling.” SAE International Journal of Aerospace 19 (2). https://doi.org/10.4271/01-19-02-0007
• Wei, Zhaoli, Zhongrui Ma, Ting Li, Longqi Ran, Jiangbo He, and Wu Zhou. 2026c. “A Parametric Vibration-Based Micro Hemispherical Resonator Gyroscope with Bias Instability of 0.083°/h.” Journal of Physics: Conference Series 3184 (1): 012020. https://doi.org/10.1088/1742-6596/3184/1/012020
• Wei, Jianli, Cong Wang, Yongqin Xu, and Jie Yan. 2016a. “A Hypersonic Cruise Flight Vehicle High-Precision Control Method Using Compound Rudder Surface.” In Modelling, Identification and Control / 834: Parallel and Distributed Computing and Networks / 835: Software Engineering. ACTAPRESS. https://doi.org/10.2316/p.2016.830-040
• Wei, Qiushuo, Feng Zha, and Lubin Chang. 2022b. “Novel Rotation Scheme for Dual-Axis Rotational Inertial Navigation System Based on Body Diagonal Rotation of Inertial Measurement Unit.” Measurement Science and Technology 33 (9): 095105. https://doi.org/10.1088/1361-6501/ac6e2c
• Wei, Jingru, Zekai Zhang, Huiliang Cao, and Xiaomin Duan. 2021. “Hybrid Temperature Compensation Model of MEMS Gyroscope Based on Genetic Particle Swarm Optimization Variational Modal Decomposition and Improved Backpropagation.” Sensors and Materials 33 (8): 2835. https://doi.org/10.18494/sam.2021.3412
• Weichelt, G., J. Urnes, and J. Jarrett. 1986. “An All-Weather Multimode Landing System for Tactical Fighter Aircraft.” In Astrodynamics Conference. AIAA 1986-2146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2146
• Weidner, J. P. 1979. Conceptual Study of a Turbojet/ramjet Inlet. NASA-TM-80141. NASA. https://ntrs.nasa.gov/citations/19790023044
• Weidner, J. 1980. “Propulsion/airframe Integration Considerations for High Altitude Hypersonic Cruise Vehicles.” In 18th Aerospace Sciences Meeting. AIAA 1980-111. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-111
• Weiler, W. J. 1972. High Energy Astronomy Observatory Star Tracker Search Program. NASA-TM-X-64680. NASA. https://ntrs.nasa.gov/citations/19720021015
• Weinacht, Paul. 2014. A Direct-Fire Trajectory Model for Supersonic, Transonic, and Subsonic Projectile Flight. Defense Technical Information Center. https://doi.org/10.21236/ada607593
• Weinstein, I., D. E. Avery, and A. J. Chapman. 1975. Aerodynamic Heating to the Gaps and Surfaces of Simulated Reusable-Surface-Insulation Tile Arrays in Turbulent Flow at Mach 6.6. NASA-TM-X-3225. NASA. https://ntrs.nasa.gov/citations/19760004291
• Weinstein, I., D. E. Avery, and L. R. Hunt. 1981. Aerodynamic Heating on the Corrugated Surface of a 10.2 Deg Half-Angle Blunted Cone at Mach 6.7. NASA-TP-1928. NASA. https://ntrs.nasa.gov/citations/19820005510
• Weinstein, Rose, James E. Hubbard, and Michael Cunningham. 2018. “Fuzzy Modeling and Parallel Distributed Compensation for Aircraft Flight Control from Simulated Flight Data.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3313
• Weinstock, H. 1968. “Design of a Precision Tilt and Rotational Vibration Isolation Systemfor Inertial Sensor Testing.” In Control and Flight Dynamics Conference. AIAA 1968-894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-894
• Weir, Kent A., and Eugene M. Wells. 1990. “A Numerical Algorithm to Propagate Navigation Error Covariance Matrices Associated with Generalized Strapdown Inertial Measurement Units.” In AIAA Guidance, Navigation and Control Conference. https://ntrs.nasa.gov/citations/19900060658
• Weitzen, Jay A., James V. Carroll, and H. James Rome. 1996. “RAIM Availability of GPS Augmented with Loran-C and Barometric Altimeter for Use in Nonprecision Approach1.” Navigation 43 (1): 71–84. https://doi.org/10.1002/j.2161-4296.1996.tb01918.x
• Welberg, Dietmar, Markus Werner, and Jean-Philippe Dutheil. 2015. “A Flight Control System for the Rocket-Propelled and Ballistic Flight Phases for a SubOrbital SpacePlane Application.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-4123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4123
• Welch, J. 1963. “An Advanced Optical-Inertial Space Navigation System.” In Summer Meeting. AIAA 1963-215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-215
• Welch, J. D. 1965. An Optical-Inertial Space Navigation System. NASA. https://ntrs.nasa.gov/citations/19650046058
• Welge, H., R. Radkey, and P. Henne. 1976. “Nacelle Aerodynamic Design and Integration Study on a Mach 2.2 Supersonic Cruise Aircraft.” In 12th Propulsion Conference. AIAA 1976-757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-757
• Welker, Troy, Richard Huffman, and Meir Pachter. 2011. “Use of Gravity Gradiometry in Precision Inertial Navigation Systems.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6643
• Wells, Doyle C. 1953. “Cooling Electric Equipment during Supersonic Flight.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/530163
• Wells, Brian. 1991. “Tactical Missile Structural Testing and Model Verification for Autopilot Design.” In Navigation and Control Conference. AIAA 1991-2616. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2616
• Wells, W., S. Banda, and D. Quam. 1981. “Aircraft Lateral Parameter Estimation from Flight Data with Unsteady Aerodynamic Modelling.” In 19th Aerospace Sciences Meeting. AIAA 1981-221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-221
• Wells, E., and J. Breakwell. 1980. “A Study to Determine the Best Utilization of Gravity Gradiometer Information to Improve Inertial Navigation System /INS/ Accuracy.” In Guidance and Control Conference. AIAA 1980-1722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1722
• Wells, W., and V. Klein. 1982. “Parameter Estimation Applied to General Aviation Aircraft: A Case Study.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1313. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1313
• Welter, G., J. Boia, M. Gakenheimer, E. Kimmer, D. Channell, and L. Hallock. 1996. “Variations on the Davenport Gyroscope Calibration Algorithm.” In Flight Mechanics/Estimation Theory Symposium 1996. https://ntrs.nasa.gov/citations/19960035752
• Wen, Zhe, Hongwei Bian, Rongying Wang, Heng Ma, and Zhonglei Zhu. 2021. “Research on the Algorithm of Solving the Optical Axis Direction of Celestial Navigation Star Sensor.” In Third International Conference on Optoelectronic Science and Materials (ICOSM 2021), edited by Siting Chen, Pei Wang. SPIE. https://doi.org/10.1117/12.2617344
• Wen, Chao Bin, Yue Gang Wang, Xin Lei Jiang, and Hong Lei Teng. 2014. “Gravity Matching Aided Navigation Using a New Mixed Filter Algorithm.” Applied Mechanics and Materials 644-650: 2067–70. https://doi.org/10.4028/www.scientific.net/amm.644-650.2067
• Wenkai, Wang, Zhongxi Hou, Zheng Guo, Lili Chen, and Jiexing Yang. 2017c. “Range Extension of Hypersonic Cruise Vehicle with Lowest Technical Merit.” In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. AIAA 2017-4004. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4004
• Wenkai, Wang, Zhongxi Hou, Duoneng Liu, Jiexing Yang, LiLi Chen, and Bingjie Zhu. 2017a. “Heat-Augmented Trajectory Optimization of Hypersonic Cruise Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2156
• Wenzel, Karl Engelbert, Andreas Masselli, and Andreas Zell. 2010. “Automatic Take off, Tracking and Landing of a Miniature UAV on a Moving Carrier Vehicle.” In Unmanned Aerial Vehicles. Springer Netherlands. https://doi.org/10.1007/978-94-007-1110-5_15
• Werrell, Kenneth P. 1985b. The Evolution of the Cruise Missile. Defense Technical Information Center. https://doi.org/10.21236/ada162646
• Werrell, Kenneth P. 1989. “The Weapon the Military Did Not Want: The Modern Strategic Cruise Missile.” Journal of Military History 53 (4): 419. https://doi.org/10.2307/1986108
• Werrell, Kenneth P. 2000. Hitting a Bullet with a Bullet a History of Ballistic Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada381863
• West, Thomas K., and Ben D. Phillips. 2018. “Multifidelity Uncertainty Quantification of a Commercial Supersonic Transport.” In 2018 Applied Aerodynamics Conference. AIAA 2018-2851. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2851
• Westerwelt, Pj. 2024. “An Experimental Determination of the Wave Drag Coefficient on Spheres.” In Spring Conference 1985. Institute of Acoustics. https://doi.org/10.25144/22473
• Weston, Christopher S., and Carlos E. Cesnik. 2024. “Hybrid-Fidelity Global-Local Aerothermoelastic Modeling for Path-Dependent Hypersonic Flight.” In AIAA SCITECH 2024 Forum. AIAA 2024-1045. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1045
• Westra, D. P., G. Lintern, D. J. Sheppard, K. E. Thomley, and R. Mauk. 1986. Simulator Design and Instructional Features for Carrier Landing: A Field Transfer Study. Defense Technical Information Center. https://doi.org/10.21236/ada169962
• Westra, D. P., C. W. Simon, S. C. Collyer, and W. S. Chambers. 1981. Simulator Design Features for Carrier Landing. I. Performance Experiments. Defense Technical Information Center. https://doi.org/10.21236/ada122064
• Wetzel, Todd Andrew. n.d. “Development of a Finite-Difference Neighboring Optimal Control Law and Application to the Optimal Landing of a Reusable Launch Vehicle.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-10526
• Wetzel, Benton E. 1954. Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well above the Wing Plane: Lateral and Directional Stability. NACA-RM-SA54H26b. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20090025891
• Whalley, Ian A. 1973. “Development of the B-1 Crew Module Parachute Recovery System.” In 4th Aerodynamic Deceleration Systems Conference. AIAA 1973-467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-467
• Wheeler, George F. 1946. A Photographic Method for Assessment of Bombing Results. Defense Technical Information Center. https://doi.org/10.21236/ada801558
• Wheeler, Jonathan M., Jacob N. Chamoun, and Michel J. F. Digonnet. 2018. “A Fiber Optic Gyroscope Driven by a Low-Coherence Laser Suitable for Aircraft Navigation.” In 26th International Conference on Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.2018.the47
• Wheeler, Jonathan M., and Michel J. F. Digonnet. 2021. “Demonstration of Strategic-Grade Noise in an Optically Gated Laser-Driven Fiber Optic Gyroscope.” In Optical Fiber Sensors Conference 2020 Special Edition. Optica Publishing Group. https://doi.org/10.1364/ofs.2020.w4.75
• Whipple, Benjamin, and Esteban A. Hernandez-Vargas. 2024. “Mechanistic Identifiability Preservation for Hybrid Neural Differential Equations.” Preprint, bioRxiv. https://doi.org/10.1101/2024.12.08.627408
• Whitcomb, Richard T. 1953. Recent Results Pertaining to the Application of the “Area Rule”. NACA-RM-L53I15a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20050019402
• Whitcomb, R. T. 1955. “Several Extensions of the Area Rule.” In NACA Conf. on Aerodyn. of High Speed Aircraft. https://ntrs.nasa.gov/citations/19740075323
• Whitcomb, R. T. 1956a. Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages. NACA-RM-L56E23A. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19660024790
• Whitcomb, Richard T. 1956b. “Zero-Lift-Drag Characteristics of Wing-Body Combinations at Transonic Speeds.” In 24th Annual Meeting of the Institute of the Aeronautical Sciences. https://ntrs.nasa.gov/citations/19650070830
• Whitcomb, Richard T. 1957. A Fuselage Addition to Delay Drag-Rise Mach Number of Subsonic Airplanes at Lifting Conditions. NACA-RM-L57H09b. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090026510
• Whitcomb, Richard T., and John R. Sevier Jr. 1960. A Supersonic Area Rule and an Application to the Design of a Wing-Body Combination with High Lift-Drag Ratios. NASA-TR-R-72. NASA. https://ntrs.nasa.gov/citations/19980223605
• Whitcombe, David W. 1961. An Introduction to Inertial Guidance Concepts for Ballistic Missiles (a Tutorial Report). Defense Technical Information Center. https://doi.org/10.21236/ad0259865
• White, John S. 1960. Investigation of the Errors of an Inertial Guidance System during Satellite Re-Entry. NASA-TN-D-322. NASA. https://ntrs.nasa.gov/citations/19980227184
• White, W. F. 1978. Flight Demonstrations of Curved, Descending Approaches and Automatic Landings Using Time Referenced Scanning Beam Guidance. NASA-TM-78745. NASA. https://ntrs.nasa.gov/citations/19780022131
• White, K. K. 1985. “A Decimal System of Celestial Navigation Based on the Second.” Journal of Navigation 38 (2): 293–95. https://doi.org/10.1017/s0373463300031416
• White, J. 1993. “Supersonic/hypersonic Flight Vehicle Forebody Wave Drag Determination Using an Euler-Based CFD Approach.” In Aerospace Design Conference. AIAA 1993-971. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-971
• White, J. 1995. “An Assessment of Missile DATCOM Prediction Accuracy Relative to Generic Body+Wing+Tail Missile Pitch Aerodynamics.” In 13th Applied Aerodynamics Conference. AIAA 1995-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1893
• White, W. F., and L. V. Clark. 1981. “Operational Considerations in Utilization of Microwave Landing System Approach and Landing Guidance.” In 1980 Aircraft Safety and Operating Probl. Conf.. https://ntrs.nasa.gov/citations/19810011522
• White, R. L., and R. B. Gounley. 1987. Satellite Autonomous Navigation with SHAD (Stellar Horizon Atmospheric Dispersion). Defense Technical Information Center. https://doi.org/10.21236/ada184988
• White, R., and F. Grant. 1973. Candidate Configuration Trade Study, Stellar-Inertial Measurement System (SIMS) for an Earth Observation Satellite (EOS), Addendum. NASA-CR-134042. NASA. https://ntrs.nasa.gov/citations/19730025112
• White, H. V., and J. C. Hung. 1978. Gyrocompassing Error Analysis for Pershing II Inertial Measurement Unit. Defense Technical Information Center. https://doi.org/10.21236/ada067516
• White, Zachary P., Adam R. Kotler, Mason R. Thornton, Jack Lahm, and Kareem A. Ahmed. 2025. “Experimental Investigation of High-Speed Ramjet Rotating Detonation Engine.” In AIAA SCITECH 2025 Forum. AIAA 2025-2103. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2103
• White, Bruce, and J. Macha. 1991. “Experimental Investigation of Added Mass during Parachute Deceleration: Preliminary Results.” In 11th Aerodynamic Decelerator Systems Technology Conference. AIAA 1991-853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-853
• White, B. A., Y. Patel, D. H. Vorley, and M. Horton. 1995. “Loop Shaping Design of a Robust Missile Autopilot.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 1. American Autom Control Council. https://doi.org/10.1109/acc.1995.529303
• White, Staci, and Paul Strykowski. 2003. “Characterizing the Performance of the Sr 30 Turbojet Engine.” In 2003 Annual Conference Proceedings. ASEE Conferences. https://doi.org/10.18260/1-2–11611
• White, Charles F., and James W. Titus. 1956. Elevation-Azimuth Servo System Specifications for Star Tracking. Defense Technical Information Center. https://doi.org/10.21236/ad0091516
• White Sands Missile Range Nm. 1997. Stress Level Testing of Missile and Rocket Systems during Development Tests (Environmental Stress Screening). Defense Technical Information Center. https://doi.org/10.21236/ada340980
• Whiting, Matthew Robert. 1996. “Differential Canard Deflection for Generation of Yawing Moment on the X-31 with and without the Vertical Tail.” PhD diss., NASA Langley Research Center. https://ntrs.nasa.gov/citations/19960012279
• Whiting, J., and J. Jobe. 1972. “Virtual Target Steering: A Unique Air-to-Surface Missile Targeting and Guidance Technique.” In Guidance and Control Conference. AIAA 1972-826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-826
• Whitlow, J. B., Jr. 1975. Comparison of Parametric Duct-Burning Turbofan and Non-Afterburning Turbojet Engines in a Mach 2.7 Transport. NASA-TM-X-71679. NASA. https://ntrs.nasa.gov/citations/19750011175
• Whitney, W. A. 1963. Results of the Phase II Long-Term Environmental Storage Test Program for the RJ43-MA-11 Ramjet Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0423790
• Whittaker, Matthew, and John L. Crassidis. 2017. “Inertial Navigation Employing Common Frame Error Representations.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1031. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1031
• Whittaker, Matthew P., and John L. Crassidis. 2018. “Linearized Analysis of Inertial Navigation Employing Common Frame Error Representations.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1600. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1600
• Whittaker, Matthew P., and John L. Crassidis. 2020. “Relative Inertial Navigation Employing a Common Frame Error Definition.” In AIAA Scitech 2020 Forum. AIAA 2020-1596. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1596
• Whyte, R., W. Hathaway, and G. Winchenbach. 1979. “Analysis of Free Flight Trajectory Data for a Complex Asymmetric Missile Configuration at Subsonic Mach Numbers.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1689. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1689
• Wiberg, D. V., A. D. Challoner, K. Shcheglov, et al. 2001. A Highly Miniaturized Inertial Grade Gyroscope for Space Applications. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/20010041293
• Widnall, William S., Giuseppe F. Gobbini, and John F. Kelley. 1982. Decentralized Relative Navigation and JTIDS/GPS/INS Integrated Navigation Systems. Defense Technical Information Center. https://doi.org/10.21236/ada116417
• Widnall, William S., and Peter A. Grundy. 1974. Doppler Velocity Sensor APN-200 Error Model and Flight Test Results. Defense Technical Information Center. https://doi.org/10.21236/ada002879
• Widnall, W., P. Grundy, and W. Murch. 1974. “Inertial Navigation System Tests Having Improved Observability of Error Sources.” In Mechanics and Control of Flight Conference. AIAA 1974-867. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-867
• Wieting, Allan R. 1989. “The Critical Role of Aerodynamic Heating Effects in the Design of Hypersonic Vehicles.” In International Conference on Finite Element Methods in Flow Problems. https://ntrs.nasa.gov/citations/19900031194
• Wignall, Thomas J., and Heather Houlden. 2020. “Uncertainty Quantification for Launch Vehicle Aerodynamic Lineloads.” In AIAA Scitech 2020 Forum. AIAA 2020-1521. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1521
• Wilbur, P. J., C. E. Mitchell, and B. D. Shaw. 1982. “The Electrothermal Ramjet.” In Joint Propulsion Conference. https://ntrs.nasa.gov/citations/19820051533
• Wilcox, J. 1972. “Maximum Likelihood Failure Detection for Redundant Inertial Instruments.” In Guidance and Control Conference. AIAA 1972-864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-864
• Wilcox, J. 1973. “Competitive Evaluation of Failure Detection Algorithms for Strapdownredundant Inertial Instruments.” In Guidance and Control Conference. AIAA 1973-853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-853
• Wilcox, Zachary, S. Bhat, R. Lind, and W. Dixon. 2009a. “Control Performance Variation Due to Nonlinear Aerothermoelasticity in a Hypersonic Vehicle: Insights for Structural Design.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6184. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6184
• Wilcox, F., T. Birch, and J. Allen. 2004. “Force, Surface Pressure, and Flowfield Measurements on a Slender Missile Configuration with Square Cross-Section at Supersonic Speeds.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-5451. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5451
• Wilcox, Fred, and Paul Whalen. 1956. Dynamics of a Supersonic Inlet with Adjustable Bypass in Combination with a J34 Turbojet Engine. NACA-RM-E55L13a. NASA. https://ntrs.nasa.gov/citations/19930088994
• Wilder, Michael, Daniel Reda, David Bogdanoff, and Dinesh Prabhu. 2007. “Free-Flight Measurements of Convective Heat Transfer in Hypersonic Ballistic-Range Environments.” In 39th AIAA Thermophysics Conference. AIAA 2007-4404. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4404
• Williams, J. E. D. 1964. “Long-Range Navigation Aids.” Journal of Navigation 17 (3): 313–15. https://doi.org/10.1017/s037346330003753x
• Williams, D. D. 1965. “Aerodynamic Requirements for Thrust Measurement in Supersonic Aircraft.” In Flight Test Instrumentation. Elsevier. https://doi.org/10.1016/b978-0-08-011074-5.50012-9
• Williams, Robert E. 1966. “Celestial Navigation Procedures.” Navigation 13 (2): 146–47. https://doi.org/10.1002/j.2161-4296.1966.tb01816.x
• Williams, Peggy S. 2004. Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20040105654
• Williams, Darryl, Matt Bartkowicz, and Graham V. Candler. 2024. “Shape Optimization for a Parametrically-Defined Hypersonic Glide Vehicle.” In AIAA SCITECH 2024 Forum. AIAA 2024-0562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0562
• Williams, Jonathan H., Robert J. Davis, and Eddie N. Rosario. 2000. Multipath Mitigation Performance of Planar GPS Adaptive Antenna Arrays for Precision Landing Ground Stations. Defense Technical Information Center. https://doi.org/10.21236/ada459739
• Williams, Brian, Nicolas Hudson, Brent Tweddle, Roland Brockers, and Larry Matthies. 2011. “Feature and Pose Constrained Visual Aided Inertial Navigation for Computationally Constrained Aerial Vehicles.” In Institute of Electrical and Electronics Engineers. https://ntrs.nasa.gov/citations/20120003288
• Williams, T., and B. Hunt. 1980. “Top Inlet System Feasibility for Transonic-Supersonic Fighter Aircraft Applications.” In Aircraft Systems Meeting. AIAA 1980-1809. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1809
• Williams, T. L., B. L. Hunt, D. B. Smeltzer, and W. P. Nelms. 1981a. “Top-Mounted Inlet System Feasibility for Transonic-Subsonic Fighter Aircraft Applications.” In AGARD Aerodyn. of Power Plant Installation. https://ntrs.nasa.gov/citations/19820005194
• Williams, T. L., B. L. Hunt, D. B. Smeltzer, and W. P. Nelms. 1981b. Top-Mounted Inlet System Feasibility for Transonic-Supersonic Fighter Aircraft. NASA-TM-81292. NASA. https://ntrs.nasa.gov/citations/19810015531
• Williams, D. D., and J. O. Yost. 1973. “Some Aspects of Inlet/engine Flow Compatibility.” Aeronautical Journal 77 (753): 483–92. https://doi.org/10.1017/s0001924000041610
• Williamson, Jack, Bradley Pascoe, Andrew Lock, and Ingo H. Jahn. 2026. “Simultaneous Vehicle Design and Trajectory Optimisation of a Multi-Stage Hypersonic Boost-Glide System.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5003
• Williamson, Walton R., Jason L. Speyer, and Charles H. Jones. 2005. Detection and Isolation of Instrumentation Failures Applied to GPS and Inertial Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada433107
• Willier, Brenton, Alexandra M. Hickey, Bradford E. Robertson, and Dimitri N. Mavris. 2024. “Unsteady Aerodynamic Uncertainty Quantification of a Blunt-Body Entry Vehicle in Free-Flight.” In AIAA SCITECH 2024 Forum. AIAA 2024-1917. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1917
• Willis, D. C., and P. G. Powell. 1965. “The Effect of Doppler on Navigation System Accuracy.” Journal of Navigation 18 (4): 452–57. https://doi.org/10.1017/s0373463300046373
• Wilson, Vernon E. 1980. Superplastic Formed and Diffusion Bonded Titanium Landing Gear Component Feasibility Study. Defense Technical Information Center. https://doi.org/10.21236/ada092788
• Wilson, J., and V. Wright. 1987. “Use of RPM Trim to Automate the Supersonic Engine/inlet Match in theSR-71A.” In 23rd Joint Propulsion Conference. AIAA 1987-1848. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1848
• Wilson, Philip, and Liwei Zhang. 2025. “Supersonic Inlet Design Using Method of Characteristics and Computational Fluid Dynamics.” In 2025 Regional Student Conferences. AIAA 2025-98188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-98188
• Wiltse, R. L. 1955. “Practical Development of Suspension Cushioning for a Guided Missile.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/550061
• Wilz, R., and R. Johnson. 1975. “Automatic All-Weather Landing Control.” In Aircraft Systems and Technology Meeting. AIAA 1975-1021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1021
• Windhorst, Robert, and Mark Ardema. 2000. “Supersonic Transport Trajectories.” In 18th Applied Aerodynamics Conference. AIAA 2000-4247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4247
• Windhorst, Robert, Mark Ardema, and Dave Kinney. 1999. “Fixed-Range Optimal Trajectories of Supersonic Aircraft by First-Order Expansions.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4069
• Wing, Willis. 1965. “Sgn- 10 Inertial Navigator.” In Guidance Control Conference. AIAA 1965-1213. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1213
• Wing, L. D. 1970. “Practical Methods for Predicting Aerodynamic Heating Effects on Sounding Rockets.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19710032983
• Wing, L. D. 1972. A Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses. NASA-TM-X-69896. NASA. https://ntrs.nasa.gov/citations/19730017274
• Wing, L. D. 1973. “A Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730038400
• Winger, Donley James. n.d. “Error Analysis of an Integrated inertial/Doppler-Satellite Navigation System with Continuous and Multiple Satellite Coverage.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180816-410
• Wingrove, R. 1972. “Applications of a Technique for Estimating Aircraft States from Recorded Flight Test Data.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-965
• Winkler, Stefan. 2011. “Observability of Star Tracker / Gyro Based Attitude Estimation Considering Time-Variant Sensor Misalignment.” In Advances in Aerospace Guidance, Navigation and Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-19817-5_29
• Winton, Scott C. 2021. “Radar Tracking.” In Handbook of Radar Signal Analysis. Chapman and Hall/CRC. https://doi.org/10.1201/9781315161402-13
• Wise, George A. 1953. Influence of End Plates on Lift and Flow Field of a Canard-Type Control Surface at a Mach Number of 2.00. NACA-RM-E53A02. NASA. https://ntrs.nasa.gov/citations/19930087437
• Wise, Kevin. 1989a. “Missile Autopilot Robustness to Uncertain Aerodynamics: Stability Hypersphere Radius Calculation.” In Guidance, Navigation and Control Conference. AIAA 1989-3553. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3553
• Wise, Kevin. 1989b. “Singular Value Robustness Tests for Missile Autopilot Uncertainties.” In Guidance, Navigation and Control Conference. AIAA 1989-3552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3552
• Wise, Kevin. 1990b. “Missile Autopilot Robustness Using the Real Multiloop Stability Margin.” In Guidance, Navigation and Control Conference. AIAA 1990-3340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3340
• Wise, Kevin. 2007. “A Trade Study on Missile Autopilot Design Using Optimal Control Theory.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6673
• Wise, Kevin, and Farhad Deylami. 1991. “Approximating a Linear Quadratic Missile Autopilot Design Using an Output Feedback Projective Control.” In Navigation and Control Conference. AIAA 1991-2613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2613
• Wise, K. A., and J. L. Sedwick. 1995. “Missile Autopilot Design Using Nonlinear h∞ Optimal Control.” In Automatic Control in Aerospace 1994 (Aerospace Control ‘94). Elsevier. https://doi.org/10.1016/b978-0-08-042238-1.50023-9
• Wittliff, C. E. 1982. A Study of Aerodynamic Heating Distributions on a Tip-Fin Controller Installed on a Space Shuttle Orbiter Model. NASA-CR-166025. NASA. https://ntrs.nasa.gov/citations/19830012726
• Wittry, J. 1969. “Description of an Inertial Test Facility Incorporating a Passively Isolated and Actively Stabilized Platform.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-863
• Wojciechowski, C. J., and P. G. Anderson. 1981. Parametric Analysis of Diffuser Requirements for High Expansion Ratio Space Engine. NASA-CR-161924. NASA. https://ntrs.nasa.gov/citations/19820006407
• Wolf, T. D., and R. C. McCracken. 1973. Ground and Flight Experience with a Strapdown Inertial Measuring Unit and a General Purpose Airborne Digital Computer. NASA-TM-X-2848. NASA. https://ntrs.nasa.gov/citations/19730020981
• Wolf, Robert L., Mullen II, and James W. 1951. Ramjet Technology. Chapter 16. Solid Fuel Ramjets. Defense Technical Information Center. https://doi.org/10.21236/ad0036130
• Wolfe, M. O. W. 1964. “Aspects of Elevated Temperature Design and Design Criteria for Supersonic Aircraft Structures.” In High Temperature Structures and Materials. Elsevier. https://doi.org/10.1016/b978-0-08-010580-2.50018-9
• Wolfenbarger, Natalie S., and Sungkoo Bae. 2016. “Star Tracker Distortion Characterization Using Localized Attitude Dependent Distortion Estimation Methods for the ICESat Mission.” In AIAA/AAS Astrodynamics Specialist Conference. AIAA 2016-5671. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5671
• Woll, Edward. 1948. “Turbojet Engine Performance Characteristics with Reference to Methods of Augmentation.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/480070
• Woloshen, John R. 1974. Experimental Lateral Landing Computer with Inertial Stabilization. Defense Technical Information Center. https://doi.org/10.21236/ada043527
• Wood, George P. 1947. Performance Possibilities of the Turbojet System as a Power Plant for Supersonic Airplanes. NACA-RM-L7H05a. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930085860
• Wood, John D. 1961. Survey on Missile Structural Dynamics,. Defense Technical Information Center. https://doi.org/10.21236/ad0421632
• Wood, R., and D. Miller. 1984. “Impact of Fuselage Incidence on the Supersonic Aerodynamics of Two Fighter Configurations.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2193. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2193
• Woodbury, Timothy D., and John Valasek. 2015. “Synthesis and Flight Test of an Automatic Landing Controller Using Quantitative Feedback Theory.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-1073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1073
• Woodruff, Stephen. 2009. “Pitch-Axis Aerodynamic Parameter Identification for NASA’s F-15B.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5722
• Woodward, Kenneth E. 1961. Lower Cost Packaging for Guided Missile Electronics. Defense Technical Information Center. https://doi.org/10.21236/ad0255658
• Woodworth, John D. 1992. “A Simplified Sight Reduction Method for Celestial Navigation.” Navigation 39 (4): 463–75. https://doi.org/10.1002/j.2161-4296.1992.tb02288.x
• Wortman, A. 1984. “On Reynolds Number Effects in Vortex Flow over Aircraft Wings.” In 22nd Aerospace Sciences Meeting. AIAA 1984-137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-137
• Wright, J. J., and D. E. Zissa. 1984. Optical Contacting for Gravity Probe Star Tracker. NASA-TM-86475. NASA. https://ntrs.nasa.gov/citations/19850002511
• Wrigley, Walter. 1950. “Schuler Tuning Characteristics in Navigational Instruments.” Navigation 2 (8): 282–90. https://doi.org/10.1002/j.2161-4296.1950.tb00579.x
• Wrigley, W. 1977a. “History of Inertial Navigation.” Navigation 24 (1): 1–6. https://doi.org/10.1002/j.2161-4296.1977.tb01262.x
• Wrigley, Walter. 1977b. “The History of Inertial Navigation.” Journal of Navigation 30 (1): 61–68. https://doi.org/10.1017/s0373463300043642
• Wu, Yuanxin. 2025b. “Crossroads of Inertial Navigation Computation across Five Decades.” Preprint, . https://doi.org/10.36227/techrxiv.174234637.71721339/v1
• Wu, Xiaosheng, Wenyuan Chen, and Weiping Zhang. 2002a. “Optimum Design of Levitating Coil and Stability Coils in the Micromachined Gyroscope of Electromagnetic Levitated Rotor.” In SPIE Proceedings, vol. 4928, edited by Guofan Jin, John S. McKillop, Kazuhiro Hane. SPIE. https://doi.org/10.1117/12.483158
• Wu, Peng, Lu Feng, Haibo Tong, and Zhuxian Zhang. 2022. “Approximate Position Estimation Method of Weak-Signal Receiver of Global Navigation Satellite Systems Assisted by Barometric Altimeter.” Traitement du Signal 39 (3): 945–50. https://doi.org/10.18280/ts.390321
• Wu, Yuanxin, Xiaoping Hu, Dewen Hu, and Tao Wu. 2005a. “Observability Analysis of Rotation Estimation by Fusing Inertial and Line-Based Visual Information: A Revisit.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6069
• Wu, Allen, Eric Johnson, and Alison Proctor. 2005b. “Vision-Aided Inertial Navigation for Flight Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-5998. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5998
• Wu, Jianhua, Gang Li, Jian Chen, Shiyou Xu, and Zengping Chen. 2015a. “Rapid High-Accuracy Modeling Simulation Method for Full Trajectory of the Ballistic Missile.” In Proceedings of PIERS 2015 in Prague, Czech Republic. The Electromagnetics Academy. https://doi.org/10.2532/piers150305044332
• Wu, Chao, Sitan Li, and Fan Yang. 2025. “Analysis of Nose Landing Gear Shimmy Based on Multi-Body Dynamics Simulations.” Journal of Physics: Conference Series 3078 (1): 012023. https://doi.org/10.1088/1742-6596/3078/1/012023
• Wu, Zhanghua, Yunnan Li, Zhishuai Yu, and Zhemin Zhu. 2024. “The Numerical Simulation and Test Verification of the Inlet Total Pressure Distortion of a Core Aero-Engine.” Gas Turbine Experiment and Research 37 (1): 26–31. https://doi.org/10.3724/j.gter.20240004
• Wu, Y., and R. Ornedo. 1990. “Kalman Filter Formulation for Transfer Alignment of Inertial Reference Units.” In Guidance, Navigation and Control Conference. AIAA 1990-3364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3364
• Wu, Helong, Lijun Sun, Yang Hu, and Jianfeng Yang. 2023a. “Integrated Navigation Algorithm Based on Vision-Inertial Extended Kalman Filter for Low-Cost Unmanned Aerial Vehicle.” In International Conference on Computer, Artificial Intelligence, and Control Engineering (CAICE 2023), edited by Aniruddha Bhattacharjya, Xin Feng. SPIE. https://doi.org/10.1117/12.2681101
• Wu, Lin, Xin Tian, Hong Ma, and Jinwen Tian. 2011a. “A Matching-Unscented Kalman Filtering for Gravity Aided Navigation.” In SPIE Proceedings, vol. 8003, edited by Tianxu Zhang, Nong Sang. SPIE. https://doi.org/10.1117/12.901640
• Wu, Junjie, and Lei Wang. 2024. “Temperature Error Compensation Method of Fiber Optic Gyroscope Based on Deep Learning.” Journal of Physics: Conference Series 2724 (1): 012031. https://doi.org/10.1088/1742-6596/2724/1/012031
• Wu, Lin, Hubiao Wang, Hua Chai, Houtse Hsu, and Yong Wang. 2015b. “Research on the Relative Positions-Constrained Pattern Matching Method for Underwater Gravity-Aided Inertial Navigation.” Journal of Navigation 68 (5): 937–50. https://doi.org/10.1017/s0373463315000235
• Wu, Lin, Hubiao Wang, Hua Chai, Lu Zhang, Houtse Hsu, and Yong Wang. 2018a. “Analysis and Selection of Global Marine Gravity/Gravity Gradient Aided Navigation Matching Areas.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-13-0029-5_74
• Wu, Zongshou, Lixin Wang, Shuanzhu Li, Can Li, Qiang Shen, and Xinsan Li. 2023b. “Segmented Regression Modeling and Temperature Drift Compensation in a Hemispherical Resonant Gyroscope Using Correlation Analysis.” Preprint, . https://doi.org/10.2139/ssrn.4499585
• Wu, Yuanxin, Meiping Wu, Xiaoping Hu, and Dewen Hu. 2009. “Self-Calibration for Land Navigation Using Inertial Sensors and Odometer: Observability Analysis.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5970. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5970
• Wu, Hao, and Zhiyu Zhang. 2023. “Analysis of the Development of Reusable Launch Vehicle Technology.” Applied and Computational Engineering 11 (1): 65–75. https://doi.org/10.54254/2755-2721/11/20230209
• Wu, Qilong, Qidan Zhu, Lunpan Wei, Lipeng Wang, and Wenqiang Jiang. 2026b. “Reliability Analysis of an Automatic Carrier Landing System Based on Predefined-Time Fault-Tolerant Control under Air-Wake Disturbances and Actuator Faults.” Aircraft Engineering and Aerospace Technology 98 (4): 516–26. https://doi.org/10.1108/aeat-08-2025-0295
• Wu, Feng, Xifang Zhu, Qingquan Xu, et al. 2019b. “Optimization of Guide Star Catalog for Daytime Star Sensors.” International Journal of Modern Physics B 34 (01n03): 2040065. https://doi.org/10.1142/s0217979220400652
• Wyatt, Demarquis. 1953. An Analysis of Turbojet-Engine-Inlet Matching. NACA-TN-3012. NASA. https://ntrs.nasa.gov/citations/19930083723
• Wyatt, David, and Mike Tooley. 2013a. “5 Inertial Navigation Accuracy.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780080941523-108
• Wyatt, David, and Mike Tooley. 2013b. “Aircraft Navigation.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780080941523-60
• Wyatt, David, and Mike Tooley. 2013c. “Inertial Navigation Systems.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780080941523-105
• Wyatt, David, and Mike Tooley. 2013d. “Microwave Landing System.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780080941523-86
• Xi, Menghan, Lin Wu, Qianqian Li, et al. 2024. “Matching Area Selection for Arctic Gravity Matching Navigation Based on Adaptive All-Field Extended Extremum Algorithm.” IET Radar, Sonar & Navigation 18 (8): 1307–17. https://doi.org/10.1049/rsn2.12571
• Xi, Xiang, Dingbang Xiao, Li Wei, et al. 2020. “Analysis of Assembly Errors and Design of Precise Micro-Regulator for Micro-Hemispherical Resonator Gyroscope (mHRG).” Journal of Mechanical Engineering 56 (13): 77. https://doi.org/10.3901/jme.2020.13.077
• Xiang, Zongwei, Guang Feng, Yiyao Jiang, Jianbin Ding, and Bingyan Jiang. 2022b. “Study on the Shimmy Stability of Aircraft Nose Landing Gear with the Radial and Axial Clearance at Torque Link Connection.” In International Conference on Mechanical Design and Simulation (MDS 2022), edited by Dongyan Shi, Guanglei Wu. SPIE. https://doi.org/10.1117/12.2639053
• Xiang, Zhiyi, Qi Wang, Rong Huang, Chongbin Xi, Xiaoming Nie, and Jian Zhou. 2021. “In-Motion Initial Alignment Method for a Laser Doppler Velocimeter-Aided Strapdown Inertial Navigation System Based on an Adaptive Unscented Quaternion H-Infinite Filter.” Measurement Science and Technology 33 (3): 035001. https://doi.org/10.1088/1361-6501/ac37e9
• Xiao, Jing, Xiusheng Duan, Xiaohui Qi, and Yifei Liu. 2019. “An Improved ICCP Matching Algorithm for Use in an Interference Environment during Geomagnetic Navigation.” Journal of Navigation 73 (1): 56–74. https://doi.org/10.1017/s0373463319000535
• Xiao, Tao, Ming Hua Pan, and Guo Li Zhu. 2012. “Temperature Drift Modeling and Compensating of Fiber Optic Gyroscope.” Applied Mechanics and Materials 220-223: 1911–16. https://doi.org/10.4028/www.scientific.net/amm.220-223.1911
• Xiao, Xiangzhi, Yanying Zhao, Hao Zhen Wu, and Guisheng Zhu. 2025. “Dynamic Analysis of Nose Landing Gear Shimmy Considering Strut Height and Experiment on the Test Platform.” Open Journal of Applied Sciences 15 (04): 919–37. https://doi.org/10.4236/ojapps.2025.154062
• Xiao, Huiyunuo, Ziyang Zhen, Zhibing Zhang, and Fengying Zheng. 2024b. “Robust Fault-Tolerant Preview Control for Automatic Landing of Carrier-Based Aircraft.” Aircraft Engineering and Aerospace Technology 96 (5): 679–89. https://doi.org/10.1108/aeat-07-2023-0193
• Xie, Zenghua, Zhong’ao Jiang, Shuisheng Jian, and Wangbin Tao. 1998. “Resonance Characteristics of Fiber Optic Ring Resonator in Fiber Optical Resonator Gyroscope.” In SPIE Proceedings, vol. 3552, edited by Shuisheng Jian, Franklin F. Tong, Reinhard Maerz. SPIE. https://doi.org/10.1117/12.318028
• Xie, Tianyi, Huanzhen Liu, Yong-hui Qiao, Guowei Pan, and Shunqing Ren. 2025. “Second-Order Coefficient Calibration Method of Accelerometer in Platform Inertial Navigation System Tested on Double Turntable Centrifuge.” Advances in Engineering Technology Research 14 (1): 475. https://doi.org/10.56028/aetr.14.1.475.2025
• Xie, Lili, and Jiazhen Lu. 2016. “Optimisation-Based Transfer Alignment and Calibration Method for Inertial Measurement Vector Integration Matching.” Journal of Navigation 70 (3): 595–606. https://doi.org/10.1017/s0373463316000680
• Xie, Hairun, Yadong Wu, Anjenq Wang, and Hua Ouyang. 2015. “Numerical Investigation of Inlet Distortion for Different Rear Mounted Engine Installations at Taking-Off Conditions.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2015-42350
• Xie, Haitong, Honggang Zeng, Mingqiang Luo, Jian Zhai, and Ziliang Guo. 2026. “Study on a Passive Control Device for Inlet Unstart Mitigation via Shock Wave Attenuation.” Preprint, . https://doi.org/10.2139/ssrn.6770201
• Xin, Ming, and S. Balakrishnan. 2003. “Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-577
• Xing, Fei, Ying Dong, and You Zheng. 2006. “Laboratory Calibration of Star Tracker with Brightness Independent Star Identification Strategy.” Optical Engineering 45 (06): 1–9. https://doi.org/10.1117/1.2213996
• Xingjian, Zhu, Wang Xueyu, and Yan Qingjin. 1985. “Convergence of Performance Calculation of Twin Spool Turbojet and Turbofan.” In Volume 1: Aircraft Engine; Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/85-igt-82
• Xingyu, Li, and Jiang Tingting. 2016. “Strap-down Inertial Navigation System Initial Alignment Based on Iterative Square-Root Cubature Kalman Filter.” International Journal of Control and Automation 9 (3): 319–28. https://doi.org/10.14257/ijca.2016.9.3.29
• Xiong, Xingguo, and Haifeng Dong. 2011. “Design of a MEMS Gyroscope with Glass-Silicon-Glass Sandwich Structure.” Micro and Nanosystemse 3 (1): 26–34. https://doi.org/10.2174/1876402911103010026
• Xiong, Ling, Kaihan Li, Jianqiao Tang, and Jie Ma. 2015. “Research on Matching Area Selection Criteria for Gravity Gradient Navigation Based on Principal Component Analysis and Analytic Hierarchy Process.” In SPIE Proceedings, vol. 9815, edited by Jianguo Liu, Hong Sun. SPIE. https://doi.org/10.1117/12.2204819
• Xiong, Ling, Jie Ma, Li Zhang, Jin-Wen Tian, and Jian Liu. 2007. “Submarine Navigation Based on Gravity Gradient-Terrain Matching.” In SPIE Proceedings, vol. 6790, edited by Yongji Wang, Jun Li, Bangjun Lei, Jingyu Yang. SPIE. https://doi.org/10.1117/12.749800
• Xiong, B., C. Tang, Q. Wang, and S. P. Zhu. 2017. “Research on the Modeling of Random Drift Error and Filtering Technology of Low Cost Mems Gyroscope.” Modelling, Measurement and Control A 90 (1): 16–31. https://doi.org/10.18280/mmc_a.900102
• Xiong, Neng, Yang Tao, Zhiyong Liu, and Jun Lin. 2018b. “Uncertainty Quantification-Based Robust Aerodynamic Optimization of Laminar Flow Nacelle.” Modern Physics Letters B 32 (12n13): 1840048. https://doi.org/10.1142/s0217984918400481
• Xiong, K., and H. Y. Zhang. 2007. “Local Approach for Fault Detection in Redundant Sensor Configuration.” In Fault Detection, Supervision and Safety of Technical Processes 2006. Elsevier. https://doi.org/10.1016/b978-008044485-7/50102-0
• Xu, Yunjun. 2005a. “Trajectory Control and Analysis for the Vertical Takeoff and Vertical Landing Reusable Launch Vehicle’s Upper Stage.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-5996. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5996
• Xu, Yunjun. 2009. “Trajectory Analysis for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle’s Upper Stage.” Journal of Aerospace Engineering 22 (1): 58–66. https://doi.org/10.1061/(asce)0893-1321(2009)22:1(58)
• Xu, Lixin. 2023. “Design of a New Sweptback Wing for a Future Supersonic Aircraft—Research on Lift Drag Characteristics and Aerodynamic Analysis.” Theoretical and Natural Science 18 (1): 1–9. https://doi.org/10.54254/2753-8818/18/20230256
• Xu, Baoxiang, Yunqiang Fan, Dongfa Ding, and Wenshuai Feng. 2018. “Study on Life Evaluation Technology of Fiber Optic Gyroscope in Space Application.” In Fiber Optic Sensing and Optical Communication, edited by Qunbi Zhuge, Jie Zhang, Songnian Fu, Ming Tang, Tuan Guo. SPIE. https://doi.org/10.1117/12.2505473
• Xu, Hongyang, Hongjun Li, Guicai Fang, and Yonghua Fan. 2021b. “Robust Sliding Mode Control for Hypersonic Cruise Missile Using Dynamic Pressure Feedback.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_337
• Xu, D. Y., Y. Shen, W. Huang, Z. Y. Guo, H. Zhang, and D. F. Xu. 2024. “Parametric Modelling and Variable-Fidelity Bayesian Optimization of Aerodynamics for a Reusable Flight Vehicle.” Fluid Dynamics 59 (6): 2083–95. https://doi.org/10.1134/s0015462824603814
• Xu, Jintao, and Ailing Tian. 2023. “Reliability Analysis of Spherical Six Axis Redundant Inertial Measurement Unit.” In Third International Conference on Sensors and Information Technology (ICSI 2023), edited by Hemachandran Kannan, Jude Hemanth. SPIE. https://doi.org/10.1117/12.2679329
• Xu, Guoping, Weifeng Tian, and Zhihua Jin. 2005. “An AGO–SVM Drift Modelling Method for a Dynamically Tuned Gyroscope.” Measurement Science and Technology 17 (1): 161–67. https://doi.org/10.1088/0957-0233/17/1/026
• Xu, Guoping, Weifeng Tian, Zhihua Jin, and Li Qian. 2007b. “Temperature Drift Modelling and Compensation for a Dynamically Tuned Gyroscope by Combining WT and SVM Method.” Measurement Science and Technology 18 (5): 1425–32. https://doi.org/10.1088/0957-0233/18/5/030
• Xu, Yongjie, Zhijun Wang, and Fangdong Dong. 2020a. “Ballistic Trajectory Modeling for Missile with Deflectable Nose.” Mechanics 26 (5): 450–56. https://doi.org/10.5755/j01.mech.26.5.27874
• Xu, Ziqin, Haonan Xu, Chang Liu, Zeyu Kang, and Zibo Wei. 2025a. “Design and Simulation of Automatic Flare Control Law for Civil Aircrafts.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2220-7_36
• Xu, Jinjiang, Feiyu Yao, Jie Zhao, et al. 2026b. “Optimization of Bias Stability in an Interferometric Fiber Optic Gyroscope via Optical Switch Modulation.” Applied Physics Letters 128 (9): 094103. https://doi.org/10.1063/5.0313770
• Xu, Wei, and Fu Zhang. 2024. “Fast-Lio: A Fast, Robust Lidar-Inertial Odometry Package by Tightly-Coupled Iterated Kalman Filter.” Preprint, . https://doi.org/10.2139/ssrn.4675587
• Xuan, Zewei. 2026. “MBSE-Based Fault Analysis of Aircraft Landing Gear.” Applied and Computational Engineering 214 (1): 224–30. https://doi.org/10.54254/2755-2721/2026.bj33521
• Xudong, 于旭东 Yu, 张鹏飞 Zhang Pengfei, 谢元平 Xie Yuanping, and 龙兴武 Long Xingwu. 2013. “Forecasting Method for Axial Ring Laser Gyroscope Drifts in Single-Axis Rotation Inertial Navigation System.” High Power Laser and Particle Beams 25 (4): 847–52. https://doi.org/10.3788/hplpb20132504.0847
• Xue, Yuanyuan, Wenjian Chen, Kang Tingting, Chen Ying, Zhang Xiajiang, and Yang Yuancheng. 2016. “Inertial Compensation Method for LOS Drift of Gyroscope Stabilization Platform.” Journal of Applied Optics 37 (2): 177–82. https://doi.org/10.5768/jao201637.0201005
• Xue, Weili, Zhen Sun, Kehui Ma, and Ling Pei. 2022. “Photorealistic Simulation Platform for Autonomous Landing of Fixed-Wing Aircraft.” Journal of Global Positioning Systems 18 (2): 103. https://doi.org/10.5081/gps.18.2.103
• Yager, Thomas J. 1993. “Aircraft Nose Gear Shimmy Studies.” SAE technical papers on CD-ROM/SAE technical paper series. https://doi.org/10.4271/931401
• Yager, Thomas J. 1996. “NASA Boeing 737 Aircraft Test Results from 1996 Joint Winter Runway Friction Measurement Program.” In International Meeting on Aircraft Performance on Contaminated Runways (IMAPCR ‘‘96). https://ntrs.nasa.gov/citations/19970000907
• Yager, Thomas J., and William A. Vogler. 1989. Current Status of Joint FAA/NASA Runway Friction Program. SAE PAPER 892340. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19900058439
• Yager, Thomas J., William A. Vogler, and Paul Baldasare. 1990. Evaluation of Two Transport Aircraft and Several Ground Test Vehicle Friction Measurements Obtained for Various Runway Surface Types and Conditions. a Summary of Test Results from Joint FAA/NASA Runway Friction Program. NASA-TP-2917. NASA. https://ntrs.nasa.gov/citations/19900006586
• Yager, Thomas J., James C. Wambold, John J. Henry, Arild Andresen, and Matthew Bastian. 2002. Joint Winter Runway Friction Program Accomplishments. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20030003719
• Yaghmaee, S., and D. Roberts. 1986. “A Numerical Algorithm for Simulating 3D Viscous Supersonic Inlet Flows.” In 24th Aerospace Sciences Meeting. AIAA 1986-552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-552
• Yakubayev, Ernest, Kyle Gschwend, Samuel Robertson, Adam Cox, Christian Perron, and Dimitri Mavris. 2026. “Towards Selection of a Hypersonic Glide Vehicle Aerothermal Common Research Model Configuration.” In AIAA SCITECH 2026 Forum. AIAA 2026-1095. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1095
• Yamada, Hidemitsu, and Kazuhiko Hasegawa. 1999. “Autopilot Using Model Reference Adaptive Control System with Variable Adaptive Gain.” Journal of the Society of Naval Architects of Japan 1999 (185): 143–50. https://doi.org/10.2534/jjasnaoe1968.1999.143
• Yamazaki, Yuki, Kazuhide Mizobata, and Kazuyuki Higashino. 2019. “Drag Reduction on the Basis of the Area Rule of the Small-Scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 17 (2): 127–33. https://doi.org/10.2322/tastj.17.127
• Yamron, J. 1968. Description of a Strapdown Inertial Measurement Unit. United Aircraft Corporate Systems Center. https://ntrs.nasa.gov/citations/19690027478
• Yan, Hong. 2013. “Near-Surface Discharge in Supersonic Inlet Control.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-530
• Yan, Li, and Chenfeng Cui. 2007. “A New Algorithm of Gravity Matching Aided Navigation.” In SPIE Proceedings, vol. 6795, edited by Cheng Wang, Shan Zhong, Jiaolong Wei. SPIE. https://doi.org/10.1117/12.774209
• Yan, Jinyun, Jie Jiang, and Guangjun Zhang. 2016. “Dynamic Imaging Model and Parameter Optimization for a Star Tracker.” Optics Express 24 (6): 5961. https://doi.org/10.1364/oe.24.005961
• Yan, Jinyun, Jie Jiang, and Guangjun Zhang. 2017b. “Modeling of Intensified High Dynamic Star Tracker.” Optics Express 25 (2): 927. https://doi.org/10.1364/oe.25.000927
• Yan, Li, Xudong Ma, Juan Shi, and Yulong Shi. 2009. “Extraction Method of Suitable Matching Regions in the Gravity-Aided Inertial Navigation.” In SPIE Proceedings, vol. 7492, edited by Yaolin Liu, Xinming Tang. SPIE. https://doi.org/10.1117/12.837840
• Yan, Daiwei, Lei Pan, and Liangxian Gu. 2008. “Estimation the Mission Effectiveness of Hypersonic Cruise Missile in Conceptual Design.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-176. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-176
• Yan, XiaoDong, and Zhi Wang. 2012. “Three-Dimensional Trajectory Planning Method for Hypersonic Glide Vehicle.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5897. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5897
• Yan, Lin, and Lei Wang. 2025. “Research on Temperature Error Model of Fiber Optic Gyroscope Drift.” In International Conference on Laser, Optical Technology, and Applications (LOTA 2025), edited by Lei Zhang, Yang Yue. SPIE. https://doi.org/10.1117/12.3091364
• Yan, Kaichen, Xiaoxu Wang, Xiquan Wang, and Qianbo Lu. 2025. “Real-Time Identification and Compensation of Phase Error for Whole-Angle Hemispherical Resonator Gyroscope Based on Forgetting Filter and Virtual Rotation.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2252-8_50
• Yan, Li, and Hualing Wu. 2007. “Research on the Selection of Suitable Matching Area in the Gravity Aided Navigation.” In SPIE Proceedings, vol. 6752, edited by Weimin Ju, Shuhe Zhao. SPIE. https://doi.org/10.1117/12.761350
• Yan, Hao, Jun Wei Yang, Liang Chen, and Jin Hui Hao. 2012. “Research on Random Drift Modeling and Error Compensation Method for MEMS Gyroscope.” Advanced materials research 466-467: 925–29. https://doi.org/10.4028/www.scientific.net/amr.466-467.925
• Yan, Fei, Wangyang Zhao, Xingling Wang, Kai Wang, and Yuanming Wang. 2021. “Research on Master-Slave Filtering of Celestial Navigation System / Inertial Navigation System.” Journal of Physics: Conference Series 1732 (1): 012189. https://doi.org/10.1088/1742-6596/1732/1/012189
• Yan, Xingxu, Junyang Zhao, Zhiqian Zhao, Zhaofa Zhou, and Zeqian Xu. 2023a. “A Method for Improving Precision Alignment Accuracy of Strapdown Inertial Navigation.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_491
• Yang, Chizhao. n.d. “Localization Algorithms for GNSS-Denied and Challenging Environments.” PhD diss., West Virginia University Libraries. https://doi.org/10.33915/etd.10278
• Yang, Eui-Hyeok. 2004. Making Precise Resonators for Mesoscale Vibratory Gyroscopes. NPO-30431. California Inst. of Tech. https://ntrs.nasa.gov/citations/20110016855
• Yang, Dong Sheng. 2012. “Technology Research of Digital Closed-Loop Fiber-Optic Gyroscope.” Applied Mechanics and Materials 241-244: 1056–59. https://doi.org/10.4028/www.scientific.net/amm.241-244.1056
• Yang, Dong Sheng. 2014. “Multiplexing Technology Research of Fiber Optic Gyroscope.” Applied Mechanics and Materials 574: 494–97. https://doi.org/10.4028/www.scientific.net/amm.574.494
• Yang, Soo Seok. 2020. “Sensitivity Analysis of Major Cost Parameters on the Launch Cost of Reusable Vehicles.” Journal of the Korean Society of Propulsion Engineers 24 (2): 35. https://doi.org/10.6108/kspe.2020.24.2.035
• Yang, Shunfu, Lu Gan, Tianyi Wang, Enze Zhu, Ling Yang, and Hu Chen. 2024a. “Compound Attitude Control Strategy for Reusable Launch Vehicle Based on Improved PSO Algorithm.” Preprint, . https://doi.org/10.20944/preprints202405.1410.v1
• Yang, Yuan, Wanxiang Gou, Chonghui Li, Shuai Tong, Chao Zhang, and Junzhang Zhang. 2024b. “Method of Star Point Extraction for Daytime Infrared Star Image.” Chinese Journal of Space Science 44 (5): 948. https://doi.org/10.11728/cjss2024.05.2023-0123
• Yang, Yong, Defeng Hu, and Menglun Yu. 2006. “Roadmap of Long-March Reusable Launch Vehicle.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-d2.4.03
• Yang, Yafei, and Xin Huo. 2008. “Determination of Optimal Observable Subspace for Strapdown Inertial Navigation Systems through Observability Analysis.” In SPIE Proceedings, vol. 7133, edited by Jiubin Tan, Xianfang Wen. SPIE. https://doi.org/10.1117/12.807615
• Yang, Xiaoxi, Baokuan Li, Yang Nie, and Zhibo Ren. 2026b. “Effects of Jet Exhaust on Engine Inlet Distortion during Carrier-Based Aircraft Takeoff.” Thermal Science 30 (2 Part B): 1547–61. https://doi.org/10.2298/tsci250222228y
• Yang, G., X. Li, Xufeng Zheng, and T. Song. 2025d. Research on Calculation Method of Vertical Deflection Based on Gravity Data. https://doi.org/10.3997/2214-4609.202572027
• Yang, Wenguo, Jieyu Liu, Can Li, and Qiang Shen. 2025e. “Supplementary Correction Algorithm for Integrated Navigation under Insufficient Initial Alignment.” Preprint, . https://doi.org/10.2139/ssrn.5624102
• Yang, G., and X. S. Song. 2023. “Circular Probability Error Based Inertial Navigation System Assists Ultra-Wide Band and Satellite Navigation System Intersection Area Fusion Positioning Algorithm.” Journal of Communications Technology and Electronics 68 (5): 540–50. https://doi.org/10.1134/s1064226923050182
• Yang, Chizhao, Jared Strader, Yu Gu, Alexander Hypes, Aaron Canciani, and Kevin Brink. 2018a. “Cooperative UAV Navigation Using Inter-Vehicle Ranging and Magnetic Anomaly Measurements.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1595
• Yang, Yiyan, Zhaoyang Tian, Xue Yang, Xiaowei Liu, and Lei Shi. 2024c. “Start/unstart Hysteresis Characteristics Driven by Embedded Rocket of a Rocket-Based Combined-Cycle Inlet.” Physics of Fluids 36 (8): 086101. https://doi.org/10.1063/5.0212881
• Yang, Chun, Ananth Vadlamani, Andrey Soloviev, Michael Veth, and Clark Taylor. 2018b. “Feature Matching Error Analysis and Modeling for Consistent Estimation in Vision-Aided Navigation.” NAVIGATION 65 (4): 609–28. https://doi.org/10.1002/navi.265
• Yang, Yuanhong, and Fuling Yang. 2016. “High Performance Fiber Optic Gyroscope with a Radiation-Tolerant and Temperature-Stable Scale Factor.” Chinese Optics Letters 14 (11): 110605–9. https://doi.org/10.3788/col201614.110605
• Yang, Xue, Yiyan Yang, Zhaoyang Tian, Junhua Zhang, and Lei Shi. 2023b. “Spatiotemporal Flow Evolution in a Rocket-Based Combined-Cycle Inlet during Ejector-to-Ramjet Mode Transition.” Physics of Fluids 35 (10): 107105. https://doi.org/10.1063/5.0171301
• Yang, Huabo, Lijun Zhang, and Yuan Cao. 2011. “Error Separation Techniques Based on Telemetry and Tracking Data for Ballistic Missile.” In InTech eBooks. https://doi.org/10.5772/24761
• Yang, Jing, Baoqiang Zhang, Qing Chen, and Guoqiang Su. 2017. “Quantification of Margins and Uncertainties Approach for Aerothermoelastic Analysis Based on Non-Intrusive Polynomial Chaos Method.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2395. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2395
• Yang, Shaohua, Xiaodong Zhang, Guanjie Wang, Rui Zhang, and Zhenwei Li. 2023a. “A Novel Integrity Monitoring Method for Slowly Growing Errors in Inertial Navigation System/global Navigation Satellite System Integrated Navigation System.” IET Radar, Sonar & Navigation 18 (3): 434–47. https://doi.org/10.1049/rsn2.12488
• Yang, Fuling, Mengyu Zhao, Shuai Liang, Linke Song, and Yan Li. 2022b. “Faraday Drift Suppression Based on Dispersion Compensation Factor and Broadband Source Parameters in a Differential Fiber Optic Gyroscope.” Optical Engineering 61 (03): 1–13. https://doi.org/10.1117/1.oe.61.3.034105
• Yang, Zhenli, Zhuangsheng Zhu, and Weigao Zhao. 2013. “A Triangle Matching Algorithm for Gravity-Aided Navigation for Underwater Vehicles.” Journal of Navigation 67 (2): 227–47. https://doi.org/10.1017/s0373463313000660
• Yanushevsky, Rafael. 2007b. “Pseudo-Classical Missile Guidance.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6781
• Yanushevsky, Rafael T. 2018a. “Analysis of PN Guided Missile Systems in the Frequency Domain.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-4
• Yanushevsky, Rafael T. 2018b. “Analysis of PN Guided Missile Systems in the Time Domain.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-3
• Yanushevsky, Rafael T. 2018c. “Basics of Missile Guidance.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-1
• Yanushevsky, Rafael T. 2018d. “Missile Guidance Software.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-12
• Yao, Dongdong, Yandong Hu, Dawei Liu, and Qunli Xia. 2023. Sliding Mode Formation Control for Multiple Hypersonic Glide Vehicles. https://doi.org/10.5220/0012150900003562
• Yao, Jie, and Fazle Hussain. 2019. “Supersonic Turbulent Boundary Layer Drag Control Using Spanwise Wall Oscillation.” Journal of Fluid Mechanics 880: 388–429. https://doi.org/10.1017/jfm.2019.727
• Yao, Zhuoer, Daochun Li, Jinwu Xiang, and Zi Kan. 2025. “Adaptive Prescribed Time Control Method for Automatic Carrier Landing System.” Guidance, Navigation and Control 05 (03): 297–309. https://doi.org/10.1142/s2737480725500062
• Yao, Yao, Xiaobo Zhang, Mingyang Zhang, and Zhanxue Wang. 2022. “Modeling and Cycle Parameter Matching of a High-Speed Variable Cycle Turbofan-Ramjet Engine.” In Volume 1: Aircraft Engine; Ceramics and Ceramic Composites. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2022-80505
• Yavuztürk, Vefa N., Eren Topbas, Ümit Kutluay, and Yigit Yazicioglu. 2017. “Flight Test Maneuver Design and Aerodynamic Parameter Estimation for Single Use Autonomous Gliding Air Vehicles.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-1865. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1865
• Ye, Shida, Yaakov Bar-Shalom, Peter K. Willett, and Ahmed Zaki. 2025b. “Maximum Likelihood Identification of an Inertial Sensor Error Model Combining GM1, WP, and WN.” In Signal Processing, Sensor/Information Fusion, and Target Recognition XXXIV, edited by Lynne L. Grewe, Erik P. Blasch, Ivan Kadar. SPIE. https://doi.org/10.1117/12.3059824
• Ye, Kun, Zhenghao Feng, Xiran Liu, and Zhengyin Ye. 2022. “Numerical Investigation of the Influence of Aerothermoelastic Dynamic Response on the Performance of the Three-Dimensional Hypersonic Inlet.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 236 (10): 2131–47. https://doi.org/10.1177/09544100211050754
• Ye, Jiangnan, Jinshun Wang, Lei Wang, Junxiang Pang, and Haorui Du. 2025a. “Improving Attitude Accuracy in Rotating Inertial Navigation Systems: Calibration and Online Compensation.” Preprint, . https://doi.org/10.2139/ssrn.5084914
• Ye, Song, and Min Zhang. 2017. “Analysis of Generalized Likelihood Test Method Deficiencies and Improvements for Fault Detection and Isolation of Redundant Strapdown Inertial Measurement Unit.” In Mechatronics and Automation Engineering. WORLD SCIENTIFIC. https://doi.org/10.1142/9789813208537_0041
• Ye, Xifa, Ouya Zhang, Xinqi Li, and Yanfen Qiu. 2019c. “Tracking Algorithm for Cruise Missile Based on IMM-Singer Model.” In AIP Conference Proceedings, vol. 2073. Author(s). https://doi.org/10.1063/1.5090750
• Ye, Tao, and Fuqiang Zhou. 2015. “Autonomous Space Object Tracking and Azimuth Determination Using Star Tracker Technique under Complex Space Environment.” In SPIE Proceedings, vol. 9524, edited by Anand K. Asundi, Yu Fu. SPIE. https://doi.org/10.1117/12.2185587
• Yeager, Richard A., and Laurence W. Gertsma. 1958. Investigation of an Underslung Half-Cone Inlet with Compression Surface Mounted Outboard from Fuselage at Mach Numbers of 1.5, 1.8, and 2.0. NACA-RM-E58A27b. NASA. https://ntrs.nasa.gov/citations/19930090049
• Yefeng, Xu, Li Kui, Yang Guoliang, and He Mengke. 2012. “Error Modeling and Compensation for Rotation-Modulation Strapdown Inertial Navigation System.” Advanced Science Letters 5 (2): 981–85. https://doi.org/10.1166/asl.2012.1850
• Yegorov, S. N., and A. F. Diumin. 1996. “Problems of Orbital Gyrocompassing.” TURKISH JOURNAL OF PHYSICS 20 (8): 915–21. https://doi.org/10.55730/1300-0101.2512
• Yeh, David, and Roger Clark. 2007. “Numerical Study of Vortex Flows around a Supersonic Transport High-Lift Configuration with Forebody Control Surfaces.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4448
• Yeh, T-J., C-Y. Su, and W-J. Wang. 2005. “Modelling and Control of a Hydraulically Actuated Two-Degree-of-Freedom Inertial Platform.” Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 219 (6): 405–17. https://doi.org/10.1243/095965105x33527
• Yeom, Hyo-Won, Hong-Gye Sung, and Vigor Yang. 2015. “A Numerical Analysis of Supersonic Intake Buzz in an Axisymmetric Ramjet Engine.” International Journal of Aeronautical and Space Sciences 16 (2): 165–76. https://doi.org/10.5139/ijass.2015.16.2.165
• Yertutanol, Aylin, Önder Akçaalan, Serdar Öğüt, Ekmel Özbay, and Abdullah Ceylan. 2021. “Fiber-Optic Gyroscope for the Suppression of a Faraday-Effect-Induced Bias Error.” Optics Letters 46 (17): 4328. https://doi.org/10.1364/ol.436195
• Yi, Baidong. 2016. “Missile System Equipment Operational Reliability Analysis.” In Proceedings of the 2016 International Conference on Artificial Intelligence: Technologies and Applications. Atlantis Press. https://doi.org/10.2991/icaita-16.2016.87
• Yi, Mi-Seon, Jae-Sung Bae, and Jae-Hyuk Hwang. 2011. “Non-Linear Shimmy Analysis of a Nose Landing Gear with Friction.” Journal of the Korean Society for Aeronautical & Space Sciences 39 (7): 605–11. https://doi.org/10.5139/jksas.2011.39.7.605
• Yi, Mi-Seon, Jae-Up Hwang, Jae-Sung Bae, and Jae-Hyuk Hwang. 2010. “Non-Linear Shimmy Analysis of a Nose Landing Gear with Free-Play.” Journal of the Korean Society for Aeronautical & Space Sciences 38 (10): 973–78. https://doi.org/10.5139/jksas.2010.38.10.973
• Yi, Yao, Shi Kun, Lu Weidong, and Jian Shuisheng. 1995. “All-Fiber Ring Resonator Gyroscope.” Chinese Physics Letters 12 (4): 213–16. https://doi.org/10.1088/0256-307x/12/4/007
• Yim, Jong-bin, You-chol Lim, and Joon Lyou. 2005. “A Stellar-Inertial Navigation Scheme.” In SPIE Proceedings, vol. 6041, edited by Yunlong Wei, Kil To Chong, Takayuki Takahashi, Shengping Liu, Zushu Li, Zhongwei Jiang, Jin Young Choi. SPIE. https://doi.org/10.1117/12.664374
• Yip, L. P. 1985. Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Airplane. NASA-TP-2382. NASA. https://ntrs.nasa.gov/citations/19850011615
• Yip, L. P., and P. F. Coy. 1982. Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Aircraft. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19820057489
• Yip, L. P., L. P. Parlett, R. L. Roensch, J. E. Felix, and H. R. Welge. 1980. “Results of a Low-Speed Wind Tunnel Test of the MDC 2.2M Supersonic Cruise Aircraft Configuration.” In Supersonic Cruise Res. 1979, Pt. 1. https://ntrs.nasa.gov/citations/19810009460
• Yip, L. P., and J. W. Paulson Jr. 1977. Effects of Deflected Thrust on the Longitudinal Aerodynamic Characteristics of a Close-Coupled Wing-Canard Configuration. NASA-TP-1090. NASA. https://ntrs.nasa.gov/citations/19780005071
• Yntema, Robert T., and Benjamin Milwitzky. 1952. An Impulse-Momentum Method for Calculating Landing-Gear Contact Conditions in Eccentric Landings. NACA-TN-2596. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19930083424
• Yoko, Matthew. 2024. “Optimal Experiment Design with Adjoint-Accelerated Bayesian Inference.” Preprint, . https://doi.org/10.52843/cassyni.by16mj
• Yoo, S., and T. Bullock. 1989. “Missile Guidance Based on Weight Adjusted Singular Perturbation.” In Guidance, Navigation and Control Conference. AIAA 1989-3482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3482
• Yoon, Hyosang, Kiwook Baeck, and Junsung Wi. 2022. “Star Tracker Geometric Calibration through Full-State Estimation Including Attitude.” International Journal of Aeronautical and Space Sciences 23 (1): 180–91. https://doi.org/10.1007/s42405-021-00432-5
• York, R., and H. Pastrick. 1976. “Optimal Terminal Guidance with Constraints at Final Time.” In Guidance and Control Conference. AIAA 1976-1916. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1916
• Yoshida, Kenji. 2009. “Supersonic Drag Reduction Technology in the Scaled Supersonic Experimental Airplane Project by JAXA.” Progress in Aerospace Sciences 45 (4–5): 124–46. https://doi.org/10.1016/j.paerosci.2009.05.002
• Yoshimoto, Minoru, and Naoki Uchiyama. 2003. “Optimization of Canard Surface Positioning of Supersonic Business Jet for Low Boom and Low Drag Design (Invited).” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3576. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3576
• Yoshino, Toshihiko, Nobuaki Yoshida, and Makoto Nara. 1986. “Geodesical Surveying Fiber-Optic Gyroscope.” In Optical Fiber Sensors. OSA. https://doi.org/10.1364/ofs.1986.86
• You, Dong Il, Yeun Deuk Jung, Sung Wook Cho, Hee Min Shin, Sang Hyup Lee, and David Hyunchul Shim. 2012. “A Guidance and Control Law Design for Precision Automatic Take-off and Landing of Fixed-Wing UAVs.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4674. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4674
• Youngblood, John N. 1977. Optimal Guidance for Modular Weapons with Digital Autopilots. Defense Technical Information Center. https://doi.org/10.21236/ada040449
• Youssef, Hussein, Stephen Reiman, Charles Dillon, and Howard Lee. 2008. “Adaptive Reconfigurable Dynamic Inversion Control for a Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7466. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7466
• Youssef, Hussein, Stephen Reiman, Charles Dillon, and Howard Lee. 2009. “Robust Adaptive Reconfigurable Control for a Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6185
• Yu, Nan. 2006. “Atom-Interferometer Gravity Gradiometer for Space and UGS Detection Applications.” In National Center for Physical Acoustics Advanced Concept for Shallow Tunnel Detection. https://ntrs.nasa.gov/citations/20060043724
• Yu, Hao. 2012. “Vibration Character Analysis and Calculation for Hemispherical Resonator Gyro.” Applied Mechanics and Materials 271-272: 1224–28. https://doi.org/10.4028/www.scientific.net/amm.271-272.1224
• Yu, N., H. Chen, and S. Samant. 1983. “Inviscid Drag Calculations for Transonic Flows.” In 6th Computational Fluid Dynamics Conference Danvers. AIAA 1983-1928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1928
• Yu, Zhengshi, and John L. Crassidis. 2016. “Accelerometer Bias Calibration Using Attitude and Angular Velocity Information.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-1140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1140
• Yu, Chih-Jen, Chih-Ching Ho, and I-Hsuan Chen. 2025b. “Heterodyne Interferometric Fiber-Optic Gyroscope.” Open Physics 23 (1): 20250229. https://doi.org/10.1515/phys-2025-0229
• Yu, Nan, James M. Kohel, James R. Kellogg, and Lute Maleki. 2005. “Towards a Space-Borne Quantum Gravity Gradiometer: Progress in Laboratory Demonstration.” In 2005 Earth-Sun System Technology Conference. https://ntrs.nasa.gov/citations/20060042890
• Yu, N., J. Kohel, and L. Maleki. 2000. “Quantum Atom Interfermoter Gravity Gradiometer in Space.” In Workshop on Quantum Optics. https://ntrs.nasa.gov/citations/20060033196
• Yu, N., J. M. Kohel, and L. Maleki. 2002a. “Development of an Atom Interferometer Gravity Gradiometer for Applications in Space.” In 7th International Workshop on Atom Optics and Interferometry. https://ntrs.nasa.gov/citations/20060029845
• Yu, Nan, James M. Kohel, Jaime Ramerez-Serrano, James R. Kellogg, Lawrence Lim, and Lute Maleki. 2004. “Progress towards a Space-Borne Quantum Gravity Gradiometer.” In Earth Science Technology Conference (ESTC). https://ntrs.nasa.gov/citations/20060043852
• Yu, N., J. M. Kohel, L. Romans, and L. Maleki. 2002b. “Quantum Gravity Gradiometer Sensor for Earth Science Applications.” In Earth Science Technology Conference - 2002. https://ntrs.nasa.gov/citations/20060029591
• Yu, Peidong, Mengkui Liu, and Yuanjun Chen. 2022a. “Performance Analysis of INS/ODO Integrated Navigation with Different Measurement Models in GNSS Denied Environment.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-2580-1_29
• Yu, Xudong, Xingwu Long, Guo Wei, Geng Li, and Tianliang Qu. 2015b. “Statistical Analysis of Nature Frequencies of Hemispherical Resonator Gyroscope Based on Probability Theory.” In SPIE Proceedings, vol. 9435, edited by Jerome P. Lynch. SPIE. https://doi.org/10.1117/12.2083768
• Yu, Xudong, Guangfeng Lu, and Hui Luo. 2016b. “Vacuum Temperature Field Simulation and Experiments of Four-Mode Differential Laser Gyroscope.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-1141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1141
• Yu, Myeong-Jong, Heung-Won Park, Chang-Bae Jeon, Myeong-Jong Yu, Heung-Won Park, and Chang-Bae Jeon. 1997. “Equivalent Nonlinear Error Models of Strapdown Inertial Navigation System.” In Guidance, Navigation, and Control Conference. AIAA 1997-3563. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3563
• Yu, yuting, and Ya Qiao. 2020. “Research on the Fault Detection Method of Low Cost Redundant Inertial Navigation Group System Based on GLT.” In ICOSM 2020: Optoelectronic Science and Materials, edited by Pei Wang, Yuan Lu. SPIE. https://doi.org/10.1117/12.2586282
• Yu, Bin, Chun Zhen Sun, and Kai Wang. 2014. “An Entry Range Correction Scheme for Reusable Launch Vehicle.” Applied Mechanics and Materials 668-669: 406–11. https://doi.org/10.4028/www.scientific.net/amm.668-669.406
• Yu, Nan, Robert J. Thompson, James R. Kellogg, David C. Aveline, Lute Maleki, and James M. Kohel. 2010b. A Transportable Gravity Gradiometer Based on Atom Interferometry. NPO-46280. California Inst. of Tech. https://ntrs.nasa.gov/citations/20100019615
• Yu, Yongjun, Jinfa Xu, Zhi Xiong, and Bingyu Liu. 2015a. “Research on SINS/CNS Gaussian Particle Filter Integrated Navigation Algorithm for Hypersonic Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-1754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1754
• Yu, Jie, Zhiqiang Zhang, Yanshuang Zhao, Hu Liang, and Ruoxiang Tang. 2023a. “A Design of Integrated Specialized Optical Device for Three-Cluster Fiber Optic Gyroscope.” In AOPC 2023: Optic Fiber Gyro, edited by Shangran Xie, Qi Wang, Benli Yu. SPIE. https://doi.org/10.1117/12.3008096
• Yuan, Donghui, Lipeng Wang, Ruotong Cao, Jialiang Liu, and Weihan Li. 2025c. “Fault Reconstruction of Carrier-Based Aircraft Automatic Landing System Based on Sliding Mode Observer.” In Springer Aerospace Technology. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-3240-4_57
• Yuan, Yu, Chenglong Wang, Mingbo Sun, Yongchao Sun, and Dapeng Xiong. 2025b. “Effects of Combustion–thermal–structural Coupling on Supersonic Combustion and Structural Response in Axisymmetric Scramjet.” Physics of Fluids 37 (4): 044105. https://doi.org/10.1063/5.0257867
• Yuan, Lishan, Ning Wang, Zhennan Wei, Guoxing Yi, and Qingshuang Zeng. 2026b. “Research on the Influence Mechanism of Assembly Stress on Hemispherical Resonator Gyroscope.” In Lecture Notes in Networks and Systems. Springer Nature Singapore. https://doi.org/10.1007/978-981-92-2879-9_19
• Yuan, Kefei, Xiaohui Yang, Guopeng Tian, and Yueyang Ben. 2024a. “A Damping Method of Grid Strapdown Inertial Navigation System for Polar Region.” Journal of Physics: Conference Series 2815 (1): 012051. https://doi.org/10.1088/1742-6596/2815/1/012051
• Yuan, GuangMin, Weizheng Yuan, Xiaobo Zhu, and HongLong Chang. 2014. “The Carrier-Generating Analysis of MEMS Gyroscope Interface Circuit.” AIP Advances 4 (3): 031337. https://doi.org/10.1063/1.4869441
• Yuceil, Kemal, Agustin Valdivia, Justin Wagner, Noel Clemens, and David Dolling. 2009. “Active Control of Supersonic Inlet Unstart Using Vortex Generator Jets.” In 39th AIAA Fluid Dynamics Conference. AIAA 2009-4022. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-4022
• Yue, 张跃 Zhang, and 储海荣 Chu Hai-rong. 2012. “Structural Characteristics of Gain Scheduling Autopilot for Transfer Trajectory Control.” Optics and Precision Engineering 20 (7): 1595–1602. https://doi.org/10.3788/ope.20122007.1595
• Yue, Shuai, Hong Nie, Ming Zhang, Mingyang Huang, and Dafu Xu. 2018b. “Optimization and Performance Analysis of Oleo-Honeycomb Damper Used in Vertical Landing Reusable Launch Vehicle.” Journal of Aerospace Engineering 31 (2): 04018002. https://doi.org/10.1061/(asce)as.1943-5525.0000825
• Yue, Shuai, Hong Nie, Ming Zhang, Mingyang Huang, He Zhu, and Dafu Xu. 2018a. “Dynamic Analysis for Vertical Soft Landing of Reusable Launch Vehicle with Landing Strut Flexibility.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (4): 1377–96. https://doi.org/10.1177/0954410017753209
• Yuksel, Yigiter, and Naser El-Sheimy. 2011. “An Optimal Sensor Fusion Method for Skew-Redundant Inertial Measurement Units.” Journal of Applied Geodesy 5 (2). https://doi.org/10.1515/jag.2011.010
• Yun, Se Hyun, and Chan Gook Park. 2014. “Position Fix in Terrain Referenced Navigation Using Statistical Verification.” IET Radar, Sonar & Navigation 8 (9): 1091–99. https://doi.org/10.1049/iet-rsn.2013.0343
• Yun Cho, Seong, Hyung Keun Lee, and Chan Gook Park. 2013. “Adaptive Redundant Inertial Measurement Unit/Global Positioning System Integration Filter Structure for Fault Tolerant Navigation.” Journal of Dynamic Systems, Measurement, and Control 136 (2): 021009. https://doi.org/10.1115/1.4025753
• Yun Cho, Seong, Hyung Keun Lee, and Hung Kyu Lee. 2012. “Observability and Estimation Error Analysis of the Initial Fine Alignment Filter for Nonleveling Strapdown Inertial Navigation System.” Journal of Dynamic Systems, Measurement, and Control 135 (2): 021005. https://doi.org/10.1115/1.4007552
• Yusefi, Abdullah, İbrahim Toy, Cemil Sungur, and Akif Durdu. 2023. “Gnss-Onboard Inertial Sensor Integration for Accurate Autonomous Vehicle Localization in Gnss-Denied Scenarios.” Preprint, . https://doi.org/10.2139/ssrn.4334509
• Yıldırım Dalkıran, Fatma, and Emre Kırteke. 2024. “Design and Implementation of a Low-Cost Parachute Landing System for Fixed-Wing Mini Unmanned Aerial Vehicles.” Journal of Aviation 8 (3): 198–205. https://doi.org/10.30518/jav.1479457
• Zaccheo, F. E. 1949. “Notes on Astro-Navigation in Polar Regions.” Journal of Navigation 2 (2): 180–83. https://doi.org/10.1017/s0373463300031805
• Zagone, Peter, and Captain Hesse Jr. 1965. “Inertial Attitude Sensors in a Strapped-Down System.” In Guidance Control Conference. AIAA 1965-1203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1203
• Zahed, Muhammad Junayed Hasan, Mohammed I. Alabsi, Travis Fields, and Dakota Hetrick. 2020. “Virtual Sensor Development for Actual Sensor Fault Detection and Flight Parameter Estimation in Real Time.” In AIAA Scitech 2020 Forum. AIAA 2020-0510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0510
• Zaher, Obadah, John Counsell, and Joseph Brindley. 2010. “Design of a Non-Linear Missile Autopilot Using Rate Actuated Inverse Dynamics (RAID).” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7578
• Zahran, Shady, Adel Moussa, Naser El-Sheimy, and Abu B. Sesay. 2018b. “Hybrid Machine Learning VDM for UAVs in GNSS-Denied Environment.” Navigation 65 (3): 477–92. https://doi.org/10.1002/navi.249
• Zakharov, A. I., M. E. Prokhorov, M. S. Tuchin, and A. O. Zhukov. 2013. “Minimum Star Tracker Specifications Required to Achieve a Given Attitude Accuracy.” Astrophysical Bulletin 68 (4): 481–93. https://doi.org/10.1134/s199034131304010x
• Zakrajsek, Andrew J., Ryan N. Vogel, Sam Naboulsi, and Michael Bohun. 2017. “Landing Gear Design Impact on Aircraft Tire Life.” In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2017-0352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0352
• Zander, Fabian. n.d. “Design and Implementation of a Fuel System for a Supersonic Solid Fuel Ramjet.” PhD diss., The University of Queensland. https://doi.org/10.14264/345636
• Zarchan, P. 1977. “Complete Statistical Analysis of Nonlinear Missile Guidance Systems: SLAM.” In Guidance and Control Conference. AIAA 1977-1094. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1094
• Zarei, Nilgoon, Albert Leung, and John D. Jones. 2012. “Modeling a Novel MEMS Gyroscope.” ECS Meeting Abstracts MA2012-01 (44): 1618–1618. https://doi.org/10.1149/ma2012-01/44/1618
• Zarinetchi, F., and S. Ezekiel. 1986. “Observation of Lock-in Behavior in a Passive Resonator Gyroscope.” Optics Letters 11 (6): 401. https://doi.org/10.1364/ol.11.000401
• Zarovsky, Jacob. 1951. System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft. NACA-RM-L51E07. NASA. https://ntrs.nasa.gov/citations/19930090535
• Zarubin, G. P., V. N. Zimin, and G. N. Kuvyrkin. 2017. “Thermal State of the Shell for Supersonic Part of the Ramjet Nozzle.” Russian Aeronautics 60 (2): 236–42. https://doi.org/10.3103/s106879981702012x
• Zavattero, Paul. 1987. “Covariance Analysis of Gravity Models for Land Navigation.” In Guidance, Navigation and Control Conference. AIAA 1987-2469. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2469
• Zeis, Joseph, Jr., Heather Lambert, Robert Calico, and Daniel Gleason. 1988. “Angle of Attack Estimation Using an Inertial Reference Platform.” In 15th Atmospheric Flight Mechanics Conference. AIAA 1988-4351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4351
• Zelenak, Maryann. 1994. “An Uncertainty Analysis of Inlet Dynamic Distortion Data Using an Analog/Digital Hybrid Editing System.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/94-gt-407
• Zellner, B., W. Sterr, and O. Herrmann. 1992. “Integration of Turbo-Expander- and Turbo-Ramjet-Engines in Hypersonic Vehicles.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-204
• Zeng, Xinyu, and Olha Lysa. 2024. “Response Time in Inertial Measurement Unit Control Algorithms.” Measuring Equipment and Metrology 85 (2): 5–8. https://doi.org/10.23939/istcmtm2024.02.005
• Zeng, Wen, Hong Mei Xia, Yu Xing Wang, and Liu Yi Wang. 2012. “Dynamic Characteristic Analysis of Inertial Navigation Platform’ Structure.” Advanced materials research 479-481: 1560–64. https://doi.org/10.4028/www.scientific.net/amr.479-481.1560
• Zha, Ge-Cheng, Doyle Knight, and Donald Smith. 1998b. “Numerical Investigations of HSCT Inlet Unstart Transient at Angle of Attack.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3583
• Zhan, Yinhu, Shaojie Chen, and Xu Zhang. 2021. “Adaptive Celestial Positioning for the Stationary Mars Rover Based on a Self-Calibration Model for the Star Sensor.” Journal of Navigation 75 (1): 160–75. https://doi.org/10.1017/s0373463321000680
• Zhang, Tong. 2017. “Three-Channel Filter Theory for Fault Detection and Isolation of Redundant Inertial Measurement Unit.” Preprint, . https://doi.org/10.26226/morressier.59c106e9d462b80292389d8b
• Zhang, HaoGuang, Kang An, Feng Tan, YanHui Wu, and WuLi Chu. 2017c. “Numerical Investigation of Effect of Inlet Distortion on Compressor Flow Field and Stability.” In Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards. American Society of Mechanical Engineers. https://doi.org/10.1115/gt2017-63369
• Zhang, C., C. Chen, and X. Shen. 2004. “Boltzmann Entropy-Based Guide Star Selection Algorithm for Star Tracker.” Electronics Letters 40 (2): 109–10. https://doi.org/10.1049/el:20040072
• Zhang, Mingyang, Zhishi Chen, Songyan Wang, Tao Chao, and Ming Yang. 2023h. “Reentry Trajectory Planning and Tracking Law of Hypersonic Glide Vehicle under the Influence of Environmental Uncertainty.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_436
• Zhang, Haiyan, Xuan Cui, Yan Suo, Shuyu Hou, Junjie Wang, and Zhoucheng Liu. 2024e. “Research on Position Model of Surface-to-Air Missile Defense against Cruise Missile Based on Rule GA.” Journal of Physics: Conference Series 2890 (1): 012008. https://doi.org/10.1088/1742-6596/2890/1/012008
• Zhang, Wenzhe, Zhihong Deng, and Lei Shi. 2021f. “A Novel Adaptability Analysis Method of Gravity Matching Area.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_458
• Zhang, Yonggang, and Zhongxing Gao. 2012. “Fiber Optic Gyroscope Vibration Error Due to Fiber Tail Length Asymmetry Based on Elastic-Optic Effect.” Optical Engineering 51 (12): 1–6. https://doi.org/10.1117/1.oe.51.12.124403
• Zhang, Yongmeng, Kechen Guo, Jiangkun Sun, Yu Sheng, W. Dingbang, and Wu Xuezhong. 2022h. “Research on Damping Error Tuning and Compensating Technology of Whole Angle Mode Hemispherical Resonator Gyroscope.” Journal of Mechanical Engineering 58 (16): 145. https://doi.org/10.3901/jme.2022.16.145
• Zhang, Hunzhuo, and Duan Huang. 2024. “PSO-CNN-Based Initial Alignment for Fiber Optic Gyroscope.” Preprint, . https://doi.org/10.20944/preprints202402.0194.v1
• Zhang, Liang, Liang Jing, Liheng Ye, and Xing Gao. 2021g. “Predefined-Time Control for a Horizontal Takeoff and Horizontal Landing Reusable Launch Vehicle.” Aircraft Engineering and Aerospace Technology 93 (6): 957–70. https://doi.org/10.1108/aeat-11-2020-0253
• Zhang, Dongsheng, and Shuming Li. 2025. “The in-Plane Deformation and Free Vibration Analysis of a Rotating Ring Resonator of a Gyroscope with Evenly Distributed Mass Imperfections.” Preprint, . https://doi.org/10.20944/preprints202507.0939.v1
• Zhang, Hengbo, Xin Liu, Qingfeng Dou, and Qiongyao Han. 2023f. “Multi-Source Error Calibration and Observability Analysis of Integrated Inertial Navigation System/Polarization Sensor Navigation System.” Journal of Physics: Conference Series 2456 (1): 012005. https://doi.org/10.1088/1742-6596/2456/1/012005
• Zhang, Kunpeng, Shuangheng Liu, Jingjing Feng, and Bo Wang. 2026c. “Dynamics, Stability, and Sensitivity Analysis of a Mode-Localization MEMS Gyroscope Subjected to Single and Dual Parametric Excitation.” Measurement Science and Technology 37 (10): 105103. https://doi.org/10.1088/1361-6501/ae49aa
• Zhang, Qian, Dejun Meng, Shenren Xu, Dingxi Wang, and Xiuquan Hang. 2025f. “Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor.” Journal of Turbomachinery 147 (8): 081013. https://doi.org/10.1115/1.4067439
• Zhang, Hao, Yanxiong Niu, Jiazhen Lu, and Yanqiang Yang. 2018g. “Star Sensor Installation Error Calibration in Stellar-Inertial Navigation System with a Regularized Backpropagation Neural Network.” Measurement Science and Technology 29 (8): 085102. https://doi.org/10.1088/1361-6501/aac6a8
• Zhang, C., X. B. Shen, and C. Y. Chen. 2005. “Boltzmann Entropy Based Star Identification Algorithm for Star Tracker.” In SPIE Proceedings, vol. 6044, edited by Deren Li, Hongchao Ma. SPIE. https://doi.org/10.1117/12.652309
• Zhang, Wenzhe, Zhengwei Sun, and Zhihong Deng. 2025h. “A Gravity Matching Area Selection Method Based on GA-Bagging-SVM.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2200-9_39
• Zhang, Liwei, Hong-Gye Sung, and Vigor Yang. 2020. “Flow and Flame Dynamics in a Hydrocarbon-Fueled Dual-Combustion Ramjet Engine.” In AIAA Scitech 2020 Forum. AIAA 2020-0648. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0648
• Zhang, Jiaxian, Jiliang Tu, Hui Liu, and Shixue Zhang. 2022f. “Investigation on the Effect of Anti-Braking System on Nose Landing Gear Shimmy.” In Advances in Transdisciplinary Engineering. IOS Press. https://doi.org/10.3233/atde221072
• Zhang, Yan Shun, and Shu Wei Wang. 2011b. “Modeling and Error Compensation of MEMS Gyroscope Dynamic Output Data within the Whole Temperature Range.” Advanced materials research 311-313: 768–71. https://doi.org/10.4028/www.scientific.net/amr.311-313.768
• Zhang, C., Y. Wang, Z. G. Jin, H. B. Ke, and H. Wang. 2022c. “Experimental Study of the Thermal Storage and Mechanical Properties of Microencapsulated Phase Change Composites during a Supersonic Cruise.” RSC Advances 12 (10): 6114–21. https://doi.org/10.1039/d1ra08434h
• Zhang, Yinuo, Zhe Wang, Jingshu Li, Ning Mao, Hongyang He, and Canye Du. 2026g. “A Novel LEAF-Based SINS Initial Alignment Method for Underwater Gravity-Vector Matching Navigation.” Preprint, . https://doi.org/10.2139/ssrn.7602298
• Zhang, Yi Ming, Wei Wang, Jie Sui, and Xue Yun Wang. 2014b. “A GPS-Assisted Calibration Algorithm for Misalignment Angle between Star Sensor and Strap-Down Inertial Navigation System.” Applied Mechanics and Materials 635-637: 1457–63. https://doi.org/10.4028/www.scientific.net/amm.635-637.1457
• Zhang, Zhijun, Limin Wang, and Jiyu Sun. 2007. “Design of Orienting and Aiming Instrument Based on Fiber Optic Gyroscope.” In SPIE Proceedings, vol. 6723, edited by Junhua Pan, James C. Wyant, Hexin Wang. SPIE. https://doi.org/10.1117/12.783692
• Zhang, Liyuan, Zhongshi Wang, Rui Xu, Dapeng Tian, and Lihong Guo. 2025k. “A Robust Adaptive Kalman Filter Based Visual Servoing Control for an Inertial Stabilization Platform.” Measurement Science and Technology 36 (10): 106204. https://doi.org/10.1088/1361-6501/ae0e8f
• Zhang, Yajie, Qi Wang, and Jian Zhou. 2023d. “A Inertial Navigation/laser Doppler Velocimeter/geomagnetic Sensor Integrated Navigation Method.” In Fourteenth International Conference on Information Optics and Photonics (CIOP 2023), edited by Yue Yang. SPIE. https://doi.org/10.1117/12.3007651
• Zhang, Yu, Zhengyou Wen, Haonan Chen, Yuchen Zhang, and Liaoni Wu. 2025l. “Trajectory Planning and Guidance Design for the Automatic Landing Phase of Reusable Launch Vehicle.” Journal of Physics: Conference Series 2977 (1): 012006. https://doi.org/10.1088/1742-6596/2977/1/012006
• Zhang, Shuo, Fei Xing, Ting Sun, Zheng You, and Minsong Wei. 2018e. “Novel Approach to Improve the Attitude Update Rate of a Star Tracker.” Optics Express 26 (5): 5164. https://doi.org/10.1364/oe.26.005164
• Zhang, Zilun, Jiasheng Xu, and Zhiwei Mei. 2026j. “Study on the Aerodynamic Characteristics of Canard Configuration Missile Influenced by Aileron.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2026-99-1610
• Zhang, Xinrui, Rui Xu, Tianji Wu, and Zhi Xiong. 2026h. “Observability Analysis of an Airborne Inertial/celestial/terrain Integrated Navigation System for High-Speed Vehicles.” Journal of Physics: Conference Series 3326 (1): 012008. https://doi.org/10.1088/1742-6596/3326/1/012008
• Zhang, Ming, Dafu Xu, Shuai Yue, and Haifeng Tao. 2018b. “Design and Dynamic Analysis of Landing Gear System in Vertical Takeoff and Vertical Landing Reusable Launch Vehicle.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (10): 3700–3713. https://doi.org/10.1177/0954410018804093
• Zhang, Zuchen, Xiaobin Xu, Zhihao Zhang, Ningfang Song, and Chunxi Zhang. 2016a. “Reflection-Induced Bias Error in an Air-Core Photonic Bandgap Fiber Optic Gyroscope.” Optics Letters 41 (2): 309. https://doi.org/10.1364/ol.41.000309
• Zhang, Kai, Xuanfei Yu, Jian Guo, Duo Zhang, and Fei Qin. 2025e. “Effect of Strut–lobe Combination on Combustion Characteristics in Multimode Combustor of Innovative Ramjet Combined-Cycle Engine.” Physics of Fluids 37 (6): 066129. https://doi.org/10.1063/5.0271888
• Zhang, Lumin, Zechu Yu, and Yongjian Yang. 1990. “Numerical Simulation of Inviscid Supersonic Flow over Multiple Bodies.” In Flight Simulation Technologies Conference and Exhibit. AIAA 1990-3099. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3099
• Zhang, Minghao, and Changsheng Yuan. 2019. “Pneumatic Canard Configuration for Control and Aerodynamic Dilemma.” In AIAA Aviation 2019 Forum. AIAA 2019-2890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2890
• Zhang, Jian Ming, and Xing Hui Zhang. 2013. “Research on Micro Inertial Sensor Error Compensation Technology in SINS.” Applied Mechanics and Materials 273: 532–36. https://doi.org/10.4028/www.scientific.net/amm.273.532
• Zhang, Hongjie, and Shifeng Zhang. 2017. “Research on Guidance Instrumentation Error Separation Method of Platform Inertial Navigation System.” In Proceedings of the 2017 5th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering (ICMMCCE 2017). Atlantis Press. https://doi.org/10.2991/icmmcce-17.2017.221
• Zhang, He, Chao Zhang, Shuai Tong, et al. 2023a. “Celestial Navigation and Positioning Method Based on Super-Large Field of View Star Sensors.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-6928-9_41
• Zhang, JianRui, HuYong Zhang, and Peng Zhao. 2026a. “Creep Behavior of a High-Strength Aluminum Alloy at Elevated Temperature: Microstructural Evolution and Physically Based Modelling.” Preprint, . https://doi.org/10.2139/ssrn.6641999
• Zhang, Peng, Dabin Zhu, Huli Dong, Zeng Wang, Jiaao Wang, and Xiying Chen. 2023b. “Considering Lateral Bending and Torsion Coupling in Shimmy Analysis of the Nose Landing Gear.” Journal of Physics: Conference Series 2658 (1): 012053. https://doi.org/10.1088/1742-6596/2658/1/012053
• Zhao, Long. 2012. “Robust Unscented Transformation Based Terrain-Aided Inertial Navigation Algorithm.” In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-29187-6_50
• Zhao, Xijing. 2014. “Modeling of Temperature Drift Based on Improved Fuzzy Inference for Fiber Optic Gyroscope.” Journal of Mechanical Engineering 50 (6): 15. https://doi.org/10.3901/jme.2014.06.015
• Zhao, Xin. 2024b. “The Underwater Gravity Matching Navigation Adaptation Area Is Preferred Based on the Multi-Starting Point TERCOM Algorithm.” Academic Journal of Science and Technology 10 (2): 82–86. https://doi.org/10.54097/v79mh113
• Zhao, Guojun, Yihan Dou, and Lei Shi. 2025b. “Key Parameters on Combustion Characteristics in a Rocket-Aided Ramjet Engine under Mach 6 Flight Conditions.” Physics of Fluids 37 (8): 087176. https://doi.org/10.1063/5.0281994
• Zhao, Wei Feng, Xiao Lin Han, and Qing Guo Fei. 2011. “Preliminary Research on the Aerothermoelastic Behaviours of Sweptback Wing.” Applied Mechanics and Materials 138-139: 874–78. https://doi.org/10.4028/www.scientific.net/amm.138-139.874
• Zhao, Lin, Jiushun Li, Jianhua Cheng, and Yong Hao. 2016a. “Damping Strapdown Inertial Navigation System Based on a Kalman Filter.” Measurement Science and Technology 27 (11): 115102. https://doi.org/10.1088/0957-0233/27/11/115102
• Zhao, Shiyu, Feng Lin, Kemao Peng, Ben Chen, and Tong Lee. 2012. “Homography-Based Vision-Aided Inertial Navigation of UAVs in Unknown Environments.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-5033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5033
• Zhao, Shuangxiang, Qingwen Liu, Yuanyuan Liu, Huilian Ma, and Zuyuan He. 2022d. “Navigation-Grade Resonant Fiber-Optic Gyroscope Using Ultra-Simple White-Light Multibeam Interferometry.” Photonics Research 10 (2): 542. https://doi.org/10.1364/prj.443496
• Zhao, Shuangxiang, Qingwen Liu, Huilian Ma, and Zuyuan He. 2022g. “White-Light-Driven Resonant Fiber-Optic Gyro Achieving Navigation-Grade Resolution.” In 27th International Conference on Optical Fiber Sensors. Optica Publishing Group. https://doi.org/10.1364/ofs.2022.f2.6
• Zhao, Xinxin, Jinguang Shi, Huajie Ren, and Zhongyuan Wang. 2024c. “Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft.” Preprint, . https://doi.org/10.2139/ssrn.4907932
• Zhao, Shengwu, Lei Shi, Wenzhe Zhang, and Zhihong Deng. 2021b. “Global Dynamic Path-Planning Algorithm in Gravity-Aided Inertial Navigation System.” IET Signal Processing 15 (8): 510–20. https://doi.org/10.1049/sil2.12056
• Zhao, Lin, and Sheng Jing Tang. 2012. “Design and Optimization of Missile Three-Loop Autopilot Based on Performance Indicators.” Applied Mechanics and Materials 203: 36–40. https://doi.org/10.4028/www.scientific.net/amm.203.36
• Zhao, Yanshuang, Ruoxiang Tang, Xiaoming Zhang, and Tao Chen. 2023a. “A Fiber Optic Gyroscope Based on Integrated Optoelectronic Devices.” In AOPC 2023: Optic Fiber Gyro, edited by Shangran Xie, Qi Wang, Benli Yu. SPIE. https://doi.org/10.1117/12.3008129
• Zhao, Yan Li, Hua Bing Wang, Xiang Dong Gao, Yuan Zheng Chen, and Zhou Yan. 2013. “A Study on Tracking Accuracy of Netted Radar.” Applied Mechanics and Materials 385-386: 1249–54. https://doi.org/10.4028/www.scientific.net/amm.385-386.1249
• Zhao, Benfei, Jiaxing Wang, and Liaoni Wu. 2026a. “Design of Automatic Landing Control Law for Multi-Disturbance Scenarios Based on TD3.” Journal of Physics: Conference Series 3303 (1): 012010. https://doi.org/10.1088/1742-6596/3303/1/012010
• Zhao, Jianxiang, Sulan Wei, Ruzhen Xiang, Jizhuo Liu, Rile Lin, and Li Chen. 2026e. “Zero-Bias Drift Compensation for a High-Speed Mode-Reversal MEMS Vibratory Gyroscope.” Preprint, . https://doi.org/10.2139/ssrn.6416151
• Zhao, Zhongwen, Xu Zhang, and Guodong Li. 2020b. “A Rapid Evaluation Method of Radar Tracking Accuracy.” In Proceedings of the 2020 4th International Conference on Electronic Information Technology and Computer Engineering. ACM. https://doi.org/10.1145/3443467.3443741
• Zhao, Y. L., Yiheng Zhou, and Yilong Zhao. 2022c. “Experimental Study of the Unstart/Restart Process of a Two-Dimensional Supersonic Inlet Induced by Backpressure.” Journal of Applied Fluid Mechanics 15 (2). https://doi.org/10.47176/jafm.15.02.33220
• Zhao, Chen, Yiwei Zhou, Shaoyin Zhao, et al. 2025f. “Research Progress on the Dynamics of Parachute Deceleration Systems.” Journal of Physics: Conference Series 3109 (1): 012028. https://doi.org/10.1088/1742-6596/3109/1/012028
• Zhao Long. 2012. “Robust Inertial Terrain Aided Navigation Algorithm.” Acta Physica Sinica 61 (10): 104301. https://doi.org/10.7498/aps.61.104301
• Zhbanov, Yu. K., and V. Ph. Zhuravlev. 2007. “Effect of Movability of the Resonator Center on the Operation of a Hemispherical Resonator Gyro.” Mechanics of Solids 42 (6): 851–59. https://doi.org/10.3103/s0025654407060039
• Zhen Ding and B. Balaji. 2012. “Comparison of the Unscented and Cubature Kalman Filters for Radar Tracking Applications.” In IET International Conference on Radar Systems (Radar 2012). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2012.1695
• Zheng, Risheng, Jun Tao Chang, Hui Xin He, and Fu Chen. 2013. “Optimal Classification of Hypersonic Inlet Start/Unstart Based on Manifold Learning.” Applied Mechanics and Materials 274: 200–203. https://doi.org/10.4028/www.scientific.net/amm.274.200
• Zheng, Qiu Ya, Jian Hu Feng, and Zun Huan Shen. 2012b. “Transonic Drag Prediction on a DLR-F6 Transport Configuration.” Advanced Materials Research 566: 676–79. https://doi.org/10.4028/www.scientific.net/amr.566.676
• Zheng, Zhichao, Songlai Han, Jin Yue, and Linglong Yuan. 2015. “Compensation for Stochastic Error of Gyros in a Dual-Axis Rotational Inertial Navigation System.” Journal of Navigation 69 (1): 169–82. https://doi.org/10.1017/s037346331500051x
• Zheng, Qinze, Yu Liang, Yuhan Yang, and Chong Pan. 2026b. “Research on Low-Drag Low-Boom Supersonic Transport Configuration Using an MDO Framework and Deep Learning Methods.” Preprint, . https://doi.org/10.2139/ssrn.6750147
• Zheng, Hui, Hubiao Wang, Lin Wu, Hua Chai, and Yong Wang. 2012a. “Simulation Research on Gravity-Geomagnetism Combined Aided Underwater Navigation.” Journal of Navigation 66 (1): 83–98. https://doi.org/10.1017/s0373463312000343
• Zheng, Junjie, Xiaoke Yan, Zhihua Jiang, and Caicheng Shi. 2005. “Trajectory Measuring of Ballistic Missile with Imaging Infrared System Based on Knowledge.” In SPIE Proceedings, vol. 5985, edited by Cheng Wang, Shan Zhong, Xiulin Hu. SPIE. https://doi.org/10.1117/12.658263
• Zheng, Yuting, Ming Zhang, Shaofei Yang, Xiazheng Shi, and Yuhan Xu. 2026a. “Dynamic Analysis of Nose Landing Gear Shimmy Considering Hydraulic Damping Characteristics.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 44 (1): 17–26. https://doi.org/10.1051/jnwpu/20264410017
• Zhimin, Han, and Hong Guanxin. 2008. “Landing Error Analysis of the Automatic Carrier Landing System.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6335
• ZhongGuo, Song, Gao Jiuxiang, Zhang Jinsheng, and Xi Xiaoli. 2018. “An Improved Method of Geomagnetic Aided Inertial Navigation Algorithm with Gyro and Accelerometer Error Corrected Online.” MATEC Web of Conferences 198: 02007. https://doi.org/10.1051/matecconf/201819802007
• Zhou, Yupeng. 2026. “An Automatic Landing Adaptive Control Method with Parameter Optimization.” Journal of Physics: Conference Series 3242 (1): 012057. https://doi.org/10.1088/1742-6596/3242/1/012057
• Zhou, Jun, Hanqiao Huang, and Jianguo Guo. 2010. “A Design Method of BTT Missile Autopilot with the Impact of Feedforward.” Modern Applied Science 4 (5). https://doi.org/10.5539/mas.v4n5p58
• Zhou, Zihan, Pin Lyu, Jizhou Lai, Xudong Zhu, and Kai Huang. 2021d. “Multi-Vehicle Collaborative Navigation Method Based on Datalink Relative Distance in GNSS Denied Environment.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_324
• Zhou, Ruiyang, and Konstantin A. Neusypin. 2023. “ADRC-Based UAV Control Scheme for Automatic Carrier Landing.” In 15th International Conference “Intelligent Systems” (INTELS’22). MDPI. https://doi.org/10.3390/engproc2023033066
• Zhou, Guang Tao, Gui Min Shi, Lei Zhang, and Kai Li. 2012. “Estimating Gyro Drift of Strapdown Inertial Navigation System Based on Star Sensor.” Advanced materials research 566: 235–38. https://doi.org/10.4028/www.scientific.net/amr.566.235
• Zhou, Shiqin, Yanji Wu, Lingqin Xia, Yu Peng, and Rongkai Sun. 1999. “Fiber Optic Gyroscope for Harsh Environment Applications.” In SPIE Proceedings, vol. 3860, edited by Michael A. Marcus, Brian Culshaw. SPIE. https://doi.org/10.1117/12.372974
• Zhou, K. J., and X. L. Zhang. 2010. “Multiwavelength Erbium-Doped Fiber Ring Laser Using a LiNbO3 Multifunction Chip for Fiber Gyroscope.” Laser Physics 20 (6): 1428–32. https://doi.org/10.1134/s1054660x1011037x
• Zhou, Jiacai, Yanying Zhao, Qiqi Li, and Longhua Zhou. 2024b. “Stability Analysis of Nonlinear Models of Nose Landing Gear Shimmy.” World Journal of Engineering and Technology 12 (01): 103–16. https://doi.org/10.4236/wjet.2024.121007
• Zhou, Hongjin, Yunhai Zhong, Hui Song, and Su Wang. 2021a. “Accelerometer Mounting Error Calibration.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-15-4972-4_6
• Zhou, Hongjin, Yunhai Zhong, Hui Song, and Su Wang. 2021b. “GPS-Aided Integrated Navigation with GFINS.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-15-4972-4_7
• Zhou, Hongjin, Yunhai Zhong, Hui Song, and Su Wang. 2021c. “Gyro-Free Inertial Navigation Principle.” In Navigation: Science and Technology. Springer Singapore. https://doi.org/10.1007/978-981-15-4972-4_2
• Zhu, Qing. 2024. “Automatic Landing Control System for Large Passenger Aircraft under Artificial Intelligence.” In Ninth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2024), edited by Jinsong Wu, Azanizawati Ma’aram. SPIE. https://doi.org/10.1117/12.3039854
• Zhu, Lihua, and Xianghong Cheng. 2013a. “An Improved Initial Alignment Method for Rocket Navigation Systems.” Journal of Navigation 66 (5): 737–49. https://doi.org/10.1017/s0373463313000295
• Zhu, Li, and Xiang Hong Cheng. 2013b. “An Improved Initial Alignment Method of Strap-Down Inertial Navigation System on a Swaying Base.” Applied Mechanics and Materials 415: 143–48. https://doi.org/10.4028/www.scientific.net/amm.415.143
• Zhu, Min, Ming Guo, and Zhaoqun Shao. 2020b. “The Elimination and Detection Method of Ballistic Missile Infrared Images Bright Line Noise in Middle Trajectory.” Journal of Physics: Conference Series 1550 (3): 032160. https://doi.org/10.1088/1742-6596/1550/3/032160
• Zhu, Zhuangsheng, Yiyang Guo, and Wen Ye. 2017. “A Real-Time Gravity Compensation Method for a High-Precision Airborne Position and Orientation System Based on a Gravity Map.” Journal of Navigation 71 (3): 711–28. https://doi.org/10.1017/s0373463317000790
• Zhu, Bing, Ding Li, Zuohu Li, Hongyang He, and Xing Li. 2021d. “Robust Adaptive Kalman Filter for Strapdown Inertial Navigation System Dynamic Alignment.” IET Radar, Sonar & Navigation 15 (12): 1583–93. https://doi.org/10.1049/rsn2.12148
• Zhu, J. J., and M. C. Mickle. n.d. “Missile Autopilot Design Using the Extended-Mean Assignment Control. I. Stabilization.” In Proceedings of the Twenty-Seventh Southeastern Symposium on System Theory. IEEE Comput. Soc. Press. https://doi.org/10.1109/ssst.1995.390575
• Zhu, Yong, BingKun Qin, and Shufen Chen. 1996. “Closed-Loop Fiber Optic Gyroscope with Homodyne Detection.” In SPIE Proceedings, vol. 2895, edited by Kim D. Bennett, Byoung Yoon Kim, Yanbiao Liao. SPIE. https://doi.org/10.1117/12.252203
• Zhu, Guisheng, Yanying Zhao, Yian Liu, Zhenyuan Ju, and Wenchong Feng. 2026b. “Modeling, Simulation, and Experimental Study of Landing Gear Shimmy Considering Strut Height Variation.” Open Journal of Applied Sciences 16 (04): 1246–68. https://doi.org/10.4236/ojapps.2026.164072
• Zhu, Chenchen, Ruipeng Zhou, and Dejun Song. 2025d. “Research on Optimization Analysis Method for Landing Dynamics of Landing Gear Based on Parameter Sensitivity.” Journal of Physics: Conference Series 3141 (1): 012036. https://doi.org/10.1088/1742-6596/3141/1/012036
• Zhuangsheng, Zhu, Guo Yiyang, and Yang Zhenli. 2015. “Study on Initial Gravity Map Matching Technique Based on Triangle Constraint Model.” Journal of Navigation 69 (2): 353–72. https://doi.org/10.1017/s0373463315000661
• Zhuo, C. F., Z. R. He, X. B. Ren, and Y. K. Wang. 2024. “Static and Dynamic Characteristics of Supersonic Cruise Missile with Damaged Wing.” Aeronautical Journal 128 (1329): 2634–55. https://doi.org/10.1017/aer.2024.52
• Zhuravlev, V. Ph. 2015. “Hemispherical Resonator Gyro with m Data Electrodes and n Control Electrodes.” Mechanics of Solids 50 (4): 375–78. https://doi.org/10.3103/s0025654415040020
• Zhuravlev, V. Ph. 2018. “Temperature Drift of a Hemispherical Resonator Gyro (HRG).” Mechanics of Solids 53 (3): 241–48. https://doi.org/10.3103/s0025654418070014
• Zimbelman, Harold. 1987. “A Parametric Analysis of Orbital Gyrocompassing for an Earth Oriented Spacecraft.” In Guidance, Navigation and Control Conference. AIAA 1987-2399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2399
• Zimpfer, Douglas. 1999. “Onorbit Flight Control Design for the Kistler K-1 Reusable Launch Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4210
• Zingg, David, Laslo Diosady, and Laura Billing. 2006. “Adaptive Airfoils for Drag Reduction at Transonic Speeds.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3656. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3656
• Ziraksaz, Mohammad. 2002. “Mini-Turbojet Engine Test Stand for Starting Test.” In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2002-4052. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4052
• Zischka, K. A. 2017. “Astro-Navigation.” In Astronavigation. Springer International Publishing. https://doi.org/10.1007/978-3-319-47994-1_2
• Zissa, D. E. 1984. Optical Analysis of the Star-Tracker Telescope for Gravity Probe. NASA-TM-86474. NASA. https://ntrs.nasa.gov/citations/19850002580
• Zope, Anup, Shanti Bhushan, Greg Burgreen, et al. 2026. “Generalized 5-DoF Model for Hypersonic Boost-Glide Vehicle Trajectory Predictions.” In AIAA SCITECH 2026 Forum. AIAA 2026-1143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1143
• Zou, Yuchun, Ziyang Zhen, Chen Yuwen, Zhibing Zhang, and Junhong Zhang. 2026. “Safety-Critical Predefined-Time Flight Control of Tailless Aircraft for Automatic Carrier Landing.” Preprint, . https://doi.org/10.2139/ssrn.6802811
• Zubarev, Yaroslav A., Anton O. Sinelnikov, and Victoria U. Mnatsakanyan. 2023. “Simulation of the Temperature Drift of the Laser Gyroscope Path Length.” RUDN Journal of Engineering Researches 24 (1): 30–39. https://doi.org/10.22363/2312-8143-2023-24-1-30-39
• Zuber, Kamil, D. J. Wright, Jebum Choi, Colin J. Hall, and Joni M. Sytsma. 2025. Compact Monolithic Star Tracker System. https://doi.org/10.52202/083088-0073
• Zubrin, Robert, and Mitchell Clapp. 1996. “The Pioneer Pathfinder: A Low-Cost Solution for a near-Term Reusable Launch Vehicle.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4605
• Zuccolo, Giovanni, Robert Christie, David MacManus, Ioannis Goulos, and Peter Martin. 2020. “Low Order Models for Transonic Afterbody Aerodynamic Characteristics.” In AIAA Scitech 2020 Forum. AIAA 2020-1997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1997
• Zucro, M. J. 1950. Survey of National Ramjet Program. Defense Technical Information Center. https://doi.org/10.21236/ad0001828
• Zumwalt, G., and S. Suwanprasert,S. 1983. “Design Study of a Dual-Cycle Turbofan-Ramjet Engine for a Hypersonicaircraft.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2484
• Zurriati, M. Ali, Wahyu Kuntjoro, Wirachman Wisnoe, and Rizal Effendy Mohd Nasir. 2011. “The Effect of Canard on Aerodynamics of Blended Wing Body.” Applied Mechanics and Materials 110-116: 4156–60. https://doi.org/10.4028/www.scientific.net/amm.110-116.4156
• Παπαφώτης, Κωνσταντίνος. n.d. “Inertial and Magnetic Sensors: Calibration and Data Funsion with Application to Navigation.” PhD diss., Εθνικό Μετσόβιο Πολυτεχνείο (ΕΜΠ), Σχολή Ηλεκτρολόγων Μηχανικών και Μηχανικών Υπολογιστών, Τομέας Επικοινωνιών, Ηλεκτρονικής και Συστημάτων Πληροφορικής. https://doi.org/10.12681/eadd/51835
• ΦΥΛΛΗΣ, ΙΩΑΝΝΗΣ. n.d. “Optimization of the Update Intervals in the Dual Global Positioning System: Inertial Navigation System.” PhD diss., University of California Los Angeles. https://doi.org/10.12681/eadd/4060
• Борисенко, О. В., and Г. С. Залевський. 2025. “Model of the Signal Scattered by a Cruise Missile at the Output of the Antenna Array of an VHF Band Radar.” Системи обробки інформації, no. 2(181): 68–77. https://doi.org/10.30748/soi.2025.181.08
• Волков, Олексій Сергійович, and Лев Михайлович Рижков. 2018. “Influence of Drift Gyroscope on the Accuracy of Complementary Filter.” Mechanics of Gyroscopic Systems 0 (36): 10–16. https://doi.org/10.20535/0203-3771362018147091
• Донской, А.Д., С.Е. Сабо, and М.А. Щиканов. 2021. “Dynamics of cruise missile flight.” Informacionno-technologicheskij vestnik, no. 1(27): 30–40. https://doi.org/10.21499/2409-1650-2021-27-1-30-40
• Жукова, Ірина. 2022. “IMPROVEMENT OF INERTIAL STABILIZED PLATFORM CONTROL SYSTEMS.” Наука і техніка сьогодні, no. 8(8). https://doi.org/10.52058/2786-6025-2022-8(8)-29-38
• Зеленков, А.А., and А.П. Голик. 2009. “Accuracy Estimate of Stabilization Process in the Automatic Landing and the Running Take-off Modes.” Electronics and Control Systems 1 (19). https://doi.org/10.18372/1990-5548.19.678
• Каликанов, А.В. 2024. “WAVE SOLID -STATE GYROSCOPE WITH LOW -TYPE VOLUMETRIC RESONATOR OPERATING IN AN INTEGRATING GYROSCOPE MODE.” Датчики и системы, no. 1(273). https://doi.org/10.25728/datsys.2024.1.3
• Каплюк, Олександр, and Ye. S. Honcharenko. 2026. “Methodology for Substantiating the Minimum Level of Energy and Ballistic Requirements for an Air-to-Air Guided Missile with a Kinetic Warhead.” Випробування та сертифікація, no. 1(11): 42–50. https://doi.org/10.37701/ts.11.2026.04
• Крылов, А. А., and П. С. Кузнецов. 2019. “MEMS Gyroscope Zero Drift Elimination at Different Temperature Dynamics.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 2: 34–39. https://doi.org/10.38013/2542-0542-2019-2-34-39
• Махдi, Касем Аббуд. 2010. “Error Models Inertial Navigation Systems for Collision Avoidance Systems.” Electronics and Control Systems 4 (26). https://doi.org/10.18372/1990-5548.26.849
• МГТУ им. Н.Э. Баумана, Н.П. Деменков, В.А. Матвеев, МГТУ им. Н.Э. Баумана, И.А. Мочалов, and МГТУ им. Н.Э. Баумана. 2018. “Fuzzy Methods of Hemispherical Resonator Gyroscope Simulation.” Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, no. 120. https://doi.org/10.18698/0236-3933-2018-3-33-50
• МГТУ им. Н.Э. Баумана, О.С. Нарайкин, Ф.Д. Сорокин, et al. 2017. “Numerical Simulation of Elastic Wave Precession in the Cylindrical Resonator of a Hemispherical Resonator Gyroscope Featuring a Non-Homogeneous Density Distribution.” Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, no. 101. https://doi.org/10.18698/0236-3941-2017-5-41-51
• Меерович, Тазьба Александр, Anatoly A. Shevchik, and A. A. Aleksandrov. 2026. “Deep Integration of Inertial and Satellite Navigation Systems Using a Linearized Kalman Filter.” Aèrokosmičeskaâ tehnika i tehnologii. 4 (2): 346–56. https://doi.org/10.52467/2949-401x-2026-4-2-346-356
• Сергеевна, Лаврищева Любовь, N. N. Staroverov, V. Novoselov, and Dmitry Yu. Strelets. 2024. 3D Parametric Optimization Technology of a Supersonic Passenger Aircraft Aerodynamic Design Using Flypoint Parametrica and Ls-Tech Framework. https://doi.org/10.53954/9785604990131_83
• Філяшкін, М. К., and О. В. Мельников. 2012. “Automatic Landing Control Plane Based on the Predictive Model Algorithm.” Electronics and Control Systems 3 (33). https://doi.org/10.18372/1990-5548.33.5507
• Черняк, Микола Григорович. 2018. “Mathematical Model of Instrumental Vibration Error of Navigation Accelerometer and Its Identification at Dynamic Tests of Accelerometer.” Mechanics of Gyroscopic Systems 0 (36): 49–61. https://doi.org/10.20535/0203-3771362018133824
• Черняк, Микола Григорович, and Вадим Александрович Колесник. 2019. “Identification of the Vibration Error of the Navigation Accelerometer during Its Static Tests.” Mechanics of Gyroscopic Systems 0 (38): 48–59. https://doi.org/10.20535/0203-3771382019202979
• Іванов, С.В., and І.О. Білич. 2012. “Accuracy Improving of Measuring Navigation System Parameters with Accelerometer Calibration Using Kalman Filtration.” Electronics and Control Systems 2 (32). https://doi.org/10.18372/1990-5548.32.2260
• 刘, 奕安. 2026. “Landing Gear Shimmy Suppression and Stability Analysis Based on Fuzzy PID Control.” International Journal of Mechanics Research 15 (01): 91–102. https://doi.org/10.12677/ijm.2026.151010

Secondary Sources

• Aircraft Tires: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604641
• Aircraft Wheels, Brakes, and Brake Controls: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604702
• Airfield Compatibility: Key Principles for Landing Gear Design. 2022. SAE International eBooks. https://doi.org/10.4271/9781468604672
• Anderson, John. 2002. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Science/Engineering/Math. https://openlibrary.org/works/OL1993329W
• Ballistic Missile and Space Electronics. 1960. Elsevier. https://doi.org/10.1016/b978-0-12-395519-7.x5001-0
• Blakelock, John H., Automatic Control of Aircraft, and Missiles. 1965. Automatic Control of Aircraft and Missiles. Wiley. https://openlibrary.org/works/OL4449715W
• Britting, Kenneth R. 1971a. Inertial Navigation Systems Analysis. Wiley-Interscience. https://openlibrary.org/works/OL7310141W
• Britting, K. R. 1971b. Inertial Navigation Systems Analysis. MIT. https://ntrs.nasa.gov/citations/19720034278
• Cantó, Begoña, Carmen Coll, and Elena Sánchez. 2011. The Problem of Global Identifiability for Systems with Tridiagonal Matrices. AIMS Press. https://doi.org/10.3934/proc.2011.2011.250
• Cao, Huiliang. 2023b. Dual-Mass Linear Vibration Silicon-Based MEMS Gyroscope. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-9247-6
• Chatfield, Averil B. 1997. Fundamentals of High Accuracy Inertial Navigation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866463
• Currey, Norman S. 1988a. Aircraft Landing Gear Design: Principles and Practices. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL4632940W
• Currey, Norman S. 1988b. Aircraft Landing Gear Design: Principles and Practices. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.861468
• Etkin, Bernard, Lloyd Duff Reid, and Dynamics of flight. 1959. Dynamics of Flight: Stability and Control. John Wiley & Sons/ Chapman & Hall. https://openlibrary.org/works/OL19844466W
• Gibson, James N. 1996. The Navaho Missile Project: The Story of the “Know-How” Missile of American Rocketry. Schiffer Pub. https://openlibrary.org/works/OL2999577W
• Gutman, Shaul. 2005. Applied Min-Max Approach to Missile Guidance and Control. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.476952
• Hill, Philip G., and Peterson. 1991. Mechanics and Thermodynamics of Propulsion [by] Philip G. Hill [and] Carl R. Peterson. https://openlibrary.org/works/OL8229940W
• Jekeli, Christopher. 2023. Inertial Navigation Systems with Geodetic Applications. De Gruyter. https://doi.org/10.1515/9783110784329
• Jenkins, Dennis R., Tony Landis, and Jay Miller. 2003. American X-Vehicles: An Inventory X-1 to X-50 Centennial of Flight Edition. CreateSpace Independent Publishing Platform. https://openlibrary.org/works/OL20394726W
• Jiang, Changhui, Yuwei Chen, Qian Meng, et al., eds. 2023a. Advanced Technologies for Position and Navigation under GNSS Signal Challenging or Denied Environments. MDPI. https://doi.org/10.3390/books978-3-0365-7631-2
• Knacke, T. W., and Parachute recovery systems design manual. 1992. Parachute Recovery Systems: Design Manual. Para Pub. https://openlibrary.org/works/OL4121303W
• Li, Xuefeng, Fan Xu, and Guoqiang Xu. 2023g. Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-4637-0
• Martinelli, Agostino. 2012. Observability Properties and Deterministic Algorithms in Visual-Inertial Structure from Motion. now Publishers Inc. https://doi.org/10.1561/9781601987396
• Mendenhall, Michael. 1992. Tactical Missile Aerodynamics: Prediction Methodology. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.470165
• Miller, Jay. 2001. The X-Planes: X-1 to X-45: 3rd Edition. Midland. https://openlibrary.org/works/OL7006680W
• Missile Guidance and Control Systems. 2004. Springer-Verlag. https://doi.org/10.1007/b97614
• Mohamed, Ahmed. 2013. Global Navigation Satellite Systems: From Stellar to Satellite Navigation. InTech eBooks. https://doi.org/10.5772/56764
• Mohamed, Majeed, and Vikalp Dongare. 2021. Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation. Springer Singapore. https://doi.org/10.1007/978-981-16-0104-0
• Naveh, Ben-Zion, and Azriel Lorber. 2001. Theater Ballistic Missile Defense. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.473852
• Nielsen, Jack Norman. 1960. Missile Aerodynamics. McGraw-Hill. https://openlibrary.org/works/OL4626547W
• Nielsen, Jack. 1988. Missile Aerodynamics. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.062902
• Papoulis, Athanasios. 2002. Probability, Random Variables, and Stochastic Processes. McGraw-Hill. https://openlibrary.org/works/OL4455624W
• Parameter Estimation Techniques and Application in Aircraft Flight Testing. 1974. NASA. https://ntrs.nasa.gov/citations/19740017456
• Ramachandra, K. V. 2018. Kalman Filtering Techniques for Radar Tracking. CRC Press. https://doi.org/10.1201/9781482273113
• Reusable Launch Vehicle: Technology Development and Test Program. 1995. National Academies Press. https://doi.org/10.17226/5115
• Schmidt, Robert Kyle. 2015a. Advances in Aircraft Landing Gear. SAE International eBooks. https://doi.org/10.4271/pt-169
• Schmidt, Robert Kyle. 2021. The Design of Aircraft Landing Gear. SAE International eBooks. https://doi.org/10.4271/9780768099430
• Seddon, John, John Seddon, and E. L. Goldsmith. 1999. Intake Aerodynamics. Blackwell Science Ltd. https://openlibrary.org/works/OL12156839W
• Shneydor, N. A. 1998. Missile Guidance and Pursuit. Woodhead Publishing Limited. https://doi.org/10.1533/9781782420590
• Tanner, John A. 1990. Aircraft Landing Gear Systems. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19910042077
• Test Techniques for Flight Control Systems of Large Transport Aircraft. 2021. Elsevier. https://doi.org/10.1016/c2018-0-00829-4
• Titterton, D. H., David Titterton, and John Weston. 2004. Strapdown Inertial Navigation Technology. Institution of Electrical Engineers. https://openlibrary.org/works/OL12278234W
• Volkov, Konstantin, ed. 2023b. Hypersonic and Supersonic Flight: Advances in Aerodynamics, Materials, and Vehicle Design. IntechOpen. https://doi.org/10.5772/intechopen.104045
• Wang, Zinan. 2017. Dual-Polarization Two-Port Fiber-Optic Gyroscope. Springer Singapore. https://doi.org/10.1007/978-981-10-2836-6
• Werrell, Kenneth P. 1985a. The Evolution of the Cruise Missile. United States Government Printing Office. https://openlibrary.org/works/OL2937070W
• Yanushevsky, Rafael. 2007a. Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281
• Yanushevsky, Rafael T. 2018e. Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954
• Zarchan, Paul. 2012. Tactical and Strategic Missile Guidance, Sixth Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.868948
• Zarchan, Paul, ed. 2019. Tactical and Strategic Missile Guidance, Seventh Edition: SET. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.105845
• Zarrop, Martin B., ed. 1979b. Optimal Experiment Design for Dynamic System Identification. Springer-Verlag. https://doi.org/10.1007/bfb0040988
• Zhao, Donghua. 2024a. Intelligent Information Processing for Polarization Compass and Inertial Integrated Navigation System. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-7135-6

Commercial Sources

• Landis. 2020a. “Flashback, The Navaho Missile, Part 1.” https://www.edwards.af.mil/News/Article/2139264/flashback-the-navaho-missile-part-1/

General Sources

• MacKenzie, Donald, and Peter D. Zimmerman. 1992. “Inventing Accuracy: A Historical Sociology of Nuclear Missile Guidance.” Physics Today 45 (2): 102–3. https://doi.org/10.1063/1.2809544
• Pope, Alan, and Robert E. Street. 1959. “Aerodynamics of Supersonic Flight.” Physics Today 12 (2): 34–36. https://doi.org/10.1063/1.3060679

Tertiary Sources

• “Aggregat.” 2026. Wikipedia. Last modified March 4, at 09:18 (UTC). https://en.wikipedia.org/w/index.php?title=Aggregat&oldid=1341661265
• “Autoland.” 2026. Wikipedia. Last modified July 28, at 18:58 (UTC). https://en.wikipedia.org/w/index.php?title=Autoland&oldid=1366560835
• “Circular Error Probable.” 2026. Wikipedia. Last modified April 24, at 08:00 (UTC). https://en.wikipedia.org/w/index.php?title=Circular_error_probable&oldid=1350828847
• “Navaho.” n.d. Encyclopedia Astronautica. Accessed October 24, 2026. http://www.astronautix.com/n/navaho.html
• “North American X-10.” 2024. Wikipedia. Last modified November 13, at 05:15 (UTC). https://en.wikipedia.org/w/index.php?title=North_American_X-10&oldid=1257092074
• Parsch, Andreas. 2002a. “North American RTV-A-5/X-10.” Directory of U.S. Military Rockets and Missiles. https://www.designation-systems.net/dusrm/app1/x-10.html
• Parsch, Andreas. 2002b. “North American SM-64 Navaho.” Directory of U.S. Military Rockets and Missiles. https://www.designation-systems.net/dusrm/app1/sm-64.html
• “Schuler Tuning.” 2026. Wikipedia. Last modified March 4, at 05:21 (UTC). https://en.wikipedia.org/w/index.php?title=Schuler_tuning&oldid=1341633917
• “SM-64 Navaho.” 2026. Wikipedia. Last modified July 17, at 19:56 (UTC). https://en.wikipedia.org/w/index.php?title=SM-64_Navaho&oldid=1364657940
• “Vertical Deflection.” 2026. Wikipedia. Last modified October 12, at 03:49 (UTC). https://en.wikipedia.org/w/index.php?title=Vertical_deflection&oldid=1379827213
• “Westinghouse J40.” 2025. Wikipedia. Last modified November 11, at 05:32 (UTC). https://en.wikipedia.org/w/index.php?title=Westinghouse_J40&oldid=1321552110

Related Posts

• Sechter, Brendan. 2025. “X-Planes: Framing and the Research Aircraft Model.” Brendan A R Sechter’s Development Blog, October 6. https://sgeos.github.io/aerospace/history/engineering/2025/10/06/x_planes_framing.html
• Sechter, Brendan. 2025. “X-Planes: Bell X-1.” Brendan A R Sechter’s Development Blog, October 7. https://sgeos.github.io/aerospace/history/engineering/2025/10/07/x_planes_bell_x1.html
• Sechter, Brendan. 2025. “X-Planes: Bell X-2.” Brendan A R Sechter’s Development Blog, October 8. https://sgeos.github.io/aerospace/history/engineering/2025/10/08/x_planes_bell_x2.html
• Sechter, Brendan. 2025. “X-Planes: Douglas X-3 Stiletto.” Brendan A R Sechter’s Development Blog, October 9. https://sgeos.github.io/aerospace/history/engineering/2025/10/09/x_planes_douglas_x3.html
• Sechter, Brendan. 2025. “X-Planes: Northrop X-4 Bantam.” Brendan A R Sechter’s Development Blog, October 10. https://sgeos.github.io/aerospace/history/engineering/2025/10/10/x_planes_northrop_x4.html
• Sechter, Brendan. 2025. “X-Planes: Bell X-5.” Brendan A R Sechter’s Development Blog, October 11. https://sgeos.github.io/aerospace/history/engineering/2025/10/11/x_planes_bell_x5.html
• Sechter, Brendan. 2025. “X-Planes: Convair X-6.” Brendan A R Sechter’s Development Blog, October 12. https://sgeos.github.io/aerospace/history/engineering/2025/10/12/x_planes_convair_x6.html
• Sechter, Brendan. 2025. “X-Planes: Lockheed X-7.” Brendan A R Sechter’s Development Blog, October 13. https://sgeos.github.io/aerospace/history/engineering/2025/10/13/x_planes_lockheed_x7.html
• Sechter, Brendan. 2025. “X-Planes: Aerojet X-8 Aerobee.” Brendan A R Sechter’s Development Blog, October 14. https://sgeos.github.io/aerospace/history/engineering/2025/10/14/x_planes_aerojet_x8.html
• Sechter, Brendan. 2025. “X-Planes: Bell X-9 Shrike.” Brendan A R Sechter’s Development Blog, October 15. https://sgeos.github.io/aerospace/history/engineering/2025/10/15/x_planes_bell_x9.html