X-Planes: Bell X-9 Shrike

The Bell X-9 Shrike was launched from a trapeze in the bomb bay of a modified bomber and then flown toward a target eighty kilometres away by radio commands from the aircraft that had just released it. It carried no pilot, it was never intended to be recovered except for its instrument package, and it existed to prove out a nuclear standoff missile. This article is the tenth 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, and the X-8.

It is the second article in a row whose subject is not an aircraft, and the two are not alike. The X-8 had to bring data back. The X-9 had to take a command out. The standard inventory of the series gives it a single page in Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50, Parsch 2002 gives the designation history, and the vehicle-level compilations are Miller 2001 The X-Planes, X-1 to X-45 and Ordway and Wakeford 1960 International Missile and Spacecraft Guide.

The Research Question

Every vehicle in this series so far has had a keystone that is ultimately physical. Transonic drag rise, aeroelastic divergence, reactor shielding mass, ramjet combustion, atmospheric optical depth. Each is a question about the behaviour of matter, and each is answered by measuring the matter.

The X-9’s binding unknown is not physical. It is a control-loop problem, and its specification is a probability.

The military characteristics the Army Air Forces published on 15 July 1945 asked for a missile launched from between 20,000 and 45,000 feet, travelling at not less than 1,200 miles per hour, over a range of not less than 100 miles, that would strike within 500 feet of the target 75 percent of the time [GAM-63 RASCAL]. Every other number in that requirement is a performance figure of the kind the earlier articles in this series have dimensioned repeatedly. The last one is different in kind, because it describes a distribution.

The Specification Is a Variance

A missile that misses by a random amount in two dimensions, with independent and equal-variance errors in range and in deflection, lands at a radius whose distribution is Rayleigh. The statistic built on it is the circular error probable, and the standard treatments are Papoulis and Pillai 2002 Probability, Random Variables and Stochastic Processes for the distribution and Driels 2013 Weaponeering, Conventional Weapon System Effectiveness and Przemieniecki 2000 Mathematical Methods in Defense Analyses for its use in weapon assessment. The probability of landing within a radius $R$ is

\[P(R) = 1 - \exp\left( -\frac{R^{2}}{2\sigma^{2}} \right) \tag{1}\]

with $\sigma$ the standard deviation along either axis. Inverting for the specification gives the variance the programme had to meet,

\[\sigma = \frac{R}{\sqrt{-2 \ln \left( 1 - P \right)}} = \frac{500 \times 0.3048}{\sqrt{2 \ln 4}} = \frac{152.4}{1.665} = 91.5 \, \text{m} \tag{2}\]

which is 300 feet. The figure more usually quoted is the circular error probable, the radius containing half the impacts, which follows from the same distribution as

\[\mathrm{CEP} = \sigma \sqrt{2 \ln 2} = 1.177 \, \sigma = 108 \, \text{m} \tag{3}\]

One hundred and eight metres at a hundred miles. That number is the X-9’s keystone, and the rest of this article is an account of what it costs.

The estimation of that quantity from a finite number of flights is a subject in its own right, since a programme of twenty-two launches, the lower of the two reported totals, cannot measure a fiftieth percentile precisely. Moranda 1959 compares the available estimators, Moranda 1960 treats the effect of a bias, and Kamat 1962 extends the comparison. A programme with twenty-two flights and a requirement stated at the seventy-fifth percentile is measuring the tail of a distribution with two dozen samples, and no acknowledgement of that difficulty appears in the record.

The size of that difficulty is computable. The relative standard error of a standard deviation estimate from $n$ samples of a normal population is

\[\frac{\sigma_{\hat{s}}}{s} \approx \frac{1}{\sqrt{2 \left( n-1 \right)}} \tag{4}\]

which for twenty-two flights is 15 percent, so a circular error probable estimated from every flight of the programme carries a confidence interval of roughly plus or minus thirty percent at two standard errors. A vehicle that measured 108 metres could not have been distinguished from one that measured 140. The estimator takes a simple form. From $n$ impacts at radial distances $r_i$ from the mean point, the maximum-likelihood estimate of the axis standard deviation under the circular normal assumption is

\[\hat{\sigma} = \sqrt{\frac{1}{2n} \sum_{i=1}^{n} r_i^{2}} \tag{5}\]

and the circular error probable follows as $1.1774 \hat{\sigma}$. A bias changes the problem qualitatively rather than quantitatively, because a systematic offset $b$ is not reduced by more sampling. The total root-mean-square miss becomes

\[m_{\text{rms}} = \sqrt{b^{2} + 2 \sigma^{2}} \tag{6}\]

so a 50 metre bias on a 91.5 metre axis standard deviation gives 139 metres against 129 for the unbiased case, an inflation of only 8 percent that twenty-two flights would not detect. Student 1908 treats the problem of estimating a mean from few samples, and Shultz 1963, Schulte and Dickinson 1968, and Gallagher 1969 work out the two-dimensional case that a circular error probable requires, with the navigation-accuracy version in Swanson 1963. A bias, as opposed to a random error, changes the statistic in a way Moranda 1960 and McNolty 1962 both analyse. It is the failure mode that a small sample hides best.

Why an Error Budget Is the Design

Independent error sources add in quadrature, so a total standard deviation of 91.5 metres decomposes as

\[\sigma_{\text{total}}^{2} = \sum_{i} \sigma_{i}^{2} \tag{7}\]

If $n$ sources contribute equally, each is permitted

\[\sigma_i = \frac{\sigma_{\text{total}}}{\sqrt{n}} \tag{8}\]

which for five contributors is 41 metres and for eight is 32 metres. Every subsystem on the vehicle is therefore specified in metres of miss distance, including subsystems that have no obvious geometric relationship to the impact point. A propulsion dispersion becomes a range error. An autopilot trim bias becomes a deflection error. A release transient becomes both.

The quadrature sum has a property that matters more than the arithmetic. Because contributions add in the square, the largest single source dominates and the small ones are nearly free. Reducing a 60 metre contribution to 30 while leaving a 70 metre contribution alone moves the total from 92 to 76, whereas halving the 70 while leaving the 60 moves it to 69. The correct order of work is therefore always to attack the largest term, and an error budget is as much a scheduling document as a specification. Ball 2003 The Fundamentals of Aircraft Combat Survivability develops the same argument for survivability, where the structure of the problem is identical.

This is the sense in which the X-9’s keystone is a control problem and not a physical one. The quantity being minimised is a variance, the contributions are additive in the square, and the design activity is the allocation of that budget.

The Two Architectures Have Opposite Error Gradients

The decisive question is where the sensor sits, and the answer follows from geometry alone.

A radar of wavelength $\lambda$ and aperture $D$ has an angular beamwidth of roughly

\[\theta \approx \frac{\lambda}{D} \tag{9}\]

and a tracking system exploiting the beam shape, by comparing returns in adjacent channels, resolves an angle finer than the beamwidth by a factor $k$ that for a good monopulse arrangement is of order twenty. The beamwidth relation and the tracking accuracy that follows are Skolnik 2008 Radar Handbook, Barton 2004 Radar System Analysis and Modeling, and, for the monopulse case, Sherman and Barton 2011 Monopulse Principles and Techniques. The theoretical limit on an angle estimate from a noisy return is the Cramer and Rao bound of Van Trees 2001 Detection, Estimation, and Modulation Theory, which makes the factor $k$ a function of signal-to-noise ratio rather than a constant. The resulting cross-range position error at a range $R$ is

\[\varepsilon_{\perp} = \frac{R \, \theta}{k} = \frac{R \lambda}{k D} \tag{10}\]

The error is proportional to range. That proportionality is the difficulty, and it cuts in opposite directions depending on which end of the engagement the radar is at.

If the radar is in the launch aircraft, $R$ is the distance from the launcher to the missile, and the entire purpose of a standoff weapon is to make that distance large. For an X-band wavelength of 0.03 metres and a one metre antenna, the beamwidth is 0.030 radians, and at the specified hundred-mile range

\[\varepsilon_{\perp} = \frac{(1.6 \times 10^{5})(0.030)}{20} = 240 \, \text{m} \tag{11}\]

against a permitted total of 91.5 metres for every source combined. The specification cannot be met from the launch aircraft at the specified range. Setting the resolution equal to the total error budget gives the range at which it could just be met,

\[R_{\max} = \frac{k \, \sigma_{\text{total}} D}{\lambda} = \frac{(20)(91.5)(1.0)}{0.03} = 61 \, \text{km} \tag{12}\]

and using the circular error probable rather than the axis standard deviation gives 72 kilometres. The X-9’s reported range was eighty kilometres [Parsch 2002]. The correspondence is close enough to state plainly and loose enough that it should not be pressed. A vehicle guided by command from its launcher reaches about as far as its launcher’s radar can resolve, and no further.

If instead the radar is in the missile, $R$ is the distance from the missile to the target, and that distance goes to zero. The same relation then gives an error that shrinks throughout the terminal phase, so that a coarse seeker on a closing trajectory outperforms a fine sensor at standoff range. With a 0.4 metre antenna inside a 0.56 metre missile body the beamwidth is 0.075 radians, which is worse, and yet

\[\varepsilon_{\perp}(2 \, \text{km}) = \frac{(2 \times 10^{3})(0.075)}{20} = 7.5 \, \text{m} \tag{13}\]

The subsequent history adopted this architecture. A modern seeker is strapped down rather than gimballed, which trades mechanical complexity for a computation and brings a look-angle constraint the guidance law must respect, and Yang et al. 2022 describe the arrangement, with the constrained guidance in Kim and Park 2022b and Tahk et al. 2024. Hirwani et al. 2022 study the carriage of two seekers of different kinds, which removes the single-sensor failure the X-9’s link represented.

The consequence is clearer as a relation than as two numbers. Writing $R_L$ for the range from the launcher and $R_T$ for the range to the target, the two architectures give

\[\varepsilon_{\text{launcher}} \propto R_L, \qquad \varepsilon_{\text{missile}} \propto R_T \tag{14}\]

and along a trajectory those two quantities move in opposite directions, since $R_L$ grows monotonically from zero while $R_T$ falls monotonically to zero. The two architectures have opposite error gradients, and that fact explains the shape of the programme. It also explains why the operational weapon the X-9 served was named for its guidance link and not for its warhead or its airframe. The acronym of the GAM-63 RASCAL stands for radar scanning link, and the link in question carried a radar picture from the missile back to an operator in the launch aircraft, who monitored or corrected the missile’s course on it. The sensor rode the missile and the judgement stayed behind. The general form of that arrangement is command guidance, and its place among the alternatives is set out in Garnell 1980 Guided Weapon Control Systems, Siouris 2004 Missile Guidance and Control Systems, and Zarchan 2012 Tactical and Strategic Missile Guidance.

Sources of Tracking Error

The beamwidth argument above treats the factor $k$ as belonging to the radar alone. In fact it depends on the radar, the target, and the noise, and the three error sources that set it were being identified in the same years the X-9 flew.

The first is thermal noise, which bounds the angle estimate from below. For a monopulse arrangement the angular error from receiver noise is

\[\sigma_{\theta,\text{noise}} = \frac{\theta}{k_m \sqrt{2 \, (S/N)}} \tag{15}\]

with $k_m$ the monopulse slope, of order 1.5. At a signal-to-noise ratio of 100 this gives $\theta/21$, the origin of the factor of twenty assumed above, and at a signal-to-noise ratio of 10 it gives $\theta/6.7$. The resolution factor is not a constant but a function of range through the radar equation. For a target of cross-section $\sigma_t$ illuminated by a transmitter of power $P_t$ and gain $G$, the received power is

\[P_r = \frac{P_t G^{2} \lambda^{2} \sigma_t}{\left( 4\pi \right)^{3} R^{4}} \tag{16}\]

so that received power, and with it the signal-to-noise ratio, falls as the fourth power of range for a reflecting target,

\[\frac{S}{N} \propto \frac{1}{R^{4}} \tag{17}\]

so the angular error degrades as $R^{2}$ once noise dominates rather than as $R$. The maximum accuracy attainable from a pulsed radar against noise was established by Swerling 1956, with the phased-array case in Brennan 1961 and the off-boresight monopulse case in Berger 1971. A beacon on the missile replaces the fourth-power law with a second-power one,

\[P_{r,\text{beacon}} = \frac{P_b G_b G \lambda^{2}}{\left( 4\pi R \right)^{2}} \tag{18}\]

and this is why command systems track beacons instead of skin returns. The improvement is large. At eighty kilometres against a one square metre target, the ratio of the two received powers is

\[\frac{P_{r,\text{beacon}}}{P_{r,\text{skin}}} = \frac{P_b G_b \left( 4\pi \right) R^{2}}{P_t G \sigma_t} \tag{19}\]

which for a one watt beacon against a hundred kilowatt radar is $8 \times 10^{5}$ divided by the radar antenna gain $G$. For the one metre X-band antenna assumed earlier, whose gain $4\pi/\theta^{2}$ at the 0.030 radian beamwidth is about $1.4 \times 10^{4}$, that still leaves a factor of about 60 in the beacon’s favour. A one watt transmitter on the missile is worth more than a hundred kilowatts on the aircraft, and the choice of a beacon is the most consequential design decision in a command-guidance system. Feldman et al. 1962 and Philco Corp Palo Alto Ca 1963 treat the beacon as an engineered subsystem, including the decoder that lets the same link carry commands, and Savage 1969 describes the later strapdown tracker that removes the launcher entirely.

The second is scintillation, the fluctuation of the return as the target’s aspect changes. Brockner 1951 measured the angular jitter it produces in conical-scanning trackers, and Dunn et al. 1959 give the general treatment.

The third is glint, the most interesting of the three because it does not average away. A target with more than one scattering centre presents an apparent centre that can lie outside the target entirely, because the phase front arriving at the antenna is not spherical. The apparent angular position wanders by an amount comparable to the target’s angular extent, so the error is

\[\sigma_{\theta,\text{glint}} \approx \frac{c_g \, L_t}{R} \tag{20}\]

with $L_t$ the target’s dimension and $c_g$ of order 0.3. Glint error falls as one over range and noise error rises as range squared, so there is a range at which the two are equal and the tracking is at its best, which for a five metre missile beacon at a signal-to-noise ratio scaling from the launcher is a few tens of kilometres. The theory originates with Delano 1953, with the later development in Lindsay 1968 and Sims and Graf 1969, and the frequency-diversity remedy in Jones et al. 1970.

None of these three sources appears in the beamwidth calculation, and together they are the reason a real command system does worse than geometry alone suggests.

All three remain live subjects. Glint is now characterised for targets the period did not have, including the multiple-vehicle formations of Dou et al. 2024, with the point-target formulation of Klinefelter et al. 2022 and the super-resolution techniques of Liu et al. 2025a attacking it from the estimation side. Monopulse error estimation is adaptive rather than fixed in Paine 2023, and the amplitude-comparison performance the factor of twenty stands for is analysed by An and Lee 2020. The target’s radar cross-section, which the period treated as a number, is now a computed field, and Bużantowicz and Walenczykowska 2025 show how much the answer depends on how much of the geometry is retained, with measurement in Tan et al. 2024 and the active case in Niu et al. 2020.

The factor $k$ that this article treated as a constant of order twenty is, in the modern literature, the output of a computation.

The Architecture Comparison Was Being Made at the Time

The argument this article reconstructs from a beamwidth was, in its qualitative form, contemporary. Locke 1950 sets out the tactical limitations of beam-rider, command, and semi-active homing guidance side by side, the same comparison the X-9’s programme was making, and Tatum 1949 sets out some of the problems of guided-missile development as they stood the year the X-9 first flew. The textbook consolidations arrive later, in Levitt 1953, Clemow 1957, and Doersam 1965.

The third architecture in that comparison fails for a different reason and can be dimensioned the same way. A beam rider flies down a beam projected from the launcher and senses its displacement from the beam centre, so its lateral error is the beam’s width at the missile’s range multiplied by the fraction of a beamwidth the missile can sense,

\[\varepsilon_{\text{beam}} = \frac{R \, \theta}{k_b} \tag{21}\]

with $k_b$ of order ten, against the twenty a monopulse tracker achieves, because the missile’s receiver is small and its signal-to-noise ratio poor. At forty kilometres that is

\[\varepsilon_{\text{beam}} = \frac{(4 \times 10^{4})(0.03)}{10} = 120 \, \text{m} \tag{22}\]

Beam riding has the same range-proportional error as command guidance and a worse constant, so its only gain is the removal of the command link, and the X-9, which was guided by radio commands from its launcher [Parsch 2002], did not use it.

What the period sources do not contain is the arithmetic. They compare the architectures on tactical grounds, and none of those consulted here derives the range limit from the antenna. That derivation is this article’s, and the Epistemic State records it as such.

The Operator in the Loop

A loop closed through a human operator has a bandwidth the human sets. The crossover model of manual control holds that a trained operator adapts until the open loop behaves as an integrator with a pure time delay,

\[Y_{\text{open}}(s) \approx \frac{\omega_c}{s} e^{-\tau s} \tag{23}\]

in which $\tau$ is the operator’s effective delay, of order 0.3 seconds including neuromuscular lag. McRuer and Krendel 1974 Mathematical Models of Human Pilot Behavior presents the model and the measurements behind it, with the broader treatment of the human as an element in a control loop in Sheridan and Ferrell 1974 Man-Machine Systems. The experimental base was assembled through the 1960s by Wilde and Westcott 1963, Young et al. 1964, and Gagne and Wierwille 1966b, surveyed by Mitchell 1964, and extended to the decision-making the crossover model omits by Cohen and Ferrell 1969. The operator’s information rate, which bounds how much of a display he can use, is the subject of Baty 1970, with the optical-tracking case in Smith 1971 and Price 1970. The display is a component of the loop and not a convenience, since the operator can only close a loop around what he can see, and the period’s console engineering is documented in Fluhr 1963, Mitchell and Kinney 1966, and Drake 1967. Radar presentation of a ground scene, the content of the RASCAL link, brings its own interpretation problem in the relief displacement and parallax of Esten 1953.

The X-9 flew before nearly all of that work was done. The crossover model was formalised in the decade after the programme ended, in the work that McRuer and Krendel 1974 Mathematical Models of Human Pilot Behavior collects, so the operator’s bandwidth was a thing the designers accommodated by experiment and not by calculation.

The field it became is now about how much of the loop to give the human rather than how fast he can close it. Liu and Kaber 2025 model the proportion of a task that should be automated, An and Niu 2025 allocate functions dynamically as workload changes, and Tong et al. 2026a measure how presentation speed cuts both ways. Situation awareness, the quantity the X-9’s operator had least of, is studied by Houweling et al. 2024 and Chen et al. 2021b, with the interface design problem in Friedrich and Vollrath 2021. Whether the operator believes the automation has become its own subject, in Grindley et al. 2026 and Wang et al. 2024d. The X-9’s designers never had to ask that question, because there was nothing to believe. Stability with a phase margin $\phi_m$ then requires

\[\omega_c \le \frac{\pi/2 - \phi_m}{\tau} \tag{24}\]

which for a 45 degree margin and a 0.3 second delay gives

\[\omega_c \le \frac{1.571 - 0.785}{0.3} = 2.6 \, \text{rad/s} \tag{25}\]

The missile’s short-period motion is considerably faster than that. Taking a supersonic normal-force slope of

\[C_{N\alpha} = \frac{4}{\sqrt{M^{2}-1}} = \frac{4}{\sqrt{1.25}} = 3.58 \ \text{per radian} \tag{26}\]

on the 6.5 square metre wing area at Mach 1.5 and 12 kilometres, where the dynamic pressure is

\[q = \tfrac{1}{2} \rho v^{2} = \tfrac{1}{2}(0.312)(443)^{2} = 3.06 \times 10^{4} \, \text{Pa} \tag{27}\]

and a static margin of half a metre against a pitch inertia of

\[I_y \approx \frac{m L^{2}}{12} = \frac{(1588)(6.93)^{2}}{12} = 6.4 \times 10^{3} \, \text{kg} \cdot \text{m}^{2} \tag{28}\]

the aerodynamic stiffness and natural frequency are

\[M_{\alpha} = q S C_{N\alpha} \, \Delta x = (3.06 \times 10^{4})(6.5)(3.58)(0.5) = 3.6 \times 10^{5} \, \text{N} \cdot \text{m/rad} \tag{29}\] \[\omega_n = \sqrt{\frac{M_{\alpha}}{I_y}} = \sqrt{\frac{3.6 \times 10^{5}}{6.4 \times 10^{3}}} = 7.5 \, \text{rad/s} \tag{30}\]

The supersonic lift-slope relation used here is the linearised result of Nielsen 1960 Missile Aerodynamics and Anderson 2002 Modern Compressible Flow, and the rigid-body equations it feeds are Etkin and Reid 1996 Dynamics of Flight, Stability and Control and Blakelock 1991 Automatic Control of Aircraft and Missiles. The missile is about three times faster than the man flying it. A human cannot stabilise a vehicle whose natural motion outruns his own bandwidth, so the operator cannot be given the control surfaces. He must be given a slower quantity to command, with an automatic inner loop holding the fast motion. The X-9 needed an autopilot for this reason, a conclusion about architecture reached from two time constants and not from preference.

The accuracy an operator achieves tracking from an aircraft was measured directly, in an airborne simulator, by Douvillier et al. 1956. The simulator study is the closest thing in the accessible literature to a measurement of the X-9’s keystone quantity, and the National Advisory Committee for Aeronautics made it, not the programme that needed it. Lenhard et al. 1963 address a comparable accuracy question for a tracked object of known ballistics, which is how a range establishes its own instrumental error.

Programme Origin

The requirement that produced the X-9 was written on 15 July 1945 [GAM-63 RASCAL]. Trinity was fired on 16 July and Hiroshima was bombed on 6 August. The specification that dimensioned this vehicle predates the first demonstration of the weapon it would eventually carry by one day, and that fact is the source of most of what is strange about the programme.

The Army Air Forces had watched Germany air-launch more than a thousand V-1 missiles from Heinkel bombers and had repeated the experiment domestically with B-17 aircraft and the Republic-Ford JB-2, a copy of the V-1. The July 1945 characteristics asked for a supersonic successor. That became project MX-767, Mastiff, and Bell received a feasibility study contract on 1 April 1946 [GAM-63 RASCAL].

Bell spent eighteen months on it and concluded that rocket propulsion could not deliver the requested range. The requirement was reduced from 300 miles to 100. In May 1947 Bell received a development contract for a supersonic air-to-surface missile compatible with the B-29, the B-36, and the B-50, under project MX-776 [GAM-63 RASCAL]. Bell’s effort was led by Walter Dornberger, who had directed the German army rocket programme at Peenemunde, who had been held in British detention for two years after the war, and who came to the United States through Operation Paperclip and joined Bell in 1950 [Walter Dornberger]. He gave his own account of the German programme in Dornberger 1954 V-2, and Neufeld 1995 The Rocket and the Reich is the standard history. The continuity deserves notice. The man who ran the programme that produced the V-1’s ballistic cousin was, ten years later, running the American programme to build the V-1’s supersonic successor, and the vehicle in this article is the testbed for it.

The Air Force then split the project, and the split is why there is an X-9 at all. MX-776A would build a reduced-scale testbed, the RTV-A-4 Shrike, to develop the aerodynamic configuration, the radio control system, the rocket propulsion, and the procedures for checking out and launching an air-to-ground missile. MX-776B would build the operational weapon, the ASM-A-2 and later B-63 and GAM-63 RASCAL. In 1951 the RTV-A-4 was redesignated X-9 [Parsch 2002] [GAM-63 RASCAL].

The programme documents survive. Bell Aerospace Co Buffalo Ny 1953 covers both projects together, Bell Aerospace Co Buffalo Ny 1954 the weapon system, and Bell Aerospace Co Buffalo Ny 1956 the project as a whole, all of them in the defence technical archive, none in the aerospace one. This is a materially better primary base than the X-8 left behind, because a weapon programme reports to a service that keeps its reports. The sibling programme at Northrop left a comparable trace, and the rocket-model tests of the MX-775B configuration by Arbic and Gillespie 1953 are the Snark equivalent of the measurements described below.

What the Split Was For

Dividing a development programme into a testbed and a weapon is a risk-reduction move, and the risk in question needs stating precisely.

It does not reduce technical risk in the ordinary sense, because the testbed must solve most of the same problems. It reduces schedule coupling. A weapon programme carries a delivery date and a production commitment, and a failure inside it stops everything downstream. A testbed carries neither, so a failure inside it costs a vehicle and a month.

The X-9 was also explicitly intended to develop something the technical literature rarely treats as a deliverable, namely the practice of operating the thing. MX-776A was also to develop the skills to check out and launch the missile and experience in training crews to maintain and deploy it, before the operational missile existed [GAM-63 RASCAL], and the vehicle later served as an instructional tool for engineering, maintenance, and support personnel [Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50]. A test programme whose output includes trained sergeants is a different kind of programme, and the training role is plausibly one reason the vehicle flew from an operational bomber instead of a research aircraft. The reporting that such a programme generates is visible in the weapon-system programming and control apparatus of Hoch 1960 and the cost estimation of Army Missile Command Redstone Arsenal AL 1963, neither of which is engineering and both of which a service pays for.

Sizing From First Principles

Reported parameters for the X-9, from Parsch 2002 and the Bell X-9 Shrike entry, are a length of 6.93 metres, a wingspan of 2.39 metres, a body diameter of 0.56 metres, a wing area of 6.5 square metres, an empty mass of 964 kilogrammes, a launch mass of 1,588 kilogrammes, a Bell XLR65-BA-1 liquid rocket of 13.3 kilonewtons, a range of about 80 kilometres, and a ceiling near 20 kilometres. Reported speed is given as greater than Mach 1.5 in one source and Mach 2.0 in another, and that disagreement is carried through the Epistemic State unresolved.

The Two-Chamber Rocket

The propellant load follows from the two masses, at 624 kilogrammes. Taking an effective exhaust velocity of 2,157 metres per second, corresponding to a specific impulse of 220 seconds for a storable propellant of the period, the class surveyed in Clark 1972 Ignition, An Informal History of Liquid Rocket Propellants and treated in Rocket Propellant Chemistry, A Design-Tradeoff Space, the total impulse is

\[I_{\text{tot}} = m_p c = (624)(2157) = 1.35 \times 10^{6} \, \text{N} \cdot \text{s} \tag{31}\]

and at the rated thrust the burn time would be

\[t_b = \frac{I_{\text{tot}}}{F} = \frac{1.35 \times 10^{6}}{1.33 \times 10^{4}} = 101 \, \text{s} \tag{32}\]

A hundred seconds is a long burn for a rocket of this size, and the first sign that the vehicle is not thrust-limited. The ideal velocity increment available is

\[\Delta v = c \ln \frac{m_0}{m_f} = 2157 \ln \frac{1588}{964} = 1077 \, \text{m/s} \tag{33}\]

added to a launch speed of about 240 metres per second, which would give a burnout speed near Mach 4.5 at altitude if nothing resisted. The vehicle is reported to have reached between Mach 1.5 [Parsch 2002] and Mach 2 [Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50]. The difference is drag, and the consequence is that a rocket sized for the mission delivers far more impulse than the airframe can absorb at any one moment.

The case for dividing the thrust between two chambers follows. Running both gives the acceleration needed to reach cruise speed quickly, and shutting one down gives a sustainer thrust matched to the drag at that speed. The thrust required in level cruise is the drag,

\[F_{\text{cruise}} = D = q S \left( C_{D0} + \frac{C_L^{2}}{\pi A e} \right) \tag{34}\]

with the lift coefficient set by the weight,

\[C_L = \frac{m g}{q S} = \frac{(1588)(9.81)}{(3.06 \times 10^{4})(6.5)} = 0.078 \tag{35}\]

The zero-lift drag coefficient can be built up rather than assumed. Skin friction on a wetted area $S_{\text{wet}}$ contributes

\[C_{D,f} = C_f \, \frac{S_{\text{wet}}}{S} \tag{36}\]

The coefficient is not arbitrary. Turbulent flat-plate friction at supersonic speeds was measured directly in the period by Dhawan 1953 and analysed with the compressibility correction by Rubesin et al. 1951, with the later direct measurements of Dershin et al. 1967, the roughness dependence of Young 1965 and Thompson 1970, and an engineering calculation method in White and Christoph 1972. For a body of 0.56 metres diameter and 6.93 metres length plus two sides of the 6.5 square metre wing the wetted area is 25 square metres, so at a turbulent flat-plate coefficient of 0.0025

\[C_{D,f} = (0.0025) \frac{25.2}{6.5} = 0.0097 \tag{37}\]

Wave drag and base drag supply the remainder. Half the drag is friction and half is compressibility, the expected split for a slender supersonic body at Mach 1.5, so the assumed total of 0.02 is a buildup, not a guess. Both halves are still being computed rather than looked up, with the wave-drag side in Abraham et al. 2024 and the friction side in Szajnecki et al. 2025, Manzoor Hasan et al. 2024, and the reduction techniques of Zeng et al. 2024, Takahashi et al. 2019, and Amico and Cafiero 2026. Zou et al. 2026 examine the leeward-side case that a manoeuvring body presents. The base drag that a rocket-powered body modifies with its own plume is Kim et al. 2023a, Kim and Kim 2026, and Zhou et al. 2021. At a zero-lift drag coefficient of 0.02 on wing area the cruise drag is then of order

\[D \approx (3.06 \times 10^{4})(6.5)(0.02) = 4.0 \times 10^{3} \, \text{N} \tag{38}\]

which is 30 percent of the rated thrust. A single chamber of a two-chamber engine is very nearly the right size for cruise, a strong indication of the arrangement’s purpose even without a direct statement in the record. The alternative of throttling a single chamber was not practical at the time and is difficult now, as the deep-throttling work of Fiore et al. 2026 and Zhou et al. 2026a shows. Throttling a pressure-fed engine means changing the injector pressure drop. The flow through an injector orifice is

\[\dot{m} = C_d A_i \sqrt{2 \rho \, \Delta p} \tag{39}\]

so the pressure drop varies as the square of the flow, and halving the thrust quarters the drop. The stability criterion is conventionally that the drop remain above about a fifth of the chamber pressure,

\[\frac{\Delta p}{p_c} \ge 0.2 \tag{40}\]

because a stiff injector decouples the chamber’s pressure oscillation from the feed system’s response. Starting at that limit and halving the flow gives

\[\frac{\Delta p}{p_c} = \frac{0.2}{4} = 0.05 \tag{41}\]

at which point the chamber and the feed system are coupled and the engine can oscillate, the mechanism Otto and Flage 1960 studied experimentally. Two chambers avoid the problem entirely, because each runs at its design point or not at all. The period’s combustion instability literature includes Princeton Univ Nj 1952, Grey 1953, Matthews 1957, and Harrje 1959.

The chamber itself must survive the burn. Coulbert 1963 treats cooling technique selection for an engine of this class, and the failure mode that a hundred-second burn invites, the progressive deterioration of a regeneratively cooled wall rather than a prompt burnthrough, is the subject of Stanley 1969, Stanley 1970, and Stanley 1971. The relations used here follow Sutton and Biblarz 2016 Rocket Propulsion Elements, Hill and Peterson 1991 Mechanics and Thermodynamics of Propulsion, and Huzel and Huang 1992 Design of Liquid Propellant Rocket Engines.

The thrust-to-weight ratio at launch is

\[\frac{F}{m_0 g} = \frac{1.33 \times 10^{4}}{(1588)(9.81)} = 0.85 \tag{42}\]

which is below unity and would matter enormously for a vehicle leaving the ground. For a vehicle released at altitude with wings already flying, it does not, and the freedom to use a thrust-to-weight ratio below one is the first benefit of air launch.

What Air Launch Is Worth

The launch aircraft supplies altitude and speed, and both are recoverable as energy the missile does not have to produce.

The specific energy delivered at release is

\[e_{\text{launch}} = g h + \tfrac{1}{2} v^{2} \tag{43}\]

which at 12.2 kilometres and Mach 0.8, where the speed of sound is 295 metres per second, is

\[e_{\text{launch}} = (9.81)(1.22 \times 10^{4}) + \tfrac{1}{2}(236)^{2} = 1.20 \times 10^{5} + 2.79 \times 10^{4} = 1.48 \times 10^{5} \, \text{J/kg} \tag{44}\]

The velocity increment that would be required to generate the same specific energy from rest is

\[v_{\text{equiv}} = \sqrt{2 e_{\text{launch}}} = \sqrt{2.96 \times 10^{5}} = 544 \, \text{m/s} \tag{45}\]

Air launch is worth about 540 metres per second, which against the 1,077 metres per second the propellant supplies is a third of the vehicle’s total energy budget delivered by an aircraft that was going to be flying anyway. The mass ratio saved follows from the rocket relation,

\[\frac{m_0}{m_f} = \exp \left( \frac{\Delta v}{c} \right) \tag{46}\]

so avoiding 544 metres per second of increment saves a mass ratio factor of $\exp(544/2157) = 1.29$, or about 22 percent of the launch mass for the same payload and burnout condition.

An energy audit of the powered phase closes to the right order. Climbing from 12.2 to 20 kilometres and accelerating to Mach 2 at that altitude gives

\[\Delta E = m g \Delta h + \tfrac{1}{2} m_f v_f^{2} - \tfrac{1}{2} m_0 v_0^{2} = 1.22 \times 10^{8} + 1.68 \times 10^{8} - 4.4 \times 10^{7} = 2.5 \times 10^{8} \, \text{J} \tag{47}\]

against a propellant kinetic energy of

\[E_p = \tfrac{1}{2} m_p c^{2} = \tfrac{1}{2}(624)(2157)^{2} = 1.45 \times 10^{9} \, \text{J} \tag{48}\]

for an overall efficiency of 17 percent, the balance going to drag, to the residual kinetic energy of the exhaust, and to the difference between an ideal expansion and a real one.

The unpowered range after burnout follows from the glide relation, in which a vehicle of lift-to-drag ratio $L/D$ trades altitude for distance at

\[R_{\text{glide}} = h \, \frac{L}{D} \tag{49}\]

so the 80 kilometre range from a 20 kilometre apex implies an effective lift-to-drag ratio of four if all of it were glide. Four is a plausible supersonic figure for a winged body of this shape, and the fact that some of the range is powered means the true glide ratio is lower, and a lower ratio makes the number more believable, not less.

The powered segment can be separated out. During the burn the vehicle covers, at a mean speed of about 400 metres per second over 101 seconds,

\[R_{\text{powered}} = \bar{v} \, t_b = (400)(101) = 40 \, \text{km} \tag{50}\]

leaving 40 kilometres of glide from the 20 kilometre apex, which implies

\[\frac{L}{D} = \frac{R_{\text{glide}}}{h} = \frac{40}{20} = 2.0 \tag{51}\]

The dynamic pressure the structure sees along that trajectory is bounded by the climb. At the 12.2 kilometre release altitude the density is 0.301 kilogrammes per cubic metre and reaching Mach 2 there would give

\[q = \tfrac{1}{2}(0.301)(590)^{2} = 5.2 \times 10^{4} \, \text{Pa} \tag{52}\]

whereas at the 20 kilometre apex the density has fallen to 0.089 and the same Mach number gives only

\[q = \tfrac{1}{2}(0.089)(590)^{2} = 1.5 \times 10^{4} \, \text{Pa} \tag{53}\]

The vehicle climbs faster than it accelerates, so the maximum dynamic pressure occurs early and is modest. This follows from air launch, since a vehicle starting at sea level would meet its peak dynamic pressure at high speed and low altitude, and it adds to the list of things the launch aircraft pays for. A lift-to-drag ratio of two is a much more comfortable figure for a supersonic winged missile than four, and the resolution of the two estimates is that roughly half the range is flown under power. The maximum lift-to-drag ratio available to a supersonic configuration is bounded by wave drag, and the classical estimate

\[\left( \frac{L}{D} \right)_{\max} \approx \frac{4 \left( M + 3 \right)}{M} \tag{54}\]

gives 10 at Mach 2 for a slender aerodynamically clean shape, against which a value of two for a body carrying cruciform wings, four control surfaces, and a blunt base is unsurprising.

The Guidance Loop and the Miss Distance

The pieces above are an operator, an autopilot, an airframe, and a tracker. Putting them together gives the quantity the specification is written in.

The guidance loop’s job is to drive the lateral separation between the missile and the commanded line to zero before the flight ends.

The article has named the law that does it for several sections, and it can now be written down properly. Proportional navigation commands a lateral acceleration proportional to the rate at which the line of sight to the target rotates,

\[a_c = N \, V_c \, \dot{\lambda} \tag{55}\]

in which $\lambda$ is the line-of-sight angle, $V_c$ the closing velocity, and $N$ the navigation constant. The rule encodes the condition for a collision. Two bodies on a constant bearing with a decreasing range collide, so a line-of-sight rate of zero is the condition for an intercept, and a guidance law that drives $\dot{\lambda}$ to zero is driving the geometry toward a collision without ever computing where the collision will be.

Writing $y$ for the lateral separation from the collision course and $t_{go}$ for the time remaining, the line-of-sight rate for small angles is

\[\dot{\lambda} = \frac{\mathrm{d}}{\mathrm{d}t} \left( \frac{y}{V_c t_{go}} \right) \tag{56}\]

and substituting into the guidance law recovers the form the rest of this section uses,

\[a_c = N \, \frac{y}{t_{go}^{2}} + N \, \frac{\dot{y}}{t_{go}} \tag{57}\]

with $N$ conventionally between three and five. The relation shows at once that the commanded acceleration diverges as the time remaining goes to zero. A correction attempted late cannot be made.

The navigation constant also fixes how much acceleration the missile needs relative to whatever it is chasing. For a target manoeuvring at $n_t$, the missile’s steady requirement is

\[\frac{n_m}{n_t} = \frac{N}{N-2} \tag{58}\]

which for $N=3$ is three and for $N=4$ is two, so a larger navigation constant demands less acceleration and more bandwidth. The X-9’s target does not manoeuvre at all. No other feature simplifies its guidance problem as much, and the absence of target manoeuvre lets a four g airframe suffice.

The loop cannot respond instantly. Lumping the operator’s delay, the autopilot’s rise time, and the airframe’s response into a single guidance time constant $\tau_g$, the classical result for the residual miss caused by that lag, driven by a disturbance the loop must remove, is

\[\frac{m}{m_0} = f \left( \frac{t_{go}}{\tau_g}, N \right) \tag{59}\]

which for a first-order loop and a step disturbance introduced at a normalised time $x = t_{go}/\tau_g$ has the asymptotic form

\[\frac{m}{m_0} \sim \frac{x^{N-1}}{(N-1)!} \, e^{-x} \tag{60}\]

so the residual miss decays exponentially in the number of time constants remaining and is multiplied by a polynomial that delays the decay. The polynomial matters and it is easy to drop. At eight time constants the exponential factor is $3.4 \times 10^{-4}$ but the polynomial factor is $8^{3}/3! = 85$, so the product is

\[\left. \frac{m}{m_0} \right|_{x=8} = \frac{8^{3}}{6} \, e^{-8} = 2.9 \times 10^{-2} \tag{61}\]

which is three percent, not the three parts in a thousand the exponential alone would suggest. Ten time constants give $7.6 \times 10^{-3}$ and twelve give $1.8 \times 10^{-3}$.

Eight time constants leave three percent of the error and three time constants leave twenty-two percent of it. The practical criterion is therefore that the loop needs of order ten time constants of flight remaining to null an error,

\[t_{go} \ge 10 \, \tau_g \tag{62}\]

Taking the guidance time constant as the sum of the operator’s 0.3 seconds, an autopilot rise time of about 0.4 seconds at the damping computed below, and an airframe lag of 0.13 seconds at the natural frequency computed above,

\[\tau_g \approx 0.30 + 0.40 + 0.13 = 0.83 \, \text{s} \tag{63}\]

so the loop needs about eight seconds of flight remaining to remove an error, which at Mach 2 is

\[R_{\text{null}} = v \, t_{go} = (590)(8.3) = 4.9 \, \text{km} \tag{64}\]

Every error still present within five kilometres of the target arrives at the target. That number reorganises the error budget, because it means the release transient, the propulsion dispersion, and the mid-course tracking errors are all correctable and only the terminal errors are not. The terminal error sources are the tracker’s noise and glint, and the operator’s residual. The accuracy of a command-guided weapon is therefore set almost entirely by what happens in its last few seconds.

The Standoff Trade

The weapon exists to keep the bomber outside something. Writing $R_d$ for the radius of the defended zone and $R_m$ for the missile’s range, the launch aircraft is safe if

\[R_m \ge R_d + v_{\text{ac}} \, t_{\text{turn}} \tag{65}\]

with the second term the distance flown while turning away. The 1945 requirement asked for a hundred miles, and the X-9’s reported fifty miles [Parsch 2002] would have placed the bomber inside a defence of any depth.

Range is one of the two grounds, with payload, on which the X-9 was not adopted as an interim weapon [Parsch 2002], and the range ground is quantitative, not qualitative. The range shortfall was not a performance disappointment but an operational disqualification, since a standoff weapon that does not stand off far enough has no role at all. Waddell 1961 and Timenes 1964 supply the tactical-analysis machinery for evaluating this trade, and Jacobs et al. 1961 the probability calculation for an air-launched weapon against a defended target.

The Cost of Canard Control

The X-9 is a canard. Its control surfaces, being two all-moving forward vertical tails and small canards with movable trailing edges, sit forward of the centre of gravity, with fixed wings aft [Parsch 2002], and the operational RASCAL used the same canard configuration [GAM-63 RASCAL].

The arrangement’s advantage is that a forward surface generates its control force in the direction the vehicle is asked to turn. It also contributes a destabilising moment, because a lifting surface ahead of the centre of gravity moves the centre of pressure forward. The vehicle’s static margin is the normal-force-weighted mean position of everything, and adding a forward surface reduces it,

\[x_{cp} = \frac{\sum_i C_{N\alpha,i} \, x_i}{\sum_i C_{N\alpha,i}} \tag{66}\]

so the aft wings must be large enough to hold the centre of pressure behind the centre of gravity in spite of the canards. The X-9’s exposed wing area is large relative to its canards for this reason, and the configuration family was measured extensively in the same period by Moul and Wineman 1952 at an exposed wing-to-canard area ratio of sixteen to one, by Baber and Moul 1955 across Mach 0.7 to 1.8, and by Brown 1957 from Mach 1.2 to 2.1. Niewald and Moul 1950 give the control effectiveness and hinge moments for the same class, and the hinge moment matters because it sizes the actuator. For a control surface of area $S_c$ and mean chord $\bar{c}$ at hinge-moment coefficient $C_h$, the moment the actuator must hold is

\[H = q \, S_c \, \bar{c} \, C_h \tag{67}\]

which for a 0.35 square metre surface of half-metre chord at the dynamic pressure computed above and a coefficient of 0.05 is

\[H = (3.06 \times 10^{4})(0.35)(0.5)(0.05) = 268 \, \text{N} \cdot \text{m} \tag{68}\]

and the power required to move it at the rate the autopilot demands is

\[P = H \, \dot{\delta} = (268)(5) = 1.3 \, \text{kW} \tag{69}\]

More than a kilowatt of actuator power is a substantial installation on a 1,588 kilogramme vehicle, and it justifies the effort spent on aerodynamic balance of the surface, which reduces $C_h$ without reducing effectiveness. The technique goes back to Harris 1935, and Scott 1966 treats the actuator that must supply whatever balance does not remove. An all-moving surface also brings a flutter boundary that a fixed surface does not, measured for half-scale models by Ruhlin and Tuovila 1961. Kleckner 1946 and Mungall 1948 develop the point for all-moving surfaces, and Pfenneberger 1966 measures it for this configuration class. The canard arrangement in its aircraft form is investigated at high subsonic speeds by Sleeman 1957 and at Mach numbers of 1.41 and 2.01 by Driver 1958 and Spearman and Driver 1959.

The compensating advantage is that the trim penalty reverses sign. A tail-controlled vehicle deflects its tail downward to pitch up, losing lift, so the surface fights the manoeuvre before assisting it. A canard adds lift where it is wanted. The trim lift for a given manoeuvre is

\[L_{\text{trim}} = L_{\text{wing}} + L_{\text{canard}} \tag{70}\]

with both terms positive in a pull-up, against a tailed configuration in which the second term is negative. For a vehicle whose purpose is to change direction accurately at high dynamic pressure, that matters more than the static-margin penalty.

The control effectiveness itself sets how hard the vehicle can manoeuvre. A canard deflection $\delta$ produces a pitching moment that trims the vehicle at an angle of attack

\[\alpha_{\text{trim}} = -\frac{C_{m\delta}}{C_{m\alpha}} \, \delta \tag{71}\]

and the resulting normal acceleration in units of gravity is

\[n = \frac{q S C_{N\alpha} \alpha_{\text{trim}}}{m g} \tag{72}\]

At the dynamic pressure computed above, one degree of trimmed angle of attack gives

\[n = \frac{(3.06 \times 10^{4})(6.5)(3.58)(0.01745)}{(1588)(9.81)} = 0.80 \tag{73}\]

so the vehicle pulls roughly 0.8 g per degree of angle of attack. The roll axis is governed by the same geometry, and Adams 1951 gives the damping available from a cruciform arrangement. Roll matters here for a reason that does not arise on an unguided vehicle. A command in the inertial frame must be resolved into body axes before the control surfaces can act on it, and that resolution requires the roll angle. An error $\Delta\phi$ in the assumed roll angle turns a commanded pitch into a combination of pitch and yaw,

\[\begin{bmatrix} a_y \\ a_z \end{bmatrix} = \begin{bmatrix} \cos \Delta\phi & -\sin \Delta\phi \\ \sin \Delta\phi & \cos \Delta\phi \end{bmatrix} \begin{bmatrix} a_{y,c} \\ a_{z,c} \end{bmatrix} \tag{74}\]

so the cross-axis leakage is $\sin \Delta\phi$ of the commanded acceleration. A ten degree roll error puts 17 percent of every correction into the wrong axis, and a guided vehicle must therefore hold roll to a small angle instead of merely averaging it as the X-8 did. That requirement is a plausible reason the X-9 carries twin dorsal and ventral fins with rudders [Parsch 2002] rather than a symmetric cruciform tail. It is also the clearest difference in requirement between a guided vehicle and an unguided one. Friedman 1951 and Eggers et al. 1957 address the wave drag that the configuration pays for its wings, with the minimum-drag body shapes of Parker 1955 and Eggers 1965 and the base drag that the tail surfaces modify in Spahr and Dickey 1951. Slender-body theory for the forebody comes from Jones and Margolis 1946 and Brown and Parker 1945, the yawed-cone case from Stone 1945, and the design synthesis of the period from Jones 1959a. Zero-lift drag at the relevant Mach numbers was measured in free flight by Gillespie and Arbic 1951, the roll damping of a comparable configuration by Scherrer and Dennis 1951, and the wing-tail interference that a cruciform layout cannot avoid by Edwards and Hikido 1953. The effect of the plume on the aftbody, which matters for a vehicle that thrusts through most of its flight, is Deep et al. 1971. A five degree limit is therefore a four g vehicle, ample for course correction and far short of what an interceptor needs. The balance is correct for a weapon that must fly accurately rather than evasively.

The Trapeze Release

The X-9 was not released directly from the bomb bay. It was launched from a trapeze in the bomb bay of a specially modified EB-50D [Parsch 2002], and a trapeze of this kind, like the cradle that lowered the RASCAL from the bomb bay of its own test B-50 [GAM-63 RASCAL], lowers the store into the free stream beneath the aircraft before release.

The reason is that a bomb bay is full of separated, unsteady flow. A store released into it experiences forces that are large, poorly repeatable, and not predictable from any steady measurement, and the resulting scatter in initial attitude and rate propagates directly into the miss distance. Lowering the vehicle clear of the cavity trades a mechanism for a variance.

The size of the error being avoided can be computed. A heading error $\varepsilon$ imparted at release and never corrected produces a lateral offset at the target of

\[\Delta y = R \sin \varepsilon \approx R \varepsilon \tag{75}\]

which over 80 kilometres gives

\[\Delta y (1^{\circ}) = (8 \times 10^{4})(0.01745) = 1.4 \, \text{km} \tag{76}\]

One degree of release error is fifteen times the entire error budget. The guidance loop must therefore remove essentially all of it, and the loop’s authority is finite. A vehicle correcting a lateral offset $\Delta y$ over a remaining range $R_r$ at a normal acceleration $a_n$ needs

\[\Delta y \le \tfrac{1}{2} a_n \left( \frac{R_r}{v} \right)^{2} \tag{77}\]

which at four g and eighty kilometres of remaining range gives a correctable offset of

\[\Delta y_{\max} = \tfrac{1}{2}(39.2) \left( \frac{8 \times 10^{4}}{590} \right)^{2} = 3.6 \times 10^{5} \, \text{m} \tag{78}\]

so manoeuvre authority is not the binding constraint at long range. It becomes binding at short range, where the same relation with two kilometres remaining gives 225 metres, the same order as the errors the guidance is trying to remove. That asymmetry is why terminal accuracy is hard and why a correction made late is worth far less than the same correction made early. The guidance loop exists to remove such errors, and it can, but only once it has acquired. The argument for the trapeze is that the loop should not have to spend its authority on an avoidable disturbance.

The separation itself is a free-fall problem to first order. Clearing a vertical distance $d$ takes

\[t = \sqrt{\frac{2 d}{g}} \tag{79}\]

so three metres of clearance takes 0.78 seconds, during which the launch aircraft travels

\[\Delta x = v_{\text{ac}} t = (236)(0.78) = 184 \, \text{m} \tag{80}\]

and the missile falls behind by the difference between its drag deceleration and the aircraft’s. The tip-off rate, the angular rate imparted as the last constraint releases, follows from the moment acting over the interval between the forward and aft attachments letting go. For a vehicle whose centre of gravity is offset a distance $\ell$ from the last remaining support, the angular acceleration is

\[\dot{q} = \frac{m g \ell}{I_y} \tag{81}\]

which for a half-metre offset gives

\[\dot{q} = \frac{(1588)(9.81)(0.5)}{6.4 \times 10^{3}} = 1.22 \, \text{rad/s}^{2} \tag{82}\]

so an asymmetric release lasting 0.1 seconds imparts 0.12 radians per second, or 7 degrees per second. Seven degrees per second is a large rate for a vehicle whose entire heading budget is a fraction of a degree, so the release mechanism is a guidance component and not a piece of structure. Paradise 1971 treats redundancy in that mechanism.

The store-separation problem in its general form is the subject of the free-flight tunnel technique of Xue et al. 2019b in the modern literature and was treated in the period by the store-interference calculations of Margolis et al. 1958.

Dependent Systems

The Command Link

The X-9 flew two guidance systems in succession. The first was a radio command system built by the Federal Telecommunications Division of RCA, and the second a preset and radar command arrangement developed by Bell [GAM-63 RASCAL].

A command link carries very little information and must carry it very reliably. The required data rate follows from the number of channels and the rate at which corrections are useful, which is set by the loop bandwidth computed above. Sampling at ten times the crossover frequency,

\[f_s = 10 \, \frac{\omega_c}{2\pi} = 10 \, \frac{2.6}{6.283} = 4.1 \, \text{Hz} \tag{83}\]

and with two command axes at eight bits of resolution the required rate is

\[C_{\text{req}} = (2)(8)(4.1) = 66 \, \text{bit/s} \tag{84}\]

Sixty-six bits per second is nothing, and the entire difficulty of the command link is therefore not capacity but integrity.

Integrity has an adversary. A jammer of power $P_j$ at range $R_j$ competes with a command transmitter of power $P_c$ at range $R_c$, and the ratio at the missile’s receiver is

\[\frac{S}{J} = \frac{P_c G_c}{P_j G_j} \left( \frac{R_j}{R_c} \right)^{2} \, \frac{B_j}{B_s} \tag{85}\]

in which the last factor is the jammer’s dilution across a bandwidth wider than the signal’s. The command link’s low data rate is therefore an asset rather than a limitation, because a narrow signal bandwidth forces the jammer to concentrate its power precisely or waste most of it. The modern statement of the same trade is low probability of intercept, in which a waveform is spread and shaped so that an adversary cannot find it in the first place, treated by Shi et al. 2025a, Savci et al. 2021, and, at the antenna, Pehlivan and Yegin 2021. Xing et al. 2023 and Chen et al. 2026e analyse the countermeasure and counter-countermeasure exchange the X-9’s link would now face. The relation also shows why a link from the launching aircraft is comparatively hard to jam and a link from a distant ground station is not, since the ratio of ranges enters squared. The capacity bound is Shannon’s, developed in Cover and Thomas 2006 Elements of Information Theory and Sklar 2001 Digital Communications, Fundamentals and Applications, and because a command channel is limited by integrity and not by capacity, command links are built with margin rather than with coding. A link that fails intermittently is worse than one that fails completely, because the vehicle continues on its last command. The received power follows the same relation as any radio path,

\[P_r = \frac{P_t G_t G_r \lambda^{2}}{\left( 4 \pi R \right)^{2}} \tag{86}\]

and at 80 kilometres and a wavelength of one metre the free-space term is

\[\left( \frac{\lambda}{4 \pi R} \right)^{2} = \left( \frac{1}{4\pi \times 8 \times 10^{4}} \right)^{2} = 9.9 \times 10^{-13} \tag{87}\]

which is $-120$ decibels, so a hundred watt transmitter with modest antennas closes the link with a very large margin at this data rate. The integrity comes from that margin. The situation mirrors the X-8’s problem, where the link was bandwidth-starved carrying data downward, and the difference explains why the two vehicles reached opposite conclusions about what their radio had to do.

The latency of the radio path is negligible at

\[t_{\text{prop}} = \frac{R}{c_0} = \frac{8 \times 10^{4}}{3 \times 10^{8}} = 0.27 \, \text{ms} \tag{88}\]

so the delay in the loop is entirely the operator and the airframe. That ceases to be true at longer ranges, and the general problem of closing a control loop across a transmission delay was studied directly by Adams 1962, whose subject is remote control across distances long enough for the delay to dominate.

The Autopilot Inner Loop

The operator commands a heading or a rate. Something else holds the attitude, and it has to, because the airframe’s natural motion is faster than the operator by the factor computed above.

An attitude autopilot closes a rate loop around the airframe with gain $K$, giving a closed-loop characteristic equation

\[s^{2} + \left( 2 \zeta_a \omega_n + K M_{\delta} \right) s + \omega_n^{2} = 0 \tag{89}\]

in which $M_{\delta}$ is the control moment per unit deflection and $\zeta_a$ the small aerodynamic damping. The rate feedback appears only in the damping term, so the loop’s function is to add damping rather than stiffness, and the damping ratio achieved is

\[\zeta = \zeta_a + \frac{K M_{\delta}}{2 \omega_n} \tag{90}\]

Reaching a well-damped response of $\zeta = 0.7$ at the 7.5 radian per second natural frequency requires an added damping term of

\[K M_{\delta} = 2 \omega_n \left( \zeta - \zeta_a \right) = (2)(7.5)(0.7 - 0.05) = 9.8 \, \text{s}^{-1} \tag{91}\]

The autopilot is a damper, not a stabiliser, because the airframe is already statically stable by design. Static stability was a design choice, not a necessity, and a statically unstable airframe with a faster autopilot would manoeuvre harder at the cost of requiring the loop to work. Franklin Powell and Emami-Naeini 2019 Feedback Control of Dynamic Systems sets out the classical apparatus for the analysis, and Blakelock 1991 Automatic Control of Aircraft and Missiles and Garnell 1980 Guided Weapon Control Systems cover this application. The period’s servomechanism literature includes Hamer 1952, Merriam 1960, and, later, Etzweiler 1969 and Wilson 1970, with Atkinson 1968 on the angular-position servomechanism that an all-moving control surface is. Fagin et al. 1969 and Van Winkle and Rossi 1966 take the step from classical design to design against a stochastic input, the kind a noisy tracker demands.

Bias in the rate gyroscope is a distinct failure and it maps straight onto the error budget, because a constant rate error integrates into a constant heading error and thence into a lateral miss. Eslinger 1964 addresses its elimination, Vaughn 1960 the test methods that establish how large it is, and Flowe and Bright 1963 the drift of a gyroscope used as an azimuth reference instead of a rate sensor. The inertial alternative to command guidance, which removes the launch aircraft from the loop at the cost of drift, is set out for the period by Duncan 1958, with the stellar update that bounds the drift in Kochi and Dibble 1963 and the midcourse formulation in Eggleston and Dunning 1961, and the redundancy and failure-detection machinery that makes an inertial system trustworthy arrives much later in Potter and Deckert 1972 and Solov and Thibodeau 1973.

Inertial drift, which the X-9’s command guidance avoided, is now small enough that the architecture has inverted. A modern weapon navigates inertially and uses external references to bound the drift rather than the reverse, and Kozlov et al. 2026 report the bias stability now achievable from a device costing a few dollars. The alignment problem that consumes the accuracy budget before flight is Zhang et al. 2022f, Lin et al. 2022, and Li et al. 2019f, and the satellite-denied case that returns the problem to something the X-9 would recognise is Khalifa and Hashim 2026. The gyroscope required to close it is the reason the canard airframe and the automatic pilot have to be analysed together, as Gardiner et al. 1950 do for a canard airframe with a canted-axis gyroscope autopilot.

Structural flexibility sets the upper limit on the gain. A rate gyroscope mounted on a bending airframe measures the bending as well as the rigid-body rate, and if the loop gain is high enough at the bending frequency the two couple. The condition for stability is that the loop gain fall below unity before the first bending mode,

\[\left| K \, G_{\text{bend}}(j\omega_1) \right| < 1 \tag{92}\]

which in practice forces a notch filter or a gain low enough to compromise the rigid-body response. The frequency in question can be estimated. A free-free beam of length $L$, bending stiffness $EI$, and mass per unit length $\mu$ has a first elastic mode at

\[\omega_1 = \left( \frac{4.730}{L} \right)^{2} \sqrt{\frac{EI}{\mu}} \tag{93}\]

and for a thin-walled tube of radius $r$ and wall thickness $t$ the second moment of area is

\[I = \pi r^{3} t \tag{94}\]

which for the X-9’s 0.28 metre radius and a three millimetre wall gives $2.1 \times 10^{-4}$ metres to the fourth, so with an aluminium modulus of 70 gigapascals and a mass per unit length of 229 kilogrammes per metre,

\[\omega_1 = \left( \frac{4.730}{6.93} \right)^{2} \sqrt{\frac{(70 \times 10^{9})(2.1 \times 10^{-4})}{229}} = 117 \, \text{rad/s} \tag{95}\]

which is 19 hertz. The bending mode sits about sixteen times above the rigid-body natural frequency, a comfortable separation of the kind that makes a short, fat missile easier to control than a long thin one. The vehicles that made this hard were the boosters, which are long and slender and whose first mode falls close to the control bandwidth. The problem was treated for missiles of this generation by Lukens et al. 1961 and Freed and Miller 1961, and it remains the reason missile autopilot bandwidth is bounded from above by structure rather than by actuators.

The Launch Aircraft Is Part of the Weapon

A standoff missile guided from its launcher does not release the launcher. The bomber must remain within radio and radar range, oriented so its antenna sees the missile, and flying a track that keeps the geometry usable, throughout the missile’s flight.

The time involved follows from the range and the speed. At Mach 2 at altitude the missile covers eighty kilometres in

\[t_f = \frac{R}{v} = \frac{8 \times 10^{4}}{590} = 136 \, \text{s} \tag{96}\]

and during that time the launch aircraft, continuing at Mach 0.8, covers

\[\Delta x_{\text{ac}} = (236)(136) = 32 \, \text{km} \tag{97}\]

Turning away is not free either. A bank at load factor $n$ gives a turn radius

\[R_t = \frac{v^{2}}{g \sqrt{n^{2}-1}} \tag{98}\]

which for a heavy bomber limited to about 1.5 g is

\[R_t = \frac{(236)^{2}}{(9.81)\sqrt{1.25}} = 5.1 \, \text{km} \tag{99}\]

and a reversal takes

\[t_{180} = \frac{\pi R_t}{v} = \frac{\pi (5.1 \times 10^{3})}{236} = 68 \, \text{s} \tag{100}\]

during which the antenna sweeps through its full gimbal range and past it. Wrestler and Clifton G. 1965 analyses the turn performance for this manoeuvre, in which an aircraft must reverse as quickly as its structure allows. The bomber spends more than two minutes committed and closes two fifths of the standoff distance it just bought unless it turns away, and turning away costs the antenna its look angle. The engagement geometry is therefore a constraint on the aircraft, not only on the missile, and a large part of why the operational concept eventually failed. The general form of the problem, in which a weapon’s guidance requirement dictates the delivery aircraft’s flight path, is treated by Smyth 1972, and Waddell 1961 and Timenes 1964, cited above for the standoff trade, apply to such an engagement as well.

Bell was thinking about the successor problem within three years of the X-9’s last flight. Ehricke 1955 and Bell Aerospace Co Buffalo Ny 1955 describe the MX-2276 advanced strategic weapon system, a boost-glide vehicle that removes the launching aircraft from the engagement entirely by not needing one, and the same company produced both studies.

The Ground and Handling Problem

The X-9’s stated objectives included checkout, launch, maintenance, and deployment experience [GAM-63 RASCAL], and those turn into hardware requirements that the analytical literature usually omits.

A liquid-propellant missile carried inside an aircraft is a stowage hazard, and the magazine problem was studied directly by Quillin and Parry 1962. Wiltse 1955 treats the suspension and cushioning that let a missile survive ground handling, Paradise 1971 the release mechanism and its redundancy, and Cunningham 1963 the general specification of what a ground-test article must demonstrate. Packaging the electronics so they survive the environment and can be produced at cost is the subject of Woodward 1961.

None of this is glamorous and all of it is why the programme existed, since a weapon that works on the range and cannot be maintained on a base is not a weapon.

Structure and Heating

At Mach 2 the vehicle is warm but not hot. The recovery temperature at the surface, with a turbulent recovery factor of 0.89, is

\[T_r = T_{\infty} \left( 1 + r \, \frac{\gamma-1}{2} M^{2} \right) = 217 \left( 1 + (0.89)(0.2)(4) \right) = 372 \, \text{K} \tag{101}\]

which is 99 degrees Celsius and requires no exotic material at all. The transient behaviour of a thin skin, the quantity that matters for a flight lasting a few minutes, follows the lumped relation

\[\rho_m c_p t \, \frac{\mathrm{d}T_w}{\mathrm{d}t} = h \left( T_r - T_w \right) \tag{102}\]

with a time constant

\[\tau = \frac{\rho_m c_p t}{h} \tag{103}\]

that for a two millimetre aluminium skin at a convective coefficient of 150 watts per square metre kelvin is

\[\tau = \frac{(2800)(900)(2 \times 10^{-3})}{150} = 34 \, \text{s} \tag{104}\]

comparable to the flight time, so the skin never reaches equilibrium. Huston et al. 1948 and Lo 1948 analysed this transient in the period, both for conical bodies in short-duration high-speed flight, the X-9’s case.

The structural sizing is set by the manoeuvre load, not by temperature. At the four g limit computed above the wing bending moment at the root is of order

\[M_{\text{root}} = n \, m g \, \frac{b}{8} = (4)(1588)(9.81) \frac{2.39}{8} = 1.86 \times 10^{4} \, \text{N} \cdot \text{m} \tag{105}\]

which a spar of modest depth carries easily, and the general apparatus is Bruhn 1973 Analysis and Design of Flight Vehicle Structures. Thermal relations are Incropera and DeWitt, Fundamentals of Heat and Mass Transfer. Heating is not a design driver here, and the negative result should be recorded, because the X-9 is the first vehicle in this series for which the answer to the thermal question is that there is no thermal question. The X-1 needed the analysis and did not have it. The X-9 could have had it and did not need it.

Instrumentation and Recovery

The X-9 carried an instrumentation package and, at the end of powered flight, could be brought down under a parachute to recover it [Parsch 2002].

That decision is the X-8’s argument arriving at a different answer for a different reason. The X-8 recovered its nose cone because photographic and emulsion records cannot be telemetered at any rate the period could achieve. The X-9’s guidance measurements could in principle be sent down by radio, so the recovery plausibly exists to retrieve hardware instead of records, which for a programme developing a guidance system means retrieving the guidance system and finding out what it did.

The descent under canopy follows the same terminal-velocity relation as any recovery,

\[v_t = \sqrt{\frac{2 m g}{\rho C_D A}} \tag{106}\]

so a 300 kilogramme package descending at 8 metres per second at sea level requires

\[A = \frac{2 m g}{\rho C_D v_t^{2}} = \frac{(2)(300)(9.81)}{(1.225)(1.4)(64)} = 53.6 \, \text{m}^{2} \tag{107}\]

corresponding to a canopy of 8.3 metres diameter. The materials problem for a supersonic deployment of that size is the subject of MacCarthy 1954 and the canopy behaviour of Meyer 1958, with the design relations in Knacke 1992 Parachute Recovery Systems Design Manual. Muehlner 1962 covers missile telemetry of the period and its evolution.

The Flight Test Record

The record is short and its shape is characteristic of a guidance programme rather than a performance one.

The first flight, in April 1949, was an unpowered glide drop of a dummy. The first attempt at a powered launch came more than a year later, in May 1950, and failed. The first fully successful flight was the fifth, in November 1950. Testing continued until January 1953. Parsch 2002 gives the sequence, and Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50 dates the first flight to 28 April 1949 and the last to 23 January 1953.

Thirty-one vehicles were built [Parsch 2002]. The number of flights is given as twenty-two in the GAM-63 RASCAL history and as twenty-eight in Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50, and the discrepancy is carried into the Epistemic State. The same history records that the programme used two different rocket thrust chambers at the outset, one from Aerojet and one from Solar, and from the sixteenth vehicle onward the Bell XLR65-BA-1. Three flights carried a warhead dispersing chemical bomblets. Warhead development for guided missiles of the period appears in Philipchuk 1952, Walters 1959, Seiple 1960, Magis 1960, and Naylor 1961, and the fuzing that decides when any of it functions in Kasdorf 1952 and Taylor 1956.

The programme was terminated well short of its originally intended number of flights because it had already met its objectives [GAM-63 RASCAL]. Ninety-three vehicles were initially ordered and thirty-one delivered [Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50]. Stopping for that reason is unusual, and no other available statement speaks as strongly to how the X-9 performed. Consideration was given to producing a limited number of Shrikes as an interim operational weapon until RASCAL was available, and the proposal died on range and payload [Parsch 2002].

The flights were conducted from Holloman Air Force Base and the associated ranges, whose instrumentation and its evolution are described by Muehlner 1962 for telemetry and, for the general problem of a missile range as an engineered object, by Gruntman 2019 writing about its Soviet counterpart.

None of the vehicles survived. The only known remaining fragment is part of a vertical stabiliser, held at the Larry Bell Museum in Mentone, Indiana [Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50].

What a Guidance Programme’s Record Looks Like

The eighteen months between the first glide drop and the first powered success is the number to attend to. It does not signal difficulty with the rocket.

A guidance system cannot be tested until the vehicle it guides flies repeatably, and a vehicle does not fly repeatably until its release, its propulsion, and its autopilot each work. The order of the record is therefore forced. Glide drops establish the release and the airframe. Powered flights establish the propulsion. Only then can the guidance loop be closed and the miss distances collected that the specification is written in.

A programme specified by a variance cannot begin measuring the thing it is specified by until most of its other work is finished, which is why guidance programmes look slow at the start and then finish abruptly.

The record also permits an inference about reliability. Four failures before the first full success, on a system whose per-flight success probability is $p$, has likelihood

\[L(p) = \left( 1 - p \right)^{4} p \tag{108}\]

which is maximised at $p = 0.2$. The best estimate from the opening of the programme is one flight in five, and the fact that the programme then completed its objectives inside thirty-one vehicles implies that $p$ rose substantially, as a development programme is meant to achieve. The formal machinery for a test-to-failure programme of this kind arrived later, in Blundell and Brashear 1962.

The number of flights required to demonstrate a reliability $p$ at confidence $1-\alpha$ with no failures is

\[n = \frac{\ln \alpha}{\ln p} \tag{109}\]

so demonstrating 90 percent reliability at 95 percent confidence needs

\[n = \frac{\ln 0.05}{\ln 0.90} = 28.4, \ \text{so 29 consecutive successes} \tag{110}\]

against a programme total of thirty-one vehicles. The X-9 could not have demonstrated its own reliability to any useful confidence even if every flight had succeeded, which is a general property of small flight-test programmes and not a criticism of this one.

Comparison With Ground Prediction

The comparison available here is unusually good, because the configuration family the X-9 belonged to was measured independently and at length by the National Advisory Committee for Aeronautics, abbreviated NACA, using the rocket-model technique described in the earlier articles of this series.

Moul and Wineman 1952, Baber and Moul 1955, and Brown 1957 each flew instrumented cruciform canard missile models across the transonic and low supersonic range, and Niewald and Moul 1950 measured control effectiveness and hinge moments for the same class. Spearman 1961 gives tunnel results for a series of cruciform-wing missiles with canard controls at Mach 2.01, and Peterson 1961 covers static stability and control of canard configurations from Mach 0.7 to 2.22. The tunnels themselves were being extended to the relevant conditions in the same years, and the instrumentation and technique reports of Diggins 1951, Smith 1953, and Adams and Rubin 1958 are the reason those measurements exist. The bomber the X-9 was to be carried by had its own tunnel programme, reported by Shantz 1953 and Anderson 1958.

This is a denser independent measurement base than any previous vehicle in this series enjoyed, and the cause is structural, not fortunate. A canard cruciform missile is a configuration family rather than a single aircraft, many organisations wanted the same derivatives, and the rocket-model technique could produce them quickly. The X-1’s transonic drag rise had to be measured by the X-1 because nothing else was shaped like an X-1.

The prediction problem is correspondingly easier and the article should say so. What the X-9 had to determine for itself was not the aerodynamics but the closed-loop behaviour, and no wind tunnel produces a miss distance.

The one place where prediction was hard is the interaction between the guidance loop and the airframe under realistic noise, and the analytical apparatus for that arrived after the X-9 finished flying. Abramovitz 1952 and Abramovitz 1953 treat the speed of response of proportional navigation systems and the effect of missile configuration on it, Stewart and Smith 1959 synthesise optimum homing guidance with statistical inputs, and Stewart 1961 gives an explicit linear filtering solution for the same problem. The two Stewart reports postdate the X-9’s last flight and the two Abramovitz reports appeared as it was ending, and the X-9’s guidance was designed and flown without them. The line continues through the three-dimensional formulation of Adler 1956, the final-value formulation of Abzug 1967, the closed-form solution of Guelman 1974, and the comparative evaluation of Price and Warren 1973. Potter 1964 separates guidance from navigation, which makes any of it tractable, and Aldrich and Krabill 1972 supply the state estimation that modern guidance assumes.

A programme that finished in January 1953 was using none of this, and the gap between what the X-9 flew and what the theory would later say it should have flown is a fair measure of how far ahead of its analysis the practice ran.

What the Data Changed

The RASCAL and Its Cancellation

The X-9’s direct consequence is the GAM-63. The operational missile used the X-9’s canard configuration and a rocket engine derived from the X-9’s, in a body nine feet longer and two feet larger in diameter. The programme was cancelled in September 1958 [GAM-63 RASCAL].

A testbed whose weapon is cancelled has an ambiguous legacy, and an honest account has to say so. The X-9 met its objectives. The weapon it served never became fully operational. The cancellation is attributed to the weapon’s limited range and accuracy and its toxic liquid propellants [Parsch 2002], to the Strategic Air Command’s judgement that it was already obsolete, and to a 1958 test record in which one of 65 scheduled launches succeeded [GAM-63 RASCAL], none of which are failures of the X-9. The standoff weapon role passed to the AGM-28 Hound Dog and later to air-launched ballistic missiles such as Skybolt, both of which Jenkins Landis and Miller 2003 American X-Vehicles, An Inventory X-1 to X-50 names among the later standoff weapons for which the X-9 served as a conceptual prototype, and Werrell 1985 The Evolution of the Cruise Missile traces the wider evolution of the category.

The Error Budget as a Method

The method survived, and the hardware did not.

Specifying a weapon by a circular error probable, decomposing that figure into an error budget allocated across subsystems, and verifying it statistically over a flight programme is now how guided weapons are procured. The statistical machinery was still being worked out while the X-9 flew, in Moranda 1959, Moranda 1960, and Kamat 1962, and the connection between accuracy and effect through a damage function was made explicit by Lilliefors 1957.

The argument as a whole leads to this relation, so it is set out in full. For a weapon with a lethal radius $R_L$ against a given target, delivered with circular error probable $\mathrm{CEP}$, the single-shot kill probability is

\[P_k = 1 - \left( \tfrac{1}{2} \right)^{\left( R_L / \mathrm{CEP} \right)^{2}} \tag{111}\]

which equals one half when the lethal radius equals the circular error probable, and rises steeply thereafter. The relation assumes a definite lethal radius, and neither the lethality nor the aim point is that clean in practice. McNolty 1965 treats the case where the lethal effect is itself a random variable, Braithwaite 1962 the extrapolation of sparse kill-probability data, and Lilliefors 1957 gives the hand computation the period used. The shape of the damage function turns out to matter more than the accuracy fed into it, as Moon 2021 finds, and the structural-response side that determines that shape is now simulated in Temsah et al. 2021 and predicted by learned models in Almustafa and Nehdi 2020. Inverting for the accuracy required to reach a given kill probability,

\[\mathrm{CEP} = \frac{R_L}{\sqrt{\log_2 \left( \dfrac{1}{1 - P_k} \right)}} \tag{112}\]

The weapon-effects relations behind the lethal radius are Glasstone and Dolan 1977 The Effects of Nuclear Weapons, with nuclear weapon yield scaling and terminal ballistics setting the conventional case. And here the programme’s founding irony becomes arithmetic. The lethal radius is not free either, and it scales with yield in a way that makes the accuracy requirement collapse. Blast effects scale with the cube root of yield, so the radius at which a given overpressure is reached is

\[R_L = R_1 \, W^{1/3} \tag{113}\]

with $W$ the yield in kilotonnes and $R_1$ the one-kilotonne radius, which for the five pounds per square inch contour that destroys ordinary structures is about 0.43 miles, or 690 metres, for an air burst [Glasstone 1962 The Effects of Nuclear Weapons, Revised Edition]. A twenty kilotonne weapon therefore gives

\[R_L = 690 \, (20)^{1/3} = 1873 \, \text{m} \tag{114}\]

and a larger warhead gives 3,200 metres at 100 kilotonnes and 6,900 metres at a megatonne. Every factor of eight in yield doubles the tolerable circular error, and this arithmetic underlies the observation that accuracy and yield are substitutes. Morton 1966 covers the scaling and the target-dependence that make the choice of overpressure contour a judgement rather than a constant, with the vulnerability of a specific class of target in Andon 1965. For a warhead with a lethal radius of 1,500 metres against a soft target, corresponding to something near ten kilotonnes on this scaling, the accuracy needed for a 90 percent kill probability is

\[\mathrm{CEP} = \frac{1500}{\sqrt{\log_2 10}} = \frac{1500}{1.82} = 823 \, \text{m} \tag{115}\]

against the 108 metres the 1945 specification demanded. The requirement that dimensioned this vehicle was about eight times tighter than the weapon it carried needed. It was written one day before Trinity, and the MX-767 project it produced was already to develop a nuclear-armed missile [GAM-63 RASCAL], so the warhead changed almost at once and the accuracy figure in the record remains the 1945 one.

This does not make the X-9 pointless. It relocates its value. The accuracy work was largely surplus to the nuclear mission and directly applicable to everything that came after it, and the reliability, the launch procedures, and the trained crews were not surplus at all.

The Configuration

The cruciform canard layout the X-9 flew became common, and the measurement base assembled around it in the early 1950s outlived both the X-9 and the RASCAL. The reports cited in the Comparison section above were still being used as design data long after the vehicles that motivated them were scrapped, and the measurement programme continued past the X-9’s end in Bright and Peterson 1960, Foster 1959a, Anderson 1961, and Robinson 1958, with the hinge-moment case extended to rolling and manoeuvring flight by Pfenneberger 1966 and the prediction technique itself criticised by Abel 1971.

A configuration family outlives the programmes that motivate it, and the family is a more durable contribution than the vehicle. The consolidated design data of the period, in Army War Coll Carlisle Barracks Pa 1952 and its later volume Advanced Fuel Research INC East Hartford CT 1957, is where such measurements ended up.

The Contemporary Literature

Cluster	Records
Proportional navigation, the miss distance and modern guidance laws	870
Rocket propulsion, throttling and combustion stability	779
Radar tracking, glint and scintillation	630
Missile airframe aerodynamics, canard and cruciform	621
Autopilots, actuators and inertial instruments	618
The human operator and control across a delay	522
Command, beam-rider and homing architectures	500
Supersonic drag, skin friction and aerodynamic heating	337
Air launch, store separation and release	306
Flight test, recovery and reliability	306
Boost-glide successors, interception and defence	242
Command links, jamming and telemetry	71
Weapon effectiveness, kill probability and lethal radius	70
Accuracy, circular error and its estimation	68
Other guided-missile and flight literature	165
Total	6,105

Optimal Guidance Laws

The guidance problem the X-9 solved by putting a man in the loop is now solved by an optimisation. Modern treatments derive the guidance law from a cost functional rather than from a geometric rule, and the proportional navigation the period was working out is recovered as a special case, a connection made explicit by Lee and Cho 2021, who show pure proportional navigation to be inverse-optimal for a particular cost, and by Jeon et al. 2020. Weiss and Shima 2019 and Weiss and Shima 2021 give the linear quadratic formulation and Lin and Xin 2019 the state-dependent Riccati approach. The impact-angle and impact-time constraints that a modern weapon carries and the X-9 did not appear in Jung and Lee 2024 and Erer et al. 2024, the biased form that a landing or a glide requires in Yang 2025 and Levin and DeLaurentis 2025, and the emulation of an optimal law by a virtual target in Merkulov et al. 2025. Disturbance attenuation with measurement feedback is treated by Or et al. 2021, and the multi-agent extension the period could not have imagined by Shalumov 2019. Closed-form solutions of the linearised equations, the analysis Abramovitz 1952 was attempting with the tools of 1952, are now available in Markham 2019 and Markham 2024. Bryson and Ho 1975 Applied Optimal Control supplies the theoretical frame for all of it.

Weiss and Shima 2021 also give the minimum-effort formulations that bound how little control authority an intercept needs, and Bhattacharjee et al. 2021 the model-predictive treatment that carries explicit constraints.

What has not changed is the error gradient argument. A guidance law of any sophistication still cannot beat the geometry of where its sensor sits. Terminal seekers exist because of that geometry, and so does the modern equivalent of the RASCAL link, a synthetic-aperture radar image formed by the weapon itself, as Sun et al. 2024 describe.

Robust Autopilots

The inner loop the X-9 needed to hold its fast airframe while the operator flew slowly is now designed against explicit uncertainty rather than against a nominal model. Simões and Cavalcanti 2023 use a structured linear parameter-varying formulation, Sun et al. 2023 a gain-scheduled multifidelity design, Zhou et al. 2023c dynamic surface control, Lee et al. 2020 robust backstepping with an explicit time-delay term, and Gao et al. 2021 a differential-game formulation. The actuator that closes the loop has its own literature, since an electromechanical surface actuator is now the default, and Maré 2022 and Ruan et al. 2021 treat its sizing and its friction, with fault identification in Quattrocchi et al. 2022 and fault-tolerant reconfiguration in Li et al. 2026a. A hydraulic actuator of the X-9’s period could fail in one way and a modern electromechanical one can fail in several, so the literature is about diagnosis, not power. The flutter boundary that an all-moving surface brings is now computed and actively suppressed in Li et al. 2023d.

Data Links and the Latency Problem

The X-9’s loop closed across a radio path short enough that its delay was negligible, and the operator was the slow element. The modern version has the delay in the network rather than in the human, and closing a loop across a variable delay is a separate subject. Ma and McDonald 2026 identify the latency thresholds at which a human operator’s performance breaks down, the direct descendant of the crossover argument above. Compensation schemes are Chen and Liu 2021 using a Smith predictor, Shen et al. 2019 and Dehghan et al. 2021 for the bilateral case, and Kim et al. 2024 for outlier detection in the delay itself. Florencio et al. 2020 cast it as a networked-control problem.

Computed Canard Aerodynamics

The derivatives the rocket-model programme measured are now computed, and the configuration continues in service. Zhao et al. 2025c give a nonlinear body-aerodynamic model for a canard-controlled round, and Tai et al. 2023a and Tai et al. 2023b identify parameters from flight, the task the rocket-model technique performed by other means. Configuration studies of the kind that filled the 1950s reports continue in Shumway and Boranian 2025, with the tunnel-and-simulation parameter estimation that succeeded the rocket-model technique in Singh and Ghosh 2023, and the modern question is not what the derivatives are but how much a wrong derivative costs, which Li et al. 2025f answer by propagating aerodynamic modelling error into the closed-loop dynamics. The X-9’s designers could not ask that question, because they had no closed-loop model to propagate the error through.

Store Separation

The problem the trapeze solved by avoidance is now solved by computation and by scaled free-flight testing. Song and Ai 2021 analyse aircraft and store compatibility for an internal weapons bay, the same geometry as the X-9’s, and the similarity laws that make a tunnel test meaningful are derived by Xue et al. 2019b, Xue et al. 2020b, and Xue et al. 2020a. Air launch persists as a category, and Stewart et al. 2026 treat the flight dynamics of a modern air-launched vehicle, with the design optimisation in Li et al. 2022e and the smallest end of the category in Elliott et al. 2025.

Where the Mission Went

The standoff strike role the RASCAL was built for did not disappear, it accelerated. Boost-glide vehicles now occupy the niche, and the guidance and control problems are recognisably the same ones scaled up, with Bao et al. 2021 integrating guidance, control, and morphing, Autenrieb and Gruhn 2026 allocating control across redundant surfaces, and Jiang et al. 2022a treating the interception problem from the weapon’s side. Chen et al. 2024 and Zang et al. 2025 take the defensive side. The X-9’s descendants are being shot at by systems the X-9’s designers assumed would not exist, and Wang et al. 2024a develop counter-guidance that treats proportional navigation as something to be defeated rather than used. Trajectory optimisation is studied for the cruise case by Shachar et al. 2025 and for the ascent case by Lei et al. 2025b, and Cheah et al. 2025 and Gao et al. 2026b address the flight-test control synthesis that such a vehicle now needs.

The other direction the mission went is multiplication. Where the X-9 carried one operator’s attention to one target, air-launched effects now go in numbers and coordinate among themselves, which changes the accuracy requirement rather than tightening it, and Burchett 2019 studies the cooperative localisation that makes it work. A weapon that can be produced in quantity substitutes redundancy for precision. The yield scaling above describes the same substitution, bought a different way.

Test Instrumentation

The measurement problem has moved from getting data down to knowing whether to believe it. Ryu et al. 2022 predict sensor data in missile flight tests to detect faults, Fontana and Di Lauro 2022 survey the sensors themselves, and Głębocki and Jacewicz 2020 combine sensitivity analysis with flight results in the way a modern version of this programme would.

Estimating the Circular Error

The statistical question the X-9 programme faced, how to estimate a percentile of a two-dimensional distribution from a few dozen samples, has not gone away, and the surprising thing is how little the answer has changed. The estimators compared by Moranda 1959 and Kamat 1962 and the bias treatment of Moranda 1960 are still the estimators, and the modern literature on weapon accuracy is largely about getting more samples rather than about extracting more from few. Where the effort has gone is into predicting the trajectory well enough that the sample is not needed, as Zang et al. 2025 and Chen et al. 2024 show for the interception problem.

A programme that flies twenty-two times still cannot measure its own seventy-fifth percentile, and no amount of estimator sophistication repairs that.

Proportional navigation, the miss distance and modern guidance laws

The guidance law and what it leaves at the target. Proportional navigation and its variants, the miss distance and its adjoint analysis, optimal, differential-game and sliding-mode laws, and integrated guidance and control. The constrained impact belongs to this century. 280 of these titles name an impact angle or an impact time, the earliest dated one is from 2003, and 270 of the 278 dated ones are from 2010 or later, which agrees with the review above, where impact-angle and impact-time constraints are what a modern weapon carries and the X-9 did not.

870 records. [Cui et al. 2023] [Lakshmi et al. 2019] [Vairavan and Ratnoo 2017] [Abedi et al. 2007] [Abramovitz 1952] [Abramovitz 1953] [Abubakar et al. 2025] [Adler 1956] [Ai et al. 2019] [Akdag and Altilar 2005] [Akhil and Ghose 2012] [Al-Ashtari 2008] [Allen 1955] [Allen 1957] [Alpert 1987] [Alpert 1988] [Alpert 2020] [An et al. 2019] [An et al. 2022] [Analysis of Proportional Navigation 2007a] [Analysis of Proportional Navigation 2007b] [Analysis of Proportional Navigation 2011b] [Analysis of Proportional Navigation 2011a] [Anderson 1979a] [Anderson 1981] [Annam et al. 2021] [Application to Missile Guidance 2010] [Arita and Ueno 2013] [Ates 2015] [Ates 2016] [Ates 2018] [Ates 2019] [Atir et al. 2009] [Atir et al. 2010] [Baba and Howe 1988] [Baba et al. 1994] [Babu et al. 1994b] [Babu et al. 1994a] [Bai 2013] [Bai et al. 2023] [Balakrishnan 1987] [Balakrishnan et al] [Balraj Sharma 2023] [Bardhan and Ghose 2015] [Beard et al. 2007] [Behara et al. 2019] [Belkhouche et al] [Bell and Pringle 2000] [Bello 1981] [Ben-Asher et al. 2003] [Bergeron et al. 2011] [Bestard and Czarnecki 2008] [Bhattacharjee et al. 2021] [Bhattacharyya and Bhattacharjee 2003] [Bhitre et al. 2013] [Bingyi and Siliang 2008] [Boberg et al. 1997] [Bollino et al. 2006] [Boumenir 2005] [Bucco and Weiss 2013] [Bucco and Weiss 2015] [Bucco et al. 2012] [Bukovska 2025] [Calise 1980] [Callen 1979] [Cao et al. 2026] [Casler 1978] [Chadwick 1985] [Chang-Kyung Ryoo et al] [Chen and Chen 2020] [Chen and Wang 2017] [Chen and Wang 2018] [Chen and Yang 1998] [Chen and Yuan 1996] [Chen et al. 2014b] [Chen et al. 2020h] [Chen et al. 2020c] [Chen et al. 2020d] [Chen et al. 2021c] [Chen et al. 2021f] [Chen et al. 2022c] [Chen et al. 2022a] [Chen et al. 2023e] [Chen et al. 2023c] [Chen et al. 2026a] [Chen Peng and Sentang Wu 2008] [Cheng et al. 2019] [Cheng et al. 2025] [Chithapuram et al. 2013] [Cho 2022] [Cho and Kim 2016] [Cho and Lee 2021] [Cho et al. 1999] [Cho et al. 2015] [Cho et al. 2020] [Cho et al. 2022] [Choudhary et al. 2023] [Cicolani 1961] [Clark and Prazenica 2017] [Clark et al. 2015b] [Cloutier et al. 1988] [Cloutier et al. 1989] [Cotting and Cox 2005] [Cramer et al. 1990] [Creaser et al. 1998] [Cui et al. 2010] [Cuk et al. 2012] [Culp and Bickley 1993] [Das and Padhi 2008] [Deng et al. 2010] [Denney 1994] [Design of Guidance Laws 2007a] [Design of Guidance Laws 2007b] [Dhabale and Ghose 2012] [Dhabale and Ghose 2018] [Dhananjay and Ghose 2014] [Dhananjay et al. 2010] [Dhananjay et al. 2015] [Dharmendrabhai et al. 2022] [Differential Game-Based Interceptor Missile 2016] [Ding Chibiao and Mao Shiyi] [Ding et al. 2026b] [Donatelli and Fleeman 1982] [Dong and Ren 2020] [Dong et al. 2014] [Dong et al. 2018] [Dong et al. 2021a] [Dong et al. 2023d] [Dong et al. 2024] [Dong et al. 2025b] [Dougherty and Speyer 1997] [Dowdle 1985] [Du et al. 2026] [Duan and Liu 2022] [Dung 2026] [Duvvuru et al. 2022] [Ebrahimi and Nasrollahi 2023] [Eguchi et al. 1991] [El-Madany and Alswailem 1995] [Eltohamy and Kuo 2015] [Erer and Merttopçuoglu 2012] [Erer and Ozgoren 2013] [Erer et al. 2015] [Erer et al. 2024] [Evduzen 2026] [;; 2003] [Fan et al. 2014] [Fan et al. 2023] [Fang and Cai 2016] [Fang and Wu 2006] [Fang et al. 2006] [Feng et al. 2012] [Feng et al. 2013b] [Feng et al. 2013c] [Feng et al. 2022] [Feng et al. 2023] [Feng Tyan 2013] [Feng Tyan and Jeng Fu Shen 2006] [Fitz-Coy and Liu 1995] [Fortenbaugh 1983] [Franzini et al. 2018] [Fresconi 2011] [Gao and Cai 2017] [Gao et al. 2017a] [Gao et al. 2021] [Gao et al. 2024] [Garcia et al. 2015a] [Garcia et al. 2017] [Gaudet and Furfaro 2012] [Ghose 1994] [Ghose and Paul 2024] [Ghosh et al. 2013] [Ghosh et al. 2014] [Ghosh et al. 2016b] [Ghosh et al. 2016a] [Gilbert and Lin 1984] [Goldan and Gutman 2012] [Gong et al. 2024] [Gopalan et al. 2017] [Grinfeld and Ben-Asher 2015] [Grubin et al. 1964] [Gu et al. 2017] [Guelman 1974] [Guelman 1990] [Guidance Law Performance Analysis 2007] [Guidance Laws for Boost-Phase 2011] [Guilin Li and Haibo Ji 2014] [Guo et al. 2013] [Guo et al. 2016] [Guo et al. 2018c] [Guo et al. 2020] [Guo et al. 2025a] [Guo et al. 2025c] [Guo et al. 2025d] [Guo-Jiang Zhang et al. 2005] [Guodong et al. 2019] [Guohua Wei et al] [Gupta et al. 1979] [Gurfil 2001c] [Gurfil 2001a] [Gurfil 2001b] [Gurfil 2003] [Gurfil et al. 1998] [Gutman 1979] [Gutman 2005] [Gutman 2008] [Gutman 2011] [Gutman and Ben-Aharon 2009] [Gutman and Goldan 2011] [Gutman and Goldan Ben-Aharon 2009] [Gutman and Palmor 2010] [Gutman and Palmor 2011] [Gutman et al. 2012] [Gözde and Ozden 2021] [Hablani 1998] [Hablani and Pearson 2004] [Han et al. 2014b] [Han et al. 2015] [Han et al. 2016b] [Han et al. 2021c] [Hao and Haoping 2014] [Hardtla et al. 1987] [Hardy 1969] [Harl et al. 2010] [Hausl 1990] [He and Lin 2016] [He et al. 2015b] [He et al. 2017a] [He et al. 2019] [He et al. 2020b] [He et al. 2026] [Heller et al. 2013] [Hexner and Pila 2010] [Higher-Order Sliding Modes 2016] [Hirwani and Ratnoo 2018a] [Hirwani and Ratnoo 2018b] [Hirwani et al. 2022] [Hodzic and Prljaca 2021] [Hodžić and Prljača 2024] [Hoffman and Mahler] [Hong et al. 2020] [Hongchao Zhao et al. 2008] [Hongwei et al. 2018] [Hou and Wu 2006] [Hou and Zhuang 2025] [Hou et al. 2017] [Hu et al. 2011] [Hu et al. 2018] [Hu et al. 2021a] [Hu et al. 2024a] [Hu et al. 2025a] [Hu et al. 2025c] [Hu et al. 2025d] [Hu et al. 2025b] [Huang et al. 2011] [Huang et al. 2022a] [Huff and Herbert 1979] [Hughes and McFarland 2000] [Hull] [Hull and Mack 1988] [Hull and Muzumdar 1993] [Hull and Seguin 1993] [Hull and Seguin 1994] [Hull et al. 1987] [Hull et al. 1990] [Ibarrondo Hernández] [Imado and Miwa 1985] [Imado and Miwa 1994] [Imado and Uehara 1996] [Imado and Uehara 1998] [Imado et al. 1996] [Imado et al. 1998] [Impact Angle and Field-of-View 2025] [Integrated Design of Estimator 2016] [Integrated Guidance and Control 2016] [Ishimoto 1995] [Itohara and Miwa 1992] [Jalali-Naieni and Arabian Arani 2020] [Jalali-Naini and Ebrahimi 2017] [Jashwanth et al. 2026] [Orr and Russell] [Jeon and Karpenko 2019] [Jeon and Lee 2017] [Jeon et al. 2010] [Jeon et al. 2016] [Jeon et al. 2020] [Ji et al. 2020] [Jialing and Jianying 2015] [Jiang et al. 2021a] [Jiang et al. 2021b] [Jianyu et al. 2017] [Jing et al. 2018] [Jing et al. 2020] [Johnson et al. 2020] [Joongsup Yun et al. 2008] [Joonhyung Park et al. 2000] [Jun-fang et al. 2016] [Jung and Lee 2024] [Jung et al. 2024] [Kang and Song 2024] [Kang et al. 2023b] [Kelley et al. 1981] [Kelley et al. 1982] [Kim and Kim 2013] [Kim and Kim 2014] [Kim and Kim 2015] [Kim and Kim 2019] [Kim and Kim 2020] [Kim and Lee 2023] [Kim and Lee 2026] [Kim and Park 2019] [Kim and Park 2022b] [Kim and Shin 2022] [Kim et al. 1985] [Kim et al. 2006] [Kim et al. 2007] [Kim et al. 2010c] [Kim et al. 2013a] [Kim et al. 2013b] [Kim et al. 2015b] [Kim et al. 2016b] [Kim et al. 2017a] [Kim et al. 2018] [Kim et al. 2019] [Kim et al. 2020] [Kim et al. 2021] [Kim et al. 2023b] [Kochenderfer et al. 2008] [Kong and Zhang 2024] [Kong et al. 2025] [Kumar and Ghose 2014] [Kumar and Mukherjee 2022] [Kumar and Ojha 2013] [Kumar et al. 2014] [Kumar et al. 2018b] [Kumar et al. 2018a] [Kumar et al. 2022] [Kumar et al. 2023a] [Lai et al. 2018] [Lam 2005] [Lam 2006] [Lam 2007] [Lawrence 1998] [Lechevin and Rabbath 2011] [Lee 2013] [Lee and Cho 2021] [Lee and Choi 2019] [Lee and Kim 2023] [Lee et al. 2003] [Lee et al. 2013a] [Lee et al. 2013b] [Lee et al. 2018b] [Lee et al. 2019a] [Lee et al. 2024a] [Lei et al. 2025a] [Levin and DeLaurentis 2024] [Levin and DeLaurentis 2025] [Li and Qian 2019] [Li and Xu 2011] [Li et al. 2006] [Li et al. 2014a] [Li et al. 2014d] [Li et al. 2019h] [Li et al. 2019g] [Li et al. 2021c] [Li et al. 2022b] [Li et al. 2022c] [Li et al. 2023b] [Li et al. 2023a] [Li et al. 2023f] [Li et al. 2024b] [Li et al. 2024c] [Li et al. 2025g] [Li et al. 2025b] [Liang Hongwei and Ma Baoli 2008] [Lianos et al. 2001] [Lin and Cheng-Hung Lin 2014] [Lin and Xin 2019] [Lin et al. 1998] [Lin et al. 2000] [Lin et al. 2010] [Lin et al. 2020] [Lin et al. 2021] [Liu 2017] [Liu et al. 2011] [Liu et al. 2017b] [Liu et al. 2019c] [Liu et al. 2019b] [Liu et al. 2019a] [Liu et al. 2020c] [Liu et al. 2023a] [Liu et al. 2024f] [Liu et al. 2024c] [Liu et al. 2025b] [Liu et al. 2025d] [Liu et al. 2026c] [Liwei and Wuxing 2006] [Lizarraga et al. 2013] [Lu 1994] [Lu et al. 2018] [Lu et al. 2023] [Lum 2003] [Luo et al. 2020a] [Lv et al. 2018] [Lyu et al. 2018] [Ma et al. 2006] [Ma et al. 2020] [Ma et al. 2022] [Ma Pei-bei et al. 2009] [Maity et al. 2013] [Majumder and Kumar 2023a] [Majumder and Kumar 2023b] [Majumder and Kumar 2024b] [Majumder and Kumar 2024a] [Majumder and Kumar 2025] [Majumder and Ranjan Kumar 2020] [Maley 2015] [Manchester and Savkin] [Manchester and Savkin 2006] [Markham 2019] [Markham 2024] [Marzat 2017] [Mehrandezh et al] [Mengxiang and Weidong 2015] [Menon and Iragavarapu 1998] [Menon et al. 2003] [Merkulov et al. 2025] [Mi et al. 2018] [Miles and Limbach 2015] [Miloh et al. 1993] [Mirzaei et al. 2022] [Mishley and Shaferman 2022] [Mishley and Shaferman 2023] [Mishra et al. 1994] [Miss Distance Analysis 1999] [Missile Guidance and Control 2004] [Miwa and Kouya 1995] [Miwa et al. 1987] [Miwa et al. 1988] [Modified Guidance Law Based 2016] [Moldavskaya and Shinar 2015] [Moon and Kim 2000] [Moon and Kim 2011] [Moon et al. 2001] [Moon et al. 2015] [Moran and Altilar 2005] [Mracek 2006] [Mracek 2024] [Mukherjee and Ghose 2012] [Mukherjee and Ghose 2013] [Munusamy and Kadam 2026] [Murray 1984] [Mushtaq et al. 2026] [Nakagawa et al. 2017] [Nam 2025] [Nath and Ghose 2020] [Nesline and Zarchan 1984a] [Nesline and Zarchan 1984b] [Newman 1996] [Nguyễn 2019] [Nguyen 2026] [Ni et al. 2023] [Ni et al. 2025a] [Ning and Sheng 2023] [Ning and Sheng 2025] [Niu et al. 2024] [No et al. 2001] [Ochi 2003] [Oh 2001] [Ohlmeyer 1996] [Ohlmeyer and Menon 2001] [Omar 2008] [Ong and Pierson 1992] [Ong and Pierson 1996] [Optimal Guidance for Intercept 2024] [Optimal Guidance Laws 2016] [Oza and Padhi 2010] [Oza and Padhi 2012] [Ozkan et al. 2008] [Park 2015] [Park and Kim 2026] [Park et al. 2016b] [Park et al. 2020] [Parraud 2006] [Pearson and Hablani 2001] [Penev 2018] [Peng Liu et al. 2017] [Perelman et al. 2010] [Perelman et al. 2011] [Liu 2007] [Lee 2007a] [Pfleghaar 1985] [Pham et al. 2012] [Phillips and Chisholm 1995] [Pin-Jar Yuan 1997] [Po-Hsu Huang et al. 2010] [Pontani and Conway 2008] [Poveda et al. 2012] [Practical Techniques 2016] [Prasanna and Ghose 2012] [Price and Warren 1973] [Qi et al. 2025] [Qian and Chen 2025] [Yu et al. 2012] [Qian et al. 2017] [Qian et al. 2019] [Qiao and Chen 2013] [Qin et al. 2019] [Qingbiao Xi et al] [Qiu et al. 2017] [Qiuqiu et al. 2016] [Qu et al. 2017] [Quinter 1970] [Raj and Ganesh 2015] [Rajasekhar and Sreenatha 2000] [Ramesh et al. 2019] [Ranajit et al. 2014] [Rao 1993] [Rao 1998] [Rao and Ghose 2012] [Rao and Ghose 2013] [Ratnoo 2015] [Ratnoo 2016] [Ratnoo and Ghose 2007] [Ratnoo and Ghose 2008b] [Ratnoo and Ghose 2008a] [Ratnoo and Ghose 2009a] [Ratnoo and Ghose 2009b] [Ratnoo and Ghose 2010] [Ratnoo and Ghose 2012] [Rawling 1969] [Rea and Putnam 2007] [Rehman et al. 2024] [Reisner and Shima 2011] [Reisner and Shima 2013] [Ren et al. 2024b] [Ren et al. 2024a] [Ren et al. 2025] [Rezaee 2026] [Rinat and Ben-Asher 1999] [Rodriguez and Aguilar 1995] [Rogers] [Rusnak] [Rusnak 1992] [Rusnak 1993] [Rusnak 1996] [Rusnak 2010c] [Rusnak 2015] [Rusnak 2023] [Rusnak and Meir] [Rusnak and Meir 1991] [Ryoo et al. 2005] [Sadat Hosseini et al. 1995] [Sahu et al. 2025] [Saleem and Ratnoo 2018] [Salih and Moshaiov 2023] [Salih and Moshaiov 2024] [Sang Baohua and Jiang Changsheng 2009] [Savvas Sadiq Ali et al. 2020] [Schleich 1982] [Se-Ah Jang et al. 2008] [Seong-Ho Song et al] [Shaferman 2017] [Shalumov 2019] [Shang and Liu 2006] [Shang et al. 2006] [Shao et al. 2018] [Shao et al. 2021] [Shaoming et al. 2014] [Sharma and Ratnoo 2019a] [Sharma and Ratnoo 2019b] [Sharma and Richards 2004] [She et al. 2011] [Sheng et al. 2021] [Shi et al. 2015] [Shi et al. 2018a] [Shima and Golan] [Shin et al. 2012] [Shinar and Forte 1986] [Shinar and Forte 1991] [Shinar and Shima] [Shinar and Zarchan 1976] [Shinar et al. 1992] [Shinar et al. 1994] [Shinar et al. 2004] [Shiraishi et al. 2019] [Shiraishi et al. 2020] [Shneydor 1998e] [Shneydor 1998a] [Shneydor 1998f] [Shneydor 1998g] [Shneydor 1998c] [Shtessel and Tournes 2012] [Singh and Hota 2021] [Singh and Kumar 2021] [Singh and Sinha 2011] [Singh et al. 2026] [Sinha and Kumar 2020] [Sinha et al. 2021] [Sivrioglu 2026] [Smith 2007] [Smith 2008] [Snider 2019] [Snyder et al. 2015] [Son and Seong 2010] [Song 2004] [Song and Choi 2018] [Song et al. 2026b] [Spacecraft Intercept Guidance Using 1993] [Sperry Gyroscope Co Great Neck Ny 1963b] [Speyer 1976] [Speyer 1997] [Speyer and Hull 1986] [Speyer et al. 1990a] [Speyer et al. 1990b] [Spratlin 1987] [Sridhar and Gupta 1980] [Stallard 1980] [Stallard 1983] [Stansbery and Balakrishnan] [Stewart et al. 1958] [Stewart et al. 1959] [Strydom and Srinivasan 2017] [Dreyfus and Elliott 1963] [Su et al. 2016] [Sun et al. 2012a] [Sun et al. 2014] [Sun et al. 2015] [Sun et al. 2017] [Surve et al. 2020] [Surve et al. 2022] [Surve et al. 2023] [Tactical Missile Guidance Laws] [Tahk and Speyer 1989] [Tahk et al. 2001] [Tahk et al. 2024] [Takano et al. 2022] [Takano et al. 2024] [Takano et al. 2026] [Takeshi Yamasaki et al. 2007] [Talole and Banavar 1998] [Talole et al. 2006] [Tamhane et al. 2016] [Tan 2019] [Tan et al. 2021] [Tardioli et al. 2016] [Tardioli et al. 2017] [Tatiya et al. 2010] [Taur 2009] [Taur and Chern 2000] [Tekin and Erer 2015b] [Tekin and Holzapfel 2017] [Tekin et al. 2017b] [Tekin et al. 2017a] [Tekin et al. 2019] [Testing Guidance Laws Performance 2007] [Tian and Yuan-li 2019] [Tian et al. 2019] [Tian et al. 2020c] [Tian et al. 2020b] [Tournes and Johnson] [Tran 2025] [Tsalik and Shima 2016] [Turetsky and Shima 2016b] [Turetsky and Shima 2016a] [Tyan 2015] [Tyan and Shen 2010] [Ulybyshev 2005] [Vaddi et al. 2007] [Vaeth] [Van et al. 2023] [Varma and Kothari 2018] [Varma et al. 2016] [Vergez 1981] [Viswanath and Deb 2012b] [Viswanath and Deb 2012a] [Vivek and Ghosh 2025] [Wang and Lu 2018] [Wang and Lyu 2026] [Wang and Tan 2018] [Wang and Wang 2014b] [Wang and Wang 2014a] [Wang and Wang 2015] [Wang and Wang 2016] [Wang and Yang 2017] [Wang and Zhang 2014] [Wang and Zhang 2022] [Wang et al. 2006a] [Wang et al. 2014a] [Wang et al. 2014b] [Wang et al. 2016c] [Wang et al. 2016f] [Wang et al. 2016e] [Wang et al. 2016d] [Wang et al. 2017a] [Wang et al. 2018e] [Wang et al. 2018a] [Wang et al. 2019b] [Wang et al. 2019c] [Wang et al. 2021d] [Wang et al. 2021f] [Wang et al. 2022d] [Wang et al. 2022e] [Wang et al. 2022f] [Wang et al. 2022g] [Wang et al. 2023b] [Wang et al. 2023a] [Wang et al. 2023f] [Wang et al. 2023c] [Wang et al. 2024e] [Wang et al. 2024g] [Wang et al. 2024h] [Wang et al. 2024a] [Wang et al. 2025b] [Wang et al. 2026] [Wang et al. 2027] [Wang Ju and Wu Siliang] [Wei et al. 2016] [Wei et al. 2017] [Wei et al. 2025] [Wei-wei et al. 2013] [Weiss 2005] [Weiss and Beld 2006] [Weiss and Bucco 2015] [Weiss and Shima 2015] [Weiss and Shima 2016] [Weiss and Shima 2019] [Wen-jin Gu et al. 2007] [White et al] [Williams et al. 1983] [Williams et al. 1988] [Williams et al. 2025] [Willman 1988] [Wu] [Wu and Hou 2009] [Wu et al. 2014a] [Wu et al. 2018b] [Wu et al. 2018a] [Wu et al. 2018c] [Wu et al. 2025d] [Wu et al. 2025a] [Wu Yanan et al. 2016] [Xia and Sheng 2023] [Xia et al. 2023] [Xiang et al. 2017] [Xiang et al. 2019] [Xiang et al. 2020a] [Xiangyu et al. 2015] [Xin and Balakrishnan 2002] [Xin et al. 2006] [Xiong et al. 2014] [Xiong et al. 2019] [Xiong et al. 2022] [Xu and Guo 2015] [Xu and Liang 2015] [Xu and Liao 2016] [Xu et al. 2017] [Xu et al. 2020] [Xu et al. 2023] [Xu et al. 2026a] [Xuehua et al. 2015] [Yamasaki et al. 2024] [Yan and Lyu 2020] [Yang 2025] [Yang and Chen 1998] [Yang and Yang 1996a] [Yang and Yang 1996b] [Yang and Yeh 1988] [Yang et al. 1987] [Yang et al. 2014b] [Yang et al. 2025b] [Yang et al. 2025c] [Yanushevsky 2018k] [Yanushevsky 2018f] [Yanushevsky 2018d] [Yanushevsky 2018e] [Yanushevsky 2026a] [Yanushevsky 2026b] [Yanushevsky 2026c] [Yao et al. 2011] [Ye and Liu 2016] [Yi et al. 2018a] [Yi et al. 2018b] [Yi et al. 2021a] [Yilmaz and Yilmaz 2019] [Yogaswara et al. 2025] [Yomchinda 2015] [Yongmin Kim and Seo] [You and Zhao 2020] [You et al. 2023a] [You et al. 2023b] [You et al. 2025] [Yu and Chen 2011] [Yu et al. 2023] [Yuan 1996] [Yuan and Chern 1992b] [Yuan and Chern 1992a] [Yuan and Chern 1992c] [Yuan and Hsu 1993] [Yuan and Hsu 1994] [Yuan et al. 1993] [Yuan et al. 2000] [Yuan et al. 2001] [Yuan et al. 2023] [Yun and Ryoo 2014] [Yun et al. 2009] [Yurttas et al. 2014] [Yuxiang Zhou et al. 2013] [Zaikang and Defu 2019d] [Zarchan 1995] [Zarchan 2011] [Bashir et al] [Zeng et al. 2014] [Zhan et al. 2025a] [Zhang and Chen 2022] [Zhang and Gao 2025] [Zhang and Ma 2019] [Zhang and She 2015] [Zhang and Sun 2025] [Zhang and Wang 2015] [Zhang and Wang 2025] [Zhang and Wen 2024] [Zhang and Yan 2023] [Zhang and Yang 2015] [Zhang and Yang 2018] [Zhang et al. 2010] [Zhang et al. 2012c] [Zhang et al. 2014b] [Zhang et al. 2014a] [Zhang et al. 2015a] [Zhang et al. 2015b] [Zhang et al. 2016c] [Zhang et al. 2018b] [Zhang et al. 2018a] [Zhang et al. 2023b] [Zhang et al. 2025c] [Zhang et al. 2026g] [Zhang Ying-chun et al. 2010] [Zhao and Yang 2018] [Zhao et al. 2014] [Zhao et al. 2016] [Zhao et al. 2021b] [Zhao et al. 2025a] [Zhao et al. 2026b] [Zhao et al. 2026c] [Zhao et al. 2026a] [Zhiming and Yao 2019] [Zhou 2003] [Zhou and Xia 2020] [Zhou et al. 1999] [Zhou et al. 2013b] [Zhou et al. 2015] [Zhou et al. 2019e] [Zhou et al. 2019d] [Zhou et al. 2019c] [Zhou et al. 2020d] [Zhou et al. 2020b] [Zhou et al. 2020a] [Zhou et al. 2020c] [Zhou et al. 2023a] [Zhou Weiwen et al. 2010] [Zhu et al. 2011] [Zhu et al. 2022] [Zhu et al. 2023a] [Zhu et al. 2025c] [Zhu et al. 2025a] [ÖZkan 2021] [Özkan and Söylemez 2023] [Özkan et al. 2008] [Özkan et al. 2011]

Rocket propulsion, throttling and combustion stability

The propulsion the two chambers stand for. Liquid and solid rocket engines and motors, injectors and feed systems, regenerative and film cooling, throttling, and thrust chamber life. 205 of these titles name combustion instability or combustion stability, 60 of them dated before 1970, against 37 that name throttling. Solid propellant motors, which this vehicle did not use, account for 79 titles and are kept as part of the same combustion literature.

779 records. [Park 2005] [Alexander et al. 2011] [Abbe et al. 1967] [Abbe et al. 1968] [Acoustic Sensitivity Measurements 1996] [Aerojet-General Corp Sacramento Ca 1963] [Akbulatov et al. 2026] [Albanese et al. 2012] [Alcock and Hagar 1989] [de Almeida and Pagliuco 2014] [Almeida et al. 2021] [Altseimer 1952] [Alves Almeida et al. 2024] [Analysis of Pressure Feasibility 1960] [Ananoff 1941] [Anderson et al. 1995] [Anderson et al. 1996] [Anderson et al. 2012] [Anderson et al. 2013] [Anderson et al. 2015] [Anderson et al. 2019] [Andriievskyi et al. 2018] [Anoop et al. 2015] [Appendix C 1992] [Armbruster et al. 2021] [Armstrong 1952] [Armstrong 1989] [Armstrong and Kilner 1953] [Armstrong and Schlumberger 1990] [Artamanov 1963] [Assessment of Thrust Chamber 2004] [Azuma et al. 2016] [Baczynski 2022] [Badinand and Fransson 2002] [Baehr 1964] [Baetz 1974] [Baetz 1975] [Bai and Chung 2012] [Bai et al. 2020] [Bairamov and Bairamov 2022] [Baker 1967] [Baker 1969] [Balepin 2001] [Balepin 2006] [Barrère and Bernard 1957] [Bartrand 1988] [Bastress et al. 1967] [Baum and Levine 1982] [Baum and Levine 1984] [Bazarov 1998] [Bazarov and Yang 1998] [Bellows et al. 1984] [Beltran and Kosvic 1966] [Belyakov 2022] [Benjamin and McConnaughey 1991] [Bennewitz et al. 2013] [Benstein 1989] [Benstein 1991] [Bermudez 2024] [Berque and Georges 1992] [Betts and Frederick 2010] [Beyer 2003] [Bheary 2026] [Bickford 1968] [Bieneck 2026a] [Bieneck 2026b] [Bjorklund et al. 1979] [Black et al. 1967] [Blackman et al. 1965] [Blair and DeGeorge 2000] [Blomshield 2007] [Bonilla Romacho et al. 2023] [Borisov 2025] [Borovik et al. 2019] [Bortoloto et al. 2023] [Bower and Thomas 2018] [Bowman 1967] [Bracco et al. 1968] [Brennan 1967] [Briones and Wuerker 1978] [Broomby and Trifoni 2024] [Brown 2022a] [Brown 2022b] [Brown and Muzzy 1969] [Brown and Muzzy 1970] [Brown and Nelson 2005] [Brownlee 1963] [Brownlee and Roberts 1963] [Brummund et al. 1996] [Bujes 1962] [Bulat et al. 2024] [Burdett 1946] [Burstein 1967] [Burstein and Chinitz 1967] [Burstein and Chinitz 1968a] [Burstein and Chinitz 1968b] [Burstein et al. 1970] [Burstein et al. 1972] [Bushnell and Busse 1966] [Campbell 1962] [Campbell 1970] [Campbell and Riccio 1995] [Candler 2001] [Cannizzo 1997] [Carpenter and Jeffus 1962] [Carpenter and Jeffus 1963] [Casiano et al. 2009] [Casiano et al. 2010] [Casiano et al. 2013] [Cervantes et al. 2024] [Cha et al. 2023] [Chadwick et al. 1992] [Chadwick et al. 1993] [Chaudhary et al. 2025] [Chaudhry et al. 2026] [Chehroudi 2008] [Chehroudi 2009] [Chehroudi 2010] [Chelner 2002] [Chelner 2003] [Chen and Cui 2025] [Chen and Zhao 2005] [Chen et al. 1993] [Chen et al. 2009] [Chen et al. 2025b] [Chen et al. 2025a] [Chen et al. 2026c] [Cheng 1956] [Cheng 1985] [Cheng and Farmer 2002] [Cheng et al. 2016] [Cheng et al. 2017b] [Cheng et al. 2018] [Cherniavskyi 2026] [Chew 1973] [Chiu 1986] [Chiu 1987] [Chu and Xu 2014] [Chu et al. 2025] [Cieśliński et al. 2024] [Cieśliński et al. 2025] [Citarella et al. 2022] [Clark 1967] [Combs 1970] [Combs and Hoehn 1964] [Combs and Schuman 1965] [Combustion Instability and Transient 2007] [Combustion Instability in Solid 1960] [Sung 2004] [Cook and Quentmeyer 1980] [Cosens and Newton 1988] [Coulbert 1963] [Cox and Turney 1967] [Crabtree 1962] [Crachi et al. 2024] [Crocco 1951] [Crocco 1952] [Crocco 1965] [Crocco and Cheng 1953] [Crocco et al. 1960] [Crocco et al. 1962] [Crone et al. 1993] [Culick 1971] [Culick 1972] [Dederra 1975] [Harrje and Sirignano 1966] [Davidian 1989] [Davidian 1990] [de Iaco Veris 2020b] [de Iaco Veris 2020a] [Dean and Shurley 1958] [DeHoff et al. 1993] [Delcher et al. 1989] [Delmonte 1967] [Delplanque and Sirignano 1996] [Design of Gas-Pressurized Propellant 1992] [Design of Rocket-Engine Control 1992] [Design of Turbopump Propellant 1992] [Dethloff 1961] [Dipprey 1972] [Dodge et al. 1972] [Dolgih 2025] [Dolgopolov et al. 2025] [Douglass et al. 1959] [Dranovsky 2007] [Dubois et al. 1995] [Dunn 1990] [Eberhart et al. 2012] [Ekimogloy et al. 2026] [Elias and Gordon 1952] [Ellerbrock and Ziegenhagen 2006] [Elliott and Rose 1957] [Ellis et al. 1953] [Erickson 1992] [Escher et al. 1999] [Han 2004] [Evans and Smith 1978] [Evans et al. 2026] [Excelco Developments INC Silver Creek NY 1963] [Fang 1984] [Farmer and Cheng 2000] [Farvin and Peddieson 1988] [Fashbaugh and Streeter 1965] [Fatuev 2006] [Feng and Wang 2007] [Ferraiuolo et al. 2016] [Ferraiuolo et al. 2022] [Ferraiuolo et al. 2023] [Ferreira and Dourado 2018] [Ferrer and Santos 2023] [Fidler et al. 2025] [Filimonov 1968] [Fint et al. 2005] [Fiore et al. 2022] [Fiore et al. 2026] [Flandro et al. 2004b] [Flandro et al. 2004a] [Fong 1964] [Fontaine 1965] [Ryu 2009] [Fougnie] [France’s Liquid Propellant Rocket-Engine 2006] [Frey et al. 2011] [Friedland 1965] [Fulbright 1977] [Fundamental Mechanisms of Combustion 1995] [Gale and Moedt 1962] [Galli] [Gallo et al. 2024a] [Gallo et al. 2024b] [Gallo et al. 2024c] [Gao et al. 2023] [Garcia et al. 2018] [Genot 2021] [Gerstley and Tobin 1975] [Ghaffar et al. 2017] [Gibart] [Giuliano et al. 2007] [Giuliano et al. 2010a] [Giuliano et al. 2010b] [Glushko 1976] [Goertz 1995] [Golovitchev and Krulle 1997] [Gordon 1950] [Gordon and Brown 1963] [Gotsulenko 2008] [Graefe and Gordon 1957] [Graham 2010] [Greatrix 2009] [Greatrix 2011] [Greatrix 2013a] [Greatrix 2013b] [Greatrix 2014] [Greatrix 2018] [Greatrix 2021] [Greenwood et al. 1970] [Grenda et al. 1991] [Grey 1953] [Grosdemange and Schaeffer 1990] [Guo et al. 2021a] [Guo et al. 2022] [Habiballah et al. 1992] [Haga 2024] [Hagemann et al. 2006] [Haglind et al. 2007] [Hakim et al. 2020] [Hald 2003] [Han et al. 2004] [Hankins 1986] [Hardesty 1970] [Hardgrove and Krieg 1984] [Harper et al. 2004] [Harris 1963] [Harrje 1959] [Harrje 1972] [Harrje et al. 1962] [Hart and McClure 1965] [Harvazinski and Houba 2022] [Harvazinski et al. 2013] [Harvazinski et al. 2014] [Harvazinski et al. 2024] [Harvey 1970] [Hauser and Helfrich 1963] [Heat Transfer in Rocket 1993] [Heister 2008] [Herbertz and Selzer 2012] [Herbertz et al. 2012] [Hermance 1961] [Hoertel 1961] [Hoff 1967] [Hoffman 1987] [Holster 1973] [Holzmann and Hayden 1988] [Hornstein 1965] [Houhou et al. 2020] [Houser 1972] [Hsieh 1961] [Hu et al. 1994] [Hu et al. 2021b] [Hu et al. 2026b] [Huang 1985] [Huang 2000] [Huang et al. 2000] [Huang et al. 2022b] [Huang et al. 2024c] [Huang et al. 2024d] [Huang et al. 2025] [Hulka 2008] [Hunley 2008] [Hyde 2002] [Hyde and Argueta 2025] [Hydrodynamic and Thermal Analysis 2025] [Immich et al. 2001] [МГТУ им. Н.Э. Баумана and Александренков 2017] [Instability Phenomenology and Case 1995b] [Instability Phenomenology and Case 1995c] [Instability Phenomenology and Case 1995a] [Instrumentation for Research 1960] [Introduction to Liquid-Propellant Rocket 1992] [Nguyen 2020] [Nguyen 2021] [Saboktakin and Monjezi 2024] [Seader and Wagner 1964] [Jacob et al. 2010] [Japan’s Liquid Propellant Rocket-Engine 2006] [Jayan and Raghunandan 2003] [Jeng and Litchford 1991] [Jensen 2005] [Jensen et al. 1962] [Jha 2024] [Ji and Sun 2015] [Jialong Ji and Bing Sun 2014] [Jin et al. 2019] [Jurado et al. 1990] [Kamijo 1983] [Kamijo et al. 1981] [Kanda 2019] [Kanda et al. 2023] [Kang and Sun 2011] [Kang et al. 2025] [Kaplan 1961] [Karnesky and Colucci 1973] [Kassoy 1997] [Kassoy 2013] [Kawatsu 2019] [Kazaroff and Pavli 1990] [Keihl 2025] [Kenny et al. 2006] [Khan and Qamar 2020] [Kim et al. 1992b] [Kim et al. 1992a] [Kim et al. 2023c] [Kimura et al. 2010] [King and Salvaggi 1975] [Kirchhartz et al. 2012] [Kleinhenz et al. 2013] [Klem 1990] [Knab et al. 1998] [Knab et al. 2002] [Knab et al. 2009] [Knab et al. 2019] [Knight et al. 2015] [Kobayashi et al. 2011] [Kolesovas and Svitra 1976] [Kose and Celik 2023] [Koubek 1963] [Kozlov et al. 1996] [Kubicki et al. 2020] [Kukushkin and Ivanchenko 1993] [Kuznetsov 1993] [Kwak and Kiris 2010] [Kwon 2020] [LaBotz and Ewen 1982] [Lacefield and Sprow 1994] [Large Eddy Simulation 2023] [Laroche et al. 2000] [Latto 1967] [Lawhead and Combs 1963] [Lawrence 1945] [Lawrence 2005] [Lee 1963] [Lee 1964] [Lee and Roh 2013] [Lee et al. 2012] [Lee et al. 2017] [Leighton 1982] [Левихин and Musteikis 2025] [Levine 1965] [Levine and Baum 1982] [Li and Guo 2022] [Li et al. 2026d] [Li et al. 2026e] [Liang et al. 2022] [Life Prediction 1995] [Lim and George 1987] [Lim et al. 2025] [Limerick 1991] [Linear Acoustic Gains 1964] [Liquid propellant rocket engines] [Liquid Propellant Rocket Engines 2006a] [Liquid Propellant Rocket Engines 2006b] [Liquid Propellant Rocket Engines 2006f] [Liquid Propellant Rocket Engines 2006d] [Liquid Propellant Rocket Engines 2006e] [Liquid Propellant Rocket Engines 2006c] [Liquid Propellant Rocket-Engine Organizations 2006] [Liquid Rocket Engine Combustion 1974] [Anderson and Yang 1995] [Liquid Rocket Engine Fluid-Cooled 1972] [Liquid Rocket Engine Self-Cooled 1977] [Rezende 2018a] [Litchford 2005] [Litchford and Jeng 1992] [Liu and Qizhi 1996] [Liu and Zhang 2000] [Liu et al. 1995] [Liu et al. 1996] [Liu et al. 1998] [Liu et al. 2020b] [Liu et al. 2023d] [Liu et al. 2023c] [Liu et al. 2023b] [Liu et al. 2024e] [Long 2014] [Lorenzetto and Crocco 1971] [Lores and Zinn 1973] [Low Frequency Oscillations 2008] [Lu et al. 2024a] [Lux et al. 2008] [Lv et al. 2023a] [Lv et al. 2023b] [Lyon INC Detroit MI 1963] [López et al. 2014] [Muthaiah et al. 2023] [Macek and Semple 1972] [Maeding et al. 2011] [Maheskumar et al. 2021] [Mani et al. 2000] [Martin 1962] [Martin 2007] [marxman and Wooldridge 1969] [Masters 1968] [Masyagin 2026] [Matthews 1957] [Mayer and Kruelle 1992] [Mayer and Tamura 1996] [McAmis et al. 1991] [McAmis et al. 1992] [McCormack 1964] [Meisl 1988] [Merits of Liquid Propellant 2006] [МГТУ им. Н.Э. Баумана et al. 2013] [Meyer and Giuliani 1993] [Miao et al. 2024] [Micci 1997] [Michigan Univ Ann Arbor 1963] [Noel and Massier 1962] [Minato et al. 2012] [Mirzamoghadam 1991] [Mishina et al. 2020] [Mishra 2017a] [Mishra 2017b] [Mitchell 1967] [Mitchell 1968] [Mitchell 1969] [Mitchell 1993] [Mitchell and Neal 1969] [Mitchell et al. 1969] [Mkrtchyan and Kochetkov 2021] [Morgan 2015] [Morita et al. 2012] [Moruzzi et al. 2018] [Mueller et al. 1999] [Mukambetov and Borovik 2022] [Multifractal Detrended Fluctuation Analysis 2023] [Mungas et al. 2013] [Murphy and Voss 1996] [Muthaiah et al. 2025] [Müller et al. 2017] [Naraghi et al. 2001] [Naraghi et al. 2006b] [Naraghi et al. 2006a] [Narayanan 2014] [Rezende 2018b] [NASA Orbit Transfer Rocket 1984] [Naval Weapons Center China Lake CA 1963] [Naval Weapons Center China Lake CA 1964] [Navaneethan et al. 2024] [Negishi et al. 2015] [Nesbitt 1946] [Newell and Rajagopal 1993] [Nguyen and Sirignano 2018] [Nguyen and Sirignano 2019] [Nguyen et al. 2017] [Nguyen et al. 2018] [Nicholls 1969] [Nie and Liu 2011b] [Nie and Liu 2011a] [Nielsen 1966] [Niino et al. 1982] [Non-linear throttling analysis of 1999] [Nonlinear Effects in Instability 1964] [Novozhilov et al. 2018] [Numerical Method and Simulations 2016] [Numerical Simulation of High-Frequency 1996] [Nusca 2007] [Nusca 2008] [Nusca 2010] [Nusca and McQuaid] [Nusca and McQuaid 2004] [Nusca and McQuaid 2006] [Nusca et al. 2007] [Nusca et al. 2008] [Nusca et al. 2010] [Obrien 1989] [Ohashi 1968] [Omata et al. 2022] [Omori 1973b] [Omori et al. 1972] [Osborn and Davis 1961] [Osborn and Schiewe 1958] [Osherov and Natan 1999] [Otto and Flage 1960] [Pace and Massa 2026] [Pages and Achipa 2026] [Pakulak et al. 1982] [Palej and Palacz 2018] [Park and Jeon 2024] [Park et al. 2016a] [Parris and Landrum 2005] [Patel 2016a] [Patel 2016b] [Pauckert 1968] [Pauckert 1970] [Pauckert and Tobin 1975] [Pelevin and Ponomarev 2018] [Pelevin and Ponomarev 2021] [Pempie and Vernin 2001] [Penner and Datner 1955] [Perlmutter and DePierre 1965] [Peschka 1992] [Pharokhipanah and Bouckenooghe 2024] [Philipchuk 1953] [Plane 1963] [Plane 1964a] [Plane 1964c] [Plane 1964b] [PlEPER et al. 1967] [Popov and Sirignano 2015] [Popov et al. 2013] [Popov et al. 2014a] [Popov et al. 2014b] [Popov et al. 2015] [Popov et al. 2016] [Porter 1968] [Powell and Zinn 1970] [Powell and Zinn 1973] [Prakash et al. 2012] [Pressurization of Liquid Propellant 2019] [Price 1964] [Price 1965] [Price 1980] [Price 1981] [Price and Dehority 1967] [Price and Flandro 1987] [Princeton Univ Nj 1952] [Pritz and Schoner 1972] [Pritz and Schoner 1973] [Prokopenko 2026] [Pshenychka 2026] [Pustovyi 2026] [Pérez Roca] [Qi 1995] [Qi et al. 2022] [Qin et al. 2016] [Quentmeyer et al. 1978] [Quillin and Parry 1962] [Kala et al. 2027] [Fontaine et al. 1968] [Rahaim et al. 2000] [Rahn et al. 2019] [Rajagopal 2015] [Rajan and Narasimhan 2005] [Ramamurthi and Jayashree 1992] [Rapp 1993] [Reardon 1997] [Reardon et al. 1964] [Reis et al. 2019] [Ren et al. 2023] [Review of Experimental Research 1960] [Rezende 2021] [Rice et al. 1998] [Rice et al. 2010] [Ringas 2022] [Robbins et al. 1960] [Roberts 2023] [Robison 1953] [Rocker 1999] [Rocket Engine Nozzle Concepts 2004] [Rocketdyne Canoga Park Ca 1961] [Romero-Calvo et al. 2023] [Roncace 1991] [Rose 1958] [Rousar 1971] [Rudinskii and Yagodnikov 2021] [Ruth et al. 1990] [Ryu et al. 2005] [Sackheim et al. 2005] [Sakaki et al. 2018] [Sale 1964] [Sankar et al. 2017] [Santhini S Lal et al. 2015] [Santhosh and Kuzhiveli 2019] [Santiago 1996] [Santos and Ferrer 2024] [Sarotte] [Scala 1957] [Schmitt et al] [Scott 1963] [Seidel 1965] [Seidel 1974] [Senchev et al. 2022] [Seshime et al. 2026] [Sforza 2017] [Shadram et al. 2019] [Sheiko 2025] [Shelley et al. 2001] [Shoji 1981] [Shoyama and Hirakawa 2024] [Shoyama et al. 2024] [Siebenhaar and Campbell 1987] [Sierra et al. 2017] [Silver et al. 2024] [Sims et al. 2004] [Simulation and Analysis 2004a] [Simulation and Analysis 2004b] [Singelmann and Mueller 1948] [Sirignano and Krieg 2016] [Sirignano and Popov 2013] [Smallwood 1966] [Smallwood 1967] [Smith 1964] [Smith et al. 1987] [Sohn et al. 2004] [Solid Rocket Combustion Instability-An 1992] [Son et al. 2023] [Song et al. 2021] [Song et al. 2026a] [Sozen et al. 2008] [Space Shuttle Orbit Maneuvering 1972] [Space Storable Regenerative Cooling 1971] [Spalding 1979] [Srinivasan et al. 2021] [Stability Testing Methodology 1995] [Stanley 1969] [Stanley 1970] [Stanley 1971] [Stechman 1993] [Stechman and Drenning 1981] [Strahle 1970b] [Strahle 1970a] [Strauss 1964] [Stuber et al. 2012] [Studhalter 1964] [Summerfield 1951a] [Summerfield 1951b] [Summerfield 1960] [Summerfield and Krier 1968] [Sun et al. 2022] [Sung and Choi 2026] [Sung et al. 2025] [Suraweera et al. 2005] [Sutton 1968] [Sutton 1970] [Sutton 2006] [Taghavi et al. 2019] [Tajima 1965] [Takeda et al. 2022] [Talley 2002] [Tang et al. 2026] [Tao et al. 2006] [Tellier 1964] [Thapa 2023] [The thermal rocket engine] [Thornburg 2002] [Thynell et al. 2014] [Tischler and Humphrey 1956] [Tishkoff et al. 1989] [Tiwari et al. 2005] [Tomazic 1955] [Torres et al. 2009] [Traudt 2024] [Tsai et al. 1999] [Tucker et al. 1993] [Tucker et al. 2015a] [Tucker et al. 2015b] [Ulas and Boysan 2013] [Umholtz 1999] [Urbano et al. 2016] [Vadera 2019] [Vaganov and Kazakov 2019] [Valler 1979] [Venkateswaran and Merkle 1996] [Venkateswaran et al. 1991] [Ventrice et al. 1979b] [Ventrice et al. 1979a] [Veres 1992] [Vetter 1977] [Viventi 1961] [Von Eckartsberg et al. 2025] [Wadel and Wadel 1997] [Wadia and Wilson 1981] [Waesche and Summerfield 1965] [Wagner and Shoji 1975] [Wagner and Waldman 1973] [Wang 2008] [Wang 2015a] [Wang 2016] [Wang et al. 2006b] [Wang et al. 2013b] [Welsh 1985] [Welton et al. 1963] [Wenyuan et al. 2025] [Wiegand 1961] [Wieseneck 1970] [Williams 1968] [Williams 2004b] [Williams 2004a] [Wong 1979] [Wong and Brown 1965] [Wong and Brown 1968] [Woodward and Summerfield 1966] [Wozney 2021] [Wu et al. 2003] [Wu et al. 2026b] [Wunderlin et al. 2024] [Xiang et al. 2020b] [Xiaofeng et al. 2011] [Xie et al. 2026] [Xiong 2018] [Xiong et al. 2020a] [Xiong et al. 2020b] [Xu et al. 2006] [Yang 2004] [Yang and Sun 2013] [Yang et al. 2009] [Yang et al. 2024] [Yang et al. 2025a] [Yin et al. 2024] [Yoon and Moon 2026] [Yoon et al. 1994] [Yu et al. 2016] [Yu et al. 2025b] [Yuan et al. 2005] [Yuhui and Zhenguo 2002] [Zhan et al. 2024] [Zhang 1984] [Zhang 2016] [Zhang 2026] [Zhang and Li 2017] [Zhang et al. 2007] [Zhang et al. 2012b] [Zhang et al. 2026b] [Zhao et al. 2024b] [Zhou et al. 2021] [Zhou et al. 2023b] [Zhou et al. 2026a] [Zhu et al. 2025b] [Zhu et al. 2026b] [Zhuang et al. 1998] [Zhuang et al. 1999] [Zinn 1966b] [Zinn 1966a] [Zinn 1968] [Zinn and Powell 1971] [Zinn and Savell 1969] [Zinn et al. 1974] [Zook 2024] [Zucrow 1947]

Radar tracking, glint and scintillation

The tracker and the errors the beamwidth calculation leaves out. Monopulse and conical-scan angle measurement, glint and scintillation, low-angle tracking and multipath, seekers, the jamming of trackers, and the filters that turn measurements into tracks. 164 of these titles name monopulse. Glint is not a closed subject. 85 titles name it, and 40 of the 74 dated ones are from 2010 or later, which agrees with the statement above that glint remains a live subject.

630 records. [Jay et al. 2024] [Acree and Maier] [Active Radar Missile Seekers 2012] [Adrian 2007] [Aldrich and Krabill 1972] [Aldrich and Krabill 1973] [Alfred et al. 2007] [Alhadhrami] [Alsaka et al. 1993] [Amrouche et al. 2017] [An and Lee 2020] [An et al. 2024] [Ananthasayanam and Sarkar 2005] [Andrews et al. 2018] [Andrews et al. 2020] [Arthur et al. 1961] [Asadsangabi et al. 2024] [Askar et al. 2018] [Asseo 1981] [Asthana and Prahlad 1989] [Asthana and Prahlada 1994] [Baker 2006] [Baker and Zyweck 2010] [Balaji et al. 2009] [Banani and Imam 2011] [Bang 2026] [Barton 1961] [Barton 1974] [Belcher] [Bell et al. 2014a] [Bell et al. 2014b] [Bell et al. 2015] [Benavoli et al. 2007] [Berger 1971] [Berger 1972] [Bergkvist and Tullsson] [Berry et al. 2017] [Bhattacharyya and Bhattacharjee 2002] [Bilik and Tabrikian] [Blair and Brandt-Pearce 1996] [Bo Liu and Wenge Chang 2013] [Bodnar 1977] [Bole et al. 2014] [Bolen 1994] [Bonney 1960] [Borden 1993] [Borden and Mumford 1983] [Bosarge 1966] [Boylan et al. 1978] [Brandenburg 1956] [Brennan 1961] [Brockner 1951] [Broden 1997] [Brooker] [Buford and Dunavant 1996] [Buford and Mobley 1994] [Burrows 2008] [Bużantowicz and Walenczykowska 2025] [Byaloshitsky 2024] [Cabib et al. 2009] [Cai 2025] [Cai et al. 2018] [Camplani et al] [Can Rao et al. 2011] [Candler and Leyva 2022] [Cao et al. 2019] [Cao Yuan et al. 2011] [Cen et al. 2025] [Chai et al. 2012] [Chang et al] [Chao et al. 2008] [Chaumette and Larzabal 2007] [Chen and Huang 1996b] [Chen and Huang 1996a] [Chen and Huang 1999] [Chen and Lian 1995] [Chen and Sheng 2010] [Gong et al. 2014] [Chen et al. 2016a] [Chen et al. 2017b] [Chen et al. 2022b] [Chen et al. 2023a] [Chen et al. 2025c] [Chen et al. 2025d] [Chen et al. 2026b] [Chen et al. 2026e] [Chen et al. 2026d] [Chen Guoying and Huang Peikang] [Chen Jianwen et al. 2006] [Cheng and Cao 2023] [Cheng et al. 2013] [Chengzeng et al. 2025] [Cho et al. 2012] [Chong and Scharf 2006] [Chow 1996] [Christiansen and Smith 2019] [Chrysler Corp Detroit Mi Missile Div 1963] [Chunpeng et al. 2022] [Clark] [Coate 2004] [Coate and Arakawa 2004] [Cooper and James 1979] [Cormack et al. 2017] [Cottrill 1992] [Cui et al. 2015] [D’Amato and Bernstein 2012] [Daeipour and Bar-Shalom] [Dai et al. 2021] [Damini et al. 2008] [Damonte and Stoddard] [Dana 2022] [De et al. 2020] [De Maio et al. 2017] [de Moura Magalhães] [Dedic et al. 2024] [Delano 1953] [Delano and Pfeffer 1956] [Deng et al. 2021] [Develet 1961] [Devi 2021] [Dickson 1986] [Jin et al. 2014] [Dmitriev et al. 2024] [Doan et al. 1995] [Doso et al. 2023] [Dou et al. 2024] [Drake 1967] [Drexler 2006] [Duan and Wang 2024] [Dumper 1997] [Dungate 1999] [Dunlop 1981] [Dunn and Howard 1959] [Dunn et al. 1959] [Durantini et al. 2017] [Englisch and Endemann 1984] [Esten 1953] [Evans] [Evans 1966] [Fan et al. 2013] [Farina et al. 2000] [Farrell 1985] [Fedele et al. 1985] [Feldman et al. 1962] [Feng Xiaobin et al] [Fluhr 1963] [Fowdur] [Fowdur et al. 2025] [Frazer and Williams 2019] [Fu et al. 2021] [Fukushima et al. 2017] [Galy et al. 2010] [Gao and Tie 2017] [Gao et al. 2018] [Gao Sun et al. 2011] [Gates and Schy 1952] [Genova 2005] [Ghosh 1991] [Gibbons and Botha 2015] [Gigleux et al. 2024] [Giuli and Tiberio 1975] [Glass and Blair 2015] [Godrich et al. 2010] [Goertzen 1972] [Gogineni and Nehorai 2010] [Gongjian Zhou et al. 2012] [Goodarzi et al. 2020] [Goodman 1965] [Gour et al. 2015] [Gray 1997] [Griesser and Balanis 1987] [Ground Target Tracking 2004a] [Ground Target Tracking 2004b] [Gruner et al. 2017] [Gruner et al. 2019] [Gu 2002] [Gu et al. 2025] [Guesalaga 1988] [Guesalaga and Tepper 1999] [Guesalaga and Tepper 2000] [Guest] [Gulko and Mescheryakov 2026] [Guo et al. 2018a] [Guo Ying and Wang Bu-hong] [Guodong and Chonglun 2013] [Guoying Chen et al] [Gupta and Fickenscher 2013] [Gökdemir et al. 2026] [Han et al. 2016a] [Hao et al. 2015] [Harbater and Margalit 2000] [Harmuth 1978] [Haykin] [Haykin and Reilly 1982] [Haykin et al. 1980] [Haykin et al. 2010] [He 2015] [He and Guo 2012] [He et al. 2024b] [Headrick et al. 1966] [Headrick et al. 1967] [Hei et al. 2023] [Henareh and Norouzi 2016] [Hender and Okabe 1983] [Ho et al. 2017] [Hokanson 2026] [Hollister and Vernturino 1978] [Hong Cheng Yin and Pei Rang Huang 2008] [Hong et al. 2019a] [Hong et al. 2019b] [Hongcheng Yin and Peikang Huang 1995] [Hongwei Li and Jun Wang 2011] [Hossein and Amindavar 2012] [Howard 1980] [Howard and Lewis 1955] [Howard et al. 2023] [Hu and Li 2019] [Hu et al. 2019] [Hu et al. 2024b] [Hua Lan et al. 2017] [Huang 1990] [Huang et al. 2013] [Huang et al. 2017b] [Huang et al. 2019] [Hughes and Leyland 1998] [Huiyuan Zhang et al. 2016] [Hultgren and Hallman 1947] [Hung and Morris] [Ijaz and Bhatti 2019] [Indiresan 1965] [殷 et al. 2014] [Jain] [Jeffrey] [Jen King Jao] [Jensen 1999] [Jianbin et al. 2006] [Jiang 2015] [Jiang 2021] [Jiang and Yu 2009] [Jiang et al. 2019] [Jiang et al. 2022b] [Jie et al. 2006b] [Jin Ming et al. 2003] [Jo and Ahn 2017] [Johann et al. 1991] [Johnson et al. 2015] [Jun et al. 2013] [Jun-jie et al. 2016] [Junji Chen et al. 2008] [Junkun et al. 2016] [Kachelmyer 1990] [Kaczmarek and Serafin 2019] [Kai-Bor Yu 2015] [Kai-Bor Yu and Murrow] [Kai-Bor Yu and Murrow] [Kalata 1984] [Kam] [Kanter 1979] [Kanter and Boothe 1978] [Keche et al. 1997] [Kemp and Corey] [Kim 2014] [Kim et al. 2010a] [Kim et al. 2010b] [Kim et al. 2022] [Kintz 2019] [Kleinman 1981] [Klinefelter et al. 2022] [Koch and Klemm 2001] [Kong et al. 2024] [Kostis et al. 2008] [Kostis et al. 2009] [Kriel and le Roux 2016] [Krishna Paik et al. 2014] [Kucuk et al. 2024] [Kumar and Kumar 2022] [Kumar and Mondal 2023] [Kyriakides 2019] [Lainiotis et al] [Lambert et al. 2009] [Lane 1967] [LanFeng et al. 2010] [LaPlant 1952] [Lawton et al. 1997] [Lebak 2002] [Lee and Zoltowski] [Lee et al. 2015b] [Lee et al. 2016] [Lee et al. 2018a] [Lenhard et al. 1963] [Levitas et al. 2016] [Li and Wang 2012] [Li and Zhao 2025] [Li Baoguo et al] [Li et al. 2013b] [Li et al. 2014c] [Li et al. 2015f] [Li et al. 2016a] [Li et al. 2017a] [Li et al. 2019e] [Li et al. 2019c] [Li et al. 2019b] [Li et al. 2020b] [Li et al. 2020c] [Li et al. 2021d] [Li et al. 2022a] [Li et al. 2023c] [Li et al. 2024d] [Li Nan and Qu Changwen 2007] [Li-hua et al. 2006] [Lin et al. 2018] [Lindsay 1968] [Litva et al] [Liu and Mo 2018] [Liu and Wang 2022] [Liu et al. 2013c] [Liu et al. 2014] [Liu et al. 2024b] [Liu et al. 2024d] [Liu et al. 2025a] [Liu Zhenyu 2003] [Lizhong Song et al] [Lo and Litva] [Lo et al. 1991] [Loomis and Graf 1974] [Low Angle Tracking 2017] [Luan et al. 2026] [Lubnau 1977] [Lutz et al. 2015] [Lv et al. 2026] [Ma Zhen-qiu and Cui Wei 2009] [Mahafza et al] [Malatji and du Plessis 2017] [Mangulis 1981] [Manuilov et al. 2007] [Maresca et al. 2008] [Markin 2011] [Marolleau et al. 2024] [McDonald et al. 1985] [McLntyre et al. 1979] [Melino 1987] [Meller 2017b] [Meller 2017a] [Meng et al. 2021] [Merritt and Gocal 1979] [Miao Sui and Xiaojian Xu 2011] [Miller 1952] [Ming Jin et al] [Mingyi et al. 2007] [Mir and Wilkinson 2008] [Missile Defense Radar Design 2009] [Mitchell et al. 2017] [Mobley 1994] [Mobley et al. 1995] [Moiseev 2022] [Mokole 1991] [Monakov 1990] [Monopulse Direction Estimation 2001] [Monopulse Direction Estimation 2013] [Moon] [Moon 2002b] [Mosca 1969] [Mrstik and Smith 1978] [Mu et al. 2012] [Mularzuk 2018] [Nadjiasngar and Charlish 2015] [Nan et al. 2010] [Narykov et al. 2014] [Neelakantaswamy and Rajaratram 1982] [Nester 1962] [Nicholls 1975] [Nicholls 1982] [Nickel] [Nickel] [Nickel 1993] [Nickel 2006] [Nickel et al. 2011] [Nie et al. 2014] [Nielsen 2001] [Niu et al. 2020] [O’Connor 2019] [Oderland et al] [Okano 2015] [Opitz 2006] [Ostrovityanov 1990] [Otsubo and Honda 2023] [Paine 2023] [Park et al. 2026a] [Patterson and Ashley 2000] [Peebles 1969] [Peebles 1985] [Peebles and Sakamoto 1980] [Peebles and Sskamoto 1980] [Peebles and Wang 1982] [Pehlivan and Yegin 2021] [Peled-Eitan and Rusnak 2019] [Peng et al. 2018] [Persico et al. 2017] [Philco Corp Palo Alto Ca 1963] [Pinto et al. 2023] [Powell] [Practical Issues for Radar 1998] [Qiao Yongjie et al. 2011b] [Qiao Yongjie et al. 2011a] [Qin and Cheng 2012] [Qingzhan Shi et al. 2016] [Qu et al. 1999] [Radar Angle-of-Arrival Estimation 2013] [Radar Measurements and Target] [Radar Resource Management 2014] [Radar Target Tracking Algorithm 2021] [Radar Tracking Algorithms 2010] [Ramakrishnan and Sarkar 2006] [Rao et al. 1993] [Rao et al. 2017] [Rebeiz 2000] [Reilly and Haykin 1982] [Reilly et al. 1988] [Ren et al. 2021] [Resnick 1966] [Rezaei et al. 2023] [Rickard 1963] [Robillard and Blore 1964] [Robins 1953] [Rogers] [Ross and Bechtel 1968] [Rutkowski et al. 2015] [Sachuk et al. 2020] [Saeedi 2020] [Sahingil 2019] [Sahoo et al. 2021] [Sahu and Das 2011] [Sakarya and Bayram 2019] [Sakarya and Sari 2019] [Sankar et al. 2013] [Sankowski et al. 2006] [Saratayon et al. 2015] [Sarunic] [Savci et al. 2021] [Schmitt 2001] [Schuck et al. 2020] [Seifer 1992] [Seifer 1994] [Seliktar et al] [Semenov et al. 2019] [Sen and Nehorai 2009b] [Sen and Nehorai 2009a] [Shan and Zhou 2021] [Shang She and Xu Yinghe] [Shang She et al] [Sharenson 1962] [Sheng-bing et al. 2016] [Shepherd 1963] [Shi et al. 2007] [Shi et al. 2016] [Shi et al. 2019a] [Shi et al. 2019b] [Shi et al. 2019c] [Shi et al. 2020] [Shi et al. 2021a] [Shi et al. 2025b] [Shi et al. 2026] [Shi-Wei Gao and Zheng Bao 1992] [Shu et al. 2015] [Sims and Graf 1969] [Sims and Graf 1971] [Siting et al. 2019] [Song et al. 2016] [Soumekh 1997] [Sozinov and Горевич 2021] [Spong] [Story et al. 2026] [Su et al. 2013] [Su et al. 2026] [Sui and Xu 2010] [Sui and Xu 2012] [Sui and Xu 2014] [Sun 1979] [Sung-Hoon Moon et al] [Sung-Hoon Moon et al] [Swerling 1956] [Szullo and Seller 2016] [SŁOwak 2025] [Ta-Sung Lee and Tser-Ya Dai 1994] [Taek Lyul Song and Dong Gwan Lee 2000] [Tafertshofer et al. 2024b] [Tafertshofer et al. 2024a] [Taha and Hudson 1986] [Takahashi et al. 2012] [Takahashi et al. 2018] [Tan et al. 2007] [Tan et al. 2024] [Tao et al. 2023] [Tao et al. 2024] [Tao Guo et al. 2010] [Theoretical Accuracy of Monopulse 1966] [Thiet 2025] [Thompson and Pappas 1973] [Thompson et al. 1974] [Thorat et al. 2023] [Thornton et al. 2022] [Tian et al. 2025] [Tiszauer 1989] [Tofani 1989] [Tomczak 1976] [Tracking Radar 1999] [Tracy and Wright 2023] [Tuyen 2025] [Tuzlukov 2026f] [Tuzlukov 2026c] [Tuzlukov 2026d] [Tuzlukov 2026j] [Tuzlukov 2026g] [Tuzlukov 2026e] [Tuzlukov 2026h] [Tuzlukov 2026i] [Vashkevich and Fedorov 2003] [Vickers and López 1975] [Walton 1995] [Wang et al. 2013a] [Wang et al. 2016b] [Wang et al. 2016a] [Wang et al. 2018b] [Wang et al. 2018d] [Wang et al. 2018c] [Wang et al. 2019e] [Wang et al. 2019d] [Wang et al. 2019a] [Wang et al. 2021e] [Wang et al. 2022b] [Wang et al. 2022i] [Wang et al. 2025c] [Wang et al. 2025a] [Wang Jun et al. 2009] [Wasilewski et al. 2025] [Wei et al. 2012] [Wei Liu et al] [Wei Wang et al. 2011] [Wei Yan and Zhaoda Zhu] [Wei-dong et al. 2009] [Wen et al. 2017] [Weng-Rong Wu 1993] [White 1974] [Widgery 2017] [Wilkin et al. 1991] [Williams and Boykin 1979] [Winton 2021] [Wong et al. 1993] [Worms] [Wright 1984] [Wu et al. 2024b] [Wu et al. 2025c] [Wu et al. 2026a] [Wu Qiongzhi 2002] [Wu Qiongzhi et al] [Wu Qiongzhi et al] [Xia and Xu 2007] [Xiao et al. 2015] [Xiaowen et al. 2025] [Xie and Xiong 2006] [Xie et al. 2010] [Xie et al. 2016a] [Xie et al. 2016b] [Xin Guo et al. 2008] [Xing et al. 2023] [Xiong and Xie 2022] [Xu and Wang 2019] [Xu et al. 2021] [Xue et al. 2019a] [Xueting Li et al. 2015] [Yang et al. 2018a] [Yang et al. 2019b] [Yang et al. 2020b] [Yi et al. 2016] [Yi et al. 2025] [Yifei et al. 2019] [Yinghua Han et al. 2009] [Yoganandam and Jitendra Das 1991] [Yong-An Zhang et al] [Yu] [Yu 1994] [Yu 2017] [Yu and Fernández 2025] [Yu WeiHua et al. 2009] [Yuan et al. 2024] [Yuan He et al. 2011] [Yueyi et al. 2007] [Yun-li Du et al. 2010] [zamani et al 2017] [Zarifi et al. 2025] [Zeng et al. 2017] [Zengliang Li et al. 2015] [Zewge and Bang 2022] [Zhai 2018] [Zhan et al. 2025b] [Zhan et al. 2026] [Zhang and Miao 2012] [Zhang et al. 2006a] [Zhang et al. 2009a] [Zhang et al. 2016b] [Zhang et al. 2017e] [Zhang et al. 2017b] [Zhang et al. 2017a] [Zhang et al. 2019a] [Zhang et al. 2019c] [Zhang et al. 2022c] [Zhang et al. 2022a] [Zhang et al. 2023c] [Zhang et al. 2024a] [Zhang et al. 2026c] [Zhang et al. 2026a] [Zhang Xiushe] [Zhao et al. 2020] [Zhao et al. 2021a] [Zhao YiNan et al] [Zhaohui et al. 2014] [Zhe et al. 2016] [Zhen Wang et al. 2004] [Zheng Lu et al. 2013] [Zheng Shouduo et al. 2015] [Zhengyan and Jianyun 2017] [Zhenyu Liu Zhimei Zhou and Yueqiu Han] [Zhou and He 2011] [Zhou and Huang 2023] [Zhou and Wu 2026] [Zhou et al. 2010b] [Zhou et al. 2019a] [Zhu et al. 2018a] [Zwagerman] [Úbeda Medina]

Missile airframe aerodynamics, canard and cruciform

The canard cruciform family and the missile airframe at large. Canard and tail control, cruciform wings and fins, induced roll and roll control, hinge moments, slender-body theory and the prediction of supersonic missile aerodynamics. The cruciform is a period word. 53 titles name it, with a median year of 1973, and one is dated 2010 or later, while the canard continues in 175 titles, 35 of them from 2010 or later.

621 records. [Abbas et al. 1992] [Abdelhamid 1985] [Abney and McDaniel 2005] [Adams 1951] [Adams and Duane 1952] [Adams and Rubin 1958] [Advanced Fuel Research INC East Hartford CT 1957] [Advanced Missile Models 1969] [Aerodynamic Hinge Moments 1991] [Aerodynamics of Arbitrary Wing 1976] [Agnone 1984] [Agrell and Elmeland 1984] [Akishita et al. 1984] [Akishita et al. 1986] [Aksu 2014] [Alhussan 2007] [Alksne 1957] [Allen 1981] [Allen and Blair 1982] [Allen and Dillenius 1979] [Allen and Pittman 1983] [Allen and Watson 1994] [Allen et al. 1978] [Allen et al. 2026] [Alviani et al. 2022] [Anderson 1961] [Anderson 1979b] [Anderson 1986] [Anderson 1987] [Anderson and Feistel 1985] [Androsenkov et al. 2007] [Application of Slender-Body Theory 2025] [Arbic and Gillespie 1952] [Arbic and Gillespie 1953] [Army War Coll Carlisle Barracks Pa 1952] [Arrow and Yost 1976] [Aswathi and Asok Kumar 2018] [Auman and Kreeger 1998] [Auman et al. 1994] [Azarova 2022] [Baber and Moul 1955] [Baldwin and Hanking 1980] [Bandyopadhyay 1989] [Bannink and Reyn 1968] [Barber and Lundstrom 1956] [Bass et al. 1993] [Bass et al. 1995] [Bayoğlu et al. 2016] [Belaidouni et al. 2017] [Belousov et al. 1990] [Benton 1964] [Bera 1975] [Bernot and Robinson 1958] [Bhowmick et al. 2025] [Bhutta and Lewis 1992] [Binion and Herron 1962] [Birch and Cleminson 2004] [Birch and Petterson 2004] [Birch et al. 2000b] [Birch et al. 2000a] [Bittle et al. 1998] [Blades et al. 2002] [Blair 1977] [Blair 1978b] [Blair 1978c] [Blair 1978a] [Blair 1990a] [Blair 1990b] [Blair and Rapp 1980] [Blair et al. 1978] [Blair et al. 1983] [Blair et al. 1992] [Blair et al. 1993] [Blake 1989] [Blake and Blake 1997] [Blake and Gillard] [Blake and Karni 2005] [Blake and Simon 1998] [Boatright 1952] [Bogatyrev 2017] [Boissevain 1954] [Bolz and Nicolaides 1950] [Bond and Swanson 1953] [Bowcutt et al. 1999] [Boyd 1965] [Boyd and Menees 1959] [Briggs 1986] [Bright and Peterson 1960] [Brooks 1970] [Brooks and Cone 1966] [Brown 1957] [Brown 1987] [Brown and Lundstrom 1952] [Brown and Parker 1945] [Bryson 2021] [Bryson 2022] [Buell and Tinling 1959] [Burchett et al. 2021] [Burchett et al. 2022] [Burkhalter 1996] [Buzantowicz 2019] [Byars et al. 1980] [Cao and Lyu 2024] [Cao et al. 2025b] [Capel-Jorquera et al. 2025] [Capone et al. 1996] [Chambers and Yip 1984] [Chambers et al. 1984] [Chandrasekharan et al. 2015] [Chang 1962] [Chaudhari et al. 2026] [Chen 2022] [Chen and Liu 2014] [Chen et al. 1991] [Chen et al. 2002] [Chen et al. 2008b] [Chen et al. 2017a] [Chen et al. 2020g] [Chubb 1952] [Clark and Hodapp 1970] [Clark et al. 1972] [Clark et al. 2017] [Clarke and Sinai 1977] [Coirier et al. 2014] [Curfman and Grigsby 1952] [Daniels and Hardy 1975] [Daniels and Hardy 1976] [Daniels and Hardy 1978] [Darvekar and Kanney 2016] [Davis 1984] [Deep et al. 1971] [Denegri et al. 2013] [DeSpirito and Sahu 2001] [DeSpirito et al. 2002] [DeSpirito et al. 2003b] [DeSpirito et al. 2003a] [Devan 1987] [Diggins 1951] [Dillenius 1986] [Dillenius and Nielsen 1979] [Dillenius et al. 1982] [Dillenius et al. 1992a] [Dillenius et al. 1992b] [Dillenius et al. 2002] [Dong et al. 2023c] [Dow and Sarver 1972] [Doyle and Rosema 2015] [Driver 1958] [Driver 1960] [Driver and Hamilton 1956] [Dryer and Beke 1952] [Dubben and Denegri 2007] [Duffy 1989] [Duncan 1950] [Durston and Schreiner 1983] [Eastman 1983] [Ghosh et al. 2023] [Han et al. 2023] [Hartman and Johnston 1987] [Edwards and Hikido 1953] [Eggers 1965] [Ehlers 1961] [Eidell et al. 2012] [Ekaterinaris 1994] [El mahdi et al 2017] [El-Mahdy et al. 2016] [Eminton and Lord 1956] [Er-El 1983] [Ericsson 1980] [ESDU Data Item Estimates 1998] [Eugene 1996] [Fano et al. 2020] [Farahmandi and Reitz 2024] [Fawcett et al. 1992] [Fedorov et al. 2007] [Feng et al. 2010] [Fikes 1977] [Fink 1966] [Fink and Anderson 1982] [Fitzgerald 1988] [Fitzgerald 1990] [Flaherty 1977] [Follé 1998] [Foster 1959a] [Foster 1959b] [Foster and Robinson 1961] [Fournier 1961] [Fradenburgh and Campbell 1953] [Fradenburgh and Kremzier 1953] [Fraenkel 1958] [Fresconi et al. 2017] [Fresconi et al. 2018] [Frick 1948] [Fricker 1996] [Gad-El-Hak and Ho 1986] [Gaiddon et al. 2003] [Gainer 1961] [Gajera 2026] [Gammal and Kennedy 1954] [Gaonkar et al. 2019] [Gates et al. 1989] [Geer 1980] [Gillespie 1956] [Gillespie and Arbic 1951] [Giragosian 1982] [Gnemmi et al. 2008] [Gold and Busan 1994] [Goldberg 1967a] [Goldberg 1967b] [Gordon 1990] [Graham 1950] [Grashof 1983] [Graves 1972] [Graves and Fournier 1974] [Graves and Robins 1980] [Gregoire 1983] [Gregoire and Krieger 1980] [Gregoriou 1989] [Griffin and Jonas 1983] [Grigsby 1952a] [Grigsby 1952b] [Grigsby 1954] [Grismer et al. 2000] [Gross et al. 1986] [Guan 2014a] [Guan 2014b] [Gur et al. 1978] [Gur et al. 1979] [Guy et al. 1999] [Guy et al. 2000] [Hall 1952a] [Hall 1952b] [Hall 2002] [Hall 2004] [Hall and Sandahl 1951] [Hanin 1983] [Hanson 1963] [Hanson et al. 1966] [Hardy 1978] [Harris 1935] [Hazelton et al. 1996] [Heiser and Burkhalter 2002] [Hemsch 1985] [Hemsch and Nielsen 1982] [Hemsch and Nielsen 1983] [Hemsch and Nielsen 1986] [Hemsch et al. 1977] [Henning 1959] [Hess and Smith 1967] [Hessman 1979] [Hessman 1982] [Holley et al. 1996] [Honkanen et al. 2011] [Hood et al. 1980] [Horton and Landrum 2006] [Howard and Kersh 1991] [Howard and O’Leary 1993] [Howard et al. 1989] [Howerton and Hathaway 1994] [Huang et al. 2002] [Hughson and Luke 2008] [Hunt 1960] [Hutt and Howe 1988] [Hwang et al. 1991] [Hypersonic Aerodynamics Slender Bodies 2025] [Inger 1991] [Innocenti and Thukral 1993] [Irfan et al. 2026] [Jabbar et al. 2026] [Jack and Burgess 1951] [Jarrett 1971] [Jasher 2012] [Jenke 1976] [Jenn and Nelson 1988b] [Jenn and Nelson 1988a] [Jernell 1970] [Jernell 1974] [Allen 2005] [Jin and Ma 2011] [Jones 1959a] [Jones and Margolis 1946] [Ooi 2024] [Jung 2003] [Kada 2015a] [Karahan and Kaynak 2026] [Kassner and Wettlaufer 1977a] [Kassner and Wettlaufer 1977b] [Kassner and Wettlaufer 1977c] [Kassner and Wettlaufer 1977d] [Katz and Levin 1986] [Kawamura and Karashima 1957] [Keith and Selberg 1984] [Kim and Kang 2025] [Kim et al. 2004a] [Kimmel and Oh 1988] [Klenke and Hemsch 1980] [Klopfer 1985] [Korst and Deep 1979] [Kremzier and Davids 1952] [Krieger 1982b] [Krieger 1982a] [Krieger and Williams 1981] [Krieger and Williams 1983] [Krieger et al. 1980] [Kumar et al. 2021] [Kumar et al. 2025] [Lamb and Trescot 1980] [Lamb et al. 1979b] [Lamb et al. 1979a] [Landers et al. 1997] [Landers et al. 2000] [Landers et al. 2003] [Lauchle 1974] [Lee 2023] [Lesage et al. 2000] [Lesieutre 2017] [Lesieutre et al. 1987] [Lesieutre et al. 1996] [Li 2014] [Li et al. 2023d] [Li et al. 2025f] [Lift/Drag Ratios of Optimised 1962] [Lighthill 1956] [Lijewski 1987] [Lin et al. 1995] [Lindsay and Jordan 1975] [Logan et al. 2006] [Longo and Das 1990] [Lord and Eminton 1954] [Lowrie 1960a] [Lu and Zhang 2022] [Lu et al. 2024b] [Lundstrom and Whitman 1959] [Lunev 1960] [Luo 2014] [Luo et al. 2013] [Luo et al. 2020b] [Ma and Jin 2011] [Ma et al. 2005] [Mahire et al. 2026] [Mahmud and Bowersox 2001] [Mahmud and Bowersox 2003] [Malfa et al. 1991] [Malmuth and Shalaev 2004] [Margolis et al. 1958] [Mason 1982] [Matthews and Schmidt 1955] [McDaniel et al. 2010] [McGrath 2004] [Mead 1953] [Meakin and Nygaard 2003] [Mendenhall 1992] [Menees and Boyd 1959] [Mesalles Ripoll et al. 2021] [Meyer 1992] [Miele and Hull 1963] [Miles 1952] [Miles 1956] [Miller 1987] [Miller et al. 2016] [Min et al. 2003] [Moore 1974] [Moore 1993] [Moore and Jenn 1990] [Moore et al. 1993] [Moore et al. 1994] [Moran and Beran 1995] [Morote 2009] [Moul and Wineman 1952] [Mracek and Ridgely 2006] [Mulder et al. 2009] [Muppidi et al. 2018] [Murman and Aftosmis 2003] [Murman et al. 2002] [Murphy 1970] [Murphy 1971] [Nason et al. 1955] [Nelson 1988a] [Nelson 1991] [Nelson and Passera 1950] [Neumeier and Hanin 1986] [New Applications of Engineering 1994] [Nguyen et al. 2026] [Nicholas et al. 1984] [Nielsen 1978] [Nielsen 1979] [Nielsen 1982] [Nielsen 1988a] [Nielsen 1988b] [Nielsen 1989] [Nielsen et al. 1984] [Nietubicz 1975] [Niewald and Moul 1950] [Nikolic and Jumper 2004] [Noetscher et al. 2019] [Nonaka et al. 2022] [Numerical and Experimental Determination 2019] [Numerical Investigation of Impinging 2025] [Numerical Study on Rolling 2014] [Nurohman et al. 2018] [Nygaard and Meakin 2002] [Obery and Krasnow 1952] [Ognjanovic et al. 2017] [Oh 1989] [Ohrenberger and Baum 1972] [Ostrander et al. 1995] [Ozcatalbas et al. 2020] [Ożóg et al. 2020] [Packard and Miller 2000] [Pagan and Molton 1991] [Panayotov et al. 2017] [Pandya and Aftosmis 2001] [Pankkonen 2011] [Panneerselvam et al. 1996] [Park and Abla 1982] [Park and Abla 1983] [Park and Chung 2012] [Park et al. 2013] [Parks 1962] [Patel et al. 2003b] [Pavlenko and Pigusov 2018] [Pavlenko and Reslan 2022] [Peng 2011] [Pepitone and Jacobson 1977] [Pepitone and Jacobson 1978] [Peterson 1961] [Pfaff 1968] [Pfeiffer 1988b] [Pfeiffer 1988a] [Platzer 2010] [Platzer and Hoffman 1966] [Pourtakdoust and Lan 1990] [Prasad et al. 2021] [Priolo and Wardlaw 1988] [Priolo et al. 1985] [Pritchard 1969] [Prizirembel and Wen 1978] [Purwadi et al. 2023] [Quam 1978] [Rainey 1951] [Rathakrishnan 2025] [Rašuo et al. 2021] [Ribner 1951] [Riou et al. 2009] [rish.M et al 2018] [Robinson 1958] [Robinson 1970] [Rom et al. 1989] [Root 1945] [Rosema 2015] [Rosema and Doyle 2011] [Rosema et al. 2007] [Rosema et al. 2009] [Ruhlin and Tuovila 1961] [Hopko 1951] [Sahu 1985] [Sahu and Fresconi 2017] [Sahu and Fresconi 2018] [Sahu and Fresconi 2019] [Sahu and Heavey 2009] [Sahu and Heavey 2010] [Sahu et al. 2000] [Sailaranta et al. 2011] [Satran 1986] [Sawyer and Hayes 1976] [Sawyer and Jackson 1982] [Schadt 1968] [Scherrer and Dennis 1951] [Schindel and Lam 1995] [Schmidt et al. 2014] [Schwind 1978] [Seaberg 1954] [Seaberg 1957] [Sebastia and Hornung 2023] [Sebastia et al. 2024] [Sekaran 1983] [Selberg and Rokhsaz 1985] [Serakos] [Sevier et al. 1953] [Sforza 2020] [Shah and Ahmed 2023] [Shah et al. 2010] [Shantz 1953] [Sheng et al. 2008] [Shewale et al. 2022] [Shistik and Sigal 2002] [Shrivastava and Mohite 2015] [Shumway and Boranian 2025] [Sieradzki 2016] [Silton and Coyle 2015] [Silton and Coyle 2016] [Simon and Blake 1999] [Sinai and Clarke 1978] [Singh and Ghosh 2023] [Singh et al. 1989] [Sinha et al. 2022] [Sirbaugh 1983] [Sivasubramanian et al. 2026] [Sleeman 1957] [Smeltzer et al. 1983] [Smith 1953] [Smith 1961] [Smith et al. 1979] [Smith et al. 1993] [Smith et al. 1994] [Smoot et al. 1972] [Solarte-Pineda et al. 2026] [Spahr 1954] [Spahr and Robinson 1951] [Spearman 1953] [Spearman 1961] [Spearman 1979] [Spearman 1983] [Spearman 1986a] [Spearman 1986b] [Spearman 1992] [Spearman and Braswell 1994] [Spearman and Driver 1958] [Spearman and Driver 1959] [Spearman and Fournier 1978] [Spearman and Robinson 1952] [Spearman and Robinson 1954] [Spearman and Sawyer 1977] [Spencer 1961] [Spencer 1981] [Srivastava 1998b] [Srivastava 1998a] [Srivastava and Srivastava 1997b] [Srivastava and Srivastava 1997a] [Stallings 1984] [Stephen et al. 2018] [Stephens 1959] [Stevens et al. 1974] [Stewart 1981] [Stewart 1986] [Stoll and Koenig 1983] [Stone 1945] [Storey 2023] [Strope and Kretzschmar 1998] [Sturek and Schiff 1980] [Sturek and Schiff 1981] [Sturek et al. 1983] [Sun et al. 1984] [Szklarski and Głębocki 2025] [Tahani et al. 2017] [Takanashi et al. 1998] [Tang and Pearson 1971] [Tang et al. 2017] [Tao et al. 2010] [Taraborrelli 2023] [Taur and Chern 1999] [Taylor 2022] [The Effects of Canard-Wing 1988] [The Generalized Missile Equations] [Theerthamalai et al. 2025] [Tkalenko 1969] [Transition Aerodynamics for Close-Coupled 1979] [Trescot 1971] [Trescot et al. 1973] [Triplet 1983] [Triplett 1984] [Tu 1992] [Tu 1994] [Tu 1996] [Tu and VanDalsem 1996] [Tucker 1948b] [Tucker 1948a] [Tucker and Nelson 1948] [Tuncer and Platzer 1996] [Underwood et al. 2007] [Uselton and Uselton 1975] [Vasile 2019] [Vaughn 2002] [Vaughn 2006] [Vaughn and Milton E. 2008] [Venkatachari et al. 2015] [Venkatachari et al. 2020] [Voronin and Shvets 1984] [Vukelich and Jenkins 1981] [Vukelich and Jenkins 1983] [Walker and Heltsley] [Wang et al. 2021g] [Wang et al. 2024c] [Ward 1950] [Wardlaw et al. 1980] [Wardlaw et al. 1985] [Warsi 1986] [Washington 1983] [Washington and Miller 1993] [Washington and Spring 1982] [Watkinson et al. 1986] [Wei et al. 2024b] [Wei et al. 2024a] [White 1995] [Whiting 1996] [Wilkins 1971] [William Ruffles and Sam M. Dakka 2016] [Williams 1982] [Wise 1953] [Xie et al. 2019] [Xu and Qiu 2011] [Yang 1995] [Yang et al. 2011b] [Yang et al. 2012] [Yi et al. 2021b] [Yip 1985] [Yip and Paulson 1977] [Yoo et al. 2023] [Zaikang and Defu 2019c] [Zhang and Yuan 2019] [Zhang and Zhang 2013] [Zhang et al. 2019d] [Zhang et al. 2025d] [Zhang et al. 2026f] [Zhao et al. 2013] [Zhao et al. 2025c] [Zhaoqing and Hailong 2016] [Zhou et al. 2013a] [Zou et al. 2026] [Çetiner et al. 2016] [ŞUmnu and GÜZelbey 2023]

Autopilots, actuators and inertial instruments

The inner loop and the instruments that feed it. Missile autopilot design by every method from classical loop shaping to sliding modes and linear parameter-varying synthesis, fin actuators, gyroscopes and their drift, inertial navigation and alignment, and the structural coupling of a flexible airframe. 289 of these titles name an autopilot. 87 name a gyroscope, 61 of the 84 dated ones are from 2010 or later, and 40 name a micro-machined, fibre-optic or resonator device, which is the inexpensive instrument The Autopilot Inner Loop credits with inverting the architecture.

618 records. [A Novel Method Based 2017] [Abd-Altief and Qian 2014] [Abdulrahim et al. 2004] [Abel 1971] [Aberg et al. 1962] [Abratanski et al. 2023] [Ada and Kural 2017] [Adamović et al. 2022] [Adaptive Neural Network Based 2016] [Ailneni et al. 2023] [Akcayir and Ozkazanc] [Alsaraj and Stuffle 2015] [Altınöz et al. 2024] [Anli Shang et al] [Anli Shang et al] [Ansary and Rahrooh] [Apostolakis and Jordan] [Application of Improved L/sub 1999] [Application of Strongly Tracking 2017] [Arnold et al. 1991] [Arrow 1982] [Arrow and Williams 1987] [Askari et al. 2021] [Astrov et al] [Astrov et al. 2007] [Atkinson 1968] [Atkinson 2016] [Avdieiev and Aleksandrov 2023] [Awad and Wang 2016a] [Awad and Wang 2016c] [Awad and Wang 2016b] [Awad and Wang 2017] [Backus 1965] [Bai et al. 2017] [Bai et al. 2022] [Ball 1978] [Ball 1979] [Banerjee et al. 2015] [Bar-Itzhack 1981] [Bar-Itzhack and Vitek 1985] [Bar-Itzhack et al. 1982] [Barrett 1993] [Basha and Swarup 2017] [Bass 1956] [Bendotti and M’Saad 1991] [Bentsman et al. 1991] [Berk Gezer and Kutay 2014] [Bialy et al. 2012] [Biannic and Apkarian 1999] [Bibel and Stalford 1991] [Biyikli et al. 2022] [Blumel and White] [Bo and Huan 2015] [Bo and Jun 2014] [Boia et al. 1994] [Bolender et al. 2007] [Bossi and Langehough 1988] [Breckenridge and Treder 1977] [Breckenridge and Treder 1978] [Brown et al] [Brugarolas et al. 1998] [Bryson and Gruenwald 2022] [Bryson et al. 2019] [Bullock and Fields 1998] [Buschek 1998] [Buschek 2001] [Buschek 2003] [Buschek and Buschek 1997] [Buschek and Dold 2001] [Butler and Pastrick 1983] [Bużantowicz 2016] [Bużantowicz 2021] [Bużantowicz et al. 2015] [Byoung-Mun Min et al. 2007] [Cai 2014] [Cao et al. 2025a] [Carestia et al. 1983] [Carroll and Cox 1983] [Casavola and Mosca 2004] [Cechowicz 2017] [Cha et al. 2024] [Chadwick 1995] [Chang et al. 2016] [Chang et al. 2019] [Chao et al. 2009] [Chen 2017] [Chen and Cui 2016] [Chen et al. 1994] [Chen et al. 2010a] [Chen et al. 2012b] [Chen et al. 2012a] [Chen et al. 2018b] [Chen et al. 2018a] [Chen et al. 2020a] [Chen et al. 2020b] [Chen Xianxiang et al. 2012] [Chi et al. 2021] [Chikovani and Golovach 2021] [Ching-Fang Lin et al] [Ching-Fang Lin et al] [Cho et al. 2011] [Chomachar and Fard 2016] [Christopher 1980] [Chung and Shapiro 1982] [Clayton and Posingies 1965] [Coelho and Hemerly 2017] [Cohen 1981] [Cole and Abramovitz 1952] [F. William Nesline; Brian H. Wells; Paul Zarchan 1981] [Cong and Kunfeng 2017] [Cooper 1965] [Costandin et al. 2021] [Crawford et al. 1972] [Dae-Seong Jeong et al. 2007] [Dangui et al. 2009] [Das et al] [Dasaro 1970] [Deng et al. 2015] [Design of Missile 2016] [DeTroye and Ellis 1994] [Devan and Chandar 2018] [Devan and Chandar 2019] [Devaud and Siguerdidjane 1999] [Devaud and Siguerdidjane 2002] [Devaud et al] [Devaud et al. 1999] [Diao et al. 2013] [Dinesh et al. 2021] [Dinter 1970] [Dong and Cai 2017] [Dong et al. 2009] [Dorsey et al. 2026] [Du 2017] [Duan 2014] [Duan Chao-yang et al. 2010] [Dutzmann and Ludtke 1969] [Eguchi et al. 1999] [Elmelhi 2013] [Elston 1963] [Engedy and Horvath 2015] [Erkan and Tatar 2024] [Eslinger 1964] [Etzweiler 1969] [Evans and Wilcox 1969] [Fagin et al. 1969] [Falkiewicz et al. 2011] [Fan and Su 2010] [Fan et al. 2008] [Fan et al. 2010] [Fan et al. 2019] [Fan et al. 2021] [Fan et al. 2024] [Farret et al. 2002] [Feng 2018] [Feng Tan et al. 2006] [Ferreres and M’saad 1994] [Ferreres and M’Saad 1995] [Fields and Bullock 1996] [Florencio et al. 2020] [Flowe and Bright 1963] [Fortescue 1982] [Fowler 1990] [Freed and Miller 1961] [Friang et al. 1996] [Full Envelope Missile Longitudinal 2000] [Gade and Mangrulkar 2018] [Galante and Sanner 2012] [Gan et al. 2013] [Gao et al. 2007] [Gao et al. 2008] [Gao et al. 2020] [Garner and Poole 1974] [Ge Ming et al. 2011] [Geng et al. 1995] [Gido et al. 1974] [Gieseking 1963] [Girard 1986] [Giurgiutiu and Pomirleanu 2000] [Glaros] [Golliday 1985] [Gopmandal and Ghosh 2019] [Graham 1967] [Gratt and McCowan 1993] [Gu et al. 2019] [Gully and Skelley 1975] [Guo et al. 2018b] [Guo et al. 2021b] [Guoxiang Gu et al] [Gurav et al. 2017] [Haddadpour 2006] [Haeussermann 1957] [Hahn 1974] [Haipeng et al. 2007] [Hamer 1952] [Han and Sabbagh 2022] [Han and Thaler 1967] [Han et al. 2020] [Han et al. 2024b] [Harcaut et al. 2001] [Harding and Lawson 1968] [Hasturk 2015] [He et al. 2015a] [Hewer et al] [Hewer et al. 1988] [Hickey 1975] [Hindman and Shell] [Hindman and Shell] [Hirokawa et al. 2001] [Ho Chul Lee et al] [Hoch 1960] [Hong et al. 2006] [Hosseini-Pishrobat and Tatar 2025] [Hostetler 2005] [Hu et al. 2008] [Huang and Lin 1993] [Huang et al. 2016a] [Hughes and Wu 2010] [Hughes et al] [Hull and Zhihua Qu 1997] [Huo et al. 2016] [Hussein et al. 2026] [Hwang et al] [Hyde and Cleminson 2004] [Iglesias and Urban 1999] [Iida et al. 2026] [Imado et al. 1991] [Incremental Stability 1999] [Ismail et al. 2023] [Istiqomah et al. 2021] [Jackson 1990] [Jackson 1992] [Jacob et al. 2023] [Jahangir and Howe 1990] [Jahangir and Howe 1993] [Jain et al. 2023] [Jain et al. 2024] [Jiang and Li 2023] [Jiang et al. 2011] [Jiang et al. 2017] [Jiang et al. 2025] [Jianmao et al. 2007] [JianQi et al. 2021] [Jie et al. 2006a] [Jin et al. 2010] [Jiu-ling Zhao and Jiu-fen Zhao 2006] [Jones and Moore 1987] [Joyce et al. 2025] [Juang et al] [Junlong et al. 2013] [Kada 2011] [Kada 2015b] [Kaertner 2006] [Kamen et al. 1988] [Kang et al. 2008] [Kang et al. 2009] [Karagöz et al. 2024] [Karelahti and Virtanen 2007] [Karelahti et al. 2006b] [Karelahti et al. 2007] [Karpinski 2021] [Kashefi and Hajatipour 2025] [Katsionov 2026] [Kawatsu et al. 2020] [Kawiecki and Smith 1994] [Kayran and Nalci 2014] [Kehoe et al. 1990] [Khalifa and Hashim 2026] [Kim and Jang 1995] [Kim and Song 1998] [Kim et al. 2004b] [Kimata et al. 2015] [Klenke 2006] [Kline et al. 2013] [Knauber 1982] [Knight 2023] [Kozlov et al. 2026] [Krause and Stein 1988] [Kruczynski et al. 1971] [Kwon 2026] [Landherr and Klein 1987] [Landherr and Klein 1989] [Lassami et al. 2006] [Lawrence et al. 1998] [Le et al. 2023] [Lee and Choi 2005] [Lee and Singh 2011] [Lee and Singh 2026] [Lee et al. 2004a] [Lee et al. 2015a] [Lee et al. 2020] [Lee et al. 2025] [Lei et al. 2011] [Lei et al. 2025b] [Leondes and Pearson 1968] [Letty and Jang 1997] [Levi and Stahlhuth 1977] [Lhachemi et al. 2016b] [Lhachemi et al. 2016a] [Li 2010] [Li and Zhang 2021] [Li et al. 2019a] [Li et al. 2019f] [Li et al. 2021a] [Li et al. 2025e] [Li et al. 2026a] [Liao and Bang 2022] [Licata 1990] [Lilian Bruyeere et al] [Lin and Fan 2009] [Lin and Hwang 2003] [Lin and Lee 1984] [Lin and Shafroth 1983] [Lin et al. 1991] [Lin et al. 2022] [Lind et al. 1999] [Liu and Chen 2011] [Liu et al. 2010c] [Liu et al. 2013b] [Liu et al. 2016] [Liu et al. 2017a] [Liu et al. 2020a] [Longenbaker 1982] [Lorenz and Bierig 2013] [Lou and Zhang 2009] [Lovtsov and Karpov 2011] [Lukens et al. 1961] [Luo et al. 2016] [Lv et al. 2019] [Ma and Li 2020] [Mahdianfar and Prempain 2016] [Mao et al. 2021] [Marchetti Tavares and Waldmann 2021] [Maré 2022] [Mason and Wedekind 1970] [Matmurodov and Toshtemirov 2025] [Mattei and Monaco 2012] [Matthews and Taylor 1969] [Maulani et al. 2026] [McDowell et al. 1995] [McFarland and Calise 1996] [McFarland and D’Souza 1994] [McFARLAND and D’Souza 1995] [McFarland and Hoque 2000] [McLain and Beard 1998] [McLain and Beard 1999] [McLaughlin et al. 2026] [Mehrabian and Roshanian] [Meng et al. 2026] [Menon et al. 1997] [Menon et al. 1999] [Merhav 1979] [Merriam 1960] [Merz 1964] [Meyers and Weiderman 1988] [Mickle and Zhu] [Mickle and Zhu] [Mickle and Zhu] [Mills et al. 2002] [Ming Xin and Balakrishnan] [Missile Attitude Control 2013] [Missile Autopilot Design Based 2017] [Missile Autopilot Design Using 2004] [Mitchell 1976] [Moghimi Rad et al. 2021] [Mohamed and Yan 2016] [Mohammadkarimi et al. 2025] [Mohenski 1998] [Moon et al. 2012] [Mooney 1962] [Moul 1953] [Mracek 2014] [Mracek and Ridgely 2005] [Mracek et al. 1997] [Mungall 1948] [Nabaa et al. 1993] [Naidu and Kumar 2022] [Nazemipour et al. 2020] [Nesline and Zarchan 1982a] [Nesline et al. 1979] [Nguyen and Cao 2024] [Nguyen et al. 2021] [Nguyen-Tat et al. 2026] [Nikiforovskii et al. 2022] [Shin 2005] [Optimal Disturbance Rejection 1992] [Ouda 2017] [Pachikara and Lind 2012] [Pain and Tiwari 2013] [Pal et al. 2014] [Park and Ahn 2020] [Parkhi et al. 2010] [Parkinson et al. 1973] [Pasik et al. 1975] [Passera 1951] [Patel et al. 2003a] [Peebles 2006] [Peter et al. 2012] [Peter et al. 2013] [Petersen et al. 2000] [Platanitis and Shkarayev 2005] [Pleasants 1975] [Podder et al. 2024] [Polynomial Approach for Design 2016] [Poole 1965] [Potter and Deckert 1972] [Practical Considerations in Robust 2016] [Pratama et al. 2019] [Prempain et al. 2001] [Priydarshi et al. 2016] [Prochazka 2026] [Qi and Jianliang 2017] [Qi and Wang 2024] [Qianchen et al. 2011] [Qiao et al. 2019] [Quan et al. 2014] [Quattrocchi et al. 2022] [Rabbath et al. 2004] [Rajagopal and Balakrishnan 2012] [Rashed et al. 2013] [Raspopov 2018] [Ratliff and Pagilla 2008] [Rawashedeh and Lumpp 2014] [Rehman et al. 2009] [Reichert 1989] [Rezazadeh Mohammadi et al. 2016] [Ridgely et al. 2006] [Rimer and Frederick] [Ristanović et al. 2012] [Robust Autopilot Design 2016] [Robust Stability Analysis 1999] [Rodríguez Martínez] [Roscoe 2001] [Ru et al. 2022] [Ruan et al. 2021] [Ruan et al. 2023] [Ruimin et al. 2015] [Ruth 1989] [Ruth 1990] [Sadr and Momeni 2011] [Salamci and Gökbilen 2007] [Salman et al. 2022] [Sankar et al. 2016] [Saussié et al. 2008] [Savage 1998a] [Savage 1998b] [Savage 2002] [Savage 2013] [Schmit and Raman 2006] [Schmit et al. 2005] [Schumacher and Khargonekar 1998] [Schumacher and McClamroch] [Schwarz 1981] [Scott 1966] [Seaberg and Smith 1951] [Seiner et al. 2000] [Sells 2015] [Shamma and Cloutier] [Shamma and Cloutier 1992a] [Shelan et al. 2020] [Shen et al. 2026] [Shiau et al. 2011] [Shibata 1986] [Shijie and Hang 2015] [Shkolnikov et al. 2000] [Shtessel 2001] [Shumaker and Brown 2009] [Shuping Tan and Zhibin Li 2010] [Siddarth et al. 2014] [Siguerdidjane and Devaud 2000] [Silvius and Sherrill 1978] [Simões and Cavalcanti 2023] [Singh 2004] [Singh 2016] [Skarpetis et al. 2018] [Slater 1956] [Smith and Keys 2018] [Sobolic et al. 2015] [Solov and Thibodeau 1973] [Song et al. 2013] [Song et al. 2019] [Sperry Gyroscope Co Great Neck Ny 1963a] [Sreekumar and Ramchandani 2005] [Sreenuch et al] [Srour and Abdulkerim 2026] [Stallard 1966] [Stallard 1976] [Stansbery and Cloutier 2001] [Stefanski 2019] [Steinicke and Michalka 2002] [Stephan et al. 2023] [Stephens and Ridgely 1995] [Stokes and Lombaerts 2023] [Sui et al. 2008] [Sun and Er 2001] [Sun and Liu 2009] [Sun et al. 2020] [Sun et al. 2023] [Taguchi et al. 2015] [Taheri-Tehrani et al. 2018] [Tahk et al] [Tailoring Theory to Practice 1999] [Talole et al. 2004] [Tamer 2021] [Tan et al. 2018] [Tavares and Waldmann 2023] [Tekin et al. 2010] [Thai et al. 2019] [Theis et al. 2015] [Theodoulis and Duc 2007b] [Theodoulis and Duc 2007a] [Theodoulis et al. 2013] [Thukral and Innocenti 1998] [Tian et al. 2020a] [Tiwari and Detroja 2024] [Tiwari and Detroja 2025] [Tsai and Chung 2026] [Tsai and Lin 2006] [Tsourdos 1998] [Tsourdos and White 2012] [Tsourdos et al. 2006] [Tsourdos et al. 2012] [Unnikrishnan and Balakrishnan 2004] [Unnikrishnan and Balakrishnan 2005] [Urban et al] [Vaddi 2006] [Van Dierendonck] [Van Winkle and Rossi 1966] [Vaughn 1960] [Wan et al. 2012] [Wang 2015b] [Wang 2025] [Wang and Chen 2018] [Wang and Qi 2013] [Wang and Shan 2020] [Wang and Wang 2009] [Wang and Wang 2018] [Wang et al. 2008] [Wang et al. 2011] [Wang et al. 2021a] [Wang et al. 2022j] [Waymeyer and Young 1964] [Wei et al. 2019a] [Wei et al. 2019b] [Wei et al. 2022] [Weijie et al. 2016] [Weil and Wise] [Wells 1991] [Wen et al. 2027] [Weng and Shi 1999] [Weng et al. 2020] [White et al] [White et al] [Williams 1987] [Wilson 1970] [Wilson et al] [Wise 1988a] [Wise 1988b] [Wise 1989b] [Wise 1989a] [Wise 1990b] [Wise 1990a] [Wise 1991] [Wise 1993] [Wise 2007] [Wise 2008] [Wise and Broy 1996] [Wise and Deylami 1991] [Wise and Hamby] [Wise and Kundur 1993] [Wise and Nguyen] [Wise and Sedwick 1994] [Wise and Sedwick 1995] [Wise et al. 1990] [Wu and Yu 2018] [Wu et al. 1996b] [Wu et al. 1996a] [Wu et al. 2002] [Xiaoxi et al. 2013] [Xieyu et al. 2022] [Xin and Balakrishnan 2003] [Xu and Pei 2016] [Xu and Tang 2010] [Xue and Nakamura 2011] [Xue et al. 2023] [Yan and Wang 2025] [Yan et al. 2017] [Yang et al. 2010] [Yang et al. 2015a] [Yin et al. 2018] [Yinqiang Zhang et al. 2010] [Yong et al. 2015] [Yoo 2017] [Youmans et al. 1990] [Yu-bin Yu and Jing Zhang 2008] [Yuan and Long 2010] [Yuan and Wu 2016] [Yue Pan et al. 2011] [Zaher et al. 2010] [Zaman et al. 2009] [Zeng et al. 2021] [Zeng et al. 2025] [Zhang et al. 2005] [Zhang et al. 2013] [Zhang et al. 2016a] [Zhang et al. 2020] [Zhang et al. 2021] [Zhang et al. 2022f] [Zhao and Tang 2012] [Zhao et al. 2018] [Zhengyu and Xiaogeng 2011] [Zhong and Xiaohong 2008] [Zhou et al. 2010a] [Zhou et al. 2018] [Zhou et al. 2023c] [Zhu and Mickle] [Zhu et al. 2024] [Zinsou 2024] [ÇLimen 2011]

The human operator and control across a delay

The man who closed the loop, and the loop he became. Manual control and its models, the crossover model, compensatory and pursuit tracking, operator workload and situation awareness, the allocation of functions between the operator and the automation, and teleoperation across a communication delay. The subject moved from the operator to the delay. The 92 titles that name manual control, manual tracking or compensatory tracking have a median year of 1983, and the 179 that name teleoperation have a median year of 2016.

522 records. [A Method for Aiding 1972] [Abdel-Malek and Marmarelis] [Abdel-Malek and Marmarelis 1988] [Abidi et al. 2016] [Abubakar et al. 2026] [Active Force Reflection Devices 1991] [Adams 1962] [Adel et al. 2017] [Agarwal et al. 1982] [Al-barzinji] [Albakri et al. 2013] [An and Niu 2025] [Andersh et al. 2009] [Anderson] [Ando et al] [Anggara 2025] [Angué et al. 1978] [Antunes et al. 2010] [Application of the Optimal 1974] [Arcara et al. 2001] [Arend et al. 2026] [Aretz et al. 1987] [Arif and Inooka 1999] [Artigas Esclusa] [Assen and Eijkman 1970] [Atashfeshan et al. 2021] [Aziminejad et al. 2008] [Ballistic Missile Office Norton AFB CA 1986] [Baron and Levison 1977] [Barr et al. 1988] [Baty 1970] [Beare and Kahn 1967] [Begum and Aqlan 2025] [Beideman et al. 1980] [Bejczy et al. 1994] [Bejczy et al. 1995] [Bekey et al. 1965] [Bekey et al. 1967] [Ben-Porat et al. 2000] [Bernard and Cruz Neira 2002] [Bi et al. 2015] [Bidwell et al. 2014] [Biezad and Schmidt 1984] [Bikas et al. 2023] [Bilateral Matched Impedance Teleoperation 1999] [Black et al. 2022] [Black et al. 2024] [Blair 1981] [Blair 1985] [Boeing Aerospace Co Seattle Wa 1975] [Boer and Kenyon 1998] [Bolat and Avci 2025] [Borst et al. 1984] [Bos et al. 1992] [Bos et al. 1993] [Bos et al. 1995] [Botturi et al. 2004] [Boy] [Brady and Tarn 2001] [Brudnak 2016] [Brudnak 2020] [Brueckner et al. 2023] [Burke et al. 2013] [Burstein and Schechter 1970] [Butlewski 2017] [Bye et al. 1999] [Cabrall et al. 2017] [Caldwell et al. 2019] [Callin et al. 1981] [Canellas and Haga 2015] [Canellas and Haga 2020] [Cass] [Cassimatis 2011] [Cassimatis 2012] [Chan 2026] [Chappell and Dunlap 2006] [Chawda and O’Malley 2011] [Chen and Liu 2021] [Chen and Wu 2009] [Chen et al. 2006b] [Chen et al. 2014a] [Chen et al. 2021b] [Chen Qihong et al] [Cheng et al. 2017a] [Chepurnov 2023] [Chernikoff and Taylor 1957] [Chornyi et al. 2024] [Christensen and Estepp 2013] [Christensen et al. 1981] [Cohen and Ferrell 1969] [Colburn 1978] [Cook 1999] [Cook 2000] [Corbridge and Cook 1999] [Corker and Bejczy 1984] [Costello 1968] [Craley and Desabrais 2007] [Crossman et al. 2012] [Davenport et al. 1981] [Deets and Szalai 1970] [Dehghan et al. 2021] [Deutsch 2006] [Dickerson et al. 2025] [Doane 2003] [Doman and Anderson 1998] [Doman and Anderson 2000] [Drakulić 2023] [Drury 1976] [Durga] [Durgun 2017] [Dynamic Function Allocation 2006] [Ebrecht 2025] [Elkind and Forgie 1959] [Elkind and Miller 1967] [Ellis et al. 1987] [Ema 1990] [Engler et al. 1980] [Ernst et al. 2019] [Feigh and Pritchett 2016] [Fialho Coelhoe] [Fifth Annual NASA-University Conference 1970] [Fiorini et al. 1987] [Fleck 1983] [Forouhar et al. 2024] [Franc and Hace 2012] [Friedrich and Vollrath 2021] [Fu and Gould 1966] [Fu et al. 2011] [Fuld 1993] [Fuld 2000] [Furukawa et al. 2004] [Bekey et al. 1966] [Gagne and Wierwille 1966b] [Gagne and Wierwille 1966a] [Gardiner et al. 1950] [Ge et al. 2026] [Georg et al. 2020] [Gerisch et al. 2013] [Glenn 1988] [Goldbeck and Ferrante 1981] [Goossens] [Govindaraj and Mitchell 1994] [Green et al. 2025] [Grindley et al. 2026] [Grote et al. 2000] [Gschwind 1976] [Guercio and Wall 1972] [Guo et al. 2015] [Guédon et al. 1995] [Hace and Franc 2014] [Hacısalihzade 2013] [Hale 1992] [Hallbert] [Haller et al. 2015] [Hancock and Scallen 1996] [Hanson 2012] [Harris 1978] [Harris et al. 1979] [Harrison] [Higashino et al. 2019] [Lin et al. 2023] [Litaker et al. 2024] [Litaker et al. 2025] [Hashtrudi-Zaad and Salcudean] [Hashtrudi-Zaad and Salcudean 1999] [Havlikova and Sediva 2012] [Hawley and Mares 2006] [Helldin and Falkman 2012] [Hess 1979] [Hicks et al. 2023] [Hildebrandt and Harrison 2003] [Hill and Bliss 1972] [Hisanosuke Kawada and Toru Namerikawa 2008] [Hoffman and Johnson 2019] [Hogan et al. 2010] [Hokayem et al. 2006] [Holden and Shinners 1973] [Hollnagel 2018] [Hollnagel and Bye 2000] [Horiuchi and Yuhara 1988] [Horiuchi and Yuhara 1989] [Hou] [Houck et al. 1986] [Houweling et al. 2024] [Hua and Yang 2011] [Hua et al. 2019] [Huang et al. 2024b] [Huang et al. 2024a] [Human-In-the-Loop Learning and Control 2023] [Hutchins 1974] [Idris et al. 2016] [Inaba and Matsuo 1995] [Inaba and Matsuo 1997] [Inbar 1991] [Innovative Flight Deck Function 2012] [Inoue and Sakaguchi 2014] [Integrated Interface for Advanced 1993] [Intelligent Sensing and Control 1993] [Ishii et al] [Istepanian 1998] [Ito and Ito 1975] [Ito et al. 1973] [Jabbour] [Jackson 1967] [Jackson 1969] [Jaeger et al. 1980] [Jagacinski et al. 1978] [Jee-Hwan Ryu and Jong-Hwan Kim] [Jex et al. 1966b] [Jex et al. 1966a] [Jin and Pagilla 2020] [Jin et al. 2024] [Joe et al. 2015] [Johnson 1995] [Johnson et al. 2001] [Jones and Hunter 1991] [Kaber et al. 2000a] [Kaber et al. 2000b] [Kao 1977] [Kapela 2026] [Kashler 1961] [Katsuyama et al. 2023] [Kawai and Namerikawa 2012] [Kay and Thorpe 1995] [Kbaier Ben Ismail and Grivard 2015] [Kenyon 1981] [Khademian and Hashtrudi-Zaad 2012] [Khan et al. 2026] [Kibbe and Stiff 1993] [Kibbe and Weisgerber 1990] [Kidwell et al. 2014] [Kim and Bejczy 1993] [Kim et al. 2008] [Kim et al. 2024] [Kivila et al. 2015] [Knacke 1985] [Knutzon] [Koochaki and Talebi 2016] [Korn and Kleinman 1978] [Kovesdi et al. 2022] [Kreifeldt 1965] [Kruger and Shaw] [Krukowski] [Krüger and Shaw 1991] [Kurochkin and Mal’tsev 1982] [Lai and Hsu 2011] [Landry 2010] [Lang and Vacroux 1969] [Larochelle and Kruijff 2012] [Larochelle et al. 2011] [Lawn and Hannaford] [Le] [Lee and Moray 1992] [Lee et al. 2024b] [Lefebvre] [Li and Chou 2025] [Li et al. 2013a] [Li et al. 2015c] [Li et al. 2015b] [Li et al. 2015h] [Li et al. 2015e] [Li et al. 2015d] [Li et al. 2015g] [Li et al. 2015a] [Li et al. 2020a] [Li et al. 2024a] [Li et al. 2025d] [Li et al. 2026c] [Lin et al. 2025] [Lin et al. 2026] [Liu and Kaber 2025] [Lopez Martinez et al. 2012] [Lopez Martinez et al. 2013] [Louca et al. 2023] [Louca et al. 2024] [Luo et al. 2019] [Luo et al. 2024] [Luz et al. 2023] [Lysaght et al. 1989] [Ma and McDonald 2026] [Madni] [Malysz and Sirouspour 2010] [Manual Control Devices 2006] [Martin et al. 1999] [Martin et al. 2016] [Martinez-Garcia et al. 2017] [Martinovsky and Traum 2006] [Martín Barrio] [Mason et al. 2007] [Masuyama 1992] [McCabe 2011] [McCandlish 1966] [McCARTHY et al. 2000] [McCracken and Aldrich 1984] [McLaughlin and Staunton 1989] [McLeod 2025] [McNeill et al. 1982] [Mehrjouyan et al. 2025] [Meiry and Young 1965] [Melchiorri 2015] [Merhav 1989] [Mettler and Andersh 2013] [Miall 1996] [Micro-Teleoperation with Manual Task 1995] [Middlebrooks et al. 1999] [Mihelj and Podobnik 2012] [Miller 1965] [Miller and Jagacinski 1986] [Miller and Pachter] [Miller et al. 1977] [Mingde et al. 2010] [Mitchell 1964] [Mitchell and Kinney 1966] [Model Assignments and the] [Mohammadi et al. 2011] [Mol et al. 2026] [Monty and Ruby 1965] [Moray et al. 1998] [Moreno 2014] [Mouloua et al. 1993] [Muckler 1961] [Muralidharan et al. 1979] [Natori 2014] [Neff and Junker 1974] [Neurodynamics-Based Teleoperation 2026] [Nicolas Marcassus 2006] [Nie et al. 2019] [Niemeyer and Slotine 1990] [Nomberg and Nisky 2023] [North and Lomnicki 1961] [North and Riley 1989] [Obšilová et al. 2016] [Oehler and von Stryk 2021] [Onnasch 2015] [Pacheco-Gutierrez et al. 2021] [Pachter et al. 2008] [Pacis et al. 2004] [Panzirsch] [Zeiger et al. 2008] [Peng et al. 2017] [Perkins] [Kazanzides et al. 2021] [Petkosek et al. 2005] [Petousakis et al. 2020] [Pew 1966] [Pilette et al. 1978] [Popovici et al. 2017] [Potter and Singhose 2012] [Potter and Singhose 2013] [Prakash et al. 2022] [Price 1970] [Pritchett et al. 2013b] [Pritchett et al. 2013a] [Proceedings of the Seventeenth 1981] [Pruett 2008] [Qiao and Cheng 2006] [Rahal] [Rakita et al. 2020] [Ratwani et al. 2010] [Real Time Unilateral Teleoperation 2011] [Reising 2005] [(René) van Paassen and Mulder 1998] [Repperger and Junker 1975] [Ridge and Bayes Identification 1976] [Roberts and Gawron 1986] [Rojas-Ramirez] [Rose et al. 1966] [Rose et al. 1967] [Rosema et al. 2014] [Rowen et al. 2019] [Rowen et al. 2021] [Ruscio et al. 2024] [Saito et al. 2022] [Sakaguchi 2011] [Salcudean] [Sallam et al. 2013] [Scallen et al. 1995] [Schipani and Messina 2007] [Schippers et al. 2025] [Scholcover and Gillan 2017] [Schroeder 1993] [Schryver] [Schryver] [Schutte 2000] [Seeley and Bliss 1966] [Seo et al. 2024] [Seok-Jae Lee and Joon Lyou 2007] [Sewoong Kim and Hamel] [Shaw 1993] [Shen et al. 2019] [Sheridan 1984] [Sheridan 1995] [Sheridan 2000] [Shibata et al. 2005] [Shin et al. 2022] [Shiotsuki 2006] [Shirley 1978] [Siapkaras 1977] [Siegel et al. 1961] [Singh and Mahmoud 2019] [Sirouspour and Salcudean 2003] [Sixteenth Annual Conference 1982] [Sklar and Sarter 1999] [Smith 1971] [Soeda 1998] [Sol Acero] [Son and Lee 2008] [Wickens et al. 2015] [Sperry Gyroscope Co Great Neck Ny 1963c] [Steinberg 2011] [Stepp and Turvey 2017] [Stornig et al. 2021] [Suenaga 1996] [Suenaga and Ihara 1991] [Suenaga et al. 1983] [Sun and Tsai 2025] [Sun et al. 2026] [Suzuki and Ohnishi 2010] [Sweet 2013] [Szakaly et al. 1989] [Takano et al. 2000] [Takashima et al. 1980] [Tang et al. 2012] [Tang et al. 2024] [Tanner et al. 2015] [Teleoperator Human Factors Study 1986] [Teng 2016] [Tervo 2010] [The 14th Annual Conference 1978] [Thibodeaux 1977] [Third Annual NASA University 1967] [Brooks et al. 1992] [Tobey and Bastress 1966] [Todosiev 1967] [Tomizuka and Whitney 1976] [Tong et al. 2026a] [Toni 1968] [Toumodge 1990] [Tvaryanas 2006] [Uddin and Ryu 2016] [Uhlemann and Geiser 1975] [van de Merwe et al. 2022] [van der El et al. 2020] [Van Orden 2001] [Vanlunteren 1977] [Vareille et al. 2007] [Vercher and Gauthier 1992] [Vertut and Coiffet 1985] [Veselic et al. 2020] [Viinikainen et al. 2014] [Vinje and Pitkin 1972] [Viviani et al. 1987] [Wang] [Wang 2010] [Wang 2026] [Wang and Bubb 2008] [Wang et al. 2012] [Wang et al. 2022h] [Wang et al. 2023e] [Wang et al. 2024j] [Wang et al. 2024f] [Wang et al. 2024d] [Wang et al. 2025d] [Ware 1972] [Washizu et al. 1978] [Webb et al. 2016] [Welch] [Wempe 1976] [Wherry 1976] [Wierwille 1965] [Wightman and Lintern 1983] [Wightman and Lintern 1985] [Wightman and Lintern 2017] [Wijlens et al. 2020] [Wilde and Westcott 1963] [Wills 1963] [Willumeit 1987] [Wolf 1978] [Wright et al. 2000] [Xu et al. 2024a] [Xu et al. 2024b] [Xu et al. 2025a] [Yan et al. 2021] [Yang et al. 2014a] [Yang et al. 2015b] [Yang et al. 2015c] [Yang et al. 2015d] [Yang et al. 2020a] [Yang et al. 2021] [Yang et al. 2023b] [Yang et al. 2023e] [Yang et al. 2023f] [Yang et al. 2023c] [Yang et al. 2023a] [Yang et al. 2023d] [Ye et al. 2024] [Yin and Berg 1981] [Yongming and Yuanqing 2015] [Yoon et al. 2025b] [Yoshida and Namerikawa 2009] [Yoshizawa and Takeda 1983] [You et al. 2026] [Young and Deutsch] [Young et al. 1964] [Yu et al. 2026] [Zaychik and Cardullo 2009] [Zaychik et al. 2009] [Zhai and Xia 2014] [Zhai and Xia 2016] [Zhai and Xia 2023g] [Zhai and Xia 2023d] [Zhai and Xia 2023f] [Zhai and Xia 2023a] [Zhai and Xia 2023b] [Zhai and Xia 2023e] [Zhai and Xia 2023c] [Zhai et al. 2023] [Zhang] [Zhang et al. 2011b] [Zhao et al. 2024a] [Zhou et al. 2024] [Zhu et al. 2023b]

Command, beam-rider and homing architectures

Where the sensor sits. Command to line of sight, beam riding, semi-active and active homing, television and optical command guidance, midcourse guidance and the strapdown seeker. The beam rider is a period architecture. 15 titles name it, with a median year of 1963, while 104 name homing.

500 records. [A Thick Film Guidance 1974] [El-gabri , A. N Ouda 2018] [Abdallah Mohamed 2019] [Abdel-Rahim et al. 1993] [Abzug 1967] [Abzug 1979] [Acho 2017] [Zarchan 2019a] [Advances in Missile Guidance 2001] [Balakrishnan et al. 2016] [Aggarwal] [Ahi and Haeri 2021] [Ali et al. 2019] [An et al. 1989] [Andrisani, ck 1995] [Anjaly and Ratnoo 2016] [Army Aviation Board Fort Rucker Al 1960] [Army Materiel Command Alexandria VA 1975] [Arthur and Kemp 2025] [Asran and El-Geneidy 2001] [Assisi 2001] [Assisi 2006] [Avinash et al. 2020] [Baba et al. 1991] [Balakrishnan and Biega] [Balakrishnan and Shen 1996] [Balakrishnan and Speyer 1986] [Balakrishnan and Speyer 1989] [Balbirnie et al. 1975] [Ballenger 1998] [Bao et al. 2021] [Basics of Missile Guidance 2007] [Becker 1973] [Ben-Asher and Speyer 2016] [Benshabat and Bar-Gill 1995] [Bezick] [Bezick et al. 1995] [Bilich et al. 2018] [Blattel 1957] [Bose 1979] [Breitner et al. 2001] [Bromberg 1992] [Budiyono and Rachman 2012] [Bużantowicz 2024] [Bużantowicz and Klicki 2026] [Campbell 1963] [Casasent 1979] [Casasent 1984] [Celmins 2007] [Chandler 1958] [Chaudhary et al. 2005] [Chelaru et al. 2024] [Chelaru et al. 2025b] [Chelaru et al. 2025a] [Chen and Yang 2001] [Chen et al. 2006a] [Chen et al. 2007a] [Chen et al. 2007b] [Chen et al. 2008a] [Chen et al. 2010b] [Chen et al. 2016b] [Chen et al. 2017c] [Chen et al. 2020f] [Chen et al. 2021a] [Chen et al. 2021d] [Chen et al. 2023d] [Chen et al. 2024] [Yang et al. 2016] [Chepurnov and Prokhorenko 2024] [Chiou et al. 1997] [Cho 2021] [Choi 2016] [Clemow 1957] [Cloutier and Stansbery 1999] [Cobb 1949] [Coe 1948] [Constancis and Sorine 1992] [Cook and Craig 1980] [Craig et al. 1980] [Cramer and Lee 1992] [Cutting and Gates 1963] [Dai et al. 2026] [Dalton and Balakrishnan 1993] [Dalton and Balakrishnan 1996] [Danchick 2016] [Dawson and Parke 1968] [Deepak 2004] [Delangre 1959] [Deng et al. 2026] [Design of CLOS Guidance 2016] [DeVorkin 1992] [Deyun and Feng 2008] [Diao et al. 2022] [Differential Geometry Applied 2016] [Dimirovski et al] [Ding et al. 2026a] [Doersam 1965] [Dong et al. 2022] [Dong et al. 2023b] [Dong et al. 2025a] [Douvillier et al. 1956] [Dowdle et al. 1982] [Du and Xia 2016] [Du and Xia 2017] [Duan and Cao 2021] [Duncan 1958] [Dwivedi et al. 2011] [Dwivedi et al. 2013] [Edwards 1971] [Eggleston and Dunning 1961] [Ehrsam et al. 1978] [El-Sheikh 1998] [El-Sheikh and Bahgat] [Elliott and Weller 1954] [Elnan and Lo 1963] [Erdos et al. 2012] [Etzkorn 2001] [Evcimen and Leblebicioglu 2013] [Fan et al. 2015] [Farrell 1968] [Faruqi 2012] [Feng et al. 2013a] [Feng et al. 2013d] [Ferris 1981] [Fiber Optic Link Tested 1981] [Fonod and Shima 2016] [Fossier 1984] [Gao et al. 2026a] [Gaudet and Furfaro 2023] [Gee 1973] [Gee 1978] [Gerber] [Golden 1980] [Gong et al. 2023] [Goodall and Ewen 1987] [Goodrick 1969] [Graf and Trimble 1980] [Green 1992] [Grimm 1993] [Guelman et al. 2012] [Gulick and Miller 1982] [Gurfil 2012] [Gurfil et al. 2001] [Gutman and Ben-Aharon 2006] [Gyu Taek Lee and Jang Gyu Lee 1995] [Hartman et al. 1991] [Haskins 2000] [He and Lee 2018] [He et al. 2020a] [Hecht 1991] [Heller 1955] [Heller et al. 2009] [Hledik 1963] [Hoberg and Rorex 1962] [Holder and Sylvester 1990] [Homing Guidance 2014] [Hong and Ryoo 2014] [Howland 1999] [Hsu et al. 1991] [Hu et al. 2023] [Huang et al. 2016b] [Huang et al. 2017a] [Hull and Speyer 1981] [Hull et al. 1983] [Hull et al. 1984] [Hull et al. 1985] [Hummel et al. 1980] [Hung 2026] [Imado] [Imado and Kuroda 1992] [Iyer 1995] [Jacobs et al. 1961] [Jafarov and Tasaltin 2001] [Jaggers 1977] [Jalali-Naini and Sajjadi 2016] [James 1986a] [James 1986c] [James 1986b] [Jian-bo et al. 2017] [Jiang et al. 2022a] [Jianmei et al. 2012] [Jin et al. 2016] [Jones et al. 1970] [Josey et al. 2019] [Jung et al. 2025] [Kada 2014] [Kaehr and Spector 1980] [Kain 1981] [Kain and Yost 1976] [Kain and Yost 1977] [Kalam 1995] [Kamran 2023] [Kasdorf 1952] [Kasdorf 1953] [Kau et al. 1983] [Kim and Grider 1973] [Kim and Lyou 2006] [Kim and Park 2022a] [Kim et al. 1997] [Kim et al. 2002] [Kim et al. 2014] [Kim et al. 2017b] [Kimel and Harnett 1963] [Klein and Rusnak 2017] [Kloss and Schulte 2013] [Knoblach 1974] [Kochi and Dibble 1963] [Kolodchak et al. 2012] [Koruba and Nocon 2014] [Koruba and Nocoń 2015] [Kowaleczko 2016] [Kreeger and Landrum 2003] [Krishnabrahmam et al. 2000] [Kuehne 1980] [Kumar et al. 1995a] [Kuo and Chiou 2000] [Kuo et al. 2001] [Kuroda and Imado 1988] [Kuroda and Imado 1989] [Kuroda and Imado 1990] [Kuroda et al. 1993] [Langley and Demetrick 1978] [Latonov 2018] [Latonov and Tikhomirov 2018] [Lawrence 1991] [Lawton and Martell 1997] [Lee et al. 2019b] [Legkiy and Unchenko 2024] [Lei et al. 2015] [Levitt 1953] [Levitt 2001] [Li 2015] [Li et al. 2021b] [Li et al. 2022d] [Li et al. 2022e] [Li et al. 2023e] [Li et al. 2024e] [Li et al. 2025a] [Li et al. 2025c] [Liang 1978] [Liang et al. 2014] [Liang et al. 2016] [Liu et al. 2018] [Locke 1950] [Lofts 2015] [Long 1950] [Lu et al. 2022] [Lukacs and Yakimenko 2007] [Luo and He 2026] [Luo and Su 2016] [Luo et al. 2023] [Luo et al. 2025] [Lusser 1952] [Abdallah 2018] [MacKenzie and Zimmerman 1992] [Magis 1960] [Maity et al. 2014] [Makena and Omwoma 2017] [Manchester and Savkin 2003] [Mathews 1960] [Matthews and Stewart 1951] [McDonald et al. 2024] [McNellis et al. 1971] [Mehra and Ehrich 1984] [Meissinger 1963] [Menon and Ohlmeyer 2001] [Meschler 1971] [Milanovic 2008] [Milgram and Bjorklund 1980] [Missile Guidance Software 2007] [Miwa and Imado 1985] [Miwa and Imado 1986] [Model of a Radar 2024] [Mondal and Padhi 2018] [Mortazavi and Almasganj 2018] [Mortensen 1974] [Mosier and Sundareshan 2001] [Mousseau 2013] [Mousseau 2015] [Moustfa et al. 2008] [Muhury et al. 2023] [Muller] [Muzumdar and Hull 1995] [Muzumdar and Hull 1996] [Myers 1965] [Myers 1966] [Nagler 2025] [Nanavati et al. 2021b] [Nanavati et al. 2021a] [Naval Ordnance Lab White Oak MD 1963] [Neoclassical Missile Guidance 2016] [Nesline 1978] [Nesline 1979] [Nesline and Nesline 1984] [Nesline and Nesline 1985] [Nesline and Nesline 1986] [Nesline and Zarchair 1985] [Nesline and Zarchan 1979] [Nesline and Zarchan 1980] [Nesline and Zarchan 1982b] [Nesline and Zarchan 1983b] [Nesline and Zarchan 1983a] [Nesline and Zarchan 1983c] [Nesline and Zarchan 1985] [Nesline and Zarchan 1981] [Ni et al. 2025b] [Ninh 2026] [Nosek 1982] [Nulk et al. 1978] [Or et al. 2021] [Ormsby and Long 1980] [Pachter and Chatterji 1990] [Pan et al. 2025] [Parayil and Ratnoo 2018] [Park 2025] [Park et al. 2026b] [Patel and Madhukar 2021] [Paus and Well 1996] [Pavic et al. 2014] [Peery 1960] [Peilin Sun et al. 2011] [Petersen et al. 2013] [Petters 1952] [Pfenneberger 1966] [Pfifer et al. 2009] [Philipchuk 1952] [Phillips 1994] [Phillips 1995] [Potter 1964] [Powell et al. 1982] [Pratt 1976] [Price and Ehling 1955] [Qiao Xiaolin and Jin Ming] [Qing et al. 2024] [Rahbar and Menhaj 2000] [Ratnoo and Shima 2010] [Ratnoo and Shima 2011] [Reich et al. 1976] [Remmler and Theobald 1967] [Research on Target Tracking 2013] [Research on the Integrated 2023] [Rishel 1967] [Rishel 1968] [Rochowicz 2021] [Rodriguez 1999] [Rodriguez 2007] [Rogers 2004] [Rusnak 2010a] [Rusnak 2010b] [Rusnak 2011] [Rusnak 2012] [Rusnak 2020] [Rusnak et al. 2010] [Ruther et al. 2022] [Sagan 1991] [Sargent 1970] [Sarma and Swamy 1989] [Savage 1969] [Schappell and Knickerbocker 1975] [Schwab 1999] [Seiple 1960] [Sells 1992] [Sethi 2024] [Shaferman and Shima 2010] [Shapin 1991] [Shefer 1990] [Sheporaitis et al. 1976] [Shi et al. 2021b] [Shieh et al. 1980] [Shima 2011] [Shima and Golan 2008] [Shima et al. 2004] [Shinar and Turetsky 2005] [Shinar et al. 2007] [Shinbrot and Carpenter 1958] [Shkolnikov et al. 2001] [Shneydor 1998d] [Shneydor 1998b] [Shortal 1952] [Shortal 1953] [Sigal and Ben-Asher 2010] [Singh and Negi 1995] [Sitton 1982] [Smith 1960] [Sonawane and Mahulikar 2013] [Song and Shin 2004] [Sperry Phoenix Co Az 1962] [Speyer et al. 1982] [Srinivasu and Ratnoo 2022] [Stallard 1973] [Stallard 1979] [Stallard 1984] [Stallard 1985] [Staros 1959] [Stewart 1955] [Stewart 1958] [Stewart 1961] [Stewart and Smith 1959] [Stojanović et al. 2024] [Strohm 2011] [Subchan 2008] [Sun et al. 2018] [Sun et al. 2021] [Sun et al. 2024] [Zarchan 2019b] [Zarchan 2019c] [Talole and Phadke 2002] [Talole et al. 2005] [Tan et al. 2022] [Tanaka and Eguchi 1990] [Tanriverdi and Cavdaroglu 2017] [Tao and Zhang 2026] [Tatum 1949] [Taub and Shima 2012] [Taur 2002] [Taur 2010] [Taur 2013] [Taylor 1956] [Tekin and Erer 2015a] [Telemetry Standards for Guided 1957] [Templeton et al. 1976] [Lee 2007b] [Tong et al. 2026b] [Tso and Lobbia 1986] [Turetsky and Glizer 2004] [Tuzlukov 2026a] [Tuzlukov 2026b] [Uricchio 1990] [Vavdiya and Kaushik 2022] [Vergez 1982] [Vergez and McClendon 1982] [Vinoth et al. 2009] [Vishwanath 2023] [VlNH 1964] [Walter et al. 2013] [Walter et al. 2014] [Walters 1959] [Wan et al. 2018] [Wang 1991] [Wang and Chen 2021] [Wang and Gao 2012] [Wang and Liu 2013] [Wang et al. 2021b] [Wang et al. 2022c] [Wang et al. 2023d] [Wang Xiaofang and Lin Hai 2010] [Wang Yandong 2011] [Webb 1979] [weibing and Kuisheng 2006] [Weiss and Shima 2021] [Whiteman 2003] [Whiting and Jobe 1972] [Wiltse 1955] [Woodward 1961] [Wu and Wang 2025] [Wu Qiang et al. 2009] [Shuang 2024] [Xu et al. 2016] [Xu et al. 2024c] [Xu Mingliang et al. 2010] [Yamasaki et al. 2011] [Yamasaki et al. 2013] [Yan and Jiang 2010] [Yang and Wang 2019] [Yang et al. 2022] [Yanushevsky 2007a] [Yanushevsky 2007b] [Yanushevsky 2018h] [Yanushevsky 2018c] [Yanushevsky 2018i] [Yanushevsky 2018b] [Yanushevsky 2018a] [Yoo and Bullock 1989] [Yu et al. 2015b] [Yu et al. 2017] [Yu et al. 2019] [Yueh and Lin 1985] [Zaeim et al. 2010] [Zaikang and Defu 2019b] [Zaikang and Defu 2019a] [Zarchan 1977] [Zarchan 1979] [Zarchan 2012b] [Zavodskikh and Kupryashkin 2021] [Zhang 2007] [Zhang 2009] [Zhang and Guo 2012] [Zhang et al. 2006b] [Zhang et al. 2019b] [Zhang et al. 2022b] [Zhang et al. 2024c] [Zhang Gang et al. 2012] [Zhao and Chen 2022] [Zhao Dawei et al] [Zhao et al. 2019] [Zhao et al. 2025b] [Zheng et al. 2018] [Zheng et al. 2022] [Zhu et al. 2014] [Ünal 2024]

Supersonic drag, skin friction and aerodynamic heating

The friction, wave drag and heating the airframe meets. Compressible turbulent skin friction and its measurement and reduction, the wave and base drag of slender bodies, and aerodynamic heating from the transient of a thin skin to the stagnation region of a glide vehicle. 84 titles name skin friction, with a median year of 1977, and 116 name aerodynamic heating.

337 records. [Abraham et al. 2024] [Acharya et al. 1978] [Acheson and Rothnie 2009] [Adcock et al. 1966] [Fletcher 1978] [Aerodynamic Heating for Gaps 1981] [Aerodynamic Heating 1979] [Al-Obaidi 2011] [Alexander 1970] [Allen 1970] [Allen and Czarnecki 1965] [Allen and Monta 1965] [Aman Prakash et al. 2024] [Amico and Cafiero 2026] [Atay and Kumartaslioglu 2024] [Avery et al. 1983] [Andrey 2011] [Babish 1966] [Balusamy et al. 2024] [Barnwell 1989] [Barnwell and Wahls 1991] [Bashkin et al. 2005] [Basin et al. 1959] [Beck 1984b] [Beck 1984a] [Bertin and Goodrich 1980] [Bhat and Lind 2009] [Biblarz et al. 1998] [Bland and Collie 1961] [Boison 1953] [Borzov et al. 1992] [Bradshaw 1977] [Brazzel 1963] [Brunner and Nerem 1971] [Bryson and Edwards 1952] [Budiansky and Mayers 1956] [Bushnell 1990] [Candler and Kelley 1999] [Carmel et al. 1958] [Cary and Hefner 1971] [Cary and Hefner 1972] [Chakravarty and Narayanaswamy 2024] [Chakravarty et al. 2024] [Chang 1992] [Chapman and Kester 1953] [Chien 1974] [Chin 1977] [Chin 1978] [Chou and Smith 1974] [Clark and Reel 1973] [Coleburn and Drimmer 1961] [Coleburn and Drimmer 1962] [Coles 1952] [Compressible Turbulent Boundary Layers 1969] [Craig and Reich 1981] [Czarnecki et al. 1965] [Dafang et al. 2010] [Daryabeigi 2001] [Das et al. 2023] [Dayman and Kurtz 1968] [Dejarnette 1983] [Dejarnette et al. 1985] [Derose 1971] [Dershin et al. 1967] [Dhawan 1953] [Dixon and Hunsaker 2023] [Dorrance 1961] [Driftmyer 1988] [Drougge 1990] [Duan and Choudhari 2012] [Duan and Choudhari 2014] [Duda 2016] [Durston and Stonum 1987] [Dwyer et al. 1971] [Eastman 1993] [Effect of Uniformly Distributed 1959] [Effects of Aerodynamic Heating 1980] [Eftekhari et al. 2025] [Eggers et al. 1957] [Elfstrom et al. 1982] [Elliott 1966] [Eremeitsev and Pilyugin 1984] [Eremeitsev and Pilyugin 1986] [Eremenko et al. 2003] [Fang et al. 2003] [Fernando et al. 1989] [Flanagan 1993] [Follé 1983] [Fomin et al. 2009] [Friedman 1951] [Fujii and Inoue 1998b] [Fujii and Inoue 1998a] [Fujii et al. 2000] [Fujita and Abe 2000] [Georgievskiy and Levin 2019] [Georgievskiy and Levin 2022] [Goddard 1957] [Goddard 1959] [Gomez et al. 2009] [Gonzalez and Elias 1978] [Goto et al. 2007] [Goto et al. 2021] [Goyne et al. 1998] [Gray 1965] [Gros 1963] [Groutage 1977] [Guan 2013] [Guo et al. 2025b] [Gupta et al. 1997] [Guy et al. 2001] [Gözükara and Ceylan 2024] [Hahn 1969] [Haines and Wood 1987] [Han 1960] [Han et al. 2022] [Harri 1964] [Harris and Davidson 1961] [Harris and Davidson 1962] [Hayashi and Aso 2003] [Hebbar and Paranjpe 1969] [Hender 1982] [Hershey and Vibrane 1961] [Higgins and Pappas 1951] [High and Bowman 1995] [Hill 1978] [Hingst and Towne 1974] [Holden 1984] [Holifield and Tufts 2024] [Hopkins 1969] [Hopkins and Inouye 1971] [Hopkins and Keener 1966] [Hopkins and Keener 1972] [Horstman et al. 1978] [Howerton et al. 2024] [Hozumi et al. 2001] [Hu et al. 2026a] [Hubner and Carroll 1993] [Huerta 1969] [Hung and Scottoline 1975] [Hunziker 1960] [Huston et al. 1948] [Hwang 1999] [Hwang 2000] [Influence of Corrugation-Roughness Shape 1980] [Isakson 1957] [Iwakawa et al. 2013] [Jassim 2017] [Jo 2026] [Joarder 2018] [Jonas 1953] [Jones and Richie 1974] [Joshi et al. 2024b] [Joshi et al. 2024a] [Joshi et al. 2025] [Jumper 1983] [Kaye and Yeh 1955] [Keel 1977] [Kennelly et al. 2000] [Khan et al. 2025] [Kianvashrad et al. 2018] [Kim 2026] [Kim and Kim 2026] [Kim et al. 2023a] [Kim et al. 2025] [Kinsler 1958] [Klimov et al. 1999] [Klunker and Ivey 1949] [Koike et al. 2018] [Komar 1966] [Kraiko and Tilliaeva 1973] [Kraiko and Tkalenko 1967] [Krause et al. 1991] [Kremeyer 2004] [Kremeyer and Pakhomov 2008] [Krieger 1980] [Kulfan 2008] [Kulfan 2009] [Kulkarni and Reddy 2009] [Lambert] [Lapshina and Ostapenko 2009] [Lee et al. 1969] [Leslie and Perry 1954] [Li and Eri 2007] [Li et al. 2009] [Li et al. 2017b] [Li et al. 2019d] [Liu 1967] [Liu et al. 2010b] [Liu et al. 2024g] [Liu et al. 2026b] [Lo 1948] [Lock 1957] [Lu et al. 2016] [Lu et al. 2025] [Luce 1949] [Mabey 1979] [Mabey and Gaudet 1975] [Machado 2008] [Machado 2018] [Maikapar 1959] [Maitra 2000] [Maklakov 2001] [Manzoor Hasan et al. 2024] [Maples 1979] [Maruyama et al. 2006] [Maruyama et al. 2009] [Masek et al. 1973] [Mashburn 1969] [Matting and Chapman 1958] [McAnally and Engel 1979] [Menssen 2026] [Meyer 1938] [Meyer 1959] [Miele 1957] [Miele 1958] [Miles and Macheret 2004] [Miner and Lewis 1972] [Miner and Lewis 1973] [Mironov and Serdyuk 2012] [Monta and Peterson 1966] [Motallebi 1994] [Murphy 1967] [Murray and Lewis 1975] [Myrabo et al. 2004] [Nakamura et al. 2014] [Naohiko et al. 2016] [Neely et al. 2003] [Negaard 1979] [Neumann and Freeman 2012] [Neumann et al. 1978] [Noffz and Curry 1991] [Nonequilibrium Stagnation Region Aerodynamic 1975] [Novean et al. 1997] [Oktay and Asma 2000] [Omori 1973a] [Owen and Bellhouse 1970] [Sahbon et al. 2023] [Spiridakos et al. 2020] [Pan et al. 2010] [Pappas 1954] [Parker 1955] [Patel et al. 2011] [Pish et al. 2019] [Prescott 1963] [Puckett 1946] [Pulliam et al] [Rafla 2019] [Raju et al. 1978] [Rallabhandi and Mavris 2003] [Rand 1963] [Readshaw 1961] [Reda 1977] [Reda 1978] [Reda et al. 1974] [Reda et al. 1975] [Riggins et al. 1998] [Riley and Dejarnette 1992] [Rosner and Cibrian 1974] [Rubesin et al. 1951] [Rumsey and Lee 1958] [Sahu 1986] [Sakarya 2017] [Sambamurthi et al. 1989] [Santos and Lewis 2003] [Sarwar et al. 2024] [Sasoh et al. 2009b] [Sasoh et al. 2009a] [Sasoh et al. 2010] [Sawyer 1977] [Schoeler 1987] [Scott et al. 1977] [Settles 1986] [Sheldon 1967] [Shih 1976] [Shimshi and Walberg 1993] [Shinichi et al. 2007] [Shuttle Eleven Cove Aerodynamic 1978] [Simeonides 2006] [Simsek et al. 2016] [Sklar and Rusak 2020] [Smith 2021] [Smith et al. 2002a] [Smits 1988] [Soloviev et al. 2001] [Soong and Chu 1983] [Spahr and Dickey 1951] [Squire 2000] [Srinivasan and Chamberlain 2004] [Srokowski et al. 1976] [Suchov et al. 2022] [Sundén and Fu 2017] [Sutton 2007] [Sutton et al. 1995] [Szajnecki et al. 2025] [Takahashi et al. 2013] [Takahashi et al. 2019] [Tamada et al. 2010] [Tang et al. 2015] [Tanno et al. 2001] [Tetervin 1963] [Thomas et al. 2022] [Thompson 1970] [Thornton 1981] [Token 1974] [Trifu and Savu 1993] [Tsuru et al. 2011] [Tucker 1950] [Venukumar et al. 2006] [Vigdorovich 2025] [Voisinet 1979] [Walker 1955] [Wang 1993] [Wang et al. 2013c] [Wang et al. 2017b] [Wang et al. 2019f] [Wang et al. 2024i] [Wazzan and Ball 1965] [White 1993] [White and Christoph 1972] [Wideman et al. 1994] [Wideman et al. 1995] [Wing 1970] [Wing 1973] [Wu et al. 2013b] [Wu et al. 2014b] [Xia et al. 2025] [Xu et al. 2022a] [Yakubayev et al. 2026] [Yisheng 2013] [Yoshida 2009] [Young 1965] [Zeng et al. 2024] [Zhao et al. 2009] [Zhao et al. 2022] [Zhou 2018] [Zhu et al. 2026a] [Zien and Ragsdale 1979]

Air launch, store separation and release

The launch aircraft’s half of the weapon. Store separation and its prediction, weapons bay cavity flow and acoustics, release mechanisms, and the air launch of missiles, targets and space boosters. 134 titles name store separation or store release, and 70 name a weapons bay or a cavity, none of them dated before 1975, which is the internal carriage the trapeze avoided by lowering the missile clear of the bay.

306 records. [Acuff and Bui 2015] [Ahmad et al. 1993] [Ahuja 2026] [Ahuja et al. 2025] [Aircraft Store Separation Motion 1980] [Aleksandrovich and Nikolayevich 2020] [Allee 1980] [Anandhanarayanan et al. 2013] [Anderson and Lopata 1996] [Arunajatesan et al. 2009] [Atwood 1993] [Atwood 1994] [Atwood 1995] [Babcock 2007] [Bacci and Saddington 2022] [Bacci and Saddington 2024] [Bacci and Saddington 2026] [Baugher and Gaitonde 2023] [Baysal 1986] [Baysal 1991] [Baysal 1995] [Ben-Gida 2022] [Ben-Gida 2023b] [Ben-Gida 2023a] [Berglind and Tysell 2010] [Berglind and Tysell 2011] [Billingsley et al. 1979] [Binkley and Vanderwyst 2012] [Black 1968] [Black 1969] [Black and Picklesimer 1971] [Blackburn and George 1964] [Blair and Stallings 1988] [Blakeley and Diamond 1991] [Bolster and Googins 1967] [Bonometti and Sorensen 2006] [Brooks 1971] [Budd 2015] [Budd 2018] [Budd and Jensen 2015] [Budd and Monheim 2015] [Budd and Webb 2016] [Bui et al. 2006] [Burton et al. 2007] [Butler et al. 1991] [Cai et al. 2023] [Cain et al. 1999] [Campbell 2024] [Carlson et al. 1995] [Carriage and Launch Characteristics 1994] [Carter 2012] [Carter and Lind 2012b] [Carter and Lind 2012a] [Cattafesta et al. 1999] [Cavallo et al. 1999] [Cenko 1994] [Cenko 2009] [Cenko 2018] [Cenko 2025] [Cenko and Lutton 2000] [Cenko et al. 1995] [Chakravarthy and Szema 1991] [Chan and Zhu 1999] [Chao et al. 1993] [Chaplin and Birch 2012] [Chapman 1998] [Chapter One 2018] [Charlton and Davis 2008] [Cheng et al. 2023] [Cherkauer et al. 2025] [Ching 2000] [Chow and Marconi 1989] [Clark 1975] [Coley 2024] [Coley and Lofthouse 2012] [Coogan and Musgrove 2017] [Corda et al. 2018] [Cougherty et al. 1985] [Cuffe and Limerick 1983] [Cui et al. 2021] [Fanggidae and Kusumahardi 2025] [Das et al. 2025] [Das et al. 2026] [Davids and Cenko 2001] [Davis and Welterlen 2003] [Davis et al. 2009] [Debasis Chakraborty 2023] [Delurgio et al. 1981] [Demir 2018] [Deslandes and Seifert 2000] [Doig et al. 2013] [Donahue 2001] [Doolan 2006] [Dougherty and Kuan 1989] [Dung 2025] [Dunworth et al. 2005] [Edefur et al. 2007] [Edge et al. 1999] [Feaux et al. 1989] [Finney 2010] [Fleeman and Donatelli 1981] [Flight Engine Performance Evaluation 1977] [Flora et al. 2013] [Flora et al. 2014] [Freeman] [Freeman and Jolly 2004] [Gao et al. 2017b] [Ge et al. 2025] [Gong and Wang 2019] [Gonzalez-Martino et al. 2023] [Goodwin et al. 1971] [Goodwin et al. 1972] [Graves and Robins 1979] [Guo et al. 2024] [Hale et al. 2026] [Hallberg and Godiksen 2007] [Hampsten 1996] [Harding and Barton 2007] [Harish et al. 2006] [Harmon and Ward 1990] [Heilig 1979] [Hendrick and Saint-Mard 1999] [High Speed Video System 2019] [Hildebrand 1979] [Hoffren and Salminen 1999] [Howitt and Platts 2002] [Hoyt 2006] [Huang and Giacobello 2022] [Hudson 2005] [Jenkins 1982] [Johnson et al. 2008] [Jolly and Coley 2026] [Jordan et al. 1997] [Joshi et al. 2023] [Katukuri 2023] [Kaykayoglu 1996] [Keen 2006] [Kelly et al. 2017] [Kim et al. 2015a] [Kohiyar et al. 1992] [Kohli et al] [Kraft and Lofthouse 2011] [Kugler 2007] [Lackey et al. 2011] [Lantagne et al] [Lasek and Sibilski 2002] [Lawrence and Fensky 1996] [Lawson and Barakos 2010] [Le et al. 2005] [Lee 2010] [Lee and Lua 2026] [Lee et al. 2004b] [Lee et al. 2011] [Leger 1975] [Lei and Zheng-yin 2016] [Lempert 1975] [Lengyel and Sosa 2021] [Lesieutre et al. 2002] [Lijewski and Lijewski 1997] [Lijewski and Suhs 1992] [Lindberg 1989] [Lohner and Baum 1991] [Lopez] [Loupy et al. 2018] [Lumb and Cayse 1992] [Lyu and Wang 2024] [Maddox 1980] [Mani et al] [Marcum 2001] [Marshall Selected to Convert 1992] [Martel] [Martineau et al. 1990] [McKinney and Polhamus 1966] [McKillip and Quackenbush 2015] [Mebarki et al. 2020] [Merrick and Reeder 2015] [Meyer et al. 1992] [Miller et al. 2018] [Mizrahi and Raveh 2018] [Mizukaki et al. 2019] [Moore and Moore 2011] [Moyer and Cenko 1994] [Moyer et al. 1995] [Naveed and Javed 2018] [Nenadić and Svorcan 2026] [Newberry and Badzey 1990] [Newman et al. 1992] [Nichols 2008] [Nichols and Westmoreland 2006] [Nichols and Westmoreland 2007] [Baysal et al. 1989] [Olejnik and Zalewski 2020] [Pace et al. 2008] [Paradise 1971] [Parkinson et al. 1995] [Pavacic 2013] [Pereira and Richardson 2023] [Peters et al. 2021] [Peters et al. 2022] [Peters et al. 2023] [Piersol 1977] [Poth et al. 1993] [Qamar and Cheok 2023] [Rafique and LinShu 2009] [Rafique et al. 2009a] [Rafique et al. 2009b] [Rafique et al. 2010b] [Rafique et al. 2010a] [Rafique et al. 2014] [Raisinghani and Rao 1983] [Raisinghani and Rao 1984] [Ray 2000] [Recording Store Separation Safe 2022] [Reed and Curry 1969] [Rigby 2013] [Rizk et al. 2002] [Rokita et al. 2012] [Roland et al. 2016] [Rollstin 1986] [Rovner 1991] [Ryan 1966] [Sainio and Krandel 1993] [Salt 2014] [Salt 2015] [Sarigul-Klijn et al. 2005] [Sarigul-Klijn et al. 2006] [Sarigulklijn et al. 2012] [Savery and Coder 2024] [Sawyer et al. 1989] [Schade 2013] [Seiner et al. 2008] [Seo et al. 2023] [Shalaev et al. 2003] [Shanks and Ahmad 1991] [Shaw and McGrath 1996] [Shaw and Smith 1977] [Shaw et al. 1987] [Shaw et al. 1988] [Sheta et al. 2015] [Si and Wang 2010] [Sickles et al. 2007] [Sickles et al. 2008] [Simulation of Store Separation 2014] [Sinha and Garg 2018] [Sinha et al. 2000] [Sinha et al. 2001] [Sivrioglu and Basaran 2024] [Sivrioglu and Başaran 2025] [Smith et al. 2002b] [Snyder et al. 2003] [Snyder et al. 2010] [Sokolov 2016] [Son and Seo 2017] [Son et al. 2021] [Song 2021] [Song and Ai 2021] [Sorensen and Schafer 2001] [Sorrells et al. 1985] [Spahr 1974] [Spahr 1975] [Spinetti and Jolly 2008] [Stallings 1982] [Stallings 1983] [Stanek 2002] [Stanek 2003] [Stanek 2007] [Stewart et al. 2024] [Stewart et al. 2026] [Stoykov 2022] [Svob and Bills 1982] [Tait et al. 2009] [Talbot and Moyer 1993] [Tembhurnikar et al. 2021] [Teng and Yu 2023] [Treece et al. 2024] [Vaddi et al. 2009] [Van Kesteren et al. 2014] [Verstraete et al. 2009] [Wang and Ma 2024] [Wang et al. 2022a] [Waters et al. 2013] [Wei and Gjestvang 2001] [Wei et al. 2018] [Welterlen 1999] [Welterlen 2000] [Wilcox 1990] [Wilcox 1991] [Wilcox 2001] [Wilcox et al. 1992] [Wolfe et al. 2024] [Wooden et al. 1998] [Xu et al. 2012] [Xue et al. 2019b] [Xue et al. 2020a] [Xue et al. 2020b] [Yang et al. 2011a] [Yao et al. 2025] [Yoo and Meade 2005] [Zhang and Zhang 2020] [zhang et al 2008] [Zhang et al. 2026d] [Zhao et al. 2023] [Zheng et al. 2013] [Zhu et al. 2018b] [Zhu et al. 2021] [Özgür et al. 2016]

Flight test, recovery and reliability

How a missile programme measures itself. Missile flight test programmes and ranges, range instrumentation, recovery parachutes and their supersonic deployment, and reliability demonstration with few or no failures. 131 titles name a parachute or a decelerator, and 76 name reliability.

306 records. [A Successful Program 1992] [A Supersonic Parachute 1949] [Adams 2014] [Air Force Life Cycle Mgmt Center Armament DIR 2013] [Akimov et al. 2021] [Allmen and Lu] [Amirkhizi et al. 2024] [Amos and Amos 1997] [An Integrated Missile Reliability 1984] [Anderson 1970] [Anderson and Watt 1971] [Angus 1986] [Approach to Reliability 1973] [Army Scientific Advisory Panel Washington Dc 1975b] [Army Scientific Advisory Panel Washington Dc 1975a] [As’ad et al. 2022] [As’ad et al. 2024] [Assessing Missile System Reliability 1972] [Balasubramanian and Shrivastava 2020] [Banerjee and Utreja 1975] [Barlog 1979] [Barnhardt et al. 2007] [Barr and Steeger 1957] [Behr 1989] [Belsterling 1965] [Benz et al. 2022] [Birkmire and Gallagher 2012] [Bleier et al. 2015] [Blumenthal and Denton 1962] [Blundell and Brashear 1962] [Boustani et al. 2019] [Boustani et al. 2020] [Boustani et al. 2022] [Bradley 1987] [Brandeau et al. 2015] [Brearley 1969] [Brooks and Dejarnette 1970] [Cadieux and Barad 2024] [Cadieux and Barad 2025] [Cadieux et al. 2023] [California Univ Regents Berkeley 2007] [Callaway 1963] [Callot 1981] [Capps 1957] [Chakoian 1969] [Charczenko 1962] [Cheng and Tam 2014] [Clark et al. 2015a] [Clemente 1958] [Coleman et al. 2026] [Colson and Thomas 1977] [Cone 1976] [Cunningham 1963] [Dahal et al. 2018b] [Dahal et al. 2018a] [Dahal et al. 2020] [Dai et al. 2006] [Dantas et al. 2022] [Dazer et al. 2021] [Dazer et al. 2022] [Demonstrated Reliability of Plastic-Encapsulated 1996] [Derkevorkian et al. 2019] [Dinh] [Doronin 2019] [Drynan] [Dugger 1982] [Eastman 1992] [Eckstrom 1975] [Ericksen et al. 1966] [Ericksen et al. 1984] [Facinelli and Nicks 1995] [Fan and Chang 2009] [Fan et al. 2022] [Fernández 2011] [Fetner 1961] [Fine et al. 1965] [Fine et al. 1966] [Freese et al. 1978] [French 1967] [French 1979] [French 1980] [French 1988] [Fukiba et al. 2023] [Gal 1974] [Gallon and Witkowski 2015] [Gallon et al. 2013] [Gaver and Jacobs 1997] [General Dynamics/Astronautics San Diego Ca 1961] [General Dynamics/Astronautics San Diego Ca 1962] [General Dynamics/Astronautics San Diegoca 1961] [Goswami et al. 2020] [Grundler and Dazer 2023] [Grundler and Dazer 2024] [Grundler et al. 2021] [Gruntman 2019] [Guo et al. 2011] [Guruswamy 2025] [Głębocki and Jacewicz 2020] [Hale 1978] [Han et al. 2014a] [Han et al. 2021b] [Hayslett et al. 1978] [Heinrich 1966] [Henke and Nerem 1968] [Hermite and Lefebvre 2019] [Hesse and Boyer 1962] [Hicks and Greenberg 1981] [Higgins and Speelman 1973] [Hinada et al. 1991] [Hiraki et al. 1997] [Holst and Rogers 1983] [Hu et al. 2020] [Hubbard 1983] [Hunt 2011] [Hunt and Wester 2013] [Interval Estimation of MTBF 1987] [Jamison 1966] [Jamison 1967] [Janda et al. 2013] [Jann 2015] [Jarmark 1986] [Jasztal and Kłosiński 2024] [Johnson and Matthews 1978] [Jones 1959b] [Just 1991] [Kain et al. 1978] [Karelahti et al. 2006a] [Karlgaard et al. 2018] [Karlgaard et al. 2019] [Kartchner 1963] [Kasouf and Weiss] [Kemmner] [Keuper 1960] [Kikumoto et al. 1998] [Kleckner 1946] [Kleyner and Elmore 2023] [Kleyner et al. 2015] [Kou and Zhan 2022] [Krasich 2004] [Krasich 2010] [Krieger 1983] [Krieger 1984] [Krolo and Bertsche] [Kumar et al. 2023b] [Lee Kingsley 1967] [Leopold 2022] [Leopold 2023] [Lewitschnig and Fanzott 2019] [Lin 1986] [Lingard and Darley 2005] [Lingard et al. 2013] [Lingard et al. 2017] [Liu et al. 2023e] [Lorenz and Lam 2026] [Lu and Rudy 2001] [Lyalin and Morozov 2005] [MacCarthy 1954] [Magill and Wehe 2002] [Malik 1976b] [Malik 1976a] [Martz and Waller 1976] [Maupin] [McGehee 1979] [McLendon and Baumann 1983] [Mettler and Towner] [Meyer 1958] [Miller et al. 2014] [Ming-Wei Lu and Rudy 2001] [Mingxiao Jiang and Dummer 2009] [Montanez and Pantano 2026] [Montgomery and Conard 1980] [Moog 1975] [Moyer 1963] [Murakami] [Nash 1981] [Nash 1990] [Neelans 1986] [Nelsen 1995] [Newirth and Bosco 1980] [Nie et al. 2023a] [Nie et al. 2023b] [Noble 1963] [Noh 2024] [O’Farrell et al. 2018] [Operational Base Missile Test 2021] [Ouyang and Zhang 2026] [Ouyang et al. 2026] [Pedersen 1961] [Pell et al. 1977] [Pepper 1967] [Pepper and Cronin 1969] [Pepper et al. 1984] [Peterson et al. 1986] [Placco 2023] [Podoprelov et al. 2021] [Potvin and Potvin 1997] [Potvin et al. 1997] [Purvis 1983] [Purvis 1984] [Qiu et al. 2021] [Rabinovitch et al. 2018] [Rabinovitch et al. 2019a] [Rabinovitch et al. 2019b] [Reliability Demonstration Test 1991] [Roelke et al. 2025] [Roloff 1957] [Rowlandson and Herlihy 1969] [Ryu et al. 2022] [Scott et al. 1983] [Shankar et al. 2018] [Shi et al. 2022] [Shrivastava 2026] [Shun-Wen Cheng] [Shyu and Hsiao 2014] [Sibol 1979] [Silbert et al. 1986] [Sims 1963] [Skarman 1978] [Slivinsky et al. 1995] [Sobel 1963] [Sobel 2015] [Sobel and Cloutier 1992] [Solberg 1993] [Soms 1988] [Sonneveldt et al. 2019] [Speelman 1975] [Speelman 1977] [Sprint Missile Subsystem Reliability 1977] [Steltzner et al. 2003] [Stewart 2013] [Sun et al. 2012b] [Sun et al. 2012c] [Sundberg 1975] [Taguchi et al. 2021] [Tai et al. 2023b] [Tai et al. 2023a] [Takabayashi et al. 2019] [Tang et al. 2021] [Test Range Instrumentation 1996] [Thakur et al. 2019] [Thang 2025] [The Fallacious Reliability Demonstration 1980] [Thomas and Thomas 2008] [Tiaden and Yakimenko 2008] [To] [National Renewable Energy Laboratory (NREL), Golden, CO. 2000] [Twinting and Sponable 1981] [Novikov 2023] [Astrakhov 2016] [Valenzuela et al. 2019] [Vishnyak 1995] [Hiền et al. 2022] [Waller 1977] [Wang 1999] [Wang 2017] [Wang et al. 2019g] [Wang et al. 2020] [Wang et al. 2021c] [Wang et al. 2022k] [Ward and Myers 1967] [Waye 1991] [Wernet et al. 2009] [West 1954] [Whalley 1973] [Whalley 2024] [White Sands Missile Range Nm 1997] [White Sands Missile Range Nm 2002] [Williams and Pohl] [Wilson and Farrow 2018] [Wilson and Farrow 2021] [Witkowski 1999] [Witkowski et al. 2009] [Witkowski et al. 2022] [Wolf and Fallon 2011] [Wu 2009] [Wu et al. 2013a] [Wu et al. 2024a] [Wyllie 2001] [Xingqiong and Lin 2009] [Xu and Feng 2018] [Xu et al. 2011] [Xu et al. 2025b] [Xue et al. 2015a] [Xue et al. 2015b] [Xue et al. 2019c] [Yadav et al. 2006] [Yang 2013] [Xue 2021] [Yang et al. 2018b] [Yang et al. 2019a] [Yang et al. 2020c] [Yasumura and Kitamura 2021] [Ye et al. 2026] [Yoon et al. 2025a] [Yu et al. 2025a] [Yuan et al. 2021] [Yusheng et al. 2009] [Zero-Failure Reliability Demonstration 2022] [Zhang 2003] [Zhang and Gao 2018] [Zhang et al. 2023e] [Zhang et al. 2023f] [Zhang et al. 2024b] [Zhang et al. 2025b] [Zhang et al. 2026e] [Zheng et al. 2023]

Boost-glide successors, interception and defence

Where the standoff mission went. Boost-glide and hypersonic glide vehicles, their trajectories, guidance, control and tracking, and the interception and defence problem from both sides. 103 of these titles name a glide, and 96 of the 103 dated ones are from 2010 or later.

242 records. [Acton 2015] [Air Force Armament Lab Eglin AFB FL 1988] [Almeida 2021] [Anderson 1958] [Ashford 1965] [Autenrieb and Gruhn 2025] [Autenrieb and Gruhn 2026] [Babish 1970] [Balakrishnan et al. 1997] [BALLISTIC MISSILE and AEROSPACE 1961] [Ballistic Missile Early Warning] [Stocker 2004] [Ballistic Missile Flight Testing 1981] [Barnett 1962] [Barr et al. 2026] [Bartusiak et al. 2022] [Barz 2026] [Berthelot et al. 2026] [Bin and Hongxin 2006] [Bittle and Plummer] [Bolender and Doman 2005] [Bolt 1981] [Bonavita et al. 2026] [Boylan et al. 2005] [Bozsóki 2014] [Burchett 2019] [Burns 2020] [Butler et al. 2022] [Butler et al. 2023] [Cai and Zhuang 2025] [Cai et al. 2026] [Cao and Wang 2026] [Carr et al. 2016] [Cheah et al. 2025] [Chen et al. 2020e] [Chen et al. 2020i] [Chen et al. 2021e] [Cheng and Lu 2023] [Cheng and Tsui 2022] [Chudej 1993] [Clark 1999] [Cliff and Kelley 1989] [Coffee and Maganty 1996] [Coupled Dynamic Model 2018] [Cruise Missiles] [Dai and Wang 2016] [Dalle et al. 2010] [Dalle et al. 2011] [Davis 1999] [Electrical Engineering, NIT, Agartala, India) and Debnath 2016] [Dendy et al. 2026] [Ding et al. 2024] [Djanal-Mann and Murugan 2025] [Dong et al. 2021b] [Dong et al. 2023a] [Dunbar and Silverman 1986] [Донской et al. 2021] [Falkiewicz et al. 2009] [Fan et al. 2017a] [Fang et al. 2024] [Faulkner 1961] [Faulkner and Ward 1961] [Fedaravičius et al. 2022] [Fei 2022] [Feng 2022] [Feng and Zhang 2016] [Feng et al. 2017] [Ficarrotta 2001] [Fiorentini et al. 2009] [First U.S. Missile Intercepts 2015] [Fontana and Di Lauro 2022] [Fowler] [Fowler 1998] [Froning et al. 1996] [Fu et al. 2024] [Gao et al. 2026b] [Garcia et al. 2014] [Garcia et al. 2015b] [Ge et al. 2018] [General Dynamics/Astronautics San Diego Ca 1964] [Gottlieb et al. 2024] [Grossman and Kul 2005] [Guo et al. 2023] [Hall 2003] [Halter and Cliff 1991] [Han et al. 2024a] [Hao and Yongqi 2024] [He et al. 2016] [He et al. 2017b] [Herman and Butler 1992] [Herrmann et al. 2025] [Hitt et al. 2013] [Holm-Hansen et al. 2010] [Hou et al. 2023] [Hoy 1989] [Hu and Liu 2013] [Huang and Li 2022] [Huang et al. 2018] [Huang et al. 2020] [Hull and Salguero 1994] [Hwang and Huh 2020] [Jaeger and Hemati 2025] [Jian-tao et al. 2009] [Jianguo et al. 2018] [Jin and Ma 2016] [Jin et al. 2021] [Jinchuan Hu et al. 2015] [Kamalvand et al. 2004] [Kashiwagi 1968] [Klimas and Kilikevičius 2025] [Knight et al. 2026] [Ko and Gong 2001] [Kou et al. 2014] [Krieger 1979] [Kumar et al. 1995b] [Kurilova and Li 2026] [Landers and Auman 2001] [Lazur et al. 1999] [Li 2021] [Li and Cui 2009] [Li and Fan 2018] [Li et al. 2014b] [Li et al. 2016b] [Li et al. 2026b] [Li et al. 2026f] [Linqi et al. 2015] [Liu et al. 2013a] [Liu et al. 2021] [Liu et al. 2023f] [Liu et al. 2024a] [Liu et al. 2025c] [Liu et al. 2026a] [Lock et al. 2025] [Lorenz et al. 1990] [Lv and Zhou 2023] [Mahmoud et al. 2017] [Maloney 2007] [Mason 2009] [Matheny and Smith 2026] [Melville and Helmich 2021] [Missile Defense Problem 2016] [Mori et al. 2002] [Narain 1991] [Nugroho et al. 2019] [O’Connor 1975] [Okuno and Watanabe 1992] [Olsen 2011] [Oppenheimer and Doman] [Pasqual and DeLaurentis 2012] [Pengyuan et al. 2014] [Pepper 1977] [Pepper 1979] [Pepper 1984] [Peri et al. 2023] [Peri et al. 2024] [Ping et al. 2017] [Ping Li et al. 2010] [Poulain et al. 2009] [Prakash and Singh 2021] [Priedhorsky and Wells 2026] [Qin et al. 2017] [Qiu et al. 2016] [Ragnoli et al. 2024] [Raivio and Ranta 2002] [Raney et al. 1993] [Rataczak et al. 2023] [Rataczak et al. 2024] [Reinhard et al. 1997] [Rizvi et al. 2017] [Rodi 2020] [Rodi 2021] [Rodi 2022] [Roth and Mavris 1999] [Scala and Nolan 1960] [Sethi 2025] [Shachar et al. 2025] [Shakiba and Serrani 2011] [Shekhawat and Sinha 2026] [Shi et al. 2012] [Shi et al. 2023] [Shima et al. 2000] [Shinar et al] [Singh et al. 2022] [Smirnov 2019] [Song et al. 2018] [Speyer et al. 1980] [Steinfeldt et al. 2013] [Stricker 1989] [Su et al. 2024] [Sun et al. 2025] [Tekin et al. 2013] [The Air Force Approach 1963] [Thongchua and Kaczmarek 1994] [Tracy and Wright 2020] [Villanueva and Abbas 2015] [Wang 2019] [Wang et al. 2024b] [Wang Zhi and Liu Zhi-ping 2010] [Waugh 1998] [Way et al. 2024] [Wei et al. 2026] [Weidong et al. 2015] [Weiguo et al. 2011] [Well 1990] [Wenfeng et al. 2017] [Werrell 1985b] [Wexler and Idan 2026] [Dukes 1962] [Williams et al. 2024] [Williamson et al. 2026] [Xie et al. 2021] [Xu et al. 2026b] [Yan and Wang 2012] [Yan et al. 2014] [Yanushevsky 2018j] [Yao et al. 2023] [Yonghua Tian et al. 2013] [Youssef et al. 2009] [Yu et al. 2015a] [Yu et al. 2022] [Yu Li and Nai-gang Cui 2008] [Yuan et al. 2026] [Zang et al. 2025] [Zhai and Yang 2020] [Zhang and Ding 2023] [Zhang and Du 2017] [Zhang and Tang 2012] [Zhang et al. 2011a] [Zhang et al. 2017f] [Zhang et al. 2017c] [Zhang et al. 2017d] [Zhang et al. 2022e] [Zhang et al. 2022d] [Zhang et al. 2023d] [Zhang et al. 2025a] [Zhao 2023] [Zhao and Hu 2011] [Zhongjie Meng et al. 2010] [Zhou et al. 2019b] [Zhou et al. 2026b] [Zope et al. 2026] [Ünal et al. 2025]

Command links, jamming and telemetry

The narrow link and its adversary. Anti-jam and low-probability-of-intercept signalling, the jamming of data links and seekers, command links and missile telemetry. 36 titles name jamming, and the earliest dated one is from 1991.

71 records. [A Missile Jamming 2025] [Bigelow et al. 1961] [Brito et al. 2019] [Bromberg and Progri] [Chen et al. 2019] [Jenila et al. 2023] [Chen 2009] [Chen et al. 2023b] [Choe et al. 2014] [Dai et al. 2009] [Dettbarn 1957] [Ding and Yi-Xuan 2012] [Ennis and Chuprun] [Fan et al. 2017b] [Fang et al. 2018] [Faulstich and Law 2006] [Filipovic and Dikic 2011] [Gosselin] [Gulliver and Felstead] [Han et al. 2021a] [Hao Xie et al. 2014] [He et al. 2014] [Hou 2024] [Kang et al. 2023a] [Keijer and Weiss 2005] [Kleider et al] [Lee 1985] [Lestage 2003] [Lim 1992] [Lowrie 1960b] [Ma et al. 2007] [Martel 2013] [McKee 1998] [Meng et al. 2023] [Mermagen 1964] [Milstein 1991] [Muehlner 1962] [Obi et al. 2022] [Otto 1993] [Park et al. 2021] [Peng et al. 2014] [Poberezhskiy and Poberezhskiy 2013] [Poehler 1961] [Rae 1961] [Rao et al. 2022] [Rauch 1957] [Ren et al. 2026] [Research on Anti-Jamming Transmission 2025] [Rice 1999] [Rice 2013] [Saglam and Yilmaz 2018] [Saliy et al. 2023] [Saratayon and Petchartee 2015] [Shao et al. 2017] [Shi et al. 2025a] [Tishchenko and Fedunov 2006] [Vujcic and Kachejian 2000] [Wang et al. 2016g] [Wei Sun and Amin] [Wenzhun et al. 2008] [Wright 2015] [Wright and Ruscus 1959] [Wu et al. 2021] [Wu et al. 2025b] [Xia 1999] [Xie et al. 2012] [Xu et al. 2022b] [Yanli et al. 2016] [Zhen and Baixiao 2019] [Zhong Ye et al] [Zoltowski 2000]

Weapon effectiveness, kill probability and lethal radius

What the accuracy buys. Single-shot kill probability, lethal radius and lethal area, damage functions, blast scaling and the vulnerability of targets. Kill probability is a subject of the 1950s and 1960s in these titles. 16 name it, and 11 of them are dated before 1970.

70 records. [Aguilar et al. 1969] [Ahmad 1993] [Almustafa and Nehdi 2020] [Andon 1965] [Bae et al. 2017] [Benson 1954] [Bhashyam and Singh 1967] [Braithwaite 1962] [Bruckart 1993] [Cameron Reed 2011] [Caraway and Randy R. 2001] [Catovic and Kljuno 2021] [Chusilp et al. 2014b] [Chusilp et al. 2014a] [Coulter 1982] [Cramer 1979] [Dai and Ray 1996] [Driels and Shin 2004] [Ehrenfeld 1959] [Fan et al. 2016] [Groves 1975] [Guo et al. 2017] [He et al. 2024a] [Heimbs et al. 2015] [Helfman et al. 1985] [Howe and McCree 1962] [Jia et al. 2023] [Jinzhao et al. 2024] [Jong Yil et al. 2014] [Juncosa and Young 1953] [Jung and Kim 2023] [Kim and Lee 2024] [Knapp 1965] [Kuroswiski et al. 2025] [Lee and Jeong 2025] [Leese 1966] [Li et al. 2025h] [Lilliefors 1957] [McNolty 1962] [McNolty 1965] [McNolty 1967] [Moon 2021] [Morton 1966] [Moskowitz 1965] [Murphy 1952] [Myers 1963] [Qi et al. 2021] [Radomski 1995] [Reches 1980] [Review on Effectiveness Evaluation 2021] [Russell 1962] [Schick 1977] [Singh and Bhashyam 1972] [Smith and Kinslow 1977] [Smith (e H) and Associates INC Sebastopol CA 1961] [Spahr 1987] [Stewart 2021] [Stiegler 1960] [Surzhikov 1999] [Temsah et al. 2021] [Timenes 1964] [Vulnerability of Quick-Reacting Sheltered 1959] [Waddell 1961] [Weidlinger 1962] [Yao and Ma 2017] [Zhang et al. 2009b] [Zhao et al. 2017] [Zhao Juanjuan 2016] [Zumwalt and Damkevala 1965] [Zumwalt and Tang 1964]

Accuracy, circular error and its estimation

The keystone statistic. The circular error probable and its estimators, radial and elliptical error distributions, bombing and weapon delivery accuracy, and the error budget. 22 titles name the circular error probable or the circular probable error, 6 of the dated ones before 1970 and 8 from 2010 or later.

68 records. [Jo 2007] [Anděl 1974] [Sandia Corp., Albuquerque, N. Mex. 1953] [Berger and Meyer 1974] [Black 2020] [Blaesild 1979] [Bodin and Zalgaller 1967] [Bossard and Pesek 1991] [Bunn 1993] [Calculating the CEP Circular 1987] [Carlson 1974] [Casasco et al. 2013] [Chaowanapreecha] [Chaowanapreecha et al. 2025] [Chevalier et al. 2017] [Chew and Boyce 1962] [Circular Normal Distribution 2014] [Circular Probable Error 2014] [Culpepper 1978] [Daniels 1952] [Day 2013] [DiDonato 2007] [Dougherty et al] [Error Budget 2018] [Estimated CEP of Weapon 1970] [Evans et al. 1985] [Gallagher 1969] [Irons and Landesberg 1981] [Jiao et al. 2024] [Kamat 1962] [Kelley 1923] [Kudriashov et al. 2018] [Leondes and Rankine 1972] [Liu et al. 2019d] [Lopez et al] [Ma et al. 2026] [Massoumnia 1991] [Maximum Likelihood Estimation 2009] [Meidunas 2008] [Moranda 1959] [Moranda 1960] [Nelson 1988b] [Papp and Rožnjik 2022] [Pearl 1908a] [Pearl 1908b] [Peng et al. 2016] [Schulte and Dickinson 1968] [Shandling and Platus 1985] [Shandling and Platus 1986] [Shipplett 1983] [Shultz 1963] [Singh 1962] [Singh 1970] [Siuru 1987] [Stewart et al. 2016] [Stoykov and Atanasov 2016] [Strohm 2013] [Student 1908] [Swanson 1963] [Thurston 1965] [Vathsal] [Vathsal 1994] [Wright 1882] [Zhang and An 2012] [Zhang et al. 2012a] [Zhou et al. 2014] [Zimmer and Turner 2017] [Zimmer et al. 2016]

Other guided-missile and flight literature

The residual, reported and not hidden. Missile and rocket literature that belongs to no other cluster, including the programme’s own RASCAL and Shrike documents, general missile design, launchers and canisters, flight simulation and handbooks.

165 records. [Aircraft and Missile Impact] [Allen et al. 1989] [Alongi 1966] [Apostol et al. 2013] [Army Missile Command Redstone Arsenal AL 1961] [Army Missile Command Redstone Arsenal AL 1963] [Athearn 2015] [Atygayev et al. 2022] [Bagley and Billions 1963b] [Bagley and Billions 1963a] [Bakeman 1962] [Balasubramanian et al. 2013] [Bell Aerospace Co Buffalo Ny 1956] [Bell Aerospace Co Buffalo Ny 1953] [Bell Aerospace Co Buffalo Ny 1954] [Bell Aerospace Co Buffalo Ny 1955] [Bhattacharya 1997] [Bishop 1977] [Bishop 1991] [Training Camp and Surface-to-Air Firing Range et al. 2017] [Bott 1997] [Bowman and Speyer 1987] [Brower 1959] [Bulbeck et al. 2000] [Bullard 1965] [Cagle 1977] [Cappellucci and Schinnerer 1986] [Carr and Cobb 2017] [Chaoqi et al. 2018] [Chhavi and Ramanan 2023] [Chireau 1966] [Choi and Jung 2019] [Church and Taylor 1959] [Clark and McLamb 1983] [Cole 1996] [Coletta et al. 1964] [Concept Analysis Corp Plymouth Mi 1989] [Corriveau et al. 2006] [Cox 1957] [Cui et al. 2013] [Dang et al. 2023] [Dobyns and McCarthy 1990] [Doro-on 2022] [Dorres 1972] [Dow 2001] [Dynamic Design Technology 2011] [Ehricke 1955] [Elliott et al. 2025] [Ellis 2013] [Ewing 1994] [Fang et al. 2023] [Farlik 2015] [Giragosian 1992] [Golodjaev 2014] [Gross 1987] [Głębocki and Jacewicz 2018] [Haber 1995] [Haglund et al. 1978] [Hague and Levin 1979] [Hammer and Elswick 1966] [Haynes 2008] [Hoefener and Stone 1981] [Holliday 1989] [Howard 1984] [Hui et al. 2015] [Human 2001] [Hwang] [Imado et al. 1989] [Integrated Missile Design 2007] [Jeler 2025] [Jiang 2024] [Johnson 2015] [Kaplan et al. 1994] [Keller 1982b] [Keller 1982a] [Kelly and Arnold, I 1995] [Kim et al. 2016a] [Knaack 1978] [Knaack 1988] [Krahmann 2017] [Ladner 2016] [Lee 1993] [Li et al. 2016c] [Lillard et al. 1997] [Lilov 1962] [Liu and Bailey 2002] [Liu et al. 2010a] [Liu Jinrong et al. 2009] [Xiao et al. 2012] [MacLaren and Walkup 1964] [Maddux 1999] [Mandt and Neighbor 1982] [McGowan et al. 2012] [McNicholl et al. 1988a] [McNicholl et al. 1988b] [Merchant 1961] [Mermagen and Murphy 2001] [Miguel 1974] [Minor] [Missile Attack Warning 2007] [Mulanax 1967] [Murphy 1972] [Murphy and Mermagen 2000] [Naylor 1961] [Neuman 1988] [Nygaard 2003] [Oshman and Arad 2001] [Oshman and Arad 2004] [Philipson 1995] [Phillips 1993] [Platus 1998] [Pollin 1973] [Priolo et al. 1991] [RAM Growth 1987] [Kuti-Mensah and Kyei 2026] [Romero 2015] [Rush 1973] [Salazar and Kintner 1981] [Schmitt 2004] [Shaw Y. Ong and Pierson] [Shi et al. 2018b] [Shi et al. 2021c] [Shinar and Tabak 1994] [Shnidman 1975] [Singh and Ghosh 2006] [Smyth 1972] [Solis 1983] [Sparta INC Huntsville AL 1992] [Spearman 1984] [Stippes 1962] [Strategic Missiles] [Sturek and Taylor 2000] [Sturek and Malcolm S. 2001] [Su Lide et al. 2011] [The Air Force Strategic 2002] [the Longitudinal Motion of 1953] [Tongmual and Yonwilad 2025] [Toomey 1983] [Topbaş et al. 2024] [Townsend 2020] [Uselton and Jenke 1977] [Van Der Maas 1962] [Vaughn and Auman 2002] [Vaughn and Auman 2003] [Verma et al. 2019] [Vertes et al. 1966] [Vichnyakova and Kukhtenko 1998] [Vishnyakova and Kukhtenko 1996] [Wang and Qin 2011] [Watkins 1946] [Wells 1981] [Willwerth 1962] [Witmer 1986] [Wood 1961] [Wrestler and Clifton G. 1965] [Xie et al. 2009] [Yang and Guohui 2019] [Yang and Wang 2012] [Yanushevsky 2018g] [Yi and Carlson 1975] [Yi et al. 2007] [Yoo et al. 2018] [Yoon et al. 2010] [Youngs and Bitinas 2010] [Zhang et al. 2023a]

Where the Framing Breaks Down

Treating the X-9 through an error budget is productive and it misleads in several ways.

The X-9 is not an X-plane in the sense the series began with. It is a subscale development article for a weapon, designated retrospectively in 1951 [Parsch 2002], and the designation carries no research content that the RTV-A-4 label did not.

The accuracy framing overstates what the vehicle was for. The programme’s stated objectives included checkout and launch procedures, crew training, and deployment experience, none of which reduce to a variance, and the programme’s history lists them among its purposes [GAM-63 RASCAL].

A testbed cannot be evaluated independently of its weapon. The X-9 succeeded and the RASCAL was cancelled [GAM-63 RASCAL], and any account that treats the first fact without the second is telling half of it.

The two-architecture argument is cleaner in retrospect than it was at the time. This article derives the launcher-guided range limit from a beamwidth and asserts that it explains the programme’s shape. The record does not show anyone making that calculation, and the inference is the author’s.

The Source Base

The survey rests on 6,105 research records assembled from Crossref, the NASA Technical Reports Server and the Defense Technical Information Center, of which 969 are report primaries, being 15.9 percent, by the identifier rule set out under The Definition of Primary. 5,868 of the records carry a year, with a median of 2008, and 36.8 percent of those are from 2015 or later. The programme’s own documents are primaries by that rule Bell Aerospace Co Buffalo Ny 1953 Bell Aerospace Co Buffalo Ny 1954 Bell Aerospace Co Buffalo Ny 1956, and so are the NACA rocket-model measurements of the configuration family Moul and Wineman 1952 Baber and Moul 1955.

The archival situation is the reverse of the X-8’s and it is better.

A weapon programme reports to a service, and the service keeps the reports. The Defense Technical Information Center holds Bell’s own project documents, reachable by digital object identifier under a single publisher prefix, and they cover the Shrike and the RASCAL together as the programme itself did. The aerospace archive holds something different and equally useful, which is the independent NACA measurement of the configuration family the X-9 belonged to.

Neither archive holds much about the guidance system, which is the vehicle’s actual subject, and that is not an accident. Guidance was the classified part.

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 Bell project documents, the NACA rocket-model and airborne-simulator reports and the period studies of guidance architectures and guidance response are reached that way, so the rule counts them. The period journal papers on which the estimator and tracking-error arguments rest, in the Journal of the American Statistical Association and the Proceedings of the Institute of Radio Engineers, are not.

The rule does not reach the journal and conference literature of the American Institute of Aeronautics and Astronautics, abbreviated AIAA. 1,892 of the records carry its 10.2514 prefix, and among them are flight test and design papers written by the people who built the vehicles they describe. 15.9 percent is therefore a lower bound on how much of this survey is first-hand.

Thin Subjects

Ten 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 trapeze and the release mechanism	trapeze, displacement gear, release mechanism	1
the tip-off rate at release	tip off, tipoff	1
the data rate of the command link	data rate, bit rate	1
the crossover model of the human operator	crossover	4
the guidance time constant and the miss it leaves	time constant, guidance lag, autopilot lag	8
the division of thrust between two chambers	dual thrust, two chamber, twin chamber, dual chamber, multi chamber, sustainer, boost sustain	7
body bending against the autopilot	bending	2
the recovery temperature of the boundary layer	recovery temperature, recovery factor, adiabatic wall temperature	0
the transient temperature of a thin skin	skin temperature, transient temperature, thin skinned	6
the lethal radius	lethal radius, lethal area, lethal volume	6

The release is the thinnest subject of all, and what literature it has treats it as hardware. The one record on a release mechanism is Paradise 1971, the one on tip-off is Stippes 1962, and no title names a trapeze, so the release-error and tip-off arithmetic in Sizing From First Principles stands on the relations shown there.

The crossover model is thin because its vocabulary does not discriminate. Four titles carry the word. Three name the model, Jackson 1967, Jackson 1969 and Martinez-Garcia et al. 2017, and one, Smirnov 2019, uses it for the scattering of a radar target, while 92 titles in the human operator cluster describe manual control under other names. The guidance time constant is thin in the same way. Six of its eight records are modern guidance laws that compensate an autopilot lag, and the residual miss of a lagged loop is otherwise carried by the miss-distance titles of the guidance cluster.

The data rate of the command link appears in one title, Kleider et al, and that title concerns an anti-jam waveform, which is consistent with this article’s finding that capacity is not the difficulty of a command link. Dividing thrust between two chambers is a solid-motor subject in these titles. Three of its seven records name a single-chamber dual-thrust motor, Hu et al. 1994, Kwon 2020 and Yang et al. 2025a, and two concern liquid engines with more than one chamber, Tang et al. 2026 and Masyagin 2026, so the inference that the X-9’s second chamber existed to match cruise drag stands on the drag arithmetic, as the Epistemic State records.

Body bending against the autopilot has two records, Freed and Miller 1961 on damping bending modes for autopilot design and Kawiecki and Smith 1994 on an actuator that avoids structural coupling. The recovery temperature appears in no title, against 132 that name aerodynamic heating, because it is a textbook relation, and the transient of a thin skin has six records, among them Huston et al. 1948 and Lo 1948, which the heating section relies on. The lethal radius has six records, and the scaling of blast with yield that the founding irony rests on is carried by Morton 1966 and by the weapon-effects handbook the article cites.

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 accuracy of a command-guided, air-launched missile and everything the article dimensions to buy it, from the statistics of the circular error probable through the tracker, the operator, the guidance law, the autopilot, the airframe, the rocket and the launch, to the weapon effects that set the requirement and the successors that inherited the mission. The missile literature and the hypersonic glide literature are this article’s subject and are admitted.

Many words this subject depends on also name something else, and a record that shares only such a word is excluded. Probable error is also a statistic of correlation coefficients, Mendelian ratios, astronomical parallaxes and water clocks, and single shot also names a film, a laser pulse and an object detector. Operator also names a mathematical operator and the crossover operator of a genetic algorithm, and the operators of ships, mines and nuclear control rooms are not the operator of a weapon. Line-of-sight guidance also steers ships, hovercraft and robots along a path, and a guided-missile destroyer is a ship. A slender body also moves through the internal waves of the ocean, an aerodynamic balance is also a force-measuring instrument, and the transient heating of skin is also a subject of thermal medicine. Air launch also delivers balloons, sondes, sonobuoys and ground-penetrating radars, radar beacons and monopulse also serve air traffic control, and the guidance of spacecraft, landers and planetary probes is a different problem. The geology, hydrology and weather of the missile ranges are not missile testing, and the policy, strategy and diplomacy of missile defence are not its engineering. Correction and retraction notices, encyclopedia volumes, journal issues and subject indexes 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, a notice such as front matter, an editorial or a news item, and a second deposit of a document already counted are not admitted either, since none of them is a research work in its own right.

Some records of doubtful relevance are kept. Robot and manipulator teleoperation across a communication delay is kept because closing a loop across a variable delay is the problem the review above names as the modern form of the X-9’s link, and the allocation of functions between operators and automation in other vehicles is kept for the same operator-in-the-loop argument. Drift compensation for micro-machined and fibre-optic gyroscopes is kept as the instrument the autopilot section’s drift argument concerns, reliability demonstration outside missiles is kept as the construct the flight test record uses, and the recovery parachutes of capsules, boosters, aircraft and airdrop are kept as recovery technique. The flight control of air-breathing hypersonic vehicles, the hinge moments of aircraft control surfaces, the multi-target tracking filters of radar networks and the combustion of solid rocket motors each share a method with this subject and are kept, as are four records the article cites for a neighbouring point, a flutter study of a piezoelectric plate, a fault-tolerance study for aeroengines, a latency study of remote driving and a study of silos under blast. A reader may weigh each accordingly.

Because every title has been read, the off-topic share that remains is a matter of reading judgement. The largest class removed is missile policy, because the word missile also names a subject of strategy, diplomacy and arms control.

Epistemic State

Historical fact, well documented. The 15 July 1945 military characteristics and their 500 feet at 75 percent accuracy requirement. The MX-767 to MX-776 lineage and the MX-776A and MX-776B split. Bell’s May 1947 development contract and Dornberger’s leadership. The RTV-A-4 designation and its 1951 redesignation to X-9. The first glide drop in April 1949, the failed powered attempt in May 1950, the first full success on the fifth flight in November 1950, and the January 1953 conclusion. Thirty-one vehicles built. Trapeze launch from a modified EB-50D with radio command guidance. RASCAL cancellation in September 1958, which one directory gives as November.

Engineering analysis, computed here. The conversion of the accuracy requirement into an axis standard deviation of 91.5 metres and a circular error probable of 108 metres, the equal-share error budget, the radar cross-range resolution and the resulting launcher-guided range limit, the opposite error gradients of the two architectures, the operator crossover frequency, the airframe short-period frequency, the propellant load and burn time, the cruise-drag argument for two chambers, the air-launch energy credit, the glide ratio, the canard trim relations and the acceleration per degree, the release-error propagation, the separation time, the command link budget and data rate, the autopilot damping requirement, the recovery temperature and skin time constant, the canopy sizing, and the kill-probability inversion. Each depends on assumed values stated where they are used.

Inference, stated as such. That the launcher-guided range limit derived from a beamwidth explains the X-9’s demonstrated range is a correspondence between two numbers and not a documented rationale, and the period sources compare guidance architectures on tactical grounds without ever performing this calculation. That the two-chamber engine existed to match cruise drag is inferred from the arithmetic and not from a source. That the trapeze exists to remove release-condition variance rather than merely to provide clearance is inferred the same way. That it lowered the X-9 clear of the bay before release is inferred from the mechanism, since the sources consulted say only that the vehicle was launched from a trapeze in the bomb bay.

Not settled by the record consulted here.

The number of X-9 flights, given as twenty-two in one account and twenty-eight in the NASA inventory, against thirty-one built.

The maximum speed, given as greater than Mach 1.5 by one compilation and Mach 2.0 by another.

The specific impulse and burn time of the XLR65-BA-1, neither of which was located, so the propulsion figures here are derived from masses and an assumed specific impulse.

Whether the X-9 ever demonstrated the accuracy the specification demanded. No source consulted states a measured circular error probable, which for a vehicle whose keystone is accuracy is a substantial gap.

The division of work between the two thrust chambers, and whether the second was shut down in cruise as the drag arithmetic suggests.

Out of Scope

The GAM-63 RASCAL is treated only where it illuminates the X-9. Its development, its cancellation, and the air-launched ballistic missile programmes that displaced it are a larger subject.

The German V-1 air-launch experience and the JB-2 programme are context rather than subject.

The classified guidance hardware is not described because the accessible record does not describe it.

Sibling testbeds of the same era, including the Northrop MX-775 series, appear only by way of comparison.

Conclusion

The X-9 is the first vehicle in this series whose keystone is a control loop and whose specification is a probability.

Reading that specification as a variance makes the design legible. One hundred and eight metres of circular error at a hundred miles, decomposed across subsystems in quadrature, is what dimensions the guidance link, the autopilot, the release mechanism, and the propulsion repeatability. It is also what forbids the obvious architecture, because a radar in the launch aircraft resolves an angle, and an angle at a hundred miles is a quarter of a kilometre. Guiding from the launcher makes the error grow with the standoff that is the entire point of the weapon. Guiding from the missile makes it shrink on approach. The weapon that resulted was named for its guidance link, and the name is the correct one.

The vehicle around that argument is unremarkable and is meant to be. A canard cruciform missile at Mach 2 needs no exotic material, its aerodynamics were being measured independently by NACA in the same years, and its rocket delivers more impulse than the airframe can use. What it needed was to fly the same way twice, and the record’s shape, with eighteen months between the first drop and the first powered success and then a programme that stopped early because it was finished, is what a guidance programme looks like.

The founding irony is that the requirement was written one day before Trinity. Five hundred feet at seventy-five percent was specified before any nuclear weapon had been demonstrated, and the weapon that flew carried a warhead for which eight times that error would have sufficed. The accuracy work was mostly surplus to the mission and mostly useful to everything afterwards, which is a fair description of a great deal of research and is not a criticism.

Equations

This section collects the 115 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 115, 60 are established and 55 are bespoke. Quantities are in International System units, with the specification of 500 feet and 100 miles converted to metres, speeds at altitude taken from a speed of sound of 295 metres per second, and several symbols reused, so that $R$ is a radius, a range or a turn radius by section, $m$ is a mass except in Equations 59 to 61, where it is a miss distance, and $\tau$ is a delay in the guidance sections and a thermal time constant in Equations 103 and 104.

Equation 1, Rayleigh Distribution of Radial Miss. With independent normal errors of equal standard deviation $\sigma$ in range and deflection, the probability of landing within a radius $R$ follows the Rayleigh cumulative distribution. Rayleigh Papoulis and Pillai 2002 Probability, Random Variables and Stochastic Processes

\[P(R) = 1 - \exp\left( -\frac{R^{2}}{2\sigma^{2}} \right) \tag{1}\]

Equation 2, Axis Standard Deviation Required by the Specification. Inverting the Rayleigh distribution for the 1945 requirement of 500 feet at 75 percent gives an axis standard deviation of 91.5 metres. GAM-63 RASCAL

\[\sigma = \frac{R}{\sqrt{-2 \ln \left( 1 - P \right)}} = \frac{500 \times 0.3048}{\sqrt{2 \ln 4}} = \frac{152.4}{1.665} = 91.5 \, \text{m} \tag{2}\]

Equation 3, Circular Error Probable. The circular error probable, the radius containing half the impacts, is $\sqrt{2 \ln 2}$ times the axis standard deviation, which gives 108 metres for the specification. circular error probable

\[\mathrm{CEP} = \sigma \sqrt{2 \ln 2} = 1.177 \, \sigma = 108 \, \text{m} \tag{3}\]

Equation 4, Relative Standard Error of a Sample Standard Deviation. For $n$ samples from a normal population the standard error of the sample standard deviation, relative to the estimate, is approximately one over the square root of twice the degrees of freedom.

\[\frac{\sigma_{\hat{s}}}{s} \approx \frac{1}{\sqrt{2 \left( n-1 \right)}} \tag{4}\]

Equation 5, Maximum-Likelihood Axis Standard Deviation. Under the circular normal assumption the maximum-likelihood estimate of the axis standard deviation is the root of the summed squared radial misses divided by twice the number of impacts.

\[\hat{\sigma} = \sqrt{\frac{1}{2n} \sum_{i=1}^{n} r_i^{2}} \tag{5}\]

Equation 6, Root-Mean-Square Miss with a Bias. A systematic offset $b$ adds in quadrature to the random radial miss, whose mean square is twice the axis variance.

\[m_{\text{rms}} = \sqrt{b^{2} + 2 \sigma^{2}} \tag{6}\]

Equation 7, Quadrature Sum of Independent Errors. The variances of independent error sources add, so the total variance is the sum of the contributors’ variances.

\[\sigma_{\text{total}}^{2} = \sum_{i} \sigma_{i}^{2} \tag{7}\]

Equation 8, Bespoke Equal Error Allocation. Assuming that $n$ sources contribute equally, each is allotted the total standard deviation divided by the square root of $n$.

\[\sigma_i = \frac{\sigma_{\text{total}}}{\sqrt{n}} \tag{8}\]

Equation 9, Antenna Beamwidth. The angular beamwidth of an antenna is roughly the wavelength divided by the aperture. beamwidth Skolnik 2008 Radar Handbook

\[\theta \approx \frac{\lambda}{D} \tag{9}\]

Equation 10, Bespoke Cross-Range Tracking Error. The article models the cross-range error as the range times the beamwidth divided by a resolution factor $k$ that it treats as a constant of order twenty.

\[\varepsilon_{\perp} = \frac{R \, \theta}{k} = \frac{R \lambda}{k D} \tag{10}\]

Equation 11, Bespoke Tracking Error from the Launcher. The cross-range error at 100 miles is evaluated for an assumed X-band wavelength of 0.03 metres, a one metre antenna and a resolution factor of twenty.

\[\varepsilon_{\perp} = \frac{(1.6 \times 10^{5})(0.030)}{20} = 240 \, \text{m} \tag{11}\]

Equation 12, Bespoke Maximum Command-Guidance Range. Setting the cross-range error equal to the 91.5 metre budget gives the range limit of a launcher radar for the assumed antenna and resolution factor.

\[R_{\max} = \frac{k \, \sigma_{\text{total}} D}{\lambda} = \frac{(20)(91.5)(1.0)}{0.03} = 61 \, \text{km} \tag{12}\]

Equation 13, Bespoke Tracking Error of a Missile Seeker. The same error model applied to an assumed 0.4 metre seeker antenna at two kilometres from the target gives 7.5 metres.

\[\varepsilon_{\perp}(2 \, \text{km}) = \frac{(2 \times 10^{3})(0.075)}{20} = 7.5 \, \text{m} \tag{13}\]

Equation 14, Bespoke Opposite Error Gradients. Under the article’s error model the error of a launcher-based sensor grows with the range from the launcher and that of a missile-borne sensor with the range to the target.

\[\varepsilon_{\text{launcher}} \propto R_L, \qquad \varepsilon_{\text{missile}} \propto R_T \tag{14}\]

Equation 15, Monopulse Angle Error from Receiver Noise. The angular error of a monopulse tracker from thermal noise is the beamwidth divided by the monopulse slope and the square root of twice the signal-to-noise ratio. Barton 2004 Radar System Analysis and Modeling

\[\sigma_{\theta,\text{noise}} = \frac{\theta}{k_m \sqrt{2 \, (S/N)}} \tag{15}\]

Equation 16, Radar Range Equation. The power received from a target of cross-section $\sigma_t$ by a monostatic radar falls as the fourth power of range. Skolnik 2008 Radar Handbook

\[P_r = \frac{P_t G^{2} \lambda^{2} \sigma_t}{\left( 4\pi \right)^{3} R^{4}} \tag{16}\]

Equation 17, Signal-to-Noise Ratio of a Skin Return. With fixed noise the signal-to-noise ratio of a reflecting target scales as the inverse fourth power of range.

\[\frac{S}{N} \propto \frac{1}{R^{4}} \tag{17}\]

Equation 18, Received Power from a Beacon. A beacon of power $P_b$ and gain $G_b$ on the missile is received over a one-way path, so its power falls only as the square of range.

\[P_{r,\text{beacon}} = \frac{P_b G_b G \lambda^{2}}{\left( 4\pi R \right)^{2}} \tag{18}\]

Equation 19, Beacon to Skin Power Ratio. Dividing the beacon equation by the radar equation gives the advantage of a beacon, which grows as the square of range.

\[\frac{P_{r,\text{beacon}}}{P_{r,\text{skin}}} = \frac{P_b G_b \left( 4\pi \right) R^{2}}{P_t G \sigma_t} \tag{19}\]

Equation 20, Glint Angle Error. The apparent position of a target with several scattering centres wanders by a fraction $c_g$ of its angular extent, so the glint error falls as one over range. Delano 1953

\[\sigma_{\theta,\text{glint}} \approx \frac{c_g \, L_t}{R} \tag{20}\]

Equation 21, Bespoke Beam-Rider Error. The article models the lateral error of a beam rider as the beam width at the missile’s range divided by a sensing factor $k_b$ of order ten.

\[\varepsilon_{\text{beam}} = \frac{R \, \theta}{k_b} \tag{21}\]

Equation 22, Bespoke Beam-Rider Error at Forty Kilometres. The beam-rider model is evaluated at forty kilometres with the assumed 0.03 radian beam and a sensing factor of ten.

\[\varepsilon_{\text{beam}} = \frac{(4 \times 10^{4})(0.03)}{10} = 120 \, \text{m} \tag{22}\]

Equation 23, Crossover Model of Manual Control. A trained operator adapts until the open loop near crossover behaves as an integrator with gain $\omega_c$ and a pure time delay $\tau$. McRuer and Krendel 1974 Mathematical Models of Human Pilot Behavior

\[Y_{\text{open}}(s) \approx \frac{\omega_c}{s} e^{-\tau s} \tag{23}\]

Equation 24, Crossover Frequency Limit for a Phase Margin. The delay of the crossover model consumes phase in proportion to frequency, so a phase margin $\phi_m$ bounds the crossover frequency. McRuer and Krendel 1974 Mathematical Models of Human Pilot Behavior

\[\omega_c \le \frac{\pi/2 - \phi_m}{\tau} \tag{24}\]

Equation 25, Bespoke Operator Crossover Frequency. The bound is evaluated for a chosen 45 degree phase margin and an operator delay taken as 0.3 seconds, which gives 2.6 radians per second.

\[\omega_c \le \frac{1.571 - 0.785}{0.3} = 2.6 \, \text{rad/s} \tag{25}\]

Equation 26, Supersonic Normal-Force Slope. Linearised supersonic theory gives a normal-force slope of four over the square root of $M^{2} - 1$, evaluated at the reported Mach 1.5. Nielsen 1960 Missile Aerodynamics Anderson 2002 Modern Compressible Flow

\[C_{N\alpha} = \frac{4}{\sqrt{M^{2}-1}} = \frac{4}{\sqrt{1.25}} = 3.58 \ \text{per radian} \tag{26}\]

Equation 27, Bespoke Dynamic Pressure at the Design Condition. The dynamic pressure is evaluated at a flight condition the article chooses, Mach 1.5 at 12 kilometres.

\[q = \tfrac{1}{2} \rho v^{2} = \tfrac{1}{2}(0.312)(443)^{2} = 3.06 \times 10^{4} \, \text{Pa} \tag{27}\]

Equation 28, Bespoke Pitch Moment of Inertia. The pitch inertia treats the vehicle as a uniform slender rod of the reported length and launch mass.

\[I_y \approx \frac{m L^{2}}{12} = \frac{(1588)(6.93)^{2}}{12} = 6.4 \times 10^{3} \, \text{kg} \cdot \text{m}^{2} \tag{28}\]

Equation 29, Bespoke Aerodynamic Pitch Stiffness. The restoring stiffness is the normal force per radian times an assumed static margin of half a metre at the chosen dynamic pressure.

\[M_{\alpha} = q S C_{N\alpha} \, \Delta x = (3.06 \times 10^{4})(6.5)(3.58)(0.5) = 3.6 \times 10^{5} \, \text{N} \cdot \text{m/rad} \tag{29}\]

Equation 30, Bespoke Short-Period Natural Frequency. The natural frequency is the square root of stiffness over inertia, evaluated with the assumed static margin and the uniform-rod inertia. Etkin and Reid 1996 Dynamics of Flight, Stability and Control

\[\omega_n = \sqrt{\frac{M_{\alpha}}{I_y}} = \sqrt{\frac{3.6 \times 10^{5}}{6.4 \times 10^{3}}} = 7.5 \, \text{rad/s} \tag{30}\]

Equation 31, Bespoke Total Impulse. The total impulse is the propellant mass times an effective exhaust velocity of 2,157 metres per second, which the article takes as representative of a storable propellant of the period.

\[I_{\text{tot}} = m_p c = (624)(2157) = 1.35 \times 10^{6} \, \text{N} \cdot \text{s} \tag{31}\]

Equation 32, Bespoke Burn Time at Rated Thrust. The burn time is the assumed total impulse divided by the rated thrust of 13.3 kilonewtons.

\[t_b = \frac{I_{\text{tot}}}{F} = \frac{1.35 \times 10^{6}}{1.33 \times 10^{4}} = 101 \, \text{s} \tag{32}\]

Equation 33, Bespoke Ideal Velocity Increment. The rocket equation is evaluated for the reported launch and empty masses with the assumed effective exhaust velocity. Sutton and Biblarz 2016 Rocket Propulsion Elements

\[\Delta v = c \ln \frac{m_0}{m_f} = 2157 \ln \frac{1588}{964} = 1077 \, \text{m/s} \tag{33}\]

Equation 34, Drag in Level Cruise. In level cruise the thrust equals the drag of a parabolic polar, a zero-lift term plus induced drag set by aspect ratio $A$ and span efficiency $e$.

\[F_{\text{cruise}} = D = q S \left( C_{D0} + \frac{C_L^{2}}{\pi A e} \right) \tag{34}\]

Equation 35, Bespoke Cruise Lift Coefficient. The lift coefficient that supports the launch weight is evaluated at the dynamic pressure of the chosen Mach 1.5 and 12 kilometre condition.

\[C_L = \frac{m g}{q S} = \frac{(1588)(9.81)}{(3.06 \times 10^{4})(6.5)} = 0.078 \tag{35}\]

Equation 36, Skin-Friction Drag Coefficient. Skin friction contributes the friction coefficient times the ratio of wetted area to reference area.

\[C_{D,f} = C_f \, \frac{S_{\text{wet}}}{S} \tag{36}\]

Equation 37, Bespoke Skin-Friction Estimate. The friction drag is evaluated for an assumed turbulent flat-plate coefficient of 0.0025 and a wetted area the article estimates at 25.2 square metres.

\[C_{D,f} = (0.0025) \frac{25.2}{6.5} = 0.0097 \tag{37}\]

Equation 38, Bespoke Cruise Drag. The cruise drag uses an assumed zero-lift drag coefficient of 0.02 at the chosen dynamic pressure.

\[D \approx (3.06 \times 10^{4})(6.5)(0.02) = 4.0 \times 10^{3} \, \text{N} \tag{38}\]

Equation 39, Injector Orifice Flow. The mass flow through an orifice of discharge coefficient $C_d$ and area $A_i$ grows as the square root of the pressure drop. Huzel and Huang 1992 Design of Liquid Propellant Rocket Engines

\[\dot{m} = C_d A_i \sqrt{2 \rho \, \Delta p} \tag{39}\]

Equation 40, Injector Stiffness Criterion. The conventional rule for combustion stability keeps the injector pressure drop above about a fifth of the chamber pressure. Huzel and Huang 1992 Design of Liquid Propellant Rocket Engines

\[\frac{\Delta p}{p_c} \ge 0.2 \tag{40}\]

Equation 41, Bespoke Injector Drop at Half Flow. An injector assumed to sit at the stiffness limit at full flow keeps only a quarter of its pressure drop when throttled to half flow.

\[\frac{\Delta p}{p_c} = \frac{0.2}{4} = 0.05 \tag{41}\]

Equation 42, Thrust-to-Weight Ratio at Launch. The rated thrust over the weight at the reported launch mass is 0.85. Parsch 2002

\[\frac{F}{m_0 g} = \frac{1.33 \times 10^{4}}{(1588)(9.81)} = 0.85 \tag{42}\]

Equation 43, Specific Energy. The specific energy of a vehicle is its potential energy per unit mass plus its kinetic energy per unit mass.

\[e_{\text{launch}} = g h + \tfrac{1}{2} v^{2} \tag{43}\]

Equation 44, Bespoke Specific Energy at Release. The specific energy is evaluated for release conditions the article assumes, 12.2 kilometres and Mach 0.8.

\[e_{\text{launch}} = (9.81)(1.22 \times 10^{4}) + \tfrac{1}{2}(236)^{2} = 1.20 \times 10^{5} + 2.79 \times 10^{4} = 1.48 \times 10^{5} \, \text{J/kg} \tag{44}\]

Equation 45, Bespoke Velocity Equivalent of Air Launch. The speed that carries the same specific energy as the assumed release condition is 544 metres per second.

\[v_{\text{equiv}} = \sqrt{2 e_{\text{launch}}} = \sqrt{2.96 \times 10^{5}} = 544 \, \text{m/s} \tag{45}\]

Equation 46, Tsiolkovsky Mass Ratio. The ratio of initial to final mass grows exponentially with the velocity increment over the effective exhaust velocity.

\[\frac{m_0}{m_f} = \exp \left( \frac{\Delta v}{c} \right) \tag{46}\]

Equation 47, Bespoke Energy Audit of the Powered Phase. The energy gained from the assumed release condition to Mach 2 at a 20 kilometre apex is summed with the burnout mass taken as the empty mass.

\[\Delta E = m g \Delta h + \tfrac{1}{2} m_f v_f^{2} - \tfrac{1}{2} m_0 v_0^{2} = 1.22 \times 10^{8} + 1.68 \times 10^{8} - 4.4 \times 10^{7} = 2.5 \times 10^{8} \, \text{J} \tag{47}\]

Equation 48, Bespoke Kinetic Energy of the Exhaust. The kinetic energy carried by the propellant at the assumed effective exhaust velocity is $1.45 \times 10^{9}$ joules.

\[E_p = \tfrac{1}{2} m_p c^{2} = \tfrac{1}{2}(624)(2157)^{2} = 1.45 \times 10^{9} \, \text{J} \tag{48}\]

Equation 49, Glide Range. A vehicle gliding at a constant lift-to-drag ratio covers that ratio times its height in horizontal distance.

\[R_{\text{glide}} = h \, \frac{L}{D} \tag{49}\]

Equation 50, Bespoke Powered Range. The distance covered under power uses a mean speed during the burn that the article assumes to be 400 metres per second.

\[R_{\text{powered}} = \bar{v} \, t_b = (400)(101) = 40 \, \text{km} \tag{50}\]

Equation 51, Bespoke Effective Glide Ratio. Attributing the 40 kilometres not flown under power to a glide from the 20 kilometre apex gives a lift-to-drag ratio of two.

\[\frac{L}{D} = \frac{R_{\text{glide}}}{h} = \frac{40}{20} = 2.0 \tag{51}\]

Equation 52, Bespoke Dynamic Pressure at Release Altitude. The dynamic pressure at Mach 2 is evaluated at the assumed release altitude of 12.2 kilometres.

\[q = \tfrac{1}{2}(0.301)(590)^{2} = 5.2 \times 10^{4} \, \text{Pa} \tag{52}\]

Equation 53, Dynamic Pressure at the Ceiling. The dynamic pressure at Mach 2 at the reported 20 kilometre ceiling uses the standard atmosphere density there.

\[q = \tfrac{1}{2}(0.089)(590)^{2} = 1.5 \times 10^{4} \, \text{Pa} \tag{53}\]

Equation 54, Supersonic Maximum Lift-to-Drag Estimate. The classical estimate of the maximum lift-to-drag ratio of a supersonic configuration falls with Mach number toward four.

\[\left( \frac{L}{D} \right)_{\max} \approx \frac{4 \left( M + 3 \right)}{M} \tag{54}\]

Equation 55, Proportional Navigation. The commanded lateral acceleration is the navigation constant times the closing velocity times the rotation rate of the line of sight. Zarchan 2012 Tactical and Strategic Missile Guidance

\[a_c = N \, V_c \, \dot{\lambda} \tag{55}\]

Equation 56, Small-Angle Line-of-Sight Rate. For small angles the line-of-sight angle is the lateral separation over the range to go, and its rate is the time derivative of that ratio.

\[\dot{\lambda} = \frac{\mathrm{d}}{\mathrm{d}t} \left( \frac{y}{V_c t_{go}} \right) \tag{56}\]

Equation 57, Proportional Navigation in Separation and Time to Go. Substituting the line-of-sight rate into the guidance law expresses the command in the lateral separation, its rate and the time to go.

\[a_c = N \, \frac{y}{t_{go}^{2}} + N \, \frac{\dot{y}}{t_{go}} \tag{57}\]

Equation 58, Acceleration Ratio Against a Manoeuvring Target. Under proportional navigation the missile’s steady acceleration requirement is $N/(N-2)$ times the target’s manoeuvre. Zarchan 2012 Tactical and Strategic Missile Guidance

\[\frac{n_m}{n_t} = \frac{N}{N-2} \tag{58}\]

Equation 59, Normalised Miss Distance. The residual miss relative to the initial disturbance depends only on the time to go in guidance time constants and on the navigation constant.

\[\frac{m}{m_0} = f \left( \frac{t_{go}}{\tau_g}, N \right) \tag{59}\]

Equation 60, Bespoke Asymptotic Miss for a First-Order Loop. For a guidance loop lumped into a single first-order lag and a step disturbance, the article takes the residual miss as a polynomial in the normalised time $x$ times $e^{-x}$.

\[\frac{m}{m_0} \sim \frac{x^{N-1}}{(N-1)!} \, e^{-x} \tag{60}\]

Equation 61, Bespoke Residual Miss at Eight Time Constants. The asymptotic form evaluated at eight time constants with a navigation constant of four leaves three percent of the initial miss.

\[\left. \frac{m}{m_0} \right|_{x=8} = \frac{8^{3}}{6} \, e^{-8} = 2.9 \times 10^{-2} \tag{61}\]

Equation 62, Bespoke Ten Time Constant Criterion. The article adopts ten guidance time constants of remaining flight as the time needed to null an error.

\[t_{go} \ge 10 \, \tau_g \tag{62}\]

Equation 63, Bespoke Guidance Time Constant. The guidance time constant is the sum of an operator delay of 0.3 seconds, an assumed autopilot rise time of 0.4 seconds and an airframe lag of 0.13 seconds.

\[\tau_g \approx 0.30 + 0.40 + 0.13 = 0.83 \, \text{s} \tag{63}\]

Equation 64, Bespoke Range Needed to Null an Error. Ten assumed guidance time constants at Mach 2 correspond to about five kilometres of flight.

\[R_{\text{null}} = v \, t_{go} = (590)(8.3) = 4.9 \, \text{km} \tag{64}\]

Equation 65, Bespoke Standoff Condition. The article defines the launch aircraft as safe when the missile’s range exceeds the defended radius plus the distance flown while turning away.

\[R_m \ge R_d + v_{\text{ac}} \, t_{\text{turn}} \tag{65}\]

Equation 66, Centre of Pressure of Combined Surfaces. The centre of pressure of a configuration is the mean of the surface positions weighted by their normal-force slopes.

\[x_{cp} = \frac{\sum_i C_{N\alpha,i} \, x_i}{\sum_i C_{N\alpha,i}} \tag{66}\]

Equation 67, Hinge Moment. The hinge moment is the dynamic pressure times the surface area, the mean chord and the hinge-moment coefficient.

\[H = q \, S_c \, \bar{c} \, C_h \tag{67}\]

Equation 68, Bespoke Hinge Moment of the Canard. The hinge moment is evaluated for an assumed 0.35 square metre surface of half-metre chord at a coefficient of 0.05 and the chosen dynamic pressure.

\[H = (3.06 \times 10^{4})(0.35)(0.5)(0.05) = 268 \, \text{N} \cdot \text{m} \tag{68}\]

Equation 69, Bespoke Actuator Power. The actuator power is the assumed hinge moment times a surface rate of five radians per second that the article takes as the autopilot’s demand.

\[P = H \, \dot{\delta} = (268)(5) = 1.3 \, \text{kW} \tag{69}\]

Equation 70, Trim Lift of a Canard Configuration. The trimmed lift is the sum of the wing lift and the canard lift.

\[L_{\text{trim}} = L_{\text{wing}} + L_{\text{canard}} \tag{70}\]

Equation 71, Trim Angle of Attack. A control deflection trims the vehicle at the angle of attack where the control moment cancels the static restoring moment.

\[\alpha_{\text{trim}} = -\frac{C_{m\delta}}{C_{m\alpha}} \, \delta \tag{71}\]

Equation 72, Normal Load Factor. The normal acceleration in units of gravity is the normal force at the trim angle divided by the weight.

\[n = \frac{q S C_{N\alpha} \alpha_{\text{trim}}}{m g} \tag{72}\]

Equation 73, Bespoke Load Factor per Degree. One degree of trimmed angle of attack at the chosen dynamic pressure gives about 0.8 g.

\[n = \frac{(3.06 \times 10^{4})(6.5)(3.58)(0.01745)}{(1588)(9.81)} = 0.80 \tag{73}\]

Equation 74, Roll Error Rotation of the Command. An error $\Delta\phi$ in the assumed roll angle rotates the commanded acceleration vector by that angle.

\[\begin{bmatrix} a_y \\ a_z \end{bmatrix} = \begin{bmatrix} \cos \Delta\phi & -\sin \Delta\phi \\ \sin \Delta\phi & \cos \Delta\phi \end{bmatrix} \begin{bmatrix} a_{y,c} \\ a_{z,c} \end{bmatrix} \tag{74}\]

Equation 75, Lateral Offset from a Heading Error. An uncorrected heading error $\varepsilon$ displaces the impact point laterally by the range times its sine.

\[\Delta y = R \sin \varepsilon \approx R \varepsilon \tag{75}\]

Equation 76, Offset from One Degree at the Reported Range. One degree of heading error over the reported 80 kilometre range displaces the impact by 1.4 kilometres. Parsch 2002

\[\Delta y (1^{\circ}) = (8 \times 10^{4})(0.01745) = 1.4 \, \text{km} \tag{76}\]

Equation 77, Bespoke Correctable Offset. The article bounds the correctable offset by assuming a constant normal acceleration held at constant speed over the remaining range.

\[\Delta y \le \tfrac{1}{2} a_n \left( \frac{R_r}{v} \right)^{2} \tag{77}\]

Equation 78, Bespoke Correctable Offset at Eighty Kilometres. At the four g limit the article derives and at Mach 2 over 80 kilometres the correctable offset is 360 kilometres.

\[\Delta y_{\max} = \tfrac{1}{2}(39.2) \left( \frac{8 \times 10^{4}}{590} \right)^{2} = 3.6 \times 10^{5} \, \text{m} \tag{78}\]

Equation 79, Free-Fall Time. A body falling freely from rest clears a distance $d$ in the square root of $2d/g$.

\[t = \sqrt{\frac{2 d}{g}} \tag{79}\]

Equation 80, Bespoke Aircraft Travel During Separation. The distance flown by the launch aircraft uses an assumed three metres of clearance and the assumed release speed of Mach 0.8.

\[\Delta x = v_{\text{ac}} t = (236)(0.78) = 184 \, \text{m} \tag{80}\]

Equation 81, Bespoke Tip-Off Angular Acceleration. The article models tip-off as the weight acting at an offset $\ell$ from the last support, with aerodynamic and aircraft loads neglected.

\[\dot{q} = \frac{m g \ell}{I_y} \tag{81}\]

Equation 82, Bespoke Tip-Off at Half a Metre. The tip-off model is evaluated for an assumed half-metre offset and the uniform-rod pitch inertia.

\[\dot{q} = \frac{(1588)(9.81)(0.5)}{6.4 \times 10^{3}} = 1.22 \, \text{rad/s}^{2} \tag{82}\]

Equation 83, Bespoke Command Sampling Rate. The article samples the command link at ten times the crossover frequency of the operator loop.

\[f_s = 10 \, \frac{\omega_c}{2\pi} = 10 \, \frac{2.6}{6.283} = 4.1 \, \text{Hz} \tag{83}\]

Equation 84, Bespoke Command Data Rate. Two command axes at an assumed eight bits each and the chosen sampling rate require 66 bits per second.

\[C_{\text{req}} = (2)(8)(4.1) = 66 \, \text{bit/s} \tag{84}\]

Equation 85, Signal-to-Jamming Ratio. The ratio of command signal to jamming at the receiver depends on the transmitter powers and gains, the square of the range ratio and the jammer’s bandwidth dilution.

\[\frac{S}{J} = \frac{P_c G_c}{P_j G_j} \left( \frac{R_j}{R_c} \right)^{2} \, \frac{B_j}{B_s} \tag{85}\]

Equation 86, Friis Transmission Equation. The power received over a one-way radio path falls as the square of range.

\[P_r = \frac{P_t G_t G_r \lambda^{2}}{\left( 4 \pi R \right)^{2}} \tag{86}\]

Equation 87, Bespoke Free-Space Loss of the Command Link. The free-space term at 80 kilometres is evaluated for a command wavelength of one metre that the article assumes.

\[\left( \frac{\lambda}{4 \pi R} \right)^{2} = \left( \frac{1}{4\pi \times 8 \times 10^{4}} \right)^{2} = 9.9 \times 10^{-13} \tag{87}\]

Equation 88, Radio Propagation Delay. The one-way delay over 80 kilometres at the speed of light is 0.27 milliseconds.

\[t_{\text{prop}} = \frac{R}{c_0} = \frac{8 \times 10^{4}}{3 \times 10^{8}} = 0.27 \, \text{ms} \tag{88}\]

Equation 89, Characteristic Equation with Rate Feedback. Rate feedback of gain $K$ through a control moment $M_{\delta}$ adds to the damping term of the short-period characteristic equation and leaves its stiffness unchanged. Blakelock 1991 Automatic Control of Aircraft and Missiles

\[s^{2} + \left( 2 \zeta_a \omega_n + K M_{\delta} \right) s + \omega_n^{2} = 0 \tag{89}\]

Equation 90, Damping Ratio with Rate Feedback. The closed-loop damping ratio is the aerodynamic damping plus the feedback term divided by twice the natural frequency. Blakelock 1991 Automatic Control of Aircraft and Missiles

\[\zeta = \zeta_a + \frac{K M_{\delta}}{2 \omega_n} \tag{90}\]

Equation 91, Bespoke Required Rate-Loop Gain. The gain needed for a chosen damping ratio of 0.7 assumes an aerodynamic damping of 0.05 and the article’s natural frequency.

\[K M_{\delta} = 2 \omega_n \left( \zeta - \zeta_a \right) = (2)(7.5)(0.7 - 0.05) = 9.8 \, \text{s}^{-1} \tag{91}\]

Equation 92, Gain Stabilisation of the First Bending Mode. The loop remains stable against structural coupling when its gain at the first bending frequency is below unity.

\[\left| K \, G_{\text{bend}}(j\omega_1) \right| < 1 \tag{92}\]

Equation 93, First Bending Mode of a Free-Free Beam. A uniform free-free beam has its first elastic mode at $(4.730/L)^{2}$ times the square root of the bending stiffness over the mass per unit length.

\[\omega_1 = \left( \frac{4.730}{L} \right)^{2} \sqrt{\frac{EI}{\mu}} \tag{93}\]

Equation 94, Second Moment of Area of a Thin-Walled Tube. A thin-walled circular tube of radius $r$ and wall thickness $t$ has a second moment of area $\pi r^{3} t$.

\[I = \pi r^{3} t \tag{94}\]

Equation 95, Bespoke First Bending Frequency of the X-9. The free-free beam is evaluated for an assumed three millimetre aluminium wall and the launch mass spread uniformly along the length.

\[\omega_1 = \left( \frac{4.730}{6.93} \right)^{2} \sqrt{\frac{(70 \times 10^{9})(2.1 \times 10^{-4})}{229}} = 117 \, \text{rad/s} \tag{95}\]

Equation 96, Bespoke Missile Flight Time. The flight time assumes that the whole 80 kilometres is flown at Mach 2.

\[t_f = \frac{R}{v} = \frac{8 \times 10^{4}}{590} = 136 \, \text{s} \tag{96}\]

Equation 97, Bespoke Launch Aircraft Travel. The launch aircraft is assumed to continue at Mach 0.8 for the missile’s flight time.

\[\Delta x_{\text{ac}} = (236)(136) = 32 \, \text{km} \tag{97}\]

Equation 98, Level Turn Radius. The radius of a level banked turn is the square of speed over gravity times the square root of $n^{2} - 1$.

\[R_t = \frac{v^{2}}{g \sqrt{n^{2}-1}} \tag{98}\]

Equation 99, Bespoke Bomber Turn Radius. The turn radius is evaluated for a bomber assumed limited to 1.5 g at the assumed release speed.

\[R_t = \frac{(236)^{2}}{(9.81)\sqrt{1.25}} = 5.1 \, \text{km} \tag{99}\]

Equation 100, Bespoke Time for a Reversal. A half circle at the assumed turn radius and speed takes 68 seconds.

\[t_{180} = \frac{\pi R_t}{v} = \frac{\pi (5.1 \times 10^{3})}{236} = 68 \, \text{s} \tag{100}\]

Equation 101, Recovery Temperature. The recovery temperature at Mach 2 uses a turbulent recovery factor of 0.89 and the standard atmosphere temperature of 217 kelvin.

\[T_r = T_{\infty} \left( 1 + r \, \frac{\gamma-1}{2} M^{2} \right) = 217 \left( 1 + (0.89)(0.2)(4) \right) = 372 \, \text{K} \tag{101}\]

Equation 102, Lumped Thin-Skin Heating. A thin skin of density $\rho_m$, specific heat $c_p$ and thickness $t$ heats at a rate set by convection from the recovery temperature. Incropera and DeWitt, Fundamentals of Heat and Mass Transfer

\[\rho_m c_p t \, \frac{\mathrm{d}T_w}{\mathrm{d}t} = h \left( T_r - T_w \right) \tag{102}\]

Equation 103, Thermal Time Constant of a Thin Skin. The skin’s thermal time constant is its heat capacity per unit area divided by the convective coefficient. Incropera and DeWitt, Fundamentals of Heat and Mass Transfer

\[\tau = \frac{\rho_m c_p t}{h} \tag{103}\]

Equation 104, Bespoke Skin Time Constant. The time constant is evaluated for an assumed two millimetre aluminium skin and a convective coefficient of 150 watts per square metre kelvin.

\[\tau = \frac{(2800)(900)(2 \times 10^{-3})}{150} = 34 \, \text{s} \tag{104}\]

Equation 105, Bespoke Wing Root Bending Moment. The article estimates the root bending moment from each half-wing carrying half the four g load, spread uniformly, so that its resultant acts a quarter of the span $b$ from the root.

\[M_{\text{root}} = n \, m g \, \frac{b}{8} = (4)(1588)(9.81) \frac{2.39}{8} = 1.86 \times 10^{4} \, \text{N} \cdot \text{m} \tag{105}\]

Equation 106, Terminal Velocity Under a Canopy. A body descends at the speed where drag on area $A$ with coefficient $C_D$ balances its weight. Knacke 1992 Parachute Recovery Systems Design Manual

\[v_t = \sqrt{\frac{2 m g}{\rho C_D A}} \tag{106}\]

Equation 107, Bespoke Canopy Area. The canopy area is evaluated for an assumed 300 kilogramme package, an assumed descent rate of eight metres per second and a drag coefficient of 1.4.

\[A = \frac{2 m g}{\rho C_D v_t^{2}} = \frac{(2)(300)(9.81)}{(1.225)(1.4)(64)} = 53.6 \, \text{m}^{2} \tag{107}\]

Equation 108, Likelihood of Four Failures Then a Success. For independent flights of success probability $p$, the likelihood of four failures followed by a success is maximised at $p = 0.2$.

\[L(p) = \left( 1 - p \right)^{4} p \tag{108}\]

Equation 109, Zero-Failure Demonstration Test. Demonstrating reliability $p$ at confidence $1 - \alpha$ with no failures needs $\ln \alpha / \ln p$ consecutive successes.

\[n = \frac{\ln \alpha}{\ln p} \tag{109}\]

Equation 110, Successes Needed for 90 Percent at 95 Percent. Demonstrating 90 percent reliability at 95 percent confidence needs 29 consecutive successes.

\[n = \frac{\ln 0.05}{\ln 0.90} = 28.4, \ \text{so 29 consecutive successes} \tag{110}\]

Equation 111, Single-Shot Kill Probability. For a definite lethal radius $R_L$ and a circular normal miss, the kill probability is one minus one half raised to the squared ratio of lethal radius to circular error probable.

\[P_k = 1 - \left( \tfrac{1}{2} \right)^{\left( R_L / \mathrm{CEP} \right)^{2}} \tag{111}\]

Equation 112, Circular Error Probable for a Kill Probability. Inverting the kill probability gives the circular error probable that a lethal radius and a required kill probability permit.

\[\mathrm{CEP} = \frac{R_L}{\sqrt{\log_2 \left( \dfrac{1}{1 - P_k} \right)}} \tag{112}\]

Equation 113, Cube-Root Blast Scaling. The radius at which a given overpressure is reached scales as the cube root of yield $W$ from the one-kilotonne radius $R_1$. Glasstone and Dolan 1977 The Effects of Nuclear Weapons

\[R_L = R_1 \, W^{1/3} \tag{113}\]

Equation 114, Bespoke Lethal Radius at Twenty Kilotonnes. Cube-root scaling from the 690 metre one-kilotonne radius for five pounds per square inch is evaluated for a yield of twenty kilotonnes that the article takes as representative. Glasstone 1962 The Effects of Nuclear Weapons, Revised Edition

\[R_L = 690 \, (20)^{1/3} = 1873 \, \text{m} \tag{114}\]

Equation 115, Bespoke Accuracy Needed for 90 Percent Kill. The circular error probable is evaluated for an assumed lethal radius of 1,500 metres against a soft target and a 90 percent kill probability.

\[\mathrm{CEP} = \frac{1500}{\sqrt{\log_2 10}} = \frac{1500}{1.82} = 823 \, \text{m} \tag{115}\]

Notation

• $\sigma$, the axis standard deviation of the miss, and with a subscript the standard deviation of one error source or of an angle estimate
• $\mathrm{CEP}$, the circular error probable, the radius containing half the impacts
• $R$, a radius about the aim point in Equations 1 and 2, a range from a radar or transmitter in the tracking and link sections, and a range to the target in Equations 75 and 96
• $P$, the probability of landing within a radius, and in Equation 69 the actuator power
• $n$, a number of samples, flights or error sources, and in Equations 72, 98 and 105 the load factor
• $b$, the systematic bias of the impact point in Equation 6 and the wing span in Equation 105
• $\lambda$, the radar or radio wavelength, and in Equations 55 and 56 the line-of-sight angle
• $D$, the antenna aperture in the tracking equations and the drag in Equations 34 and 38
• $k$, the factor by which a tracker resolves an angle finer than the beamwidth
• $\theta$, the angular beamwidth
• $\varepsilon_{\perp}$, the cross-range position error of a tracker
• $k_m$, the monopulse slope
• $\sigma_t$, the radar cross-section of the target
• $P_t$, the transmitter power
• $G$, the gain of the radar antenna
• $P_b$, the power of the beacon on the missile
• $c_g$, the glint factor, of order 0.3
• $L_t$, the dimension of the target
• $k_b$, the fraction of a beamwidth that a beam rider can sense, of order ten
• $\omega_c$, the crossover frequency of the operator loop
• $\tau$, the operator’s effective delay, and in Equations 103 and 104 the thermal time constant of the skin
• $\phi_m$, the phase margin
• $C_{N\alpha}$, the normal force curve slope per radian
• $M$, the Mach number
• $q$, the dynamic pressure in pascals
• $\rho$, the air density
• $I_y$, the pitch moment of inertia
• $M_{\alpha}$, the aerodynamic restoring stiffness in pitch
• $\omega_n$, the undamped natural frequency of the pitch motion
• $c$, the effective exhaust velocity of the rocket
• $m_p$, the propellant mass
• $m_0$, the launch mass, except in Equations 59 to 61, where it is the initial miss
• $m_f$, the mass at burnout
• $I_{\text{tot}}$, the total impulse
• $t_b$, the burn time
• $F$, the rocket thrust
• $S$, the wing reference area
• $C_{D0}$, the zero-lift drag coefficient
• $C_L$, the lift coefficient
• $C_f$, the turbulent skin-friction coefficient
• $S_{\text{wet}}$, the wetted area
• $C_d$, the discharge coefficient of an injector orifice
• $A_i$, the injector orifice area
• $\Delta p$, the injector pressure drop
• $p_c$, the chamber pressure
• $e_{\text{launch}}$, the specific energy at release
• $h$, the altitude, and in Equations 102 and 103 the convective heat transfer coefficient
• $\frac{L}{D}$, the lift-to-drag ratio
• $N$, the navigation constant
• $V_c$, the closing velocity
• $t_{go}$, the time remaining to intercept
• $n_t$, the manoeuvre acceleration of the target
• $\tau_g$, the guidance time constant that lumps the operator, autopilot and airframe lags
• $x_{cp}$, the position of the centre of pressure
• $H$, the hinge moment of a control surface
• $C_h$, the hinge-moment coefficient
• $\bar{c}$, the mean chord of the control surface
• $\delta$, the control surface deflection
• $\Delta\phi$, the error in the assumed roll angle
• $a_n$, the normal acceleration available for correction
• $\ell$, the offset of the centre of gravity from the last remaining support
• $\dot{q}$, the pitch angular acceleration at release
• $v_{\text{ac}}$, the speed of the launch aircraft
• $B_j$, the jammer bandwidth
• $B_s$, the signal bandwidth
• $c_0$, the speed of light
• $K$, the gain of the rate feedback loop
• $M_{\delta}$, the control moment per unit deflection
• $\zeta$, the damping ratio of the pitch motion
• $\zeta_a$, the aerodynamic damping ratio without feedback
• $\omega_1$, the frequency of the first bending mode
• $EI$, the bending stiffness of the body
• $\mu$, the mass per unit length of the body
• $R_t$, the turn radius of the launch aircraft
• $T_r$, the recovery temperature reached by the surface under the boundary layer
• $T_{\infty}$, the free-stream static temperature
• $\gamma$, the ratio of specific heats of air
• $T_w$, the skin temperature
• $v_t$, the terminal descent velocity under the canopy
• $C_D$, the drag coefficient of the canopy
• $P_k$, the single-shot kill probability
• $R_L$, the lethal radius of the warhead in Equations 111 to 114, and in Equation 14 the range from the launcher
• $W$, the yield in kilotonnes
• $R_1$, the radius of the five pounds per square inch contour for one kilotonne

References

Primary Sources, Peer-Reviewed

• (René) van Paassen, M. M., and Max Mulder. 1998. “Identification of Human Operator Control Behaviour in Multiple-Loop Tracking Tasks.” IFAC Proceedings Volumes 31 (26): 455–60. https://doi.org/10.1016/s1474-6670(17)40135-2
• “99/02715 Non-Linear Throttling Analysis of Thrust and Mixture Ratio for a Liquid Oxygen/kerosine Rocket Engine.” 1999. Fuel and Energy Abstracts 40 (4): 282. https://doi.org/10.1016/s0140-6701(99)98484-9
• Abbe, C. J., C. W. McLAUGHLIN, and R. R. Weiss. 1968. “Influence of Storable Propellant Liquid Rocket Design Parameters on Combustion Instability.” Journal of Spacecraft and Rockets 5 (5): 584–90. https://doi.org/10.2514/3.29308
• Abd-Altief, M. A., and Longjun Qian. 2014. “Multi-Stages Robust Autopilot for Nonlinear Command Line of Sight Guided System.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6895669
• Abdel-Malek, A., and V. Z. Marmarelis. 1988. “Modeling of Task-Dependent Characteristics of Human Operator Dynamics Pursuit Manual Tracking.” IEEE Transactions on Systems, Man, and Cybernetics 18 (1): 163–72. https://doi.org/10.1109/21.87065
• Abdel-Malek, A., and V. Marmarelis. 1990. “A Model of Human Operator Behavior during Pursuit Manual Tracking-What Does It Reveal?” In 1990 IEEE International Conference on Systems, Man, and Cybernetics Conference Proceedings. IEEE. https://doi.org/10.1109/icsmc.1990.142202
• 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
• Abedi, Mostafa, H. Bolandi, F. Fani Saberi, and M. R. Jahed-Motlagh. 2007. “An Adaptive RBF Neural Guidance Law Surface to Air Missile Considering Target and Control Loop Uncertainties.” In 2007 IEEE International Symposium on Industrial Electronics. IEEE. https://doi.org/10.1109/isie.2007.4374608
• Abidi, K., Y. Yildiz, and B. E. Korpe. 2016. “Explicit Time-Delay Compensation in Teleoperation: An Adaptive Control Approach.” International Journal of Robust and Nonlinear Control 26 (15): 3388–3403. https://doi.org/10.1002/rnc.3513
• 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
• Abubakar, Abdulrazaq Nafiu, Ali Nasir, Abdul-wahid A. Saif, and Jamilu Umar Yahya. 2025. “Command Filtered Based Fault Tolerant Impact Angle-Constrained Integrated Guidance and Control for STT Missiles Intercepting Maneuvering Target.” In 2025 37th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc65474.2025.11091068
• Abubakar, Ahmad, Yahya Zweiri, Abdel Gafoor Haddad, Mubarak Yakubu, Ruqayya Alhammadi, and Lakmal Seneviratne. 2026. “Physics-Informed LSTM-Based Delay Compensation Framework for High-Fidelity Teleoperation of Wheeled Mobile Robots.” Robotics and Autonomous Systems 197: 105265. https://doi.org/10.1016/j.robot.2025.105265
• Abzug, M. J. 1967. “Final-Value Homing Missile Guidance.” Journal of Spacecraft and Rockets 4 (2): 279–80. https://doi.org/10.2514/3.28850
• Abzug, Malcolm J. 1979. “Vector Methods in Homing Guidance.” Journal of Guidance and Control 2 (3): 253–55. https://doi.org/10.2514/3.55870
• Acho, Leonardo. 2017. “Iterative Learning Control for Homing Guidance Design of Missiles.” Defence Technology 13 (5): 360–66. https://doi.org/10.1016/j.dt.2017.01.002
• Acree, J. J., and M. W. Maier. 1996. “Radar Detection of Missile Plumes Embedded in Elevated Atmospheric Ducts.” In 1996 IEEE Aerospace Applications Conference. Proceedings, vol. 3. IEEE. https://doi.org/10.1109/aero.1996.496056
• “Active Force Reflection Devices in Teleoperation.” 1991. IEEE Control Systems 11 (1): 52–56. https://doi.org/10.1109/37.103357
• Acton, James M. 2015. “Hypersonic Boost-Glide Weapons.” Science & Global Security 23 (3): 191–219. https://doi.org/10.1080/08929882.2015.1087242
• Adams, Douglas S. 2014. “Mortar Deployment Extensibility for the Low Density Supersonic Decelerator Parachute.” In 2014 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2014.6836489
• Adler, Fred P. 1956. “Missile Guidance by Three-Dimensional Proportional Navigation.” Journal of Applied Physics 27 (5): 500–507. https://doi.org/10.1063/1.1722411
• Adrian, Odile. 2007. “Future Surface Radar Technology: From Air Defence to Air and Missile Defence.” In 2007 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2007.374189
• “Advanced Missile Models and Methods for Availability Prediction.” 1969. Microelectronics Reliability 8 (4): 291. https://doi.org/10.1016/0026-2714(69)90326-6
• Aggarwal, R. K. n.d. “Optimal Missile Guidance for Weaving Targets.” In Proceedings of 35th IEEE Conference on Decision and Control, vol. 3. IEEE. https://doi.org/10.1109/cdc.1996.573533
• Ahi, Behzad, and Mohammad Haeri. 2021. “Novel Command to Line of Sight Guidance with Practical Limitations.” Asian Journal of Control 24 (3): 1426–36. https://doi.org/10.1002/asjc.2529
• Ahmad, Ibrahim A. 1993. “Nonparametric Estimation of the CDF of Weapon Effectiveness on Target Performance.” Applied Mathematics and Computation 57 (2–3): 289–303. https://doi.org/10.1016/0096-3003(93)90153-6
• “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
• 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
• Akhil, G., and D. Ghose. 2012. “Biased PN Based Impact Angle Constrained Guidance Using a Nonlinear Engagement Model.” In 2012 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2012.6315574
• Akishita, Sadao, Ryujiro Kurosaki, Kanzo Okada, and Tomoji Hirata. 1986. “Theoretical Prediction of Roll Moment on Wing-Controlled Missile.” Journal of Aircraft 23 (11): 808–13. https://doi.org/10.2514/3.45385
• Albakri, Abdulrahman, Chao Liu, and Philippe Poignet. 2013. “Stability and Performance Analysis of Three-Channel Teleoperation Control Architectures for Medical Applications.” In 2013 IEEE/RSJ International Conference on Intelligent Robots and Systems. IEEE. https://doi.org/10.1109/iros.2013.6696391
• Aldrich, G. T., and W. B. Krabill. 1973. “An Application of Kalman Techniques to Aircraft and Missile Radar Tracking.” AIAA Journal 11 (7): 932–38. https://doi.org/10.2514/3.50544
• Aleksandrovich, Lyapin Nikita, and Evdokimenkov Veniamin Nikolayevich. 2020. “Assessment of the Air-Launched Weapons Impact on the Effectiveness of the Unmanned Aerial Vehicle Control Guaranteeing Algorithm during the Air Target Interception.” In 2020 International Conference on Dynamics and Vibroacoustics of Machines (DVM). IEEE. https://doi.org/10.1109/dvm49764.2020.9243877
• Alfred, Q. Md., T. Chakravarty, G. Singh, and S. K. Sanyal. 2007. “A Novel Implementation Technique of Conical Scan Radar Using a Programmable Phased Array.” International Journal of Infrared and Millimeter Waves 28 (10): 881–87. https://doi.org/10.1007/s10762-007-9252-6
• Allen, Jerry M., and A. B. Blair. 1982. “Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile.” Journal of Spacecraft and Rockets 19 (2): 155–59. https://doi.org/10.2514/3.62226
• Allmen, C. R., and M.-W. Lu. 1993. “Sample Size for Failure Detection and Reliability Demonstration.” In Annual Reliability and Maintainability Symposium 1993 Proceedings. IEEE. https://doi.org/10.1109/rams.1993.296825
• Almustafa, M. K., and M. L. Nehdi. 2020. “Machine Learning Model for Predicting Structural Response of RC Slabs Exposed to Blast Loading.” Engineering Structures 221: 111109. https://doi.org/10.1016/j.engstruct.2020.111109
• 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
• Alpert, Joel. 2020. “Adjoint Analysis of Guidance Systems for Time-Series Inputs Using Fourier Analysis.” Journal of Guidance, Control, and Dynamics 43 (7): 1359–64. https://doi.org/10.2514/1.g005166
• Altseimer, John H. 1952. “Photographic Techniques Applied to Combustion Studies-Two-Dimensional Transparent Thrust Chamber.” Journal of the American Rocket Society 22 (2): 86–91. https://doi.org/10.2514/8.4432
• Alviani, Robert, Devon Fano, Jonathan Poggie, and Gregory Blaisdell. 2022. “Aerodynamic Heating in the Gap between a Missile Body and a Control Fin.” Journal of Spacecraft and Rockets 59 (4): 1111–24. https://doi.org/10.2514/1.a35183
• Amico, Enrico, and Gioacchino Cafiero. 2026. “A Short Review of Unconventional Riblet Designs for Skin-Friction Drag Reduction in Turbulent Flows.” Chinese Journal of Aeronautics 39 (10): 104278. https://doi.org/10.1016/j.cja.2026.104278
• Amrouche, Naima, Ali Khenchaf, and Daoud Berkani. 2017. “Multiple Mode Multi-Target Tracking in High Noise Environment Using Radar Measurements.” In 2017 Sensor Signal Processing for Defence Conference (SSPD). IEEE. https://doi.org/10.1109/sspd.2017.8233245
• An, Do-Jin, and Joon-Ho Lee. 2020. “Performance Analysis of Amplitude Comparison Monopulse Direction-of-Arrival Estimation.” Applied Sciences 10 (4): 1246. https://doi.org/10.3390/app10041246
• An, Yueqi, and Jianwei Niu. 2025. “Innovative Dynamic Function Allocation: Enhancing UAV Supervisory Control Performance by Integrating Operator Fatigue and Flight Hazard Mitigation.” International Journal of Industrial Ergonomics 110: 103848. https://doi.org/10.1016/j.ergon.2025.103848
• An, Binghe, Yongii Wang, and Lei Liu. 2019. “Guidance Law with Impact Angle and Impact Time Constraints.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865228
• An, Qiang, Chunmao Yeh, Yaobing Lu, Yaomin He, and Jian Yang. 2024. “Time-Varying Angle Estimation of Multiple Unresolved Extended Targets via Monopulse Radar.” IEEE Transactions on Aerospace and Electronic Systems 60 (4): 4650–67. https://doi.org/10.1109/taes.2024.3379315
• An, Binghe, Zongzhun Zheng, Bo Wang, Huijin Fan, Lei Liu, and Yongji Wang. 2022. “Time-to-Go Estimation for Guidance Law with Impact Angle Constraint.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9902439
• Anandhanarayanan, K., Konark Arora, Vaibhav Shah, R. Krishnamurthy, and Debasis Chakraborty. 2013. “Separation Dynamics of Air-to-Air Missile Using a Grid-Free Euler Solver.” Journal of Aircraft 50 (3): 725–31. https://doi.org/10.2514/1.c031791
• Ananoff, A. 1941. “Problems of the Reaction Engine: How a Liquid Fuel Rocket Motor Functions.” Astronautics 11 (48): 9–13. https://doi.org/10.2514/8.10288
• Andersh, Jon, Bernard Mettler, and Nikos Papanikolopoulos. 2009. “Experimental Investigation of Teleoperation Performance for Miniature Rotorcraft.” 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.2009.5400721
• Anderson, Gerald M. 1981. “Comparison of Optimal Control and Differential Game Intercept Missile Guidance Laws.” Journal of Guidance and Control 4 (2): 109–15. https://doi.org/10.2514/3.56061
• Anderson, Seth B. 1987. “A Look at Handling Qualities of Canard Configurations.” Journal of Guidance, Control, and Dynamics 10. https://ntrs.nasa.gov/citations/19870044952
• Anderson, M. R. 1994. “A Model of the Human Operator Using Sensitivity Function Shaping.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 2. IEEE. https://doi.org/10.1109/acc.1994.752321
• Anderson, Gerald M., and George W. Watt. 1971. “Air-to-Air Missile Trajectories for Maximization of Launch Range.” Journal of Spacecraft and Rockets 8 (7): 747–51. https://doi.org/10.2514/3.59721
• Ando, N., Joo-Ho Lee, and H. Hashimoto. 1999. “A Study on Influence of Time Delay in Teleoperation: Quantitative Evaluation on Time Perception and Operability of Human Operator.” In IEEE SMC’99 Conference Proceedings. 1999 IEEE International Conference on Systems, Man, and Cybernetics (Cat. No.99CH37028), vol. 5. IEEE. https://doi.org/10.1109/icsmc.1999.815712
• Andrews, Jonathan, Alex Brooks, and Mervin Budge. 2020. “A Unified Equation Characterizing a Monopulse Angle Tracking Unit.” In 2020 SoutheastCon. IEEE. https://doi.org/10.1109/southeastcon44009.2020.9368275
• Andrews, Jonathan, Mervin Budge, and Laurie Joiner. 2018. “An Examination of Dichotomous and Centroid Tracking of a Monopulse Angle Tracking Unit.” In SoutheastCon 2018. IEEE. https://doi.org/10.1109/secon.2018.8479084
• Angus, John E. 1986. “Interval Estimation of MTBF Based on Minimal Information from a Reliability Demonstration Test.” IEEE Transactions on Reliability 35 (4): 427–28. https://doi.org/10.1109/tr.1986.4335494
• 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
• Annam, Chandrakanth, Ashwini Ratnoo, and Debasish Ghose. 2021. “Singular-Perturbation-Based Guidance of Pulse Motor Interceptors with Look Angle Constraints.” Journal of Guidance, Control, and Dynamics 44 (7): 1356–70. https://doi.org/10.2514/1.g005508
• Ansary, O., and A. Rahrooh. n.d. “Optimal Control of a Moving Missile Tracking a Roving Target.” In Proceedings of Southcon ‘95. IEEE. https://doi.org/10.1109/southc.1995.516088
• Antunes, Rui M., Fernando V. Coito, and Herminio Duarte-Ramos. 2010. “Human-Machine Control Model Approach to Enhance Operator Skills.” In 2010 International Conference on Mechanical and Electrical Technology. IEEE. https://doi.org/10.1109/icmet.2010.5598392
• 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
• “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
• “Application of the Optimal Control Model for the Human Operator to Reliability Assessment.” 1974. Microelectronics Reliability 13 (1): 11. https://doi.org/10.1016/0026-2714(74)90129-2
• “Approach to Reliability for the SM-2 Missile.” 1973. Microelectronics Reliability 12 (5): 409. https://doi.org/10.1016/0026-2714(73)90040-1
• Arcara, Paolo, Claudio Melchiorri, and Stefano Stramigioli. 2001. “Intrinsically Passive Control in Bilateral Teleoperation Mimo Systems.” In 2001 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2001.7076076
• Arend, Matthias G., Sabine J. Schlittmeier, Alexander Mertens, and Verena Nitsch. 2026. “Measuring Situation Awareness during Teleoperation: Scenarios, Sensitivity, and Predictiveness of Operator Performance.” IEEE Access 14: 140439–59. https://doi.org/10.1109/access.2026.3730643
• Arif, M., and H. Inooka. 1999. “Iterative Manual Control Model of Human Operator.” Biological Cybernetics 81 (5–6): 445–55. https://doi.org/10.1007/s004220050574
• Armbruster, Wolfgang, Justin S. Hardi, and Michael Oschwald. 2021. “Flame-Acoustic Response Measurements in a High-Pressure, 42-Injector, Cryogenic Rocket Thrust Chamber.” Proceedings of the Combustion Institute 38 (4): 5963–70. https://doi.org/10.1016/j.proci.2020.05.020
• Artamanov, K. I. 1963. “Stability of Liquid Fuel Rocket Engine Operation.” AIAA Journal 1 (1): 263–66. https://doi.org/10.2514/3.1522
• Arthur, J. S., J. C. Henry, G. H. Pettengill, and P. B. Sebring. 1961. “The Millstone Radar in Satellite and Missile Tracking.” Planetary and Space Science 7: 81–93. https://doi.org/10.1016/0032-0633(61)90289-6
• 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
• Askari, Sina, Mohammad Asadian, and Andrei Shkel. 2021. “Performance of Quad Mass Gyroscope in the Angular Rate Mode.” Micromachines 12 (3): 266. https://doi.org/10.3390/mi12030266
• Asran, A., and M. El-Geneidy. 2001. “Adaptive Fuzzy Controller of Command Guided Missile.” IFAC Proceedings Volumes 34 (13): 639–44. https://doi.org/10.1016/s1474-6670(17)39064-x
• Assen, A. Van, and E. G. Eijkman. 1970. “Reaction Time and Performance in Learning a Two Dimensional Compensatory Tracking Task.” Ergonomics 13 (6): 707–17. https://doi.org/10.1080/00140137008931196
• Asseo, Sabi. 1981. “Detection of Target Multiplicity Using Monopulse Quadrature Angle.” IEEE Transactions on Aerospace and Electronic Systems AES-17 (2): 271–80. https://doi.org/10.1109/taes.1981.309155
• “Assessing Missile System Reliability.” 1972. Microelectronics Reliability 11 (6): 476. https://doi.org/10.1016/0026-2714(72)90035-2
• Asthana, C. B., and Prahlada. 1994. “Evaluation of Missile Seeker Dwell Time for Three-Dimensional Aerial Engagements.” Journal of Guidance, Control, and Dynamics 17 (1): 211–14. https://doi.org/10.2514/3.21181
• Astrov, I., A. Pedai, and E. Rustern. n.d. “Simulation of Two-Rate Adaptive Hybrid Control with Neural and Neuro-Fuzzy Networks for Stochastic Model of Missile Autopilot.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 3. IEEE. https://doi.org/10.1109/wcica.2004.1342067
• Aswathi, C. S., and A. Asok Kumar. 2018. “Sliding Mode Control Strategy for Stabilization of Missile Roll Dynamics.” In 2018 IEEE Recent Advances in Intelligent Computational Systems (RAICS). IEEE. https://doi.org/10.1109/raics.2018.8635056
• Atashfeshan, Nooshin, Mohammad Saidi-Mehrabad, and Hamideh Razavi. 2021. “A Novel Dynamic Function Allocation Method in Human-Machine Systems Focusing on Trigger Mechanism and Allocation Strategy.” Reliability Engineering & System Safety 207: 107337. https://doi.org/10.1016/j.ress.2020.107337
• Atir, Ronen, Gyorgy Hexner, Haim Weiss, and Tal Shima. 2010. “Target Maneuver Adaptive Guidance Law for a Bounded Acceleration Missile.” Journal of Guidance, Control, and Dynamics 33 (3): 695–706. https://doi.org/10.2514/1.47276
• Atwood, Christopher A. 1995. “Computation of a Controlled Store Separation from a Cavity.” Journal of Aircraft 32 (4): 846–52. https://doi.org/10.2514/3.46800
• Autenrieb, Johannes, and Patrick Gruhn. 2026. “Control Allocation Algorithm for Hypersonic Glide Vehicles with Input Limitations.” Journal of Guidance, Control, and Dynamics 49 (8): 2260–76. https://doi.org/10.2514/1.g009588
• Awad, Ahmed, and Haoping Wang. 2016b. “Roll-Pitch-Yaw Autopilot Design for Nonlinear Time-Varying Missile Using Partial State Observer Based Global Fast Terminal Sliding Mode Control.” Chinese Journal of Aeronautics 29 (5): 1302–12. https://doi.org/10.1016/j.cja.2016.04.020
• Awad, A., and H. Wang. 2016c. “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
• Azarova, Olga A. 2022. “Basics of Control of the Bow Shock Wave, Drag and Lift Forces, and Stability in a Steady Supersonic Flow past an AD Body Using Permanently Operating Thermally Stratified Energy Deposition.” Energies 15 (22): 8627. https://doi.org/10.3390/en15228627
• Aziminejad, A., M. Tavakoli, R. V. Patel, and M. Moallem. 2008. “Stability and Performance in Delayed Bilateral Teleoperation: Theory and Experiments.” Control Engineering Practice 16 (11): 1329–43. https://doi.org/10.1016/j.conengprac.2008.03.005
• Babcock, Judson. 2007. “Applied Computational Fluid Dynamics in Support of Aircraft/Store Compatibility and Weapons Integration-2007 Edition.” In 2007 DoD High Performance Computing Modernization Program Users Group Conference. IEEE. https://doi.org/10.1109/hpcmp-ugc.2007.11
• Babu, K. Ravindra, I. G. Sarma, and K. N. Swamy. 1994a. “Switched Bias Proportional Navigation for Homing Guidance against Highly Maneuvering Targets.” Journal of Guidance, Control, and Dynamics 17 (6): 1357–63. https://doi.org/10.2514/3.21356
• Bacci, David, and Alistair J. Saddington. 2026. “Statistical Analysis of Store Release from a Weapon Bay at Transonic Mach Number.” Defence Technology 60: 64–78. https://doi.org/10.1016/j.dt.2025.11.032
• Bai, Xiao, Peng Cheng, Qinglian Li, Liyong Sheng, and Zhongtao Kang. 2020. “Effects of Self-Pulsation on Combustion Instability in a Liquid Rocket Engine.” Experimental Thermal and Fluid Science 114: 110038. https://doi.org/10.1016/j.expthermflusci.2019.110038
• Bai, Mo, and J. N. Chung. 2012. “Enhanced Cooling of a Liquid-Fueled Rocket Thrust Chamber by Metal Foams.” Journal of Propulsion and Power 28 (2): 434–43. https://doi.org/10.2514/1.b34422
• Bai, Yilan, Qibin Hu, Yu Long, Ke Ma, Chuangye Zhao, and Mengying Zhang. 2022. “Parachute Deployment Fault Identification and Landing Point Prediction of Spacecraft Recovery System Based on Swin Transformer and Edge Detection.” In 2022 5th International Conference on Mechatronics, Robotics and Automation (ICMRA). IEEE. https://doi.org/10.1109/icmra56206.2022.10145682
• Bai, Linling, Yu Wang, Enmei Wang, Chenliang Wang, and Jianzhong Qiao. 2023. “Three-Dimensional Anti-Disturbance Guidance for Impact Angle Control with Field-of-View Constraint.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10239946
• Balaji, S., R. Santhakumar, and S. Rajalakshmi. 2009. “Estimation of Angle Glint for Different Radar Targets.” In 2009 First Asian Himalayas International Conference on Internet. IEEE. https://doi.org/10.1109/ahici.2009.5340314
• Balakrishnan, S. N., and J. L. Speyer. 1989. “Assumed Density Filter with Application to Homing Missile Guidance.” Journal of Guidance, Control, and Dynamics 12 (1): 4–12. https://doi.org/10.2514/3.20361
• Balakrishnan, S. N., D. T. Stansbery, J. H. Evers, and J. R. Cloutier. n.d. “Analytical Guidance Laws and Integrated Guidance/autopilot for Homing Missiles.” In Proceedings of IEEE International Conference on Control and Applications. IEEE. https://doi.org/10.1109/cca.1993.348311
• Balasubramanian, R., Vaibhav Shah, Konark Arora, R. Krishnamurthy, and Debasis Chakraborty. 2013. “Numerical Investigations of Lateral Characteristics of an Air-to-Air Missile.” Journal of Aircraft 50 (1): 88–95. https://doi.org/10.2514/1.c031761
• Balasubramanian, Aswin, and Pankaj Shrivastava. 2020. “Trade-off between Sample Size and Test Time: Lessons Learned in Optimizing Reliability Demonstration Test Plan.” In 2020 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams48030.2020.9153592
• Ball, J. N. 1979. “Rolling Tail Design and Behavior as Affected by Actuator Hinge Moment Limits.” Journal of Aircraft 16 (8): 527–31. https://doi.org/10.2514/3.58559
• “Ballistic Missile Flight Testing.” 1981. Adelphi Papers 21 (165): 19–34. https://doi.org/10.1080/05679328108448596
• Bannink, W. J., and J. W. Reyn. 1968. “Lift and Drag Characteristics of a Delta-Wing-Half-Cone Configuration with Subsonic Leading Edges, Using Slender-Body Theory.” Journal of Engineering Mathematics 2 (2): 187–205. https://doi.org/10.1007/bf01535561
• Bao, Cunyu, Peng Wang, and Guojian Tang. 2021. “Integrated Method of Guidance, Control and Morphing for Hypersonic Morphing Vehicle in Glide Phase.” Chinese Journal of Aeronautics 34 (5): 535–53. https://doi.org/10.1016/j.cja.2020.11.009
• 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-Itzhack, I. Y., and Y. Vitek. 1985. “The Enigma of False Bias Detection in a Strapdown System during Transfer Alignment.” Journal of Guidance, Control, and Dynamics 8 (2): 175–80. https://doi.org/10.2514/3.19956
• Bardhan, Rajarshi, and Debasish Ghose. 2015. “Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law.” Journal of Guidance, Control, and Dynamics 38 (3): 384–402. https://doi.org/10.2514/1.g000940
• Barnwell, Richard W., and Richard A. Wahls. 1991. “Skin Friction Law for Compressible Turbulent Flow.” AIAA Journal 29 (3): 380–86. https://doi.org/10.2514/3.10589
• Barr, R. E., R. D. Hamlin, L. D. Abraham, and D. E. Greene. 1988. “Electromyographic Evaluation of Operator Performance in Manual Control Tracking.” In Proceedings of the Annual International Conference of the IEEE Engineering in Medicine and Biology Society. IEEE. https://doi.org/10.1109/iembs.1988.94761
• Barr, K., and E. J. Steeger. 1957. “Supersonic Rain Erosion Testing of Missile Radomes.” Journal of Jet Propulsion 27 (9): 1034–37. https://doi.org/10.2514/8.12440
• Barrère, M., and J. J. Bernard. 1957. “Influence of the Injector Pressure Drop on Low Frequency Instability in Liquid Propellant Rockets.” Symposium (International) on Combustion 6 (1): 487–92. https://doi.org/10.1016/s0082-0784(57)80065-4
• 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
• Barton, D. K. 1974. “Low-Angle Radar Tracking.” Proceedings of the IEEE 62 (6): 687–704. https://doi.org/10.1109/proc.1974.9509
• Bartusiak, Emily R., Hanxiang Hao, Michael A. Jacobs, et al. 2022. “A Stochastic Grammar Approach to Predict Flight Phases of a Hypersonic Glide Vehicle.” In 2022 IEEE Aerospace Conference (AERO). IEEE. https://doi.org/10.1109/aero53065.2022.9843362
• 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
• Basin, Michael A., Richard H. Macneal, and John H. Shields. 1959. “Direct-Analog Method of Analysis of the Influence of Aerodynamic Heating on the Static Characteristics of Thin Wings.” Journal of the Aerospace Sciences 26 (3): 145–54. https://doi.org/10.2514/8.7978
• Bass, Robert W. 1956. “Improved on-Off Missile Stabilization.” Journal of Jet Propulsion 26 (8): 644–48. https://doi.org/10.2514/8.7113
• Bazarov, Vladimir G., and Vigor Yang. 1998. “Liquid-Propellant Rocket Engine Injector Dynamics.” Journal of Propulsion and Power 14 (5): 797–806. https://doi.org/10.2514/2.5343
• Behara, Kali Charan, K. S. Akash, Shakeel Ahamed, and Satadal Ghosh. 2019. “Proportional Navigation-Benchmarked Guidance Strategy Using Artificial Neural Networks.” In 2019 IEEE 15th International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2019.8899623
• Belaidouni, Habib, Marija Samardžić, Saša Živković, and Mirko Kozić. 2017. “Computational Fluid Dynamics and Experimental Data Comparison of a Missile-Model Roll Derivative.” Journal of Spacecraft and Rockets 54 (3): 672–82. https://doi.org/10.2514/1.a33674
• Belkhouche, F., B. Belkhouche, and P. Rastgoufard. 2004. “A Linearized Model for the Line of Sight Guidance Law.” In PLANS 2004. Position Location and Navigation Symposium (IEEE Cat. No.04CH37556). IEEE. https://doi.org/10.1109/plans.2004.1308994
• Bell, Kristine L., Christopher J. Baker, Graeme E. Smith, Joel T. Johnson, and Muralidhar Rangaswamy. 2014a. “Fully Adaptive Radar for Target Tracking Part I: Single Target Tracking.” In 2014 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2014.6875604
• Bell, Kristine L., Christopher J. Baker, Graeme E. Smith, Joel T. Johnson, and Muralidhar Rangaswamy. 2014b. “Fully Adaptive Radar for Target Tracking Part II: Target Detection and Track Initiation.” In 2014 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2014.6875605
• Bell, Kristine L., Joel T. Johnson, Graeme E. Smith, Christopher J. Baker, and Muralidhar Rangaswamy. 2015. “Cognitive Radar for Target Tracking Using a Software Defined Radar System.” In 2015 IEEE Radar Conference (RadarCon). IEEE. https://doi.org/10.1109/radar.2015.7131213
• 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-Asher, Joseph Z., Nathan Farber, and Sergei Levinson. 2003. “New Proportional Navigation Law for Ground-to-Air Systems.” Journal of Guidance, Control, and Dynamics 26 (5): 822–25. https://doi.org/10.2514/2.5118
• Ben-Gida, Hadar. 2023a. “Detached Eddy Simulations of Cavity-Store Interactions at Subsonic Turbulent Flow.” Aerospace 10 (11): 935. https://doi.org/10.3390/aerospace10110935
• Bendotti, P., and M. M’Saad. 1991. “On the Adaptive Control of Missile Autopilots.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791450
• Benshabat, D. G., and A. Bar-Gill. 1995. “Robust Command-to-Line-of-Sight Guidance via Variable-Structure Control.” IEEE Transactions on Control Systems Technology 3 (3): 356–61. https://doi.org/10.1109/87.406984
• Benton, Edward R. 1964. “Supersonic Magnus Effect on a Finned Missile.” AIAA Journal 2 (1): 153–55. https://doi.org/10.2514/3.2252
• Bentsman, Joseph, Mark Wilcutts, and Ame J. Pearlstein. 1991. “Sensing and Actuation in a Liquid Propellant Rocket Engine.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791943
• Benz, Achim, Alexander Grundler, Thomas Herzig, Martin Dazer, and Bernd Bertsche. 2022. “Reliability Demonstration Test Planning for Field Load Spectra – an Approach for Identifying the Optimal Test Parameters Considering Individual Cost and Time Constraints.” In 2022 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams51457.2022.9894007
• Bera, Rajendra K. 1975. “On the Wave Drag Integral for Slender Bodies.” Journal of Aircraft 12 (11): 908–10. https://doi.org/10.2514/3.44499
• Berger, H. 1971. “Angular Accuracy of Amplitude Monopulse off-Boresight Radar.” Proceedings of the IEEE 59 (3): 411–12. https://doi.org/10.1109/proc.1971.8181
• Berger, Henry. 1972. “On the Optimum Squint Angles of Amplitude Monopulse Radar and Beacon Tracking Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-8 (4): 545–47. https://doi.org/10.1109/taes.1972.309555
• Bergkvist, B., and B.-E. Tullsson. n.d. “Track While Scan Monopulse-a Technique for Improving Angular Accuracy and Resolution.” In IEEE International Conference on Radar. IEEE. https://doi.org/10.1109/radar.1990.201203
• 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
• Bezick, Scott, Ilan Rusnak, and W. Steven Gray. 1995. “Guidance of a Homing Missile via Nonlinear Geometric Control Methods.” Journal of Guidance, Control, and Dynamics 18 (3): 441–48. https://doi.org/10.2514/3.21407
• Bhat, Sanketh, and Rick Lind. 2009. “Control-Oriented Analysis of Thermal Gradients for a Hypersonic Vehicle.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160180
• Bhattacharjee, Diganta, Animesh Chakravarthy, and Kamesh Subbarao. 2021. “Nonlinear Model Predictive Control and Collision-Cone-Based Missile Guidance Algorithm.” Journal of Guidance, Control, and Dynamics 44 (8): 1481–97. https://doi.org/10.2514/1.g005879
• Bhitre, Nitin, Achintya K. Sarkar, and Radhakant Padhi. 2013. “Three-Dimensional Impact Angle Constrained MPSP Guidance of Air-to-Air Missiles.” In 2013 IEEE International Conference on Control Applications (CCA). IEEE. https://doi.org/10.1109/cca.2013.6662862
• Bi, Wen-hao, An Zhang, and Shui-da Bao. 2015. “Dynamic Function Allocation Method for Aircraft Cockpit Based on Operator Functional State.” In 2015 15th International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.1109/iccas.2015.7364847
• 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
• Bieneck, Panu. 2026a. “On Pressures in the Liquid Propellant Rocket Engine Part I: An Alternative Calculation Method.” Journal of the British Interplanetary Society 79 (1): 8. https://doi.org/10.59332/jbis-079-01-0008
• Bieneck, Panu. 2026b. “On Pressures in the Liquid Propellant Rocket Engine Part II: An Experimental Review.” Journal of the British Interplanetary Society 79 (1): 12–16. https://doi.org/10.59332/jbis-079-01-0012
• 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
• Bikas, Lampros N., Antonis Sidiropoulos, George A. Rovithakis, and Zoe Doulgeri. 2023. “Model-Free Control of Bilateral Robotic Teleoperation with Delays and Prescribed Performance Guarantees.” IFAC-PapersOnLine 56 (2): 9972–77. https://doi.org/10.1016/j.ifacol.2023.10.700
• “Bilateral Matched Impedance Teleoperation with Application to Excavator Control.” 1999. IEEE Control Systems 19 (6): 29–37. https://doi.org/10.1109/37.806913
• Bilik, I., and J. Tabrikian. 2006. “Target Tracking in Glint Noise Environment Using Nonlinear Non-Gaussian Kalman Filter.” In 2006 IEEE Conference on Radar. IEEE. https://doi.org/10.1109/radar.2006.1631813
• Bin, Meng, and Wu Hongxin. 2006. “Adaptive Control Based on Characteristic Model for a Hypersonic Flight Vehicle.” In 2007 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.4346800
• Bingyi, Fang, and Wu Siliang. 2008. “Multiple Targets Vector Miss Distance Measurement Accuracy Based on 2-D Assignment Algorithms.” Journal of Systems Engineering and Electronics 19 (1): 76–80. https://doi.org/10.1016/s1004-4132(08)60049-3
• Bishop, Wayne S. 1977. “Electrochemical Battery Trends for Aircraft and Missile Applications.” Journal of Aircraft 14 (9): 922–23. https://doi.org/10.2514/3.58873
• Biyikli, Rabiya, Raziye Tekin, and Ilkay Yavrucuk. 2022. “Control Allocation Strategies for a Hybrid Controlled Missile with NDI Autopilot.” In 2022 13th Asian Control Conference (ASCC). IEEE. https://doi.org/10.23919/ascc56756.2022.9828187
• Black, Robert L. 1969. “High-Speed Store Separation: Correlation between Wind-Tunnel and Flight-Test Data.” Journal of Aircraft 6 (1): 42–45. https://doi.org/10.2514/3.43999
• Black, David G., Dragan Andjelic, and Septimiu E. Salcudean. 2024. “Evaluation of Communication and Human Response Latency for (Human) Teleoperation.” IEEE Transactions on Medical Robotics and Bionics 6 (1): 53–63. https://doi.org/10.1109/tmrb.2024.3349612
• Blair, A. B., James L. Dillon, and Carolyn B. Watson. 1993. “Experimental Study of Tail-Span Effects on a Canard-Controlled Missile.” Journal of Spacecraft and Rockets 30 (5): 635–40. https://doi.org/10.2514/3.25576
• 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
• 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
• Bleier, Michael, Ferdinand Settele, Markus Krauss, Alexander Knoll, and Klaus Schilling. 2015. “Risk Assessment of Flight Paths for Automatic Emergency Parachute Deployment in UAVs.” IFAC-PapersOnLine 48 (9): 180–85. https://doi.org/10.1016/j.ifacol.2015.08.080
• 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
• 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
• Boer, E. R., and R. V. Kenyon. 1998. “Estimation of Time-Varying Delay Time in Nonstationary Linear Systems: An Approach to Monitor Human Operator Adaptation in Manual Tracking Tasks.” IEEE Transactions on Systems, Man, and Cybernetics - Part A: Systems and Humans 28 (1): 89–99. https://doi.org/10.1109/3468.650325
• Boison, J. Christopher. 1953. “Mean Skin-Friction Coefficients for Biconvex Airfoils in Supersonic Flow.” Journal of the Aeronautical Sciences 20 (11): 787–787. https://doi.org/10.2514/8.2840
• Bolat, Fevzi Çakmak, and Mustafa Cem Avci. 2025. “Development and Validation of a Human-Machine Interface for Unmanned Aerial Vehicle (UAV) Control via Hand Gesture Teleoperation.” Expert Systems with Applications 273: 126828. https://doi.org/10.1016/j.eswa.2025.126828
• Bolz, Ray E., and John D. Nicolaides. 1950. “A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling Missile.” Journal of the Aeronautical Sciences 17 (10): 609–21. https://doi.org/10.2514/8.1748
• 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
• 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
• Borden, Brett, and Michael Mumford. 1983. “A Statistical Glint/Radar Cross Section Target Model.” IEEE Transactions on Aerospace and Electronic Systems AES-19 (5): 781–85. https://doi.org/10.1109/taes.1983.309383
• Borovik, Igor, Evgeniy Strokach, Alexander Kozlov, et al. 2019. “Influence of Polyisobutylene Kerosene Additive on Combustion Efficiency in a Liquid Propellant Rocket Engine.” Aerospace 6 (12): 129. https://doi.org/10.3390/aerospace6120129
• Bortoloto, Evandro Rostirolla, Francisco Carlos Parquet Bizarria, and José Walter Parquet Bizarria. 2023. “Petri Nets Applied in Purge Algorithm Analysis for a Rocket Engine Test with Liquid Propellant.” Aerospace 10 (3): 212. https://doi.org/10.3390/aerospace10030212
• Borzov, V. Yu., I. V. Rybka, and A. S. Yur’ev. 1992. “Estimation of Energy Consumption for Body Drag Reduction in a Supersonic Flow.” Journal of Engineering Physics and Thermophysics 63 (6): 1171–75. https://doi.org/10.1007/bf00853515
• Bos, J. F. T., H. G. Stassen, and A. van Lunteren. 1992. “Aiding the Operator in the Manual Control of a Space Manipulator.” IFAC Proceedings Volumes 25 (9): 215–20. https://doi.org/10.1016/s1474-6670(17)50195-0
• Bos, J. F. T., H. G. Stassen, and A. van Lunteren. 1995. “Aiding the Operator in the Manual Control of a Space Manipulator.” Control Engineering Practice 3 (2): 223–30. https://doi.org/10.1016/0967-0661(94)00080-z
• Bosarge, W. E. 1966. “Application of a Multivariate Error Model in Measuring Accuracies of Radar Tracking Configurations.” IEEE Transactions on Aerospace and Electronic Systems AES-2 (4): 529–39. https://doi.org/10.1109/taes.1966.4501885
• Bossi, J. A., and M. A. Langehough. 1988. “Multivariable Autopilot Designs for a Bank-to-Turn Missile.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789784
• Botturi, D., A. Castellani, D. Moschini, and P. Fiorini. 2004. “Performance Evaluation of Task Control in Teleoperation.” In IEEE International Conference on Robotics and Automation, 2004. Proceedings. ICRA ‘04. 2004. IEEE. https://doi.org/10.1109/robot.2004.1308833
• Boumenir, A. 2005. “Sampling the Miss-Distance and Transmission Function.” Journal of Mathematical Analysis and Applications 310 (1): 197–208. https://doi.org/10.1016/j.jmaa.2005.02.001
• Bradshaw, P. 1977. “An Improved Van Driest Skin-Friction Formula for Compressible Turbulent Boundary Layers.” AIAA Journal 15 (2): 212–14. https://doi.org/10.2514/3.7315
• Breckenridge, W. G., and A. J. Treder. 1978. “In-Flight Gyro Drift Rate Calibration on the Viking Orbiters.” Journal of Guidance and Control 1. https://ntrs.nasa.gov/citations/19790028598
• Brennan, L. 1961. “Angular Accuracy of a Phased Array Radar.” IRE Transactions on Antennas and Propagation 9 (3): 268–75. https://doi.org/10.1109/tap.1961.1145000
• Brito, Antonio, Pedro Sebastiao, and Nuno Souto. 2019. “Jamming for Unauthorized UAV Operations-Communications Link.” In 2019 International Young Engineers Forum (YEF-ECE). IEEE. https://doi.org/10.1109/yef-ece.2019.8740828
• Brockner, C. E. 1951. “Angular Jitter in Conventional Conical-Scanning, Automatic-Tracking Radar Systems.” Proceedings of the IRE 39 (1): 51–55. https://doi.org/10.1109/jrproc.1951.230421
• Bromberg, M. C., and I. F. Progri. 2006. “An Anti-Jam GPS Receiver, Using Markov Chain, Monte Carlo Integration.” In 2006 IEEE/ION Position, Location, And Navigation Symposium. IEEE. https://doi.org/10.1109/plans.2006.1650696
• Brooker, G. M. 2003. “Conical-Scan Antennas for W-Band Radar Systems.” In 2003 Proceedings of the International Conference on Radar (IEEE Cat. No.03EX695). IEEE. https://doi.org/10.1109/radar.2003.1278776
• Brower, H. P. 1959. “Missile-Borne Frequency Standard.” In 13th Annual Symposium on Frequency Control. IEEE. https://doi.org/10.1109/freq.1959.199381
• Brown, R. S., and R. J. Muzzy. 1970. “Linear and Nonlinear Pressure Coupled Combustion Instability of Solid Propellants.” AIAA Journal 8 (8): 1492–1500. https://doi.org/10.2514/3.5929
• 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
• Brugarolas, P. B., V. Fromion, and M. G. Safonov. 1998. “Robust Switching Missile Autopilot.” In Proceedings of the 1998 American Control Conference. ACC (IEEE Cat. No.98CH36207). IEEE. https://doi.org/10.1109/acc.1998.703297
• Brummund, U., A. Cessou, and A. Vogel. 1996. “Plif Imaging Measurements of a Co-Axial Rocket Injector Spray at Elevated Pressure.” Symposium (International) on Combustion 26 (1): 1687–95. https://doi.org/10.1016/s0082-0784(96)80393-6
• Brunner, Thomas W., and Robert M. Nerem. 1971. “Theoretical Drag Prediction for Trailing Decelerators at Supersonic Speeds.” Journal of Aircraft 8 (12): 1022–28. https://doi.org/10.2514/3.59200
• Bryson, A. E., and R. H. Edwards. 1952. “The Effect of Nonuniform Surface Temperature on the Transient Aerodynamic Heating of Thin-Skinned Bodies.” Journal of the Aeronautical Sciences 19 (7): 471–75. https://doi.org/10.2514/8.2343
• Bucco, D., and M. Weiss. 2015. “Adjoint Analysis of Guidance Systems with Nonstandard Inputs.” Journal of Guidance, Control, and Dynamics 38 (9): 1800–1809. https://doi.org/10.2514/1.g001010
• Budiansky, Bernard, and J. Mayers. 1956. “Influence of Aerodynamic Heating on the Effective Torsional Stiffness of Thin Wings.” Journal of the Aeronautical Sciences 23 (12): 1081–93. https://doi.org/10.2514/8.3735
• Bulat, P. V., A. I. Musteikis, N. V. Prodan, M. E. Renev, and K. N. Volkov. 2024. “Simulation of Intra-Chamber Processes in a Low-Thrust Rocket Engine with a Hydrogen-Air Mixture and Counterflow Cooling.” Acta Astronautica 225: 243–51. https://doi.org/10.1016/j.actaastro.2024.09.029
• Burchett, Bradley T. 2019. “Unscented Kalman Filters for Range-Only Cooperative Localization of Swarms of Munitions in Three-Dimensional Flight.” Aerospace Science and Technology 85: 259–69. https://doi.org/10.1016/j.ast.2018.12.015
• Burdett, Harry W. 1946. “The Variable Nozzle as a Means of Maintaining Rocket Engine Efficiency When Throttling.” Journal of the American Rocket Society 00 (68): 39–41. https://doi.org/10.2514/8.4117
• 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
• 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
• Bużantowicz, Witold. 2021. “Tuning of a Linear-Quadratic Stabilization System for an Anti-Aircraft Missile.” Aerospace 8 (2): 48. https://doi.org/10.3390/aerospace8020048
• Bye, Andreas, Erik Hollnagel, and Tor Steinar Brendeford. 1999. “Human–machine Function Allocation: A Functional Modelling Approach.” Reliability Engineering & System Safety 64 (2): 291–300. https://doi.org/10.1016/s0951-8320(98)00069-6
• 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
• Cai, Changxin, Fangqing Wen, and Dongmei Huang. 2018. “New Approach to Angle Estimation for Bistatic MIMO Radar with Unknown Spatially Colored Noise.” IEEE Access 6: 24249–55. https://doi.org/10.1109/access.2018.2829537
• 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
• Calise, Anthony J. 1980. “Optimal Thrust Control with Proportional Navigation Guidance.” Journal of Guidance and Control 3 (4): 312–18. https://doi.org/10.2514/3.55995
• Campbell, J. F. 1963. “Mechanical Design of an Advanced Missile Guidance Beacon.” Proceedings of the IEEE 51 (3): 515–515. https://doi.org/10.1109/proc.1963.1977
• Camplani, S., G. Petrillo, and D. Pistoia. 2001. “Best Management of FM Waveform by a Missile-Borne Pulsed Doppler Radar during High-Manoeuvring Target Tracking in Strong Clutter Environment.” In Proceedings of the 2001 IEEE Radar Conference (Cat. No.01CH37200). IEEE. https://doi.org/10.1109/nrc.2001.923002
• Can Rao, Rongfeng Li, and Lingyan Dai. 2011. “Monopulse Estimation with Multipoint Constrained Adaptation in Mainlobe Jamming.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159733
• 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
• Canellas, Marc C., and Rachel A. Haga. 2015. “Toward Meaningful Human Control of Autonomous Weapons Systems through Function Allocation.” In 2015 IEEE International Symposium on Technology and Society (ISTAS). IEEE. https://doi.org/10.1109/istas.2015.7439432
• Cao, Ruihao, Tuo Han, Chaoyong Li, and Shaoming He. 2026. “Analytical 3D Proportional Navigation Guidance for Field-of-View Constrained Impact Time Control.” Aerospace Science and Technology 172: 111680. https://doi.org/10.1016/j.ast.2026.111680
• Cao, Rui, and Huitao Lyu. 2024. “A Hinge Moment Alleviation Control Strategy for Morphing Tail Aircraft Based on a Data-Driven Method.” Actuators 13 (9): 369. https://doi.org/10.3390/act13090369
• Cao Yuan, Fang Weihua, Li Lin, Tian Keyu, and Yang Jin. 2011. “A Quantitive Method to Assess Monopulse Radar Seeker Angle Measurement Performance in the Presence of Noise Jamming.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159934
• Cary, Aubrey M., and Jerry N. Hefner. 1972. “Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow.” AIAA Journal 10 (9): 1188–93. https://doi.org/10.2514/3.50348
• Casavola, Alessandro, and Edoardo Mosca. 2004. “Bank-to-Turn Missile Autopilot Design via Observer-Based Command Governor Approach.” Journal of Guidance, Control, and Dynamics 27 (4): 705–10. https://doi.org/10.2514/1.11163
• Casiano, Matthew J., James R. Hulka, and Vigor Yang. 2010. “Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review.” Journal of Propulsion and Power 26 (5): 897–923. https://doi.org/10.2514/1.49791
• Casler, Richard James, Jr. 1978. “Dual-Control Guidance Strategy for Homing Interceptors Taking Angle-Only Measurements.” Journal of Guidance and Control 1 (1): 63–70. https://doi.org/10.2514/3.55744
• Catovic, Alan, and Elvedin Kljuno. 2021. “A Novel Method for Determination of Lethal Radius for High-Explosive Artillery Projectiles.” Defence Technology 17 (4): 1217–33. https://doi.org/10.1016/j.dt.2020.06.015
• Cen, Haodi, Ting Shu, Jin He, and Wenxian Yu. 2025. “Adaptive Subarray Digital Beamforming with Robust Mainlobe Maintenance for Monopulse Angle Estimation in Complicated Jamming Environments.” In 2025 IEEE International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar52380.2025.11031522
• 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
• Cha, Jihyoung, Erik Andersson, and Alexis Bohlin. 2023. “A Numerical Approach to Optimize the Design of a Pintle Injector for LOX/GCH4 Liquid-Propellant Rocket Engine.” Aerospace 10 (7): 582. https://doi.org/10.3390/aerospace10070582
• Cha, Jihyoung, Sangho Ko, and Soon-Young Park. 2024. “Particle-Filter-Based Fault Diagnosis for the Startup Process of an Open-Cycle Liquid-Propellant Rocket Engine.” Sensors 24 (9): 2798. https://doi.org/10.3390/s24092798
• Chadwick, W. R. 1985. “Miss Distance of Proportional Navigation Missile with Varying Velocity.” Journal of Guidance, Control, and Dynamics 8 (5): 662–66. https://doi.org/10.2514/3.20038
• Chan, Tobias. 2026. “LeCal: Latency-Aware Curation and Alignment for LeRobot Teleoperation Datasets.” In 2026 IEEE 20th International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca69928.2026.11618027
• 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
• Chang, Jen-Fu. 1992. “Minimizing Supersonic Wave Drag with Physical Constraints at Design and off-Design Mach Numbers.” Journal of Aircraft 29 (4): 716–18. https://doi.org/10.2514/3.46228
• Chang, Jing, Jérôme Cieslak, Ali Zolghadri, Jorge Dávila, and Jun Zhou. 2016. “Quadrotor Attitude Estimation with Gyroscope Bias Reconstruction Capabilities.” IFAC-PapersOnLine 49 (5): 260–65. https://doi.org/10.1016/j.ifacol.2016.07.123
• 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, D.-C., W. Rusch, and F. Young. 1979. “Gregorian Corrected Offset Fed Reflector with Conical Scan Capability.” In 1979 Antennas and Propagation Society International Symposium, vol. 17. Institute of Electrical and Electronics Engineers. https://doi.org/10.1109/aps.1979.1148144
• Chang-Kyung Ryoo, Hangju Cho, and Min-Jea Tahk. 2003. “Closed-Form Solutions of Optimal Guidance with Terminal Impact Angle Constraint.” In Proceedings of 2003 IEEE Conference on Control Applications, 2003. CCA 2003.. IEEE. https://doi.org/10.1109/cca.2003.1223469
• Chao, Wang, Yin Hongcheng, and Huang Peikang. 2008. “Comparison between Two Concepts of Angular Glint: General Considerations.” Journal of Systems Engineering and Electronics 19 (4): 635–42. https://doi.org/10.1016/s1004-4132(08)60132-2
• 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
• Chapman, Dean R., and Robert H. Kester. 1953. “Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic Velocities.” Journal of the Aeronautical Sciences 20 (7): 441–48. https://doi.org/10.2514/8.2688
• “Chapter One: Chinese and Russian Air-Launched Weapons: A Test for Western Air Dominance.” 2018. Military Balance 118 (1): 7–18. https://doi.org/10.1080/04597222.2018.1416966
• Chaudhry, Akanksha, Nagendra Kumar, Sudarshan Kumar, Rohit Sehrawat, and Arvind Kumar. 2026. “Experimental Studies on Pulse-Triggered Combustion Instability in Solid Rocket Motor.” Combustion Science and Technology: 1–14. https://doi.org/10.1080/00102202.2026.2667319
• Cheah, Sze Kwan, Diganta Bhattacharjee, Maziar S. Hemati, and Ryan J. Caverly. 2025. “Control Synthesis for Hypersonic Vehicle Flight Testing with Input–Output-Sampled Nonlinearities.” Journal of Guidance, Control, and Dynamics 48 (4): 855–69. https://doi.org/10.2514/1.g008331
• Chehroudi, Bruce. 2010. “Physical Hypothesis for the Combustion Instability in Cryogenic Liquid Rocket Engines.” Journal of Propulsion and Power 26 (6): 1153–60. https://doi.org/10.2514/1.38451
• Chelaru, Teodor-Viorel, Cristian Emil Constantinescu, Valentin Pană, and Costin Ene. 2025a. “Stability of a Single-Channel Rolling Aerospace Vehicle with Semi-Automatic Command to Line of Sight.” Aerospace 12 (10): 921. https://doi.org/10.3390/aerospace12100921
• Chen, Chen, Guobiao Cai, Xiaoyang Hu, et al. 2026c. “Optical Diagnostics of Liquid Contamination in Liquid Propellant Rocket Engine Plumes: Part I–liquid Film Evolution on Engine Walls.” Aerospace Science and Technology 177: 112266. https://doi.org/10.1016/j.ast.2026.112266
• 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, Bin, Tongxin Dang, Kaibin Zhagn, and Yiming Li. 2026d. “Scattered Field Calculation and Angular Glint Analysis in near-Field Region.” Journal of Systems Engineering and Electronics 37 (1): 104–11. https://doi.org/10.23919/jsee.2025.000056
• Chen, Yadong, Xiangjun Ding, Jianan Wang, Chunyan Wang, and Jiayuan Shan. 2021c. “Impact Time Constrained Cooperative Guidance Law Design via Line-of-Sight Shaping.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550043
• Chen, Jian, Nannan Du, and Yu Han. 2020a. “Decoupling Attitude Control of a Hypersonic Glide Vehicle Based on a Nonlinear Extended State Observer.” International Journal of Aerospace Engineering 2020: 1–11. https://doi.org/10.1155/2020/4905698
• Chen, Shiwei, Junfang Fan, Wei Wang, Yi Ji, and Ning Liu. 2022c. “Terminal Impact-Angle-Constrained Guidance Law of Miniature Munition Based on High-Order Fully Actuated System Approach.” In 2022 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac57257.2022.10055130
• Chen, Erkang, Changsheng Gao, and Wuxing Jing. 2016b. “Virtual Displacement Guidance for Hypersonic Glide Vehicle.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554180
• Chen, Rumeng, Siyuan He, Yunhua Zhang, and Yan Zhu. 2023a. “Angular Glint Calculation Based on Forward Attributed Scattering Center Models.” In 2023 International Applied Computational Electromagnetics Society Symposium (ACES-China). IEEE. https://doi.org/10.23919/aces-china60289.2023.10249645
• Chen, Wenxue, Yudong Hu, Changsheng Gao, and Ruoming An. 2024. “Trajectory Tracking Guidance of Interceptor via Prescribed Performance Integral Sliding Mode with Neural Network Disturbance Observer.” Defence Technology 32: 412–29. https://doi.org/10.1016/j.dt.2023.07.018
• 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, Jeng-Heng, Sou-Chen Lee, and Daniel B. DeBra. 1994. “Gyroscope Free Strapdown Inertial Measurement Unit by Six Linear Accelerometers.” Journal of Guidance, Control, and Dynamics 17 (2): 286–90. https://doi.org/10.2514/3.21195
• Chen, Xinbo, Yaohua Li, Siming Guo, and Yu Pan. 2026b. “Error Correction Method for Maneuvering Target Tracking of Pulse Radar Based on Adaptive Interacting Multiple Model.” In 2026 2nd International Conference on Navigation, Detection and Control (CNDC). IEEE. https://doi.org/10.1109/cndc70899.2026.11707966
• Chen, Han, Kewei Li, Chao Wang, et al. 2017a. “Analysis of Aerodynamic Characteristics of a Modular Assembled Missile with Canard Rudder and Arc Tail.” In 2017 9th International Conference on Modelling, Identification and Control (ICMIC). IEEE. https://doi.org/10.1109/icmic.2017.8321598
• Chen, Haifei, and Zhengxiong Liu. 2021. “Time-Delay Prediction–Based Smith Predictive Control for Space Teleoperation.” Journal of Guidance, Control, and Dynamics 44 (4): 872–79. https://doi.org/10.2514/1.g005714
• Chen, Sitong, Yaiun Meng, Jun Tu, Longfei Wu, Xiaomin Chen, and Tianxu Qi. 2023b. “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, Chiung-Chu, Michael J. Nusca, Anthony J. Kotlar, and Michael J. McQuaid. 2009. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2009 DoD High Performance Computing Modernization Program Users Group Conference. IEEE. https://doi.org/10.1109/hpcmp-ugc.2009.25
• Chen, Hao, Liping Pang, Xiaoru Wanyan, Shuang Liu, Yufeng Fang, and Da Tao. 2021b. “Effects of Air Route Alternation and Display Design on an Operator’s Situation Awareness, Task Performance and Mental Workload in Simulated Flight Tasks.” Applied Sciences 11 (12): 5745. https://doi.org/10.3390/app11125745
• Chen, Kai, Sensen Pei, Fuqiang Shen, and Shangbo Liu. 2021e. “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, Liang, and Weixing Sheng. 2010. “Performance Analysis for Angle Measurement of Monopulse Radar with Non-Consistent Amplitude-Phase Features.” In 2010 International Conference on Microwave and Millimeter Wave Technology. IEEE. https://doi.org/10.1109/icmmt.2010.5524773
• Chen, Xinzhu, Ting Shu, Kai-Bor Yu, and Wenxian Yu. 2016a. “Multiple Jamming Cancellation Using Adaptive Subarray DBF for Monopulse Angle Estimation.” In 2016 IEEE International Symposium on Phased Array Systems and Technology (PAST). IEEE. https://doi.org/10.1109/array.2016.7832661
• Chen, Xinzhu, Ting Shu, Kai-Bor Yu, and Wenxian Yu. 2017b. “Enhanced ADBF Architecture for Monopulse Angle Estimation in Multiple Jammings.” IEEE Antennas and Wireless Propagation Letters 16: 2684–87. https://doi.org/10.1109/lawp.2017.2740958
• Chen, Robert H., Jason L. Speyer, and Dimitrios Lianos. 2007b. “Homing Missile Guidance and Estimation under Agile Target Acceleration.” Journal of Guidance, Control, and Dynamics 30 (6): 1577–89. https://doi.org/10.2514/1.30107
• Chen, Wenxue, Peng Sui, Yingjing Qian, and Changsheng Gao. 2026a. “Cubic Bézier Shaping Impact Angle Constrained Guidance for Intercepting Maneuvering Targets.” Nonlinear Dynamics 114 (3): 192. https://doi.org/10.1007/s11071-025-12057-4
• Chen, Zhe, Shengjing Tang, and Jie Guo. 2014b. “Three-Dimensional Optimal Sliding Mode Guidance with Impact Angle Constraint.” In Proceeding of the 11th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2014.7053392
• Chen, Xiaotian, and Jinzhi Wang. 2017. “Optimal Control Based Guidance Law with Impact Angle Constraint.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028310
• Chen, Xiaotian, and Jinzhi Wang. 2018. “Field-of-View Constrained Impact Angle Control Guidance Law against Stationary Targets.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483273
• Chen, Shiwei, Wei Wang, Junfang Fan, and Yi Ji. 2023c. “Impact Angle Constraint Guidance Law Using Fully-Actuated System Approach.” Aerospace Science and Technology 136: 108220. https://doi.org/10.1016/j.ast.2023.108220
• Chen, Lin, Song Wang, Chao Li, Hong-Xu Zhang, and Guan-Jun Yang. 2025a. “Durable RSZ/YSZ Coatings with 1600 °C Thermal Shock Resistance for Rocket Engine Thrust Chamber Applications.” Ceramics International 51 (27): 54903–13. https://doi.org/10.1016/j.ceramint.2025.09.216
• Chen, Yadong, Jianan Wang, Jiayuan Shan, and Ming Xin. 2021a. “Cooperative Guidance for Multiple Powered Missiles with Constrained Impact and Bounded Speed.” Journal of Guidance, Control, and Dynamics 44 (4): 825–41. https://doi.org/10.2514/1.g005578
• Chen, Yadong, Jianan Wang, Chunyan Wang, Jiayuan Shan, and Ming Xin. 2020h. “Three-Dimensional Cooperative Homing Guidance Law with Field-of-View Constraint.” Journal of Guidance, Control, and Dynamics 43 (2): 389–97. https://doi.org/10.2514/1.g004681
• Chen, Po-Yu, and Wen-Jong Wu. 2009. “Toward a Human Nature Based Automation System with Dynamic Function Allocation Model Supported for Pervasive Systems.” In 2009 10th International Symposium on Pervasive Systems, Algorithms, and Networks. IEEE. https://doi.org/10.1109/i-span.2009.129
• Chen, Ye, Shufan Wu, and Xiaoliang Wang. 2022a. “Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint.” Journal of Guidance, Control, and Dynamics 45 (12): 2369–78. https://doi.org/10.2514/1.g007030
• Chen, Dalin, Yiren Yang, and Chenguang Fan. 2008b. “Nonlinear Flutter of a Two-Dimension Thin Plate Subjected to Aerodynamic Heating by Differential Quadrature Method.” Acta Mechanica Sinica 24 (1): 45–50. https://doi.org/10.1007/s10409-007-0130-1
• Chen, Jian, Zichao Zhang, Ke Yi, Yu Han, and Zhang Ren. 2022b. “Snake-Hot-Eye-Assisted Multi-Process-Fusion Target Tracking Based on a Roll-Pitch Semi-Strapdown Infrared Imaging Seeker.” Journal of Bionic Engineering 19 (4): 1124–39. https://doi.org/10.1007/s42235-022-00195-z
• Chen, Kai, Jun Zhou, Fu-Qiang Shen, Han-Yan Sun, and Hao Fan. 2020b. “Hypersonic Boost–glide Vehicle Strapdown Inertial Navigation System / Global Positioning System Algorithm in a Launch-Centered Earth-Fixed Frame.” Aerospace Science and Technology 98: 105679. https://doi.org/10.1016/j.ast.2020.105679
• Chen Jianwen, Xu Dihua, and Liu Bingqi. 2006. “Performance Analysis of Meter Band Radar Height-Finding Approach for Low-Angle Tracking.” In 2006 IEEE Antennas and Propagation Society International Symposium. IEEE. https://doi.org/10.1109/aps.2006.1710742
• Chen Peng and Sentang Wu. 2008. “Guidance Law Design for Air-to-Surface Missile to Attack Low Velocity Target.” In 2008 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2008.4598010
• Chen Qihong, Fei Shumin, and Song Aiguo. 2003. “Robust Control with Observer of Internet-Based Teleoperation.” In Proceedings of the 2003 American Control Conference, 2003., vol. 1. IEEE. https://doi.org/10.1109/acc.2003.1239088
• 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
• Cheng, Sin-I. 1956. “High-Frequency Combustion Instability in Liquid Propellant Rocket with Concentrated Combustion and Distributed Time Lag.” Journal of Jet Propulsion 26 (2): 87–92. https://doi.org/10.2514/8.6930
• Cheng, Ting, and Congchong Cao. 2023. “Kalman Filter Based on Intermediate Transition State for Radar Target Tracking with Nonlinear Measurements.” Digital Signal Processing 143: 104251. https://doi.org/10.1016/j.dsp.2023.104251
• Cheng, Ruizhou, Panfeng Huang, and Zhenyu Lu. 2017a. “Adaptive Teleoperation Control Method Based on RBF-Neural Networks and Performance Analysis.” In 2017 IEEE International Conference on Real-time Computing and Robotics (RCAR). IEEE. https://doi.org/10.1109/rcar.2017.8311911
• Cheng, Peng, Qinglian Li, Zhongtao Kang, and Xinqiao Zhang. 2016. “Combustion Dynamics of an Extreme Fuel-Rich Throttleable Rocket Engine during Continuously Throttling Process.” Combustion Science and Technology 189 (4): 717–31. https://doi.org/10.1080/00102202.2016.1248238
• Cheng, Peng, Qinglian Li, Jiping Wu, and Zhongtao Kang. 2018. “Dynamic Response of a Dual-Manifold Injector Rocket Engine to Throttling.” Journal of Propulsion and Power 34 (6): 1553–60. https://doi.org/10.2514/1.b36799
• Cheng, Zhongtao, Bo Wang, Lei Liu, and Yongji Wang. 2019. “Adaptive Polynomial Guidance with Impact Angle Constraint under Varying Velocity.” IEEE Access 7: 104210–17. https://doi.org/10.1109/access.2019.2930001
• Cheng, Yuanbing, Rusheng Yu, Hong Gu, and Weimin Su. 2013. “Multi-SVD Based Subspace Estimation to Improve Angle Estimation Accuracy in Bistatic MIMO Radar.” Signal Processing 93 (7): 2003–9. https://doi.org/10.1016/j.sigpro.2012.12.021
• Chengzeng, Chen, Liu Dan, Xu Xiaojian, and Lu Yaobing. 2025. “A Processing Technique for Accurate Target Angle Estimation Using Wideband Monopulse Radars.” Journal of Systems Engineering and Electronics 36 (2): 370–79. https://doi.org/10.23919/jsee.2024.000091
• Cherkauer, Samuel A., Carson J. Karle, Evan M. Hiland, et al. 2025. “Design and Flight Test of an Air-Launched Medical Aid Delivery Uncrewed Aerial Vehicle.” Aerospace 12 (11): 977. https://doi.org/10.3390/aerospace12110977
• Chew, Victor, and Ray Boyce. 1962. “Distribution of Radial Error in the Bivariate Elliptical Normal Distribution.” Technometrics 4 (1): 138. https://doi.org/10.2307/1266181
• Chi, Haihong, Lianghua Wang, and Xingyi Liu. 2021. “Disturbance Compensation Based Backstepping Control for Hypersonic Vehicle.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550037
• 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, Tan Kok. 2000. “Grid Survey Approach to Store Separation Trajectory Prediction.” Journal of Aircraft 37 (4): 736–38. https://doi.org/10.2514/2.2662
• 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
• Chithapuram, Chethan, Yogananda Jeppu, and Cherukuri Aswani Kumar. 2013. “Artificial Intelligence Learning Based on Proportional Navigation Guidance.” In 2013 International Conference on Advances in Computing, Communications and Informatics (ICACCI). IEEE. https://doi.org/10.1109/icacci.2013.6637338
• Cho, Namhoon. 2021. “Nonlinear Optimal Missile Guidance for Stationary Target Interception with Pendulum Motion Perspective.” In 2021 American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc50511.2021.9483418
• Cho, Sungjin. 2022. “Analytic Solution for Nonlinear Impact-Angle Guidance Law with Time-Varying Thrust.” Mathematics 10 (21): 4034. https://doi.org/10.3390/math10214034
• Cho, Namhoon, and Youdan Kim. 2016. “Modified Pure Proportional Navigation Guidance Law for Impact Time Control.” Journal of Guidance, Control, and Dynamics 39 (4): 852–72. https://doi.org/10.2514/1.g001618
• Cho, Namhoon, Jinrae Kim, and Seokwon Lee. 2020. “Feasible Initial Conditions for Bias Proportional Navigation Guidance Laws under Look Angle Constraints.” In 2020 28th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med48518.2020.9183280
• Cho, Namhoon, Jinrae Kim, Seokwon Lee, and Youdan Kim. 2022. “Generalized Analysis of Biased Proportional Navigation Guidance with Fractional Power Error Feedback.” Journal of Guidance, Control, and Dynamics 45 (9): 1598–1613. https://doi.org/10.2514/1.g006850
• Cho, Dongsoo, H. Jin Kim, and Min-jea Tahk. 2015. “Impact Angle Constrained Sliding Mode Guidance against Maneuvering Target with Unknown Acceleration.” IEEE Transactions on Aerospace and Electronic Systems 51 (2): 1310–23. https://doi.org/10.1109/taes.2015.140358
• Cho, Namhoon, and Seokwon Lee. 2021. “Look-Angle-Constrained Control of Arrival Time with Exact Knowledge of Time-to-Go.” Journal of Guidance, Control, and Dynamics 44 (10): 1902–8. https://doi.org/10.2514/1.g006000
• Cho, Hangju, Chang Kyung Ryoo, and Min-Jea Tahk. 1999. “Implementation of Optimal Guidance Laws Using Predicted Missile Velocity Profiles.” Journal of Guidance, Control, and Dynamics 22 (4): 579–88. https://doi.org/10.2514/2.4420
• Choe, Sangho, Euny Ko, and Janghyuk Lee. 2014. “Tactical Data Link with Cognitive Anti-Jamming Capability and Its Simulator.” In International Symposium on Performance Evaluation of Computer and Telecommunication Systems (SPECTS 2014). IEEE. https://doi.org/10.1109/spects.2014.6880000
• Choi, Wonhong, and Sunghun Jung. 2019. “Launch Performance Degradation of the Rupture-Type Missile Canister.” Applied Sciences 9 (7): 1290. https://doi.org/10.3390/app9071290
• 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
• Choudhary, Aman, A. Vivek, and Satadal Ghosh. 2023. “Proportional Navigation-Based Guidance for an Autonomous Interdiction Mission against a Stationary Target.” In 2023 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas57906.2023.10155962
• 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
• Christopher, P. A. T. 1980. “Roll-Attitude Control of a Missile Having a Strong Aerodynamic Non-Linearity.” International Journal of Control 31 (2): 209–18. https://doi.org/10.1080/00207178008961038
• Chu, Wei, Kangkang Guo, Yiheng Tong, Yongjie Ren, Boqi Xu, and Wansheng Nie. 2025. “Longitudinal Combustion Instability in a Hypergolic Liquid Bipropellant Combustor with Single Dual-Swirl Coaxial Injector.” Chinese Journal of Aeronautics 38 (3): 103274. https://doi.org/10.1016/j.cja.2024.10.006
• Chung, J. C., and E. Y. Shapiro. 1982. “Modal Synthesis of Missile Autopilot Control Law.” In 1982 American Control Conference. IEEE. https://doi.org/10.23919/acc.1982.4788041
• Chunpeng, Shi, He Junxiu, Han Xiaofei, and Zhang Xiaoyu. 2022. “Research on Anti-Jamming Technology of Missile-Borne Radar Seeker in Complex Electromagnetic Environment.” In 2022 IEEE International Conference on Electrical Engineering, Big Data and Algorithms (EEBDA). IEEE. https://doi.org/10.1109/eebda53927.2022.9744753
• Chusilp, Pawat, Weerawut Charubhun, and Otsin Nilubol. 2014a. “Effects of the Cookie Cutter Function Shapes on Monte Carlo Simulations of Weapon Effectiveness.” In the 2014 Seventh IEEE Symposium on Computational Intelligence for Security and Defense Applications (CISDA). IEEE. https://doi.org/10.1109/cisda.2014.7035622
• Cieśliński, Dawid, Adam Okniński, Michał Ranachowski, et al. 2025. “On Development of Green Storable Liquid Rocket Engine with Thrust Variation.” Acta Astronautica 234: 560–74. https://doi.org/10.1016/j.actaastro.2025.05.020
• Citarella, Roberto, Michele Ferraiuolo, Michele Perrella, and Venanzio Giannella. 2022. “Thermostructural Numerical Analysis of the Thrust Chamber of a Liquid Propellant Rocket Engine.” Materials 15 (15): 5427. https://doi.org/10.3390/ma15155427
• Clark, C. R. n.d. “Main Beam Jammer Cancellation and Target Angle Estimation with a Polarization-Agile Monopulse Antenna.” In Proceedings of the IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1989.47623
• Clark, Frank L., and Theodore R. Reel. 1973. “Reference Temperature Method for Predicting Turbulent Compressible Skin-Friction Coefficient.” AIAA Journal 11 (2): 239–40. https://doi.org/10.2514/3.6734
• 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
• Cloutier, J. R., J. H. Evers, and J. J. Feeley. 1988. “An Assessment of Air-to-Air Missile Guidance and Control Technology.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789705
• Cloutier, J. R., J. H. Evers, and J. J. Feeley. 1989. “Assessment of Air-to-Air Missile Guidance and Control Technology.” IEEE Control Systems Magazine 9 (6): 27–34. https://doi.org/10.1109/37.41440
• Coe, J. C. 1948. “Telemetering Guided-Missile Performance.” Proceedings of the IRE 36 (11): 1404–14. https://doi.org/10.1109/jrproc.1948.232300
• Coelho, Fernando Antonio Almeida, and Elder Moreira Hemerly. 2017. “Block Dynamic Surface Control Applied to a Sea-Skimming Missile.” Journal of Guidance, Control, and Dynamics 40 (5): 1286–92. https://doi.org/10.2514/1.g002298
• Cohen, Harry, and William Ferrell. 1969. “Human Operator Decision-Making in Manual Control.” IEEE Transactions on Man Machine Systems 10 (2): 41–47. https://doi.org/10.1109/tmms.1969.299895
• Coles, Donald. 1952. “Direct Measurement of Supersonic Skin Friction.” Journal of the Aeronautical Sciences 19 (10): 717–717. https://doi.org/10.2514/8.2441
• Cong, Wang, and Lu Kunfeng. 2017. “Control Surface Optimization of Hypersonic Vehicle Based on Adaptive Backstepping Method.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027876
• Constancis, Pierre, and Michel Sorine. 1992. “Wideband Control of Gyro/accelerometer Multisensors in a Strapdown Guidance System.” Journal of Guidance, Control, and Dynamics 15 (4): 855–60. https://doi.org/10.2514/3.20917
• 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
• Costello, Richard. 1968. “The Surge Model of the Well-Trained Human Operator in Simple Manual Control.” IEEE Transactions on Man Machine Systems 9 (1): 2–9. https://doi.org/10.1109/tmms.1968.300028
• “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
• 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
• Crocco, L. 1951. “Aspects of Combustion Stability in Liquid Propellant Rocket Motors Part I: Fundamentals. Low Frequency Instability with Monopropellants.” Journal of the American Rocket Society 21 (6): 163–78. https://doi.org/10.2514/8.4393
• Crocco, L. 1952. “Aspects of Combustion Stability in Liquid Propellant Rocket Motors Part II: Low Frequency Instability with Bipropellants. High Frequency Instability.” Journal of the American Rocket Society 22 (1): 7–16. https://doi.org/10.2514/8.4410
• Crocco, Luigi. 1965. “Theoretical Studies on Liquid-Propellant Rocket Instability.” Symposium (International) on Combustion 10 (1): 1101–28. https://doi.org/10.1016/s0082-0784(65)80249-1
• Crocco, Luigi, and Sin-I. Cheng. 1953. “High-Frequency Combustion Instability in Rocket Motor with Concentrated Combustion.” Journal of the American Rocket Society 23 (5): 301–13. https://doi.org/10.2514/8.4623
• Crocco, Luigi, Jerry Grey, and David T. Harrje. 1960. “Theory of Liquid PropelIant Rocket Combustion Instability and Its Experimental Verification.” ARS Journal 30 (2): 159–68. https://doi.org/10.2514/8.5020
• Crocco, Luigi, David T. Harrje, and Frederick H. Reardon. 1962. “Transverse Combustion Instability in Liquid Propellant Rocket Motors.” ARS Journal 32 (3): 366–73. https://doi.org/10.2514/8.6022
• Crossman, Jacob, Robert Marinier, and Edwin B. Olson. 2012. “A Hands-off, Multi-Robot Display for Communicating Situation Awareness to Operators.” In 2012 International Conference on Collaboration Technologies and Systems (CTS). IEEE. https://doi.org/10.1109/cts.2012.6261036
• Cui, Shenghui, Jiaxin Li, Shifeng Zhang, Xibin Bai, and Dongming Sui. 2021. “Overall Parameters Design of Air-Launched Rockets Using Surrogate Based Optimization Method.” Aerospace 9 (1): 15. https://doi.org/10.3390/aerospace9010015
• Cui, Shumei, Shaofei Wang, and Shaopeng Wu. 2013. “Magnetic Field Shielding of Electromagnetic Launch Missile.” In 2013 19th IEEE Pulsed Power Conference (PPC). IEEE. https://doi.org/10.1109/ppc.2013.6627435
• Dae-Seong Jeong, Kwang-Jin Choi, Hyun-Wook Woo, and Jong-Gi Kim. 2007. “Controller Design of Missile Actuator Using DSP.” In 2007 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2007.4406678
• Daeipour, E., and Y. Bar-Shalom. 1994. “An Interacting Multiple Model Approach for Target Tracking with Glint Noise.” In Proceedings of 1994 IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1994.328116
• Dafang, Wu, Su Fei, Liu Chengxiang, et al. 2010. “Experimental Study on Mechanical Behaviors of Al-Alloys under Transient Aerodynamic Heating.” International Journal of Mechanics and Materials in Design 6 (4): 331–40. https://doi.org/10.1007/s10999-010-9140-4
• Dahal, Nimesh, Katsuyoshi Fukiba, Yusuke Ito, Kazuki Mizuta, and Yusuke Maru. 2020. “Classification of Supersonic Flow over a Rigid Parachute Model with Suspension Lines.” Aerospace Science and Technology 105: 105954. https://doi.org/10.1016/j.ast.2020.105954
• Dai, Jinhui, Xiuci Mo, Wenqiang Pu, Junkun Yan, Penghui Wang, and Hongwei Liu. 2021. “Resource Allocation for Multiple Target Tracking in Active and Passive Radar Network.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028566
• Dai, Jinhong, and Junfeng Wang. 2016. “Recognition of Warheads Based on Features of Range Profiles in Ballistic Missile Defense.” In 2016 CIE International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2016.8059177
• 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
• Dalton, J., and S. N. Balakrishnan. 1996. “A Neighboring Optimal Adaptive Critic for Missile Guidance.” Mathematical and Computer Modelling 23 (1–2): 175–88. https://doi.org/10.1016/0895-7177(95)00226-x
• Damini, Anthony, Mike McDonald, and Vince Mantle. 2008. “Image-While-Scan Results from the X-Band Wideband Experimental Airborne Radar.” In 2008 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2008.4721020
• Damonte, J., and D. Stoddard. n.d. “An Analysis of Conical Scan Antennas for Tracking.” In IRE International Convention Record, vol. 4. Institute of Electrical and Electronics Engineers. https://doi.org/10.1109/irecon.1956.1150441
• Daniels, Peter, and Samuel R. Hardy. 1976. “Roll-Rate Stabilization of a Missile Configuration with Wrap-around Fins.” Journal of Spacecraft and Rockets 13 (7): 446–48. https://doi.org/10.2514/3.27918
• Dantas, Joao P. A., Andre N. Costa, Felipe L. L. Medeiros, Diego Geraldo, Marcos R. O. A. Maximo, and Takashi Yoneyama. 2022. “Supervised Machine Learning for Effective Missile Launch Based on beyond Visual Range Air Combat Simulations.” In 2022 Winter Simulation Conference (WSC). IEEE. https://doi.org/10.1109/wsc57314.2022.10015384
• 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
• Das, Arpan, Errol Hale, Michael Candon, and Pier Marzocca. 2026. “Machine-Learning-Based Real-Time Trajectory Prediction of Store Release from Cavity.” Journal of Aircraft: 1–14. https://doi.org/10.2514/1.c038854
• Das, Priya G., and Radhakant Padhi. 2008. “Nonlinear Model Predictive Spread Acceleration Guidance with Impact Angle Constraint for Stationary Targets.” IFAC Proceedings Volumes 41 (2): 13016–21. https://doi.org/10.3182/20080706-5-kr-1001.02201
• Dazer, Martin, Alexander Grundler, Thomas Herzig, Daniel Engert, and Bernd Bertsche. 2021. “Effect of Interval Censoring on the Probability of Test Success in Reliability Demonstration.” In 2021 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams48097.2021.9605747
• De, Sampurna, S. Elayaperumal, and A. A. Bazil Raj. 2020. “Angle Estimation Using Modified Subarray Level Monopulse Ratio Algorithm and S-Curve in Digital Phased Array Radar.” In 2020 Second International Conference on Inventive Research in Computing Applications (ICIRCA). IEEE. https://doi.org/10.1109/icirca48905.2020.9182859
• Dean, Leo E., and Lucian A. Shurley. 1958. “Analysis of Regenerative Cooling in Rocket Thrust Chambers.” Journal of Jet Propulsion 28 (2): 104–10. https://doi.org/10.2514/8.7243
• Dedic, E., D. Henry, M. Lihoreau, and H. Aubert. 2024. “3D Tracking of Small Moving Targets from a Multi-Target Tracking Algorithm Applied to Millimeter-Wave Radar Images.” In 2024 21st European Radar Conference (EuRAD). IEEE. https://doi.org/10.23919/eurad61604.2024.10734870
• Dehghan, Seyed Ali Mohamad, Hamid Reza Koofigar, Hamid Sadeghian, and Mohsen Ekramian. 2021. “Observer-Based Adaptive Force–position Control for Nonlinear Bilateral Teleoperation with Time Delay.” Control Engineering Practice 107: 104679. https://doi.org/10.1016/j.conengprac.2020.104679
• Delano, Richard. 1953. “A Theory of Target Glint or Angular Scintillation in Radar Tracking.” Proceedings of the IRE 41 (12): 1778–84. https://doi.org/10.1109/jrproc.1953.274368
• Delano, R., and Irwin Pfeffer. 1956. “The Effect of AGC on Radar Tracking Noise.” Proceedings of the IRE 44 (6): 801–10. https://doi.org/10.1109/jrproc.1956.274997
• Delplanque, J.-P., and W. A. Sirignano. 1996. “Transcritical Liquid Oxygen Droplet Vaporization: Effect on Rocket Combustion Instability.” Journal of Propulsion and Power 12 (2): 349–57. https://doi.org/10.2514/3.24035
• “Demonstrated Reliability of Plastic-Encapsulated Microcircuits for Missile Applications.” 1996. Microelectronics Reliability 36 (4): 535. https://doi.org/10.1016/0026-2714(96)84383-6
• Denegri, Charles M., James A. Dubben, and Sergey L. Kernazhitskiy. 2013. “Underwing Missile Aerodynamic Effects on Flight-Measured Limit-Cycle Oscillations.” Journal of Aircraft 50 (5): 1637–45. https://doi.org/10.2514/1.c032216
• Deng, Bing, Xian-zhong Liu, and Hong-xing Wang. 2010. “Novel Way of Scalar Miss Distance Measurement.” In 2010 International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2010.499
• DeSpirito, James, Milton E. Vaughn, and W. David Washington. 2003a. “Numerical Investigation of Canard-Controlled Missile with Planar and Grid Fins.” Journal of Spacecraft and Rockets 40 (3): 363–70. https://doi.org/10.2514/2.3971
• 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
• Devan, Viswanath, and Ts Chandar. 2018. “Cascaded LQR Control for Missile Roll Autopilot.” In 2018 International CET Conference on Control, Communication, and Computing (IC4). IEEE. https://doi.org/10.1109/cetic4.2018.8530937
• Devan, Viswanath, and T. S. Chandar. 2019. “Proportional Linear Quadratic Regulator Based Robust Missile Roll Autopilot.” In TENCON 2019 - 2019 IEEE Region 10 Conference (TENCON). IEEE. https://doi.org/10.1109/tencon.2019.8929643
• Devaud, E., and H. Siguerdidjane. 1999. “Two Time-Scale Dynamic Missile Autopilot Based on Quadratic Observer.” In 1999 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.1999.7099415
• Devaud, Emmanuel, and Houria Siguerdidjane. 2002. “A Missile Autopilot Based on Feedback Linearization.” European Journal of Control 8 (6): 553–60. https://doi.org/10.3166/ejc.8.553-560
• 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
• Develet, Jean A. 1961. “Thermal-Noise Errors in Simultaneous-Lobing and Conical-Scan Angle-Tracking Systems.” IRE Transactions on Space Electronics and Telemetry SET-7 (2): 42–51. https://doi.org/10.1109/iret-set.1961.5008758
• Deyun, Zhou, and Zhou Feng. 2008. “Data Fusion Control and Guidance of Surface-to-Air Missile under the Complex Circumstance Based on Neural-Net Technology.” Journal of Systems Engineering and Electronics 19 (5): 996–1002. https://doi.org/10.1016/s1004-4132(08)60187-5
• Dhabale, Ashwin, and Debasish Ghose. 2018. “Curvature Constrained Cubic Spline Impact Angle Guidance for Intercepting Stationary Targets.” IEEE Transactions on Aerospace and Electronic Systems 54 (4): 1750–66. https://doi.org/10.1109/taes.2018.2801396
• Dhananjay, N., and D. Ghose. 2014. “Accurate Time-to-Go Estimation for Proportional Navigation Guidance.” Journal of Guidance, Control, and Dynamics 37 (4): 1378–83. https://doi.org/10.2514/1.g000082
• Dhananjay, N., D. Ghose, and A. Kuduvalli. 2015. “Generation of a Class of Proportional Navigation Guided Interceptor Phantom Tracks.” Journal of Guidance, Control, and Dynamics 38 (11): 2206–15. https://doi.org/10.2514/1.g001180
• Dhananjay, N., Kai-Yew Lum, and Jian-Xin Xu. 2010. “Analysis of Proportional-Navigation Guidance Law with Delayed Line-of-Sight Rate.” In IEEE Icca 2010. IEEE. https://doi.org/10.1109/icca.2010.5524249
• 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
• Dimirovski, G. M., D. D. Mohenski, and S. M. Deskovski. 2003. “A Simulator for Line-of-Sight Missile Control and Guidance Systems: Object-Oriented Design.” In 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652), vol. 6. IEEE. https://doi.org/10.1109/aero.2003.1235207
• Ding, Xiangjun, Jianan Wang, Junhui Liu, and Jiayuan Shan. 2026a. “Approach Angle Constrained and Varying Speed Cooperative Guidance against Maneuvering Targets.” Defence Technology 57: 56–70. https://doi.org/10.1016/j.dt.2025.09.030
• Ding, Wang, and Zhao Yi-Xuan. 2012. “Multi-Subchannel Spread Spectrum for Anti-Jam Communications.” In 2012 International Conference on Industrial Control and Electronics Engineering. IEEE. https://doi.org/10.1109/icicee.2012.50
• Doersam, C. H. 1965. “Space Vehicle Electronics, Principles of Guided Missile Design.” Proceedings of the IEEE 53 (3): 335–335. https://doi.org/10.1109/proc.1965.3739
• Dolgopolov, S., O. Cherniavskyi, and S. Shevchenko. 2025. “Mathematical Modeling of Dynamic Processes in the Branched Reconfigurable Fuel Feed System of a Liquid-Propellant Rocket Engine.” CEAS Space Journal. https://doi.org/10.1007/s12567-025-00691-y
• Doman, David B., and Mark R. Anderson. 2000. “A Fixed-Order Optimal Control Model of Human Operator Response.” Automatica 36 (3): 409–18. https://doi.org/10.1016/s0005-1098(99)00161-2
• Dong, Chen, Tao Chao, Song-yan Wang, Ming Yang, and Xiangyu Sun. 2014. “Impact Angle Constrained Terminal Guidance Based on Dynamic Output Feedback with Guaranteed Convergence Speed.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896719
• Dong, Chunyun, Zhi Guo, and Xiaolong Chen. 2021b. “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, Chunyun, Zexian Huang, Fangfang Wu, Ding Liu, and Xubin Ping. 2023a. “Constrained Reentry Trajectory Design Using Whale Optimization Algorithm for Hypersonic Glide Vehicle.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10239805
• Dong, Xiaofei, and Zhang Ren. 2020. “Impact Angle Constrained Distributed Cooperative Guidance against Maneuvering Targets with Undirected Communication Topologies.” IEEE Access 8: 117867–76. https://doi.org/10.1109/access.2020.3004128
• Dong, Wei, Chunyan Wang, Jianan Wang, Hungsun Son, and Ming Xin. 2022. “Unified Method for Field-of-View-Limited Homing Guidance.” Journal of Guidance, Control, and Dynamics 45 (8): 1415–34. https://doi.org/10.2514/1.g006710
• Dong, Wei, Chunyan Wang, Jianan Wang, and Ming Xin. 2023d. “Varying-Gain Proportional Navigation Guidance for Precise Impact Time Control.” Journal of Guidance, Control, and Dynamics 46 (3): 535–52. https://doi.org/10.2514/1.g007174
• Dong, Xining, Baoshu Xu, Chengshuo Zhang, and Boyu Gao. 2023b. “Research on Terminal Guidance Control of Quadrotor UAV Based on Strapdown Seeker.” In 2023 2nd International Conference on Advanced Sensing, Intelligent Manufacturing (ASIM). IEEE. https://doi.org/10.1109/asim62342.2023.00009
• Dong, Fei, Xiaoyu Zhang, and Panlong Tan. 2024. “Non-Singular Terminal Sliding Mode Cooperative Guidance Law under Impact Angle Constraint.” Journal of the Franklin Institute 361 (14): 107079. https://doi.org/10.1016/j.jfranklin.2024.107079
• Dorrance, William H. 1961. “Dissociation Effects upon Compressible Turbulent Boundary Layer Skin Friction and Heat Transfer.” ARS Journal 31 (1): 61–70. https://doi.org/10.2514/8.5385
• 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
• Dougherty, John J., and Jason L. Speyer. 1997. “Near-Optimal Guidance Law for Ballistic Missile Interception.” Journal of Guidance, Control, and Dynamics 20 (2): 355–61. https://doi.org/10.2514/2.4046
• Dowdle, John, Michael Athans, Sol Gully, and Alan Willsky. 1982. “An Optimal Control and Estimation Algorithm for Missile Endgame Guidance.” In 1982 21st IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1982.268329
• Du, Xiao, and Qunli Xia. 2016. “The Research of Guidance Performance of the Phased Array Seeker with Platform for Air-to-Air Missile.” Optik 127 (22): 10322–34. https://doi.org/10.1016/j.ijleo.2016.08.071
• Du, Xiao, and Qunli Xia. 2017. “Research on Strap-down Seeker Guidance Information for Rolling Interceptor.” Optik 129: 183–99. https://doi.org/10.1016/j.ijleo.2016.10.042
• Duan, Guang-Ren. 2014. “Missile Attitude Control—a Direct Parametric Approach.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6897012
• 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, Dandan, and Chunsheng Liu. 2022. “Event-Based Optimal Guidance Laws Design for Missile-Target Interception Systems Using Fuzzy Dynamic Programming Approach.” ISA Transactions 128: 243–55. https://doi.org/10.1016/j.isatra.2021.10.037
• 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
• Duda, Piotr. 2016. “A Method for Transient Thermal Load Estimation and Its Application to Identification of Aerodynamic Heating on Atmospheric Reentry Capsule.” Aerospace Science and Technology 51: 26–33. https://doi.org/10.1016/j.ast.2016.01.015
• 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
• Dunn, J., D. Howard, and A. King. 1959. “Phenomena of Scintillation Noise in Radar-Tracking Systems.” Proceedings of the IRE 47 (5): 855–63. https://doi.org/10.1109/jrproc.1959.287280
• Durantini, A., A. Farina, A. Fonte, et al. 2017. “Closed Formulas for Evaluating Radar Monopulse Accuracy.” In 2017 18th International Radar Symposium (IRS). IEEE. https://doi.org/10.23919/irs.2017.8008182
• Duvvuru, Ramesh, Arnab Maity, and J. Umakant. 2022. “Three-Dimensional Field of View and Impact Angle Constrained Guidance with Terminal Speed Maximization.” Aerospace Science and Technology 126: 107552. https://doi.org/10.1016/j.ast.2022.107552
• Dwivedi, Prasiddha Nath, Abhijit Bhattacharya, and Radhakant Padhi. 2011. “Suboptimal Midcourse Guidance of Interceptors for High-Speed Targets with Alignment Angle Constraint.” Journal of Guidance, Control, and Dynamics 34 (3): 860–77. https://doi.org/10.2514/1.50821
• Eastman, Donald W. 1993. “Comparison of Missile Flight-Test Drag with Aerodynamic Predictions.” Journal of Spacecraft and Rockets 30 (6): 682–88. https://doi.org/10.2514/3.26373
• Ebrecht, Lars. 2025. “Hierarchical Task Analysis of Current Two Pilot Cockpit Operations towards a Flexible Human-Automation Task Allocation.” In 2025 AIAA DATC/IEEE 44th Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc66011.2025.11257213
• “Effect of Uniformly Distributed Roughness on Turbulent Skin-Friction Drag at Supersonic Speeds.” 1959. Wear 2 (6): 492–93. https://doi.org/10.1016/0043-1648(59)90190-5
• Ehlers, F. Edward. 1961. “On the Lift, Drag, and Moment on a Ring Concentric to a Cylindrical Body in Supersonic Flow.” Journal of the Aerospace Sciences 28 (2): 170–71. https://doi.org/10.2514/8.8908
• 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
• Elias, I., and Robert Gordon. 1952. “Longitudinal Vibrations of Gas at Ambient Pressure in a Rocket Thrust Chamber.” Journal of the American Rocket Society 22 (5): 263–68. https://doi.org/10.2514/8.4489
• Elkind, J. I., and C. D. Forgie. 1959. “Characteristics of the Human Operator in Simple Manual Control Systems.” IRE Transactions on Automatic Control AC-4 (1): 44–55. https://doi.org/10.1109/tac.1959.6429402
• Ellerbrock, Hartwig, and Stefan Ziegenhagen. 2006. “Liquid Rocket Engine Test Facility Engineering Challenges.” Acta Astronautica 59 (12): 1123–34. https://doi.org/10.1016/j.actaastro.2006.04.013
• Elliott, Connor, Vishnu Saj, Hunter Denton, and Moble Benedict. 2025. “Design and Flight Dynamics of a Hand-Launched Foldable Micro Air Vehicle.” Aerospace 12 (9): 754. https://doi.org/10.3390/aerospace12090754
• Ellis, Herbert, Irving Odgers, A. J. Stosick, N. Van de Verg, and Robert S. Wick. 1953. “Experimental Investigation of Combustion Instability in Rocket Motors.” Symposium (International) on Combustion 4 (1): 880–85. https://doi.org/10.1016/s0082-0784(53)80112-8
• Ellis, Stephen R., Mitchelle E. Tyler, Blake Hannaford, Lawrence W. Stark, and Won S. Kim. 1987. “Quantitative Evaluation of Perspective and Stereoscopic Displays in Three-Axis Manual Tracking Tasks.” IEEE Transactions on Systems, Man, and Cybernetics SMC-17. https://ntrs.nasa.gov/citations/19870047305
• Elnan, Odin R. S., and Hsu Lo. 1963. “Interception of High-Speed Target by Beam Rider Missile.” AIAA Journal 1 (7): 1637–39. https://doi.org/10.2514/3.1870
• Eltohamy, Khaled Gamal, and Chen-Yuan Kuo. 2015. “Analysis of Nonlinear Missile Guidance Systems through Linear Adjoint Method.” Smart Science 3 (4): 170–75. https://doi.org/10.1080/23080477.2015.11670488
• 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
• Ennis, M., and S. Chuprun. n.d. “Distributed Anti-Jam Wireless Communications Network.” In MILCOM 97 MILCOM 97 Proceedings, vol. 3. IEEE. https://doi.org/10.1109/milcom.1997.644977
• Erer, Koray S., and Osman Merttopçuoglu. 2012. “Indirect Impact-Angle-Control against Stationary Targets Using Biased Pure Proportional Navigation.” Journal of Guidance, Control, and Dynamics 35 (2): 700–704. https://doi.org/10.2514/1.52105
• Erer, Koray S., Raziye Tekin, and Haichao Hong. 2024. “Computational Impact-Time Guidance with Biased Proportional Navigation.” Journal of Guidance, Control, and Dynamics 47 (6): 1249–55. https://doi.org/10.2514/1.g007910
• 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
• Etzweiler, G. 1969. “Practical Servomechanism Design.” IEEE Transactions on Automatic Control 14 (5): 604–6. https://doi.org/10.1109/tac.1969.1099278
• Evans, E. D. 2000. “Radar Systems and Technologies for Navy Air and Missile Defense.” In Record of the IEEE 2000 International Radar Conference [Cat. No. 00CH37037]. IEEE. https://doi.org/10.1109/radar.2000.851795
• F. William Nesline; Brian H. Wells; Paul Zarchan. 1981. “Combined Optimal/Classical Approach to Robust Missile Autopilot Design.” Journal of Guidance, Control, and Dynamics 4 (3): 316–22. https://doi.org/10.2514/3.56084
• 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
• “The Fallacious Reliability Demonstration Test.” 1980. Microelectronics Reliability 20 (5): 757–58. https://doi.org/10.1016/0026-2714(80)90436-9
• Fan, Jun-fang, Xiao-qian An, Peng Lin, and Si-yu Dong. 2015. “A Modified Biased Pursuit Guidance for Missile with Strapdown Seeker.” In 2015 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2015.7382798
• 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, Tsai-Hung, and Chia-Chen Chang. 2009. “A Bayesian Zero-Failure Reliability Demonstration Test of High Quality Electro-Explosive Devices.” Quality and Reliability Engineering International 25 (8): 913–20. https://doi.org/10.1002/qre.1009
• Fan, Junfang, Denghui Dou, and Yi Ji. 2023. “Impact-Angle Constraint Guidance and Control Strategies Based on Deep Reinforcement Learning.” Aerospace 10 (11): 954. https://doi.org/10.3390/aerospace10110954
• Fan, Jianhui, Jiaao Hao, Chih-Yung Wen, and Xiaopeng Xue. 2022. “Numerical Investigation of Supersonic Flow over a Parachute-like Configuration Including Turbulent Flow Effects.” Aerospace Science and Technology 121: 107330. https://doi.org/10.1016/j.ast.2022.107330
• 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, Jun-fang, Peng Lin, Ying Chen, and Si-yu Dong. 2014. “A PN/SMC Hybrid Guidance Law for Missile with Narrow Field-of-View Strapdown Seeker.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896715
• Fan, Yu, Fang Lu, Wuxuan Zhu, Guangzhou Bai, and Liang Yan. 2017a. “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, Xinyue, Haonan Jiang, Yuanli Cai, Junshuai Luo, Hong Shen, and Yifan Deng. 2024. “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, Bingyi, and Siliang Wu. 2006. “Angle-Parameterizations Range-Only Target Tracking for Scalar Miss Distance Measurement System.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.344520
• Fang, Bingyi, Siliang Wu, and Guohua Wei. 2006. “Vector Miss Distance Measurement Based on Range-Only Target Tracking.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343456
• Fang, Ke, Qingzhen Zhang, Yingxin Wang, Kun Ni, and Chengyang Zhou. 2018. “Track Fusion and Anti-Jamming Algorithm Based on Multi-Missile Detection Information.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018966
• Farina, A., G. Gabatel, and R. Sanzullo. 2000. “Estimation of Target Direction by Pseudo-Monopulse Algorithm.” Signal Processing 80 (2): 295–310. https://doi.org/10.1016/s0165-1684(99)00129-2
• Farlik, Jan. 2015. “Simulation of Surface-to-Air Missile Units: Cluster Design.” In International Conference on Military Technologies (ICMT) 2015. IEEE. https://doi.org/10.1109/miltechs.2015.7153687
• 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
• 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
• Farvin, M. A., and John Peddieson. 1988. “Mathematical Modeling of Liquid-Rocket Combustion Instability.” Mathematical and Computer Modelling 11: 570–74. https://doi.org/10.1016/0895-7177(88)90557-2
• 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, Yanqi. 2022. “Switched Control of Hypersonic Vehicle Based on Threshold Event-Triggered Mechanism.” In 2022 34th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc55256.2022.10033500
• Feng, Dan, Mingshan Hou, and Wencong Wang. 2022. “Fixed-Time Integrated Guidance and Control with Impact Angle Constraint.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9901553
• Feng, Lei, Wang Lu, Fenglin Wang, Fan Zhang, and Qiangui Sun. 2023. “Optimal Penetration Guidance Law for High-Speed Vehicles against an Interceptor with Modified Proportional Navigation Guidance.” Symmetry 15 (7): 1337. https://doi.org/10.3390/sym15071337
• 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, Zhigang, and Qi Wang. 2007. “Research on Health Evaluation System of Liquid-Propellant Rocket Engine Ground-Testing Bed Based on Fuzzy Theory.” Acta Astronautica 61 (10): 840–53. https://doi.org/10.1016/j.actaastro.2007.01.071
• Feng, Dingwei, Siliang Wu, and Guohua Wei. 2012. “Multi-Targets Miss Distance Measurement Using Sequential Range-Doppler Image.” In 2012 IEEE 11th International Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2012.6491938
• 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
• Feng Tyan. 2013. “Adaptive PPN Guidance Law with Impact Angle Constraint.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6579807
• Feng Tyan and Jeng Fu Shen. 2006. “A Simple Adaptive GIPN Missile Guidance Law.” In 2006 American Control Conference. IEEE. https://doi.org/10.1109/acc.2006.1655379
• Feng Xiaobin, Huang Peikang, and Fan Zhengfang. 2001. “Analysis Spectral-Power-Density of Glint of Radar-Extended Target.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984909
• Fernández, Arturo J. 2011. “Optimal Reliability Demonstration Test Plans for $k$-out-of-$n$ Systems of Gamma Distributed Components.” IEEE Transactions on Reliability 60 (4): 833–44. https://doi.org/10.1109/tr.2011.2161701
• Ferraiuolo, Michele, Venanzio Giannella, Enrico Armentani, and Roberto Citarella. 2023. “Numerical Investigation on the Service Life of a Liquid Rocket Engine Thrust Chamber.” Metals 13 (3): 470. https://doi.org/10.3390/met13030470
• Ferraiuolo, Michele, Michele Perrella, Venanzio Giannella, and Roberto Citarella. 2022. “Thermal–Mechanical FEM Analyses of a Liquid Rocket Engines Thrust Chamber.” Applied Sciences 12 (7): 3443. https://doi.org/10.3390/app12073443
• Ferraiuolo, Michele, Vincenzo Russo, and Kambiz Vafai. 2016. “A Comparative Study of Refined and Simplified Thermo-Viscoplastic Modeling of a Thrust Chamber with Regenerative Cooling.” International Communications in Heat and Mass Transfer 78: 155–62. https://doi.org/10.1016/j.icheatmasstransfer.2016.09.003
• 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
• “Fiber Optic Link Tested for Missile Guidance.” 1981. Information Display 1981 (5): 18–18. https://doi.org/10.1002/j.2637-496x.1981.tb01863.x
• 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
• Filimonov, V. I. 1968. “Investigation of Instability of Combustion in Liquid-Propellant Rocket Motors.” Soviet Applied Mechanics 4 (9): 80–81. https://doi.org/10.1007/bf00895855
• Fine, T., R. Nock, and R. Sansom. 1966. “A Statistical Technique for the Design of Missile Flight Test Programs to Measure Accuracy Information.” Journal of Spacecraft and Rockets 3 (5): 645–50. https://doi.org/10.2514/3.28508
• Fiore, Matteo, Marco Fabiani, and Francesco Nasuti. 2026. “Two-Phase Heat Transfer in Deep Throttling of Liquid Rocket Engines.” Acta Astronautica 247: 50–66. https://doi.org/10.1016/j.actaastro.2026.04.060
• Fiorentini, Lisa, Andrea Serrani, Michael A. Bolender, and David B. Doman. 2009. “Nonlinear Control of Non-Minimum Phase Hypersonic Vehicle Models.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160211
• Fitzgerald, Robert J. 1990. “Reduction of Missile Navigation Errors by Roll Programming.” Journal of Guidance, Control, and Dynamics 13 (4): 755–58. https://doi.org/10.2514/3.25397
• Flora, Thomas J., Mark F. Reeder, Andrew Lofthouse, and Neal Kraft. 2014. “Dynamic Store Release of Ice Models from a Cavity into Mach 2.9 Flow.” Journal of Aircraft 51 (6): 1927–41. https://doi.org/10.2514/1.c032459
• Florencio, Heitor, Adrião Dória Neto, and Daniel Martins. 2020. “ISA 100.11a Networked Control System Based on Link Stability.” Sensors 20 (18): 5417. https://doi.org/10.3390/s20185417
• Fonod, Robert, and Tal Shima. 2016. “Multiple Model Adaptive Evasion against a Homing Missile.” Journal of Guidance, Control, and Dynamics 39 (7): 1578–92. https://doi.org/10.2514/1.g000404
• Fontana, Simone, and Federica Di Lauro. 2022. “An Overview of Sensors for Long Range Missile Defense.” Sensors 22 (24): 9871. https://doi.org/10.3390/s22249871
• Forouhar, Moein, Hamid Sadeghian, Daniel Perez Suay, Abdeldjallil Naceri, and Sami Haddadin. 2024. “A Tactile Lightweight Exoskeleton for Teleoperation: Design and Control Performance.” In 2024 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros58592.2024.10802732
• Fossier, Mike W. 1984. “The Development of Radar Homing Missiles.” Journal of Guidance, Control, and Dynamics 7 (6): 641–51. https://doi.org/10.2514/3.19908
• Fowdur, Jaya Shradha, Feyza Eksen, Lucas Paes Moreira, and Paweł Banyś. 2025. “Unsupervised Adaptive Background Subtraction in Distributed Radar Target Tracking Systems.” In 2025 IEEE Radar Conference (RadarConf25). IEEE. https://doi.org/10.1109/radarconf2559087.2025.11205131
• 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
• Franc, Marko, and Ales Hace. 2012. “FPGA Implementation of the Bilateral Control Algorithm for a High Performance Haptic Teleoperation.” In 2012 12th IEEE International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2012.6197093
• Franzini, Giovanni, Luca Tardioli, Lorenzo Pollini, and Mario Innocenti. 2018. “Visibility Augmented Proportional Navigation Guidance.” Journal of Guidance, Control, and Dynamics 41 (4): 987–95. https://doi.org/10.2514/1.g002897
• Frazer, G. J., and C. G. Williams. 2019. “Decametric Radar for Missile Defence.” In 2019 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2019.8835810
• 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, J. A. 2005. “Applied Computational Fluid Dynamics in Support of Aircraft/Store Compatibility and Weapons Integration: 2005 Edition.” In 2005 Users Group Conference (DOD-UGC’05). IEEE. https://doi.org/10.1109/dodugc.2005.12
• Freeman, J. A., and B. A. Jolly. 2004. “Applied Computational Fluid Dynamics in Support of Aircraft/store Compatibility and Weapons Integration: 2004 Edition.” In 2004 Users Group Conference (DOD_UGC’04). IEEE. https://doi.org/10.1109/dod_ugc.2004.5
• French, Kenneth E. 1967. “Comment on ‘a Method for Calculating Parachute Opening Forces for General Deployment Conditions’.” Journal of Spacecraft and Rockets 4 (10): 1407–8. https://doi.org/10.2514/3.59571
• French, Kenneth E. 1980. “Effects of Line Ties on Parachute Deployment.” Journal of Spacecraft and Rockets 17 (3): 260–62. https://doi.org/10.2514/3.57735
• Friedrich, Max, and Mark Vollrath. 2021. “Human–Machine Interface Design for Monitoring Safety Risks Associated with Operating Small Unmanned Aircraft Systems in Urban Areas.” Aerospace 8 (3): 71. https://doi.org/10.3390/aerospace8030071
• Fu, Maozhong, Chunxian Gao, Yuhan Li, Zhenmiao Deng, and Daqing Chen. 2021. “Monopulse-Radar Angle Estimation of Multiple Targets Using Multiple Observations.” IEEE Transactions on Aerospace and Electronic Systems 57 (2): 968–83. https://doi.org/10.1109/taes.2020.3035434
• Fujii, Keisuke, and Yasutoshi Inoue. 1998a. “Aerodynamic Heating Measurement on Afterbody of Hypersonic Flight Experiment.” Journal of Spacecraft and Rockets 35 (6): 736–41. https://doi.org/10.2514/2.3409
• Fukushima, Hirofumi, Ryuhei Takahashi, and Nobuhiro Suzuki. 2017. “Minimum Constrained Adaptive Monopulse Estimation in Radio Interference.” In 2017 Sensor Signal Processing for Defence Conference (SSPD). IEEE. https://doi.org/10.1109/sspd.2017.8233243
• Fuld, Robert B. 2000. “The Fiction of Function Allocation, Revisited.” International Journal of Human-Computer Studies 52 (2): 217–33. https://doi.org/10.1006/ijhc.1999.0286
• Gade, Murali Mohan, and K. K. Mangrulkar. 2018. “Modeling and PWM Control of Electro-Pneumatic Actuator for Missile Applications.” IFAC-PapersOnLine 51 (1): 237–42. https://doi.org/10.1016/j.ifacol.2018.05.057
• Gallo, Giuseppe, Hiroki Kojima, Landon Kamps, and Harunori Nagata. 2024b. “Experimental Investigation of Regenerative Cooling Performance in Hybrid Rocket Engines.” Thermal Science and Engineering Progress 49: 102481. https://doi.org/10.1016/j.tsep.2024.102481
• Gallo, Giuseppe, Yuta Miyahara, Landon Kamps, and Harunori Nagata. 2024c. “Regenerative Cooling in Hybrid Rocket Engines Based on Self-Pressurized Liquid Nitrous Oxide.” Applied Thermal Engineering 254: 123928. https://doi.org/10.1016/j.applthermaleng.2024.123928
• Galy, Jerome, Eric Chaumette, and Pascal Larzabal. 2010. “Joint Detection Estimation Problem of Monopulse Angle Measurement.” IEEE Transactions on Aerospace and Electronic Systems 46 (1): 397–413. https://doi.org/10.1109/taes.2010.5417170
• Gao, Jiwei, and Yuan-Li Cai. 2017. “Three-Dimensional Impact Angle Constrained Guidance Laws with Fixed-Time Convergence.” Asian Journal of Control 19 (6): 2240–54. https://doi.org/10.1002/asjc.1571
• Gao, Mengya, Wanchun Chen, and Wenbin Yu. 2020. “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, Yuan, Liang-xian Gu, and Lei Pan. 2008. “Application of Variable Structure Control in Missile Electromechanical Actuator System.” In 2008 International Conference on Intelligent Computation Technology and Automation (ICICTA). IEEE. https://doi.org/10.1109/icicta.2008.151
• Gao, Qunchang, Tianyu Jin, and Shaoming He. 2026a. “Analytical Optimal Line-of-Sight Guidance for Aircraft Defense.” Journal of Guidance, Control, and Dynamics 49 (8): 2409–19. https://doi.org/10.2514/1.g009805
• Gao, Yuxin, Chunsheng Liu, Sen Jiang, and Shaojie Zhang. 2021. “Zero-Sum Differential Games-Based Fast Adaptive Robust Optimal Sliding Mode Control Design for Uncertain Missile Autopilot with Constrained Input.” International Journal of Control 95 (7): 1789–1801. https://doi.org/10.1080/00207179.2021.1872802
• Gao, Han, Yinde Liu, Yangshuo Liu, and Chen Yang. 2026b. “Resilient Prescribed Performance Control for Hypersonic Morphing Flight Vehicle with Measurement Uncertainty.” Journal of Guidance, Control, and Dynamics: 1–13. https://doi.org/10.2514/1.g009823
• Gao, Chang, Hongwei Liu, Shenghua Zhou, et al. 2018. “Maneuvering Target Tracking with Recurrent Neural Networks for Radar Application.” In 2018 International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2018.8557284
• 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, Yunwan, Ke Xu, Jinyu Fu, Liang Chen, Huajie Zhu, and Xuehai Chen. 2024. “Fixed-Time Guidance Law for Multiple Missiles with Impact Angle Constraint against Maneuvering Target.” In 2024 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac63892.2024.10864947
• Gao Sun, Mingchao Zhu, Shengli Yin, and Hongguang Jia. 2011. “Optical Axis Stabilization of Semi-Strapdown Seeker Based on Disturbance Observer.” In 2011 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2011.5949054
• Garcia, Eloy, David W. Casbeer, and Meir Pachter. 2015b. “Cooperative Strategies for Optimal Aircraft Defense from an Attacking Missile.” Journal of Guidance, Control, and Dynamics 38 (8): 1510–20. https://doi.org/10.2514/1.g001083
• Garcia, Eloy, David W. Casbeer, Khanh Pham, and Meir Pachter. 2014. “Cooperative Aircraft Defense from an Attacking Missile.” In 53rd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2014.7039839
• Ge, Xianliang, Hanlin Xu, Ke Zhang, Hao Ni, Jie Xu, and Xiaolei Song. 2026. “Effects of Human–Automation Authority Allocation on Multitasking Performance under Workload Conditions.” International Journal of Human–Computer Interaction: 1–20. https://doi.org/10.1080/10447318.2026.2647133
• Ge Ming, Han Xuefeng, and Jia Hongguang. 2011. “The Parameter Optimization of Missile Actuator Based on Spatial RSSR Linkage Mechanism.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5777570
• Geer, James. 1980. “Electromagnetic Scattering by a Slender Body of Revolution: Axially Incident Plane Wave.” SIAM Journal on Applied Mathematics 38 (1): 93–102. https://doi.org/10.1137/0138007
• Genot, Aurelien. 2021. “Aluminum Combustion Instabilities: Dimensionless Numbers Controlling the Instability in Solid Rocket Motors.” Combustion and Flame 232: 111563. https://doi.org/10.1016/j.combustflame.2021.111563
• 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
• Ghose, Debasish. 1994. “Capture Region for True Proportional Navigation Guidance with Nonzero Miss-Distance.” Journal of Guidance, Control, and Dynamics 17 (3): 627–28. https://doi.org/10.2514/3.21245
• Ghosh, Subir. 1991. “A New Monopulse Feed System for Increased Tracking Accuracy of Radars.” In 1991 21st European Microwave Conference. IEEE. https://doi.org/10.1109/euma.1991.336496
• Ghosh, Satadal, Debasish Ghose, and Soumyendu Raha. 2013. “Capturability of Augmented Proportional Navigation (APN) Guidance with Nonlinear Engagement Dynamics.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6579805
• Ghosh, Satadal, Debasish Ghose, and Soumyendu Raha. 2014. “Capturability of Augmented Pure Proportional Navigation Guidance against Time-Varying Target Maneuvers.” Journal of Guidance, Control, and Dynamics 37 (5): 1446–61. https://doi.org/10.2514/1.g000561
• Ghosh, Satadal, Debasish Ghose, and Soumyendu Raha. 2016a. “Composite Guidance for Impact Angle Control against Higher Speed Targets.” Journal of Guidance, Control, and Dynamics 39 (1): 98–117. https://doi.org/10.2514/1.g001232
• Ghosh, Satadal, Debasish Ghose, and Soumyendu Raha. 2016b. “Unified Time-to-Go Algorithms for Proportional Navigation Class of Guidance.” Journal of Guidance, Control, and Dynamics 39 (6): 1188–1205. https://doi.org/10.2514/1.g001472
• Gibbons, I. F., and J. J. Botha. 2015. “Tactical Radar Missile Challenges.” In 2015 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radarconf.2015.7411852
• Gieseking, D. 1963. “An Optimum Bistable Controller for Increased Missile Autopilot Performance.” IEEE Transactions on Automatic Control 8 (4): 306–11. https://doi.org/10.1109/tac.1963.1105588
• 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
• Gilbert, William H., and Ching-Fang Lin. 1984. “New Missile Guidance and Control Technology Panel Discussion.” In 1984 American Control Conference. IEEE. https://doi.org/10.23919/acc.1984.4788475
• Girard, Donald D. 1986. “Nonlinear Flutter Analysis of a Missile Fin/Actuator.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4789104
• Giuli, D., and R. Tiberio. 1975. “A Modified Monopulse Technique for Radar Tracking with Low-Angle Multipath.” IEEE Transactions on Aerospace and Electronic Systems AES-11 (5): 741–48. https://doi.org/10.1109/taes.1975.307983
• 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
• Glass, John D., and W. D. Blair. 2015. “Monopulse DOA Estimation Using Adjacent Matched Filter Samples.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119218
• Goddard, Frank E. 1959. “Effect of Uniformly Distributed Roughness on Trubulent Skin-Friction Drag at Supersonic Speeds.” Journal of the Aerospace Sciences 26 (1): 1–15. https://doi.org/10.2514/8.7911
• Godrich, Hana, Vlad M. Chiriac, Alexander M. Haimovich, and Rick S. Blum. 2010. “Target Tracking in MIMO Radar Systems: Techniques and Performance Analysis.” In 2010 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2010.5494453
• Gogineni, Sandeep, and Arye Nehorai. 2010. “Target Tracking Using Monopulse MIMO Radar with Distributed Antennas.” In 2010 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2010.5494628
• Gökdemir, Burak, Yaser Dalveren, Ali Kara, and Mohammad Derawi. 2026. “Velocity and Angle Tracking of Fast Targets Using a Bandwidth-Coded Hybrid Chirp FMCW Radar.” Sensors 26 (6): 1751. https://doi.org/10.3390/s26061751
• Goldan, Orly, and Shaul Gutman. 2012. “Adjoint Stability and Miss Distance in Proportional Navigation.” Journal of Guidance, Control, and Dynamics 35 (4): 1089–93. https://doi.org/10.2514/1.56143
• Goldberg, Louis M. 1967b. “Application of Parameter Management to Roll Rate Control in the Ballistic Missile Target System.” Journal of Spacecraft and Rockets 4 (9): 1243–47. https://doi.org/10.2514/3.29059
• Golliday, C. 1985. “Data Link Communications in Tactical Air Command and Control Systems.” IEEE Journal on Selected Areas in Communications 3 (5): 779–91. https://doi.org/10.1109/jsac.1985.1146251
• Gong, Xiaopeng, Wanchun Chen, Zhongyuan Chen, and Wenjie Yuan. 2024. “Closed-Form Solutions of Miss Distance for Higher-Order Guidance System.” IEEE Transactions on Aerospace and Electronic Systems 60 (2): 2331–49. https://doi.org/10.1109/taes.2024.3353717
• Gongjian Zhou, Taifan Quan, and T. Kirubarajan. 2012. “Pseudo States Estimation for Maneuvering Target Tracking in Doppler Radar Systems.” In 2012 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2012.6212235
• Goodarzi, Mahdi, Mohammad Ali Sebt, and Hossein Darvishi. 2020. “Target and Image Elevation Angles Separation Algorithm for Low-Angle Tracking with Monopulse Antenna.” In 2020 28th Iranian Conference on Electrical Engineering (ICEE). IEEE. https://doi.org/10.1109/icee50131.2020.9261076
• Goodman, J. W. 1965. “Some Effects of Target-Induced Scintillation on Optical Radar Performance.” Proceedings of the IEEE 53 (11): 1688–1700. https://doi.org/10.1109/proc.1965.4341
• Goossens, A. A. H. E. n.d. “Development and Evaluation of Level 3 Situation Awareness Support Functions for a UAV Operator Station.” In The 23rd Digital Avionics Systems Conference (IEEE Cat. No.04CH37576). IEEE. https://doi.org/10.1109/dasc.2004.1390839
• Gopalan, Akhil, Ashwini Ratnoo, and Debasish Ghose. 2017. “Generalized Time-Optimal Impact-Angle-Constrained Interception of Moving Targets.” Journal of Guidance, Control, and Dynamics 40 (8): 2115–20. https://doi.org/10.2514/1.g002384
• 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, Robert. 1950. “Heat-Transfer Problems in Liquid-Propellant Rocket Motors.” Journal of the American Rocket Society 00 (81): 65–78. https://doi.org/10.2514/8.4316
• Gosselin, J. n.d. “Simple Chip Combining Metric Improvements for Anti-Jam Applications.” In MILCOM 92 Conference Record. IEEE. https://doi.org/10.1109/milcom.1992.244008
• 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
• Gotsulenko, V. V. 2008. “Distinctive Features of the Intrachamber Instability of Combustion in Liquid-Propellant Rocket Engines.” Journal of Engineering Physics and Thermophysics 81 (5): 935–40. https://doi.org/10.1007/s10891-009-0121-0
• Gözükara, Arif Cem, and Uygar Ateş Ceylan. 2024. “Numerical Method for Predicting Transient Aerodynamic Heating in Hemispherical Domes.” Computation 12 (8): 162. https://doi.org/10.3390/computation12080162
• Graham, Ernest W. 1950. “The Pressure on a Slender Body of Nonuniform Cross-Sectional Shape in Axial Supersonic Flow.” Journal of the Aeronautical Sciences 17 (3): 173–75. https://doi.org/10.2514/8.1562
• 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
• Greatrix, David R. 2011. “Scale Effects on Solid Rocket Combustion Instability Behaviour.” Energies 4 (1): 90–107. https://doi.org/10.3390/en4010090
• 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
• Griesser, T., and C. Balanis. 1987. “Oceanic Low-Angle Monopulse Radar Tracking Errors.” IEEE Journal of Oceanic Engineering 12 (1): 289–95. https://doi.org/10.1109/joe.1987.1145238
• Grindley, Ben, Tom Cherrett, James Scanlan, and Katherine L. Plant. 2026. “Exploring the Relationship between Operator Experience, Propensity to Trust Automation and Perceived System Trustworthiness of Uncrewed Air Vehicles.” Ergonomics: 1–12. https://doi.org/10.1080/00140139.2026.2625177
• Grinfeld, Natan, and Joseph Z. Ben-Asher. 2015. “Minimal-Jerk Missile Guidance Law.” Journal of Guidance, Control, and Dynamics 38 (8): 1520–25. https://doi.org/10.2514/1.g001088
• Gross, Harry N., Phillip R. Chandler, and Robert A. Eslinger. 1986. “Renewed Interest in Hinge Moment Models for Failure Detection and Isolation.” In 1986 American Control Conference. IEEE. https://doi.org/10.23919/acc.1986.4789163
• Grote, Gudela, Cornelia Ryser, Toni WĀLer, Anna Windischer, and Steffen Weik. 2000. “KOMPASS: A Method for Complementary Function Allocation in Automated Work Systems.” International Journal of Human-Computer Studies 52 (2): 267–87. https://doi.org/10.1006/ijhc.1999.0289
• Grundler, Alexander, and Martin Dazer. 2024. “Reliability Demonstration Test Planning for Systems Using Prior Knowledge.” IEEE Access 12: 3339–55. https://doi.org/10.1109/access.2023.3347035
• Gruner, Patrik, Tobias Chaloun, and Christian Waldschmidt. 2017. “Enhanced Angle Estimation Accuracy of Ultra Compact Radars Inspired by a Biomimetic Approach.” In 2017 IEEE MTT-S International Microwave Symposium (IMS). IEEE. https://doi.org/10.1109/mwsym.2017.8058886
• Gruner, Patrik, Tobias Chaloun, and Christian Waldschmidt. 2019. “Enhancing Angle Estimation Accuracy of Ultra Compact Two-Channel Radar MMICs at 160 GHz Using a Biomimetic Antenna Array.” In 2019 IEEE MTT-S International Microwave Symposium (IMS). IEEE. https://doi.org/10.1109/mwsym.2019.8701007
• Gruntman, Mike. 2019. “From Tyuratam Missile Range to Baikonur Cosmodrome.” Acta Astronautica 155: 350–66. https://doi.org/10.1016/j.actaastro.2018.12.021
• Gu, Haoyu, Baolin Zhao, Hao Zhou, Xianxue Liu, and Wei Su. 2019. “MEMS Gyroscope Bias Drift Self-Calibration Based on Noise-Suppressed Mode Reversal.” Micromachines 10 (12): 823. https://doi.org/10.3390/mi10120823
• Guan, Xiaohui. 2014b. “Supersonic Wing–Body Two-Level Wave Drag Optimization Using Extended Far-Field Composite-Element Methodology.” AIAA Journal 52 (5): 981–90. https://doi.org/10.2514/1.j052305
• Guelman, Mauricio, Klaus Schilling, and Danna Linn Barnett. 2012. “Formation Flight Line of Sight Guidance.” Acta Astronautica 71: 163–69. https://doi.org/10.1016/j.actaastro.2011.08.004
• Guesalaga, Andrés R. 1988. “A Digital Method of Demodulation and Filtering for Angular Errors in Conical Scan Tracking Radars.” Microprocessing and Microprogramming 23 (1–5): 327–31. https://doi.org/10.1016/0165-6074(88)90376-6
• Guesalaga, A., and S. Tepper. 2000. “Synthesis of Automatic Gain Controllers for Conical Scan Tracking Radar.” IEEE Transactions on Aerospace and Electronic Systems 36 (1): 302–9. https://doi.org/10.1109/7.826334
• Guest, I. W. 1991. “Algorithm to Reduce Glint Induced Radar Tracking Errors on a Highly Dynamic Target.” In COMSIG 1991 Proceedings: South African Symposium on Communications and Signal Processing. IEEE. https://doi.org/10.1109/comsig.1991.278218
• Guilin Li and Haibo Ji. 2014. “A Finite Time Convergent Guidance Law with Terminal Angle Constraint Considering Missile Autopilot.” In Proceeding of the 11th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2014.7053376
• Gulliver, T. A., and E. B. Felstead. n.d. “Anti-Jam by Fast FH NCFSK-Myths and Realities.” In Proceedings of MILCOM ‘93 - IEEE Military Communications Conference, vol. 1. IEEE. https://doi.org/10.1109/milcom.1993.408523
• Guo, Changrong, Jiebo Chen, Keyan Guo, Wenjie Zhang, Zhiming Zhou, and Zhen Liu. 2025a. “Design of Impact Angle Constrained Guidance Law Based on Deep Reinforcement Learning.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487415
• Guo, Yanning, Matt Hawkins, and Bong Wie. 2013. “Applications of Generalized Zero-Effort-Miss/Zero-Effort-Velocity Feedback Guidance Algorithm.” Journal of Guidance, Control, and Dynamics 36 (3): 810–20. https://doi.org/10.2514/1.58099
• Guo, Dong, Peng Jiang, Zixuan Liang, and Zhang Ren. 2018c. “Three-Dimensional Guidance Method for Air to Ground Missile with Impact Time Constraint.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8484215
• Guo, Huairui, Tongdan Jin, and Adamantios Mettas. 2011. “Designing Reliability Demonstration Tests for One-Shot Systems under Zero Component Failures.” IEEE Transactions on Reliability 60 (1): 286–94. https://doi.org/10.1109/tr.2010.2085552
• Guo, Yuheng, Xiang Li, Houjun Zhang, Ming Cai, and Feng He. 2020. “Data-Driven Method for Impact Time Control Based on Proportional Navigation Guidance.” Journal of Guidance, Control, and Dynamics 43 (5): 955–66. https://doi.org/10.2514/1.g004669
• Guo, Jing, Chao Liu, and Philippe Poignet. 2015. “Stable and Enhanced Position-Force Tracking for Bilateral Teleoperation with Time Delay.” In 2015 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2015.7330829
• Guo, Kun-Yi, Quan-You Qu, Ai-Xi Feng, and Xin-Qing Sheng. 2016. “Miss Distance Estimation Based on Scattering Center Model Using Time-Frequency Analysis.” IEEE Antennas and Wireless Propagation Letters 15: 1012–15. https://doi.org/10.1109/lawp.2015.2490088
• Guo, Kangkang, Yongjie Ren, Peng Chen, Wei Lin, Yiheng Tong, and Wansheng Nie. 2021a. “Analysis of Spontaneous Longitudinal Combustion Instability in an O2/CH4 Single-Injector Rocket Combustor.” Aerospace Science and Technology 119: 107209. https://doi.org/10.1016/j.ast.2021.107209
• 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, Kun-Yi, Guang-Liang Xiao, Yun Zhai, and Xin-Qing Sheng. 2018a. “Angular Glint Error Simulation Using Attributed Scattering Center Models.” IEEE Access 6: 35194–35205. https://doi.org/10.1109/access.2018.2846538
• Guo, Kangkang, Boqi Xu, Yongjie Ren, Yiheng Tong, and Wansheng Nie. 2022. “Analysis of Tangential Combustion Instability Modes in a LOX/Kerosene Liquid Rocket Engine Based on OpenFOAM.” Frontiers in Energy Research 9: 810439. https://doi.org/10.3389/fenrg.2021.810439
• Guo, Yuyan, Chenguang Yang, and Bin Xu. 2023. “Overload Tracking Control for Hypersonic Flight Vehicle with Coupling Coordination.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10240784
• Guo Ying and Wang Bu-hong. 2005. “Effective Array Calibration Criterions for Radar Low-Angle Tracking.” In 2005 IEEE Antennas and Propagation Society International Symposium, vol. 2B. IEEE. https://doi.org/10.1109/aps.2005.1552043
• Guo-Jiang Zhang, Yu Yao, and Ke-Mao Ma. 2005. “Line of Sight Rate Estimation of Strapdown Imaging Guidance System Based on Unscented Kalman Filter.” In 2005 International Conference on Machine Learning and Cybernetics. IEEE. https://doi.org/10.1109/icmlc.2005.1527195
• Guodong, Zhang, and Li Chonglun. 2013. “An UKF Target Tracking Method with Effective Suppression of Angular Glint.” In 2013 10th IEEE International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2013.6565106
• Guohua Wei, Siliang Wu, and Erke Mao. 2004. “Estimation of Vector Miss Distance Based on Source Localization.” In Proceedings of the 2004 IEEE Radar Conference (IEEE Cat. No.04CH37509). IEEE. https://doi.org/10.1109/nrc.2004.1316497
• Guoying Chen, Peikang Huang, and Hongcheng Yin. 1996. “A Statistical Model of Radar Target Glint Based on Discrete Differenced Gaussian Noise.” In IEEE Antennas and Propagation Society International Symposium. 1996 Digest, vol. 2. IEEE. https://doi.org/10.1109/aps.1996.549863
• Gupta, Anshu, and Thomas Fickenscher. 2013. “Evaluative Comparison of Clutter Canceller Beamformer and Amplitude Comparison Monopulse Estimation Scheme in HF SWR.” In 2013 Asia-Pacific Microwave Conference Proceedings (APMC). IEEE. https://doi.org/10.1109/apmc.2013.6694868
• Gur, I., J. Shinar, and J. Rom. 1979. “Prediction of Roll Controllability of Slender Cruciform Canard ConfigurationsI. Gur, J. Shinar, and J. Rom.” Journal of Spacecraft and Rockets 16 (4): 238–44. https://doi.org/10.2514/3.57650
• Gurav, Bhimashankar, John Economou, Alistair Saddington, and Kevin Knowles. 2017. “Multi-Mode Electric Actuator Dynamic Modelling for Missile Fin Control.” Aerospace 4 (2): 30. https://doi.org/10.3390/aerospace4020030
• Gurfil, P. 2001a. “Robust Zero Miss Distance Guidance for Missiles with Parametric Uncertainties.” In Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148). IEEE. https://doi.org/10.1109/acc.2001.946148
• Gurfil, Pini. 2001b. “Synthesis of Zero Miss Distance Missile Guidance via Solution of an Optimal Tuning Problem.” Control Engineering Practice 9 (10): 1117–30. https://doi.org/10.1016/s0967-0661(01)00057-0
• Gurfil, Pini. 2003. “Zero-Miss-Distance Guidance Law Based on Line-of-Sight Rate Measurement Only.” Control Engineering Practice 11 (7): 819–32. https://doi.org/10.1016/s0967-0661(02)00208-3
• Gurfil, Pini, Mario Jodorkovsky, and Moshe Guelman. 1998. “Finite Time Stability Approach to Proportional Navigation Systems Analysis.” Journal of Guidance, Control, and Dynamics 21 (6): 853–61. https://doi.org/10.2514/2.4348
• Gurfil, Pini, Mario Jodorkovsky, and Moshe Guelman. 2001. “Neoclassical Guidance for Homing Missiles.” Journal of Guidance, Control, and Dynamics 24 (3): 452–59. https://doi.org/10.2514/2.4765
• Guruswamy, Guru P. 2025. “A Body-Fitted Structured Grid Approach to Simulate Breathing Mode Oscillations during Parachute Deployment.” Aerospace Science and Technology 156: 109747. https://doi.org/10.1016/j.ast.2024.109747
• Gutman, Shaul. 1979. “On Optimal Guidance for Homing Missiles.” Journal of Guidance and Control 2 (4): 296–300. https://doi.org/10.2514/3.55878
• Gutman, Shaul. 2008. “Can Lead-Lag Guidance Compensator Guarantee Zero-Miss-Distance?” Journal of Guidance, Control, and Dynamics 31 (3): 779–82. https://doi.org/10.2514/1.34042
• Gutman, Shaul, and Orly Goldan Ben-Aharon. 2009. “Proportional Navigation Miss Distance in the Presence of Bounded Inputs.” Journal of Guidance, Control, and Dynamics 32 (4): 1143–51. https://doi.org/10.2514/1.41713
• Gutman, Shaul, Orly Goldan, and Sergey Rubinsky. 2012. “Guaranteed Miss Distance in Guidance Systems with Bounded Controls and Bounded Noise.” Journal of Guidance, Control, and Dynamics 35 (3): 816–23. https://doi.org/10.2514/1.55723
• Gutman, Oren, and Zalman J. Palmor. 2011. “Proportional Navigation against Multiple Targets.” Journal of Guidance, Control, and Dynamics 34 (6): 1728–33. https://doi.org/10.2514/1.53373
• Gyu Taek Lee and Jang Gyu Lee. 1995. “Improved Command to Line-of-Sight for Homing Guidance.” IEEE Transactions on Aerospace and Electronic Systems 31 (1): 506–10. https://doi.org/10.1109/7.366337
• Głębocki, Robert, and Mariusz Jacewicz. 2020. “Sensitivity Analysis and Flight Tests Results for a Vertical Cold Launch Missile System.” Aerospace 7 (12): 168. https://doi.org/10.3390/aerospace7120168
• Hablani, Hari B., and David W. Pearson. 2004. “Miss Distance Error Analysis of Exoatmospheric Interceptors.” Journal of Guidance, Control, and Dynamics 27 (2): 283–89. https://doi.org/10.2514/1.9168
• Hace, Ales, and Marko Franc. 2014. “Pseudo-Sensorless High-Performance Bilateral Teleoperation by Sliding-Mode Control and FPGA.” IEEE/ASME Transactions on Mechatronics 19 (1): 384–93. https://doi.org/10.1109/tmech.2013.2241778
• Haddadpour, Hassan. 2006. “Aeroservoelastic Stability of Supersonic Slender-Body Flight Vehicles.” Journal of Guidance, Control, and Dynamics 29 (6): 1423–27. https://doi.org/10.2514/1.13591
• Haeussermann, Walter. 1957. “Stability Areas of Missile Control Systems.” Journal of Jet Propulsion 27 (7): 787–95. https://doi.org/10.2514/8.12939
• Hague, D. S., and Alan D. Levin. 1979. “High Performance Dash-on-Warning Air Mobile Missile System.” Journal of Aircraft 16 (8): 551–56. https://doi.org/10.2514/3.58563
• 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
• Hakim, Arif Nur, Hudoro Tahdi, and Faishol Luthfy Mahendra. 2020. “Implementation of Simple Throttling for Liquid Rocket Engine ECX1000H2-4.” In 2020 6th International Conference on Science and Technology (ICST). IEEE. https://doi.org/10.1109/icst50505.2020.9732776
• Hallbert, B. P. 1997. “Situation Awareness and Operator Performance: Results from Simulator-Based Studies.” In Proceedings of the 1997 IEEE Sixth Conference on Human Factors and Power Plants, 1997. ‘Global Perspectives of Human Factors in Power Generation’. IEEE. https://doi.org/10.1109/hfpp.1997.624933
• Hamer, Howard. 1952. “Linear Circuit Theory and Servomechanism Design.” Electrical Engineering 71 (7): 614–15. https://doi.org/10.1109/ee.1952.6437583
• 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, Tuo, Qinglei Hu, Hyo-Sang Shin, Antonios Tsourdos, and Ming Xin. 2021c. “Sensor-Based Robust Incremental Three-Dimensional Guidance Law with Terminal Angle Constraint.” Journal of Guidance, Control, and Dynamics 44 (11): 2016–30. https://doi.org/10.2514/1.g006038
• Han, Lei, Ping Jiang, Yuanliang Yu, and Bo Guo. 2014a. “Bayesian Reliability Evaluation for Customized Products with Zero-Failure Data under Small Sample Size.” In 2014 10th International Conference on Reliability, Maintainability and Safety (ICRMS). IEEE. https://doi.org/10.1109/icrms.2014.7107334
• 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, K. W., and G. J. Thaler. 1967. “Analysis and Design of Missile and Aircraft Control Systems.” Journal of Aircraft 4 (2): 121–24. https://doi.org/10.2514/3.43807
• Han, Xiao, Bo Wang, Lei Liu, and Huijin Fan. 2024a. “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, Kwang-Hee, Ick-Ho Whang, and Won-Sang Ra. 2024b. “Optimal Design Method for Cruciform Missile Autopilot via Generalization of Three-Loop Topology.” International Journal of Control, Automation and Systems 22 (12): 3616–31. https://doi.org/10.1007/s12555-024-0578-9
• Han, Yang, Zhiqiang Zheng, and Yuhai Chong. 2015. “Integrated Guidance and Control Design for Guided Bomb with Terminal Angle Constraint.” In 2015 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2015.7279495
• Hao, Li, and She Haoping. 2014. “Guidance Law Modeling Based on the Ideal Line-of-Sight with Constraint of the Terminal Flight Angle and Acceleration.” In The 26th Chinese Control and Decision Conference (2014 CCDC). IEEE. https://doi.org/10.1109/ccdc.2014.6852318
• Hao, Li, Deng Jia-hao, Wang Xuan, Wang Yong, and Luo Guo-hua. 2015. “Monopulse DOA Estimation of Two Unresolved Targets with SNR Estimation.” In 2015 IEEE Advanced Information Technology, Electronic and Automation Control Conference (IAEAC). IEEE. https://doi.org/10.1109/iaeac.2015.7428633
• 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 Xie, Jun Hu, and Wen-Yan Yin. 2014. “Anti-Jamming Performance Simulation and Analysis of Tactical Data Link Communication System.” In 2014 International Symposium on Electromagnetic Compatibility. IEEE. https://doi.org/10.1109/emceurope.2014.6931066
• Harbater, Z., and A. Margalit. 2000. “A Bit System That Guarantees Better Accuracy for Monopulse Antenna Detection Systems.” IEEE Antennas and Propagation Magazine 42 (6): 82–86. https://doi.org/10.1109/74.894184
• 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
• Harmuth, Henning F. 1978. “Low-Angle Tracking by Carrier-Free Radar.” IEEE Transactions on Electromagnetic Compatibility EMC-20 (3): 419–25. https://doi.org/10.1109/temc.1978.303674
• Hart, R. W., and F. T. McClure. 1965. “Theory of Acoustic Instability in Solid-Propellant Rocket Combustion.” Symposium (International) on Combustion 10 (1): 1047–65. https://doi.org/10.1016/s0082-0784(65)80246-6
• Hashtrudi-Zaad, K., and S. E. Salcudean. 2000. “Analysis and Evaluation of Stability and Performance Robustness for Teleoperation Control Architectures.” In Proceedings 2000 ICRA. Millennium Conference. IEEE International Conference on Robotics and Automation. Symposia Proceedings (Cat. No.00CH37065), vol. 4. IEEE. https://doi.org/10.1109/robot.2000.845141
• Hasturk, Ozgur. 2015. “A Novel Electromechanical Actuator for Missile Jet Vane Thrust Control.” In 2015 IEEE International Conference on Advanced Intelligent Mechatronics (AIM). IEEE. https://doi.org/10.1109/aim.2015.7222718
• Havlikova, Marie, and Sona Sediva. 2012. “Reliability Analysis of the Human Operator.” In Proceedings of the 13th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/carpathiancc.2012.6228641
• Haykin, S. n.d. “Where Do We Stand on High Resolution in Low-Angle Tracking Radar?” In Fourth Annual ASSP Workshop on Spectrum Estimation and Modeling. IEEE. https://doi.org/10.1109/spect.1988.206168
• 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
• He, Xingcai, Wanchun Chen, and Liang Yang. 2019. “An Intercept Guidance Law with Impact-Angle-Constrained Based on Linear Gauss Pseudospectral Model Predictive Control.” In 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2019.8881042
• He, Xingcai, Wanchun Chen, and Liang Yang. 2020b. “Suboptimal Impact-Angle-Constrained Guidance Law Using Linear Pseudospectral Model Predictive Spread Control.” IEEE Access 8: 102040–50. https://doi.org/10.1109/access.2020.2996752
• He, Songhua, and Tenglong Guo. 2012. “Main-Lobe Jamming Suppression for Missile-Borne Phased Array High-Repetition Stepped Frequency Radar.” In 2012 IEEE International Conference on Information Science and Technology. IEEE. https://doi.org/10.1109/icist.2012.6221771
• 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, Shaoming, Defu Lin, and Jiang Wang. 2015b. “Robust Terminal Angle Constraint Guidance Law with Autopilot Lag for Intercepting Maneuvering Targets.” Nonlinear Dynamics 81 (1–2): 881–92. https://doi.org/10.1007/s11071-015-2037-x
• 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. 2017b. “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, Shaoming, Tao Song, and Defu Lin. 2017a. “Impact Angle Constrained Integrated Guidance and Control for Maneuvering Target Interception.” Journal of Guidance, Control, and Dynamics 40 (10): 2653–61. https://doi.org/10.2514/1.g002201
• He, Fan, Housheng Su, and Yaofeng Su. 2026. “Zero-Effort-Miss/Zero-Effort-Angle-Error Guidance for UAV Interception in Nonadvantageous Engagements with Terminal Angle Constraint.” IEEE Transactions on Aerospace and Electronic Systems 62: 7747–63. https://doi.org/10.1109/taes.2026.3672747
• He, Xiaodong, Jun Zhu, Jun Wang, Dongping Du, and Bin Tang. 2014. “False Target Deceptive Jamming for Countering Missile-Borne SAR.” In 2014 IEEE 17th International Conference on Computational Science and Engineering. IEEE. https://doi.org/10.1109/cse.2014.364
• Hebbar, K. Sheshagiri, and P. A. Paranjpe. 1969. “Skin Friction in Compressible Turbulent Boundary Layers.” AIAA Journal 7 (4): 793–96. https://doi.org/10.2514/3.5228
• Hei, Yanlin, Min Wang, Zhongxiang Shen, and Wen Wu. 2023. “Radial Line Slot Array of Low Radar Cross Section for Target Detection and Radar Stealth in Missile-Borne Sensing Systems.” IEEE Sensors Journal 23 (22): 28084–94. https://doi.org/10.1109/jsen.2023.3319969
• Heimbs, Sebastian, Josef Ritzer, and Johannes Markmiller. 2015. “A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft.” International Journal of Aerospace Engineering 2015: 1–8. https://doi.org/10.1155/2015/897213
• Heinrich, Helmut G. 1966. “Aerodynamics of the Supersonic Guide Surface Parachute.” Journal of Aircraft 3 (2): 105–11. https://doi.org/10.2514/3.43713
• Helldin, Tove, and Goran Falkman. 2012. “Human-Centered Automation for Improving Situation Awareness in the Fighter Aircraft Domain.” In 2012 IEEE International Multi-Disciplinary Conference on Cognitive Methods in Situation Awareness and Decision Support. IEEE. https://doi.org/10.1109/cogsima.2012.6188379
• Heller, D. M. 1955. “Making a Guided Missile.” Journal of Jet Propulsion 25 (9): 8–9. https://doi.org/10.2514/8.6755
• Heller, Carmit, Isaac Yaesh, and Joseph Z. Ben-Asher. 2013. “Optimal Setting of the Proportional-Navigation Gain.” Journal of Guidance, Control, and Dynamics 36 (3): 887–90. https://doi.org/10.2514/1.59226
• Henareh, N., and Y. Norouzi. 2016. “Game Theory Modeling of MIMO Radar and ARM Missile Engagement.” In 2016 8th International Symposium on Telecommunications (IST). IEEE. https://doi.org/10.1109/istel.2016.7881875
• Hermite, Xavier, and Fabien Lefebvre. 2019. “A Test Reduction Strategy for Reliability Demonstration.” Procedia Structural Integrity 19: 130–39. https://doi.org/10.1016/j.prostr.2019.12.016
• Hess, Ronald A. 1979. “A Rationale for Human Operator Pulsive Control Behavior.” Journal of Guidance and Control 2 (3): 221–27. https://doi.org/10.2514/3.55864
• Hess, J. L., and A. M. O. Smith. 1967. “Static-Pressure Probes Derived from Supersonic Slender-Body Theory.” Journal of Aircraft 4 (5): 409–15. https://doi.org/10.2514/3.43860
• Hesse, W. J., and L. J. Boyer. 1962. “Airborne Range Stations for Control of Nuclear Missile Test Vehicles.” IRE Transactions on Nuclear Science 9 (1): 363–68. https://doi.org/10.1109/tns2.1962.4315930
• Hewer, G. A., R. Klabunde, and C. Kenney. n.d. “A Structured Singular Value Approach to Missile Autopilot Analysis.” In IEEE Digest on Aerospace Applications Conference. IEEE. https://doi.org/10.1109/aero.1988.38673
• Hewer, G. A., Richard Klabunde, and Charles Kenney. 1988. “A Structured Singular Value Approach to Missile Autopilot Analysis II.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789737
• Higashino, Akihisa, Yuh Yamashita, and Koichi Kobayashi. 2019. “Control of Bilateral Teleoperation System Consisting of Heterogeneous Manipulators with Communication Delay.” IFAC-PapersOnLine 52 (16): 747–52. https://doi.org/10.1016/j.ifacol.2019.12.052
• 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
• Hirwani, Vijay, Ashwini Ratnoo, and Yerrapragada Krishna. 2022. “Polynomial Guidance Law for Dual-Seeker Interceptors.” Journal of Guidance, Control, and Dynamics 45 (3): 533–44. https://doi.org/10.2514/1.g006291
• Hisanosuke Kawada and Toru Namerikawa. 2008. “Bilateral Control of Nonlinear Teleoperation with Time Varying Communication Delays.” In 2008 American Control Conference. IEEE. https://doi.org/10.1109/acc.2008.4586489
• Ho, M. T., H. A. Krichene, and G. F. Ricciardi. 2017. “Jamming Mitigation in Digital Monopulse Angle Estimation.” In 2017 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2017.7944396
• 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
• Hodzic, Mirza, and Naser Prljaca. 2021. “Simulation of Short Range Missile Guidance Using Proportional Navigation.” In 2021 20th International Symposium INFOTEH-JAHORINA (INFOTEH). IEEE. https://doi.org/10.1109/infoteh51037.2021.9400676
• Hogan, Brendan, Ellen J. Bass, and David Westbrook. 2010. “A Human-Automation Interaction Approach to the Evaluation of Resource Allocation Strategies in Adaptive Distributed Sensor Networks.” In 2010 IEEE International Conference on Systems, Man and Cybernetics. IEEE. https://doi.org/10.1109/icsmc.2010.5642301
• Hokanson, Jeffrey M. 2026. “Optimized Squintings for Amplitude Monopulse Direction-of-Arrival Estimation.” In 2026 IEEE Radar Conference (RadarConf’26). IEEE. https://doi.org/10.1109/radarconf2663773.2026.11675525
• Hokayem, P. F., D. M. Stipanovic, and M. W. Spong. 2006. “Suboptimal Master-Slave Teleoperation Control with Delays.” In 2006 American Control Conference. IEEE. https://doi.org/10.1109/acc.2006.1656518
• Holder, E. J., and V. B. Sylvester. 1990. “An Analysis of Modern versus Classical Homing Guidance.” IEEE Transactions on Aerospace and Electronic Systems 26 (4): 599–606. https://doi.org/10.1109/7.55553
• Hollister, Walter M., and Michael S. Vernturino. 1978. “Radar Beacon Tracking with Downlinked Heading and Airspeed.” Journal of Guidance and Control 1 (1): 21–25. https://doi.org/10.2514/3.55739
• Hollnagel, Erik, and Andreas Bye. 2000. “Principles for Modelling Function Allocation.” International Journal of Human-Computer Studies 52 (2): 253–65. https://doi.org/10.1006/ijhc.1999.0288
• Hong, Daseon, Minjeong Kim, and Sungsu Park. 2020. “Study on Reinforcement Learning-Based Missile Guidance Law.” Applied Sciences 10 (18): 6567. https://doi.org/10.3390/app10186567
• Hong, Xilei, Zhennan Liang, Yuanyuan Song, and Shanqing Hu. 2019a. “Angular Glint Analysis Based on Parametric Model of Target.” In 2019 IEEE International Conference on Signal, Information and Data Processing (ICSIDP). IEEE. https://doi.org/10.1109/icsidp47821.2019.9173462
• Hong, Ju-Hyeon, Sang-Sup Park, Chang-Hun Lee, and Chang-Kyung Ryoo. 2019b. “Study on Parasite Effect with Strapdown Seeker in Consideration of Time Delay.” Journal of Guidance, Control, and Dynamics 42 (6): 1383–92. https://doi.org/10.2514/1.g004040
• Hong, Jin-woo, Joon-hyung Yeom, Seong-ho Song, and In-joong Ha. 2006. “A Singular Perturbation-like Method to Compensate the Effect of Fin-Actuator Dynamics in Nonlinear Missile Control.” In 2006 SICE-ICASE International Joint Conference. IEEE. https://doi.org/10.1109/sice.2006.315403
• Hong Cheng Yin and Pei Rang Huang. 2008. “Further Comparison between Two Concepts of Radar Target Angular Glint.” IEEE Transactions on Aerospace and Electronic Systems 44 (1): 372–80. https://doi.org/10.1109/taes.2008.4517012
• Hongchao Zhao, Ruchuan Zhang, and Hongyun Yu. 2008. “Extended Proportional Navigation Guidance Law for Anti-Warship Missile Based on Lyapunov Stability.” In 2008 7th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2008.4594219
• Hongcheng Yin and Peikang Huang. 1995. “Unification and Comparison between Two Concepts of Radar Target Angular Glint.” IEEE Transactions on Aerospace and Electronic Systems 31 (2): 778–83. https://doi.org/10.1109/7.381924
• Hongwei, Huo, Dong Chaoyi, Lan Jian, and Wang Yulong. 2018. “Measurement Method of the Air Miss Distance and ExplosionDistance of Proximity Fuse.” In 2018 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2018.8623450
• Hongwei Li and Jun Wang. 2011. “Maneuvering Target Tracking Using IMMPF in Passive Coherent Location Radar with Glint Noise.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159728
• Hopkins, Edward J., and Mamoru Inouye. 1971. “An Evaluation of Theories for Predicting Turbulent Skin Friction Andheat Transfer on Flat Plates at Supersonic and Hypersonic Mach Numbers.” AIAA Journal 9 (6): 993–1003. https://doi.org/10.2514/3.6323
• Horiuchi, S., and N. Yuhara. 1988. “Detection of System Failure by Human Operator – Mathematical Model and Experiments.” IFAC Proceedings Volumes 21 (5): 267–72. https://doi.org/10.1016/s1474-6670(17)53918-x
• Hosseini-Pishrobat, Mehran, and Erdinc Tatar. 2025. “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
• Hou, Zhiwei, Lei Liu, and Yongji Wang. 2017. “Time-to-Go Estimation for Terminal Sliding Mode Based Impact Angle Constrained Guidance.” Aerospace Science and Technology 71: 685–94. https://doi.org/10.1016/j.ast.2017.10.016
• Hou, Linfei, Honglin Liu, Ting Yang, Shuaibin An, and Rui Wang. 2023. “An Intelligent Autonomous Morphing Decision Approach for Hypersonic Boost-Glide Vehicles Based on DNNs.” Aerospace 10 (12): 1008. https://doi.org/10.3390/aerospace10121008
• Hou, Shujuan, and Siliang Wu. 2006. “Multi-Targets Miss Distance Measurement Based on a Sequence of Image Processing Techniques.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.345590
• Hou, Zhiwei, and Xuebin Zhuang. 2025. “Impact Angle Constrained Three Dimensional All-Aspect Guidance against Maneuvering Target.” Aerospace Science and Technology 165: 110410. https://doi.org/10.1016/j.ast.2025.110410
• Houweling, Koen Pieter, Steven C. Mallam, Koen van de Merwe, and Kjetil Nordby. 2024. “The Effects of Augmented Reality on Operator Situation Awareness and Head-Down Time.” Applied Ergonomics 116: 104213. https://doi.org/10.1016/j.apergo.2023.104213
• Howard, Dean D. 1980. “Comments on ‘Millimeter-Wave Missile Seeker Aimpoint Wander Phenomenon’.” Journal of Guidance and Control 3 (3): 284–85. https://doi.org/10.2514/3.55987
• 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
• Howard, William W., Charles E. Thornton, and R. Michael Buehrer. 2023. “Timely Target Tracking in Cognitive Radar Networks.” In 2023 IEEE Radar Conference (RadarConf23). IEEE. https://doi.org/10.1109/radarconf2351548.2023.10149692
• Hsu, Y. C., James Younger, and S. N. Balakrishnan. 1991. “Estimation of Process Noise Covariance in Homing Guidance.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791816
• Hu, Qinglei, Ruihao Cao, Tuo Han, and Ming Xin. 2021a. “Field-of-View Limited Guidance with Impact Angle Constraint and Feasibility Analysis.” Aerospace Science and Technology 114: 106753. https://doi.org/10.1016/j.ast.2021.106753
• Hu, Runsheng, Riccardo M. G. Ferrari, Zhenyu Chen, et al. 2021b. “System Analysis and Controller Design for the Electric Pump of a Deep-Throttling Rocket Engine.” Aerospace Science and Technology 114: 106729. https://doi.org/10.1016/j.ast.2021.106729
• Hu, Qinglei, Tuo Han, and Ming Xin. 2018. “New Impact Time and Angle Guidance Strategy via Virtual Target Approach.” Journal of Guidance, Control, and Dynamics 41 (8): 1755–65. https://doi.org/10.2514/1.g003436
• Hu, Wenfeng, Bo He, Ying Bai, Linlin Tang, and Wansheng Nie. 2026b. “A POD-DeepONet Based Parameter Identification Framework for the Phenomenological Model of Liquid Rocket Engine Combustion Instability.” Aerospace Science and Technology 177: 112837. https://doi.org/10.1016/j.ast.2026.112837
• Hu, Chaofang, and Yanwen Liu. 2013. “Adaptive Fuzzy DSC Control Based on ISpS for Hypersonic Vehicle.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6560962
• Hu, Hong, Rengli Liu, Xuelian Zhong, and Haitao Deng. 2019. “Altitude Estimation of Missile-Borne Radar Seeker Based on Front-Downward View and Range-Doppler Analysis.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048577
• Hu, Wenlin, Chenfeng Sun, and Dongbing Li. 2020. “Bayesian Estimations of Reliability on One Type of Missile with Zero-Failure Data.” In 2020 International Conference on Artificial Intelligence and Electromechanical Automation (AIEA). IEEE. https://doi.org/10.1109/aiea51086.2020.00048
• Hu, Jing, Weibo Sun, Mingyang Zhang, Tao Chao, and Ming Yang. 2023. “Guidance Method for Re-Entry Glide Vehicle Considering No-Fly Zone Avoidance.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10240299
• Hu, Zhengdong, Xuemei Tang, and Yueping Wang. 2011. “A 3-Dimensional Robust Guidance Law with Impact Angle Constraint.” In 2011 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2011.5968330
• Hu, Zhe, Liang Xiao, and Wenjun Yi. 2025c. “A Generalized Super-Twisting Extended State Observer for Angle-Constrained Terminal Sliding Mode Guidance Law.” Aerospace 12 (3): 252. https://doi.org/10.3390/aerospace12030252
• Hu, Zhe, Wenjun Yi, Weichen Qian, and Hongqiao Yin. 2025d. “Predefined-Time Cooperative Guidance Law for Multiple Missiles with Terminal Angle Constraint.” In 2025 4th International Symposium on Aerospace Engineering and Systems (ISAES). IEEE. https://doi.org/10.1109/isaes66870.2025.11274350
• Hu, Zhe, Wenjun Yi, and Liang Xiao. 2025b. “Deep Reinforcement Learning-Based Impact Angle-Constrained Adaptive Guidance Law.” Mathematics 13 (6): 987. https://doi.org/10.3390/math13060987
• Hu, Juan, Lei Zuo, Zhengyu Lan, and Chao He. 2024b. “Joint Trajectory Optimization and Power Allocation for Target Tracking in Airborne Radar Network with Missing Data.” In 2024 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar58436.2024.10994019
• Hua, Changchun, and Yana Yang. 2011. “Transparency Performance Improvement for Bilateral Teleoperation with Direct Force-Feedback Control.” In 2011 IEEE International Workshop on Haptic Audio Visual Environments and Games. IEEE. https://doi.org/10.1109/have.2011.6088403
• Hua Lan, Zhishan Zhang, ZengfuWang, and Quan Pan. 2017. “Random Sample Consensus Algorithm for Multiple Target Tracking in over-the-Horizon Radar.” In 2017 18th International Radar Symposium (IRS). IEEE. https://doi.org/10.23919/irs.2017.8008099
• Huang, J., and C. F. Lin. 1993. “Sliding Mode Control of HAVE DASH II Missile Systems.” In 1993 American Control Conference. IEEE. https://doi.org/10.23919/acc.1993.4792833
• Huang, Ming, Yuanyuan Liu, Gongliu Yang, and Xiao Zhou. 2016a. “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, Xulei, Yuan Qi, and Weijie Zhang. 2019. “Rotating Strapdown Seeker Missile Target Sight Angular Velocity Extraction Method.” In 2019 IEEE 9th Annual International Conference on CYBER Technology in Automation, Control, and Intelligent Systems (CYBER). IEEE. https://doi.org/10.1109/cyber46603.2019.9066714
• Huang, Lan, Jianmei Song, Minqiang Zhang, and Gaohua Cai. 2016b. “Optical Flow Based Guidance System Design for Semi-Strapdown Image Homing Guided Missiles.” Chinese Journal of Aeronautics 29 (5): 1345–54. https://doi.org/10.1016/j.cja.2016.08.011
• Huang, Wei, Jiancheng Xu, Huaxing Wu, and Junbing Li. 2017a. “Error Analysis for Guidance Control Parameters of Air to Surface SAR Missile.” In 2017 9th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC). IEEE. https://doi.org/10.1109/ihmsc.2017.67
• Huang, Yangang, Zhenhai Xu, and Ziyuan Xiong. 2013. “Study on Monopulse Angle Measurement Method Based on Virtual Polarization Matching.” Journal of Electronics (China) 30 (5): 447–53. https://doi.org/10.1007/s11767-013-3089-z
• Huang, Shukun, Zhenyuan Zhang, Mingqi Chen, Zhaoyang Wu, Qiang Li, and Zhong Ming. 2024a. “Designing of a Dexterous Hand and Performance Evaluation Based on Teleoperation.” In 2024 International Conference on Intelligent Robotics and Automatic Control (IRAC). IEEE. https://doi.org/10.1109/irac63143.2024.10871387
• Huang, Jingshuai, Hongbo Zhang, Guojian Tang, and Weimin Bao. 2017b. “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, Jingshuai, Hongbo Zhang, Shang Wu, Guojian Tang, and Weimin Bao. 2020. “An Interacting-Multiple-Model Method for Tracking a Hypersonic Glide Target.” In 2020 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc49329.2020.9164342
• Hubner, J. P., and B. F. Carroll. 1993. “Thin-Oil-Film Interferometric Skin-Friction Measurements in Short-Duration Supersonic Flow.” Experiments in Fluids 15-15 (4–5): 315–22. https://doi.org/10.1007/bf00223409
• 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, Yaoluo, Ying Nan, Shaodong Chen, Quanxin Ding, and Shengliang Wu. 2015. “Dynamic Attack Zone of Air-to-Air Missile after Being Launched in Random Wind Field.” Chinese Journal of Aeronautics 28 (5): 1519–28. https://doi.org/10.1016/j.cja.2015.08.013
• Huiyuan Zhang, Liangshuai Guo, Zichang Liang, and Xiaobing Wang. 2016. “Bi-Static Angular Glint Calculation on Complex Targets in near-Regions via Multilevel Fast Multipole Algorithm.” In 2016 Progress in Electromagnetic Research Symposium (PIERS). IEEE. https://doi.org/10.1109/piers.2016.7734684
• Hull, D. G. n.d. “Dual Control Guidance Law for Homing Missiles.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.721002
• Hull, David G., and Jean-Marie Seguin. 1994. “Guidance Law for Hypersonic Gliders Based on Piecewise Constant Control.” Journal of Guidance, Control, and Dynamics 17 (5): 903–7. https://doi.org/10.2514/3.21288
• Hull, D. G., J. L. Speyer, and D. B. Burris. 1990. “Linear-Quadratic Guidance Law for Dual Control of Homing Missiles.” Journal of Guidance, Control, and Dynamics 13 (1): 137–44. https://doi.org/10.2514/3.20527
• Hull, D. G., J. L. Speyer, and C. Y. Tseng. 1985. “Maximum-Information Guidance for Homing Missiles.” Journal of Guidance, Control, and Dynamics 8 (4): 494–97. https://doi.org/10.2514/3.20010
• 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
• Hultgren, R. D., and L. B. Hallman. 1947. “The Theory and Application of the Radar Beacon.” Proceedings of the IRE 35 (7): 716–30. https://doi.org/10.1109/jrproc.1947.234257
• Hung, E. K. L., and J. E. Morris. n.d. “A Technique to Refine the Elevation Estimates in Low-Angle Tracking Data Measured with an Array Antenna.” In IEEE International Conference on Radar. IEEE. https://doi.org/10.1109/radar.1990.201204
• Hunt, Eric E. 2011. “Developing the Stockpile Reliability Program Plan for a New Missile.” In 2011 Proceedings - Annual Reliability and Maintainability Symposium. IEEE. https://doi.org/10.1109/rams.2011.5754450
• Hunt, E. E., and J. A. Wester. 2013. “Optimizing the Non-Destructive Test Program for a Missile Inventory.” In 2013 Proceedings Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams.2013.6517748
• Hunziker, Raul R. 1960. “On the Calculation of the Minimum Wave Plus Vortex Drag of Supersonic Wings.” Zeitschrift für angewandte Mathematik und Physik ZAMP 11 (6): 504–8. https://doi.org/10.1007/bf01595402
• Huo, Xin, Jiping Peng, Kemao Ma, Jinpeng Zhang, and Jipeng Dong. 2016. “A Pitch Autopilot Design for Blended Aero and Reaction-Jet Air-to-Air Missile via Piecewise Sliding Mode Control.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7829130
• Hutt, G. R., and A. J. Howe. 1988. “Effects of Cross Section and Nose Geometry on Slender-Body Supersonic Aerodynamics.” Journal of Spacecraft and Rockets 25 (2): 189–92. https://doi.org/10.2514/3.25970
• Hwang, T. W., M. Tahk, and C. Park. 2005. “Adaptive Sliding Mode Neural Net Control for Missile Autopilot.” In 2005 International Conference on Control and Automation, vol. 1. IEEE. https://doi.org/10.1109/icca.2005.1528086
• Idris, Husni, Gabriele Enea, and Timothy A. Lewis. 2016. “Function Allocation between Automation and Human Pilot for Airborne Separation Assurance.” IFAC-PapersOnLine 49 (19): 25–30. https://doi.org/10.1016/j.ifacol.2016.10.456
• Ijaz, Tooba, and Aamer Iqbal Bhatti. 2019. “Comparison of Monopulse and MUSIC Estimator for Angular Parameters Estimation.” In 2019 International Conference on Electrical, Communication, and Computer Engineering (ICECCE). IEEE. https://doi.org/10.1109/icecce47252.2019.8940709
• Imado, F. 2004. “A Study on a Missile Guidance System against a Randomly Maneuvering Air-to-Surface Missile.” In Proceedings of the 2004 IEEE International Conference on Control Applications, 2004.. IEEE. https://doi.org/10.1109/cca.2004.1387249
• Imado, Fumiaki, Takeshi Kuroda, and Susumu Miwa. 1991. “Optimal Thrust Control of a Missile with a Pulse Motor.” Journal of Guidance, Control, and Dynamics 14 (2): 377–82. https://doi.org/10.2514/3.20649
• Imado, Fumiaki, and Susumu Miwa. 1994. “Missile Guidance Algorithm against High-g Barrel Roll Maneuvers.” Journal of Guidance, Control, and Dynamics 17 (1): 123–28. https://doi.org/10.2514/3.21168
• Imado, Fumiaki, and Sachio Uehara. 1998. “High-g Barrel Roll Maneuvers against Proportional Navigation from Optimal Control Viewpoint.” Journal of Guidance, Control, and Dynamics 21 (6): 876–81. https://doi.org/10.2514/2.4351
• Inaba, T., and Y. Matsuo. 1997. “Loop-Shaping Characteristics of a Human Operator in a Force Reflective Manual Control System.” In 1997 IEEE International Conference on Systems, Man, and Cybernetics. Computational Cybernetics and Simulation. IEEE. https://doi.org/10.1109/icsmc.1997.633230
• “Incremental Stability of the Extended Missile Autopilot.” 1999. In Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251). IEEE. https://doi.org/10.1109/acc.1999.786196
• 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
• Inoue, Yasuyuki, and Yutaka Sakaguchi. 2014. “Periodic Change in Phase Relationship between Target and Hand Motion during Visuo-Manual Tracking Task: Behavioral Evidence for Intermittent Control.” Human Movement Science 33: 211–26. https://doi.org/10.1016/j.humov.2013.10.002
• “Integrated Interface for Advanced Teleoperation.” 1993. IEEE Control Systems 13 (5): 15–20. https://doi.org/10.1109/37.236318
• “An Integrated Missile Reliability Growth Program.” 1984. Microelectronics Reliability 24 (6): 1097. https://doi.org/10.1016/0026-2714(84)90909-0
• “Intelligent Sensing and Control for Advanced Teleoperation.” 1993. IEEE Control Systems 13 (3): 19–28. https://doi.org/10.1109/37.214941
• “Interval Estimation of MTBF Based on Minimal Information from a Reliability Demonstration Test.” 1987. Microelectronics Reliability 27 (6): 1031. https://doi.org/10.1016/0026-2714(87)90802-x
• Isakson, Gabriel. 1957. “A Simple Model Study of Transient Temperature and Thermal Stress Distribution Due to Aerodynamic Heating.” Journal of the Aeronautical Sciences 24 (8): 611–19. https://doi.org/10.2514/8.3917
• Ishii, E., H. Nishi, and K. Ohnishi. 2006. “Improvement of Performance in Bilateral Teleoperation by Using FPGA.” In 9th IEEE International Workshop on Advanced Motion Control, 2006.. IEEE. https://doi.org/10.1109/amc.2006.1631690
• 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
• Jacobs, Edgar M., George W. Morgenthaler, and Robert A. Sebastian. 1961. “Probability of Satellite Interception by an Air Launched Pre-Guided Missile.” ARS Journal 31 (3): 352–56. https://doi.org/10.2514/8.5479
• Jahangir, E., and R. M. Howe. 1993. “Time-Optimal Attitude Control Scheme for a Spinning Missile.” Journal of Guidance, Control, and Dynamics 16 (2): 346–53. https://doi.org/10.2514/3.21009
• Jain, A. K. n.d. “Generating Statistically Correlated Glint and RCS for Empirically Based RF Target Models.” In Conference Proceedings Southeastcon ‘81.. IEEE. https://doi.org/10.1109/secon.1981.673601
• Jalali-Naini, Seyed Hamid, and Mohammad Ebrahimi. 2017. “Second-Order Optimal Line-of-Sight Guidance Law for Minimum and Nonminimum Phase Control Systems.” In 2017 International Conference on Mechanical, System and Control Engineering (ICMSC). IEEE. https://doi.org/10.1109/icmsc.2017.7959476
• Jamison, Lelan R. 1967. “A Method for Calculating Parachute Opening Forces for General Deployment Conditions.” Journal of Spacecraft and Rockets 4 (4): 498–502. https://doi.org/10.2514/3.28894
• Jashwanth, Punyamurthy, Saurabh Kumar, and Shashi Ranjan Kumar. 2026. “True-Proportional Navigation Based Exact-Time Convergent Impact Time Guidance.” In 2026 IEEE 18th International Workshop on Variable Structure Systems (VSS). IEEE. https://doi.org/10.1109/vss69650.2026.11655764
• Jee-Hwan Ryu and Jong-Hwan Kim. 2005. “Stable and High Performance Teleoperation with Time Domain Passivity Control: Reference Energy Following Scheme.” In ICAR ‘05. Proceedings., 12th International Conference on Advanced Robotics, 2005.. IEEE. https://doi.org/10.1109/.2005.1507497
• Jeffrey, T. W. n.d. “Track Quality Estimation for Multiple-Target Tracking Radars.” In Proceedings of the IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1989.47619
• Jen King Jao. 1994. “A Matched Array Beamforming Technique for Low Angle Radar Tracking in Multipath.” In Proceedings of 1994 IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1994.328119
• 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. 1988b. “Sideslip Effects on Fin-Fin Interference in Supersonic Missile Aerodynamics.” Journal of Spacecraft and Rockets 25 (6): 385–92. https://doi.org/10.2514/3.26017
• Jensen, J. R. 1999. “Angle Measurement with a Phase Monopulse Radar Altimeter.” IEEE Transactions on Antennas and Propagation 47 (4): 715–24. https://doi.org/10.1109/8.768812
• Jeon, In-Soo, Mark Karpenko, and Jin-Ik Lee. 2020. “Connections between Proportional Navigation and Terminal Velocity Maximization Guidance.” Journal of Guidance, Control, and Dynamics 43 (2): 383–88. https://doi.org/10.2514/1.g004672
• Jeon, In-Soo, and Jin-Ik Lee. 2017. “Impact-Time-Control Guidance Law with Constraints on Seeker Look Angle.” IEEE Transactions on Aerospace and Electronic Systems 53 (5): 2621–27. https://doi.org/10.1109/taes.2017.2698837
• Jeon, In-Soo, Jin-Ik Lee, and Min-Jea Tahk. 2010. “Homing Guidance Law for Cooperative Attack of Multiple Missiles.” Journal of Guidance, Control, and Dynamics 33 (1): 275–80. https://doi.org/10.2514/1.40136
• Jeon, In-Soo, Jin-Ik Lee, and Min-Jea Tahk. 2016. “Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation.” Journal of Guidance, Control, and Dynamics 39 (8): 1885–90. https://doi.org/10.2514/1.g001681
• Jex, H. R., J. D. McDonnell, and A. V. Phatak. 1966b. “A ``Critical’’ Tracking Task for Manual Control Research.” IEEE Transactions on Human Factors in Electronics HFE-7 (4): 138–45. https://doi.org/10.1109/thfe.1966.232660
• Ji, Yi, Pei Pei, Defu Lin, Jianting Zhao, and Wei Wang. 2020. “Compound Robust Flight Time and Heading Angle Constrained Guidance Law.” IFAC-PapersOnLine 53 (2): 9452–57. https://doi.org/10.1016/j.ifacol.2020.12.2417
• Jia, Yachao, Zhen Yang, Yupeng He, Xingyu Wang, and Deyun Zhou. 2023. “Dynamic Effectiveness Evaluation Method for beyond-Visual-Range Air-to-Air Missile after Launch.” In 2023 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus58632.2023.10318387
• Jialing, Zhou, and Yang Jianying. 2015. “Integrated Missile Guidance and Control Design with Smooth Adaptive Sliding Mode Control.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260451
• 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
• Jian-tao, Wang, Qin Yu-liang, Deng Bin, and Li Xiang. 2009. “A Modified Omega-K Algorithm for Missile-Borne SAR Imaging with the Dive Trajectory.” In 2009 2nd Asian-Pacific Conference on Synthetic Aperture Radar. IEEE. https://doi.org/10.1109/apsar.2009.5374305
• Jianbin, Lu, Hu Weidong, and Yu Wenxian. 2006. “Adaptive Beam Scheduling Algorithm for an Agile Beam Radar in Multi-Target Tracking.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343564
• Jiang, Yifu, Zhihong Deng, and Yongqing Zhang. 2025. “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, Zhanyuan, Jianquan Ge, Qiangqiang Xu, and Tao Yang. 2021a. “Impact Time Control Cooperative Guidance Law Design Based on Modified Proportional Navigation.” Aerospace 8 (8): 231. https://doi.org/10.3390/aerospace8080231
• Jiang, Zhanyuan, Jianquan Ge, Qiangqiang Xu, and Tao Yang. 2021b. “A Modified Proportional Navigation Guidance Law for Impact Time Control.” In 2021 6th International Conference on Automation, Control and Robotics Engineering (CACRE). IEEE. https://doi.org/10.1109/cacre52464.2021.9501293
• Jiang, Zhi-peng, Hua-ting Han, Gang Feng, and Xin-sheng Dai. 2011. “Research on Algorithms of Land-to-Air Missile Launch Control System Based on CAN Bus.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5777239
• Jiang, Xiaoming, Aiping Li, and Chang Zhang. 2017. “An Inertial Stability and Tracking Control Method for the Nonlinear Driving Missile Launcher.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028127
• Jiang, Defu, Ming Liu, Yiyue Gao, and Yang Gao. 2019. “Time-Matching Extended Target Probability Hypothesis Density Filter for Multi-Target Tracking of High Resolution Radar.” Signal Processing 157: 151–60. https://doi.org/10.1016/j.sigpro.2018.12.002
• 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, Yi-cheng, and Chun-xi Yu. 2009. “A Novel Approach for Angle Measuring Improvement in Monopulse Tracking.” In 2009 Sixth International Conference on Fuzzy Systems and Knowledge Discovery. IEEE. https://doi.org/10.1109/fskd.2009.148
• Jianguo, Guo, Li Yifei, and Zhou Jun. 2018. “Finite Time Control for Generic Hypersonic Vehicle.” In 2018 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2018.8407770
• 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
• Jianyu, Zhao, Yu Jianqiao, and Yang Kun. 2017. “Optimal Linear Quadratic Guidance Law with Terminal Impact Angle Constraint.” In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2017.7978462
• Jie, Chen, Pan Changpeng, and Gu Wenjin. 2006a. “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
• Jie, Zhou, Wang Jian-ming, and Xing Wen-ge. 2006b. “Study on Low-Angle Tracking Technique for Shipboard Phased Array Radar.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343591
• Jin, Junfeng, and Min Ma. 2016. “Data Association Algorithm for Ballistic Missile Target Based on Optimal Assignment Strategy.” In 2016 CIE International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2016.8059446
• Jin, Junfeng, Min Ma, and Chang Liu. 2021. “Group Targets Splitting Algorithm for Ballistic Missile Penetration Applications.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028257
• Jin, Guoqiang, Qinghua Ma, and Yangyang Zhao. 2016. “Guidance System Design for Downward-Looking Strapdown Homing Miniature Munitions.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554199
• Jin, Zongyao, and Prabhakar R. Pagilla. 2020. “Subgoal Learning via Operator Command Quantification for Human-Machine Shared Control Task Modeling.” In 2020 American Control Conference (ACC). IEEE. https://doi.org/10.23919/acc45564.2020.9147762
• 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, Yushu, Xu Xu, Qingchun Yang, and Shaohua Zhu. 2019. “Numerical Investigation of Flame Appearance and Heat Flux and in a Deep-Throttling Variable Thrust Rocket Engine.” Aerospace Science and Technology 88: 457–67. https://doi.org/10.1016/j.ast.2019.03.042
• Jin, Du, Rui Zhang, Yuan Li, Yuki Ban, and Shin’Ichi Warisawa. 2024. “Mitigating Latency Effects on Subjective Experience in Robot Teleoperation Using a VR-Enabled Virtual Spring.” In 2024 IEEE International Symposium on Mixed and Augmented Reality (ISMAR). IEEE. https://doi.org/10.1109/ismar62088.2024.00144
• Jin Ming, Qiao Xiaolin, Zhao Yinan, and Jia Shilou. 2003. “Analyses and Compensation for Radar Target Angular Glint.” In 6th International SYmposium on Antennas, Propagation and EM Theory, 2003. Proceedings. 2003. IEEE. https://doi.org/10.1109/isape.2003.1276726
• Jinchuan Hu, Jinglin Li, and Wanchun Chen. 2015. “Longitudinal Characteristics of Steady Glide Trajectory for Hypersonic Vehicle.” In 2015 International Conference on Control, Automation and Information Sciences (ICCAIS). IEEE. https://doi.org/10.1109/iccais.2015.7338676
• Jing, Liang, Liang Zhang, Jifeng Guo, and Naigang Cui. 2020. “Fixed-Time Cooperative Guidance Law with Angle Constraint for Multiple Missiles against Maneuvering Target.” IEEE Access 8: 73268–77. https://doi.org/10.1109/access.2020.2987821
• Jing, Jiawei, Liangyu Zhao, and Zhiqi Niu. 2018. “Observer-Based Integrated Guidance and Control under Terminal Impact Angle Constraint.” In 2018 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2018.8623527
• Jinzhao, Pan, Xu Yun, and Xu Chengjun. 2024. “Assessment and Analysis of Anti-Portable Missile Damage System Based on Fusion Data Link Network.” In 2024 IEEE 6th International Conference on Power, Intelligent Computing and Systems (ICPICS). IEEE. https://doi.org/10.1109/icpics62053.2024.10797167
• Jiu-ling Zhao and Jiu-fen Zhao. 2006. “Application of BPNN and CBR on Fault Diagnosis for Missile Electronic Command System.” In 2006 6th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2006.1714187
• Jo, Jeil, and Jaemin Ahn. 2017. “A Study on Jamming Technique against Monopulse Type Missile.” In 2017 International Conference on Information and Communication Technology Convergence (ICTC). IEEE. https://doi.org/10.1109/ictc.2017.8190835
• Joarder, R. 2018. “On the Mechanism of Wave Drag Reduction by Concentrated Laser Energy Deposition in Supersonic Flows over a Blunt Body.” Shock Waves 29 (4): 487–97. https://doi.org/10.1007/s00193-018-0868-3
• Joe, Jeffrey C., John O’Hara, Jacques V. Hugo, and Johanna H. Oxstrand. 2015. “Function Allocation for Humans and Automation in the Context of Team Dynamics.” Procedia Manufacturing 3: 1225–32. https://doi.org/10.1016/j.promfg.2015.07.204
• Johnson, Nicholas, Michael Civerolo, and Nicholas Lumsden. 2015. “Techniques and Methods for Adaptive Single Antenna Radar System Polarization Optimization for Anti Jam and Anti Clutter Applications.” In 2015 IEEE Radar Conference (RadarCon). IEEE. https://doi.org/10.1109/radar.2015.7130997
• Jones, H. C. 1959b. “The Relation between Sample Size and Confidence in Test-to-Failure Reliability Programs.” IRE Transactions on Reliability and Quality Control PGRQC-16: 24–33. https://doi.org/10.1109/ire-pgrqc.1959.5007206
• 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
• Joongsup Yun, Chang-Kyung Ryoo, and Taek-Lyul Song. 2008. “Strapdown Sensors and Seeker Based Guidance Filter Design.” In 2008 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2008.4694686
• Joonhyung Park, R. G. Rhinehart, and P. T. Kabamba. 2000. “Miss Analysis in Lambert Interceptions with Application to a New Guidance Law.” In Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334). IEEE. https://doi.org/10.1109/acc.2000.876720
• Joshi, Hemant, Peter Thomas, Christabel Tan, and Hongwei Wu. 2025. “Improved Vortex Lattice Method for Drag Prediction of Supersonic Wings Using Shock Cone Modelling.” Engineering with Computers 41 (5): 3815–31. https://doi.org/10.1007/s00366-025-02192-2
• 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
• 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-fang, Fan, Wang Gang, Chen Ying, and Dong Si-yu. 2016. “Impact-Angle-Constraint Look Angle Guidance for Miniature Missile.” In 2016 16th International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.1109/iccas.2016.7832432
• Jun-jie, Wang, Zhao Feng, Liu Jin, Ai Xiao-feng, and Wang Lian-dong. 2016. “Repeating Decoy Discrimination Based on Angular Glint.” In 2016 CIE International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2016.8059574
• Jung, Cheol-Goo, and Chang-Hun Lee. 2024. “Optimal Impact Angle Control Guidance Law Considering Aerodynamic Drag.” Journal of Guidance, Control, and Dynamics 47 (11): 2435–43. https://doi.org/10.2514/1.g008234
• Jung, Yeontaek, Hanna Lee, Youngjun Lee, Youdan Kim, and Jaemyung Ahn. 2024. “Composite Zero-Effort-Miss Guidance with Predictor–Corrector Steps for Ballistic Interception.” Journal of Guidance, Control, and Dynamics 47 (2): 311–25. https://doi.org/10.2514/1.g007760
• Junji Chen, Fang Yang, Kai Zhang, and Jiadong Xu. 2008. “Angular Glint Modeling and Simulation for Complex Targets.” In 2008 International Conference on Microwave and Millimeter Wave Technology. IEEE. https://doi.org/10.1109/icmmt.2008.4540856
• Junkun, Yan, Pu Wenqiang, Liu Hongwei, and Bao Zheng. 2016. “Joint Power and Bandwidth Allocation for Centeralized Target Tracking in Multiple Radar System.” In 2016 CIE International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2016.8059263
• 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
• Kaber, David B., Emrah Onal, and Mica R. Endsley. 2000a. “Design of Automation for Telerobots and the Effect on Performance, Operator Situation Awareness, and Subjective Workload.” Human Factors and Ergonomics in Manufacturing 10 (4): 409–30. https://doi.org/10.1002/1520-6564(200023)10:4<409::aid-hfm4>3.0.co;2-v
• 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
• Kada, B. 2014. “Arbitrary-Order Sliding-Mode-Based Homing-Missile Guidance for Intercepting Highly Maneuverable Targets.” Journal of Guidance, Control, and Dynamics 37 (6): 1999–2013. https://doi.org/10.2514/1.g000001
• Kada, Belkacem. 2015a. “Robust Stability Analysis and Topological Dynamics of a Nonminimum Phase Supersonic Tactical Missile.” In 2015 3rd International Conference on Control, Engineering & Information Technology (CEIT). IEEE. https://doi.org/10.1109/ceit.2015.7233157
• Kai-Bor Yu and D. J. Murrow. n.d. “Adaptive Digital Beamforming Radar for Monopulse Angle Estimation in Jamming.” In Proceedings of the Tenth IEEE Workshop on Statistical Signal and Array Processing (Cat. No.00TH8496). IEEE. https://doi.org/10.1109/ssap.2000.870126
• Kai-Bor Yu and D. J. Murrow. 2000. “Adaptive Digital Beamforming for Preserving Monopulse Target Angle Estimation Accuracy in Jamming.” In Proceedings of the 2000 IEEE Sensor Array and Multichannel Signal Processing Workshop. SAM 2000 (Cat. No.00EX410). IEEE. https://doi.org/10.1109/sam.2000.878050
• Kain, J. E., and D. J. Yost. 1977. “Command to Line-of-Sight Guidance: A Stochastic Optimal Control Problem.” Journal of Spacecraft and Rockets 14 (7): 438–44. https://doi.org/10.2514/3.57220
• Kala, Anisha Selva R., Jeraldin D. Auxillia, and Jessi Flora J․. 2027. “A Bernoulli Featured GRU Flow Sensor for Propellant Flowrate and Mixture Ratio Estimation in Transient Phase of Liquid Propellant Rocket Engine with SHAP-Interpretability.” Aerospace Science and Technology 180: 113700. https://doi.org/10.1016/j.ast.2026.113700
• 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
• Kamen, E. W., T. E. Bullock, and C.-H. Song. 1988. “Adaptive Control Applied to Missile Autopilots.” In 1988 American Control Conference. IEEE. https://doi.org/10.23919/acc.1988.4789782
• Kanda, Takeshi, Yuuki Mishina, Shoma Hayasako, Shunta Muramatsu, Kanna Yamada, and Rina Kato. 2023. “Experimental Study on High-Frequency Combustion Instability of Liquid-Propellant Rocket Engines Using off-Design Combustion Model.” Acta Astronautica 202: 595–608. https://doi.org/10.1016/j.actaastro.2022.11.006
• Kang, Seonhyeok, H. Jin Kim, Jin-Ik Lee, Byung-Eul Jun, and Min-Jea Tahk. 2009. “Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile.” Journal of Guidance, Control, and Dynamics 32 (5): 1622–28. https://doi.org/10.2514/1.39812
• Kang, Baowen, Feng Shang, and HaoYi Liu. 2023a. “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, Yu-Dong, and Bing Sun. 2011. “Numerical Simulation of Liquid Rocket Engine Thrust Chamber Regenerative Cooling.” Journal of Thermophysics and Heat Transfer 25 (1): 155–64. https://doi.org/10.2514/1.47701
• Kang, Honglong, Pengyu Wang, Shenghui Wei, and Shenmin Song. 2023b. “Three-Dimensional Impact-Time-Constrained Proportional Navigation Guidance Using Range-Varying Gain.” Aerospace Science and Technology 140: 108419. https://doi.org/10.1016/j.ast.2023.108419
• Kanter, Irving. 1979. “The Effect of Jamming on Monopulse Accuracy.” IEEE Transactions on Aerospace and Electronic Systems AES-15 (5): 738–41. https://doi.org/10.1109/taes.1979.308866
• Kaplan, C. J. 1961. “Selection of a Pressurization System for a Storable Liquid Propellant Rocket Engine.” ARS Journal 31 (6): 786–93. https://doi.org/10.2514/8.5635
• 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
• Karelahti, Janne, and Kai Virtanen. 2007. “Adaptive Controller for the Avoidance of an Unknownly Guided Air Combat Missile.” In 2007 46th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.2007.4434604
• Karelahti, Janne, Kai Virtanen, and Tuomas Raivio. 2006a. “Game Optimal Support Time of a Medium Range Air-to-Air Missile.” Journal of Guidance, Control, and Dynamics 29 (5): 1061–69. https://doi.org/10.2514/1.17910
• Karelahti, Janne, Kai Virtanen, and Tuomas Raivio. 2007. “Near-Optimal Missile Avoidance Trajectories via Receding Horizon Control.” Journal of Guidance, Control, and Dynamics 30 (5): 1287–98. https://doi.org/10.2514/1.26024
• Karpinski, Michal. 2021. “Conceptual Design of an Experimental Dual-Control Surface-to-Air Missile.” In 2021 International Conference on Military Technologies (ICMT). IEEE. https://doi.org/10.1109/icmt52455.2021.9502796
• Kashefi, Saeed, and Majid Hajatipour. 2025. “A New Design of Adaptive Predictive Autopilot for Skid-to-Turn Missile with Uncertain Dynamics through State Prediction.” Control Theory and Technology 24 (1): 24–37. https://doi.org/10.1007/s11768-025-00282-6
• 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
• Katsuyama, Yutaka, Toshio Sato, Zheng Wen, et al. 2023. “A Predictive Approach for Compensating Transmission Latency in Remote Robot Control for Improving Teleoperation Efficiency.” In GLOBECOM 2023 - 2023 IEEE Global Communications Conference. IEEE. https://doi.org/10.1109/globecom54140.2023.10437076
• Katukuri, Mahender. 2023. “Target-Interception Feasibility Assessment Methodology for Air-Launched Weapon Systems.” In 2023 3rd International Conference on Range Technology (ICORT). IEEE. https://doi.org/10.1109/icort56052.2023.10249134
• Katz, Joseph, and Daniel Levin. 1986. “Self-Induced Roll Oscillations Measured on a Delta Wing/canard Configuration.” Journal of Aircraft 23 (11): 814–19. https://doi.org/10.2514/3.45386
• Kawai, Yasunori, and Toru Namerikawa. 2012. “Improving Tracking Performance of Passivity Based PID-Type Teleoperation Systems with Communication Delay.” SICE Journal of Control, Measurement, and System Integration 5 (6): 335–41. https://doi.org/10.9746/jcmsi.5.335
• Kawatsu, Kaname. 2019. “PHM by Using Multi-Physics System-Level Modeling and Simulation for EMAs of Liquid Rocket Engine.” In 2019 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2019.8741827
• 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
• Kazanzides, Peter, Balazs P. Vagvolgyi, Will Pryor, Anton Deguet, Simon Leonard, and Louis L. Whitcomb. 2021. “Teleoperation and Visualization Interfaces for Remote Intervention in Space.” Frontiers in Robotics and AI 8. https://ntrs.nasa.gov/citations/20210018087
• Kbaier Ben Ismail, Dhouha, and Olivier Grivard. 2015. “A Model-Driven Approach to the a Priori Estimation of Operator Workload.” In 2015 IEEE International Multi-Disciplinary Conference on Cognitive Methods in Situation Awareness and Decision. IEEE. https://doi.org/10.1109/cogsima.2015.7107967
• Keen, Joseph M. 2006. “Applied Computational Fluid Dynamics in Support of Aircraft/Store Compatibility and Weapons Integration.” In 2006 HPCMP Users Group Conference (HPCMP-UGC’06). IEEE. https://doi.org/10.1109/hpcmp-ugc.2006.5
• Kelley, H. J., E. M. Cliff, and F. H. Lutze. 1982. “Boost–glide Range-Optimal Guidance.” Optimal Control Applications and Methods 3 (3): 293–98. https://doi.org/10.1002/oca.4660030307
• Kemp, J. W., and L. E. Corey. 2000. “Determining the Effect of Sidelobe Structure on Angle of Arrival Measurements Using Monopulse Techniques.” In Proceedings IEEE Southeastcon’99. Technology on the Brink of 2000 (Cat. No.99CH36300). IEEE. https://doi.org/10.1109/secon.1999.766148
• Khademian, Behzad, and Keyvan Hashtrudi-Zaad. 2012. “Dual-User Teleoperation Systems: New Multilateral Shared Control Architecture and Kinesthetic Performance Measures.” IEEE/ASME Transactions on Mechatronics 17 (5): 895–906. https://doi.org/10.1109/tmech.2011.2141673
• 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
• Khan, Taj Wali, and Ihtzaz Qamar. 2020. “Optimum Characteristic Length of Gas Generator for Liquid Propellant Rocket Engine.” Acta Astronautica 176: 1–12. https://doi.org/10.1016/j.actaastro.2020.06.021
• Kim, Won S., and Antal K. Bejczy. 1993. “Demonstration of a High-Fidelity Predictive/Preview Display Technique for Telerobotic Servicing in Space.” IEEE Transactions on Robotics and Automation 9 (5). https://ntrs.nasa.gov/citations/19970020676
• Kim, Byoung Soo, Anthony J. Calise, and Ramachandra J. Sattigeri. 2007. “Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight.” Journal of Guidance, Control, and Dynamics 30 (5): 1386–99. https://doi.org/10.2514/1.27758
• Kim, Y. S., H. S. Cho, and Z. Bien. 1985. “A New Guidance Law for Homing Missiles.” Journal of Guidance, Control, and Dynamics 8 (3): 402–4. https://doi.org/10.2514/3.19994
• Kim, Duk Hyun, Jae Hoon Choi, and Oh Joon Kwon. 2015a. “Detached Eddy Simulation of Weapons Bay Flows and Store Separation.” Computers & Fluids 121: 1–10. https://doi.org/10.1016/j.compfluid.2015.07.022
• Kim, M., and Kelly Grider. 1973. “Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories.” IEEE Transactions on Aerospace and Electronic Systems AES-9 (6): 852–59. https://doi.org/10.1109/taes.1973.309659
• Kim, Eugene, Myeonghwan Hwang, Taeyoon Lim, Chanyeong Jeong, Seungha Yoon, and Hyunrok Cha. 2024. “Communication Delay Outlier Detection and Compensation for Teleoperation Using Stochastic State Estimation.” Sensors 24 (4): 1241. https://doi.org/10.3390/s24041241
• Kim, Youngwoo, Minjae Jeong, Suhun Cho, Donghun Park, and Solkeun Jee. 2025. “Porous Surface Design with Stability Analysis for Turbulent Transition Control in Hypersonic Boundary Layer.” Aerospace 12 (6): 518. https://doi.org/10.3390/aerospace12060518
• Kim, Seunghyun, and H. Jin Kim. 2013. “Robust Proportional Navigation Guidance against Highly Maneuvering Targets.” In 2013 13th International Conference on Control, Automation and Systems (ICCAS 2013). IEEE. https://doi.org/10.1109/iccas.2013.6703864
• Kim, Mingu, and Youdan Kim. 2014. “Lyapunov-Based Pursuit Guidance Law with Impact Angle Constraint.” IFAC Proceedings Volumes 47 (3): 2509–14. https://doi.org/10.3182/20140824-6-za-1003.00233
• Kim, Jinrae, and Youdan Kim. 2019. “Impact Time Control Guidance with Finite-Time Convergence Based on Pure Proportional Navigation.” In 2019 18th European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2019.8795943
• Kim, Hyeong-Geun, and H. Jin Kim. 2020. “Field-of-View Constrained Guidance Law for a Maneuvering Target with Impact Angle Control.” IEEE Transactions on Aerospace and Electronic Systems 56 (6): 4974–83. https://doi.org/10.1109/taes.2020.2996306
• Kim, Jin Seong, and Man Young Kim. 2026. “Prediction of the Radiative Base Heating from the Solid Rocket Exhaust Plume.” Aerospace Science and Technology 178: 112974. https://doi.org/10.1016/j.ast.2026.112974
• Kim, Ga-Young, Byoung-Ik Kim, Tae-Wuk Bae, Young-Choon Kim, Sang-Ho Ahn, and Kyu-Ik Sohng. 2010a. “Implementation of a Reticle Seeker Missile Simulator for Jamming Effect Analysis.” In 2010 2nd International Conference on Image Processing Theory, Tools and Applications. IEEE. https://doi.org/10.1109/ipta.2010.5586729
• Kim, Dae Hyuk, Nakwan Kim, Hyeonjin Cho, and Su Yong Kim. 2014. “A Guidance Logic Development for Wake Homing Guidance System (ICCAS 2014).” In 2014 14th International Conference on Control, Automation and Systems (ICCAS 2014). IEEE. https://doi.org/10.1109/iccas.2014.6987984
• Kim, Seung-Hwan, Yoon-Sik Kim, and Chanho Song. 2004b. “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, Ki-Pyo, and Chang-Hun Lee. 2023. “Fixed Range Horizon MPPI-Based Missile Computational Guidance for Constrained Impact Angle.” International Journal of Control, Automation and Systems 21 (6): 1866–84. https://doi.org/10.1007/s12555-022-0660-0
• Kim, Hyungbin, and Seokwon Lee. 2026. “Integrated Guidance-Filter Design for Semi-Active Laser Homing Missiles under Lock-on and Lock-off Maneuvers.” Aerospace Science and Technology 170: 111535. https://doi.org/10.1016/j.ast.2025.111535
• Kim, Hyeong-Geun, Jun-Yong Lee, and H. Jin Kim. 2018. “Look Angle Constrained Impact Angle Control Guidance Law for Homing Missiles with Bearings-Only Measurements.” IEEE Transactions on Aerospace and Electronic Systems 54 (6): 3096–3107. https://doi.org/10.1109/taes.2018.2843600
• Kim, Hyeong-Geun, Jun-Yong Lee, Hyoun Jin Kim, Hyuck-Hoon Kwon, and Jang-Seong Park. 2020. “Look-Angle-Shaping Guidance Law for Impact Angle and Time Control with Field-of-View Constraint.” IEEE Transactions on Aerospace and Electronic Systems 56 (2): 1602–12. https://doi.org/10.1109/taes.2019.2924175
• Kim, Jong-ju, and Joon Lyou. 2006. “Absolute Stability Margin in Missile Guidance Loop.” In 2006 SICE-ICASE International Joint Conference. IEEE. https://doi.org/10.1109/sice.2006.315407
• 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, Tae-Hun, and Bong-Gyun Park. 2022a. “Rapid Homing Guidance Using Jerk Command and Time-Delay Estimation Method.” IEEE Transactions on Aerospace and Electronic Systems 58 (1): 729–42. https://doi.org/10.1109/taes.2021.3101584
• Kim, Tae-Hun, and Bong-Gyun Park. 2022b. “Three-Dimensional Look Angle Rate Constrained Guidance for Strapdown Imaging Seeker Equipped Missiles.” International Journal of Control, Automation and Systems 20 (1): 160–74. https://doi.org/10.1007/s12555-021-0008-6
• Kim, Tae-Hun, Bong-Gyun Park, and Min-Jea Tahk. 2013a. “Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint.” Journal of Guidance, Control, and Dynamics 36 (6): 1810–16. https://doi.org/10.2514/1.59252
• Kim, Du Yong, Luke Rosenberg, Branko Ristic, and Robin Guan. 2022. “Maritime Target Tracking from an Airborne Multi-Channel Radar.” In 2022 IEEE Radar Conference (RadarConf22). IEEE. https://doi.org/10.1109/radarconf2248738.2022.9764322
• Kim, Hyeong-Geun, and Jongho Shin. 2022. “Integrated Autopilot Guidance Based on Zero-Effort-Miss Formulation for Tail-Controlled Missiles.” Applied Sciences 12 (14): 7120. https://doi.org/10.3390/app12147120
• 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. 2016b. “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
• Kintz, Andrew L. 2019. “Non-Coherent Angle and Angle-Rate Estimator for a Slewing Monopulse Antenna.” In 2019 IEEE International Symposium on Phased Array System & Technology (PAST). IEEE. https://doi.org/10.1109/past43306.2019.9021006
• Kirchhartz, Rainer M., David J. Mee, and Raymond J. Stalker. 2012. “Supersonic Skin-Friction Drag with Tangential Wall Slot Fuel Injection and Combustion.” AIAA Journal 50 (2): 313–24. https://doi.org/10.2514/1.j051073
• Kivila, Arto, James Potter, and William Singhose. 2015. “Manual Tracking Using Touchscreen Interfaces.” In 2015 10th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc.2015.7244606
• Kleider, J. E., S. Gifford, K. Nolan, D. Hughes, and S. Chuprun. 2005. “Demonstrating Robust High Data Rate Capability on a Software Defined Radio Using Anti-Jam Wideband OFDM Waveforms.” In MILCOM 2005 - 2005 IEEE Military Communications Conference. IEEE. https://doi.org/10.1109/milcom.2005.1605911
• Klein, Itzik, and Ilan Rusnak. 2017. “Loop-Shaping Approach to Mitigate Radome Effects in Homing Missiles.” Journal of Guidance, Control, and Dynamics 40 (7): 1789–95. https://doi.org/10.2514/1.g000850
• Kleyner, Andre, and David Elmore. 2023. “Reliability Demonstration Based on the Results of a Super Extended Life Test.” In 2023 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams51473.2023.10088206
• Kleyner, Andre, David Elmore, and Benzion Boukai. 2015. “A Bayesian Approach to Determine Test Sample Size Requirements for Reliability Demonstration Retesting after Product Design Change.” Quality Engineering 27 (3): 289–95. https://doi.org/10.1080/08982112.2014.990035
• 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
• Klinefelter, Eric, Jason Merlo, Hayder Radha, and Jeffrey A. Nanzer. 2022. “A Point Target Model for Interferometric Radar Angular Velocity Estimation.” IEEE Transactions on Microwave Theory and Techniques 70 (3): 1562–70. https://doi.org/10.1109/tmtt.2021.3136265
• Kloss, Tobias, and Axel Schulte. 2013. “Design of a Guided Missile Operator Assistant System for High-Tempo Intervention Support.” In Engineering Psychology and Cognitive Ergonomics. Applications and Services. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-39354-9_30
• Kohli, S., L. Tellman, and K. Bolin. 1994. “High Performance GPS Receiver for Air Launched Munitions.” In Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS’94. IEEE. https://doi.org/10.1109/plans.1994.303309
• Komar, James J. 1966. “Skin-Friction Predictions in Turbulent Compressible Flow.” AIAA Journal 4 (7): 1307–8. https://doi.org/10.2514/3.3668
• Kong, Lingfeng, Zhizhao Xu, Youping Jiang, and Rongying Shao. 2024. “Design and Performance Optimization of Missile-Borne Synthetic Aperture Radar Target Echo Simulation System.” In 2024 IEEE International Conference on Signal, Information and Data Processing (ICSIDP). IEEE. https://doi.org/10.1109/icsidp62679.2024.10868575
• Kong, Xinwan, and Cheng Zhang. 2024. “Parameter Optimization Method for Predictor–Corrector Guidance with Impact Angle Constraint.” International Journal of Aerospace Engineering 2024 (1): 4540925. https://doi.org/10.1155/ijae/4540925
• Kong, Xinwan, Cheng Zhang, and Fenfen Xiong. 2025. “Impact Speed and Angle Constrained Guidance Law for Unpowered Gliding Vehicle.” Chinese Journal of Aeronautics 38 (4): 103196. https://doi.org/10.1016/j.cja.2024.08.027
• Koochaki, Fatemeh, and Heidar A. Talebi. 2016. “Position Coordination of Nonlinear Teleoperation for Unrestricted Non-Passive Environment and Operator in the Presence of Time Delay.” In 2016 4th International Conference on Control, Instrumentation, and Automation (ICCIA). IEEE. https://doi.org/10.1109/icciautom.2016.7483197
• Koruba, Zbigniew, and Lukasz Nocon. 2014. “Programmed Control of the Flat Track Anti-Tank Guided Missile.” In Proceedings of the 2014 15th International Carpathian Control Conference (ICCC). IEEE. https://doi.org/10.1109/carpathiancc.2014.6843604
• Kose, Yigithan Mehmet, and Murat Celik. 2023. “Regenerative Cooling Comparison of LOX/LCH4 and LOX/LC3H8 Rocket Engines Using the One-Dimensional Regenerative Cooling Modelling Tool ODREC.” Applied Sciences 14 (1): 71. https://doi.org/10.3390/app14010071
• Kostis, Theodoros G., Konstantinos G. Galanis, and Socrates K. Katsikas. 2008. “Simulator Implementation of an IF-ISAR System for Studies in Target Glint.” In 2008 Panhellenic Conference on Informatics. IEEE. https://doi.org/10.1109/pci.2008.41
• 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
• 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
• Kraiko, A. N., and N. I. Tilliaeva. 1973. “On Constructing the Contour of Minimum Wave Drag in an Inhomogeneous Supersonic Flow.” Journal of Applied Mathematics and Mechanics 37 (3): 449–67. https://doi.org/10.1016/0021-8928(73)90088-9
• Krasich, Milena. 2010. “Accelerated Reliability Demonstration and Assurance Test Design.” In 2010 Proceedings - Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams.2010.5448027
• Krause, James M., Gary L. Hartmann, and George D. Ianculescu. 1991. “Thermal Control for Hypersonic Vehicle Propulsion.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791945
• 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
• Krieger, Robert J. 1984. “Supersonic Missile Aerodynamic and Performance Relationships for Long-Range Mission Profiles.” Journal of Spacecraft and Rockets 21 (3): 234–40. https://doi.org/10.2514/3.25643
• Krieger, Robert J., and John E. Williams. 1983. “Accuracy Criteria for Evaluating Supersonic Missile Aerodynamic Coefficient Predictions.” Journal of Spacecraft and Rockets 20 (4): 323–30. https://doi.org/10.2514/3.25601
• Krolo, A., and B. Bertsche. 2003. “An Approach for the Advanced Planning of a Reliability Demonstration Test Based on a Bayes Procedure.” In Annual Reliability and Maintainability Symposium, 2003.. IEEE. https://doi.org/10.1109/rams.2003.1181940
• Krüger, J. J., and I. S. Shaw. 1991. “The Application of a New Fuzzy Model Identification Technique to a Human Tracking Control Operator.” IFAC Proceedings Volumes 24 (3): 947–52. https://doi.org/10.1016/s1474-6670(17)52471-4
• 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
• Kumar, Shashi Ranjan, and Debasish Ghose. 2014. “Three Dimensional Impact Angle Constrained Guidance Law Using Sliding Mode Control.” In 2014 American Control Conference. IEEE. https://doi.org/10.1109/acc.2014.6858936
• Kumar, Manav, and Sharifuddin Mondal. 2023. “State Estimation of Radar Tracking System Using a Robust Adaptive Unscented Kalman Filter.” Aerospace Systems 6 (2): 375–81. https://doi.org/10.1007/s42401-023-00216-7
• Kumar, Shashi Ranjan, and Dwaipayan Mukherjee. 2022. “True-Proportional-Navigation Inspired Finite-Time Homing Guidance for Time Constrained Interception.” Aerospace Science and Technology 123: 107499. https://doi.org/10.1016/j.ast.2022.107499
• Kumar, Amit, and Aparajita Ojha. 2013. “Performance Evaluation of Certain Proportional Navigation Guidance Schemes.” In 2013 International Conference on Control, Automation, Robotics and Embedded Systems (CARE). IEEE. https://doi.org/10.1109/care.2013.6733766
• Kumar, Shashi Ranjan, Sachit Rao, and Debasish Ghose. 2014. “Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints.” Journal of Guidance, Control, and Dynamics 37 (4): 1114–30. https://doi.org/10.2514/1.62737
• Kumar, Renjith R., Hans Seywald, and Eugene M. Cliff. 1995a. “Near-Optimal Three-Dimensional Air-to-Air Missile Guidance against Maneuvering Target.” Journal of Guidance, Control, and Dynamics 18 (3): 457–64. https://doi.org/10.2514/3.21409
• Kumar, Renjith R., Hans Seywald, Eugene M. Cliff, and Henry J. Kelley. 1995b. “Three-Dimensional Air-to-Air Missile Trajectory Shaping.” Journal of Guidance, Control, and Dynamics 18 (3): 449–56. https://doi.org/10.2514/3.21408
• Kumar, Ramesh, Jaspreet Singh, Pankaj Yadav, et al. 2023b. “Parachute Deployment System for Safe Recovery of a Drone.” Materials Today: Proceedings. https://doi.org/10.1016/j.matpr.2023.04.114
• Kuo, C.-Y., D. Soetanto, and Ying-Chwan Chiou. 2001. “Geometric Analysis of Flight Control Command for Tactical Missile Guidance.” IEEE Transactions on Control Systems Technology 9 (2): 234–43. https://doi.org/10.1109/87.911375
• 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
• Kurochkin, I. V., and A. A. Mal’tsev. 1982. “A Stochastic Model for the Human Operator in a Manual Control System for a Dynamic Object.” Radiophysics and Quantum Electronics 25 (1): 44–51. https://doi.org/10.1007/bf01035025
• Kuroswiski, Andre R., Annie S. Wu, and Angelo Passaro. 2025. “Optimized Prediction of Weapon Effectiveness in BVR Air Combat Scenarios Using Enhanced Regression Models.” IEEE Access 13: 21759–72. https://doi.org/10.1109/access.2025.3535555
• Lai, Chao, Weihong Wang, Zhenghua Liu, Tingting Liang, and Shenao Yan. 2018. “Three-Dimensional Impact Angle Constrained Partial Integrated Guidance and Control with Finite-Time Convergence.” IEEE Access 6: 53833–53. https://doi.org/10.1109/access.2018.2871051
• Lainiotis, D. G., I. A. Marinitsis, and S. K. Katsikas. n.d. “Adaptive Nonlinear Algorithms for Radar Tracking with Roll Angle Measurements of Maneuvering Targets.” In Proceedings of MELECON ‘94. Mediterranean Electrotechnical Conference. IEEE. https://doi.org/10.1109/melcon.1994.381135
• Lam, Vincent C. 2007. “Acceleration-Compensated Zero-Effort-Miss Guidance Law.” Journal of Guidance, Control, and Dynamics 30 (4): 1159–63. https://doi.org/10.2514/1.26948
• LanFeng, Zhou, Zhang Min, and Zhao YiNan. 2010. “Angle Estimation for Two Unresolved Swerling I Targets in Monopulse Radar.” In 2010 International Conference on Microwave and Millimeter Wave Technology. IEEE. https://doi.org/10.1109/icmmt.2010.5524829
• Lang, Robert, and Andre Vacroux. 1969. “Operator-Centered Adaptive Compensation of Continuous Manual Control Systems.” IEEE Transactions on Man Machine Systems 10 (2): 53–59. https://doi.org/10.1109/tmms.1969.299897
• 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
• LaPlant, O. 1952. “Tracking Noise Measurements on a Manual Tracking Radar.” Transactions of the IRE Professional Group on Antennas and Propagation PGAP-4: 135–135. https://doi.org/10.1109/tpgap.1952.237411
• Larochelle, Benoit, and Geert-Jan M. Kruijff. 2012. “Multi-View Operator Control Unit to Improve Situation Awareness in USAR Missions.” In 2012 IEEE RO-MAN: The 21st IEEE International Symposium on Robot and Human Interactive Communication. IEEE. https://doi.org/10.1109/roman.2012.6343896
• Larochelle, Benoit, Geert-Jan M. Kruijff, Nanja Smets, Tina Mioch, and Peter Groenewegen. 2011. “Establishing Human Situation Awareness Using a Multi-Modal Operator Control Unit in an Urban Search & Rescue Human-Robot Team.” In 2011 RO-MAN. IEEE. https://doi.org/10.1109/roman.2011.6005237
• Lassami, Bilal, Stephane Font, and Houria Siguerdidjane. 2006. “Nonsmooth Optimization for Nonlinear Missile Autopilot: Improvement under Time Domain Constraints.” In 2006 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2006.285992
• Lauchle, Gerald C. 1974. “Dynamic Hinge Moment of a Low Aspect Ratio Control Surface.” Journal of Hydronautics 8 (3): 119–20. https://doi.org/10.2514/3.62987
• Lawrence, Lovell. 1945. “A Liquid Propellant Rocket Motor.” Journal of the American Rocket Society 00 (64): 8–10. https://doi.org/10.2514/8.4056
• Lawrence, Richard V. 1998. “Interceptor Line-of-Sight Rate Steering: Necessary Conditions for a Direct Hit.” Journal of Guidance, Control, and Dynamics 21 (3): 471–76. https://doi.org/10.2514/2.4260
• Lawson, S. J., and G. N. Barakos. 2010. “Computational Fluid Dynamics Analyses of Flow over Weapons-Bay Geometries.” Journal of Aircraft 47 (5): 1605–23. https://doi.org/10.2514/1.c000218
• 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
• Lee, B. H. K. 2010. “Effect of Captive Stores on Internal Weapons Bay Floor Pressure Distributions.” Journal of Aircraft 47 (2): 732–36. https://doi.org/10.2514/1.46684
• Lee, Suwon. 2023. “Quaternion-Based 3D Attitude Tracking Algorithm Using Virtual Roll Angle for Missile Systems.” International Journal of Control, Automation and Systems 21 (10): 3391–3404. https://doi.org/10.1007/s12555-022-0587-5
• Lee, Seokwon, and Namhoon Cho. 2021. “Inverse Optimality of Pure Proportional Navigation Guidance for Stationary Targets.” Journal of Guidance, Control, and Dynamics 44 (11): 2081–90. https://doi.org/10.2514/1.g006018
• Lee, Seung-phil, Byung-lae Cho, Sang-min Lee, Ji-eun Kim, and Young-soo Kim. 2015b. “Unambiguous Angle Estimation of Unresolved Targets in Monopulse Radar.” IEEE Transactions on Aerospace and Electronic Systems 51 (2): 1170–77. https://doi.org/10.1109/taes.2014.140178
• 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, Daniel, and Han-Lim Choi. 2019. “Three-Dimensional Impact Angle Guidance Laws for Precision Guided Munition.” In 2019 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2019.8741995
• Lee, Ho Chul, Yong Seok Choi, and Jae Weon Choi. 2004a. “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, Bum Seok, Jae Hoon Choi, and Oh Joon Kwon. 2011. “Numerical Simulation of Free-Flight Rockets Air-Launched from a Helicopter.” Journal of Aircraft 48 (5): 1766–75. https://doi.org/10.2514/1.c031365
• Lee, Hunjo, Jiwoong Han, and Gi-Hun Yang. 2024b. “Development of Variable Scaling Teleoperation Framework for Improving Teleoperation Performance.” International Journal of Control, Automation and Systems 22 (3): 936–45. https://doi.org/10.1007/s12555-022-1099-z
• Lee, Youngjun, and Youdan Kim. 2023. “Minimizing Look Angle Rate Guidance Law Considering Impact Angle and Field-of-View Limit.” IFAC-PapersOnLine 56 (2): 9393–98. https://doi.org/10.1016/j.ifacol.2023.10.230
• Lee, Youngjun, Jinrae Kim, and Youdan Kim. 2025. “Missile Autopilot Design via Neural Koopman Embedding.” Journal of Aerospace Information Systems 22 (10): 804–15. https://doi.org/10.2514/1.i011660
• Lee, Seokwon, Youdan Kim, Yongwoo Lee, Gwanyoung Moon, and Byung-Eul Jeon. 2020. “Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty.” IEEE Transactions on Aerospace and Electronic Systems 56 (6): 4269–87. https://doi.org/10.1109/taes.2020.2990819
• Lee, Chang-Hun, Tae-Hun Kim, and Min-Jea Tahk. 2013b. “Interception Angle Control Guidance Using Proportional Navigation with Error Feedback.” Journal of Guidance, Control, and Dynamics 36 (5): 1556–61. https://doi.org/10.2514/1.58454
• Lee, Suwon, Seokwon Lee, and Youdan Kim. 2019a. “Active Sampling-Based Data-Driven Reachability Verification for Proportional Navigation Guidance Law.” IFAC-PapersOnLine 52 (12): 1–6. https://doi.org/10.1016/j.ifacol.2019.11.060
• Lee, Shing Chung, and Kim Boon Lua. 2026. “Aeroacoustic Optimizations of Internal Bay Cavity Flow Control Devices.” Journal of Aircraft: 1–11. https://doi.org/10.2514/1.c038959
• Lee, John, and Neville Moray. 1992. “Trust, Control Strategies and Allocation of Function in Human-Machine Systems.” Ergonomics 35 (10): 1243–70. https://doi.org/10.1080/00140139208967392
• Lee, BoYa, Qiuqiu Wen, and Guanqun Zhou. 2018b. “The Impact Angle Guidance Law Parameter Design Strategy Consider Final Speed Constraint.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018701
• Lee, T.-S., and M. D. Zoltowski. n.d. “Beamspace Domain ML Based Low Angle Radar Tracking with an Array of Antennas.” In Digest on Antennas and Propagation Society International Symposium. IEEE. https://doi.org/10.1109/aps.1989.134775
• Lei, Wengui, Wanchun Chen, Liang Yang, and Xiaopeng Gong. 2025b. “Singular Optimal Control of Ascent Stage for a Surface-to-Air Missile.” Chinese Journal of Aeronautics 38 (8): 103333. https://doi.org/10.1016/j.cja.2024.103333
• Lei, Yang, and Ye Zheng-yin. 2016. “The Interference Aerodynamics Caused by the Wing Elasticity during Store Separation.” Acta Astronautica 121: 116–29. https://doi.org/10.1016/j.actaastro.2015.12.039
• Leondes, Cornelius T., and John L. Pearson. 1968. “Missile Autopilot Adaption Using Control- Surface Hinge-Moment Feedback.” Journal of Spacecraft and Rockets 5 (2): 154–59. https://doi.org/10.2514/3.29207
• 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
• Leopold, Tobias. 2022. “Increasing the Robustness of Reliability Demonstration Test Planning.” In 2022 6th International Conference on System Reliability and Safety (ICSRS). IEEE. https://doi.org/10.1109/icsrs56243.2022.10067460
• 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, Winston, and Daniel DeLaurentis. 2024. “Neighboring Optimal Maximum Range Glide Phugoid-Damping Guidance Law.” In 2024 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero58975.2024.10521344
• Levin, Winston C., and Daniel A. DeLaurentis. 2025. “Neighboring Optimal Guidance Law for Maximum Range Glide.” Journal of Guidance, Control, and Dynamics 48 (3): 638–45. https://doi.org/10.2514/1.g008757
• Levine, R. S. 1965. “Experimental Status of High Frequency Liquid Rocket Combustion Instability.” Symposium (International) on Combustion 10 (1): 1083–99. https://doi.org/10.1016/s0082-0784(65)80248-x
• Levine, Jay N., and Joseph D. Baum. 1982. “Modeling of Nonlinear Combustion Instability in Solid Propellant Rocket Motors.” Symposium (International) on Combustion 19 (1): 769–76. https://doi.org/10.1016/s0082-0784(82)80252-x
• Levitas, Boris, Michail Drozdov, Irina Naidionova, Sergej Jefremov, and Jonas Matuzas. 2016. “MIMO UWB Radar for Moving Target Tracking.” In 2016 17th International Radar Symposium (IRS). IEEE. https://doi.org/10.1109/irs.2016.7497393
• Levitt, I. M. 1953. “Development of the Guided Missile.” Journal of the Franklin Institute 255 (3): 253–54. https://doi.org/10.1016/0016-0032(53)90021-0
• Lewitschnig, Horst, and Armin Fanzott. 2019. “Fractional Failures Sampling—an Alternative to Zero Failures Sampling Plans.” IEEE Transactions on Reliability 68 (2): 609–19. https://doi.org/10.1109/tr.2018.2884874
• 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, Xiangxiang, Wanchun Chen, Zhongyuan Chen, and Heng Shi. 2023a. “A Guidance Law with Both Impact Time and Impact Angle Constraints Based on Circular Guidance.” In 2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae59650.2023.10424448
• Li, Jinping, Hong Chen, Shizhong Zhang, Xiaoyuan Zhang, and Hongru Yu. 2017b. “On the Response of Coaxial Surface Thermocouples for Transient Aerodynamic Heating Measurements.” Experimental Thermal and Fluid Science 86: 141–48. https://doi.org/10.1016/j.expthermflusci.2017.04.011
• Li, Keyi, Xi Chen, and Gongjian Zhou. 2016a. “Maneuvering Target Tracking in Constraint Coordinates with Radar Measurements.” In 2016 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2016.7485319
• Li, Hang, Wusheng Chou, and Lingda Meng. 2025d. “Finite-Time Adaptive Fuzzy Prescribed Performance Control for Teleoperation with Asymmetric Time Delays and Uncertainties.” International Journal of Robust and Nonlinear Control 35 (8): 2982–95. https://doi.org/10.1002/rnc.7818
• 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, Songzhou, Zhou Di, and Yutang Li. 2025g. “Pursuing Probability Calculation Based on the Rule of Nullifying the Line-of-Sight Rate.” Journal of Guidance, Control, and Dynamics 48 (10): 2348–57. https://doi.org/10.2514/1.g008719
• Li, Yixuan, Wanshuang Ding, Jiating Su, Wenbin Yu, and Wanchun Chen. 2026b. “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, Zhibing, Quanlin Dong, Xiaoyue Zhang, and Yuanfei Gao. 2022b. “Impact Angle-Constrained Integrated Guidance and Control for Supersonic Skid-to-Turn Missiles Using Backstepping with Global Fast Terminal Sliding Mode Control.” Aerospace Science and Technology 122: 107386. https://doi.org/10.1016/j.ast.2022.107386
• Li, Zhengda, Lionel Ganippa, and Thanos Megaritis. 2026e. “Review of Liquid Rocket Engine Injector Design and Technology.” Aerospace 13 (4): 344. https://doi.org/10.3390/aerospace13040344
• Li, Shutong, Yanbin Gao, and Meng Liu. 2019f. “Multistage Attitude Determination Alignment for Velocity-Aided in-Motion Strapdown Inertial Navigation System with Different Velocity Models.” Sensors 19 (3): 665. https://doi.org/10.3390/s19030665
• 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, Zhaolong, Xuqing Geng, Wenjie Ai, and Minghu Tan. 2025b. “Cooperative Guidance Law with Angle Constraint Based on Reinforcement Learning.” In 2025 Asian Conference on Artificial Intelligence Technology (ACAIT). IEEE. https://doi.org/10.1109/acait67930.2025.11522112
• Li, Hui, and Yingqing Guo. 2022. “Modeling, Simulation and Characteristic Analysis of a Liquid-Propellant Rocket Engine Control Valve.” In 2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae56000.2022.9852836
• Li, Junjie, Dewei Han, Jian Xu, Kang Li, and Zhaoyuan Ma. 2026c. “Design and Evaluation of Avatar: An Ultra-Low-Latency Immersive Human–machine Interface for Teleoperation.” Displays 92: 103292. https://doi.org/10.1016/j.displa.2025.103292
• Li, Yaowen, You He, Gang Li, and Yu Liu. 2019e. “Modified Smooth Variable Structure Filter for Radar Target Tracking.” In 2019 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar41533.2019.171325
• Li, Hongyan, Shaoming He, Jiang Wang, Hyo-Sang Shin, and Antonios Tsourdos. 2021b. “Near-Optimal Midcourse Guidance for Velocity Maximization with Constrained Arrival Angle.” Journal of Guidance, Control, and Dynamics 44 (1): 172–80. https://doi.org/10.2514/1.g005250
• Li, Ao, Xiaoxiang Hu, Shaohua Yang, and Kejun Dong. 2024b. “Adaptive Terminal Time and Impact Angle Constraint Cooperative Guidance Strategy for Multiple Vehicles.” Drones 8 (4): 134. https://doi.org/10.3390/drones8040134
• Li, Hongwei, Xuejun Ji, and Guoqing Zhao. 2013b. “TOA-Based Target Tracking Using Improved Particle Filter in Passive Bistatic Radar with Glint Noise.” In 2013 6th International Congress on Image and Signal Processing (CISP). IEEE. https://doi.org/10.1109/cisp.2013.6743851
• Li, Wenling, Yingmin Jia, Junping Du, and Jun Zhang. 2014c. “PHD Filter for Multi-Target Tracking with Glint Noise.” Signal Processing 94: 48–56. https://doi.org/10.1016/j.sigpro.2013.06.012
• Li, Xinyan, Sange Li, and Zhaoxing Gao. 2025a. “Assessment of Anti-Jamming Capabilities in Infrared-Guided Missile Systems.” Physica D: Nonlinear Phenomena 481: 134737. https://doi.org/10.1016/j.physd.2025.134737
• Li, Yaowen, Gang Li, Yu Liu, Xiao-Ping Zhang, and You He. 2021d. “A Robust Nonlinear Filter for Doppler Radar Target Tracking.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028376
• Li, Bocun, Ling Li, Huaming Zhang, and Yichuan Zhu. 2024e. “Three-Dimensional Cooperative Guidance against Aerial Target for Unpowered Glide Vehicle.” In 2024 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac63892.2024.10864770
• Li, Jixin, Xiaogeng Liang, and Keqiang Xia. 2022a. “Anti-Jamming Trajectory Planning of Infrared Imaging Air-to-Air Missile.” In 2022 IEEE 6th Information Technology and Mechatronics Engineering Conference (ITOEC). IEEE. https://doi.org/10.1109/itoec53115.2022.9734422
• Li, Junhui, Shiyao Lin, Baokui Geng, Kuanrong Hu, and Wei Wang. 2024c. “Command Filter Based Integrated Guidance and Control Design with Impact Angle Constraint.” In 2024 43rd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc63176.2024.10662176
• Li, Jiahe, Yanming Liu, and Jiang Wang. 2019d. “Evaluation Method of Riblets Effects and Application on a Missile Surface.” Aerospace Science and Technology 95: 105418. https://doi.org/10.1016/j.ast.2019.105418
• Li, Yuling, Zheng Liu, Zilong Wang, Yixin Yin, and Baoyong Zhao. 2020a. “Adaptive Control of Teleoperation Systems with Prescribed Tracking Performance: A BLF-Based Approach.” International Journal of Control 95 (6): 1600–1610. https://doi.org/10.1080/00207179.2020.1866212
• Li, Ni, Zhenhua Lv, Shaodan Wang, Guanghong Gong, and Lei Ren. 2015f. “A Real-Time Infrared Radiation Imaging Simulation Method of Aircraft Skin with Aerodynamic Heating Effect.” Infrared Physics & Technology 71: 533–41. https://doi.org/10.1016/j.infrared.2015.06.014
• Li, Panhu, Xinhua Mao, and Lan Ding. 2016c. “Wavefront Curvature Correction for Missile Borne Spotlight SAR Polar Format Image.” In 2016 CIE International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2016.8059214
• Li, Xuyou, Qingwen Meng, Meng Liu, and Yanda Guo. 2021a. “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, Tong, and Huaming Qian. 2019. “Design of Three-Dimensional Adaptive Sliding Mode Guidance Law with Impact Angle Constraint.” In 2019 IEEE 3rd Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC). IEEE. https://doi.org/10.1109/imcec46724.2019.8983888
• Li, Chuanjiang, Yanchao Sun, Teng Lv, Guangfu Ma, and Junzi Xiao. 2014a. “A Fuzzy Guidance Law Design with Terminal-Angle Constraint.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896720
• Li, Hongyan, Hong Tao, Jiang Wang, and Shaoming He. 2023e. “Three-Dimensional Optimal Homing Guidance without Terminal Maneuverability Advantage.” Journal of Guidance, Control, and Dynamics 46 (9): 1774–84. https://doi.org/10.2514/1.g007483
• Li, Yunbo, Chao Wang, Shu-Yue Dong, Jia-Lin Shen, and Hai-Peng Wang. 2020b. “Fast Estimated Calculation of Wideband Radar Angular Glint Using Single Frequency Method.” IEEE Access 8: 212541–47. https://doi.org/10.1109/access.2020.3040436
• Li, Hongyan, Jiang Wang, Shaoming He, and Chang-Hun Lee. 2021c. “Nonlinear Optimal Impact-Angle-Constrained Guidance with Large Initial Heading Error.” Journal of Guidance, Control, and Dynamics 44 (9): 1663–76. https://doi.org/10.2514/1.g005868
• Li, Chendi, Jiang Wang, and Peng Huang. 2022d. “Optimal Cooperative Line-of-Sight Guidance for Defending a Guided Missile.” Aerospace 9 (5): 232. https://doi.org/10.3390/aerospace9050232
• Li, Jiaxin, Donghui Wang, and Weihua Zhang. 2022e. “Surrogate-Based Optimization Design for Air-Launched Vehicle Using Iterative Terminal Guidance.” Aerospace 9 (6): 300. https://doi.org/10.3390/aerospace9060300
• Li, Shancheng, Yong Wang, and Haibo Zhang. 2026a. “Adaptive Fuzzy Fault Estimation and Fault-Tolerant Control Method Considering Sensor and Actuator Faults for Aeroengines.” Aerospace Science and Technology 168: 110887. https://doi.org/10.1016/j.ast.2025.110887
• Li, Zhiyu, Guohua Wei, and Siliang Wu. 2006. “Fast Measurement of Vector Miss Distance Based on FFT.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343351
• Li, Leyao, Yiqing Xie, Yufeng Wang, and Jianpeng Li. 2025e. “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, Shikang, Xianzhe Xu, Rentuo Tao, Yawei Chen, and Linghao Xia. 2024d. “Orbital Angular Momentum Based Monopulse Angle Estimation against Cross-Eye Jamming.” In 2024 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar58436.2024.10993742
• Li, Zhengnan, Tao Yang, and Zhiwei Feng. 2016b. “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, Guanlin, Qiangwei Yang, and Xudong Huang. 2023f. “Virtual Target Based Terminal Guidance Law for Cruise Projectile Considering Impact Angle Constraint.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10240335
• Li, Peiqing, Zhichun Yang, and Wei Tian. 2023d. “Nonlinear Aeroelastic Analysis and Active Flutter Control of Functionally Graded Piezoelectric Material Plate.” Thin-Walled Structures 183: 110323. https://doi.org/10.1016/j.tws.2022.110323
• Li, Yechen, Jie Yao, Qing Shen, and Wei Cui. 2019c. “Dual-Channel Monopulse Angle Estimation Method for Weak Target Based on Reference Signal.” In 2019 IEEE International Conference on Signal, Information and Data Processing (ICSIDP). IEEE. https://doi.org/10.1109/icsidp47821.2019.9173299
• Li, Zeren, Hanghang Ye, Hao Cui, Zhengyu Guo, and Yunze Cai. 2019h. “Sliding Mode Control-Based Guidance Law with Damping Term and Angle Constraint.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865893
• Li, Guchong, Wei Yi, Meng Jiang, and Lingjiang Kong. 2017a. “Distributed Fusion with PHD Filter for Multi-Target Tracking in Asynchronous Radar System.” In 2017 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2017.7944432
• Li, Qiang, Xiaming Yuan, and Jihong Zhu. 2025f. “Influence of Aerodynamic Modeling Errors on the Dynamic Characteristics of a Missile.” Aerospace 12 (7): 619. https://doi.org/10.3390/aerospace12070619
• Li, Shunli, Qiuyi Zhang, Jinlun Li, Hongxin Zhao, Xiaoxing Yin, and Mei Yang. 2020c. “Monopulse Antenna Based on Singular Spoof Surface Plasmon Polariton Structure for Angle Measurement.” Electronics 9 (12): 2156. https://doi.org/10.3390/electronics9122156
• Li, Guanghua, Hongbo Zhang, Guojian Tang, and Yu Xie. 2014b. “Maneuver Modes Analysis for Hypersonic Glide Vehicles.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007281
• Li, Shikang, Meng Zhang, Xianzhe Xu, Rentuo Tao, and Yawei Chen. 2023c. “Monopulse Angle Measurement with Orbital Angular Momentum Charge Distribution.” In 2023 20th European Radar Conference (EuRAD). IEEE. https://doi.org/10.23919/eurad58043.2023.10289373
• Li, Yuan-Sheng, Xin Zhao, Si-Hong She, Meng-Chen Ma, and Shen-min Song. 2019g. “SDRE Optimal Sliding Mode Guidance Law Design with Attack Angle Constraint.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865531
• Li, Mingjie, Chijun Zhou, Lei Shao, Humin Lei, and Changxin Luo. 2022c. “An Improved Predictor-Corrector Guidance Algorithm for Reentry Glide Vehicle Based on Intelligent Flight Range Prediction and Adaptive Crossrange Corridor.” International Journal of Aerospace Engineering 2022: 1–18. https://doi.org/10.1155/2022/7313586
• Li Baoguo, Zhao Hongzhong, and Fu Qiang. 2005. “Research on High Accuracy Angle Measuring Technology of MMW Monopulse Radar.” In IEEE International Radar Conference, 2005.. IEEE. https://doi.org/10.1109/radar.2005.1435926
• Li Nan and Qu Changwen. 2007. “Research on Jamming Synthetic Aperture Radar Technologies.” In 2007 1st Asian and Pacific Conference on Synthetic Aperture Radar. IEEE. https://doi.org/10.1109/apsar.2007.4418674
• Li-hua, Liu, Wang Zhuang, and Hu Wei-dong. 2006. “Precession Period Extraction of Ballistic Missile Based on Radar Measurement.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343186
• Liang, Xiao-Ling, Ming-Zhe Hou, and Guang-Ren Duan. 2014. “Adaptive Filtered Backstepping Control for Integrated Missile Guidance and Autopilot.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6897003
• Liang, Xiaoling, Ning Wang, Yancheng Liu, Shuailin Lv, and Bin Xu. 2016. “Command Filtered Adaptive Control for Integrated Missile Guidance and Autopilot with Terminal Angular Constraint.” In 2016 12th World Congress on Intelligent Control and Automation (WCICA). IEEE. https://doi.org/10.1109/wcica.2016.7578525
• Liang, Xuanye, Lijun Yang, Gaofeng Wang, and Jingxuan Li. 2022. “Hopf Bifurcation Analysis of the Combustion Instability in a Liquid Rocket Engine.” Aerospace 9 (10): 593. https://doi.org/10.3390/aerospace9100593
• Liang Hongwei and Ma Baoli. 2008. “A Nonlinear Adaptive Guidance Law for Missile Interceptions.” In 2008 27th Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2008.4605316
• 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
• “Life Prediction of the Thrust Chamber Wall of a Reusable Rocket Engine.” 1995. Journal of Propulsion and Power 11 (6): 1279–87. https://doi.org/10.2514/3.23969
• Lilian Bruyeere, Antonios Tsourdos, and Brian A. White. 2005. “Polynomial Eigenstructure Assignment, Application to Missile Autopilot.” In Proceedings of 2005 IEEE Conference on Control Applications, 2005. CCA 2005.. IEEE. https://doi.org/10.1109/cca.2005.1507320
• Lillard, L. N., H. E. Evans, and J. J. Spaulding. 1997. “Minimum Variance Missile Launch and Impact Estimation by Fusing Observations from Multiple Sensors.” In 1997 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.1997.574879
• Lilov, L. 1962. “The Soviet Missile Programme: ANTI-MISSILE MISSILES.” Survival 4 (2): 86–91. https://doi.org/10.1080/00396336208440310
• Lin, Guohuai, Xun Chen, Jiecai Long, Jianfeng Sun, and Renquan Lu. 2026. “NN-Based Fixed-Time Human-in-the-Loop Formation Control for Nonlinear MASs with Time-Varying Delay.” Neurocomputing 678: 133101. https://doi.org/10.1016/j.neucom.2026.133101
• Lin, Jium-Ming, and Cheng-Hung Lin. 2014. “A Novel Intelligent Neural Guidance Law Design by Using Adjoint Method.” In 2014 International Conference on Machine Learning and Cybernetics. IEEE. https://doi.org/10.1109/icmlc.2014.7009133
• Lin, Yu-Ping, Lin Chun-Liang, and Chun-Wei Huang. 2010. “Design of a 3-D Modified Proportional Navigation Guidance Law.” In IEEE Icca 2010. IEEE. https://doi.org/10.1109/icca.2010.5524156
• Lin, Mu, Xiangjun Ding, Chunyan Wang, Li Liang, and Jianan Wang. 2021. “Three-Dimensional Fixed-Time Cooperative Guidance Law with Impact Angle Constraint and Prespecified Impact Time.” IEEE Access 9: 29755–63. https://doi.org/10.1109/access.2021.3057428
• 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, Hai, Jun-Xiang Ge, and Jie Wang. 2018. “Simulation of Suppression Technology of Angular Glint Based on MIMO Radar.” In 2018 Asia-Pacific Microwave Conference (APMC). IEEE. https://doi.org/10.23919/apmc.2018.8617319
• Lin, Chih-Min, Chun-Fei Hsu, Shing-Kuo Chang, and Rong-Jong Wai. 2000. “Guidance Law Evaluation for Missile Guidance Systems.” Asian Journal of Control 2 (4): 243–50. https://doi.org/10.1111/j.1934-6093.2000.tb00029.x
• Lin, Defu, Yi Ji, Wei Wang, Yuchen Wang, Hui Wang, and Fubiao Zhang. 2020. “Three-Dimensional Impact Angle-Constrained Adaptive Guidance Law Considering Autopilot Lag and Input Saturation.” International Journal of Robust and Nonlinear Control 30 (9): 3653–71. https://doi.org/10.1002/rnc.4955
• Lin, Tsung-Chi, Achyuthan Unni Krishnan, and Zhi Li. 2023. “The Impacts of Unreliable Autonomy in Human-Robot Collaboration on Shared and Supervisory Control for Remote Manipulation.” IEEE Robotics and Automation Letters 8 (8): 4641–48. https://doi.org/10.1109/lra.2023.3287039
• 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, Ching-Fang, and Marc W. Shafroth. 1983. “A Missile Control Strategy for Maneuvering Targets.” In 1983 American Control Conference. IEEE. https://doi.org/10.23919/acc.1983.4788275
• Lin, Li-Gang, and Ming Xin. 2019. “Missile Guidance Law Based on New Analysis and Design of SDRE Scheme.” Journal of Guidance, Control, and Dynamics 42 (4): 853–68. https://doi.org/10.2514/1.g003544
• Lindsay, James E. 1968. “Angular Glint and the Moving, Rotating, Complex Radar Target.” IEEE Transactions on Aerospace and Electronic Systems AES-4 (2): 164–73. https://doi.org/10.1109/taes.1968.5408954
• Linqi, Ye, Zong Qun, and Zhang Xiuyun. 2015. “Adaptive Control for a Non-Minimum Phase Hypersonic Vehicle Model.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7259769
• Litva, J., T. Lo, and T. Wong. 1991. “A New Technique for Low-Angle Radar Tracking.” In [1991] IEEE Pacific Rim Conference on Communications, Computers and Signal Processing Conference Proceedings. IEEE. https://doi.org/10.1109/pacrim.1991.160697
• Liu, Mei-Kao. 1967. “Skin-Friction Drag at Supersonic-Hypersonic Speeds with Transition.” Journal of Aircraft 4 (3): 264–65. https://doi.org/10.2514/3.43830
• Liu, Zhigao. 2017. “Constant Bearing Guidance Law for Homing Missiles.” In 2017 10th International Symposium on Computational Intelligence and Design (ISCID). IEEE. https://doi.org/10.1109/iscid.2017.168
• Liu, W., and B. J. R. Bailey. 2002. “Sample Size Determination for Constructing a Constant Width Confidence Interval for a Binomial Success Probability.” Statistics & Probability Letters 56 (1): 1–5. https://doi.org/10.1016/s0167-7152(01)00029-3
• Liu, Zhuoqi, Yuanli Cai, Yihang Liu, Yifan Deng, and Haonan Jiang. 2023f. “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, Mengxiang, Qi Fan, Jian Zhao, and Yan Su. 2020a. “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, Jun, Zhanpeng Gao, Jian Huang, and Wenjun Yi. 2026c. “Nonlinear Integral Sliding Mode Guidance Law with Impact Time and Angle Constraints Based on Look Angle Shaping.” In 2026 Joint International Conference on Automation-Intelligence-Safety (ICAIS) & International Symposium on Autonomous Systems (ISAS). IEEE. https://doi.org/10.1109/icaisisas68969.2026.11567733
• Liu, Yizhe, Jialiang Han, and Shuo Zhang. 2025b. “Linearized Lower Bounds on the Discrete Time Miss Distance for a Missile-Borne Radar Seeker under Target-Specific Maneuvers.” In 2025 6th International Conference on Electrical, Electronic Information and Communication Engineering (EEICE). IEEE. https://doi.org/10.1109/eeice65049.2025.11034323
• Liu, Jian-xia, Zhong-xi Hou, and Xiao-qing Chen. 2010c. “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, Bojun, Mingshan Hou, and Dan Feng. 2019c. “Nonlinear Mapping Based Impact Angle Control Guidance with Seeker’s Field-of-View Constraint.” Aerospace Science and Technology 86: 724–36. https://doi.org/10.1016/j.ast.2019.02.009
• Liu, Bojun, Mingshan Hou, and Yajun Li. 2019b. “Field-of-View and Impact Angle Constrained Guidance Law for Missiles with Time-Varying Velocities.” IEEE Access 7: 61717–27. https://doi.org/10.1109/access.2019.2916798
• Liu, Bojun, Mingshan Hou, Ying Yu, and Zhonghua Wu. 2020c. “Three-Dimensional Impact Angle Control Guidance with Field-of-View Constraint.” Aerospace Science and Technology 105: 106014. https://doi.org/10.1016/j.ast.2020.106014
• Liu, Yuming, Yan Huang, Hui Zhang, et al. 2025a. “Angular Super-Resolution for Target Positioning Using Dual-Antenna Dielectric Radar.” IEEE Transactions on Instrumentation and Measurement 74: 1–13. https://doi.org/10.1109/tim.2024.3485444
• Liu, Yunmei, and David B. Kaber. 2025. “Models of Automation Proportion in Human-in-the-Loop Systems and Operator Situation Awareness Responses.” Ergonomics: 1–14. https://doi.org/10.1080/00140139.2025.2608273
• Liu, Peng, Jian Li, Tuan Hua, and He Zhang. 2023e. “Simulation Test of the Aerodynamic Environment of a Missile-Borne Pulsed Laser Forward Detection System at High Flight Speed.” Photonics 10 (12): 1363. https://doi.org/10.3390/photonics10121363
• Liu, Yuanzhe, Peijin Liu, Zhuopu Wang, Wen Ao, and Yu Guan. 2023c. “Numerical Investigation of Combustion Instability in a Single-Element Liquid Rocket Engine: Intermittency Routes before and after Thermoacoustic Instability.” Aerospace Science and Technology 143: 108691. https://doi.org/10.1016/j.ast.2023.108691
• Liu, Yuanzhe, Peijin Liu, Zhuopu Wang, Wen Ao, Guanyu Xu, and Yu Guan. 2023b. “Numerical Investigation of Combustion Instability in a Liquid Rocket Engine: Interaction Effect between Hydrodynamics and Acoustic Mode.” Aerospace Science and Technology 143: 108711. https://doi.org/10.1016/j.ast.2023.108711
• Liu, Bowei, Yanli Ma, Yi Jiang, Weichen Wang, Yongyuan Li, and Liwu Shao. 2010b. “Numerical Simulation on Aerodynamic Heating Process and Research on the Missile Head Structure.” In 2010 Fifth International Conference on Frontier of Computer Science and Technology. IEEE. https://doi.org/10.1109/fcst.2010.47
• Liu, Xiao, and Bo Mo. 2018. “Line-of-Sight Estimation for Missile with Roll-Pitch Seeker.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8482856
• Liu, Shanzhong, Xiumin Qu, and Yongbin Liu. 2016. “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, Xinge, Haibin Sun, and Jiayuan Shan. 2017a. “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, Di, Bing Sun, Taiping Wang, Jiawen Song, and Jianwei Zhang. 2020b. “Thermo-Structural Analysis of Regenerative Cooling Thrust Chamber Cylinder Segment Based on Experimental Data.” Chinese Journal of Aeronautics 33 (1): 102–15. https://doi.org/10.1016/j.cja.2019.09.023
• Liu, Zhiman, and Yifei Wang. 2022. “Analysis and Simulation of Influence of Attitude Error on Strapdown Seeker Angle Rate Extraction.” In 2022 12th International Conference on CYBER Technology in Automation, Control, and Intelligent Systems (CYBER). IEEE. https://doi.org/10.1109/cyber55403.2022.9907634
• Liu, Tianya, Fengshuo Wang, and Peng Li. 2025d. “Miss Distance Minimization in Missile Penetration Trajectory Planning.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487432
• Liu, Wangkui, Yiyin Wei, and Guangren Duan. 2017b. “Integrated Guidance and Control with Impact Angle Constraint.” In 2017 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2017.8242887
• Liu, Wangkui, Yiyin Wei, Guangren Duan, and Mingzhe Hou. 2019a. “Extended State Observer-Based Integrated Guidance and Control with Impact Angle Constraint and Input Saturation.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866130
• Liu, Da-wei, Qun-li Xia, Yun-li Du, and Ti-ti Zuo. 2011. “Miss Distance and Impact Angle Error of Trajectory Shaping Guidance Law Based on Statistical Linearization Adjoint Method.” Energy Procedia 13: 6370–77. https://doi.org/10.1016/j.egypro.2011.12.317
• Liu, Yuanhe, Nianhao Xie, Kebo Li, and Yan’gang Liang. 2024c. “Missile Guidance Law Design Based on Free-Time Convergent Error Dynamics.” Journal of Systems Engineering and Electronics 35 (5): 1315–25. https://doi.org/10.23919/jsee.2024.000103
• Liu, Yang, Yu Xie, Wei Li, and Yuanlong Zhang. 2021. “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, Baijun, Pengfei Xing, and Chenggang Bai. 2024a. “Fast Finite-Time Extended State Observer Based Fast Nonsingular Integral Terminal Sliding Mode Control for Hypersonic Glide Vehicles.” In 2024 43rd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc63176.2024.10662442
• Liu, Rui, Jindong Zhang, Yaxin Ji, and Daiyin Zhu. 2024d. “Multibeam Generalized Monopulse Angle Estimation for APAR.” IEEE Sensors Journal 24 (24): 41311–22. https://doi.org/10.1109/jsen.2024.3482702
• Liu, Shuo, Zhiheng Zhang, Chushu Yi, Jing Chen, and Lina Lu. 2025c. “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 Zhenyu. 2003. “Tracking Radar Digital Matched-Filter ASIC Design and Its Error Analysis.” In 2003 5th International Conference on ASIC Proceedings (IEEE Cat No 03TH8690) ICASIC-03. IEEE. https://doi.org/10.1109/icasic.2003.1277326
• Liwei, Zheng, and Jing Wuxing. 2006. “Adaptive Variable Structure Guidance Using Zero Effort Miss.” In 2006 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.280816
• Lizarraga, Mariano, Renwick Curry, and Gabriel Hugh Elkaim. 2013. “Flight Test Results for an Improved Line of Sight Guidance Law for UAVs.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6579937
• Lizhong Song, Xiaolin Qiao, and Xiande Meng. 2004. “Angle Glint Suppression for Millimeter-Wave Radar Based on Polarization Filtering.” In ICMMT 4th International Conference on, Proceedings Microwave and Millimeter Wave Technology, 2004.. IEEE. https://doi.org/10.1109/icmmt.2004.1411609
• Lo, T., and J. Litva. n.d. “Early Results of Multipath Measurements on Lake Ontario (Low Angle Radar Tracking).” In Digest on Antennas and Propagation Society International Symposium. IEEE. https://doi.org/10.1109/aps.1989.134817
• Loomis, Jester M., and Edward R. Graf. 1974. “Frequency-Agility Processing to Reduce Radar Glint Pointing Error.” IEEE Transactions on Aerospace and Electronic Systems AES-10 (6): 811–20. https://doi.org/10.1109/taes.1974.307889
• 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
• Lopez, J. L., W. R. Lawrence, C. Stewart, and J. White. n.d. “Data Link Effects on Weapon Accuracy.” In IEEE Proceedings on Southeastcon. IEEE. https://doi.org/10.1109/secon.1990.117888
• Lopez Martinez, C. A., R. van de Molengraft, and M. Steinbuch. 2012. “Robust Performance Control Design for Bilateral Teleoperation under Time-Varying Bounded Operator and Environment Dynamics.” In 2012 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2012.6315374
• Lopez Martinez, Cesar A., R. van de Molengraft, and M. Steinbuch. 2013. “High Performance Teleoperation Using Switching Robust Control.” In 2013 World Haptics Conference (WHC). IEEE. https://doi.org/10.1109/whc.2013.6548439
• Lord, W. T., and E. Eminton. 1954. “Slender Bodies of Minimum Wave Drag.” Journal of the Aeronautical Sciences 21 (8): 569–70. https://doi.org/10.2514/8.3128
• 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
• Louca, Joe, Kerstin Eder, John Vrublevskis, and Antonia Tzemanaki. 2024. “Impact of Haptic Feedback in High Latency Teleoperation for Space Applications.” ACM Transactions on Human-Robot Interaction 13 (2): 1–21. https://doi.org/10.1145/3651993
• Louca, Joe, John Vrublevskis, Kerstin Eder, and Antonia Tzemanaki. 2023. “Elicitation of Trustworthiness Requirements for Highly Dexterous Teleoperation Systems with Signal Latency.” Frontiers in Neurorobotics 17: 1187264. https://doi.org/10.3389/fnbot.2023.1187264
• Loupy, G. J. M., G. N. Barakos, and N. J. Taylor. 2018. “Cavity Flow over a Transonic Weapons Bay during Door Operation.” Journal of Aircraft 55 (1): 339–54. https://doi.org/10.2514/1.c034344
• Lowrie, Richard W. 1960a. “A Device for Automatically Tracking the Roll Position of a Missile.” IRE Transactions on Space Electronics and Telemetry SET-6 (2): 67–69. https://doi.org/10.1109/iret-set.1960.5008717
• Lowrie, Richard. 1960b. “A Secure Digital Command Link.” IRE Transactions on Space Electronics and Telemetry SET-6 (3/4): 103–14. https://doi.org/10.1109/iret-set.1960.5008729
• Lu, Ningbo, Jianguo Guo, Zongyi Guo, and Guoqing Wang. 2023. “Asymmetric BLOS Constraint-Involved Intelligent Integrated Guidance and Control Approach for Flight Vehicle Equipped with Strapdown Seeker.” Advances in Space Research 72 (10): 4461–73. https://doi.org/10.1016/j.asr.2023.08.004
• Lu, Ming-Wei, and Richard J. Rudy. 2001. “Reliability Demonstration Test for a Finite Population.” Quality and Reliability Engineering International 17 (1): 33–38. https://doi.org/10.1002/qre.377
• Lu, Tianyu, Liang Wang, Teng Shang, and Yunpeng Liu. 2018. “The Guidance Strategy for Maneuvering Target with Phased Array Radar Seeker.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018862
• Lu, Chao, Guangming Zhang, and Xiaodong Lv. 2025. “A Control Method for Thermal Structural Tests of Hypersonic Missile Aerodynamic Heating.” Mathematics 13 (3): 380. https://doi.org/10.3390/math13030380
• Lu, Xin, Silong Zhang, and Jiang Qin. 2024a. “Effects of Ammonia Combustion on Skin Friction Characteristics for Supersonic Flow.” International Journal of Mechanical Sciences 263: 108793. https://doi.org/10.1016/j.ijmecsci.2023.108793
• Luan, Yuzhe., Mingrou. Shi, Zi. He, Dazhi. Ding, and Hongcheng. Yin. 2026. “Regulation Technique of near-Field Angular Glint Based on the Shooting and Bouncing Method.” In 2026 IEEE International Conference on Computational Electromagnetics (ICCEM). IEEE. https://doi.org/10.1109/iccem68495.2026.11628950
• Lubnau, Donald G. 1977. “Maximum Likelihood Estimate of Target Angles for a Conical Scan Tracking System in the Presence of Speckle.” Applied Optics 16 (1): 184. https://doi.org/10.1364/ao.16.000184
• Lunev, V. V. 1960. “Motion of a Slender Blunted Body in the Atmosphere with High Supersonic Speed.” ARS Journal 30 (4): 414–16. https://doi.org/10.2514/8.5089
• Luo, Yue, Kai Huang, Miao Wang, and Guoqing Wang. 2024. “Iterative Function Allocation of Single Pilot Operations Based on Biclustering Method.” International Journal of Human–Computer Interaction 41 (14): 9026–40. https://doi.org/10.1080/10447318.2024.2417147
• Luo, Hongbing, Haibo Ji, Xinghu Wang, and Xinyu Qu. 2020a. “Cooperative Robust Line-of-Sight Guidance Law for Aerial Target Defense.” In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE. https://doi.org/10.1109/icuas48674.2020.9213909
• Luo, Haowen, Zichao Liu, Tianyu Jin, Chang-Hun Lee, and Shaoming He. 2025. “Computational Predictor–Corrector Homing Guidance for Constrained Impact.” Journal of Guidance, Control, and Dynamics 48 (6): 1366–80. https://doi.org/10.2514/1.g008968
• Luo, Hongbing, Gaoyong Tan, Han Yan, Xinghu Wang, and Haibo Ji. 2023. “Cooperative Line-of-Sight Guidance with Optimal Evasion Strategy for Three-Body Confrontation.” ISA Transactions 133: 262–72. https://doi.org/10.1016/j.isatra.2022.07.018
• Luo, Jing, Chenguang Yang, Ning Wang, and Min Wang. 2019. “Enhanced Teleoperation Performance Using Hybrid Control and Virtual Fixture.” International Journal of Systems Science 50 (3): 451–62. https://doi.org/10.1080/00207721.2018.1562128
• 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
• Lutz, Steffen, Christian Erhart, Thomas Walter, and Robert Weigel. 2015. “8 Channel MIMO Long Range Radar Concept for Angular Estimation in Multi Target Scenarios.” In 2015 IEEE MTT-S International Conference on Microwaves for Intelligent Mobility (ICMIM). IEEE. https://doi.org/10.1109/icmim.2015.7117955
• Lux, Johannes, Dmitry Suslov, and Oskar Haidn. 2008. “On Porous Liquid Propellant Rocket Engine Injectors.” Aerospace Science and Technology 12 (6): 469–77. https://doi.org/10.1016/j.ast.2007.11.004
• 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, Junjie, Guanquan Du, Ping Jin, and Ruizhi Li. 2023a. “Heat Transfer Analysis and Structural Optimization for Spiral Channel Regenerative Cooling Thrust Chamber.” International Journal of Aerospace Engineering 2023: 1–17. https://doi.org/10.1155/2023/8628107
• Lv, Junjie, Yushan Gao, Ping Jin, et al. 2023b. “A Simplified One-Dimensional Transient Heat Transfer Model for Rocket Thrust Chamber.” Applied Thermal Engineering 218: 119379. https://doi.org/10.1016/j.applthermaleng.2022.119379
• 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, Peng, Guohua Wei, and Wei Cui. 2018. “Impact of Acceleration on Miss Distance Parameter Estimation.” Journal of Guidance, Control, and Dynamics 41 (5): 1175–82. https://doi.org/10.2514/1.g003205
• Lv, Tiancheng, Renli Zhang, Weixing Sheng, and Yubing Han. 2026. “Angle Estimation of Retrodirective Cross-Eye Jammer Based on Joint-Transmit-and-Receive-Beam Synthesis and Complex-Monopulse-Ratio Vector.” IEEE Transactions on Aerospace and Electronic Systems 62: 8531–45. https://doi.org/10.1109/taes.2025.3639004
• Lyu, Shi, Zheng H. Zhu, Shuo Tang, and Xiaodong Yan. 2018. “Hybrid Cooperative Guidance Law for Active Aircraft Defense against a Guided Missile.” Journal of Guidance, Control, and Dynamics 41 (2): 535–41. https://doi.org/10.2514/1.g003059
• Ma, Biao, Mou Chen, Yaohua Shen, and Mihai Lungu. 2022. “Inverse Optimal Zero Effort Miss Guidance Based on Disturbance Observer.” Aerospace 9 (12): 767. https://doi.org/10.3390/aerospace9120767
• Ma, Qiancai, Yi Ji, Zhiqi Niu, Qiuxiong Gou, and Liangyu Zhao. 2020. “Impact Angle Constraint Dual-Layer Adaptive Guidance Law with Actuator Faults.” IEEE Access 8: 115823–36. https://doi.org/10.1109/access.2020.3003915
• Ma, Qinghua, and Haiqing Li. 2020. “Design of Attitude Control Law for over-Shoulder Launch of Helicopter-Borne Air-to-Ground Missile.” In 2020 IEEE 5th Information Technology and Mechatronics Engineering Conference (ITOEC). IEEE. https://doi.org/10.1109/itoec49072.2020.9141705
• Ma, Shufen, Erke Mao, and Shujuan Hou. 2006. “Estimation of Miss Distance Parameters Based on Dopplerlet Transform and Matching Pursuitalgorithm.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.346020
• Ma, Xingjian, and Anthony D. McDonald. 2026. “Identifying Critical Breakpoints and Latency Effects during Remote Backup Driving.” IEEE Transactions on Human-Machine Systems 56 (4): 804–14. https://doi.org/10.1109/thms.2026.3691492
• Ma Pei-bei, Zhang You-an, Ji Jun, and Zhang Xiao-jie. 2009. “Three-Dimensional Guidance Law with Terminal Impact Angle Constraint.” In 2009 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2009.5246554
• Mabey, Dennis G., and Laurie Gaudet. 1975. “Performance of Small Skin Friction Balances at Supersonic Speeds.” Journal of Aircraft 12 (10): 819–25. https://doi.org/10.2514/3.44494
• Maddox, Arthur R. 1980. “Store Separation Trajectory Analysis.” Journal of Aircraft 17 (11): 769–73. https://doi.org/10.2514/3.44686
• Madni, A. M. 1988. “HUMANE: A Knowledge-Based Simulation Environment for Human-Machine Function Allocation.” In Proceedings of the IEEE 1988 National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1988.195107
• Mahafza, B., S. Welstead, D. Champagne, R. Manadhar, T. Worthington, and S. Campbell. 1998. “Real-Time Radar Signal Simulation for the Ground Based Radar for National Missile Defense.” In Proceedings of the 1998 IEEE Radar Conference, RADARCON’98. Challenges in Radar Systems and Solutions (Cat. No.98CH36197). IEEE. https://doi.org/10.1109/nrc.1998.677978
• 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
• Mahmoud, AbdelMageed, Zhou Hao, Chen Wanchun, and Liang Yang. 2017. “Ascent and Glide Trajectory Optimization for Hypersonic Vehicle.” In 2017 International Conference on Control, Artificial Intelligence, Robotics & Optimization (ICCAIRO). IEEE. https://doi.org/10.1109/iccairo.2017.35
• Maikapar, G. I. 1959. “On the Wave Drag of Non Anixymmetric Bodies at Supersonic Speeds.” Journal of Applied Mathematics and Mechanics 23 (2): 528–31. https://doi.org/10.1016/0021-8928(59)90104-2
• Maitra, S. N. 2000. “Aerodynamic Heating of Ballistic Missile Including the Effects of Gravity.” Sadhana 25 (5): 463–73. https://doi.org/10.1007/bf02703627
• Maity, Arnab, Harshal B. Oza, and Radhakant Padhi. 2013. “Generalized Model Predictive Static Programming and Its Application to 3D Impact Angle Constrained Guidance of Air-to-Surface Missiles.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6580614
• Maity, Arnab, Harshal B. Oza, and Radhakant Padhi. 2014. “Generalized Model Predictive Static Programming and Angle-Constrained Guidance of Air-to-Ground Missiles.” Journal of Guidance, Control, and Dynamics 37 (6): 1897–1913. https://doi.org/10.2514/1.g000038
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2024a. “Three-Dimensional Impact Angle Constrained Nonlinear Guidance with Predefined Convergence Time.” Nonlinear Dynamics 112 (12): 9983–10008. https://doi.org/10.1007/s11071-024-09564-1
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2020. “Finite-Time Convergent Impact Angle Constrained Sliding Mode Guidance.” IFAC-PapersOnLine 53 (1): 87–92. https://doi.org/10.1016/j.ifacol.2020.06.015
• Malatji, Tsholofelo M., and Warren P. du Plessis. 2017. “Jammer Signal Effectiveness against a Conical-Scan Missile Seeker.” In 2017 IEEE Africon. IEEE. https://doi.org/10.1109/afrcon.2017.8095548
• Malysz, Pawel, and Shahin Sirouspour. 2010. “Cooperative Teleoperation Control with Projective Force Mappings.” In 2010 IEEE Haptics Symposium. IEEE. https://doi.org/10.1109/haptic.2010.5444641
• Manchester, I. R., and A. V. Savkin. 2002. “Circular Navigation Guidance Law for Precision Missile/target Engagements.” In Proceedings of the 41st IEEE Conference on Decision and Control, 2002., vol. 2. IEEE. https://doi.org/10.1109/cdc.2002.1184692
• Manchester, Ian R., and Andrey V. Savkin. 2006. “Circular-Navigation-Guidance Law for Precision Missile/Target Engagements.” Journal of Guidance, Control, and Dynamics 29 (2): 314–20. https://doi.org/10.2514/1.13275
• Mangulis, V. 1981. “Frequency Diversity in Low-Angle Radar Tracking.” IEEE Transactions on Aerospace and Electronic Systems AES-17 (1): 149–53. https://doi.org/10.1109/taes.1981.309050
• Manuilov, B. D., P. N. Bashly, and D. V. Klimukhin. 2007. “On Increasing the Accuracy of Monopulse Antenna Arrays under Conditions of Informational Conflict.” In 2007 7th International Symposium on Electromagnetic Compatibility and Electromagnetic Ecology. IEEE. https://doi.org/10.1109/emceco.2007.4371672
• Manzoor Hasan, Asif, Johan Larsson, Sergio Pirozzoli, and Rene Pecnik. 2024. “Estimating Mean Profiles and Fluxes in High-Speed Turbulent Boundary Layers Using Inner/Outer-Layer Scalings.” AIAA Journal 62 (2): 848–53. https://doi.org/10.2514/1.j063335
• 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
• Maré, Jean-Charles. 2022. “A Preliminary Top-Down Parametric Design of Electromechanical Actuator Position Control.” Aerospace 9 (6): 314. https://doi.org/10.3390/aerospace9060314
• Maresca, Salvatore, Maria Greco, Fulvio Gini, and Lucio Verrazzani. 2008. “Radar Tracking of a Move-Stop-Move Maneuvering Target in Clutter.” In 2008 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2008.4720825
• Markham, Keith C. 2019. “Planar Proportional Navigation Equation Solutions for Periodic Inputs.” Journal of Guidance, Control, and Dynamics 42 (9): 2093–97. https://doi.org/10.2514/1.g004334
• Markham, Keith C. 2024. “Solutions of Linearized Proportional Navigation Equation for Missile with First-Order Lagged Dynamics.” Journal of Guidance, Control, and Dynamics 47 (3): 589–96. https://doi.org/10.2514/1.g008064
• Markin, Evgeny. 2011. “Stability Criterion of Radar Angle Tracking Systems in Real Time under Conditions of Polarization Jamming.” In 2011 IEEE RadarCon (RADAR). IEEE. https://doi.org/10.1109/radar.2011.5960536
• 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
• Martel, J. D. 2003. “Applied Computational Fluid Dynamics (ACFD) in Support of Aircraft-Store Compatibility and Weapons Integration.” In 2003 User Group Conference. Proceedings. IEEE. https://doi.org/10.1109/dodugc.2003.1253385
• Martel, Cedric. 2013. “Low Profile and Anti-Jam GPS Array.” In 2013 IEEE Antennas and Propagation Society International Symposium (APSURSI). IEEE. https://doi.org/10.1109/aps.2013.6711268
• Martin, Rodney A. 2007. “Unsupervised Anomaly Detection and Diagnosis for Liquid Rocket Engine Propulsion.” In 2007 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2007.352949
• Martin, Lynne, Nancy Bienert, Lauren Claudatos, Vimmy Gujral, Joshua Kraut, and Joey Mercer. 2016. “Effects of Task Allocation on Air Traffic Management Human-Automation System Performance.” In 2016 IEEE/AIAA 35th Digital Avionics Systems Conference (DASC). IEEE. https://doi.org/10.1109/dasc.2016.7777996
• Martinez-Garcia, Miguel, Timothy Gordon, and Lei Shu. 2017. “Extended Crossover Model for Human-Control of Fractional Order Plants.” IEEE Access 5: 27622–35. https://doi.org/10.1109/access.2017.2778013
• 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
• Marxman, Gerald A., and Charles E. Wooldridge. 1969. “Finite-Amplitude Axial Instability in Solid-Rocket Combustion.” Symposium (International) on Combustion 12 (1): 115–27. https://doi.org/10.1016/s0082-0784(69)80396-6
• 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
• Masuyama, Eitaro. 1992. “Human Frequency Characteristics in Manual Tracking of Three Input Waves.” Ergonomics 35 (5–6): 525–40. https://doi.org/10.1080/00140139208967834
• Mathews, Kenneth C. 1960. “Missile Orientation Errors in Command Guidance Systems.” ARS Journal 30 (1): 46–50. https://doi.org/10.2514/8.4983
• 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
• Maupin, D. L. n.d. “Missile Test Confidence via Test Systems Certification and Associated Data Analysis.” In Proceedings, IEEE AUTOTESTCON. IEEE. https://doi.org/10.1109/autest.2002.1047950
• Mayer, Wolfgang, and Hiroshi Tamura. 1996. “Propellant Injection in a Liquid Oxygen/gaseous Hydrogen Rocket Engine.” Journal of Propulsion and Power 12 (6): 1137–47. https://doi.org/10.2514/3.24154
• McCARTHY, John C., Enda Fallon, and Liam Bannon. 2000. “Dialogues on Function Allocation.” International Journal of Human-Computer Studies 52 (2): 191–201. https://doi.org/10.1006/ijhc.1999.0284
• McDonald, Kenneth, Zhihua Qu, and Edward Daughtery. 2024. “Optimal Generalized Vector Explicit (GENEX) Homing Guidance of Nonholonomic Systems.” In 2024 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero58975.2024.10521417
• 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
• McLntyre, C. M., J. R. Kerr, M. H. Lee, and J. H. Churnside. 1979. “Enhanced Variance of Irradiance from Target Glint.” Applied Optics 18 (19): 3211. https://doi.org/10.1364/ao.18.003211
• Mehra, Raman, and Ralph Ehrich. 1984. “Air-to-Air Missile Guidance for Strapdown Seekers.” In The 23rd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1984.272186
• 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
• Mehrandezh, M., M. N. Sela, R. G. Fenton, and B. Benhabib. 1999. “Proportional Navigation Guidance in Robot Trajectory Planning for Intercepting Moving Objects.” In Proceedings 1999 IEEE International Conference on Robotics and Automation (Cat. No.99CH36288C), vol. 1. IEEE. https://doi.org/10.1109/robot.1999.769945
• Mehrjouyan, Ali, Mohammad B. Menhaj, Erfan Askarzadeh, and Amir Hooshiar. 2025. “Transparency-Enhanced Observer-Based Adaptive Backstepping Torque–position Control for Teleoperation Systems with Position Error Constraint and Time-Varying Delay.” European Journal of Control 81: 101153. https://doi.org/10.1016/j.ejcon.2024.101153
• 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
• Melino, Costantino. 1987. “Average Monopulse Angle Tracking Response to Two Unresolved Sources.” IEEE Transactions on Aerospace and Electronic Systems AES-23 (5): 634–43. https://doi.org/10.1109/taes.1987.310857
• Meller, Michal. 2017a. “Experimental Evaluation of Estimator Mean Square Error Curve for Cognitive Tracking Radar.” In 2017 Signal Processing Symposium (SPSympo). IEEE. https://doi.org/10.1109/sps.2017.8053675
• Meller, Michal. 2017b. “Radar Time Budget Optimization Subject to Angle Accuracy Constraint via Cognitive Approach.” In 2017 18th International Radar Symposium (IRS). IEEE. https://doi.org/10.23919/irs.2017.8008150
• Meng, Qingliang, Yunxin Li, Ning Ma, Yue Pan, and Weidong Song. 2023. “Research on Integrated Simulation Method for Anti-Jamming Verification of Air Defense Missile.” In 2023 38th Youth Academic Annual Conference of Chinese Association of Automation (YAC). IEEE. https://doi.org/10.1109/yac59482.2023.10401844
• 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
• Mengxiang, Chen, and Zhang Weidong. 2015. “H2 Optimal Proportional Navigation Guidance Law.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260424
• 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
• Merkulov, Gleb, Martin Weiss, and Tal Shima. 2025. “Virtual Target Approach for Emulation of Optimal Guidance Using Proportional Navigation.” Journal of Guidance, Control, and Dynamics 48 (5): 1099–1111. https://doi.org/10.2514/1.g008726
• Merriam, C. W. 1960. “An Optimization Theory for Feedback Control System Design.” Information and Control 3 (1): 32–59. https://doi.org/10.1016/s0019-9958(60)90257-6
• Merz, Antony W. 1964. “Missile Attitude Stabilization by Lyapunov’s Second Method.” Journal of Spacecraft and Rockets 1 (6): 598–604. https://doi.org/10.2514/3.27709
• Meschler, Paul A. 1971. “Rocket Guidance with a Steering Angle-Rate Constraint.” Journal of Spacecraft and Rockets 8 (11): 1167–68. https://doi.org/10.2514/3.30362
• “A Method for Aiding Human Operator Performance in a Noncompensatory Tracking Task.” 1972. IEEE Transactions on Systems, Man, and Cybernetics SMC-2 (5): 670–74. https://doi.org/10.1109/tsmc.1972.4309198
• Mettler, Berenice, and Jon Andersh. 2013. “Fundamental Control Characteristics of Curvilinear Motion in Human and Automatic Path Tracking Tasks.” In 2013 American Control Conference. IEEE. https://doi.org/10.1109/acc.2013.6580852
• 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, Rudolf X. 1959. “Magnetohydrodynamics and Aerodynamic Heating.” ARS Journal 29 (3): 187–92. https://doi.org/10.2514/8.4717
• Mi, Wenhao, Jiayuan Shan, and Yongshan Liu. 2018. “Adaptive Unscented Kalman Filter Based Line of Sight Rate for Strapdown Seeker.” In 2018 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2018.8623793
• Miall, R. C. 1996. “Task-Dependent Changes in Visual Feedback Control: A Frequency Analysis of Human Manual Tracking.” Journal of Motor Behavior 28 (2): 125–35. https://doi.org/10.1080/00222895.1996.9941739
• Miao, Xun, Jianxin Hu, Yiyi Xu, et al. 2024. “Thermal–structural Response and Life Prediction of Lattice Regenerative Cooling Thrust Chambers in Liquid Rocket Engines Based on a Simplified Viscoplastic Model.” International Communications in Heat and Mass Transfer 159: 108254. https://doi.org/10.1016/j.icheatmasstransfer.2024.108254
• Miao Sui and Xiaojian Xu. 2011. “Angular Glint Calculation via Adaptive Cross Approximation Algorithm.” In 2011 IEEE International Symposium on Antennas and Propagation (APSURSI). IEEE. https://doi.org/10.1109/aps.2011.5997094
• 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
• Mickle, M. C., and J. J. Zhu. n.d.-b. “A Nonlinear Roll-Yaw Missile Autopilot Based on Plant Inversion and PD-Spectral Assignment.” In Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171), vol. 4. IEEE. https://doi.org/10.1109/cdc.1998.762072
• “Micro-Teleoperation with Manual Task Execution Posture.” 1995. IEEE Control Systems 15 (1): 22–29. https://doi.org/10.1109/37.341860
• Miele, Angelo. 1957. “Optimum Burning Program as Related to Aerodynamic Heating for a Missile Traversing the Earth’s Atmosphere.” Journal of Jet Propulsion 27 (12): 1231–40. https://doi.org/10.2514/8.12515
• Miguel, Anthony San. 1974. “Design of Missile-Aircraft Component White Noise Isolators.” Journal of Aircraft 11 (11): 704–9. https://doi.org/10.2514/3.44404
• Miles, John W. 1952. “Slender Body Theory for Supersonic Unsteady Flow.” Journal of the Aeronautical Sciences 19 (4): 280–81. https://doi.org/10.2514/8.2249
• Miles, John W. 1956. “On the Sonic Drag of a Slender Body.” Journal of the Aeronautical Sciences 23 (2): 146–54. https://doi.org/10.2514/8.3522
• Miller, Duncan C. 1965. “The Effects of Performance-Scoring Criteria on Compensatory Tracking Behavior.” IEEE Transactions on Human Factors in Electronics HFE-6 (1): 62–65. https://doi.org/10.1109/thfe.1965.6591257
• Miller, R. B., and M. Pachter. n.d. “Manual Tracking Control with Amplitude and Rate Constrained Actuators.” In Proceedings of 35th IEEE Conference on Decision and Control, vol. 3. IEEE. https://doi.org/10.1109/cdc.1996.573616
• Miloh, T., M. Pachter, and A. Segal. 1993. “The Effect of a Finite Roll Rate on the Miss-Distance of a Bank-to-Turn Missile.” Computers & Mathematics with Applications 26 (6): 43–54. https://doi.org/10.1016/0898-1221(93)90116-d
• Ming Jin, Yinan Zhao, Xiaolin Qiao, and Shilou Jia. 2004. “Target Angular Glint under Radar Non-Uniform Illumination.” In ICMMT 4th International Conference on, Proceedings Microwave and Millimeter Wave Technology, 2004.. IEEE. https://doi.org/10.1109/icmmt.2004.1411490
• 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
• Ming-Wei Lu and R. J. Rudy. 2001. “Laboratory Reliability Demonstration Test Considerations.” IEEE Transactions on Reliability 50 (1): 12–16. https://doi.org/10.1109/24.935011
• Mingde, Gong, Yang Bin, and Yamada Hironao. 2010. “Performance Experiment of a Hydraulic Force Feedback Teleoperation Robot Based on Position and Rate Control.” In 2010 Second International Conference on Intelligent Human-Machine Systems and Cybernetics. IEEE. https://doi.org/10.1109/ihmsc.2010.121
• Mingxiao Jiang and Daniel J. Dummer. 2009. “Bayesian Reliability Demonstration Test in a Design for Reliability Process.” In 2009 Annual Reliability and Maintainability Symposium. IEEE. https://doi.org/10.1109/rams.2009.4914645
• Mingyi, Fan, Ge Jianjun, Qiu Wei, and Wu Manqing. 2007. “MonoPulse Angle Measurement for an Airborne Side-Looking Phased Array PD Radar.” In 2007 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2007.374214
• Minor, L. G. n.d. “Application of Pattern Recognition and Image Processing Techniques to Lock-on-after-Launch Missile Technology.” In Conference Proceedings Southeastcon ‘81.. IEEE. https://doi.org/10.1109/secon.1981.673487
• Mir, Hasan S., and John D. Wilkinson. 2008. “Task Scheduling Algorithm for an Air and Missile Defense Radar.” In 2008 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radar.2008.4720998
• Mishra, S. K., I. G. Sarma, and K. N. Swamy. 1994. “Performance Evaluation of Two Fuzzy-Logic-Based Homing Guidance Schemes.” Journal of Guidance, Control, and Dynamics 17 (6): 1389–91. https://doi.org/10.2514/3.21368
• “Miss Distance Analysis in a New Guidance Law.” 1999. In Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251). IEEE. https://doi.org/10.1109/acc.1999.786613
• “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
• Mitchell, C. E., L. Crocco, and W. A. Sirignano. 1969. “Nonlinear Longitudinal Instability in Rocket Motors with Concentrated Combustion.” Combustion Science and Technology 1 (1): 35–64. https://doi.org/10.1080/00102206908952190
• Mitchell, Adam E., Graeme E. Smith, Kristine L. Bell, and Muralidhar Rangaswamy. 2017. “Single Target Tracking with Distributed Cognitive Radar.” In 2017 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2017.7944213
• Miwa, Susumu, and Fumiaki Imado. 1986. “Clutter Effect on the Guidance of a Semi-Active Radar Homing Missile.” Journal of Guidance, Control, and Dynamics 9 (3): 268–73. https://doi.org/10.2514/3.20102
• Miwa, Susumu, Fumiaki Imado, and Takeshi Kuroda. 1988. “Clutter Effect on the Miss Distance of a Radar Homing Missile.” Journal of Guidance, Control, and Dynamics 11 (4): 336–42. https://doi.org/10.2514/3.20316
• Moghimi Rad, Saber, Alireza Khosravi, and Pouria Sarhadi. 2021. “Pitch Autopilot Design for an Autonomous Aerial Vehicle in the Presence of Amplitude and Rate Saturation.” Aerospace Science and Technology 108: 106371. https://doi.org/10.1016/j.ast.2020.106371
• Mohammadi, Alireza, Mahdi Tavakoli, and Horacio J. Marquez. 2011. “Control of Nonlinear Bilateral Teleoperation Systems Subject to Disturbances.” In IEEE Conference on Decision and Control and European Control Conference. IEEE. https://doi.org/10.1109/cdc.2011.6160185
• 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
• Mol, Nicky, J. Micah Prendergast, David A. Abbink, and Luka Peternel. 2026. “Fitts’ List Revisited: An Empirical Study on Function Allocation in a Two-Agent Physical Human-Robot Collaborative Position/Force Task.” IEEE Robotics and Automation Letters 11 (1): 202–9. https://doi.org/10.1109/lra.2025.3632607
• Moldavskaya, Elina, and Josef Shinar. 2015. “Distribution of the Zero-Effort Miss Distance Estimation Error in Interception Problems.” Applied Mathematics and Computation 269: 217–31. https://doi.org/10.1016/j.amc.2015.07.073
• Monakov, A. A. 1990. “Angular Glint in Polarization Double-Channel Systems.” In International Symposium on Antennas and Propagation Society, Merging Technologies for the 90’s. IEEE. https://doi.org/10.1109/aps.1990.115426
• 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
• Moon, Sei-Hoon. 2021. “Weapon Effectiveness and the Shapes of Damage Functions.” Defence Technology 17 (2): 617–32. https://doi.org/10.1016/j.dt.2020.04.009
• Moon, Han-Bit, Young-Kwang Jung, and Won-Sang Ra. 2015. “Terminal Acceleration Stabilizing Guidance Law for Impact Angle Constrained Interception of a Non-Maneuvering Target.” International Journal of Control, Automation and Systems 13 (6): 1410–22. https://doi.org/10.1007/s12555-014-0196-z
• Moon, Jongki, Kiseok Kim, and Youdan Kim. 2001. “Design of Missile Guidance Law via Variable Structure Control.” Journal of Guidance, Control, and Dynamics 24 (4): 659–64. https://doi.org/10.2514/2.4792
• Moore, F. G., F. Wilcox, and T. Hymer. 1994. “Base Drag Prediction on Missile Configurations.” Journal of Spacecraft and Rockets 31 (5): 759–65. https://doi.org/10.2514/3.26509
• 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
• Moreno, Robinson Jimenez. 2014. “Tracking of Human Operator Arms Oriented to the Control of Two Robotic Arms.” In 2014 XIX Symposium on Image, Signal Processing and Artificial Vision. IEEE. https://doi.org/10.1109/stsiva.2014.7010125
• Mortazavi, Mohammad Reza, and Farshad Almasganj. 2018. “Optimal Midcourse Guidance of an Air-to-Air Missile via SVM and RVM.” Soft Computing 23 (15): 6603–16. https://doi.org/10.1007/s00500-018-3308-5
• Mortensen, R. E. 1974. “Strapdown Guidance Error Analysis.” IEEE Transactions on Aerospace and Electronic Systems AES-10 (4): 451–57. https://doi.org/10.1109/taes.1974.307798
• Mosca, Edoardo. 1969. “Angle Estimation in Amplitude Comparison Monopulse Systems.” IEEE Transactions on Aerospace and Electronic Systems AES-5 (2): 205–12. https://doi.org/10.1109/taes.1969.309906
• Motallebi, F. 1994. “Comment on ‘Skin Friction and Velocity Profile Family for Compressible Turbulent Boundary Layers’.” AIAA Journal 32 (9): 1938–39. https://doi.org/10.2514/3.12200
• Mrstik, A. V., and P. G. Smith. 1978. “Multipath Limitations on Low-Angle Radar Tracking.” IEEE Transactions on Aerospace and Electronic Systems AES-14 (1): 85–102. https://doi.org/10.1109/taes.1978.308582
• Mu, Hai-Jian, Kun-Yi Guo, Xin-Qing Sheng, and Hong-Yuan Yu. 2012. “Strict Formulas of Angular Glint Linear Deviation of Complex Target with Polarization Consideration.” In ISAPE2012. IEEE. https://doi.org/10.1109/isape.2012.6408986
• Mukherjee, Dwaipayan, and Debasish Ghose. 2013. “Zero-Miss-Distance Guidance Strategies for Nonminimum-Phase Interceptors.” Journal of Guidance, Control, and Dynamics 36 (2): 629–34. https://doi.org/10.2514/1.58536
• Mularzuk, Roman. 2018. “Monopulse Estimation of Direction of Arrival in Case of Multiple Incoherent Sources.” In 2018 22nd International Microwave and Radar Conference (MIKON). IEEE. https://doi.org/10.23919/mikon.2018.8405304
• 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
• Murray, Taft. 1984. “Correlation of Linear and Nonlinear Radome Error Induced Miss Distance Predictions.” In 1984 American Control Conference. IEEE. https://doi.org/10.23919/acc.1984.4788474
• Muthaiah, M., Suraj Saini, and S. Varunkumar. 2025. “Whistling Potential of Throttling Orifices and Its Connection to Liquid Rocket Combustion Instability.” Applied Acoustics 229: 110361. https://doi.org/10.1016/j.apacoust.2024.110361
• 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
• Myrabo, L. N., Yu. P. Raizer, M. N. Shneider, and R. Bracken. 2004. “Reduction of Drag and Energy Consumption during Energy Release Preceding a Blunt Body in Supersonic Flow.” High Temperature 42 (6): 901–10. https://doi.org/10.1007/s10740-005-0011-x
• Nadjiasngar, Roaldje, and Alexander Charlish. 2015. “A Performance Model for Target Tracking with a Radar Network.” In 2015 IEEE Radar Conference. IEEE. https://doi.org/10.1109/radarconf.2015.7411887
• Nakagawa, S., T. Yamasaki, H. Takano, and I. Yamaguchi. 2017. “Disturbance-Compensated Intercept Guidance Using Line-of-Sight Rate Information.” In 2017 11th Asian Control Conference (ASCC). IEEE. https://doi.org/10.1109/ascc.2017.8287201
• Nakamura, Toshiya, Yukihiro Kamimura, Hirotaka Igawa, and Yoshiki Morino. 2014. “Inverse Analysis for Transient Thermal Load Identification and Application to Aerodynamic Heating on Atmospheric Reentry Capsule.” Aerospace Science and Technology 38: 48–55. https://doi.org/10.1016/j.ast.2014.07.015
• Nan, Yu, Jin Ming, and Qiao Xiao-lin. 2010. “The Monopulse Angle Estimation Based on the Radon-Ambiguity Transform.” In 2010 First International Conference on Pervasive Computing, Signal Processing and Applications. IEEE. https://doi.org/10.1109/pcspa.2010.205
• Nanavati, Rohit V., Shashi Ranjan Kumar, and Arnab Maity. 2021a. “Lead-Angle-Based Three-Dimensional Guidance for Angle-Constrained Interception.” Journal of Guidance, Control, and Dynamics 44 (1): 190–99. https://doi.org/10.2514/1.g005454
• Nanavati, Rohit, Shashi Ranjan Kumar, and Arnab Maity. 2021b. “Time-Constrained Individual Homing Guidance against Stationary Targets.” In 2021 Seventh Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/icc54714.2021.9703126
• Narykov, Alexey S., Oleg A. Krasnov, and Alexander Yarovoy. 2014. “Effectiveness-Based Radar Resource Management for Target Tracking.” In 2014 International Radar Conference. IEEE. https://doi.org/10.1109/radar.2014.7060253
• Nash, Franklin R. 1990. “Making Reliability Estimates When Zero Failures Are Seen in Laboratory Aging.” MRS Proceedings 184: 3. https://doi.org/10.1557/proc-184-3
• Natori, Kenji. 2014. “Mechanical Power Factor as Performance Index of Bilateral Teleoperation Systems.” In 2014 IEEE 13th International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2014.6823377
• Naveed, Aamir, and Ali Javed. 2018. “Effects of Variation in Flow Field on Store Separation.” In 2018 15th International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast.2018.8312212
• 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
• Neelakantaswamy, Perambur S., and Arthur Rajaratram. 1982. “Boresight Error in the Conical Scan Method of Autoboresighting a Laser Beam on a Specular Point-Target.” Applied Optics 21 (19): 3607. https://doi.org/10.1364/ao.21.003607
• Neff, J., and A. Junker. 1974. “Effection of Motion on the Parameters of the Human Operator Engaged in a Roll Axis Tracking Task.” In 1974 IEEE Conference on Decision and Control including the 13th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1974.270424
• Nenadić, Ilija, and Jelena Svorcan. 2026. “Comparative Numerical Investigation of Gravitational and Impulse Store Separation in Highly Subsonic Flow.” Aerospace 13 (4): 336. https://doi.org/10.3390/aerospace13040336
• Nesbitt, M. W. 1946. “Liquid Propellant Rocket Development.” Journal of the American Rocket Society 00 (68): 1–11. https://doi.org/10.2514/8.4111
• 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. 1984. “Homing Missile Autopilot Response Sensitivity to Stability Derivative Variations.” In The 23rd IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1984.272187
• 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
• Nesline, F. William, and Paul Zarchair. 1985. “Digital Homing Guidance: Stability vs Performance Tradeoffs.” Journal of Guidance, Control, and Dynamics 8 (2): 255–61. https://doi.org/10.2514/3.19968
• Nesline, F. William, and Paul Zarchan. 1981. “A New Look at Classical vs Modern Homing Missile Guidance.” Journal of Guidance and Control 4 (1): 78–85. https://doi.org/10.2514/3.56054
• Nesline, F. William, and Paul Zarchan. 1983c. “Missile Guidance Design Tradeoffs for High-Altitude Air Defense.” Journal of Guidance, Control, and Dynamics 6 (3): 207–12. https://doi.org/10.2514/3.19817
• Nesline, F. William, and Paul Zarchan. 1985. “Line-of-Sight Reconstruction for Faster Homing Guidance.” Journal of Guidance, Control, and Dynamics 8 (1): 3–8. https://doi.org/10.2514/3.19927
• Nester, W. 1962. “A Study of Tracking Accuracy in Monopulse Phased Arrays.” IRE Transactions on Antennas and Propagation 10 (3): 237–46. https://doi.org/10.1109/tap.1962.1137873
• 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
• Neumeier, Y., and M. Hanin. 1986. “Roll Divergence of a Canard-Controlled Missile with a Freely Spinning Tail.” Journal of Guidance, Control, and Dynamics 9 (6): 633–37. https://doi.org/10.2514/3.20157
• Newman, Brett. 1996. “Strategic Intercept Midcourse Guidance Using Modified Zero Effort Miss Steering.” Journal of Guidance, Control, and Dynamics 19 (1): 107–12. https://doi.org/10.2514/3.21586
• Nguyen, Dinh-Hong, Thi-Dieu-Linh Dang, Kiem-Chien Nguyen, and Duc-Hung Bui. 2026. “LMI-Based Robust Optimal Roll Control for a Tactical Missile under Disturbances and Uncertainty.” IEEE Access 14: 142837–63. https://doi.org/10.1109/access.2026.3733117
• Nguyen, Tuan M., Pavel P. Popov, and William A. Sirignano. 2018. “Longitudinal Combustion Instability in a Rocket Engine with a Single Coaxial Injector.” Journal of Propulsion and Power 34 (2): 354–73. https://doi.org/10.2514/1.b36516
• Nguyen, Tuan M., and William A. Sirignano. 2019. “Spontaneous and Triggered Longitudinal Combustion Instability in a Single-Injector Liquid-Rocket Combustor.” AIAA Journal 57 (12): 5351–64. https://doi.org/10.2514/1.j057743
• Ni, Weilin, Jiaqi Liu, Zhi Li, Peng Liu, and Haizhao Liang. 2023. “Cooperative Guidance Strategy for Active Spacecraft Protection from a Homing Interceptor via Deep Reinforcement Learning.” Mathematics 11 (19): 4211. https://doi.org/10.3390/math11194211
• Ni, Hao, Ying Xin, Chaozhen Liu, Hao Xie, and Ningyu He. 2025a. “Composite Guidance Law Based on PPF and Fixed-Time Observer with Impact Angle Constraint.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11487672
• Nicholls, L. A. 1975. “Use of Zero Counting for Estimating the Zero-Frequency Spectral Density of Radar Glint for Known Target Types.” IEEE Transactions on Aerospace and Electronic Systems AES-11 (4): 644–47. https://doi.org/10.1109/taes.1975.308131
• Nichols, Robert H., and Shawn Westmoreland. 2007. “Comparison of Computational Fluid Dynamics Approaches for Simulating Weapons Bay Flow.” Journal of Aircraft 44 (3): 1019–24. https://doi.org/10.2514/1.23067
• Nickel, U. n.d.-a. “Generalised Monopulse Estimation and Its Performance.” In Proceedings of the 3rd IEEE International Symposium on Signal Processing and Information Technology (IEEE Cat. No.03EX795). IEEE. https://doi.org/10.1109/isspit.2003.1341088
• Nickel, U. R. O. n.d.-b. “Monopulse Estimation with Subarray Output Adaptive Beamforming and Low Sidelobe Sum and Difference Beams.” In Proceedings of International Symposium on Phased Array Systems and Technology. IEEE. https://doi.org/10.1109/past.1996.566100
• Nickel, U. 2006. “Overview of Generalized Monopulse Estimation.” IEEE Aerospace and Electronic Systems Magazine 21 (6): 27–56. https://doi.org/10.1109/maes.2006.1662039
• Nickel, Ulrich R. O., Eric Chaumette, and Pascal Larzabal. 2011. “Monopulse Estimation of Swerling I–II Extended Targets.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159583
• Nicolas Marcassus. 2006. “Theoretical and Experimental Overview of Bilateral Teleoperation Control Laws.” In 2006 14th Mediterranean Conference on Control and Automation. IEEE. https://doi.org/10.1109/med.2006.236964
• Nie, Haisheng, Yanyu Lu, Chunhui Wang, Genke Yang, and Shan Fu. 2019. “The Relationship between Emotion State and Human Performance in the Teleoperation Task.” In 2019 IEEE 15th International Conference on Control and Automation (ICCA). IEEE. https://doi.org/10.1109/icca.2019.8899948
• Nie, Shunchen, Li Yu, Yanjun Li, Zhihong Sun, and Bowen Qiu. 2023a. “Fluid Structure Interaction of Supersonic Parachute with Material Failure.” Chinese Journal of Aeronautics 36 (10): 90–100. https://doi.org/10.1016/j.cja.2023.06.026
• Nielsen, R. O. 2001. “Accuracy of Angle Estimation with Monopulse Processing Using Two Beams.” IEEE Transactions on Aerospace and Electronic Systems 37 (4): 1419–23. https://doi.org/10.1109/7.976976
• Niemeyer, Gunter, and Jean-Jacques E. Slotine. 1990. “Stable Adaptive Teleoperation.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4790931
• Ning, Hongru, and Yongzhi Sheng. 2023. “Three-Dimensional Cooperative Guidance Law with Impact Angle Constrained Based on Fixed-Time Convergent Error Dynamics.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10451561
• Niu, Liqiang, Yongjun Xie, Peiyu Wu, and Chungang Zhang. 2020. “ARCS: Active Radar Cross Section for Multi-Radiator Problems in Complex EM Environments.” Sensors 20 (12): 3371. https://doi.org/10.3390/s20123371
• No, Tae Soo, John E. Cochran, and Eul Gon Kim. 2001. “Bank-to-Turn Guidance Law Using Lyapunov Function and Nonzero Effort Miss.” Journal of Guidance, Control, and Dynamics 24 (2): 255–60. https://doi.org/10.2514/2.4736
• Nomberg, Reut, and Ilana Nisky. 2023. “Human-in-the-Loop Stability Analysis of Haptic Rendering with Time Delay – the Effect of Delayed Feedback Control in the Operator Model.” IEEE Robotics and Automation Letters 8 (10): 6379–86. https://doi.org/10.1109/lra.2023.3301773
• North, J. D., and Z. A. Lomnicki. 1961. “Further Experiments on Human Operators in Compensatory Tracking Tasks.” Ergonomics 4 (4): 339–53. https://doi.org/10.1080/00140136108930535
• Nugroho, Gesang, Yarabisa Yanuar, and Praberta Ardi Wibowo. 2019. “Flight Test of Pasopati Electrical Cruise Missile.” In 2019 International Conference on Advanced Mechatronics, Intelligent Manufacture and Industrial Automation (ICAMIMIA). IEEE. https://doi.org/10.1109/icamimia47173.2019.9223373
• Nusca, M., C.-C. Chen, and M. McQuaid. 2007. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2007 DoD High Performance Computing Modernization Program Users Group Conference. IEEE. https://doi.org/10.1109/hpcmp-ugc.2007.17
• Nusca, Michael J., Chiung-Chu Chen, and Michael J. McQuaid. 2008. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2008 DoD HPCMP Users Group Conference. IEEE. https://doi.org/10.1109/dod.hpcmp.ugc.2008.28
• Nusca, Michael J., Chiung-Chu Chen, and Michael J. McQuaid. 2010. “Modeling the Combustion Chamber Dynamics of Selectable-Thrust Rocket Motors.” In 2010 DoD High Performance Computing Modernization Program Users Group Conference. IEEE. https://doi.org/10.1109/hpcmp-ugc.2010.37
• Nusca, M. J., and M. J. McQuaid. 2004. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2004 Users Group Conference (DOD_UGC’04). IEEE. https://doi.org/10.1109/dod_ugc.2004.8
• Nusca, M. J., and M. J. McQuaid. 2005. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2005 Users Group Conference (DOD-UGC’05). IEEE. https://doi.org/10.1109/dodugc.2005.20
• Nusca, Michael J., and Michael J. McQuaid. 2006. “Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines.” In 2006 HPCMP Users Group Conference (HPCMP-UGC’06). IEEE. https://doi.org/10.1109/hpcmp-ugc.2006.14
• O’Connor, Daniel. 2019. “Early Days of Phased Array Radars for Ballistic Missile Detection and Tracking.” In 2019 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar41533.2019.171388
• O’Farrell, Clara, Chris Karlgaard, Jake A. Tynis, and Ian G. Clark. 2018. “Overview and Reconstruction of the ASPIRE Project’s SR01 Supersonic Parachute Test.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396502
• Obi, Victor, Grant Evans, and Sungkyun Lim. 2022. “Design of a Miniaturized, High Gain, Anti-Jam Global Positioning System (GPS) Antenna.” In SoutheastCon 2022. IEEE. https://doi.org/10.1109/southeastcon48659.2022.9764029
• Obšilová, L., M. Havlíková, and Z. Bradáč. 2016. “Human Operator Neuromuscular Actuation System Model.” IFAC-PapersOnLine 49 (25): 260–65. https://doi.org/10.1016/j.ifacol.2016.12.044
• 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
• Oehler, Martin, and Oskar von Stryk. 2021. “A Flexible Framework for Virtual Omnidirectional Vision to Improve Operator Situation Awareness.” In 2021 European Conference on Mobile Robots (ECMR). IEEE. https://doi.org/10.1109/ecmr50962.2021.9568840
• Ohrenberger, John T., and Eric Baum. 1972. “A Theoretical Model of the near Wake of a Slender Body in Supersonic Flow.” AIAA Journal 10 (9): 1165–72. https://doi.org/10.2514/3.50344
• Omata, Noriyasu, Daiwa Satoh, Seiji Tsutsumi, Kaname Kawatsu, and Masaharu Abe. 2022. “Model-Based Supervised Sensor Placement Optimization to Detect Propellant Leak in a Liquid Rocket Engine.” Acta Astronautica 195: 234–42. https://doi.org/10.1016/j.actaastro.2022.02.009
• Omori, Satoaki. 1973b. “Eddy Viscosity Calculation along the Chemical Rocket Thrust Chamber Wall Using Turbulent Kinetic Energy.” Combustion Science and Technology 7 (6): 229–40. https://doi.org/10.1080/00102207308952363
• Ong, Shaw Y., and Bion L. Pierson. 1996. “Optimal Planar Evasive Aircraft Maneuvers against Proportional Navigation Missiles.” Journal of Guidance, Control, and Dynamics 19 (6): 1210–15. https://doi.org/10.2514/3.21773
• Onnasch, Linda. 2015. “Crossing the Boundaries of Automation—Function Allocation and Reliability.” International Journal of Human-Computer Studies 76: 12–21. https://doi.org/10.1016/j.ijhcs.2014.12.004
• 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
• Oppenheimer, M. W., and D. B. Doman. 2006. “Control of an Unstable, Nonminimum Phase Hypersonic Vehicle Model.” In 2006 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2006.1655985
• “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
• Or, Barak, Joseph Z. Ben-Asher, and Isaac Yaesh. 2021. “Optimal Disturbance Attenuation Approach with Measurement Feedback to Missile Guidance.” Journal of Guidance, Control, and Dynamics 44 (5): 1080–86. https://doi.org/10.2514/1.g005468
• Oshman, Yaakov, and David Arad. 2004. “Enhanced Air-to-Air Missile Tracking Using Target Orientation Observations.” Journal of Guidance, Control, and Dynamics 27 (4): 595–606. https://doi.org/10.2514/1.11155
• Ostrovityanov, R. V. 1990. “Angular Glint in Polarization Agility Systems.” In International Symposium on Antennas and Propagation Society, Merging Technologies for the 90’s. IEEE. https://doi.org/10.1109/aps.1990.115425
• Otsubo, Kaito, and Kazuhiro Honda. 2023. “A Method for Resolving the Phase Difference Ambiguity in Interferometric Monopulse Angle of Arrival Estimation.” IEICE Communications Express 12 (3): 102–7. https://doi.org/10.1587/comex.2022xbl0183
• 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, Hongyang, and Yang Zhang. 2026. “Effect of Forebody Shape and Trailing Distance on the Inflation Performance of a Supersonic Disk-Gap-Band Parachute.” Aerospace Science and Technology 168: 110828. https://doi.org/10.1016/j.ast.2025.110828
• Ouyang, Hongyang, Yang Zhang, and Zhaoxu Lian. 2026. “Numerical Investigation on the Inflation Dynamics of a Supersonic Parachute Cluster.” Aerospace Science and Technology 178: 112419. https://doi.org/10.1016/j.ast.2026.112419
• Owen, F. K., and B. J. Bellhouse. 1970. “Skin-Friction Measurement at Supersonic Speeds.” AIAA Journal 8 (7): 1358–60. https://doi.org/10.2514/3.5904
• Oza, Harshal B., and Radhakant Padhi. 2012. “Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles.” Journal of Guidance, Control, and Dynamics 35 (1): 153–64. https://doi.org/10.2514/1.53647
• Özkan, Bülent, M. Kemal Özgören, and Gökmen Mahmutyazicioğlu. 2011. “Comparison of the Notable Acceleration- and Angle-Based Guidance Laws for a Short-Range Air-to-Surface Missile.” IFAC Proceedings Volumes 44 (1): 3527–32. https://doi.org/10.3182/20110828-6-it-1002.01093
• Özkan, Bülent, M. Kemal Özgören, and Gökmen Mahmutyazιcιoğlu. 2008. “Implementation of Linear Homing Guidance Law on a Two-Part Homing Missile.” IFAC Proceedings Volumes 41 (2): 13999–14004. https://doi.org/10.3182/20080706-5-kr-1001.02370
• Özkan, Bülent, and Mehmet Turan Söylemez. 2023. “Investigation of the Performance Characteristics of the Angle-Based Proportional Navigation Guidance Law.” IFAC-PapersOnLine 56 (2): 7020–25. https://doi.org/10.1016/j.ifacol.2023.10.612
• Pace, Henry, and Luca Massa. 2026. “Effect of Regressing Walls and Skin Friction on Supersonic Solid Fuel Combustion.” Journal of Propulsion and Power 42 (2): 176–92. https://doi.org/10.2514/1.b40147
• Pacheco-Gutierrez, Salvador, Hanlin Niu, Ipek Caliskanelli, and Robert Skilton. 2021. “A Multiple Level-of-Detail 3D Data Transmission Approach for Low-Latency Remote Visualisation in Teleoperation Tasks.” Robotics 10 (3): 89. https://doi.org/10.3390/robotics10030089
• Pachter, Meir, and Gano B. Chatterji. 1990. “An Integrated Approach for Homing Guidance of Space Based Interceptors.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4791242
• 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
• 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, Bing, Dafang Wu, and Yong Xia. 2010. “High-Temperature Deformation Field Measurement by Combining Transient Aerodynamic Heating Simulation System and Reliability-Guided Digital Image Correlation.” Optics and Lasers in Engineering 48 (9): 841–48. https://doi.org/10.1016/j.optlaseng.2010.04.007
• Parayil, Anjaly, and Ashwini Ratnoo. 2018. “Cooperative Beam-Rider Guidance for Unmanned Aerial Vehicle Rendezvous.” Journal of Intelligent & Robotic Systems 95 (2): 585–99. https://doi.org/10.1007/s10846-018-0873-x
• Park, Gary D., and Mike H. Abla. 1983. “Determination of Horizontal Tail Load and Hinge Moment Characteristics from Flight Data.” Journal of Guidance, Control, and Dynamics 6 (3): 170–75. https://doi.org/10.2514/3.19811
• Park, Soon-Young, and Jaemyung Ahn. 2020. “Deep Neural Network Approach for Fault Detection and Diagnosis during Startup Transient of Liquid-Propellant Rocket Engine.” Acta Astronautica 177: 714–30. https://doi.org/10.1016/j.actaastro.2020.08.019
• Park, Bong-Gyun, and Tae-Hun Kim. 2026. “Composite Guidance Law for Air-to-Ground Missiles Considering Fiber-Optic Line and Look Angle Constraints.” Aerospace 13 (10): 919. https://doi.org/10.3390/aerospace13100919
• Park, Bong-Gyun, Tae-Hun Kim, and Min-Jea Tahk. 2016b. “Range-to-Go Weighted Optimal Guidance with Impact Angle Constraint and Seeker’s Look Angle Limits.” IEEE Transactions on Aerospace and Electronic Systems 52 (3): 1241–56. https://doi.org/10.1109/taes.2016.150415
• 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
• Parkinson, R. C., V. A. Skorodelov, I. I. Serdijk, and V. Ya. Neiland. 1995. “RADEM: An Air Launched, Rocket Demonstrator for Future Advanced Launch Systems.” Acta Astronautica 37: 215–22. https://doi.org/10.1016/0094-5765(95)00089-i
• Parks, P. C. 1962. “Pitch-Yaw Stability of a Missile Oscillating in Roll via the Second Method of Lyapunov.” Journal of the Aerospace Sciences 29 (7): 874–874. https://doi.org/10.2514/8.9621
• Patel, Vikas, and H. Madhukar. 2021. “Beam Steering and Beam Stabilization of Active Electronically Scanned Array (AESA) Seeker for Missile Guidance.” In 2021 International Conference on Control, Automation, Power and Signal Processing (CAPS). IEEE. https://doi.org/10.1109/caps52117.2021.9730685
• Pavic, Milos, Slobodan Mandic, Danilo Cuk, and Bojan Pavkovic. 2014. “A New Type of Flight Simulator for Manual Command to Line-of-Sight Guided Missile.” Optik 125 (21): 6579–85. https://doi.org/10.1016/j.ijleo.2014.06.163
• 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
• Peebles, Peyton Z., and T.k. Wang. 1982. “Noise Angle Accuracy of Several Monopulse Architectures.” IEEE Transactions on Aerospace and Electronic Systems AES-18 (6): 712–21. https://doi.org/10.1109/taes.1982.309290
• Pehlivan, Mustafa, and Korkut Yegin. 2021. “X-Band Low-Probability Intercept Marine Radar Antenna Design with Improved Bandwidth and High Isolation.” IEEE Transactions on Antennas and Propagation 69 (12): 8949–54. https://doi.org/10.1109/tap.2021.3096952
• Peilin Sun, Qian Cai, Jun Tang, Ning Li, and Jinsong Du. 2011. “On Spreading Chaff Cloud for Countering the Terminal Guidance Missile.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159673
• Peled-Eitan, Liat, and Ilan Rusnak. 2019. “Optimal Radar Tracking in Cartesian Coordinates with Range, Doppler and Angle Measurements.” In 2019 27th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med.2019.8798503
• Peng, Weishi, YangWang Fang, Renjun Zhan, and Weijia Wang. 2016. “Weapon Systems Accuracy Evaluation Using the Error Spectrum.” Aerospace Science and Technology 58: 369–79. https://doi.org/10.1016/j.ast.2016.08.032
• 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, Siting, Yuan Liang, Hong Jiang, Qingdong Li, Xiwang Dong, and Zhang Ren. 2018. “Application of an Adaptive Cubature Kalman Filter in Target Tracking Model of Infrared Semi-Strapdown Seeker.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018685
• Peng Liu, Liu Yan, Feng Xue, and Jiaqi Liu. 2017. “Study on the Effect of the Modeling and Filtering Error Sources on Guidance Laws of Missile Navigation.” In 2017 6th International Conference on Industrial Technology and Management (ICITM). IEEE. https://doi.org/10.1109/icitm.2017.7917912
• Pengyuan, Liu, Jiang Xiong, and Zhang Wangwei. 2014. “WTA Model Study of Air Defense Missile System Based on Particle Algorithm.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007420
• Penner, S. S., and P. P. Datner. 1955. “Combustion Problems in Liquid-Fuel Rocket Engines.” Symposium (International) on Combustion 5 (1): 11–29. https://doi.org/10.1016/s0082-0784(55)80009-4
• Pepitone, Thomas R., and Ira D. Jacobson. 1978. “Resonant Behavior of a Symmetric Missile Having Roll Orientation-Dependent Aerodynamics.” Journal of Guidance and Control 1 (5): 335–39. https://doi.org/10.2514/3.55789
• Pepper, William B. 1967. “A 20-Ft-Diam Ribbon Parachute for Deployment at Dynamic Pressures above 400 Psf.” Journal of Aircraft 4 (3): 265–67. https://doi.org/10.2514/3.43831
• Pepper, William B., and Dennis C. Cronin. 1969. “Experimental Research on Parachute Deployment Load Control by Use Ofline Ties.” Journal of Aircraft 6 (1): 79–80. https://doi.org/10.2514/3.44012
• Perelman, Andrey, Tal Shima, and Ilan Rusnak. 2011. “Cooperative Differential Games Strategies for Active Aircraft Protection from a Homing Missile.” Journal of Guidance, Control, and Dynamics 34 (3): 761–73. https://doi.org/10.2514/1.51611
• Peri, Lakshmi Narayana Phaneendra, Antonella Ingenito, and Paolo Teofilatto. 2024. “Large-Eddy Simulations of a Hypersonic Re-Entry Capsule Coupled with the Supersonic Disk-Gap-Band Parachute.” Aerospace 11 (1): 94. https://doi.org/10.3390/aerospace11010094
• Petousakis, Giannis, Manolis Chiou, Grigoris Nikolaou, and Rustam Stolkin. 2020. “Human Operator Cognitive Availability Aware Mixed-Initiative Control.” In 2020 IEEE International Conference on Human-Machine Systems (ICHMS). IEEE. https://doi.org/10.1109/ichms49158.2020.9209582
• Pfleghaar, Wolfgang. 1985. “The General Class of Optimal Proportional Navigation.” Journal of Guidance, Control, and Dynamics 8 (1): 144–47. https://doi.org/10.2514/3.19947
• Pham, Trung-Dung, Qui Tran, and Duc-Vuong Vu. 2012. “Fuzzy Guidance Law for Surface-to-Air Missile in the Command Control Systems.” In 2012 International Conference on Control, Automation and Information Sciences (ICCAIS). IEEE. https://doi.org/10.1109/iccais.2012.6466610
• Phillips, Craig. 1995. “Terminal Homing Performance of Semiactive Missiles against Multitarget Raids.” Journal of Guidance, Control, and Dynamics 18 (6): 1427–33. https://doi.org/10.2514/3.21564
• Pin-Jar Yuan. 1997. “Optimal Guidance of Proportional Navigation.” IEEE Transactions on Aerospace and Electronic Systems 33 (3): 1007–12. https://doi.org/10.1109/7.599325
• Ping, Sun, Du Yanli, Zhang Peng, and Xiang Kai. 2017. “The Nonlinear Anti-Windup Control of Hypersonic Glide Vehicles with Input Saturation and Uncertainties.” In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2017.7979315
• Ping Li, Wanchun Chen, and Hao Zhou. 2010. “Quasi-Equilibrium Glide Trajectory Design of Waverider-Based Hypersonic Vehicle.” In 2010 International Conference on Mechanical and Electrical Technology. IEEE. https://doi.org/10.1109/icmet.2010.5598391
• 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
• Platzer, Max F., and Gilbert H. Hoffman. 1966. “Supersonic Quasi-Slender Body Theory for Slowly Oscillating Bodies.” AIAA Journal 4 (9): 1693–94. https://doi.org/10.2514/3.3763
• PlEPER, J. L., L. E. Dean, and R. S. Valentine. 1967. “Mixture Ratio Distribution: Its Impact on Rocket Thrust Chamber Performance.” Journal of Spacecraft and Rockets 4 (6): 786–89. https://doi.org/10.2514/3.28952
• Po-Hsu Huang, Ting-Kuo Wang, and Li-Chen Fu. 2010. “A Sliding-Mode Based Guidance Law for Intercepting Missile with Passive Ranging Law.” In Proceedings of the 2010 American Control Conference. IEEE. https://doi.org/10.1109/acc.2010.5531441
• Poberezhskiy, Y. S., and G. Y. Poberezhskiy. 2013. “On Adaptive Robustness Approach to Anti-Jam Signal Processing.” In 2013 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2013.6496827
• 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
• Poehler, H. A. 1961. “Plasma-Enhanced Breakdown of Telemetry Antennas during Ballistic Missile Powered Flight.” IRE Transactions on Space Electronics and Telemetry SET-7 (4): 90–95. https://doi.org/10.1109/iret-set.1961.5008780
• Pontani, Mauro, and Bruce A. Conway. 2008. “Optimal Interception of Evasive Missile Warheads: Numerical Solution of the Differential Game.” Journal of Guidance, Control, and Dynamics 31 (4): 1111–22. https://doi.org/10.2514/1.30893
• Popov, Pavel P., William A. Sirignano, and Athanasios Sideris. 2015. “Propellant Injector Influence on Liquid-Propellant Rocket Engine Instability.” Journal of Propulsion and Power 31 (1): 320–31. https://doi.org/10.2514/1.b35400
• Potter, J. J., and W. E. Singhose. 2012. “Effects of Input Shaping on Manual Tracking with Oscillatory Controlled-Element Dynamics.” In 2012 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2012.6315556
• Potter, James Jackson, and William Singhose. 2013. “Improving Manual Tracking of Systems with Oscillatory Dynamics.” IEEE Transactions on Human-Machine Systems 43 (1): 46–52. https://doi.org/10.1109/tsmca.2012.2214031
• Prakash, Jai, Michele Vignati, Edoardo Sabbioni, and Federico Cheli. 2022. “Vehicle Teleoperation: Successive Reference-Pose Tracking to Improve Path Tracking and to Reduce Time-Delay Induced Instability.” In 2022 IEEE Vehicle Power and Propulsion Conference (VPPC). IEEE. https://doi.org/10.1109/vppc55846.2022.10003367
• Prasanna, H. M., and D. Ghose. 2012. “Retro-Proportional-Navigation: A New Guidance Law for Interception of High Speed Targets.” Journal of Guidance, Control, and Dynamics 35 (2): 377–86. https://doi.org/10.2514/1.54892
• Pratama, Tommy, Rusdhianto Ea Kadir, and Zulkifli Hidayat. 2019. “Model Prediction Control for Missile Autopilot and Navigation.” In 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia (CENIM). IEEE. https://doi.org/10.1109/cenim48368.2019.8973362
• Prempain, E., I. Postlethwaite, and Dave Vorley. 2001. “A Gain Scheduled Autopilot Design for a Bank-to-Turn Missile.” In 2001 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2001.7076224
• Price, E. W. 1965. “Experimental Solid Rocket Combustion Instability.” Symposium (International) on Combustion 10 (1): 1067–82. https://doi.org/10.1016/s0082-0784(65)80247-8
• Price, H. G. 1981. “Cooling of High-Pressure Rocket Thrust Chambers with Liquid Oxygen.” Journal of Spacecraft and Rockets 18 (4): 338–43. https://doi.org/10.2514/3.57826
• 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
• Pritz, Capt. W. L., and R. J. Schoner. 1973. “Verification of a Comprehensive Thrust Chamber Compatibility Model for Liquid Rocket Engines.” Journal of Spacecraft and Rockets 10 (9): 558–63. https://doi.org/10.2514/3.61926
• 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
• 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
• Pulliam, W., M. Jones, J. A. Schetz, and K. Murphy. n.d. “Fiber Optic Pressure/skin Friction Gage for Supersonic Flow Applications.” In ICIASF’97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities. IEEE. https://doi.org/10.1109/iciasf.1997.644753
• Purvis, James W. 1983. “Prediction of Parachute Line Sail during Lines-First Deployment.” Journal of Aircraft 20 (11): 940–45. https://doi.org/10.2514/3.56727
• Qi, Feng. 1995. “Regenerative Cooling for Liquid Rocket Engines.” Journal of Thermal Science 4 (1): 54–58. https://doi.org/10.1007/bf02653165
• Qi, Yuanjie, Yuqiang Cheng, and Zhenzhen Zhang. 2021. “Life Prediction and Damage Calculation of Reusable Liquid Rocket Engine Thrust Chamber.” In 2021 3rd International Symposium on Robotics & Intelligent Manufacturing Technology (ISRIMT). IEEE. https://doi.org/10.1109/isrimt53730.2021.9596851
• Qi, Yuanjie, Yuqiang Cheng, and Yan Zhang. 2022. “Life Analysis of Reusable Liquid Rocket Engine Thrust Chamber.” Aerospace 9 (12): 788. https://doi.org/10.3390/aerospace9120788
• 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, Qiang, Dianzong Yang, Taideng Zhan, Danpeng Huang, Lei Tian, and Jianjun Ma. 2025. “Predefined-Time Sliding Mode Guidance Law for Active Defense with Safe Distance.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11486925
• Qian, Muhua, and Donghe Chen. 2025. “Impact-Angle-Constrained Guidance via Virtual Targets for Large Initial Heading Errors.” IEEE Access 13: 197985–95. https://doi.org/10.1109/access.2025.3634607
• Qian, Shaoke, Sheng Huang, Xinbo Song, and Wei Zhang. 2019. “Zero Miss Distance of 3D PPNG with Time-Varying Speed.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865375
• Qianchen, Yuan, Zhang Qingzhen, and Zhang Huiping. 2011. “A Compound Control System of Axial Moving Mass and Aerodynamic Force for Mass Moment Missile.” In 2011 First International Conference on Instrumentation, Measurement, Computer, Communication and Control. IEEE. https://doi.org/10.1109/imccc.2011.238
• Qiao, Yupeng, and Daizhan Cheng. 2006. “Attitude Control of Missile with Time-Delay.” In 2006 Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2006.280966
• Qiao, Haiyan, Meng Liu, Hao Meng, Mengjun Wang, and Wei Ke. 2019. “Improved Multistage in-Motion Attitude Determination Alignment Method for Strapdown Inertial Navigation System.” Sensors 19 (20): 4568. https://doi.org/10.3390/s19204568
• Qiao Xiaolin and Jin Ming. 2001. “Angular Glint Suppression for Mm-Wave Terminal Guidance Radar Based on Polarization Agility and RCS Weighting.” In Proceedings of the 2001 IEEE Radar Conference (Cat. No.01CH37200). IEEE. https://doi.org/10.1109/nrc.2001.923014
• Qiao Yongjie, Liu Jinrong, Bai Liping, Ding Hong, and Li Xiangru. 2011b. “Detection Probability of Early Warning Radar against Hypersonic Cruise Missile.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159904
• Qiao Yongjie, Liu Jinrong, Ding Hong, Xu Zhongfu, and Wei Heng. 2011a. “Detection Ability Modeling of Balloon-Borne Radar against Cruise Missile.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159809
• Qin, Zhen, Xiaoye Qi, and Yongling Fu. 2019. “Terminal Guidance Based on Bézier Curve for Climb-and-Dive Maneuvering Trajectory with Impact Angle Constraint.” IEEE Access 7: 2969–77. https://doi.org/10.1109/access.2018.2883405
• Qingbiao Xi, Dongli Yuan, and Jianguo Yan. n.d. “The Application of Feedback Linearized Guidance Law in the Homing Guidance of the Aerocraft.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 1. IEEE. https://doi.org/10.1109/wcica.2004.1340713
• Qingzhan Shi, Deping Zhang, Kelei Wei, and Naichang Yuan. 2016. “An Improved Method of Data Alignment for Angle Measurement in Monopulse Radar.” In 2016 Progress in Electromagnetic Research Symposium (PIERS). IEEE. https://doi.org/10.1109/piers.2016.7734913
• Qiu, Zhijie, Wei Dai, and Gaozhi Guan. 2021. “Research on Stall Recovery Parachute Flight Deployment Tests.” In 2021 International Symposium on Computer Science and Intelligent Controls (ISCSIC). IEEE. https://doi.org/10.1109/iscsic54682.2021.00016
• 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
• Quattrocchi, Gaetano, Pier C. Berri, Matteo D. L. Dalla Vedova, and Paolo Maggiore. 2022. “An Improved Fault Identification Method for Electromechanical Actuators.” Aerospace 9 (7): 341. https://doi.org/10.3390/aerospace9070341
• Rabbath, C. A., Nicolas Lechevin, and Noriyuki Hori. 2004. “Optimal Dual-Rate Digital Redesign with Application to Missile Control.” Journal of Guidance, Control, and Dynamics 27 (6): 1083–87. https://doi.org/10.2514/1.6399
• Radomski, Marek. 1995. “Kill Probability in Antiaircraft Firing Theory.” Journal of Aircraft 32 (6): 1396–99. https://doi.org/10.2514/3.56927
• Rafique, Amer Farhan, He LinShu, Ali Kamran, and Qasim Zeeshan. 2010a. “Multidisciplinary Design of Air Launched Satellite Launch Vehicle: Performance Comparison of Heuristic Optimization Methods.” Acta Astronautica 67 (7–8): 826–44. https://doi.org/10.1016/j.actaastro.2010.05.016
• Rahbar, N., and M. B. Menhaj. 2000. “Fuzzy-Logic-Based Closed-Loop Optimal Law for Homing Missiles Guidance.” Journal of Guidance, Control, and Dynamics 23 (3): 573–74. https://doi.org/10.2514/2.4572
• Raj, K. David Solomon, and I. Sri Satya Ganesh. 2015. “Estimation of Line-of-Sight Rate in a Homing Missile Guidance Loop Using Optimal Filters.” In 2015 International Conference on Communications and Signal Processing (ICCSP). IEEE. https://doi.org/10.1109/iccsp.2015.7322916
• Rajasekhar, V., and A. G. Sreenatha. 2000. “Fuzzy Logic Implementation of Proportional Navigation Guidance.” Acta Astronautica 46 (1): 17–24. https://doi.org/10.1016/s0094-5765(99)00189-7
• Raju, B. Basava, Ramesh Chandra, and M. Subba Rao. 1978. “Transient Temperatures in Laminated Composite Conical Shells Due to Aerodynamic Heating.” AIAA Journal 16 (6): 547–48. https://doi.org/10.2514/3.60929
• “RAM Growth of the PATRIOT Missile System.” 1987. Microelectronics Reliability 27 (6): 1035. https://doi.org/10.1016/0026-2714(87)90839-0
• Ramakrishnan, S., and Binay K. Sarkar. 2006. “Performance Comparison of Spherical and Elliptical Earth Models for Low Angle Tracking in Radars.” In 2006 International Radar Symposium. IEEE. https://doi.org/10.1109/irs.2006.4338078
• Ramamurthi, K., and A. Jayashree. 1992. “Optimization of Mixture Ratio Distribution in Liquid Propellant Rocket Thrust Chamber.” Journal of Propulsion and Power 8 (3): 605–8. https://doi.org/10.2514/3.23521
• Ramesh, D., Arnab Maity, A. K. Sarkar, and J. Umakant. 2019. “Fixed Final Time Field of View and Impact Angle Constrained Guidance.” In 2019 27th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med.2019.8798534
• Ranajit, Das, Majumder Santanu Bijoy, and R. N. Bhattacherjee. 2014. “Gimbal Angle Constrained PN Guidance Law.” IFAC Proceedings Volumes 47 (1): 1–6. https://doi.org/10.3182/20140313-3-in-3024.00076
• Rao, M. N. 1993. “New Analytical Solutions for Proportional Navigation.” Journal of Guidance, Control, and Dynamics 16 (3): 591–94. https://doi.org/10.2514/3.21051
• Rao, S. K. 1998. “Comments on ‘Optimal Guidance of Proportional Navigation’.” IEEE Transactions on Aerospace and Electronic Systems 34 (3): 981–82. https://doi.org/10.1109/7.705907
• Rao, Sachit, and Debasish Ghose. 2012. “Sliding Mode Control Based Terminal Impact Angle Constrained Guidance Laws Using Dual Sliding Surfaces.” In 2012 12th International Workshop on Variable Structure Systems. IEEE. https://doi.org/10.1109/vss.2012.6163523
• Rao, Sachit, and Debasish Ghose. 2013. “Terminal Impact Angle Constrained Guidance Laws Using Variable Structure Systems Theory.” IEEE Transactions on Control Systems Technology 21 (6): 2350–59. https://doi.org/10.1109/tcst.2013.2276476
• Rao, Ning, Hua Xu, Yue Zhang, Dan Wang, Lei Jiang, and Xiang Peng. 2022. “Joint Optimization of Jamming Link and Power Control in Communication Countermeasures: A Multiagent Deep Reinforcement Learning Approach.” Wireless Communications and Mobile Computing 2022 (1): 7962686. https://doi.org/10.1155/2022/7962686
• 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
• Rašuo, Boško, Nenad Vidanović, Gordana Kastratović, and Nikola Mirkov. 2021. “Aerodynamic-Thermal/structural Design Optimization of Missile Fin Configuration during Supersonic Flight Condition.” PAMM 20 (1): e202000220. https://doi.org/10.1002/pamm.202000220
• 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
• Ratliff, Ryan T., and Prabhakar R. Pagilla. 2008. “Fault Tolerant Robust Flight Control Using Surface Actuator Hinge Moments.” In 2008 American Control Conference. IEEE. https://doi.org/10.1109/acc.2008.4586722
• Ratnoo, Ashwini. 2016. “Analysis of Two-Stage Proportional Navigation with Heading Constraints.” Journal of Guidance, Control, and Dynamics 39 (1): 197–200. https://doi.org/10.2514/1.g001533
• Ratnoo, Ashwini, and Debasish Ghose. 2008a. “Impact Angle Constrained Interception of Stationary Targets.” Journal of Guidance, Control, and Dynamics 31 (6): 1817–22. https://doi.org/10.2514/1.37864
• Ratnoo, Ashwini, and Debasish Ghose. 2009b. “State-Dependent Riccati-Equation-Based Guidance Law for Impact-Angle-Constrained Trajectories.” Journal of Guidance, Control, and Dynamics 32 (1): 320–26. https://doi.org/10.2514/1.37876
• Ratnoo, Ashwini, and Debasish Ghose. 2010. “Impact Angle Constrained Guidance against Nonstationary Nonmaneuvering Targets.” Journal of Guidance, Control, and Dynamics 33 (1): 269–75. https://doi.org/10.2514/1.45026
• Ratnoo, Ashwini, and Debasish Ghose. 2012. “Kill-Band-Based Lateral Impact Guidance without Line-of-Sight Rate Information.” Journal of Guidance, Control, and Dynamics 35 (6): 1740–50. https://doi.org/10.2514/1.57074
• Ratnoo, Ashwini, and Tal Shima. 2011. “Line-of-Sight Interceptor Guidance for Defending an Aircraft.” Journal of Guidance, Control, and Dynamics 34 (2): 522–32. https://doi.org/10.2514/1.50572
• Ratwani, Raj M., J. Malcolm McCurry, and J. Gregory Trafton. 2010. “Single Operator, Multiple Robots: An Eye Movement Based Theoretic Model of Operator Situation Awareness.” In 2010 5th ACM/IEEE International Conference on Human-Robot Interaction (HRI). IEEE. https://doi.org/10.1109/hri.2010.5453191
• 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
• 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
• Rawling, A. G. 1969. “On Nonzero Miss Distance.” Journal of Spacecraft and Rockets 6 (1): 81–83. https://doi.org/10.2514/3.29539
• Reardon, Frederick H. 1997. “Liquid Rocket Engine Combustion Instability.” Combustion and Flame 109 (3): 501–3. https://doi.org/10.1016/s0010-2180(96)00180-0
• Reardon, F. H., L. Crocco, and D. T. Harrje. 1964. “Velocity Effects in Transverse Mode Liquid Propellant Rocket Combustion Instability.” AIAA Journal 2 (9): 1631–41. https://doi.org/10.2514/3.2631
• Reda, Daniel C., Francis C. Ketter, and Chien Fan. 1975. “Compressible Turbulent Skin Friction on Rough and Rough/ Wavy Walls.” AIAA Journal 13 (5): 553–54. https://doi.org/10.2514/3.49761
• Reed, J. F., and W. H. Curry. 1969. “A Comparison between Transonic Wind-Tunnel and Full-Scale Store Separation Characteristics.” Journal of Aircraft 6 (3): 281–83. https://doi.org/10.2514/3.44050
• Rehman, Muhammad Haris, Sajjad Asghar, Muhammad Abid, and Abdul Qayyum Khan. 2024. “Guidance and Control of a Spinning 155mm Artillery Shell Using Vector Form of Proportional Navigation Guidance.” In 2024 21st International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast61650.2024.10877193
• Reisner, Daniel, and Tal Shima. 2013. “Optimal Guidance-to-Collision Law for an Accelerating Exoatmospheric Interceptor Missile.” Journal of Guidance, Control, and Dynamics 36 (6): 1695–1708. https://doi.org/10.2514/1.61258
• “Reliability Demonstration Test and OC Curves for Attribute Data.” 1991. Microelectronics Reliability 31 (5): 1046. https://doi.org/10.1016/0026-2714(91)90111-j
• 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, Jinglei, Changping Wang, Zhenya Wang, and Feng Fang. 2024b. “Finite-Time Convergence Guidance Law with Impact Angle Constraint in Active Aircraft Defense.” In 2024 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac63892.2024.10864686
• Ren, Bin, Honglun Wang, and Tiancai Wu. 2025. “Contextual DRL-Empowered Integrated Guidance and Evasion Approach for Hypersonic Glide Vehicles.” Nonlinear Dynamics 114 (1): 17. https://doi.org/10.1007/s11071-025-11899-2
• Ren, Haiwei, Wei Yi, Xiujuan Lu, and Chengxin Yang. 2021. “Online Beam Scheduling for Multi-Target Tracking in Linear Wireless Array Radar.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028090
• Repperger, Daniel, and Andrew Junker. 1975. “A Maximum Likelihood Approach for Identifying Human Operator Remnant in a Tracking Task.” In 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes. IEEE. https://doi.org/10.1109/cdc.1975.270750
• Resnick, S. 1966. “A Note on the Angle Accuracy of a Monopulse Radar Using Logarithmic Normalization.” Proceedings of the IEEE 54 (8): 1111–12. https://doi.org/10.1109/proc.1966.5035
• Rezazadeh Mohammadi, M., M. Fathi Jegarkandi, and A. Moarrefianpour. 2016. “Robust Roll Autopilot Design to Reduce Couplings of a Tactical Missile.” Aerospace Science and Technology 51: 142–50. https://doi.org/10.1016/j.ast.2016.02.001
• “Ridge and Bayes Identification for the Quasilinear Human Controller in Compensatory Tracking.” 1976. IEEE Transactions on Systems, Man, and Cybernetics SMC-6 (10): 705–8. https://doi.org/10.1109/tsmc.1976.4309423
• Rimer, M., and D. K. Frederick. 1988. “Solutions of the Second IEEE Benchmark Control Problem (Missile Autopilot).” In Proceedings of the IEEE 1988 National Aerospace and Electronics Conference. IEEE. https://doi.org/10.1109/naecon.1988.195042
• Rishel, R. W. 1968. “Optimal Terminal Guidance of an Air-to-Surface Missile.” Journal of Spacecraft and Rockets 5 (6): 649–54. https://doi.org/10.2514/3.29325
• Ristanović, Milan, Žarko Ćojbašić, and Dragan Lazić. 2012. “Intelligent Control of DC Motor Driven Electromechanical Fin Actuator.” Control Engineering Practice 20 (6): 610–17. https://doi.org/10.1016/j.conengprac.2012.02.009
• “Robust Stability Analysis of a Lateral Flight Control System for a Missile.” 1999. In Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251). IEEE. https://doi.org/10.1109/acc.1999.786199
• Rodriguez, Armando A., and Ricardo Aguilar. 1995. “Graphical Visualization of Missile–target Air-to-Air Engagements: An Educational Tool for Designing and Evaluating Missile Guidance and Control Systems.” Computer Applications in Engineering Education 3 (1): 5–20. https://doi.org/10.1002/cae.6180030103
• Rogers, S. R. n.d.-a. “Course and Miss-Distance Estimation for Constant-Heading Targets with Variable Speed.” In IEEE Conference on Aerospace and Electronics. IEEE. https://doi.org/10.1109/naecon.1990.112791
• Rogers, S. R. n.d.-b. “Effect of Glint Errors on Steady-State Tracking Accuracies of Maneuvering Targets.” In IEEE International Conference on Radar. IEEE. https://doi.org/10.1109/radar.1990.201205
• Roloff, H. A. 1957. “Telemetering Receiving System at the Air Force Missile Test Center.” IRE Transactions on Telemetry and Remote Control TRC-3 (1): 1–1. https://doi.org/10.1109/irettrc.1957.6541527
• Romero-Calvo, Á., Vladislav Urbansky, Vadim Yudintsev, Hanspeter Schaub, and Valeriy Trushlyakov. 2023. “Novel Propellant Settling Strategies for Liquid Rocket Engine Restart in Microgravity.” Acta Astronautica 202: 214–28. https://doi.org/10.1016/j.actaastro.2022.10.012
• Roncace, Elizabeth A. 1991. “Liquid Oxygen Cooling of Hydrocarbon Fueled Rocket Thrust Chambers.” Journal of Propulsion and Power 7 (5): 717–23. https://doi.org/10.2514/3.23384
• Root, L. E. 1945. “The Effective Use of Aerodynamic Balance on Control Surfaces.” Journal of the Aeronautical Sciences 12 (2): 149–63. https://doi.org/10.2514/8.11215
• Roscoe, Kelly M. 2001. “Equivalency between Strapdown Inertial Navigation Coning and Sculling Integrals/Algorithms.” Journal of Guidance, Control, and Dynamics 24 (2): 201–5. https://doi.org/10.2514/2.4718
• Ross, R. Alexander, and Marley E. Bechtel. 1968. “Scattering-Center Theory and Radar Glint Analysis.” IEEE Transactions on Aerospace and Electronic Systems AES-4 (5): 756–62. https://doi.org/10.1109/taes.1968.5408694
• Rowen, Aaron, Martha Grabowski, and Jean-Philippe Rancy. 2021. “Moving and Improving in Safety-Critical Systems: Impacts of Head-Mounted Displays on Operator Mobility, Performance, and Situation Awareness.” International Journal of Human-Computer Studies 150: 102606. https://doi.org/10.1016/j.ijhcs.2021.102606
• Rowen, Aaron, Martha Grabowski, Jean-Philippe Rancy, and Alyssa Crane. 2019. “Impacts of Wearable Augmented Reality Displays on Operator Performance, Situation Awareness, and Communication in Safety-Critical Systems.” Applied Ergonomics 80: 17–27. https://doi.org/10.1016/j.apergo.2019.04.013
• 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
• Ruan, Zhihu, Xukai Ding, Yang Gao, Zhengcheng Qin, and Hongsheng Li. 2023. “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, Wei, Quanlin Dong, Xiaoyue Zhang, and Zhibing Li. 2021. “Friction Compensation Control of Electromechanical Actuator Based on Neural Network Adaptive Sliding Mode.” Sensors 21 (4): 1508. https://doi.org/10.3390/s21041508
• Rudinskii, A. V., and D. A. Yagodnikov. 2021. “Electrophysics of the Combustion of Hydrocarbon Fuel in the Liquid Propellant Rocket Engine Chamber.” High Temperature 59 (2–6): 268–76. https://doi.org/10.1134/s0018151x2103010x
• 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
• Rusnak, I. n.d. “Optimal Guidance for High Order Maneuvering Target and High Order Missile.” In Proceedings. ICCON IEEE International Conference on Control and Applications. IEEE. https://doi.org/10.1109/iccon.1989.770497
• Rusnak, Ilan. 1992. “Guidance Law Based on an Exponential Cost Criterion for High Order Missile and Maneuvering Target.” In 1992 American Control Conference. IEEE. https://doi.org/10.23919/acc.1992.4792563
• Rusnak, Ilan. 1996. “Exponential Criterion-Based Guidance Law for Acceleration Constrained Missile and Maneuvering Target.” Journal of Guidance, Control, and Dynamics 19 (3): 718–21. https://doi.org/10.2514/3.21684
• Rusnak, Ilan. 2010a. “Bounds on the RMS Miss of Radar-Guided Missiles.” Journal of Guidance, Control, and Dynamics 33 (6): 1718–23. https://doi.org/10.2514/1.50262
• Rusnak, Ilan. 2010b. “Games Based Guidance in Anti Missile Defence for High Order Participants.” In Melecon 2010 - 2010 15th IEEE Mediterranean Electrotechnical Conference. IEEE. https://doi.org/10.1109/melcon.2010.5475962
• Rusnak, Ilan. 2011. “Bounds on the Root-Mean-Square Miss of Radar-Guided Missiles against Sinusoidal Target Maneuvers.” Journal of Guidance, Control, and Dynamics 34 (4): 1060–69. https://doi.org/10.2514/1.52460
• Rusnak, Ilan. 2012. “Bound on Root-Mean-Square Miss of Radar-Guided Missiles for Short Terminal Phase Period.” Journal of Guidance, Control, and Dynamics 35 (2): 665–69. https://doi.org/10.2514/1.55556
• Rusnak, Ilan. 2015. “Bounds on the Miss of Multiple-Model-Based Terminal Guidance Laws.” Journal of Guidance, Control, and Dynamics 38 (6): 1001–11. https://doi.org/10.2514/1.g000267
• Rusnak, Ilan. 2020. “Bounds on the Miss of Radar-Guided Missiles with Discrete Guidance.” Journal of Guidance, Control, and Dynamics 43 (4): 825–30. https://doi.org/10.2514/1.g004811
• Rusnak, Ilan. 2023. “Optimal Pure-Pursuit Missile Guidance.” Aerotecnica Missili & Spazio 103 (1): 51–60. https://doi.org/10.1007/s42496-023-00185-2
• Rusnak, I., and L. Meir. n.d. “Optimal Guidance for Acceleration Constrained Missile and Maneuvering Target.” In The Sixteenth Conference of Electrical and Electronics Engineers in Israel,. IEEE. https://doi.org/10.1109/eeis.1989.720142
• Rusnak, Ilan, and Levi Meir. 1991. “Optimal Guidance for High-Order and Acceleration Constrained Missile.” Journal of Guidance, Control, and Dynamics 14 (3): 589–96. https://doi.org/10.2514/3.20679
• Rusnak, Ilan, Haim Weiss, Rei Eliav, and Tal Shima. 2010. “Missile Guidance with Constrained Terminal Body Angle.” In 2010 IEEE 26-th Convention of Electrical and Electronics Engineers in Israel. IEEE. https://doi.org/10.1109/eeei.2010.5662094
• Rutkowski, Adam Konrad, Miroslaw Czyzewski, Andrzej Witczak, and Adam Kawalec. 2015. “Protection of Radar against Anti-Radiation Missile Using Single Electromagnetic Decoy.” In 2015 16th International Radar Symposium (IRS). IEEE. https://doi.org/10.1109/irs.2015.7226303
• Ryoo, Chang-Kyung, Hangju Cho, and Min-Jea Tahk. 2005. “Optimal Guidance Laws with Terminal Impact Angle Constraint.” Journal of Guidance, Control, and Dynamics 28 (4): 724–32. https://doi.org/10.2514/1.8392
• Ryu, Sang-Gyu, Jae Jin Jeong, and David Hyunchul Shim. 2022. “Sensor Data Prediction in Missile Flight Tests.” Sensors 22 (23): 9410. https://doi.org/10.3390/s22239410
• Sachuk, I., P. Kushch, A. Kalyta, P. Open’ko, V. Orlenko, and S. Bondarenko. 2020. “The Results of System Analysis of Functional Diagrams and Operation Algorithms of Tracking Systems of Tracking Radar of Antiaircraft Missile Armament with Digital Processing of Error Signal.” In 2020 IEEE 2nd International Conference on Advanced Trends in Information Theory (ATIT). IEEE. https://doi.org/10.1109/atit50783.2020.9349335
• 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
• Saeedi, Jamal. 2020. “Feasibility Study and Conceptual Design of Missile-Borne Synthetic Aperture Radar.” IEEE Transactions on Systems, Man, and Cybernetics: Systems 50 (3): 1122–33. https://doi.org/10.1109/tsmc.2017.2718114
• 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
• Sahoo, Udaya Kumar, Shyam Sundar Kundu, Bijayananda Patnaik, and Srinivasarao Chintagunta. 2021. “Ground-Based Passive Radar and on-Board Beacon for Airborne Target Tracking with GPS Based Time Synchronization.” In 2021 2nd International Conference on Range Technology (ICORT). IEEE. https://doi.org/10.1109/icort52730.2021.9581439
• Sahu, Anila Kumar, and Manas Ranjan Das. 2011. “4×4 Rectangular Patch Array Antenna for Bore Sight Application of Conical Scan S-Band Tracking Radar.” In 2011 Indian Antenna Week (IAW). IEEE. https://doi.org/10.1109/indianaw.2011.6264931
• Sahu, Naman Kumar, Sayantan Pal, and Sikha Hota. 2025. “Impact Angle Constrained 3D Guidance Law for Stationary Target Interception.” In 2025 IEEE Space, Aerospace and Defence Conference (SPACE). IEEE. https://doi.org/10.1109/space65882.2025.11171040
• Saito, Yuki, Hiroshi Asai, Tomoya Kitamura, Wataru Iida, Takahiro Nozaki, and Kouhei Ohnishi. 2022. “Performance Improvement of Bilateral Teleoperation with Hydraulic Actuator by Friction Compensation.” In 2022 IEEE 17th International Conference on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc51637.2022.9729300
• Sakaguchi, Yutaka. 2011. “Intermittent Motor Control Observed in Visuo-Manual Tracking.” Neuroscience Research 71: e249. https://doi.org/10.1016/j.neures.2011.07.1085
• Sakaki, Kazuki, Tomokazu Funahashi, Shinji Nakaya, et al. 2018. “Longitudinal Combustion Instability of a Pintle Injector for a Liquid Rocket Engine Combustor.” Combustion and Flame 194: 115–27. https://doi.org/10.1016/j.combustflame.2018.04.017
• 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
• Saleem, Abdul, and Ashwini Ratnoo. 2018. “Two Stage Proportional Navigation Guidance Law for Impact Time Control.” In 2018 Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/indiancc.2018.8307997
• Salih, Adham, and Amiram Moshaiov. 2024. “Neuro-Evolution-Based Generic Missile Guidance Law for Many-Scenarios.” Applied Soft Computing 152: 111210. https://doi.org/10.1016/j.asoc.2023.111210
• Sallam, Mohamed, Ahmed Ramadan, and Mohamed Fanni. 2013. “Position Tracking for Bilateral Teleoperation System with Varying Time Delay.” In 2013 IEEE/ASME International Conference on Advanced Intelligent Mechatronics. IEEE. https://doi.org/10.1109/aim.2013.6584248
• 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
• Sang Baohua and Jiang Changsheng. 2009. “Integrated Guidance and Control for a Missile in the Pitch Plane Based upon Subspace Stabilization.” In 2009 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2009.5195157
• 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
• Sankowski, Miroslaw, Tomasz Rutkowski, and Piotr Uruski. 2006. “Evaluation of Multi-Radar Detection of Ballistic Missile.” In 2006 International Radar Symposium. IEEE. https://doi.org/10.1109/irs.2006.4338082
• 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
• Saratayon, Peerayudh, Pattapong Sripho, and Soraphob Suparchaiparnitchapong. 2015. “Design of COTS Dual-Circularly Polarized Conical-Scan Cassegrain Antenna for Rocket Tracking.” In 2015 Asian Conference on Defence Technology (ACDT). IEEE. https://doi.org/10.1109/acdt.2015.7111598
• Sarigul-Klijn, Marti, Nesrin Sarigul-Klijn, Bob Morgan, et al. 2006. “Flight Testing of a New Earth-to-Orbit Air Launch Method.” Journal of Aircraft 43 (3): 577–83. https://doi.org/10.2514/1.18559
• Sarunic, P. W. n.d. “Adaptive Variable Update Rate Target Tracking for a Phased Array Radar.” In Proceedings International Radar Conference. IEEE. https://doi.org/10.1109/radar.1995.522565
• Sasoh, Akihiro, Yohei Sekiya, Takeharu Sakai, Jae-Hyung Kim, and Atsushi Matsuda. 2010. “Supersonic Drag Reduction with Repetitive Laser Pulses through a Blunt Body.” AIAA Journal 48 (12): 2811–17. https://doi.org/10.2514/1.j050174
• Savage, Paul G. 1998a. “Strapdown Inertial Navigation Integration Algorithm Design Part 1: Attitude Algorithms.” Journal of Guidance, Control, and Dynamics 21 (1): 19–28. https://doi.org/10.2514/2.4228
• Savage, Paul G. 1998b. “Strapdown Inertial Navigation Integration Algorithm Design Part 2: Velocity and Position Algorithms.” Journal of Guidance, Control, and Dynamics 21 (2): 208–21. https://doi.org/10.2514/2.4242
• 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. 2013. “Blazing Gyros: The Evolution of Strapdown Inertial Navigation Technology for Aircraft.” Journal of Guidance, Control, and Dynamics 36 (3): 637–55. https://doi.org/10.2514/1.60211
• Savci, Kubilay, Gaspare Galati, and Gabriele Pavan. 2021. “Low-PAPR Waveforms with Shaped Spectrum for Enhanced Low Probability of Intercept Noise Radars.” Remote Sensing 13 (12): 2372. https://doi.org/10.3390/rs13122372
• Scallen, S. F., P. A. Hancock, and J. A. Duley. 1995. “Pilot Performance and Preference for Short Cycles of Automation in Adaptive Function Allocation.” Applied Ergonomics 26 (6): 397–403. https://doi.org/10.1016/0003-6870(95)00054-2
• Schippers, Hendrik, Tim Gebauer, Karsten Heimann, and Christian Wietfeld. 2025. “RISE: Multi-Link Proactive Low-Latency Video Streaming for Teleoperation in Fading Channels.” In 2025 IEEE 101st Vehicular Technology Conference (VTC2025-Spring). IEEE. https://doi.org/10.1109/vtc2025-spring65109.2025.11174790
• Schryver, J. C. 1988a. “Operator Model-Based Design and Evaluation of Advanced Systems: Computational Models.” In Conference Record for 1988 IEEE Fourth Conference on Human Factors and Power Plants,. IEEE. https://doi.org/10.1109/hfpp.1988.27489
• Schryver, J. C. 1988b. “Operator Model-Based Design Evaluation of Advanced Systems: Conceptual Models.” In Conference Record for 1988 IEEE Fourth Conference on Human Factors and Power Plants,. IEEE. https://doi.org/10.1109/hfpp.1988.27488
• Schuck, Tod M., Mark A. Freisel, David B. Reese, and Michael A. Villa. 2020. “Phenomenology Based Missile Classification Using Radar Micro-Doppler Processing.” In 2020 IEEE International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar42522.2020.9114805
• Schumacher, C. J., and P. P. Khargonekar. 1998. “Stability Analysis of a Missile Control System with a Dynamic Inversion Controller.” In Proceedings of the 1998 American Control Conference. ACC (IEEE Cat. No.98CH36207). IEEE. https://doi.org/10.1109/acc.1998.707303
• 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
• Se-Ah Jang, Chang-Kyung Ryoo, Keeyoung Choi, and Min-Jea Tahk. 2008. “Guidance Algorithms for Tactical Missiles with Strapdown Seeker.” In 2008 SICE Annual Conference. IEEE. https://doi.org/10.1109/sice.2008.4655108
• Seeley, H. F., and J. C. Bliss. 1966. “Compensatory Tracking with Visual and Tactile Displays.” IEEE Transactions on Human Factors in Electronics HFE-7 (2): 84–90. https://doi.org/10.1109/thfe.1966.232328
• Seifer, A. D. 1992. “Monopulse-Radar Angle Tracking in Noise or Noise Jamming.” IEEE Transactions on Aerospace and Electronic Systems 28 (3): 622–38. https://doi.org/10.1109/7.256285
• Seifer, A. D. 1994. “Monopulse-Radar Angle Measurement in Noise.” IEEE Transactions on Aerospace and Electronic Systems 30 (3): 950–57. https://doi.org/10.1109/7.303771
• Sekaran, V. G. 1983. “Subsonic Rolling Moments for Wing Roll Control of a Cruciform Missile Model.” Journal of Spacecraft and Rockets 20 (2): 97–98. https://doi.org/10.2514/3.28362
• Seliktar, Y., E. J. Holder, and D. B. Williams. 1998. “An Adaptive Monopulse Processor for Angle Estimation in a Mainbeam Jamming and Coherent Interference Scenario.” In Proceedings of the 1998 IEEE International Conference on Acoustics, Speech and Signal Processing, ICASSP ‘98 (Cat. No.98CH36181), vol. 4. IEEE. https://doi.org/10.1109/icassp.1998.681543
• Sells, Ray. 2015. “A Novel Missile Autopilot with Remarkable Robustness.” In 2015 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2015.7119223
• Sen, Satyabrata, and Arye Nehorai. 2009a. “OFDM MIMO Radar Design for Low-Angle Tracking Using Mutual Information.” In 2009 3rd IEEE International Workshop on Computational Advances in Multi-Sensor Adaptive Processing (CAMSAP). IEEE. https://doi.org/10.1109/camsap.2009.5413311
• Sen, Satyabrata, and Arye Nehorai. 2009b. “OFDM MIMO Radar for Low-Grazing Angle Tracking.” In 2009 Conference Record of the Forty-Third Asilomar Conference on Signals, Systems and Computers. IEEE. https://doi.org/10.1109/acssc.2009.5470152
• Seok-Jae Lee and Joon Lyou. 2007. “Neurofuzzy Modeling of Manual Control System with a Human Operator.” In 2007 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2007.4407002
• Seong-Ho Song, Jin-Woo Hong, and In-Joong Ha. 2005. “L/sub 2/ Stability and Performance Analysis of Missile Systems with Linear Autopilots and PN Guidance Laws.” In Proceedings of the 2005, American Control Conference, 2005.. IEEE. https://doi.org/10.1109/acc.2005.1469959
• Serakos, D. n.d. “Nonlinear Controllers for a Tail-Fin Controlled Missile.” In Proceedings of Southeastcon ‘93. IEEE. https://doi.org/10.1109/secon.1993.465725
• Sewoong Kim and W. R. Hamel. 2002. “Force Assistance Function for Human-Machine Cooperative Telerobotics Using Fuzzy Logic.” In Proceedings 2002 IEEE International Conference on Robotics and Automation (Cat. No.02CH37292), vol. 2. IEEE. https://doi.org/10.1109/robot.2002.1014860
• 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
• 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
• Shalumov, Vitaly. 2019. “Optimal Cooperative Guidance Laws in a Multiagent Target–Missile–Defender Engagement.” Journal of Guidance, Control, and Dynamics 42 (9): 1993–2006. https://doi.org/10.2514/1.g004054
• 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
• Shan, Chenghao, and Weidong Zhou. 2021. “A Zigzag Maneuver Target Tracking Algorithm with Colored Glint Measurement Noise.” In 2021 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma52036.2021.9512671
• Shandling, Jennifer, and Daniel H. Platus. 1986. “Control of Missile Dispersion via Roll Rate Modulation.” Journal of Guidance, Control, and Dynamics 9 (6): 638–44. https://doi.org/10.2514/3.20158
• Shang, Yanhai, and Zhe Liu. 2006. “A Comparative Study of Several Compression Algorithms for Miss Distance Measurement.” In 2006 CIE International Conference on Radar. IEEE. https://doi.org/10.1109/icr.2006.343194
• Shang, Yanhai, Zhe Liu, and Jianyu Yang. 2006. “A Hybrid Compression Algorithm for Doppler Signal in Miss Distance Measurement.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.346000
• Shang She, Zhang Shouhong, and Zhang Xiushe. 2001. “Investigation on Low-Angle Tracking Technique for HRR Radar.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984842
• Shankar, Ajay, Sebastian Elbaum, and Carrick Detweiler. 2018. “Towards Aerial Recovery of Parachute-Deployed Payloads.” In 2018 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE. https://doi.org/10.1109/iros.2018.8594082
• Shao, Jiang, Yang Xu, Jinpeng Zhang, Sijie Li, and Delin Luo. 2018. “A Sliding Mode Variable-Structure Guidance Law with Terminal Impact Angle Constraint.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018699
• Shao, Shijia, Taige Zhang, and Fang Ye. 2017. “Jamming Resource Allocation Aimed to Data Link Based on Simulant Annealing Algorithm.” In 2017 Progress in Electromagnetics Research Symposium - Fall (PIERS - FALL). IEEE. https://doi.org/10.1109/piers-fall.2017.8293276
• Shaoming, He, Lin Defu, and Wang Jiang. 2014. “Terminal Sliding Mode Based Impact Angle Guidance Law with Observability Enhancement.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007222
• Sharenson, S. 1962. “Angle Estimation Accuracy with a Monopulse Radar in the Search Mode.” IRE Transactions on Aeronautical and Navigational Electronics ANE-9 (3): 175–79. https://doi.org/10.1109/tane3.1962.4201876
• Sharma, Yash Raj, and Ashwini Ratnoo. 2019a. “A Bearings-Only Trajectory Shaping Guidance Law with Look-Angle Constraint.” IEEE Transactions on Aerospace and Electronic Systems 55 (6): 3303–15. https://doi.org/10.1109/taes.2019.2906090
• Sharma, Yash Raj, and Ashwini Ratnoo. 2019b. “A New Guidance Law for Look-Angle Constrained Interception of Moving Targets.” In 2019 27th Mediterranean Conference on Control and Automation (MED). IEEE. https://doi.org/10.1109/med.2019.8798591
• Shaw, I. S. 1993. “Fuzzy Model of a Human Control Operator in a Compensatory Tracking Loop.” International Journal of Man-Machine Studies 39 (2): 305–32. https://doi.org/10.1006/imms.1993.1063
• Shaw, Leonard, Rodney Clark, and Dick Talmadge. 1988. “F-111 Generic Weapons Bay Acoustic Environment.” Journal of Aircraft 25 (2): 147–53. https://doi.org/10.2514/3.45555
• Shaw Y. Ong and B. L. Pierson. n.d. “Optimal Evasive Aircraft Maneuvers against a Surface-To-Air Missile.” In Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,. IEEE. https://doi.org/10.1109/aerocs.1993.720980
• She, Haoping, Shuxing Yang, Hui Ni, and Horst Baier. 2011. “A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint.” International Journal of Computational Intelligence Systems 4 (6): 1319. https://doi.org/10.2991/ijcis.2011.4.6.24
• Shelan, Sameh Fathey, Mohammed Abozied Hassan, Hossam Hendy, and Yehia Zakarya Elhalwagy. 2020. “Missile Roll Autopilot Redesign Based Advanced Fin Actuation System Modeling.” In 2020 2nd Novel Intelligent and Leading Emerging Sciences Conference (NILES). IEEE. https://doi.org/10.1109/niles50944.2020.9257900
• 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
• Sheng, Yongzhi, Zhuo Zhang, and Lei Xia. 2021. “Fractional-Order Sliding Mode Control Based Guidance Law with Impact Angle Constraint.” Nonlinear Dynamics 106 (1): 425–44. https://doi.org/10.1007/s11071-021-06820-6
• Sheridan, T. B. 1995. “Teleoperation, Telerobotics and Telepresence: A Progress Report.” Control Engineering Practice 3 (2): 205–14. https://doi.org/10.1016/0967-0661(94)00078-u
• Sheridan, T. B. 2000. “Function Allocation: Algorithm, Alchemy or Apostasy?” International Journal of Human-Computer Studies 52 (2): 203–16. https://doi.org/10.1006/ijhc.1999.0285
• Shi, Chenguang, Lintao Ding, Wei Qiu, Fei Wang, and Jianjiang Zhou. 2020. “Joint Optimization of Target Assignment and Resource Allocation for Multi-Target Tracking in Phased Array Radar Network.” In 2020 IEEE Radar Conference (RadarConf20). IEEE. https://doi.org/10.1109/radarconf2043947.2020.9309151
• Shi, Zhenqing, Xiaolong Liang, Jiaqiang Zhang, and Qixi Fu. 2018b. “Modeling and Simulation Analysis on Three-Dimensional Air-to-Air Missile Attack Zone of Two Aircrafts.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018858
• Shi, Xiaoli, Yongcai Liu, Xinmin Wang, and Changqing Wang. 2007. “Angular Glint of Aircraft Formation and Its Applications.” In 2007 International Conference on Mechatronics and Automation. IEEE. https://doi.org/10.1109/icma.2007.4303743
• Shi, M. R., Y. Z. Luan, Z. He, and D. Z. Ding. 2025b. “Wideband Angular Glint Characteristics under near-Field IPO Technology.” In 2025 International Conference on Microwave and Millimeter Wave Technology (ICMMT). IEEE. https://doi.org/10.1109/icmmt65948.2025.11187922
• 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, Chenguang, Wei Qiu, Fei Wang, Sana Salous, and Jianjiang Zhou. 2019c. “Stackelberg Game-Theoretic Low Probability of Intercept Performance Optimization for Multistatic Radar System.” Electronics 8 (4): 397. https://doi.org/10.3390/electronics8040397
• Shi, Chenguang, Zhao Shi, Sana Salous, and JianJiang Zhou. 2021a. “Joint Optimization of Radar Assignment and Resource Allocation for Target Tracking in Phased Array Radar Network.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028227
• Shi, Zhen, Jian Wang, Chendi He, and Xiaohui Chi. 2015. “Research on Three-Dimensional Impact Angle Constrained Guidance Laws.” In 2015 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2015.7237594
• Shi, Qiao, Yujie Wang, Zhengchun Zhou, Guolong Cui, and Pingzhi Fan. 2025a. “Low Probability of Intercept Signal Design for MIMO Integrated Sensing and Communication Systems.” IEEE Transactions on Communications 73 (9): 8155–65. https://doi.org/10.1109/tcomm.2025.3545623
• Shi, Mengyang, Yuepeng Wu, Yesheng Gao, Wenxuan Shi, Bin Yuan, and Xingzhao Liu. 2026. “A Single-Channel Wide-Beam Radar Angle Estimation Accuracy Improvement Method by Nonlinear Wavefront Modulation.” IEEE Transactions on Radar Systems 4: 911–24. https://doi.org/10.1109/trs.2026.3687266
• Shi, Wenhui, Shuai Yue, Zhiqian Li, et al. 2022. “Dynamic Simulation and Parameter Analysis of Weaved Composite Material for Unmanned Aerial Vehicle Parachute Recovery in Deployment Phase.” Crystals 12 (6): 758. https://doi.org/10.3390/cryst12060758
• Shi, Shaokun, Jiufen Zhao, and Hao You. 2018a. “Design of Bias Proportional Navigation Guidance Law for Motion Target with Impact Angle Constraint.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019209
• Shi, Chenguang, Jianjiang Zhou, and Fei Wang. 2016. “LPI Based Resource Management for Target Tracking in Distributed Radar Network.” In 2016 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2016.7485222
• Shi, Zhifu, Daizhong Zhou, Shunhong Wang, and Lefei Pan. 2012. “Simulation of Skip-Glide Trajectory for Hypersonic Vehicle in near Space.” In System Simulation and Scientific Computing. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-34381-0_29
• Shi, Heng, Jihong Zhu, Minchi Kuang, and Libing Hou. 2021c. “Optimal Launch Time Selection in Target-Missile-Defender Scenario.” In 2021 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc54610.2021.9654988
• Shi-Wei Gao and Zheng Bao. 1992. “Radar Low-Angle Tracking with Subarray Level ML Tracking Algorithms.” In [Proceedings] ICASSP-92: 1992 IEEE International Conference on Acoustics, Speech, and Signal Processing. IEEE. https://doi.org/10.1109/icassp.1992.226338
• 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
• Shieh, L. S., M. Datta-Barua, R. E. Yates, and J. P. Leonard. 1980. “Computer-Aided Methods for Redesigning the Stabilized Pitch Control System of a Semi-Active Terminal Homing Missile.” Computers & Electrical Engineering 7 (3): 185–200. https://doi.org/10.1016/0045-7906(80)90006-3
• 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. 2011. “Optimal Cooperative Pursuit and Evasion Strategies against a Homing Missile.” Journal of Guidance, Control, and Dynamics 34 (2): 414–25. https://doi.org/10.2514/1.51765
• Shima, T., and O. M. Golan. 2003. “Bounded Differential Games Guidance Law for a Dual Controlled Missile.” In Proceedings of the 2003 American Control Conference, 2003., vol. 1. IEEE. https://doi.org/10.1109/acc.2003.1238979
• Shin, Jaeyong, Junewhee Ahn, and Jaeheung Park. 2022. “Stereoscopic Low-Latency Vision System via Ethernet Network for Humanoid Teleoperation.” In 2022 19th International Conference on Ubiquitous Robots (UR). IEEE. https://doi.org/10.1109/ur55393.2022.9826285
• Shinar, J., and I. Forte. 1986. “On the Optimal Pure Strategy Sets for a Mixed Missile Guidance Law Synthesis.” In 1986 25th IEEE Conference on Decision and Control. IEEE. https://doi.org/10.1109/cdc.1986.267418
• Shinar, J., and I. Forte. 1991. “On the Optimal Pure Strategy Sets for a Mixed Missile Guidance Law Synthesis.” IEEE Transactions on Automatic Control 36 (11): 1296–1300. https://doi.org/10.1109/9.100942
• Shinar, J., I. Forte, and B. Kantor. 1992. “Mixed Strategy Guidance (MSG): A New High Performance Missile Guidance Law.” In 1992 American Control Conference. IEEE. https://doi.org/10.23919/acc.1992.4792369
• Shinar, J., I. Forte, and B. Kantor. 1994. “Mixed Strategy Guidance: A New High-Performance Missile Guidance Law.” Journal of Guidance, Control, and Dynamics 17 (1): 129–35. https://doi.org/10.2514/3.21169
• Shinar, J., and T. Shima. n.d. “A Game Theoretical Interceptor Guidance Law for Ballistic Missile Defence.” In Proceedings of 35th IEEE Conference on Decision and Control, vol. 3. IEEE. https://doi.org/10.1109/cdc.1996.573534
• Shinar, J., and R. Tabak. 1994. “New Results in Optimal Missile Avoidance Analysis.” Journal of Guidance, Control, and Dynamics 17 (5): 897–902. https://doi.org/10.2514/3.21287
• Shinar, Josef, Vladimir Turetsky, and Yaakov Oshman. 2007. “Integrated Estimation/Guidance Design Approach for Improved Homing against Randomly Maneuvering Targets.” Journal of Guidance, Control, and Dynamics 30 (1): 154–61. https://doi.org/10.2514/1.22916
• Shiotsuki, Tetsuo. 2006. “Time Delay Compensation of Human Operator in Position Tracking Tasks.” In 2006 SICE-ICASE International Joint Conference. IEEE. https://doi.org/10.1109/sice.2006.315370
• Shoyama, Tadayoshi, Yutaka Wada, Mitsuru Shimagaki, Tomoyuki Hashimoto, and Satoshi Takada. 2024. “Liquid Propellant Rocket Engine Cycles Partially Using Electric Turbopump.” Acta Astronautica 224: 138–47. https://doi.org/10.1016/j.actaastro.2024.08.005
• Shrivastava, Pankaj. 2026. “Examining the Challenges of Bayesian Approach in Reliability Demonstration Test.” In 2026 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/rams50514.2026.11424549
• Shu, Ting, Bin Tang, Kejun Yin, Qingyang Sun, Yangchun Chen, and Wenxian Yu. 2015. “Development of Multichannel Real-Time Hardware-in-the-Loop Radar Environment Simulator for Missile-Borne Synthetic Aperture Radar.” In 2015 IEEE Radar Conference (RadarCon). IEEE. https://doi.org/10.1109/radar.2015.7131026
• Shumway, Nathan M., and John E. Boranian. 2025. “Impact of Missile Cross-Sectional Shape on Aerodynamic Performance at Supersonic Speeds.” Journal of Spacecraft and Rockets 62 (6): 1918–28. https://doi.org/10.2514/1.a36230
• Shun-Wen Cheng. 2003. “Very Long Range Anti-Air Missile Systems Design.” In 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652), vol. 6. IEEE. https://doi.org/10.1109/aero.2003.1235208
• Shuping Tan and Zhibin Li. 2010. “Switching Control Design for a Hypersonic Flight Vehicle.” In 2010 Chinese Control and Decision Conference. IEEE. https://doi.org/10.1109/ccdc.2010.5498526
• 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
• Simeonides, George A. 2006. “Extrapolation-to-Flight of Aerodynamic Heating Measurements and Determination of in-Flight Radiation-Equilibrium Surface Temperature in Hypersonic/high Enthalpy Flow Conditions.” Shock Waves 16 (1): 25–34. https://doi.org/10.1007/s00193-006-0040-3
• Simões, Alberto M., and Vinícius M. G. B. Cavalcanti. 2023. “Missile Autopilot Design via Structured Robust Linear Parameter-Varying Synthesis.” Journal of Guidance, Control, and Dynamics 46 (8): 1649–56. https://doi.org/10.2514/1.g007580
• Sims, R., and E. Graf. 1971. “The Reduction of Radar Glint by Diversity Techniques.” IEEE Transactions on Antennas and Propagation 19 (4): 462–68. https://doi.org/10.1109/tap.1971.1139956
• Singh, N. 1970. “Spherical Probable Error (Spe) and Its Estimation.” Metrika 15 (1): 149–63. https://doi.org/10.1007/bf02613568
• Singh, N., and N. Bhashyam. 1972. “Effect of the Variable Offset Distance on the Kill Probability.” Metrika 19 (1): 39–47. https://doi.org/10.1007/bf01893276
• Singh, Manish Arjun, and Shashi Ranjan Kumar. 2021. “Impact Angle Constrained Guidance with Collision Avoidance from Multiple Moving Obstacles.” In 2021 International Symposium of Asian Control Association on Intelligent Robotics and Industrial Automation (IRIA). IEEE. https://doi.org/10.1109/iria53009.2021.9588757
• Singh, Harsh V. P., and Qusay Mahmoud. 2019. “LSTM-Based Approach to Monitor Operator Situation Awareness via HMI State Prediction.” In 2019 IEEE International Conference on Industrial Internet (ICII). IEEE. https://doi.org/10.1109/icii.2019.00064
• Sinha, Abhinav, Rohit V. Nanavati, and Shashi Ranjan Kumar. 2021. “Impact Angle Constrained Integrated Guidance and Control for a Dual-Controlled Interceptor.” In 2021 Seventh Indian Control Conference (ICC). IEEE. https://doi.org/10.1109/icc54714.2021.9703136
• Sirignano, William A., and Jeremy Krieg. 2016. “Two-Time-Variable Perturbation Theory for Liquid-Rocket Combustion Instability.” Journal of Propulsion and Power 32 (3): 755–76. https://doi.org/10.2514/1.b35954
• Sirignano, William A., and Pavel P. Popov. 2013. “Two-Dimensional Model for Liquid-Rocket Transverse Combustion Instability.” AIAA Journal 51 (12): 2919–34. https://doi.org/10.2514/1.j052512
• Sirouspour, M. R., and S. E. Salcudean. 2003. “Suppressing Operator-Induced Oscillations in Manual Control Systems with Movable Bases.” IEEE Transactions on Control Systems Technology 11 (4): 448–59. https://doi.org/10.1109/tcst.2003.813386
• Siting, Peng, Zhao Qian, Ma Yichao, and Xu Cheng. 2019. “Observability Enhancement of the Target Tracking Model Based on Infrared Semi-Strapdown Seeker.” In 2019 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus48101.2019.8996025
• Siuru, William D. 1987. “Bombing Error Sensitivities Using a Simplified Aerodynamic Trajectory.” Journal of Aircraft 24 (6): 414–15. https://doi.org/10.2514/3.45462
• Sivrioglu, Selim. 2026. “Lyapunov Based Robust Proportional Navigation Guidance for Highly Accelerated Targets.” In 2026 11th International Conference on Recent Advances in Air and Space Technologies (RAST). IEEE. https://doi.org/10.1109/rast69551.2026.11672490
• Sivrioglu, Selim, and Sinan Başaran. 2025. “Control of a VTOL Aircraft Model with Air-Launched Missile Release Impact and Wind Disturbances.” In 2025 9th International Conference on Mechanical Engineering and Robotics Research (ICMERR). IEEE. https://doi.org/10.1109/icmerr64601.2025.10949912
• 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
• Smith, Austin L. 2008. “Proportional Navigation with Adaptive Terminal Guidance for Aircraft Rendezvous.” Journal of Guidance, Control, and Dynamics 31 (6): 1832–36. https://doi.org/10.2514/1.33535
• Smith, Edmund H., Sheshagiri K. Hebbar, and Max F. Platzer. 1994. “Aerodynamic Characteristics of a Canard-Controlled Missile at High Angles of Attack.” Journal of Spacecraft and Rockets 31 (5): 766–72. https://doi.org/10.2514/3.26510
• Sobel, Kenneth, and James R. Cloutier. 1992. “Eigenstructure Assignment for the Extended Medium Range Air-to-Air Missile.” Journal of Guidance, Control, and Dynamics 15 (2): 529–31. https://doi.org/10.2514/3.20869
• Sobolic, Frantisek M., Gerardo Cruz, and Dennis S. Bernstein. 2015. “An Inner-Loop/outer-Loop Architecture for an Adaptive Missile Autopilot.” In 2015 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2015.7170840
• Sohn, Chae Hoon, Woo-Seok Seol, Alexander A. Shibanov, and Valery P. Pikalov. 2004. “On the Method for Hot-Fire Modeling of High-Frequency Combustion Instability in Liquid Rocket Engines.” KSME International Journal 18 (6): 1010–18. https://doi.org/10.1007/bf02990873
• Solarte-Pineda, Jhonathan, Pedro David Bravo-Mosquera, Michelle Fernandino Westin, and Breno Moura Castro. 2026. “Unsteady Aerodynamics and Hinge Moment Calculations of Control Surfaces at Transonic Speeds.” Journal of Aircraft 63 (5): 2124–38. https://doi.org/10.2514/1.c038573
• Son, Min, Michael Börner, Wolfgang Armbruster, and Justin S. Hardi. 2023. “Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities.” Aerospace 10 (5): 452. https://doi.org/10.3390/aerospace10050452
• Son, Hyoung Il, and Doo Yong Lee. 2008. “Two-Channel Control for Scaled Teleoperation.” In 2008 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2008.4694348
• Son, Dong Hee, and Sang Man Seong. 2010. “PNG Law for Missile Guidance under Time Delayed Look Angle Measurement.” In ICCAS 2010. IEEE. https://doi.org/10.1109/iccas.2010.5670296
• 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, Jian-mei. 2004. “Research on Attitude Pursuit Guidance Law for Strapdown Homing System.” Chinese Journal of Aeronautics 17 (4): 235–39. https://doi.org/10.1016/s1000-9361(11)60243-4
• Song, Wei, and Bangcheng Ai. 2021. “Analysis of Aircraft-Store Compatibility for Internal Weapons Separation.” Aerospace Science and Technology 110: 106528. https://doi.org/10.1016/j.ast.2021.106528
• Song, Jaebong, and Han-Lim Choi. 2018. “Elliptical Trajectory Based Three-Dimensional Impact Angle Control Guidance.” In 2018 IEEE Aerospace Conference. IEEE. https://doi.org/10.1109/aero.2018.8396790
• Song, Huiseong, Seokwon Lee, Namhoon Cho, and Youdan Kim. 2018. “Cooperative Defense Strategy for Active Aircraft Protection Considering Launch Time of Defense Missile.” In 2018 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2018.8550089
• Song, Jie, Tao Liang, Qinglian Li, et al. 2021. “Study on the Heat Transfer Characteristics of Regenerative Cooling for LOX/LCH4 Variable Thrust Rocket Engine.” Case Studies in Thermal Engineering 28: 101664. https://doi.org/10.1016/j.csite.2021.101664
• 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, Tao, Yijing Wang, Hong Tao, and Zeliang Wu. 2026b. “Optimal Field-of-View and Impact-Angle Constrained Guidance against a Maneuvering Target.” Aerospace Science and Technology 179: 113238. https://doi.org/10.1016/j.ast.2026.113238
• 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, Jie, Dongdong Zhang, Peng Cui, Lin Wang, Yanhui Tang, and Xiangyi Liu. 2026a. “Investigation on Subcritical Regenerative Cooling for Ignition Experiments on LOX/LNG Rocket Engine.” Aerospace 13 (7): 593. https://doi.org/10.3390/aerospace13070593
• Soong, Chyi-Yeou, and Sing Chu. 1983. “A Semi-Empirical Approach for the Prediction of Aft-Body Drag of Supersonic Projectiles with Base Bleeding.” Journal of the Chinese Institute of Engineers 6 (1): 21–30. https://doi.org/10.1080/02533839.1983.9676719
• Spahr, Harold R. 1975. “Theoretical Store Separation Analyses of a Prototype Store.” Journal of Aircraft 12 (10): 807–11. https://doi.org/10.2514/3.59875
• Speelman, Ralph J. 1977. “Parachute Deployment Process Testing Technique.” Journal of Aircraft 14 (4): 401–2. https://doi.org/10.2514/3.58791
• Speyer, J. 1976. “An Adaptive Terminal Guidance Scheme Based on an Exponential Cost Criterion with Application to Homing Missile Guidance.” IEEE Transactions on Automatic Control 21 (3): 371–75. https://doi.org/10.1109/tac.1976.1101206
• Speyer, Jason L., Kevin D. Kim, and Minjea Tahk. 1990b. “Passive Homing Missile Guidance Law Based on New Target Maneuver Models.” Journal of Guidance, Control, and Dynamics 13 (5): 803–12. https://doi.org/10.2514/3.25405
• Spong, R. N. 1999. “An Efficient Method for Computing Azimuth and Elevation Angle Estimates from Monopulse Ratio Measurements of a Phased Array Pencil Beam Radar with Two-Dimensional Angle Steering.” In Proceedings of the 1999 IEEE Radar Conference. Radar into the Next Millennium (Cat. No.99CH36249). IEEE. https://doi.org/10.1109/nrc.1999.767352
• “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
• Sridhar, B., and N. K. Gupta. 1980. “Missile Guidance Laws Based on Singular Perturbation Methodology.” Journal of Guidance and Control 3 (2): 158–65. https://doi.org/10.2514/3.55964
• Srivastava, B. 1998a. “Aerodynamic Performance of Supersonic Missile Body- and Wing Tip-Mounted Lateral Jets.” Journal of Spacecraft and Rockets 35 (3): 278–86. https://doi.org/10.2514/2.3352
• Stallard, D. 1966. “A Missile Adaptive Roll Autopilot with a New Dither Principle.” IEEE Transactions on Automatic Control 11 (3): 368–78. https://doi.org/10.1109/tac.1966.1098375
• Stallard, D. 1973. “Discrete Optimal Terminal Control with Application to Missile Guidance.” IEEE Transactions on Automatic Control 18 (4): 373–77. https://doi.org/10.1109/tac.1973.1100351
• Stallard, David V. 1983. “Biased Optimal Guidance for a Bank-to-Turn Missile.” In 1983 American Control Conference. IEEE. https://doi.org/10.23919/acc.1983.4788273
• Stanley, James K. 1971. “Deterioration of Stainless Steel Regeneratively Cooled Thrust Chambers.” Journal of Spacecraft and Rockets 8 (4): 329–34. https://doi.org/10.2514/3.30274
• Stansbery, D. T., and S. N. Balakrishnan. 1994. “Approximate Analytical Guidance Schemes for Homing Missiles.” In Proceedings of 1994 American Control Conference - ACC ‘94, vol. 2. IEEE. https://doi.org/10.1109/acc.1994.752354
• Staros, Basil. 1959. “Selection of an Aerodynamic Configuration for Improved Beam Rider Guidance.” ARS Journal 29 (2): 115–18. https://doi.org/10.2514/8.4694
• Stechman, R. Carl. 1993. “Advanced Thrust Chamber Materials for Earth Storable Bipropellant Rocket Engines.” Acta Astronautica 29 (2): 109–15. https://doi.org/10.1016/0094-5765(93)90028-u
• Steinberg, Richard K. 2011. “The Perceptual Cognitive Mapping for Missile Defense Command and Control Displays.” In 2011 IEEE International Multi-Disciplinary Conference on Cognitive Methods in Situation Awareness and Decision Support (CogSIMA). IEEE. https://doi.org/10.1109/cogsima.2011.5753437
• Stephan, Ralph, Eike Stumpf, Henri Schottmüller, Tobias Röben, Nikolaus Dreyer, and Thomas Immler. 2023. “Methodology for Preliminary Flight Control Actuator Design.” Journal of Aircraft 60 (5): 1538–52. https://doi.org/10.2514/1.c036717
• Stewart, Reuben-Wayne, Jack Dooher, and Moble Benedict. 2026. “Flight Dynamics of a Hover-Capable Air-Launched Unmanned Aerial Vehicle.” Aerospace 13 (7): 616. https://doi.org/10.3390/aerospace13070616
• 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
• Stornig, Antonia, Aymen Fakhreddine, Hermann Hellwagner, Petar Popovski, and Christian Bettstetter. 2021. “Video Quality and Latency for UAV Teleoperation over LTE: A Study with ns3.” In 2021 IEEE 93rd Vehicular Technology Conference (VTC2021-Spring). IEEE. https://doi.org/10.1109/vtc2021-spring51267.2021.9448676
• Story, Mark, Timothy Deller, and Tony Allen. 2026. “Practical Three-Dimensional Curvilinear Aperture Monopulse Synthetic Aperture Radar.” In 2026 IEEE Radar Conference (RadarConf’26). IEEE. https://doi.org/10.1109/radarconf2663773.2026.11674862
• Su, Wenshan, Lei Chen, and Kebo Li. 2016. “Acceleration Requirement Analysis for True Proportional Navigation Guidance and Its Modification.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554219
• Su Lide, He Jianhua, and Wang Jianqiang. 2011. “Assessment for Effectiveness of Missile-Gun Integrated Weapon System Based on FSKA Model.” In 2011 International Conference on Electric Information and Control Engineering. IEEE. https://doi.org/10.1109/iceice.2011.5777513
• Subchan, S. 2008. “A Direct Multiple Shooting for the Optimal Trajectory of Missile Guidance.” In 2008 IEEE International Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.2008.4629675
• “A Successful Program for Missile Reliability.” 1992. Microelectronics Reliability 32 (4): 588. https://doi.org/10.1016/0026-2714(92)90532-p
• 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
• Sui, Miao, and Xiaojian Xu. 2010. “NFIPO Based Technique for near-Field Angular Glint Calculation of Radar Targets.” In 2010 International Conference on Electromagnetics in Advanced Applications. IEEE. https://doi.org/10.1109/iceaa.2010.5653084
• Sui, Miao, and Xiaojian Xu. 2012. “Angular Glint of Complex Targets for High Range Resolution Radar.” In 2012 International Conference on Electromagnetics in Advanced Applications. IEEE. https://doi.org/10.1109/iceaa.2012.6328762
• Sui, Miao, and Xiaojian Xu. 2014. “Angular Glint Calculation and Analysis of Radar Targets via Adaptive Cross Approximation Algorithm.” Journal of Systems Engineering and Electronics 25 (3): 411–21. https://doi.org/10.1109/jsee.2014.00047
• Summerfield, Martin. 1951b. “A Theory of Unstable Combustion in Liquid Propellant Rocket Systems.” Journal of the American Rocket Society 21 (5): 108–14. https://doi.org/10.2514/8.4374
• Sun, Tingting, Hairong Chu, Baiqiang Zhang, et al. 2015. “Line-of-Sight Rate Estimation Based on UKF for Strapdown Seeker.” Mathematical Problems in Engineering 2015: 1–14. https://doi.org/10.1155/2015/185149
• Sun, Y. L., and M. J. Er. 2001. “A Novel Approach towards Sideslip Velocity Autopilot for an Agile Missile Using Hybrid PID Control.” In 2001 European Control Conference (ECC). IEEE. https://doi.org/10.23919/ecc.2001.7076234
• Sun, Jin, Guolin Li, and Cheng Xu. 2012b. “Prior Distribution of Missile Range Trial Successive Test Data Based on Random Weighting.” In 2012 Fourth International Conference on Computational and Information Sciences. IEEE. https://doi.org/10.1109/iccis.2012.212
• 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, Jingliang, Chunsheng Liu, and Jiao Dai. 2018. “Robust Optimal Control for Missile-Target Guidance Systems via Adaptive Dynamic Programming.” In 2018 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2018.8623174
• Sun, Jiarui, Guangtao Ran, Chuanjiang Li, Yanning Guo, and Ju H. Park. 2025. “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, Zhichao, Hang Ren, Huarui Sun, Gary G. Yen, Junjie Wu, and Jianyu Yang. 2024. “Terminal Trajectory Planning for Synthetic Aperture Radar Imaging Guidance Based on Chronological Iterative Search Framework.” IEEE Transactions on Cybernetics 54 (5): 3065–78. https://doi.org/10.1109/tcyb.2022.3231974
• Sun, Shih-Chieh, and Yun-Cheng Tsai. 2025. “A Modular AIoT Framework for Low-Latency Real-Time Robotic Teleoperation in Smart Cities.” In 2025 IEEE Annual Congress on Artificial Intelligence of Things (AIoT). IEEE. https://doi.org/10.1109/aiot66900.2025.00034
• Sun, Shih-Chieh, Yun-Cheng Tsai, Han-Wen Kuo, and Shen-Chi Chen. 2026. “Low-Latency Human-in-the-Loop Robotic Teleoperation with Control–Media Separation Using MQTT and WebRTC.” IEEE Journal of Selected Areas in Sensors 3: 425–38. https://doi.org/10.1109/jsas.2026.3729555
• 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, Quan, Zhewei Zhang, Jing Feng, and Zhengqiang Pan. 2012c. “A Zero-Failure Reliability Demonstration Approach Based on Degradation Data.” In 2012 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering. IEEE. https://doi.org/10.1109/icqr2mse.2012.6246381
• Sun, Wei, Yatin Zhang, and Yu Wang. 2021. “Jamming Technology of Infrared Guided Missile Based on Surface-Type Infrared Decoy Method.” In 2021 33rd Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc52312.2021.9601649
• Sun, Sheng, HuaMing Zhang, HaiBin Zhao, ChunMei Yu, and Wei Wang. 2014. “Guidance Law with Finite Time Convergence Subject to Impact Angle Constraint.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896696
• Sung, Bu-Kyeng, and Jeong-Yeol Choi. 2026. “Rotating Detonation as a Limit Cycle State of Rocket Tangential Combustion Instability.” Proceedings of the Combustion Institute 42: 106192. https://doi.org/10.1016/j.proci.2026.106192
• Sung, Bu-Kyeng, Jiro Kasahara, and Jeong-Yeol Choi. 2025. “Numerical Investigation on the Detonative Tangential Combustion Instability in a Rocket Combustor.” Combustion and Flame 275: 114092. https://doi.org/10.1016/j.combustflame.2025.114092
• Sung-Hoon Moon, Dong-Seog Han, Hae-Sock Oh, and Myeorig-Je Cho. 2003a. “Monopulse Angle Estimation with Constrained Adaptive Beamforming Using Simple Mainlobe Maintenance Technique.” In IEEE Military Communications Conference, 2003. MILCOM 2003., vol. 2. IEEE. https://doi.org/10.1109/milcom.2003.1290425
• Sung-Hoon Moon, Dong-Seog Han, Myeong-Je Cho, and Young-Kil Kwag. 2003b. “A New Gsc Using Monopulse Angle Estimation Technique for Fast Target Tracking.” In IEEE International Symposium on Phased Array Systems and Technology, 2003.. IEEE. https://doi.org/10.1109/past.2003.1256974
• “A Supersonic Parachute.” 1949. Journal of the Franklin Institute 247 (2): 132. https://doi.org/10.1016/0016-0032(49)90725-5
• Surve, Prajakta, Arnab Maity, and Shashi Ranjan Kumar. 2020. “Quaternion Based Three-Dimensional Impact Angle Constrained Guidance.” IFAC-PapersOnLine 53 (2): 9446–51. https://doi.org/10.1016/j.ifacol.2020.12.2416
• Surve, Prajakta, Arnab Maity, and Shashi Ranjan Kumar. 2022. “Polynomial Based Impact Time and Impact Angle Constrained Guidance.” IFAC-PapersOnLine 55 (1): 486–91. https://doi.org/10.1016/j.ifacol.2022.04.080
• Suzuki, Atsushi, and Kouhei Ohnishi. 2010. “Performance Conditioning of Time Delayed Bilateral Teleoperation System by Scaling down Compensation Value of Communication Disturbance Observer.” In 2010 11th IEEE International Workshop on Advanced Motion Control (AMC). IEEE. https://doi.org/10.1109/amc.2010.5464075
• Swerling, Peter. 1956. “Maximum Angular Accuracy of a Pulsed Search Radar.” Proceedings of the IRE 44 (9): 1146–55. https://doi.org/10.1109/jrproc.1956.275167
• Szullo, Adam, and Rudolf Seller. 2016. “Maneuvering Target Tracking in Wide Area Multilateration Radar System.” In 2016 17th International Radar Symposium (IRS). IEEE. https://doi.org/10.1109/irs.2016.7497345
• Ta-Sung Lee and Tser-Ya Dai. 1994. “Optimum Beamformers for Monopulse Angle Estimation Using Overlapping Subarrays.” IEEE Transactions on Antennas and Propagation 42 (5): 651–57. https://doi.org/10.1109/8.299564
• Taek Lyul Song and Dong Gwan Lee. 2000. “Effective Filtering of Target Glint.” IEEE Transactions on Aerospace and Electronic Systems 36 (1): 234–40. https://doi.org/10.1109/7.826325
• Tafertshofer, Markus, Oliver Arnold, and Erwin Biebl. 2024b. “Radar Target Generation for Angular Resolution Testing in a Compact Test Range with Two Antennas.” In 2024 Kleinheubach Conference. IEEE. https://doi.org/10.23919/ieeeconf64570.2024.10739122
• Tafertshofer, Markus, Oliver Arnold, Florian Pfeiffer, Daniel Korthauer, and Erwin Biebl. 2024a. “Applying a Biprism in Radar Test Ranges for Angular Measurements.” In 2024 International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar58436.2024.10994133
• Taghavi, Seyed Reza, Mohammad Ali Dehnavi, and Ali Ghafouri. 2019. “Numerical Analysis of Reactive Turbulent Flow in the Thrust Chamber of RD-108 Engine Rocket.” Defence Technology 15 (4): 565–75. https://doi.org/10.1016/j.dt.2018.12.004
• Taheri-Tehrani, Parsa, Anthony Dorian Challoner, and David A. Horsley. 2018. “Micromechanical Rate Integrating Gyroscope with Angle-Dependent Bias Compensation Using a Self-Precession Method.” IEEE Sensors Journal 18 (9): 3533–43. https://doi.org/10.1109/jsen.2018.2810843
• 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
• Tahk, Min-Jea, Eui-Taek Jeong, Chang-Hun Lee, and Sung-Jin Yoon. 2024. “Attitude Hold Proportional Navigation Guidance for Interceptors with off-Axis Seeker.” Journal of Guidance, Control, and Dynamics 47 (5): 1015–25. https://doi.org/10.2514/1.g007806
• Tai, Shang, Lixin Wang, Yanling Wang, Chen Bu, and Ting Yue. 2023a. “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
• Tai, Shang, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu, and Ting Yue. 2023b. “Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test.” Aerospace 10 (4): 350. https://doi.org/10.3390/aerospace10040350
• “Tailoring Theory to Practice in Tactical Missile Control.” 1999. IEEE Control Systems 19 (6): 49–55. https://doi.org/10.1109/37.806916
• Tait, Gregory, Michael Hatfield, Bradley Bernard, and Manuel Rodriguez. 2009. “Electromagnetic Complex Cavity Characterization of a Fighter Aircraft Main Weapons Bay.” In 2009 IEEE International Symposium on Electromagnetic Compatibility. IEEE. https://doi.org/10.1109/isemc.2009.5284712
• Takahashi, Ryuhei, Kazufumi Hirata, Teruyuki Hara, and Atsushi Okamura. 2012. “Derivation of Monopulse Angle Accuracy for Phased Array Radar to Achieve Cramer-Rao Lower Bound.” In 2012 IEEE International Conference on Acoustics, Speech and Signal Processing (ICASSP). IEEE. https://doi.org/10.1109/icassp.2012.6288441
• Takahashi, Hidemi, Hidetoshi Iijima, Mitsuru Kurita, and Seigo Koga. 2019. “Evaluation of Skin Friction Drag Reduction in the Turbulent Boundary Layer Using Riblets.” Applied Sciences 9 (23): 5199. https://doi.org/10.3390/app9235199
• Takahashi, Ryuhei, Takayuki Inaba, Toru Takahashi, and Hirohisa Tasaki. 2018. “Digital Monopulse Beamforming for Achieving the CRLB for Angle Accuracy.” IEEE Transactions on Aerospace and Electronic Systems 54 (1): 315–23. https://doi.org/10.1109/taes.2017.2756519
• Takashima, M., S. Yoshizawa, and J. Nagumo. 1980. “Human Operator Dynamics in Manual Tracking Systems with Auditory Input.” Biological Cybernetics 37 (3): 159–66. https://doi.org/10.1007/bf00355454
• Takeshi Yamasaki, Hirotoshi Sakaida, Keisuke Enomoto, Hiroyuki Takano, and Yoriaki Baba. 2007. “Robust Trajectory-Tracking Method for UAV Guidance Using Proportional Navigation.” In 2007 International Conference on Control, Automation and Systems. IEEE. https://doi.org/10.1109/iccas.2007.4406558
• Talole, S. E., and Ravi N. Banavar. 1998. “Proportional Navigation through Predictive Control.” Journal of Guidance, Control, and Dynamics 21 (6): 1004–6. https://doi.org/10.2514/2.4339
• Talole, S. E., A. Ghosh, and S. B. Phadke. 2006. “Proportional Navigation Guidance Using Predictive and Time Delay Control.” Control Engineering Practice 14 (12): 1445–53. https://doi.org/10.1016/j.conengprac.2005.11.003
• Tamer, Aykut. 2021. “Aeroelastic Response of Aircraft Wings to External Store Separation Using Flexible Multibody Dynamics.” Machines 9 (3): 61. https://doi.org/10.3390/machines9030061
• Tamhane, Bhagyashri, Shailaja Kurode, and Prasad Parkhi. 2016. “Novel Two-Stage Observer for Line-of-Sight Rate Estimation.” Journal of Guidance, Control, and Dynamics 39 (11): 2586–93. https://doi.org/10.2514/1.g002063
• Tan, Xiaojun. 2019. “A Novel Sliding Mode Guidance Law with Impact Angle and Time Constraints.” In 2019 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac48633.2019.8997296
• Tan, Adrian Eng-Choon, Michael Yan-Wah Chia, and Karumudi Rambabu. 2007. “Angle Accuracy of Antenna Noise Corrupted Ultra-Wideband Monopulse Receiver.” In 2007 IEEE International Conference on Ultra-Wideband. IEEE. https://doi.org/10.1109/icuwb.2007.4381012
• Tan, Gaoyong, Hongbing Luo, Haibo Ji, Fei Liao, and Wenhua Wu. 2021. “Cooperative Line-of-Sight Guidance Laws for Active Aircraft Defense in Three-Dimensional Space.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550616
• Tan, Gaoyong, Hongbing Luo, Fei Liao, Xinghu Wang, and Haibo Ji. 2022. “Cooperative Strategy for Aircraft Defense Line-of-Sight Guidance in Three-Dimensional Space.” In 2022 41st Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc55666.2022.9902492
• 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, Xin, Chaoqi Wang, Yang Fang, Bai Wu, Dongyan Zhao, and Jiansheng Hu. 2024. “Radar Target Radar Cross-Section Measurement Based on Enhanced Imaging and Scattering Center Extraction.” Sensors 24 (19): 6315. https://doi.org/10.3390/s24196315
• Tang, Meng, Yun Huang, Xiangdong Zhu, Qinghua Zeng, Xiaohu Zhu, and Xincheng Wang. 2026. “Research on the Variable-Thrust Dynamic Characteristics of the Dual-Thrust-Chamber Staged Catalytic Decomposition Cycle H2O2/kerosene Rocket Engine.” Acta Astronautica 249: 737–53. https://doi.org/10.1016/j.actaastro.2026.07.046
• Tang, Jiang, Xiaofang Xie, Qinghua Chen, and Tao Sun. 2012. “Research on Missile Remote Control Data Link Simulation.” In 2012 2nd International Conference on Consumer Electronics, Communications and Networks (CECNet). IEEE. https://doi.org/10.1109/cecnet.2012.6201893
• Tang, Xingyuan, Libin Zeng, Kaixin Deng, et al. 2024. “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
• Tang, Qinhong, Jiufen Zhao, Shaokun Shi, and Zhifeng Zhao. 2017. “Design of Omnidirectional Steepest Roll Control Law for Vertical Launching Missile.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028304
• Tanno, H., A. Paull, and R. J. Stalker. 2001. “Skin-Friction Measurements in a Supersonic Combustor with Crossflow Fuel Injection.” Journal of Propulsion and Power 17 (6): 1333–38. https://doi.org/10.2514/2.5883
• Tao, Li, Zhang Yi, Yang Dan, et al. 2023. “Design and Implement for Infrared Imaging Strapdown Seeker Simulation and Test System.” In 2023 42nd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc58697.2023.10240152
• Tao, Zhengxin, and Shifeng Zhang. 2026. “Cooperative Guidance Method for Seeker-Less Missile and Beacon Aircraft.” Journal of Systems Engineering and Electronics 37 (2): 687–96. https://doi.org/10.23919/jsee.2026.000094
• Tao, Min, Yuxuan Zhang, and Xianfeng Zhang. 2024. “Low-Angle Tracking of Shipborne Radar.” In 2024 IEEE 6th International Conference on Power, Intelligent Computing and Systems (ICPICS). IEEE. https://doi.org/10.1109/icpics62053.2024.10796622
• Tao Guo, Qunli Xia, and Zaikang Qi. 2010. “Study on Strapdown Decoupling Technology for Rolling Missile Using RF Interferometer Seeker.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5632400
• Tardioli, Luca, Giovanni Franzini, Lorenzo Pollini, and Mario Innocenti. 2016. “Development of a Visibility Augmented Proportional Navigation Guidance: A Game-Theoretic Approach.” In 2016 IEEE 55th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc.2016.7799212
• Tatiya, Mayuri, Namrata Bhatia, and Radhakant Padhi. 2010. “Impact Angle Constrained Suboptimal Terminal Guidance of Interceptors for Air Defence.” IFAC Proceedings Volumes 43 (15): 130–35. https://doi.org/10.3182/20100906-5-jp-2022.00023
• Tavares, Yuri M., and Jacques Waldmann. 2023. “H∞ Loop Shaping Using Polytopic Weights and Pole Assignment to Missile Autopilot.” IEEE Access 11: 125–33. https://doi.org/10.1109/access.2022.3232464
• Tekin, Raziye, and Koray S. Erer. 2015b. “Switched-Gain Guidance for Impact Angle Control under Physical Constraints.” Journal of Guidance, Control, and Dynamics 38 (2): 205–16. https://doi.org/10.2514/1.g000766
• Tekin, Raziye, Koray S. Erer, and Florian Holzapfel. 2017a. “Adaptive Impact Time Control via Look-Angle Shaping under Varying Velocity.” Journal of Guidance, Control, and Dynamics 40 (12): 3247–55. https://doi.org/10.2514/1.g002981
• Tekin, Raziye, Koray S. Erer, and Florian Holzapfel. 2017b. “Polynomial Shaping of the Look Angle for Impact-Time Control.” Journal of Guidance, Control, and Dynamics 40 (10): 2668–73. https://doi.org/10.2514/1.g002751
• “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
• Tembhurnikar, Payal, Mrunal Bhosale, Pramila Bote, Shreya Jadhav, Vijaykumar Gorfad, and Devabrata Sahoo. 2021. “Computational Analysis of Flow Field over Missile Separated from Weapon Bay Cavity at Mach 2 and 5.” In 2021 IEEE Pune Section International Conference (PuneCon). IEEE. https://doi.org/10.1109/punecon52575.2021.9686526
• Temsah, Yehya, Ali Jahami, and Charles Aouad. 2021. “Silos Structural Response to Blast Loading.” Engineering Structures 243: 112671. https://doi.org/10.1016/j.engstruct.2021.112671
• Tervo, Kalevi. 2010. “Discrete Data-Based State Feedback Model of Human Operator.” In Proceedings of 2010 IEEE/ASME International Conference on Mechatronic and Embedded Systems and Applications. IEEE. https://doi.org/10.1109/mesa.2010.5552074
• Thai, Sovanna, Spilios Theodoulis, Clément Roos, and Jean-Marc Biannic. 2019. “Robust Design for the Roll-Channel Autopilot of a Canard-Guided Dual-Spin Projectile.” IFAC-PapersOnLine 52 (12): 232–37. https://doi.org/10.1016/j.ifacol.2019.11.248
• 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
• 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, Vincent Gassmann, Thomas Brunner, and Philippe Wernert. 2013. “Fixed Structure Robust Control Design for the 155mm Canard-Guided Projectile Roll-Channel Autopilot.” In 21st Mediterranean Conference on Control and Automation. IEEE. https://doi.org/10.1109/med.2013.6608714
• “Theoretical Accuracy of Monopulse Radar Receivers.” 1966. IEEE Transactions on Aerospace and Electronic Systems AES-2 (2): 234–36. https://doi.org/10.1109/taes.1966.4501749
• “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
• Thorat, Ashutosh A., Abhishek Dixit, and Pooja Agrawal. 2023. “Gimbal Stabilization on a Missile Seeker with a Fractional Order PID Controller.” In 2023 14th International Conference on Computing Communication and Networking Technologies (ICCCNT). IEEE. https://doi.org/10.1109/icccnt56998.2023.10307678
• Thornton, Charles E., R. Michael Buehrer, and Anthony F. Martone. 2022. “Online Meta-Learning for Scene-Diverse Waveform-Agile Radar Target Tracking.” In 2022 IEEE Radar Conference (RadarConf22). IEEE. https://doi.org/10.1109/radarconf2248738.2022.9763914
• Thukral, A., and M. Innocenti. 1998. “A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering.” IEEE Transactions on Control Systems Technology 6 (3): 359–71. https://doi.org/10.1109/87.668037
• Tian, Jiayi, Xibin Bai, Huabo Yang, and Shifeng Zhang. 2020c. “Time-Varying Asymmetric Barrier Lyapunov Function-Based Impact Angle Control Guidance Law with Field-of-View Constraint.” IEEE Access 8: 185346–59. https://doi.org/10.1109/access.2020.3030158
• Tian, Ye, Yuanli Cai, Zhenhua Yu, and Yifan Deng. 2019. “Three-Dimensional Fast Fixed-Time Convergence Guidance Law with Impact Angle Constraint.” IEEE Access 7: 180467–81. https://doi.org/10.1109/access.2019.2958312
• Tian, Jiayi, Neng Xiong, Shifeng Zhang, Huabo Yang, and Zhenyu Jiang. 2020b. “Integrated Guidance and Control for Missile with Narrow Field-of-View Strapdown Seeker.” ISA Transactions 106: 124–37. https://doi.org/10.1016/j.isatra.2020.06.012
• Tian, Yan, and Cai Yuan-li. 2019. “General Evasion Guidance for Air-Breathing Hypersonic Vehicles with Game Theory and Specified Miss Distance.” In 2019 IEEE 9th Annual International Conference on CYBER Technology in Automation, Control, and Intelligent Systems (CYBER). IEEE. https://doi.org/10.1109/cyber46603.2019.9066556
• Tian, Jiayi, Shifeng Zhang, and Huabo Yang. 2020a. “Enhanced Extended State Observer Based Control for Missile Acceleration Autopilot.” ISA Transactions 96: 143–54. https://doi.org/10.1016/j.isatra.2019.06.009
• 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
• Tong, Mu, Siu Shing Man, Ying Liu, and Liyuan Bao. 2026a. “The Dual Effects of Information Presentation Speed on Operator Performance in Dynamic Tasks: A Study in Supervisory Control and Data Acquisition Interfaces.” Ergonomics: 1–13. https://doi.org/10.1080/00140139.2026.2686854
• Topbaş, Eren, H. Deniz Karaca, Yiğit Yazicioğlu, and Çoşku Kasnakoğlu. 2024. “An Experimental Design-Based Approach for Modelling of Weapon Engagement Zone of an Air-to-Air Missile.” Journal of Simulation 19 (3): 349–64. https://doi.org/10.1080/17477778.2024.2403424
• Tournes, C., and C. D. Johnson. n.d. “Augmented Proportional Navigation Guidance Using Subspace-Stabilization.” In Proceedings of the Thirty-Fourth Southeastern Symposium on System Theory (Cat. No.02EX540). IEEE. https://doi.org/10.1109/ssst.2002.1027091
• Tracy, Cameron L., and David Wright. 2020. “Modeling the Performance of Hypersonic Boost-Glide Missiles.” Science & Global Security 28 (3): 135–70. https://doi.org/10.1080/08929882.2020.1864945
• Tracy, Cameron L., and David Wright. 2023. ““Computational Fluid Dynamics Analysis of the Infrared Emission from a Generic Hypersonic Glide Vehicle”—a Response.” Science & Global Security 31 (1–2): 41–47. https://doi.org/10.1080/08929882.2023.2215587
• Triplett, William E. 1984. “Wind Tunnel Correlation Study of Aerodynamic Modeling for F/A-18 Wing-Store Tip-Missile Flutter.” Journal of Aircraft 21 (5): 329–34. https://doi.org/10.2514/3.44968
• Tsalik, Ronny, and Tal Shima. 2016. “Optimal Guidance around Circular Trajectories for Impact-Angle Interception.” Journal of Guidance, Control, and Dynamics 39 (6): 1278–91. https://doi.org/10.2514/1.g001759
• 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
• Tsuru, Taira, Sadatake Tomioka, and Hiroyuki Yamasaki. 2011. “Accuracy of Direct Skin-Friction Measurements in High-Enthalpy Supersonic Flows.” AIAA Journal 49 (6): 1267–71. https://doi.org/10.2514/1.j050691
• 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
• Turetsky, Vladimir, and Valery Y. Glizer. 2004. “Zero Miss Interception Guidance: Cheap Control Approach.” IFAC Proceedings Volumes 37 (6): 635–40. https://doi.org/10.1016/s1474-6670(17)32247-4
• Turetsky, Vladimir, and Tal Shima. 2016a. “Hybrid Evasion Strategy against a Missile with Guidance Law of Variable Structure.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7525399
• Turetsky, Vladimir, and Tal Shima. 2016b. “Target Evasion from a Missile Performing Multiple Switches in Guidance Law.” Journal of Guidance, Control, and Dynamics 39 (10): 2364–73. https://doi.org/10.2514/1.g000461
• Tyan, Feng. 2015. “Analysis of General Ideal Proportional Navigation Guidance Laws.” Asian Journal of Control 18 (3): 899–919. https://doi.org/10.1002/asjc.1205
• Tyan, Feng, and Jeng Fu Shen. 2010. “SDRE Missile Guidance Law.” In IEEE Icca 2010. IEEE. https://doi.org/10.1109/icca.2010.5524364
• Uddin, Riaz, and Jeha Ryu. 2016. “Predictive Control Approaches for Bilateral Teleoperation.” Annual Reviews in Control 42: 82–99. https://doi.org/10.1016/j.arcontrol.2016.09.003
• Ulas, A., and E. Boysan. 2013. “Numerical Analysis of Regenerative Cooling in Liquid Propellant Rocket Engines.” Aerospace Science and Technology 24 (1): 187–97. https://doi.org/10.1016/j.ast.2011.11.006
• Ulybyshev, Yuri. 2005. “Terminal Guidance Law Based on Proportional Navigation.” Journal of Guidance, Control, and Dynamics 28 (4): 821–24. https://doi.org/10.2514/1.12545
• 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
• 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
• Urbano, A., L. Selle, G. Staffelbach, et al. 2016. “Exploration of Combustion Instability Triggering Using Large Eddy Simulation of a Multiple Injector Liquid Rocket Engine.” Combustion and Flame 169: 129–40. https://doi.org/10.1016/j.combustflame.2016.03.020
• Uricchio, William. 1990. “High-Definition Television, Big Screen Television and Television-Guided Missiles, 1945.” Historical Journal of Film, Radio and Television 10 (3): 311–15. https://doi.org/10.1080/01439689000260241
• Uselton, Bob L., and Leroy M. Jenke. 1977. “Experimental Missile Pitch- and Moll-Damping Characteristics at Large.” Journal of Spacecraft and Rockets 14 (4): 241–47. https://doi.org/10.2514/3.57188
• Vaganov, M. A., and V. I. Kazakov. 2019. “The Multichannel Optical Spectrometer for Diagnostics of the Liquid Propellant Rocket Engine.” In 2019 Wave Electronics and its Application in Information and Telecommunication Systems (WECONF). IEEE. https://doi.org/10.1109/weconf.2019.8840114
• Van, Hai Tran, Dien Nguyen Ngoc, and Pham Trung Dung. 2023. “Field-of-View and Impact Angle Constrained Guidance Law for Missile with Reducing Sensitivity on Initial Errors Based on Optimal Error Dynamics.” In 2023 12th International Conference on Control, Automation and Information Sciences (ICCAIS). IEEE. https://doi.org/10.1109/iccais59597.2023.10382396
• van der El, Kasper, Daan M. Pool, Marinus M. van Paassen, and Max Mulder. 2020. “Effects of Target Trajectory Bandwidth on Manual Control Behavior in Pursuit and Preview Tracking.” IEEE Transactions on Human-Machine Systems 50 (1): 68–78. https://doi.org/10.1109/thms.2019.2947577
• Van Winkle, E., and J. G. Rossi. 1966. “Neo-Modern Control Theory: Linear and Nonlinear Servomechanism Design.” IEEE Transactions on Industrial Electronics and Control Instrumentation IECI-13 (1): 72–82. https://doi.org/10.1109/tieci.1966.6592656
• Vashkevich, S. A., and M. E. Fedorov. 2003. “Raising the Accuracy of a Panoramic Monopulse Radar.” Measurement Techniques 46 (9): 912–18. https://doi.org/10.1023/b:mete.0000008453.97694.c4
• 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
• Venkatachari, Balaji Shankar, Gary C. Cheng, and Chau-Lyan Chang. 2020. “Effect of Counterflowing Jet on Supersonic Slender-Body Configurations: A Numerical Study.” Journal of Spacecraft and Rockets 57 (6): 1204–21. https://doi.org/10.2514/1.a34736
• Ventrice, M. B., J. C. Fang, and K. R. Purdy. 1979a. “Simulation of Liquid Propellant Rocket Engine Combustion InsEabilities.” AIAA Journal 17 (12): 1372–78. https://doi.org/10.2514/3.61316
• Vercher, J.-L., and G. M. Gauthier. 1992. “Oculo-Manual Coordination Control: Ocular and Manual Tracking of Visual Targets with Delayed Visual Feedback of the Hand Motion.” Experimental Brain Research 90 (3). https://doi.org/10.1007/bf00230944
• 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
• Vergez, Paul L., and James R. McClendon. 1982. “Optimal Control and Estimation for Strapdown Seeker Guidance of Tactical Missiles.” Journal of Guidance, Control, and Dynamics 5 (3): 225–26. https://doi.org/10.2514/3.19767
• Viinikainen, Mikko, Janne Tuominen, Pekka Alho, and Jouni Mattila. 2014. “Improving the Performance of DTP2 Bilateral Teleoperation Control System with Haptic Augmentation.” Fusion Engineering and Design 89 (9–10): 2278–82. https://doi.org/10.1016/j.fusengdes.2014.04.045
• Villanueva, Fredy M., and Hussain Abbas. 2015. “Small Launch Vehicle Optimal Design Configuration from Ballistic Missile Components.” In 2015 12th International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE. https://doi.org/10.1109/ibcast.2015.7058509
• Vinje, Edward W., and Edward T. Pitkin. 1972. “Human Operator Dynamics for Aural Compensatory Tracking.” IEEE Transactions on Systems, Man, and Cybernetics SMC-2 (4): 504–12. https://doi.org/10.1109/tsmc.1972.4309160
• Vinoth, M. S., Potharaju S. R. P. Saradhi, and Potharaju S. R. Aditya. 2009. “Intelligent Guided Missile.” In 2009 International Conference on Intelligent Agent & Multi-Agent Systems. IEEE. https://doi.org/10.1109/iama.2009.5228041
• Viswanath, Devan, and Dipankar Deb. 2012a. “Disturbance Observer Based Sliding Mode Control for Proportional Navigation Guidance.” IFAC Proceedings Volumes 45 (1): 163–68. https://doi.org/10.3182/20120213-3-in-4034.00031
• Viswanath, Devan, and Dipankar Deb. 2012b. “A New Nonlinear Guidance Law Formulation for Proportional Navigation Guidance.” In 2012 12th International Workshop on Variable Structure Systems. IEEE. https://doi.org/10.1109/vss.2012.6163500
• Vivek, A., and Satadal Ghosh. 2025. “Proportional-Navigation-Based All-Aspect Approach against Nonmaneuvering Target Using Phase-Plane Trajectory Shaping.” Journal of Guidance, Control, and Dynamics 48 (3): 537–54. https://doi.org/10.2514/1.g008450
• VlNH, N. X. 1964. “Comment on ‘‘Interception of High-Speed Target by Beam Rider Missile.’.” AIAA Journal 2 (2): 409–409. https://doi.org/10.2514/3.2316
• 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
• Walter, Leif, Gunther Schloffel, Spilios Theodoulis, Philippe Wernert, Ekaterina Kostina, and Florian Holzapfel. 2014. “Optimal Control and Numerical Optimization for Missile Interception Guidance.” In 2014 European Control Conference (ECC). IEEE. https://doi.org/10.1109/ecc.2014.6862503
• Wan, Shizheng, Xiaofei Chang, and Jie Yan. 2018. “Differentiator-Based Output-Feedback SlidingMode Control for Angle Constrained Midcourse Guidance.” In 2018 9th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae.2018.8467629
• Wang, Kent. 1991. “An Assessment of Tactical Surface-to-Air Missile Midcourse Guidance Technology.” In 1991 American Control Conference. IEEE. https://doi.org/10.23919/acc.1991.4791495
• Wang, Yiteng. 2015a. “Analysis of a Liquid Rocket Combustion Chamber Cooling.” In 2015 Eighth International Conference on Internet Computing for Science and Engineering (ICICSE). IEEE. https://doi.org/10.1109/icicse.2015.33
• Wang, Wendai. 2017. “Planning Reliability Demonstration Test with Performance Requirements.” In 2017 Annual Reliability and Maintainability Symposium (RAMS). IEEE. https://doi.org/10.1109/ram.2017.7889733
• Wang, Wuhong, and Herner Bubb. 2008. “A Theoretical Framework for Ecological Function Allocation in Human-Machine Interface.” In 2008 International Symposium on Knowledge Acquisition and Modeling. IEEE. https://doi.org/10.1109/kam.2008.131
• Wang, Wei, and Xiyuan Chen. 2018. “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, Jianan, Xiangjun Ding, Yadong Chen, Chunyan Wang, and Ming Xin. 2022d. “Field-of-View Constrained Three-Dimensional Impact Angle Control Guidance for Speed-Varying Missiles.” IEEE Transactions on Aerospace and Electronic Systems 58 (5): 3992–4003. https://doi.org/10.1109/taes.2022.3157807
• Wang, Jianan, Xiangjun Ding, Chunyan Wang, Kewei Xia, and Ming Xin. 2023b. “Look Angle Tracking Based Three-Dimensional Impact Time Control Guidance Law with Field-of-View Constraint.” International Journal of Robust and Nonlinear Control 33 (16): 9951–68. https://doi.org/10.1002/rnc.6886
• Wang, Chunyan, Wei Dong, Jianan Wang, and Ming Xin. 2022e. “Impact-Angle-Constrained Cooperative Guidance for Salvo Attack.” Journal of Guidance, Control, and Dynamics 45 (4): 684–703. https://doi.org/10.2514/1.g006342
• Wang, Xu, Junfang Fan, Denghui Dou, Yi Ji, Yafeng Li, and Jinmin Wu. 2023a. “A Deep Reinforcement Learning-Based Guidance Law with Impact Angle Constraint.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10451246
• Wang, Ziwei, Haolin Fei, Tao Xue, et al. 2025d. “Multilateral Collaborative Teleoperation with Self-Tuning Authority via Prescribed Performance Control.” In 2025 IEEE 64th Conference on Decision and Control (CDC). IEEE. https://doi.org/10.1109/cdc57313.2025.11312154
• Wang, Hui, Zuoyu Guan, and Lijun Yu. 2014a. “The Application of Proportional Navigation in the Process of UAV Air Combat Guidance and Optimization of Proportional Parameter.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896318
• Wang, Pengyu, Yanning Guo, Guangfu Ma, Chang-Hun Lee, and Bong Wie. 2022f. “New Look-Angle Tracking Guidance Strategy for Impact Time and Angle Control.” Journal of Guidance, Control, and Dynamics 45 (3): 545–57. https://doi.org/10.2514/1.g006229
• Wang, Yadong, Shaoming He, Jiang Wang, and Chang-Hun Lee. 2022b. “Dynamic Estimation and Compensation of Time Delay for Missiles with Strapdown Seeker.” Journal of Guidance, Control, and Dynamics 45 (4): 781–91. https://doi.org/10.2514/1.g006389
• Wang, Keran, Wenjun Hou, Huiwen Ma, and Leyi Hong. 2024d. “Eye-Tracking Characteristics: Unveiling Trust Calibration States in Automated Supervisory Control Tasks.” Sensors 24 (24): 7946. https://doi.org/10.3390/s24247946
• Wang, Xinxin, Xianlin Huang, Shuchen Ding, and Hongqian Lu. 2019b. “Fixed-Time Guidance Law for Intercepting Maneuvering Targets with Impact Angle Constraint.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866644
• Wang, Fude, Teng Li, Zhihu Kou, and Wenhao Li. 2022a. “Design Simulation and Development of Aircraft Air-Launch Platform.” In 2022 2nd International Conference on Algorithms, High Performance Computing and Artificial Intelligence (AHPCAI). IEEE. https://doi.org/10.1109/ahpcai57455.2022.10087863
• Wang, Shenghui, Kun Li, Yu Wang, and Haibo Ji. 2018e. “A Three-Dimensional Robust Nonlinear Guidance Law Considering Dynamics of Missile Autopilot.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018880
• Wang, Lei, Yanzhong Li, Zhixiang Zhao, and Zhan Liu. 2013c. “Transient Thermal and Pressurization Performance of LO2 Tank during Helium Pressurization Combined with outside Aerodynamic Heating.” International Journal of Heat and Mass Transfer 62: 263–71. https://doi.org/10.1016/j.ijheatmasstransfer.2013.03.021
• Wang, Mingguang, Guang Li, Lingxue Zhao, and Lixia Wei. 2021g. “Roll Controller Design for Miniature Air-to-Ground Missile Based on ADRC.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9549951
• Wang, Zhihua, Chengrui Liu, and Huimin Fu. 2011. “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, Yanping, Yutong Liu, Yang Li, Yun Lin, Wen Hong, and Ziheng Zhao. 2019d. “Millimeter-Wave Radar Imaging Reconstruction Based on Angle Accuracy Probability Model.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048515
• Wang, Chao, Yongshan Liu, and Jianmei Song. 2016b. “A Hardware-in-the-Loop Simulation for LOS Rate Estimation of Strapdown Seeker Based on EKF.” In 2016 14th International Conference on Control, Automation, Robotics and Vision (ICARCV). IEEE. https://doi.org/10.1109/icarcv.2016.7838644
• Wang, Dongli, Huaping Liu, Fuchun Sun, and Yonggui Du. 2012. “Shared Control Teleoperation for Targets Acquisition.” In 2012 24th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2012.6244584
• Wang, Tong, Xi Liu, Sheng Zhong, and Hangzai Luo. 2022j. “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, Xianghua, and Xiao Lu. 2018. “Three-Dimensional Impact Angle Constrained Distributed Guidance Law Design for Cooperative Attacks.” ISA Transactions 73: 79–90. https://doi.org/10.1016/j.isatra.2017.12.009
• Wang, Chenxing, Yueyong Lv, Pengyu Wang, and Yuxin Yang. 2027. “Impact-Angle-Constrained Cooperative Guidance Based on Varying-Gain Proportional Navigation.” Aerospace Science and Technology 180: 113701. https://doi.org/10.1016/j.ast.2026.113701
• Wang, Xinxin, and Xu Lyu. 2026. “Terminal Impact Angle and Field-of-View Constrained Guidance Law with Autopilot Dynamics.” Journal of the Franklin Institute 363 (12): 108794. https://doi.org/10.1016/j.jfranklin.2026.108794
• Wang, Haoliang, and Mengying Ma. 2024. “Trajectory Design in Boost Phase of Air-Launched Rocket Based on the Effective Specific Impulse.” In 2024 7th International Symposium on Autonomous Systems (ISAS). IEEE. https://doi.org/10.1109/isas61044.2024.10552537
• 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, S., M. Song, Y. Fei, et al. 2023e. “Prospect-Theoretic Modeling of Team Cognition for Task Allocation towards Human-Automation Symbiosis.” In 2023 IEEE International Conference on Industrial Engineering and Engineering Management (IEEM). IEEE. https://doi.org/10.1109/ieem58616.2023.10406811
• Wang, Xiang Hua, and Chee Pin Tan. 2018. “3-D Impact Angle Constrained Distributed Cooperative Guidance for Maneuvering Targets without Angular-Rate Measurements.” Control Engineering Practice 78: 142–59. https://doi.org/10.1016/j.conengprac.2018.06.014
• Wang, Xiang Hua, Chee Pin Tan, and Li Ping Cheng. 2019c. “Impact Time and Angle Constrained Integrated Guidance and Control with Application to Salvo Attack.” Asian Journal of Control 22 (3): 1211–20. https://doi.org/10.1002/asjc.1991
• Wang, Ziyao, Shengjing Tang, and Jie Guo. 2022c. “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, Xianghua, and Jinzhi Wang. 2014a. “Partial Integrated Guidance and Control for Missiles with Three-Dimensional Impact Angle Constraints.” Journal of Guidance, Control, and Dynamics 37 (2): 644–57. https://doi.org/10.2514/1.60133
• Wang, Xianghua, and Jinzhi Wang. 2015. “Partial Integrated Guidance and Control with Impact Angle Constraints.” Journal of Guidance, Control, and Dynamics 38 (5): 925–36. https://doi.org/10.2514/1.g000141
• Wang, Sen, and Wei-Hong Wang. 2016. “Intercetp Angle Constrained Guidance Law Using Adaptive Extended State Observer.” In 2016 13th International Computer Conference on Wavelet Active Media Technology and Information Processing (ICCWAMTIP). IEEE. https://doi.org/10.1109/iccwamtip.2016.8079877
• 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, Yadong, Jiang Wang, Shaoming He, Hyo-Sang Shin, and Antonios Tsourdos. 2021f. “Optimal Guidance with Active Observability Enhancement for Scale Factor Error Estimation of Strapdown Seeker.” IEEE Transactions on Aerospace and Electronic Systems 57 (6): 4347–62. https://doi.org/10.1109/taes.2021.3096870
• Wang, Jiang, Yinhan Wang, Hongyan Li, and Yaning Wang. 2024a. “Analytical Optimal Counter Guidance against Proportional Navigation.” Journal of Guidance, Control, and Dynamics 47 (12): 2631–40. https://doi.org/10.2514/1.g008370
• Wang, Yaning, Hui Wang, Defu Lin, and Wei Wang. 2022g. “Nonlinear Guidance Laws for Maneuvering Target Interception with Virtual Look Angle Constraint.” IEEE Transactions on Aerospace and Electronic Systems 58 (4): 2807–22. https://doi.org/10.1109/taes.2021.3139845
• Wang, Kangjie, Junli Wang, Zhiyuan Liu, Sheng Zhang, Baosheng Zhang, and Wenyong Quan. 2024i. “Thermal Modal Analysis of Hypersonic Composite Wing on Transient Aerodynamic Heating.” Scientific Reports 14 (1): 11012. https://doi.org/10.1038/s41598-024-61900-y
• Wang, Zhengtao, Ningyu Wang, and Borui Tang. 2025b. “Impact Angle Control Guidance Law Considering Field-of-View Constraint Based on Deep Reinforcement Learning.” IFAC-PapersOnLine 59 (20): 793–98. https://doi.org/10.1016/j.ifacol.2025.11.249
• Wang, Zhe, Wen-Qin Wang, and Jie Xiong. 2016a. “Cognitive Target Tracking Using FDA Radar for Increased SINR Performance.” In 2016 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2016.7485252
• Wang, Sen, Weihong Wang, and Shaofeng Xiong. 2016c. “Impact Angle Constrained Three-Dimensional Integrated Guidance and Control for STT Missile in the Presence of Input Saturation.” ISA Transactions 64: 151–60. https://doi.org/10.1016/j.isatra.2016.04.026
• Wang, Junxiang, Xianpeng Wang, Dingjie Xu, and Guoan Bi. 2018d. “Robust Angle Estimation for MIMO Radar with the Coexistence of Mutual Coupling and Colored Noise.” Sensors 18 (3): 832. https://doi.org/10.3390/s18030832
• Wang, Ziang, Lei Wang, Qi Yi, and Yimin Liu. 2025c. “An MARL Based Multi-Target Tracking Algorithm under Jamming against Radar.” In 2025 IEEE International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar52380.2025.11031502
• Wang, Kun, Zhenyu Wei, and Pengyu Wang. 2026. “Look-Angle-Shaped Impact Time Control Guidance with Field-of-View Constraints.” Aerospace Science and Technology 176: 112131. https://doi.org/10.1016/j.ast.2026.112131
• Wang, Ju, Si-liang Wu, and Xiao-lin Shi. 2006a. “Investigation of Maneuvering Target Localization in Vector Miss Distance Measurement System.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.346119
• Wang, Zhuo, Zhenyu Wu, Tao Wang, and Bo Zhang. 2021b. “Development of Infrared-Guided Missile Precision Detection Simulator.” Machines 9 (9): 198. https://doi.org/10.3390/machines9090198
• Wang, Weihong, Shaofeng Xiong, Sen Wang, Siyang Song, and Chao Lai. 2016f. “Three Dimensional Impact Angle Constrained Integrated Guidance and Control for Missiles with Input Saturation and Actuator Failure.” Aerospace Science and Technology 53: 169–87. https://doi.org/10.1016/j.ast.2016.03.015
• Wang, Xinglong, Zhe Xu, Xuemei Wang, Jun Zhang, and Hongbin Qiu. 2018c. “Research on Filtering Method of Monopulse Radar Angular Glint Suppression.” In 2018 IEEE 3rd Advanced Information Technology, Electronic and Automation Control Conference (IAEAC). IEEE. https://doi.org/10.1109/iaeac.2018.8577577
• Wang, Chengze, Jiamin Yan, Rui Lyu, Zhuo Liang, and Yang Chen. 2024g. “Optimal Guidance Law for Critical Safe Miss Distance Evasion.” Aerospace 11 (12): 1041. https://doi.org/10.3390/aerospace11121041
• Wang, Xianghua, and Qiwei Yang. 2017. “Cooperative Guidance Law Design for Salvo Attacks with Impact Angle Constraint.” In 2017 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2017.8243335
• Wang, Pei, and Ke Zhang. 2014. “Research on Line-of-Sight Rate Extraction of Strapdown Seeker.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896740
• Wang, Peng, and Xiaobing Zhang. 2022. “Inverse Optimal Missile Guidance Law under Constraints Based on Prescribed-Time Explicit Reference Governor.” ISA Transactions 129: 395–404. https://doi.org/10.1016/j.isatra.2021.12.016
• Wang, Chenfei, Xiaoyu Zhang, and Fie Dong. 2024h. “Terminal Guidance Law of Missile Based on Soft Actor-Critic with Impact Angle Constraint.” In 2024 43rd Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc63176.2024.10661814
• Wang, Xingliang, Youan Zhang, and Huali Wu. 2016e. “Sliding Mode Control Based Impact Angle Control Guidance Considering the Seeker׳s Field-of-View Constraint.” ISA Transactions 61: 49–59. https://doi.org/10.1016/j.isatra.2015.12.018
• Wang, Huaji, Dayuan Zhang, Tao Zhang, Humin Lei, Yexing Wang, and Pengfei Zhang. 2018a. “Capturability Analysis of Pure Proportional Navigation Guidance Law for Intercepting Hypersonic Targets.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019183
• Wang, Jieyao, Shiyong Zhong, and Yong Jiang. 2016d. “Involute Guidance Laws with Terminal Impact Angle Constraints.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828782
• Wang Ju and Wu Siliang. 2004. “Investigation of Multiple Target Location in Vector Miss Distance Measurement Syatem.” In Proceedings 7th International Conference on Signal Processing, 2004. Proceedings. ICSP ‘04. 2004., vol. 3. IEEE. https://doi.org/10.1109/icosp.2004.1442169
• Wang Xiaofang and Lin Hai. 2010. “Research on Shooter Modeling of Image Guided Missile Based on Neural Network.” In 2010 2nd International Conference on Advanced Computer Control. IEEE. https://doi.org/10.1109/icacc.2010.5487155
• Wang Yandong. 2011. “Scanning Program of Image Guided Missile Basing on Parabolic Trajectory.” In 2011 3rd International Conference on Advanced Computer Control. IEEE. https://doi.org/10.1109/icacc.2011.6016436
• Wang Zhi and Liu Zhi-ping. 2010. “Aero-Elastic Stability Design of Spinning Ballistic Missile with Sliding Mode Control.” In 2010 International Conference On Computer Design and Applications. IEEE. https://doi.org/10.1109/iccda.2010.5541016
• Waymeyer, W. K., and T. H. Young. 1964. “Coupling in Cruciform-Missile Control Systems.” IEEE Transactions on Applications and Industry 83 (75): 397–401. https://doi.org/10.1109/tai.1964.5407710
• Wazzan, Ahmed R., and W. H. Ball. 1965. “Body Shape Effects on Skin Friction in Supersonic Flow.” AIAA Journal 3 (9): 1770–72. https://doi.org/10.2514/3.55194
• Webb, Jeremy D., Songpo Li, and Xiaoli Zhang. 2016. “Using Visuomotor Tendencies to Increase Control Performance in Teleoperation.” In 2016 American Control Conference (ACC). IEEE. https://doi.org/10.1109/acc.2016.7526794
• Wei, Kai, Shaosong Chen, Dongdong Tang, Yihang Xu, Xujian Lyu, and Qing Chen. 2024a. “Evolution and Influence of Multivortex Structure on the Head of Canard-Controlled Missile at High Angle of Attack.” International Journal of Aerospace Engineering 2024 (1): 6074417. https://doi.org/10.1155/2024/6074417
• Wei, Kai, Shaosong Chen, Dongdong Tang, Yihang Xu, Xujian Lyu, and Qing Chen. 2024b. “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, Xiqing, Sha Du, and Jiandun Li. 2025. “Impact Angle Constrained Adaptive Prescribed Time Guidance against Maneuvering Target.” International Journal of Aerospace Engineering 2025 (1): 4935747. https://doi.org/10.1155/ijae/4935747
• Wei, Changzhu, Yepeng Han, Naigang Cui, and Hechuan Xu. 2017. “Fifth-Degree Cubature Kalman Filter Estimation of Seeker Line-of-Sight Rate Using Augmented-Dimensional Model.” Journal of Guidance, Control, and Dynamics 40 (9): 2355–62. https://doi.org/10.2514/1.g002809
• Wei, Xiaofang, Chaofang Hu, and Na Wang. 2019a. “Fault-Tolerant Control for Disturbed Hypersonic Vehicle Based on Tube-MPC.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866177
• Wei, Xiaokai, Jie Li, Debiao Zhang, et al. 2019b. “Optimization of a New High Rotary Missile-Borne Stabilization Platform.” Sensors 19 (19): 4143. https://doi.org/10.3390/s19194143
• Wei, Yiyin, Wangkui Liu, and Guangren Duan. 2016. “Missile Guidance Law with Impact Angle Constraint and Acceleration Saturation.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7554186
• Wei, Gao, Chen Songsong, and Hu Xiaoguang. 2012. “Design Scheme of Seeker Equivalent Device of Missile-Borne Synthetic Aperture Radar.” In IEEE 10th International Conference on Industrial Informatics. IEEE. https://doi.org/10.1109/indin.2012.6301376
• Wei Liu, Tao Zeng, and Teng Long. 2002. “Simulation on Characteristic of Angle-Tracking for Semi-Continuous Wave Radar.” In 6th International Conference on Signal Processing, 2002., vol. 2. IEEE. https://doi.org/10.1109/icosp.2002.1180063
• Wei Sun and M. Amin. 2003. “A Self-Coherence Based Anti-Jam GPS Receiver.” In IEEE Workshop on Statistical Signal Processing, 2003. IEEE. https://doi.org/10.1109/ssp.2003.1289340
• Wei Wang, Xianpeng Wang, and Xin Li. 2011. “An Angle Estimation Algorithm for MIMO Radar in the Presence of Colored Noise Fields.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159484
• Wei Yan and Zhaoda Zhu. 1996. “Target Tracking with Glint Noise Using an RBF Neural Network.” In Proceedings of the IEEE 1996 National Aerospace and Electronics Conference NAECON 1996, vol. 1. IEEE. https://doi.org/10.1109/naecon.1996.517649
• Wei-dong, Qin, Can-bin Yin, and Xin Jia. 2009. “A Novel Algorithm for Missile Borne Linear Array Antenna Synthetic Aperture Radar Imaging.” In 2009 4th IEEE Conference on Industrial Electronics and Applications. IEEE. https://doi.org/10.1109/iciea.2009.5138388
• 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
• Weiguo, Wang, Yang Suochang, Zhang Jianguo, and Sun Mingliang. 2011. “The Design of Test System for Launcher Equipment of One Air Defence Missile Based on FPGA.” In 2011 First International Conference on Instrumentation, Measurement, Computer, Communication and Control. IEEE. https://doi.org/10.1109/imccc.2011.160
• Weijie, Kong, Yuan Hao, Li Peng, and Zheng Zhiqiang. 2016. “Adaptive Higher Order Sliding Mode Attitude Control for Hypersonic Glide Vehicles.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7553885
• 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
• Weiss, Martin. 2005. “Adjoint Method for Missile Performance Analysis on State-Space Models.” Journal of Guidance, Control, and Dynamics 28 (2): 236–48. https://doi.org/10.2514/1.7342
• Weiss, Martin, and Domenic Bucco. 2015. “Adjoint Method for Hybrid Guidance Loop State-Space Models.” Journal of Guidance, Control, and Dynamics 38 (4): 614–22. https://doi.org/10.2514/1.62954
• Weiss, Martin, and Tal Shima. 2015. “Optimal Linear-Quadratic Missile Guidance Laws with Penalty on Command Variability.” Journal of Guidance, Control, and Dynamics 38 (2): 226–37. https://doi.org/10.2514/1.g000738
• Weiss, Martin, and Tal Shima. 2016. “Minimum Effort Pursuit/Evasion Guidance with Specified Miss Distance.” Journal of Guidance, Control, and Dynamics 39 (5): 1069–79. https://doi.org/10.2514/1.g001623
• Weiss, Martin, and Tal Shima. 2019. “Linear Quadratic Optimal Control-Based Missile Guidance Law with Obstacle Avoidance.” IEEE Transactions on Aerospace and Electronic Systems 55 (1): 205–14. https://doi.org/10.1109/taes.2018.2849901
• Weiss, Martin, and Tal Shima. 2021. “Linear Quadratic Minimum-Effort, Specify-Performance Approach to Missile Guidance.” Journal of Guidance, Control, and Dynamics 44 (3): 559–71. https://doi.org/10.2514/1.g005017
• Welch, D. L. n.d. “Design Enhancement through Human Factored Function Allocation.” In AIAA/IEEE Digital Avionics Systems Conference. 13th DASC. IEEE. https://doi.org/10.1109/dasc.1994.369463
• Well, Klaus H. 1990. “Medium Range Intercept Maneuvers with a Missile.” In 1990 American Control Conference. IEEE. https://doi.org/10.23919/acc.1990.4791147
• Wen, Zhengyou, Zonghua Sun, and Liaoni Wu. 2027. “Prescribed-Time-MFESO-Based Attitude Control with Control Barrier Functions for Hypersonic Stage Separation under Hinge-Moment Constraints.” Aerospace Science and Technology 180: 113659. https://doi.org/10.1016/j.ast.2026.113659
• Wen, Fangqing, Xiaodong Xiong, Jian Su, and Zijing Zhang. 2017. “Angle Estimation for Bistatic MIMO Radar in the Presence of Spatial Colored Noise.” Signal Processing 134: 261–67. https://doi.org/10.1016/j.sigpro.2016.12.017
• Wen-jin Gu, Jin-yong Yu, and Ru-chuan Zhang. 2007. “A Three-Dimensional Missile Guidance Law with Angle Constraint Based on Sliding Mode Control.” In 2007 IEEE International Conference on Control and Automation. IEEE. https://doi.org/10.1109/icca.2007.4376367
• Wenfeng, Ma, Wang Peng, and Tang Guojian. 2017. “Adaptive Control for Hypersonic Vehicle Based on Error Characteristic Model.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8027899
• 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
• Weng-Rong Wu. 1993. “Target Racking with Glint Noise.” IEEE Transactions on Aerospace and Electronic Systems 29 (1): 174–85. https://doi.org/10.1109/7.249123
• Wenyuan, Zhou, Xu Bo, Li Sen, Rao Sihang, Xu Hui, and Xu Xu. 2025. “Research on Flow and Heat Transfer of Regenerative Cooling in Thrust Chamber of Space Orbit Control Engine.” In 2025 11th International Conference on Mechanical Engineering and Aerospace Engineering (MEAE). IEEE. https://doi.org/10.1109/meae68077.2025.11557652
• Wenzhun, Huang, Wang Yongsheng, and Ye Xiangyang. 2008. “Studies on Novel Anti-Jamming Technique of Unmanned Aerial Vehicle Data Link.” Chinese Journal of Aeronautics 21 (2): 141–48. https://doi.org/10.1016/s1000-9361(08)60018-7
• West, Charles F. 1954. “The Integrated Air Force Missile Test Center Data Processing Facility.” Transactions of the IRE Professional Group on Radio Telemetry and Remote Control 1 (1): 1–7. https://doi.org/10.1109/tpgrt.1954.4335624
• White, W. D. 1974. “Low-Angle Radar Tracking in the Presence of Multipath.” IEEE Transactions on Aerospace and Electronic Systems AES-10 (6): 835–52. https://doi.org/10.1109/taes.1974.307892
• 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
• White, B. A., R. Zbikowski, and A. Tsourdos. 2003. “Aim Point Guidance: An Extension of Proportional Navigation to the Control of Terminal Guidance.” In Proceedings of the 2003 American Control Conference, 2003., vol. 1. IEEE. https://doi.org/10.1109/acc.2003.1238978
• Wideman, Jeffrey K., James L. Brown, John B. Miles, and Oktay Ozcan. 1995. “Skin-Friction Measurements in Three-Dimensional, Supersonic Shock-Wave/boundary-Layer Interaction.” AIAA Journal 33 (5): 805–11. https://doi.org/10.2514/3.12503
• Wilde, R. W., and J. H. Westcott. 1963. “The Characteristics of the Human Operator Engaged in a Tracking Task.” Automatica 1 (1): 5–19. https://doi.org/10.1016/0005-1098(63)90003-7
• Wilkins, M. L. 1971. “Calculation of a Slender Body Moving through Air at Supersonic and Subsonic Velocities.” AIAA Journal 9 (10): 2073–75. https://doi.org/10.2514/3.6469
• Williams, D. T., and W. H. Boykin. 1979. “Millimeter-Wave Missile Seeker Aimpoint Wander Phenomenon.” Journal of Guidance and Control 2 (3): 196–203. https://doi.org/10.2514/3.55861
• 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
• Willman, Warren W. 1988. “Effects of Strapdown Seeker Scale-Factor Uncertainty on Optimal Guidance.” Journal of Guidance, Control, and Dynamics 11 (3): 199–206. https://doi.org/10.2514/3.20294
• Willumeit, H. P. 1987. “Human Decision Making and Manual Control.” Applied Ergonomics 18 (3): 249. https://doi.org/10.1016/0003-6870(87)90022-6
• Wilson, R. F., J. R. Cloutier, and R. K. Yedavalli. 1992. “Lyapunov-Constrained Eigenstructure Assignment for the Design of Robust Mode-Decoupled Roll-Yaw Missile Autopilots.” In [Proceedings 1992] The First IEEE Conference on Control Applications. IEEE. https://doi.org/10.1109/cca.1992.269786
• Wilson, Kevin J., and Malcolm Farrow. 2021. “Assurance for Sample Size Determination in Reliability Demonstration Testing.” Technometrics 63 (4): 523–35. https://doi.org/10.1080/00401706.2020.1867646
• 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, Kevin A. 1991. “Missile Autopilot Robustness to Uncertain Aerodynamics: Stability Hypersphere Radius Calculation.” Journal of Guidance, Control, and Dynamics 14 (1): 166–75. https://doi.org/10.2514/3.20618
• Wise, Kevin A. 1993. “Missile Autopilot Robustness Using the Real Multiloop Stability Margin.” Journal of Guidance, Control, and Dynamics 16 (2): 354–62. https://doi.org/10.2514/3.21010
• 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
• Worms, J. G. 1998. “Monopulse Estimation and SLC Configurations.” In Proceedings of the 1998 IEEE Radar Conference, RADARCON’98. Challenges in Radar Systems and Solutions (Cat. No.98CH36197). IEEE. https://doi.org/10.1109/nrc.1998.677977
• Wright, James W. 1984. “Radar Glint-A Survey.” Electromagnetics 4 (2–3): 205–27. https://doi.org/10.1080/02726348408908114
• Wright, David. 2015. “Research Note to Hypersonic Boost-Glide Weapons by James M. Acton: Analysis of the Boost Phase of the HTV-2 Hypersonic Glider Tests.” Science & Global Security 23 (3): 220–29. https://doi.org/10.1080/08929882.2015.1088734
• Wright, Peter, Andy Dearden, and Bob Fields. 2000. “Function Allocation: A Perspective from Studies of Work Practice.” International Journal of Human-Computer Studies 52 (2): 335–55. https://doi.org/10.1006/ijhc.1999.0292
• 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, Xiaoyue. 2009. “Reliability Demonstration Test Model for Binomial System with Reliability Growth.” In 2009 8th International Conference on Reliability, Maintainability and Safety. IEEE. https://doi.org/10.1109/icrms.2009.5270170
• Wu, Xiangyang, Shihua Bi, Zheng Zhu, and Weinan Wu. 2014a. “Adaptive Sliding Mode Control for Missile Guidance Law.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896757
• Wu, Fanchen, Zheng Chen, Xueming Shao, and Kun Wang. 2025d. “Nonlinear Optimal Guidance with Constraints on Impact Time and Impact Angle.” Automatica 181: 112500. https://doi.org/10.1016/j.automatica.2025.112500
• Wu, Rong, Yingzi Guan, Changzhu Wei, and Naigang Cui. 2018b. “Fixed-Time Disturbance Observer Based Nonsingular Fast Terminal Sliding Mode Guidance with Impact Angle Constraint.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018640
• Wu, Yifan, Yuxuan Li, Yuhao Shen, Lizhen Yang, Nan Wu, and Hai Lin. 2024b. “Beam Tracing with Physical Optics for Angular Glint Calculation in near Field.” In 2024 Photonics & Electromagnetics Research Symposium (PIERS). IEEE. https://doi.org/10.1109/piers62282.2024.10618174
• Wu, Yumei, Haifeng Li, and Yongli Yu. 2013a. “Design of Safety-Critical Software Reliability Demonstration Test Based on Bayesian Theory.” In 2013 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE). IEEE. https://doi.org/10.1109/qr2mse.2013.6625734
• Wu, Fen, Andy Packard, and Gary Balas. 2002. “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, Jiale, Chenguang Shi, Zhifeng Wu, and Jianjiang Zhou. 2026a. “Joint Beamforming Design for Low Probability of Intercept in Transmit Subaperturing MIMO Radar.” Journal of Systems Engineering and Electronics 37 (1): 94–103. https://doi.org/10.23919/jsee.2025.000098
• Wu, Ying, and Qi Wang. 2025. “Guidance Information Estimation for Strapdown Imaging Seeker by Using UKF.” In 2025 37th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc65474.2025.11090520
• Wu, Jiayang, Huabo Yang, Hao Yang, Jiexin Zhou, and Shifeng Zhang. 2025c. “Multiframe Target Localization with Strapdown Seeker Based on Self-Adaptive L-SHADE.” International Journal of Aerospace Engineering 2025 (1): 1619772. https://doi.org/10.1155/ijae/1619772
• Wu, Zihao, Fang Yangwang, and WenXing Fu. 2018c. “Multi-Missile Centralized Cooperative Guidance Law with Packet Loss.” In 2018 Chinese Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac.2018.8623667
• Wu, Nan, and Jia Yu. 2018. “Robust Controller Design of Hypersonic Vehicle in Uncertainty Models.” In 3rd International Conference on Electromechanical Control Technology and Transportation. SCITEPRESS - Science and Technology Publications. https://doi.org/10.5220/0006969302880293
• Wu, YanZhou, YuanWei Zeng, Jing Li, and Qi Yang. 2024a. “Assessment of Missile Health Status Based on Test Data Combination Weighting and Cloud Models.” In 2024 Global Reliability and Prognostics and Health Management Conference (PHM-Beijing). IEEE. https://doi.org/10.1109/phm-beijing63284.2024.10874523
• Wu Qiongzhi, Long Teng, Li Dan, and Wang Fei. 2001. “Conical Scan Step-Frequency Radar Signal Processing.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984783
• Wu Yanan, Zhang Ran, and Li Huifeng. 2016. “Terminal Guidance with Impact Angle Constraint Based on a Practical Flight Strategy.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828799
• Xia, Shuhan, Junfang Fan, Jiaqi Huang, Yi Ji, and Pei Pei. 2023. “An Adaptive Fading CKF-Based Method for Estimating the Line of Sight Rate with Strapdown Seeker.” In 2023 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac59555.2023.10450265
• Xia, Lei, and Yongzhi Sheng. 2023. “Fractional Order Differential Sliding Mode Guidance Law with Impact Angle Constraint.” In 2023 35th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc58219.2023.10326498
• Xia, Zhenhua, Yubin Song, and Xuke Zhu. 2025. “Skin-Friction Scaling in Compressible Turbulent Channel Flows.” AIAA Journal 63 (7): 2810–16. https://doi.org/10.2514/1.j065219
• Xia, Yingqing, and Penggen Xu. 2007. “Radar Target’s Angular Glint Based on the RCS.” In 2007 International Symposium on Microwave, Antenna, Propagation and EMC Technologies for Wireless Communications. IEEE. https://doi.org/10.1109/mape.2007.4393794
• Xiang, Shengwen, Hongqi Fan, and Qiang Fu. 2019. “Error Distribution of Zero-Effort Miss Distance under Mode Mismatch.” International Journal of Control 94 (3): 643–52. https://doi.org/10.1080/00207179.2019.1610579
• Xiang, Shengwen, Hongqi Fan, and Qiang Fu. 2020a. “Distribution of Miss Distance for Pursuit-Evasion Problem.” IEEE/CAA Journal of Automatica Sinica 7 (4): 1161–68. https://doi.org/10.1109/jas.2019.1911552
• Xiang, Jixin, Bing Sun, Taiping Wang, and Junya Yuan. 2020b. “Effects of Angled Film-Cooling on Cooling Performance in a GO2/GH2 Subscale Thrust Chamber.” Applied Thermal Engineering 166: 114627. https://doi.org/10.1016/j.applthermaleng.2019.114627
• Xiangyu, Sun, Chao Tao, Wang Songyan, and Yang Ming. 2015. “Impact Angle Constrained Terminal Guidance Based on Continuous Nonsmooth Control Method.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7259779
• Xiaofeng, Zhang, Zhu Xiaoping, and Yang Jun. 2011. “Design of Variable Structure Stability Control Loop for Anti-Air Missile with Swing Nozzle Thrust Vector Control.” In 2011 Third International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2011.254
• Xiaoxi, Cui, Lou Yingming, Wu Tao, Zhang Dongxiang, Wang Linping, and Zhang Nan. 2013. “Command Optimization for Missile Roll Autopilot.” In 2013 25th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2013.6561555
• Xie, Junhao, Xiaodong Feng, Yeshu Yuan, and Shaobin Li. 2010. “Application of Monopulse Techniques in Angle-Measuring of Single-Beam Mechanical Scanning Radar.” In 2010 3rd International Congress on Image and Signal Processing. IEEE. https://doi.org/10.1109/cisp.2010.5648282
• Xie, Yuan, Weijie Lu, Xiongfeng Liu, et al. 2026. “Experimental Study on the Operating Characteristics of a Nitrous Oxide/kerosene Pintle-Type Throttling Rocket Engine.” Aerospace Science and Technology 178: 112400. https://doi.org/10.1016/j.ast.2026.112400
• Xie, Da Gang, Nan Wu, Chun Wang, and Qi Feng Liu. 2012. “Anti-Jamming Performance Simulation of Tactical Data Link Communication System.” In ISAPE2012. IEEE. https://doi.org/10.1109/isape.2012.6408957
• Xie, Junhao, and Weiming Xiong. 2006. “Analysis of Angular Resolution with Angular Accuracy for Monopulse.” In 2006 International Radar Symposium. IEEE. https://doi.org/10.1109/irs.2006.4338079
• Xie, Mingchi, Wei Yi, Thia Kirubajaran, and Lingjiang Kong. 2016b. “Receive-Beam Allocation for Multiple Target Tracking with Distributed MIMO Radar Systems.” In 2016 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2016.7485153
• Xie, Mingchi, Wei Yi, and Lingjiang Kong. 2016a. “Joint Selection and Power Allocation Strategy for Target Tracking in Decentralized Multiple Radar Systems.” In 2016 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2016.7485307
• Xie, Huaying, Hongzhong Zhao, and Qiang Fu. 2009. “Taylor Expansion and Its Application in Missile-Borne SAR Imaging.” In 2009 2nd Asian-Pacific Conference on Synthetic Aperture Radar. IEEE. https://doi.org/10.1109/apsar.2009.5374291
• Xie, Huan, Lixia Zhao, Wei Li, Bin Chen, ShengLin Xia, and Jun Yin. 2019. “The Optimization Study on the Mitigation Strategy of Hinge Moment of Aircraft with Multi-Control Surfaces.” In 2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence (ICUSAI). IEEE. https://doi.org/10.1109/icusai47366.2019.9124755
• 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 Guo, Yang Li, Feng Liu, and Teng Long. 2008. “A Method of Improving Angle Precision of Conical Scan LFMCW Radar.” In 2008 International Conference on Radar. IEEE. https://doi.org/10.1109/radar.2008.4653959
• Xing, Huaixi, Qinghua Xing, and Kun Wang. 2023. “Radar Anti-Jamming Countermeasures Intelligent Decision-Making: A Partially Observable Markov Decision Process Approach.” Aerospace 10 (3): 236. https://doi.org/10.3390/aerospace10030236
• Xingqiong, Yang, and Wan Lin. 2009. “Reliability Demonstration Testing Procedure for Weibull Distribution about Zero Failure-Data.” In 2009 First International Workshop on Database Technology and Applications. IEEE. https://doi.org/10.1109/dbta.2009.124
• Xiong, Yu, Jianguo Guo, and Jun Zhou. 2019. “Sliding Mode Control for Integrated Missile Guidance and Control System.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8865764
• Xiong, Fenfen, Chao Li, Yue Zhao, and Xiao Hu. 2022. “Rocket Landing Guidance Using Convex Optimization and Proportional Navigation Considering Performance-Limited Engine.” Acta Astronautica 201: 209–23. https://doi.org/10.1016/j.actaastro.2022.07.033
• Xiong, Juntao, Feng Liu, and William A. Sirignano. 2020a. “Combustion Dynamics Simulation of a 30-Injector Rocket Engine.” Combustion Science and Technology 194 (9): 1914–42. https://doi.org/10.1080/00102202.2020.1847097
• Xiong, Juntao, Hugh Morgan, Jeremy Krieg, Feng Liu, and William A. Sirignano. 2020b. “Nonlinear Combustion Instability in a Multi-Injector Rocket Engine.” AIAA Journal 58 (1): 219–35. https://doi.org/10.2514/1.j058036
• Xiong, Shaofeng, Weihong Wang, Xiaodong Liu, Sen Wang, and Zengqiang Chen. 2014. “Guidance Law against Maneuvering Targets with Intercept Angle Constraint.” ISA Transactions 53 (4): 1332–42. https://doi.org/10.1016/j.isatra.2014.03.007
• Xiong, Yuanyi, and Wenchong Xie. 2022. “Multi-Difference Beams Adaptive Iterative Monopulse Estimation Method for Airborne Radar.” Digital Signal Processing 120: 103260. https://doi.org/10.1016/j.dsp.2021.103260
• Xu, Honglin, Weibo Chen, and Xiaolei Ning. 2016. “Simulation Research on Missile Tracking under the Guidance of Online Real Radar.” In Theory, Methodology, Tools and Applications for Modeling and Simulation of Complex Systems. Springer Singapore. https://doi.org/10.1007/978-981-10-2666-9_53
• 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, Dan, and Zhixin Feng. 2018. “A Fuzzy Bayesian Based Zero-Failure Accelerated Life Demonstration Test Design Method.” In 2018 Prognostics and System Health Management Conference (PHM-Chongqing). IEEE. https://doi.org/10.1109/phm-chongqing.2018.00037
• Xu, Qiangqiang, Jianquan Ge, and Tao Yang. 2020. “Multiple Missiles Cooperative Guidance Based on Proportional Navigation Guidance.” In 2020 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc49329.2020.9164151
• Xu, Xingyuan, and Chenxian Guo. 2015. “Capture Zone of Biased Proportional Navigation Guidance Law.” In 2015 IEEE International Conference on Information and Automation. IEEE. https://doi.org/10.1109/icinfa.2015.7279419
• Xu, Weijie, Yi Li, He Jia, and Shuo Tang. 2025b. “A Study on the Theoretical Model of Parachute Permeability under Supersonic and High-Pressure-Difference Conditions.” Aerospace Science and Technology 166: 110570. https://doi.org/10.1016/j.ast.2025.110570
• Xu, Xingyuan, and Zhizhong Liao. 2016. “Influence of Initial Heading Angle for the Optimal Guidance Law with Impact Angle Constraint.” In 2016 IEEE International Conference on Information and Automation (ICIA). IEEE. https://doi.org/10.1109/icinfa.2016.7831919
• Xu, Shengli, Mengwen Lu, Yuchen Zhou, Bo Zhang, and Hanqiao Huang. 2026a. “Bounded-Acceleration Impact Time Control Guidance Based on Look-Angle Shaping.” ISA Transactions 172: 105–17. https://doi.org/10.1016/j.isatra.2026.03.013
• Xu, Zhaoqing, and Hailong Pei. 2016. “Robust Controller Design for BTT Missile Equipped with Grid Fin.” In 2016 35th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2016.7555031
• Xu, Jing-Zhe, Huai-Lin Peng, Ming-Feng Ge, Zhi-Wei Liu, Huaicheng Yan, and Jie Liu. 2025a. “Hierarchical Prescribed-Performance Nonlinear Control for Teleoperation of Networked Secondary Robots with Coupling Constraints.” IEEE Transactions on Control of Network Systems 12 (1): 1006–17. https://doi.org/10.1109/tcns.2024.3431728
• Xu, Xin, Feng Shang, and Shuo Yang. 2022b. “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. “Air-Launched Rocket Attitude Control of Separation Stage Based on RCS.” In 2010 3rd International Conference on Advanced Computer Theory and Engineering(ICACTE). IEEE. https://doi.org/10.1109/icacte.2010.5579561
• Xu, Jiaxuan, and Haipeng Wang. 2019. “Synthetic Aperture Radar Jamming Semi-Physical Simulation System Based on NI PXI Platform.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048547
• Xu, Ke, Huanqing Wang, and Peter Xiaoping Liu. 2024b. “Predefined-Time Control for Single-Master-Multiple-Slave Teleoperation Systems with Prescribed Performance.” Nonlinear Dynamics 112 (15): 13233–47. https://doi.org/10.1007/s11071-024-09717-2
• Xu, Chen, Yang Wang, Zhiqi Niu, Sheng Luo, and Fenghuai Du. 2023. “Fixed-Time Convergent Guidance Law with Angle Constraint and Autopilot Lag Compensation Using Partial-State Feedback.” Aerospace 10 (11): 964. https://doi.org/10.3390/aerospace10110964
• Xu, Zhe, Zhu Yang, Xuemei Wang, Guohaojun Shao, and Hui Zhao. 2017. “Three-Dimensional Guidance Law with Attack Angle Constraint Considering the Dynamic Characteristics of the Control System.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028280
• Xu, Baoxiong, Jianxin Yi, Xianrong Wan, Feng Cheng, Ziping Gong, and Xiongtao Fu. 2021. “Effects of Measurement Model on Target Tracking Performance for Passive Bistatic Radar.” In 2021 CIE International Conference on Radar (Radar). IEEE. https://doi.org/10.1109/radar53847.2021.10028010
• 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
• Xue, Xiao-peng, Hiroto Koyama, Yoshiaki Nakamura, and Chih-Yung Wen. 2015a. “Effects of Suspension Line on Flow Field around a Supersonic Parachute.” Aerospace Science and Technology 43: 63–70. https://doi.org/10.1016/j.ast.2015.02.014
• Xue, Xiao-Peng, Yusuke Nishiyama, Yoshiaki Nakamura, Koichi Mori, and Chih-Yung Wen. 2015b. “Parametric Study on Aerodynamic Interaction of Supersonic Parachute System.” AIAA Journal 53 (9): 2796–2801. https://doi.org/10.2514/1.j053824
• Xue, Fei, Huaqiang Wang, Zenghui Jiang, and Yuchao Wang. 2020b. “Derivation and Verification of a Similarity Law for Wind-Tunnel Free-Flight Tests of Heavy-Store Separation.” Acta Astronautica 174: 123–30. https://doi.org/10.1016/j.actaastro.2020.04.061
• Xue, Fei, Yuchao Wang, and Han Qin. 2020a. “Derivation and Validation of Wind Tunnel Free-Flight Similarity Law for Store Separation from Aircraft.” Aerospace Science and Technology 97: 105614. https://doi.org/10.1016/j.ast.2019.105614
• Xue, Junqi, Xuchen Wu, Xiaopeng Yang, Manjun Lu, and Yao Yao. 2019a. “Adaptive Monopulse Angle Estimation Method for Distributed Radar in Presence of Mainlobe Jamming.” In 2019 IEEE International Conference on Signal, Information and Data Processing (ICSIDP). IEEE. https://doi.org/10.1109/icsidp47821.2019.9173028
• Xue, Liang, Bo Yang, Xinguo Wang, Guangbin Cai, Bin Shan, and Honglong Chang. 2023. “MIMU Optimal Redundant Structure and Signal Fusion Algorithm Based on a Non-Orthogonal MEMS Inertial Sensor Array.” Micromachines 14 (4): 759. https://doi.org/10.3390/mi14040759
• Xuehua, Weng, Chao Tao, Wang Songyan, and Yang Ming. 2015. “Terminal Angle Constrained Optimal Guidance Law with Finite Time Convergence.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260460
• Xueting Li, Wei Yi, Guolong Cui, Lingjiang Kong, and Xiaobo Yang. 2015. “Radar Selection for Single-Target Tracking in Radar Networks.” In 2015 IEEE Radar Conference (RadarCon). IEEE. https://doi.org/10.1109/radar.2015.7131058
• Yadav, Om Prakash, Nanua Singh, and Parveen S. Goel. 2006. “Reliability Demonstration Test Planning: A Three Dimensional Consideration.” Reliability Engineering & System Safety 91 (8): 882–93. https://doi.org/10.1016/j.ress.2005.09.001
• Yamasaki, Takeshi, S. N. Balakrishnan, and Hiroyuki Takano. 2013. “Modified Command to Line-of-Sight Intercept Guidance for Aircraft Defense.” Journal of Guidance, Control, and Dynamics 36 (3): 898–902. https://doi.org/10.2514/1.58566
• Yan, Pengpeng, Yonghua Fan, Zhe Liu, and Jin Zhang. 2017. “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, Han-xin, and Chun-lan Jiang. 2010. “Research on Terminal Efficiency of Air-Air Missile against Hypersonic Weapons with GIF(Guidance Integrated Fuzing).” In 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR 2010). IEEE. https://doi.org/10.1109/car.2010.5456681
• Yan, Xiaodong, and Shi Lyu. 2020. “Robust Intercept Guidance Law with Predesigned Zero-Effort Miss Distance Convergence for Capturing Maneuvering Targets.” Journal of the Franklin Institute 357 (2): 1118–36. https://doi.org/10.1016/j.jfranklin.2019.10.021
• Yan, Xiaodong, Shi Lyu, and Shuo Tang. 2014. “Analysis of Optimal Initial Glide Conditions for Hypersonic Glide Vehicles.” Chinese Journal of Aeronautics 27 (2): 217–25. https://doi.org/10.1016/j.cja.2014.02.019
• Yan, Shengyuan, Kai Yao, and Cong Chi Tran. 2021. “Using Artificial Neural Network for Predicting and Evaluating Situation Awareness of Operator.” IEEE Access 9: 20143–55. https://doi.org/10.1109/access.2021.3055345
• Yang, Y.-R. 1995. “Kbm Method of Analyzing Limit Cycle Flutter of a Wing with an External Store and Comparison with a Wind-Tunnel Test.” Journal of Sound and Vibration 187 (2): 271–80. https://doi.org/10.1006/jsvi.1995.0520
• Yang, Guangbin. 2013. “Heuristic Degradation Test Plans for Reliability Demonstration.” IEEE Transactions on Reliability 62 (1): 305–11. https://doi.org/10.1109/tr.2013.2241200
• Yang, Runqiu. 2025. “Biased-Proportional-Navigation-Based Predictor–Corrector Landing Guidance for Reusable Launch Vehicles.” Journal of Guidance, Control, and Dynamics 48 (7): 1591–1605. https://doi.org/10.2514/1.g008911
• Yang, Hao, Xibin Bai, and Shifeng Zhang. 2022. “Layout Design of Strapdown Array Seeker and Extraction Method of Guidance Information.” Aerospace 9 (7): 373. https://doi.org/10.3390/aerospace9070373
• Yang, Ciann-Dong, and Hsin-Yuan Chen. 1998. “Nonlinear H Robust Guidance Law for Homing Missiles.” Journal of Guidance, Control, and Dynamics 21 (6): 882–90. https://doi.org/10.2514/2.4321
• Yang, Sifeng, Feng Chen, and Zhouming Tan. 2009. “The Application of Data Mining Technique in Data Analyzing and Processing of Liquid Propellant Rocket Engine Test.” In 2009 Sixth International Conference on Fuzzy Systems and Knowledge Discovery. IEEE. https://doi.org/10.1109/fskd.2009.734
• Yang, Ting, Yi Li Fu, and Mahdi Tavakoi. 2015c. “FPAA-Based Control of Bilateral Teleoperation Systems.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260553
• Yang, Ting, Yili Fu, and Mahdi Tavakoli. 2015b. “Digital versus Analog Control of Bilateral Teleoperation Systems: A Task Performance Comparison.” Control Engineering Practice 38: 46–56. https://doi.org/10.1016/j.conengprac.2015.01.008
• Yang, Wang, and Zhu Guohui. 2019. “Design and Simulation Analysis of Missile-Borne SAR System.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048410
• Yang, Yana, Changchun Hua, and Xinping Guan. 2014a. “Adaptive Prescribed Performance Control for Nonlinear Networked Teleoperation System under Time Delay.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6895898
• Yang, Yana, Changchun Hua, and Xinping Guan. 2015d. “Synchronization Control for Bilateral Teleoperation System with Prescribed Performance under Asymmetric Time Delay.” Nonlinear Dynamics 81 (1–2): 481–93. https://doi.org/10.1007/s11071-015-2006-4
• Yang, Peng, Xiaoting Ji, Rina Wu, Xiangyun Liu, and Muyao Xue. 2025a. “Evaluation and Experimental Verification Methods of Combustion Instability in Single Chamber Dual Thrust Solid Rocket Motors.” In 2025 International Conference of Mechanical Engineering on Aerospace (CoMEA). IEEE. https://doi.org/10.1109/comea66280.2025.11241701
• Yang, Young Rok, Sung Ki Jung, Tae Hwan Cho, and Rho Shin Myong. 2012. “Aerodynamic Shape Optimization System of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients.” Journal of Spacecraft and Rockets 49 (2): 243–49. https://doi.org/10.2514/1.a32064
• Yang, Xiaoyan, Donghai Li, and Dazhong Lao. 2014b. “On the Active Disturbance Rejection Control Based Guidance Law Design with Angle Constraint.” In Proceedings of the 33rd Chinese Control Conference. IEEE. https://doi.org/10.1109/chicc.2014.6896724
• Yang, Gongliu, Yuanyuan Liu, Ming Li, and Shunguang Song. 2015a. “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, Yuxin, Tianwei Song, Chenxing Wang, and Yueyong Lyu. 2025b. “Optimal Midcourse Guidance Law and Cooperative Encirclement Hunting of Hypersonic Missile Group on Radau Pseudo-Spectral Method.” IFAC-PapersOnLine 59 (20): 1362–67. https://doi.org/10.1016/j.ifacol.2025.11.346
• Yang, Yang, Hongtao Su, Junsheng Huang, Qinzhen Hu, and Shenghua Zhou. 2018a. “Adaptive Monopulse Estimation in Mainlobe Jamming for Multistatic Radar.” In 2018 IEEE Radar Conference (RadarConf18). IEEE. https://doi.org/10.1109/radar.2018.8378567
• Yang, Wei, and Bing Sun. 2013. “Numerical Simulation of Liquid Film and Regenerative Cooling in a Liquid Rocket.” Applied Thermal Engineering 54 (2): 460–69. https://doi.org/10.1016/j.applthermaleng.2013.02.021
• Yang, Jin-zhu, and Zhao-fei Wang. 2012. “Numerical Simulation of Launch Tube Based on Container–type Missile Launch Technology.” Procedia Engineering 31: 302–7. https://doi.org/10.1016/j.proeng.2012.01.1028
• Yang, Yao, Mingang Wang, Qiang Li, and Gang Zhao. 2010. “Application Research on Time Optimal Synthesis Function for Missile Electromechanical Actuator Control System.” In 2010 International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2010.791
• Yang, Ciann-Dong, and Chi-Ching Yang. 1996a. “Analytical Solution of Generalized Three-Dimensional Proportional Navigation.” Journal of Guidance, Control, and Dynamics 19 (3): 721–24. https://doi.org/10.2514/3.21685
• Yang, Ciann-Dong, and Chi-Ching Yang. 1996b. “Analytical Solution of Three-Dimensional Realistic True Proportional Navigation.” Journal of Guidance, Control, and Dynamics 19 (3): 569–77. https://doi.org/10.2514/3.21659
• Yang, Ciann-Dong, and Fang-Bo Yeh. 1988. “Optimal Proportional Navigation.” Journal of Guidance, Control, and Dynamics 11 (4): 375–77. https://doi.org/10.2514/3.20323
• Yang, Ciann-Dong, Fang-Bo Yeh, and Jen-Heng Chen. 1987. “The Closed-Form Solution of Generalized Proportional Navigation.” Journal of Guidance, Control, and Dynamics 10 (2): 216–18. https://doi.org/10.2514/3.20205
• Yang, Qi, Wei Yi, and Mahendra Mallick. 2020b. “A Decentralized PHD Filter for Multi-Target Tracking in Asynchronous Multi-Static Radar System.” In 2020 IEEE Radar Conference (RadarConf20). IEEE. https://doi.org/10.1109/radarconf2043947.2020.9266320
• Yang, Xue, Li Yu, Min Liu, and Haofei Pang. 2020c. “Fluid Structure Interaction Simulation of Supersonic Parachute Inflation by an Interface Tracking Method.” Chinese Journal of Aeronautics 33 (6): 1692–1702. https://doi.org/10.1016/j.cja.2020.03.005
• Yang, Dianzong, Taideng Zhan, Qiang Qi, Danpeng Huang, and Jianjun Ma. 2025c. “Reinforcement Learning Based Impact Angle Constrained Guidance Law Considering Time-Varying Velocity.” In 2025 44th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc64809.2025.11178753
• Yanli, Du, Sun Dongyang, Leng Xuefei, and Fu Jian. 2016. “Self-Organizing Functional-Link-Network-Based Control for Hypersonic Glide Vehicles.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531399
• Ye, Zhenxin, Sheng Gu, Shengping Gong, and Siyu Zhang. 2026. “Fluid–Structure Interaction Simulation of a Supersonic Reefed Parachute Cluster during the Inflation Process.” Aerospace 13 (9): 818. https://doi.org/10.3390/aerospace13090818
• Ye, Qing, and Chunsheng Liu. 2016. “A Nonsingular SMC-Based Guidance Law for an Accelerating Exoatmospheric Missile.” In 2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/cgncc.2016.7828784
• Ye, Yang, Tianyu Zhou, Qi Zhu, William Vann, and Jing Du. 2024. “Brain Functional Connectivity under Teleoperation Latency: A fNIRS Study.” Frontiers in Neuroscience 18: 1416719. https://doi.org/10.3389/fnins.2024.1416719
• Yi, Xin, Ling Li, and Haibin Zhao. 2021a. “Adaptive Terminal Sliding Mode Guidance Law with Impact Angle Constraint.” In 2021 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac53003.2021.9728169
• Yi, Ke, Siyuan Liu, Jianglong Yu, QingDong Li, Zhang Ren, and Junbiao Wu. 2016. “Integration Control Design for a Semi-Strapdown Seeker Missile.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531027
• Yi, Ke, Kai Tang, Sihong She, Mohan Li, and Zhaoming Tan. 2018a. “Integrated Guidance and Control for Semi-Strapdown Missiles.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8482808
• Yi, Ke, Kai Tang, Yuan Yang, and Qianyi Wang. 2018b. “Optimal Guidance for Guided Projectile with Impact Angle Constraint.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9018714
• Yi, Qi, Lei Wang, Ziang Wang, and Yimin Liu. 2025. “Joint Task Selection and Resource Allocation for Multi-Target Tracking under Suppression Jamming in Networked Radar Systems.” In 2025 IEEE International Radar Conference (RADAR). IEEE. https://doi.org/10.1109/radar52380.2025.11032051
• Yi, Yu-sheng, Lin-rang Zhang, Xin Liu, Nan Liu, and Dong Shen. 2007. “Study on Imaging Algorithm for Missile-Borne Side-Looking SAR.” In 2007 1st Asian and Pacific Conference on Synthetic Aperture Radar. IEEE. https://doi.org/10.1109/apsar.2007.4418639
• Yilmaz, Gozde, and Derya Yilmaz. 2019. “Evaluation of Pure Proportional Navigation and Velocity Pursuit Guidance Methods for Missiles.” In 2019 3rd International Symposium on Multidisciplinary Studies and Innovative Technologies (ISMSIT). IEEE. https://doi.org/10.1109/ismsit.2019.8932784
• Yin, Tingting, Fangxiu Jia, and Jiyan Yu. 2018. “Research on Roll Control System for Fixed Canard Rudder of the Dual-Spin Trajectory Correction Projectile.” Wireless Personal Communications 103 (1): 83–98. https://doi.org/10.1007/s11277-018-5427-9
• 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
• Yisheng, Rong. 2013. “Drag Reduction Research in Supersonic Flow with Opposing Jet.” Acta Astronautica 91: 1–7. https://doi.org/10.1016/j.actaastro.2013.04.015
• Yomchinda, Thanan. 2015. “A Study of Autonomous Evasive Planar-Maneuver against Proportional-Navigation Guidance Missiles for Unmanned Aircraft.” In 2015 Asian Conference on Defence Technology (ACDT). IEEE. https://doi.org/10.1109/acdt.2015.7111613
• 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-An Zhang, Di Zhou, and Guang-Ren Duan. n.d. “Simplified Multiple Model Filtering of Target Glint.” In Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788), vol. 2. IEEE. https://doi.org/10.1109/wcica.2004.1340923
• Yongmin Kim and J. H. Seo. n.d. “The Realization of the Three Dimensional Guidance Law Using Modified Augmented Proportional Navigation.” In Proceedings of 35th IEEE Conference on Decision and Control, vol. 3. IEEE. https://doi.org/10.1109/cdc.1996.573514
• Yongming, Qin, and Xia Yuanqing. 2015. “Control of Bilateral Teleoperation with Time Delay Considering Operator Force Sending.” In 2015 34th Chinese Control Conference (CCC). IEEE. https://doi.org/10.1109/chicc.2015.7260696
• Yoo, Chung-Hee. 2017. “Active Control of Aeroelastic Vibrations for Electromechanical Missile Fin Actuation Systems.” Journal of Guidance, Control, and Dynamics 40 (12): 3299–3306. https://doi.org/10.2514/1.g002821
• Yoo, Kyungwoo, Joohwan Chun, and Jinwoo Shin. 2018. “Target Tracking and Classification for Missile Using Interacting Multiple Model (IMM).” In 2018 International Conference on Radar (RADAR). IEEE. https://doi.org/10.1109/radar.2018.8557241
• Yoo, Seungmin, Shinkyu Jeong, Jongho Jung, and Kangkuk You. 2023. “Multi-Objective Aerodynamic Shape Design Optimization of Canard-Controlled Missiles for Reducing Induced Roll.” Optimization and Engineering 25 (2): 841–69. https://doi.org/10.1007/s11081-023-09827-7
• Yoon, Sung, and Insang Moon. 2026. “Tank Head Startup Analysis of a Gas Generator Cycle Liquid Rocket Engine.” Aerospace 13 (9): 768. https://doi.org/10.3390/aerospace13090768
• Yoon, Kun Su, Jae Hyun Park, In Gyu Kim, and Kwang Su Ryu. 2010. “New Modeling Algorithm for Improving Accuracy of Weapon Launch Acceptability Region.” In 29th Digital Avionics Systems Conference. IEEE. https://doi.org/10.1109/dasc.2010.5655454
• Yoon, Yonghan, Min-Sik Yang, Cheol-Ho Bai, and Jaesool Shim. 2025a. “Bayesian Zero-Failure Reliability Demonstration Tests: Sample Size Estimation and Its Limitation.” Journal of Mechanical Science and Technology 39 (7): 3651–66. https://doi.org/10.1007/s12206-025-2409-1
• Yoshida, Kouei, and Toru Namerikawa. 2009. “Stability and Tracking Properties in Predictive Control with Adaptation for Bilateral Teleoperation.” In 2009 American Control Conference. IEEE. https://doi.org/10.1109/acc.2009.5160049
• You, Hao, Xinlong Chang, and Jiufen Zhao. 2025. “Three-Dimensional Line-of-Sight-Angle-Constrained Leader-Following Cooperative Interception Guidance Law with Prespecified Impact Time.” Chinese Journal of Aeronautics 38 (1): 103151. https://doi.org/10.1016/j.cja.2024.07.023
• You, Hao, Xinlong Chang, Jiufen Zhao, Shunhong Wang, and Youhong Zhang. 2023a. “Three-Dimensional Impact-Angle-Constrained Cooperative Guidance Strategy against Maneuvering Target.” ISA Transactions 138: 262–80. https://doi.org/10.1016/j.isatra.2023.02.030
• You, Hao, Xinlong Chang, Jiufen Zhao, Shunhong Wang, and Youhong Zhang. 2023b. “Three-Dimensional Impact-Angle-Constrained Fixed-Time Cooperative Guidance Algorithm with Adjustable Impact Time.” Aerospace Science and Technology 141: 108574. https://doi.org/10.1016/j.ast.2023.108574
• You, Yuqi, Pin Yang, and Zhongting Chen. 2026. “Predictability of Trajectory Modulates Manual Tracking: From Real-Time Feedback to Internal-Model-Based Control.” Cognitive Psychology 164: 101798. https://doi.org/10.1016/j.cogpsych.2026.101798
• Young, M. J., and S. E. Deutsch. 1997. “Integrating Human Performance into the Design Process: The Operator Model Architecture.” In Proceedings of the 1997 IEEE Sixth Conference on Human Factors and Power Plants, 1997. ‘Global Perspectives of Human Factors in Power Generation’. IEEE. https://doi.org/10.1109/hfpp.1997.624855
• Young, L. R., D. M. Green, J. I. Elkind, and J. A. Kelly. 1964. “Adaptive Dynamic Response Characteristics of the Human Operator in Simple Manual Control.” IEEE Transactions on Human Factors in Electronics HFE-5 (1): 6–13. https://doi.org/10.1109/thfe.1964.231648
• Yu, K.-B. 1991. “High-Resolution Multiple Target Angle Tracking.” In Proceedings of the 1991 IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1991.114719
• Yu, Kai-Bor. 2017. “Partial Adaptivity for Monopulse Angle Estimation in Jamming.” In 2017 IEEE International Conference on Signal Processing, Communications and Computing (ICSPCC). IEEE. https://doi.org/10.1109/icspcc.2017.8242472
• Yu, Qi, Wanchun Chen, Hongkui Wei, Chao Wang, and Jinchuan Hu. 2023. “Online Analytical Guidance for a Solid-Fuel Launch Vehicle in Boost Phase Based on Generalized Zero Effort Miss.” In 2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE. https://doi.org/10.1109/icmae59650.2023.10424594
• Yu, Kai-Bor, and Manuel F. Fernández. 2025. “Maintenance of Monopulse Beams for Adaptive Nulling and Target Angle Tracking Using Uniform Rectangular Arrays.” In 2025 IEEE Radar Conference (RadarConf25). IEEE. https://doi.org/10.1109/radarconf2559087.2025.11205049
• Yu, Shutian, Xinyue Ni, Xiaoyan Li, Tingliang Hu, and Fansheng Chen. 2022. “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, Rourou, Youchao Sun, Yuhan Li, and Chaochao Guo. 2026. “A Quantum-Like Many-Body Wave Function-Based Modeling Approach for Dynamic Human-Machine Function Allocation.” In 2026 IEEE International Conference on Human-Machine Systems (ICHMS). IEEE. https://doi.org/10.1109/ichms69701.2026.11602357
• Yu, Ji-Feng, Suo-Chang Yang, and Yun-wei Zhang. 2019. “Flight Trajectory Correction of Target Missile and Design of Tracking Guidance.” In 2019 International Conference on Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE). IEEE. https://doi.org/10.1109/qr2mse46217.2019.9021272
• Yu, Yingrong, Ke Yi, Qingdong Li, Xiwang Dong, and Zhang Ren. 2017. “Guidance Information Estimation of the Semi-Strapdown Infrared Imaging Seeker.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028341
• Yu, Nanjia, Bo Zhao, Gongnan Li, and Jue Wang. 2016. “Experimental and Simulation Study of a Gaseous oxygen/Gaseous Hydrogen Vortex Cooling Thrust Chamber.” Acta Astronautica 118: 11–20. https://doi.org/10.1016/j.actaastro.2015.09.017
• Yu Li and Nai-gang Cui. 2008. “Maximum Crossrange for Hypersonic Boost-Glide Missile.” In 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2008.4776361
• Yu-bin Yu and Jing Zhang. 2008. “Use Roll Actuator to Reduce Coupling of BTT Missile.” In 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2008.4776261
• Yuan, Pin-Jar, and Jeng-Shing Chern. 1992a. “Analytic Study of Biased Proportional Navigation.” Journal of Guidance, Control, and Dynamics 15 (1): 185–90. https://doi.org/10.2514/3.20817
• Yuan, Pin-Jar, and Jeng-Shing Chern. 1992b. “Ideal Proportional Navigation.” Journal of Guidance, Control, and Dynamics 15 (5): 1161–65. https://doi.org/10.2514/3.20964
• Yuan, Pin-Jar, and Jeng-Shing Chern. 1992c. “Solutions of True Proportional Navigation for Maneuvering and Nonmaneuvering Targets.” Journal of Guidance, Control, and Dynamics 15 (1): 268–71. https://doi.org/10.2514/3.20828
• Yuan, Shuai, Zhanpeng Gao, and Wenjun Yi. 2026. “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, Pin-Jar, and Shih-Che Hsu. 1993. “Exact Closed-Form Solution of Generalized Proportional Navigation.” Journal of Guidance, Control, and Dynamics 16 (5): 963–66. https://doi.org/10.2514/3.21109
• Yuan, Pin-Jar, and Shih-Che Hsu. 1994. “Rendezvous Guidance with Proportional Navigation.” Journal of Guidance, Control, and Dynamics 17 (2): 409–11. https://doi.org/10.2514/3.21213
• Yuan, Jing, and Yong Long. 2010. “The Missile Flight Control System Reliability Analysis Based on Hybrid Fault Trees.” In 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR 2010). IEEE. https://doi.org/10.1109/car.2010.5456653
• Yuan, Zekun, Bo Mo, Jie Zhao, and Donghui Zhao. 2023. “A Modified Three-Dimensional Sliding Mode Guidance Law with Impact Angle Constraint.” In 2023 38th Youth Academic Annual Conference of Chinese Association of Automation (YAC). IEEE. https://doi.org/10.1109/yac59482.2023.10401569
• Yuan, Ye, Jianwei Wei, and Wei Yi. 2024. “Online Route Planning for Airborne Radar Networks with Multi-Target Tracking.” In 2024 IEEE Radar Conference (RadarConf24). IEEE. https://doi.org/10.1109/radarconf2458775.2024.10549563
• 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 He, Timofey Savelyev, and Alexander Yarovoy. 2011. “Two-Stage Algorithm for Extended Target Tracking by Multistatic UWB Radar.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159660
• Yue Pan, Ping Song, Kejie Li, Ran Lin, and Wei Huang. 2011. “A Filtering Method of Gyroscope Random Drift for Miniature Unmanned Helicopter.” In Proceedings of 2011 International Conference on Computer Science and Network Technology. IEEE. https://doi.org/10.1109/iccsnt.2011.6182068
• Yueh, William R., and Ching-Fang Lin. 1985. “Optimal Controller for Homing Missile.” Journal of Guidance, Control, and Dynamics 8 (3): 408–11. https://doi.org/10.2514/3.19997
• Yueyi, Kang, Zhang Dabiao, and Jin Huilong. 2007. “Cause of Formation and Correcting Method for Wind Error of Tracking Radar.” In 2007 8th International Conference on Electronic Measurement and Instruments. IEEE. https://doi.org/10.1109/icemi.2007.4350501
• Yun, Joongsup, and Chang-Kyung Ryoo. 2014. “Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter.” Journal of Guidance, Control, and Dynamics 37 (2): 484–96. https://doi.org/10.2514/1.61327
• Yun-li Du, Qun-li Xia, and Tao Guo. 2010. “Study on Stability of Strapdown Seeker Scale Factor Error Parasitical Loop.” In 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering. IEEE. https://doi.org/10.1109/cmce.2010.5609905
• Yurttas, Ragip, Emrah Oduncu, and Murat Samil Aslan. 2014. “Analysis of Jamming Effectiveness on Miss Distance.” In 2014 22nd Signal Processing and Communications Applications Conference (SIU). IEEE. https://doi.org/10.1109/siu.2014.6830569
• Yusheng, Yi, Zhang Linrang, Li Yan, Liu Nan, and Liu Xin. 2009. “Range Doppler Algorithm for Bistatic Missile-Borne Forward-Looking SAR.” In 2009 2nd Asian-Pacific Conference on Synthetic Aperture Radar. IEEE. https://doi.org/10.1109/apsar.2009.5374268
• 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
• 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
• Zang, Hongyan, Changsheng Gao, Yudong Hu, and Wuxing Jing. 2025. “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
• Zarchan, Paul. 1979. “Complete Statistical Analysis of Nonlinear Missile Guidance Systems: SLAM.” Journal of Guidance and Control 2 (1): 71–78. https://doi.org/10.2514/3.55834
• Zarchan, Paul. 1995. “Proportional Navigation and Weaving Targets.” Journal of Guidance, Control, and Dynamics 18 (5): 969–74. https://doi.org/10.2514/3.21492
• Zarchan, Paul. 2011. “Kill Vehicle Guidance and Control Sizing for Boost-Phase Intercept.” Journal of Guidance, Control, and Dynamics 34 (2): 513–21. https://doi.org/10.2514/1.50927
• Zarifi, Davood, Ali Farahbakhsh, and Michal Mrozowski. 2025. “An Ultrawideband Monopulse Feed with Slant Polarization for Tracking Radar Systems.” Scientific Reports 15 (1): 3593. https://doi.org/10.1038/s41598-025-87956-y
• Zeng, Yangzhi, Xiaodong Shao, Qinglei Hu, Haifeng Hu, and Hao Pan. 2021. “Fault Diagnosis of Liquid Rocket Engine Thrust Chamber Based on Improved Augmented Particle Filter.” In 2021 40th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc52363.2021.9550493
• Zeng, Xianfa, Jieyao Wang, and Xiaohu Wang. 2014. “Trajectory Correcting and Tracking Based Impact Angle Constrained Circular Guidance.” In Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. IEEE. https://doi.org/10.1109/cgncc.2014.7007597
• Zeng, Xin, Sujie Xian, Zhilin Wu, and Kun Liu. 2025. “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
• Zeng, Yonghu, Jing Zhao, Hui Han, Xiong Xu, and Huanyao Dai. 2017. “INS Error Correction Method Based on Passive Radar Angle Tracking Information.” In 2017 2nd International Conference on Frontiers of Sensors Technologies (ICFST). IEEE. https://doi.org/10.1109/icfst.2017.8210547
• Zewge, Natnael S., and Hyochoong Bang. 2022. “Reentry-Phase Tracking of a Ballistic Missile in the Presence of Radar Glint Noise.” In 2022 22nd International Conference on Control, Automation and Systems (ICCAS). IEEE. https://doi.org/10.23919/iccas55662.2022.10003874
• Zhai, Di-Hua, and Yuanqing Xia. 2014. “Robust Saturation-Based Control of Bilateral Teleoperation without Velocity Measurements: CONTROL OF TELEOPERATION WITHOUT VELOCITY MEASUREMENTS.” International Journal of Robust and Nonlinear Control 25 (15): 2582–2607. https://doi.org/10.1002/rnc.3214
• Zhai, Di-Hua, and Yuanqing Xia. 2016. “Adaptive Stabilization of Nonlinear Teleoperation Systems: An SIIOS Approach.” International Journal of Robust and Nonlinear Control 26 (17): 3696–3722. https://doi.org/10.1002/rnc.3528
• 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, Lei, Tuan M. Nguyen, Juntao Xiong, Feng Liu, and William A. Sirignano. 2024. “Combustion Dynamics of Ten-Injector Rocket Engine Using Flamelet Progress Variable.” Combustion and Flame 267: 113538. https://doi.org/10.1016/j.combustflame.2024.113538
• Zhan, Taideng, Dianzong Yang, Danpeng Huang, Mingjie Zhang, and Jianjun Ma. 2025a. “Impact Angle Constrained Cooperative Guidance Law for Multiple Missiles with Nonuniform Field-Of-View Limit.” In 2025 44th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/ccc64809.2025.11178718
• Zhan, Siheng, Liang Zhou, and Wei Cai. 2025b. “Impact of Interferer Azimuth on Angle Estimation Accuracy after Interference Cancellation in Monopulse Phased Array Radar.” In 2025 IEEE 8th International Symposium on Electromagnetic Compatibility (ISEMC). IEEE. https://doi.org/10.1109/isemc68048.2025.11292202
• Zhan, Siheng, Liang Zhou, Bin Wang, and Jin Meng. 2026. “Impact of Beam Steering on Angle Measurement Accuracy of 2D Monopulse Phased Array Radar with Interference Cancellation.” In 2026 IEEE 9th International Symposium on Electromagnetic Compatibility (ISEMC). IEEE. https://doi.org/10.1109/isemc70545.2026.11588772
• Zhang, Yu-Lin. 1984. “State-Space Analysis of the Dynamic Characteristics of a Variable Thrust Liquid Propellant Rocket Engine.” Acta Astronautica 11 (7–8): 535–41. https://doi.org/10.1016/0094-5765(84)90093-6
• 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. 2026g. “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, Bin, Shi-Lu Chen, and Min Xu. 2010. “An Optimal Nonlinear Variable Structure Guidance Law Considering Missile Dynamics of Autopilot.” In 2010 2nd International Conference on Information Engineering and Computer Science. IEEE. https://doi.org/10.1109/iciecs.2010.5678288
• Zhang, Peng, and Yanli Du. 2017. “The Robust Maneuver Flight Control of Hypersonic Glide Vehicles with Input Saturation Using Disturbance Observer.” In IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society. IEEE. https://doi.org/10.1109/iecon.2017.8217148
• Zhang, Danyao, Qingyu Du, Yijia Xie, and Jianzhong Qiao. 2018b. “A New Composite Proportional Navigation Entry Guidance Strategy for Glider under Multiple Uncertainties.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483281
• Zhang, Ruitao, Wenxing Fu, Zhan Chen, Hang Guo, and Yangwang Fang. 2025c. “Group Cooperative Midcourse Guidance Law for Heterogeneous Missile Formation with Optimal Detection Efficiency.” Chinese Journal of Aeronautics 38 (10): 103499. https://doi.org/10.1016/j.cja.2025.103499
• Zhang, HuiQiang, YongJing Ga, Bing Wang, and XiLin Wang. 2012b. “Analysis of Combustion Instability via Constant Volume Combustion in a LOX/RP-1 Bipropellant Liquid Rocket Engine.” Science China Technological Sciences 55 (4): 1066–77. https://doi.org/10.1007/s11431-012-4743-7
• Zhang, Fubin, Xiaohua Gao, and Wenbo Song. 2022f. “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, Xiaowen, Yesheng Gao, Kaizhi Wang, and Xingzhao Liu. 2017e. “Optimal Waveform Design for Target Tracking and Estimation in Cognitive Radar.” In 2017 IEEE Radar Conference (RadarConf). IEEE. https://doi.org/10.1109/radar.2017.7944192
• Zhang, Zhi-kai, and Qing Guo. 2012. “Terminal Guidance Method in Glide Attack Phase of Aerodynamic Missile.” In Proceedings of the 10th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2012.6358054
• Zhang, Peijun, Ruizhi He, Luhua Liu, and Guojian Tang. 2017f. “Rapid Generation of Boost Trajectory for Boost-Glide Missile.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028140
• Zhang, H. W., Y. L. He, and W. Q. Tao. 2007. “Numerical Study of Film and Regenerative Cooling in a Thrust Chamber at High Pressure.” Numerical Heat Transfer, Part A: Applications 52 (11): 991–1007. https://doi.org/10.1080/10407780701364379
• Zhang, Jungen, Hongbing Ji, and Qikun Xue. 2009a. “A New Approach Based on Particle Filter for Target Tracking with Glint Noise.” In 2009 IEEE International Conference on Systems, Man and Cybernetics. IEEE. https://doi.org/10.1109/icsmc.2009.5346071
• Zhang, Dian, Ping Jiang, and Yunyan Xing. 2024b. “A System Reliability Demonstration Test Design Method Based on Subsystem Test Data.” Quality and Reliability Engineering International 41 (1): 98–112. https://doi.org/10.1002/qre.3664
• Zhang, Bo, Alexandre Kruszewski, and Jean-Pierre Richard. 2011b. “A Novel Control Scheme for Teleoperation with Guaranteed Performance under Time-Varying Delays.” In 2011 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2011.5968191
• Zhang, Jiawei, Juanmian Lei, Jintao Yin, and Jianping Niu. 2020. “The Numerical Investigation on the Rolling Decoupling of a Canard-Controlled Missile Using the Jet Control System.” Engineering Applications of Computational Fluid Mechanics 14 (1): 1062–77. https://doi.org/10.1080/19942060.2020.1799866
• Zhang, Yong-Peng, Bao-Ye Li, and Chao Gao. 2019a. “Design of a Real-Time Monopulse Tracking Data Processing Algorithms for Missile-Borne SAR Radar.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048327
• 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, Ke, Peng Li, Ming Lv, and Xiaoma Liu. 2015a. “Integrated Guidance and Control Design of Missile with Terminal Impact Angle Constraint.” In 2015 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2015.7237591
• Zhang, Zhenxing, Junyun Liu, Wangshu Chen, Shaojie Song, and Jianwu Zou. 2018a. “Composite Finite-Time Guidance Law for Homing Missile.” In 2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC). IEEE. https://doi.org/10.1109/gncc42960.2018.9019063
• Zhang, Haowei, Weijian Liu, Taiyong Fei, Hao Zhou, and Junwei Xie. 2022c. “An Efficient Radar-Target Assignment and Power Allocation Strategy for Low-Angle Tracking in the MIMO-Multisite Radar System.” Signal Processing 200: 108645. https://doi.org/10.1016/j.sigpro.2022.108645
• Zhang, Yi-Xiong, Qi-Fan Liu, Ru-Jia Hong, Ping-Ping Pan, and Zhen-Miao Deng. 2016b. “A Novel Monopulse Angle Estimation Method for Wideband LFM Radars.” Sensors 16 (6): 817. https://doi.org/10.3390/s16060817
• Zhang, Yunxi, Jia Liu, and Kuansheng Zou. 2016c. “Sliding-Mode Guidance Law with Impact Angle Constraint Accounting for Autopilot Lag.” In 2016 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2016.7531063
• Zhang, Yongfang, Yanjun Lu, Xiaolei Shi, and An Zhang. 2009b. “Simulation and Evaluation of the Combat Effectiveness of Television Remote Control Missile.” In 2009 International Conference on Measuring Technology and Mechatronics Automation. IEEE. https://doi.org/10.1109/icmtma.2009.180
• Zhang, Mingjie, and Jianjun Ma. 2019. “Adaptive Fixed-Time Cooperative Intercept Guidance Law with Line-Of-Sight Angle Constraint.” In 2019 IEEE International Conference on Mechatronics and Automation (ICMA). IEEE. https://doi.org/10.1109/icma.2019.8816552
• Zhang, Yongshu, Mingwei Shen, Di Wu, Daiyin Zhu, and Yudong Zhang. 2023c. “Reduced Complexity Mutiple-Target Angle-Doppler-Range Estimation Using Space-Time Cascaded Monopulse Processing.” Digital Signal Processing 143: 104239. https://doi.org/10.1016/j.dsp.2023.104239
• Zhang, Yu, and Shiyan Sun. 2025. “Distributed Fixed-Time Cooperative Guidance Law for Simultaneous Attack with Impact Angle Constraint.” IEEE Access 13: 95307–20. https://doi.org/10.1109/access.2025.3574457
• Zhang, Yunxi, Mingwei Sun, and Zengqiang Chen. 2012c. “Finite-Time Convergent Guidance Law with Impact Angle Constraint Based on Sliding-Mode Control.” Nonlinear Dynamics 70 (1): 619–25. https://doi.org/10.1007/s11071-012-0482-3
• Zhang, Wei, Houjun Sun, and Xin Lv. 2006a. “A Design Method of Parameters for Airborne Conical Scan Pulsed Doppler Radar Seeker.” In 2006 8th international Conference on Signal Processing. IEEE. https://doi.org/10.1109/icosp.2006.346034
• Zhang, Rouhe, Zhili Sun, and Changzhu Wei. 2022e. “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, Yi, Houjun Sun, Xiaowen Xu, and Qing huo Liu. 2017b. “Amplitude Angle Monopulse Estimation for the Four-Channel Hybrid Polarimetric Radar System.” IEEE Antennas and Wireless Propagation Letters: 1–1. https://doi.org/10.1109/lawp.2017.2751298
• Zhang, Dian, Yunlei Tan, Ping Jiang, and Guang Jin. 2025b. “Design of Reliability Demonstration Test Plan for Weibull Products.” In 2025 Global Reliability and Prognostics and Health Management Conference (PHM-Xian). IEEE. https://doi.org/10.1109/phm-xian66756.2025.11427661
• Zhang, Dian, Yunlei Tan, Ping Jiang, and Guang Jin. 2026e. “Reliability Demonstration Test Design Based on Soft Failure Data.” In 2026 8th International Conference on System Reliability and Safety Engineering (SRSE). IEEE. https://doi.org/10.1109/srse70977.2026.11694941
• Zhang, Dong, and Shuo Tang. 2012. “The Propulsion/Flight Dynamics Coupling Analysis for Air-Breathing Hypersonic Vehicle.” In 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics. IEEE. https://doi.org/10.1109/ihmsc.2012.19
• Zhang, Feng, Kang-sheng Tian, and Mu-lin Xi. 2011a. “The Ballistic Missile Tracking Method Using Dynamic Model.” In Proceedings of 2011 IEEE CIE International Conference on Radar. IEEE. https://doi.org/10.1109/cie-radar.2011.6159659
• Zhang, Chencheng, Zhiqiang Tong, Hongquan Liu, and Weijian Pang. 2024c. “Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control.” In 2024 IEEE International Conference on Unmanned Systems (ICUS). IEEE. https://doi.org/10.1109/icus61736.2024.10840132
• Zhang, Xue, and Qi Wang. 2025. “Zero-Sum Differential Games Guidance Law Accounting for Impact-Angle-Constrained Using Adaptive Dynamic Programming.” Journal of Intelligent & Robotic Systems 111 (1): 21. https://doi.org/10.1007/s10846-024-02217-w
• Zhang, Bing, Hengxin Wang, Ming Hou, and Sitong Chen. 2026d. “Numerical Simulation of Flow-Control Effects on Flow Field and Store Separation Trajectory in a Curved-Lip Cavity.” International Journal of Aerospace Engineering 2026 (1): 4180583. https://doi.org/10.1155/ijae/4180583
• Zhang, Qingzhen, Zhenbo Wang, and Fei Tao. 2014a. “Optimal Guidance Law Design for Impact with Terminal Angle of Attack Constraint.” Optik 125 (1): 243–51. https://doi.org/10.1016/j.ijleo.2013.06.065
• Zhang, Kuanqiao, Chuanchuan Wang, Ning Zhu, Jingke Zhang, and Huabing Wang. 2023b. “Fixed-Time Convergent Backstepping Sliding Mode Guidance Law with Impact Angle Constraint.” In 2023 35th Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc58219.2023.10327283
• Zhang, Jiahui, and Qiuqiu Wen. 2024. “Closed-Form Guidance Law for Velocity Maximization with Impact Angle Constraint.” Journal of Systems Engineering and Electronics 35 (5): 1295–1303. https://doi.org/10.23919/jsee.2024.000078
• Zhang, Haiyang, Shunxiang Wu, Zhu Li, and Delin Luo. 2016a. “Agile Turn Autopilot Design of over-the-Shoulder Launched Air-to-Air Missile Based on Sliding Mode Control Theory.” In 2016 11th International Conference on Computer Science & Education (ICCSE). IEEE. https://doi.org/10.1109/iccse.2016.7581619
• Zhang, X. T., Z. G. Wu, and C. Yang. 2013. “New Flutter-Suppression Method for a Missile Fin with an Actuator.” Journal of Aircraft 50 (3): 989–94. https://doi.org/10.2514/1.c031961
• Zhang, Wei, Lingyue Xia, and Hangcong Fu. 2017c. “Analytical Decoupling Control of a Generic Hypersonic Vehicle Based on Internal Model Control.” In 2017 36th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2017.8028337
• Zhang, Qiyue, Hongtao Xie, Peng Dong, Guobiao Cai, Hui Tian, and Ruizhi Li. 2026b. “Investigation on Additive Manufactured CuCrZr Alloy Regenerative Cooling Thrust Chamber: Material Properties and Structural Mechanical Response.” Advances in Astronautics. https://doi.org/10.1007/s42423-026-00213-w
• Zhang, Dian, Yunyan Xing, and Ping Jiang. 2023e. “Reliability Demonstration Test Design Method Based on Two-Stage Test with Zero Failure Data.” In 2023 Global Reliability and Prognostics and Health Management Conference (PHM-Hangzhou). IEEE. https://doi.org/10.1109/phm-hangzhou58797.2023.10482542
• Zhang, Dian, Yunyan Xing, and Ping Jiang. 2023f. “A System Reliability Demonstration Test Design Method Based on Subsystem Test Data.” In 2023 5th International Conference on System Reliability and Safety Engineering (SRSE). IEEE. https://doi.org/10.1109/srse59585.2023.10336103
• Zhang, Junbiao, Jiajun Xiong, Lingzhi Li, Qiushi Xi, Xin Chen, and Fan Li. 2022d. “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, Wenguang, and Jin Yan. 2023. “Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint.” International Journal of Aerospace Engineering 2023: 1–17. https://doi.org/10.1155/2023/5568394
• Zhang, Kuanqiao, and Suochang Yang. 2018. “Fast Convergent Nonsingular Terminal Sliding Mode Guidance Law with Impact Angle Constraint.” In 2018 37th Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2018.8483369
• Zhang, Yongmeng, Sheng Yu, Jiangkun Sun, et al. 2021. “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, Daxi, and Yulin Zhang. 2020. “Multidisciplinary Design and Optimization of an Innovative Nano Air Launch Vehicle with a Twin-Fuselage UAV as Carrier Aircraft.” Acta Astronautica 170: 397–411. https://doi.org/10.1016/j.actaastro.2019.11.012
• 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, Yongfang, An Zhang, and Yanjun Lu. 2006b. “Modeling and Simulation of Air-to-Ground TV Seeking Guidance Missile System.” In 2006 International Conference on Communication Technology. IEEE. https://doi.org/10.1109/icct.2006.341964
• Zhang, Wen, Xuanzhi Zhao, Song Chen, and Huifang Duan. 2017a. “Adaptive Target Tracking under Glint Noise.” In 2017 14th International Computer Conference on Wavelet Active Media Technology and Information Processing (ICCWAMTIP). IEEE. https://doi.org/10.1109/iccwamtip.2017.8301447
• Zhang, Guanglei, Rong Zhou, and Yifeng Wu. 2022a. “Constrained Adaptive Monopulse Estimation for Planar Arrays.” In 2022 5th International Conference on Information Communication and Signal Processing (ICICSP). IEEE. https://doi.org/10.1109/icicsp55539.2022.10050638
• Zhang, Hanxiang, Saeed Zolfaghary Pour, Powei Liu, et al. 2024a. “Boosting Estimation Accuracy of Low-Cost Monopulse Receiver via Deep Neural Network.” In 2024 IEEE Wireless and Microwave Technology Conference (WAMICON). IEEE. https://doi.org/10.1109/wamicon60123.2024.10522859
• Zhang Xiushe. 2001. “Engineering Problems of Low-Angle Tracking Radars.” In 2001 CIE International Conference on Radar Proceedings (Cat No.01TH8559). IEEE. https://doi.org/10.1109/icr.2001.984622
• Zhang Ying-chun, Li Jing-jing, and Li Hua-yi. 2010. “Line of Sight Rate Estimation of Strapdown Imaging Seeker Based on Particle Filter.” In 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics. IEEE. https://doi.org/10.1109/isscaa.2010.5633193
• Zhao, Yang, Guang-Bin Cai, and Sheng-Xiu Zhang. 2018. “LPV Model Reference Control Method for Hypersonic Vehicle Control System.” In 2018 Chinese Control And Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2018.8407903
• Zhao, Bin, and Jie Chen. 2022. “Asynchronous Fusion Method of Guidance Information for Strapdown Missile Swarm.” In 2022 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac57257.2022.10055084
• Zhao, Shilei, Wanchun Chen, and Liang Yang. 2021b. “Optimal Guidance Law with Impact-Angle Constraint and Acceleration Limit for Exo-Atmospheric Interception.” Aerospace 8 (12): 358. https://doi.org/10.3390/aerospace8120358
• Zhao, Chunlei, Zhiwei He, Ming Fang, Shoujiang Yu, and Yifan Guo. 2021a. “Online Least-Squares Learning for Monopulse Angle Tracking and Waveform Estimation.” In 2021 2nd China International SAR Symposium (CISS). IEEE. https://doi.org/10.23919/ciss51089.2021.9652262
• Zhao, Mengke, Libing Hou, Heng Shi, Luhua Yang, Minchi Kuang, and Jihong Zhu. 2026b. “Evasive Guidance Law against Proportional Navigation Considering Dynamic Lag.” Engineering. https://doi.org/10.1016/j.eng.2026.08.026
• Zhao, Boyang, Bin Huang, Zixuan Wang, et al. 2026c. “Event-Triggered Three-Dimensional Impact-Angle-Constrained Guidance Law Based on a Super-Twisting Observer.” In 2026 5th International Symposium on Control Engineering and Robotics (ISCER). IEEE. https://doi.org/10.1109/iscer70245.2026.11681400
• Zhao, Yao, Yongzhi Sheng, and Xiangdong Liu. 2014. “Sliding Mode Control Based Guidance Law with Impact Angle Constraint.” Chinese Journal of Aeronautics 27 (1): 145–52. https://doi.org/10.1016/j.cja.2013.12.011
• Zhao, Yao, Yongzhi Sheng, and Xiangdong Liu. 2016. “Impact Angle Constrained Guidance for All-Aspect Interception with Function-Based Finite-Time Sliding Mode Control.” Nonlinear Dynamics 85 (3): 1791–1804. https://doi.org/10.1007/s11071-016-2795-0
• Zhao, Xinxin, Jinguang Shi, Huajie Ren, and Zhongyuan Wang. 2025c. “Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft.” Aerospace 12 (6): 558. https://doi.org/10.3390/aerospace12060558
• Zhao, Xin, Jiang Wang, Yaning Wang, and Yinhan Wang. 2025a. “Analytical Trajectory Prediction for Intercepting Aerial Vehicles Using Proportional Navigation Guidance Law.” In 2025 4th Conference on Fully Actuated System Theory and Applications (FASTA). IEEE. https://doi.org/10.1109/fasta65681.2025.11138473
• Zhao, Jianbo, and Shuxing Yang. 2018. “Integrated Cooperative Guidance Framework and Cooperative Guidance Law for Multi-Missile.” Chinese Journal of Aeronautics 31 (3): 546–55. https://doi.org/10.1016/j.cja.2017.12.013
• Zhao, Jianbo, Shuxing Yang, and Fenfen Xiong. 2019. “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, Yaming, Nanjia Yu, Tianwen Li, and Chuang Zhou. 2024b. “Experimental Study on the Combustion and Pressure Drop Characteristics of a Pintle Injector for LOX/kerosene Rocket Engine.” Acta Astronautica 219: 208–19. https://doi.org/10.1016/j.actaastro.2024.03.018
• Zhao, Shu-yuan, Bo-ming Zhang, and Shan-yi Du. 2009. “Probabilistic Modeling of Transient Heat Transfer and Assessment of Thermal Reliability of Fibrous Insulation under Aerodynamic Heating Conditions.” International Journal of Thermal Sciences 48 (7): 1302–10. https://doi.org/10.1016/j.ijthermalsci.2008.11.004
• Zhao, Linlin, Jiayuan Zhang, Yinuo Hu, Lei Qian, and Xiaoying Sun. 2024a. “Analysis on Tail-Distribution of End-to-End Latency in MEC-Based Tactile Teleoperation Systems.” In 2024 IEEE Wireless Communications and Networking Conference (WCNC). IEEE. https://doi.org/10.1109/wcnc57260.2024.10570967
• 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 Juanjuan. 2016. “Operational Effectiveness of Excursion Link for Antagonizing Anti-Radiation Missile.” In 2016 2nd IEEE International Conference on Computer and Communications (ICCC). IEEE. https://doi.org/10.1109/compcomm.2016.7924713
• Zhao YiNan, Zhou ZhiQuan, and Qiao XiaoLin. 2005. “Angle Estimation for Two Closely Spaced Targets with Polarization Monopulse Radar.” In 2005 Asia-Pacific Microwave Conference Proceedings, vol. 1. IEEE. https://doi.org/10.1109/apmc.2005.1606354
• Zhaohui, Hu, Luo Jixun, and Yang Liu. 2014. “Research on Anti-Jamming Performance Test Planning of Active Radar Guided Air-to-Air Missile.” In 2014 Seventh International Symposium on Computational Intelligence and Design. IEEE. https://doi.org/10.1109/iscid.2014.10
• 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
• Zhe, Zheng, Zhai Jiahuan, Jia Dongrui, Zhou Leichzen, and Zhou Yang. 2016. “The Principle and Implementation of Monopulse Antenna Angle Error Signal Simulator.” In 2016 8th IEEE International Conference on Communication Software and Networks (ICCSN). IEEE. https://doi.org/10.1109/iccsn.2016.7586658
• Zhen, Shang, and Chen Baixiao. 2019. “Research on Anti-Jamming Technology of Missile-Borne SAR in Complex Electromagnetic Environment.” In 2019 6th Asia-Pacific Conference on Synthetic Aperture Radar (APSAR). IEEE. https://doi.org/10.1109/apsar46974.2019.9048366
• Zhen Wang, A. Sinha, P. Willett, and Y. Bar-shalom. 2004. “Angle Estimation for Two Unresolved Targets with Monopulse Radar.” IEEE Transactions on Aerospace and Electronic Systems 40 (3): 998–1019. https://doi.org/10.1109/taes.2004.1337470
• Zheng, Yongbin, Huimin Chen, and Zongtan Zhou. 2018. “Angle Measurement of Objects outside the Linear Field of View of a Strapdown Semi-Active Laser Seeker.” Sensors 18 (6): 1673. https://doi.org/10.3390/s18061673
• Zheng, Huiling, Jun Yang, and Yu Zhao. 2023. “Reliability Demonstration Test Plan for Degraded Products Subject to Gamma Process with Unit Heterogeneity.” Reliability Engineering & System Safety 240: 109617. https://doi.org/10.1016/j.ress.2023.109617
• Zheng Shouduo, Ye Wei, and Fan Qinghui. 2015. “A Kind of Method Research of Monopulse Radar Angular Glint Suppression.” In 2015 12th IEEE International Conference on Electronic Measurement & Instruments (ICEMI). IEEE. https://doi.org/10.1109/icemi.2015.7494325
• Zhengyan, Zhang, and Zhang Jianyun. 2017. “Target Angle Tracking Algorithm Based on the Covariance Matrix for Bistatic MIMO Radar.” In 2017 IEEE 17th International Conference on Communication Technology (ICCT). IEEE. https://doi.org/10.1109/icct.2017.8359722
• Zhengyu, Guo, and Liang Xiaogeng. 2011. “Pole Placement Controller Design for Relaxed Stable Stability Missile.” In 2011 International Conference on Electronics, Communications and Control (ICECC). IEEE. https://doi.org/10.1109/icecc.2011.6067734
• Zhenyu Liu Zhimei Zhou and Yueqiu Han. n.d. “Tracking Radar Digital Matched-Filter ASIC Design and Its Error Analysis.” In Asia-Pacific Conference on Circuits and Systems, vol. 1. IEEE. https://doi.org/10.1109/apccas.2002.1115039
• 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 Ye, D. Lee, G. J. Saulnier, and M. J. Medley. n.d. “Anti-Jam, Anti-Multipath Spread Spectrum OFDM System.” In Conference Record of Thirty-Second Asilomar Conference on Signals, Systems and Computers (Cat. No.98CH36284), vol. 2. IEEE. https://doi.org/10.1109/acssc.1998.751633
• Zhongjie Meng, Jianzhong Dong, Panfeng Huang, and Jie Yan. 2010. “Multi-Constrained Fast Trajectory Optimization of Glide Phase for Hypersonic Vehicle.” In 2010 8th World Congress on Intelligent Control and Automation. IEEE. https://doi.org/10.1109/wcica.2010.5554861
• Zhou, Hao, Tao Cheng, Xiaoming Liu, and Wanchun Chen. 2020d. “Three-Dimensional Geometric Descent Guidance with Impact Angle Constraint.” IEEE Access 8: 64932–48. https://doi.org/10.1109/access.2020.2984353
• Zhou, Shuai, Fangmian Dong, Meng Zhang, Xinyao Lei, Chengkui Wu, and Hongjun Liu. 2026a. “Analysis of Throttling Characteristics and Sensitivity of a Mixed Mode Staged Combustion Cycle Liquid Rocket Engine.” Acta Astronautica 249: 704–24. https://doi.org/10.1016/j.actaastro.2026.07.044
• Zhou, Zhen-yu, and Zhi-yi He. 2011. “Research on Suppressing Angle Glint of Complex Target.” In 2011 7th International Conference on Wireless Communications, Networking and Mobile Computing. IEEE. https://doi.org/10.1109/wicom.2011.6040620
• Zhou, Zhen-yu, Zhi-yi He, Xin Zhao, and Ye Luo. 2010b. “Practicable Research on Suppressing Angular Glint Base on the Target’s RCS Weights.” In 2010 6th International Conference on Wireless Communications Networking and Mobile Computing (WiCOM). IEEE. https://doi.org/10.1109/wicom.2010.5600721
• Zhou, Shou, Cheng Hu, Pan Wu, and Shifeng Zhang. 2020b. “Impact Angle Control Guidance Law Considering the Seeker’s Field-of-View Constraint Applied to Variable Speed Missiles.” IEEE Access 8: 100608–19. https://doi.org/10.1109/access.2020.2997805
• Zhou, Zeyang, and Jun Huang. 2023. “Facilitating Learning Adaptive V-Tail of a Supersonic Missile for Radar Cross-Section Reduction during Interval Flight.” Heliyon 9 (10): e20984. https://doi.org/10.1016/j.heliyon.2023.e20984
• Zhou, Jianping, Wei Li, Qunli Xia, and Huan Jiang. 2023c. “Robust Missile Autopilot Design Based on Dynamic Surface Control.” Journal of Systems Engineering and Electronics 34 (1): 160–71. https://doi.org/10.23919/jsee.2022.000154
• Zhou, Man, Dapeng Mao, Mingyue Zhang, Lihong Guo, and Mingde Gong. 2018. “A Hybrid Control with PID–Improved Sliding Mode for Flat-Top of Missile Electromechanical Actuator Systems.” Sensors 18 (12): 4449. https://doi.org/10.3390/s18124449
• Zhou, Di, Chundi Mu, and Wenli Xu. 1999. “Adaptive Sliding-Mode Guidance of a Homing Missile.” Journal of Guidance, Control, and Dynamics 22 (4): 589–94. https://doi.org/10.2514/2.4421
• Zhou, Hongyu, Xiaogang Wang, and Naigang Cui. 2019b. “Glide Trajectory Optimization for Hypersonic Vehicles via Dynamic Pressure Control.” Acta Astronautica 164: 376–86. https://doi.org/10.1016/j.actaastro.2019.08.012
• Zhou, Xinghe, Weihong Wang, and Chao Lai. 2019d. “A Novel Guidance Law Using Integral Terminal Sliding Mode with Impact Angle Constraint.” In 2019 Chinese Control Conference (CCC). IEEE. https://doi.org/10.23919/chicc.2019.8866557
• Zhou, Xinghe, Weihong Wang, Zhenghua Liu, Chen Liang, and Chao Lai. 2019c. “Impact Angle Constrained Three-Dimensional Integrated Guidance and Control Based on Fractional Integral Terminal Sliding Mode Control.” IEEE Access 7: 126857–70. https://doi.org/10.1109/access.2019.2939418
• Zhou, Xinghe, Weihong Wang, Weibo Xia, and Chen Liang. 2020a. “Fixed Time Integrated Guidance and Control with Impact Angle Constraint.” In 2020 IEEE 16th International Conference on Control & Automation (ICCA). IEEE. https://doi.org/10.1109/icca51439.2020.9264375
• Zhou, Fansen, Lei Wang, Wei Zheng, Xiang Zhou, and Xin Wen. 2026b. “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, He, and Jianxin Wu. 2026. “An Adaptive Monopulse Angle Estimation Method via Polarization Fusion for MIMO Conformal Arrays.” Signal Processing 238: 110153. https://doi.org/10.1016/j.sigpro.2025.110153
• Zhou, Guanqun, and Qunli Xia. 2020. “A Guidance Strategy for Strapdown Seeker Considering Minimum Field-of-View Angle Constraint.” International Journal of Aerospace Engineering 2020: 1–11. https://doi.org/10.1155/2020/5247257
• Zhou, Wei, Junhao Xie, Yeshu Yuan, and Shaobin Li. 2014. “Angle Measurement Accuracy Analysis of Sum-Difference Amplitude-Comparison Monopulse in Onshore or Shipborne ISAR.” In 2014 19th International Conference on Digital Signal Processing. IEEE. https://doi.org/10.1109/icdsp.2014.6900722
• Zhou, Wei, Shuxing Yang, and Jinlong Dong. 2013a. “Coning Motion Instability of Spinning Missiles Induced by Hinge Moment.” Aerospace Science and Technology 30 (1): 239–45. https://doi.org/10.1016/j.ast.2013.08.008
• Zhou, Chuang, Nanjia Yu, Shuwen Wang, et al. 2023b. “The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines.” Aerospace 10 (1): 65. https://doi.org/10.3390/aerospace10010065
• Zhou, Shou, Shifeng Zhang, and Donghui Wang. 2020c. “Impact Angle Control Guidance Law with Seeker’s Field-of-View Constraint Based on Logarithm Barrier Lyapunov Function.” IEEE Access 8: 68268–79. https://doi.org/10.1109/access.2020.2986355
• Zhou, Rong, Chenxiao Zhang, and Guanglei Zhang. 2019a. “Generalized Space- Time Adaptive Monopulse Angle Estimation Approach.” In 2019 International Conference on Control, Automation and Information Sciences (ICCAIS). IEEE. https://doi.org/10.1109/iccais46528.2019.9074719
• Zhou, Yanzhang, Dianxin Zhao, Zhen Li, Shihao Li, and Qingpeng Zhang. 2024. “A Human-Centered Human-Machine Function Allocation Method Based on Reinforcement Learning.” In 2024 12th International Conference on Information Systems and Computing Technology (ISCTech). IEEE. https://doi.org/10.1109/isctech63666.2024.10845228
• Zhou, Zhi-tan, Chang-fang Zhao, Chen-yu Lu, and Gui-gao Le. 2021. “Numerical Studies on Four-Engine Rocket Exhaust Plume Impinging on Flame Deflectors with Afterburning.” Defence Technology 17 (4): 1207–16. https://doi.org/10.1016/j.dt.2020.06.016
• Zhou Weiwen, Liang Xiaogeng, and Jia Xiaohong. 2010. “Finite-Time Stability Analysis of Proportional Navigation Guidance System.” In 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems. IEEE. https://doi.org/10.1109/icicisys.2010.5658711
• Zhu, Shiquan, Zhihua Chen, Hui Zhang, Zhengui Huang, and Huanhao Zhang. 2018b. “Investigations on the Influence of Control Devices to the Separation Characteristics of a Missile from the Internal Weapons Bay.” Journal of Mechanical Science and Technology 32 (5): 2047–57. https://doi.org/10.1007/s12206-018-0414-3
• Zhu, Boyu, Youmin Gong, Jie Mei, and Guangfu Ma. 2025c. “Three-Phase Zero-Effort-Miss/Zero-Effort-Velocity Guidance with Elevation Angle Constraint.” In 2025 China Automation Congress (CAC). IEEE. https://doi.org/10.1109/cac67268.2025.11486706
• Zhu, Yaonan, Bingheng Jiang, Qibin Chen, Tadayoshi Aoyama, and Yasuhisa Hasegawa. 2023b. “A Shared Control Framework for Enhanced Grasping Performance in Teleoperation.” IEEE Access 11: 69204–15. https://doi.org/10.1109/access.2023.3292410
• Zhu, Yalu, Feng Liu, and William A. Sirignano. 2026b. “Simulation of Multi-Injector H2-O2 Rocket Combustion Instability.” AIAA Journal 64 (1): 205–23. https://doi.org/10.2514/1.j065542
• Zhu, Lin, Shuang Qiu, and Yubing Han. 2018a. “Combined Constrained Adaptive Sum and Difference Beamforming in Monopulse Angle Estimation.” IEEE Antennas and Wireless Propagation Letters 17 (12): 2314–18. https://doi.org/10.1109/lawp.2018.2873818
• Zhu, Huatian, Linan Wang, Yujun Wang, Xinhe Wang, and Qiyu Yin. 2023a. “Finite-Time Three-Dimensional Cooperative Guidance Law for Moving Target with Line-of-Sight Angle Constraint.” In 2023 International Conference on Neuromorphic Computing (ICNC). IEEE. https://doi.org/10.1109/icnc59488.2023.10462891
• Zhu, Huatian, Guanghui Wen, Linan Wang, and Jinhu Lü. 2025a. “Impact-Angle-Constrained Cooperative Guidance: An Event-Triggered Finite-Time Strategy.” IEEE Transactions on Aerospace and Electronic Systems 61 (4): 10038–49. https://doi.org/10.1109/taes.2025.3556115
• Zhu, Zheng, Yuanqing Xia, Mengyin Fu, and Shuo Wang. 2011. “An Observer-Based Missile Guidance Law.” In 2011 Chinese Control and Decision Conference (CCDC). IEEE. https://doi.org/10.1109/ccdc.2011.5968387
• Zhu, Di, Yongbin Zheng, Wanying Xu, and Shengjian Bai. 2022. “An Accurate Line-of-Sight Rate Estimation Method Based on LSTM Recurrent Neural Network for Strapdown Imaging Seeker.” IEEE Sensors Journal 22 (22): 21827–36. https://doi.org/10.1109/jsen.2022.3208013
• 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
• Zinn, Ben T. 1968. “A Theoretical Study of Nonlinear Combustion Instability in Liquid-Propellant Rocket Engines.” AIAA Journal 6 (10): 1966–72. https://doi.org/10.2514/3.4908
• Zinn, Ben T., and Eugene A. Powell. 1971. “Nonlinear Combustion Instability in Liquid-Propellant Rocket Engines.” Symposium (International) on Combustion 13 (1): 491–503. https://doi.org/10.1016/s0082-0784(71)80051-6
• Zinn, B. T., and C. T. Savell. 1969. “A Theoretical Study of Three-Dimensional Combustion Instability in Liquid-Propellant Rocket Engines.” Symposium (International) on Combustion 12 (1): 139–47. https://doi.org/10.1016/s0082-0784(69)80398-x
• Zou, Sheng, Ming Yu, Xianxu Yuan, Siwei Dong, and Yulu Liu. 2026. “High-Speed Turbulent Boundary Layer over the Leeward Side of the Lifting Body Model HyTRV.” Aerospace Science and Technology 175: 111936. https://doi.org/10.1016/j.ast.2026.111936
• Zucrow, M. J. 1947. “Liquid Propellant Rocket Power Plants.” Journal of the American Rocket Society 00 (72): 26–44. https://doi.org/10.2514/8.4186
• Zwagerman, P. K. 1988. “Air-to-Ground Ranging Using Electronic Roll Stabilization of Monopulse Data.” In Proceedings of the 1988 IEEE National Radar Conference. IEEE. https://doi.org/10.1109/nrc.1988.10949

Primary Sources, Non-Peer-Reviewed

• The 14th Annual Conference on Manual Control. 1978. NASA-CP-2060. NASA. https://ntrs.nasa.gov/citations/19790007417
• “8. the Longitudinal Motion of a Missile.” 1953. In Discontinuous Automatic Control. Princeton University Press. https://doi.org/10.1515/9781400877218-010
• ;;. 2003. “Expected Miss Distance Concept and Its Applications to Aircraft Guidance Law for Arbitrary Flight Trajectory Tracking.” Journal of Control Automation and Systems Engineering 9 (6): 478–88. https://doi.org/10.5302/j.icros.2003.9.6.478
• Abbas, Jehad, R. Ibrahim, and Ronald Gibson. 1992. “Nonlinear Flutter of Orthotropic Composite Panel under Aerodynamic Heating.” In Dynamics Specialists Conference. AIAA 1992-2132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2132
• Abbe, C., C. McLaughlin, and E. Weiss. 1967. “Influence of Storable Propellant Liquid Rocket Design Parameters on Combustion Instability.” In 3rd Propulsion Joint Specialist Conference. AIAA 1967-474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-474
• Abdallah, M. 2018. “Modelling and Simulation of an Anti-Tank Guided Missile.” International Journal of Engineering Research and V7 (09). https://doi.org/10.17577/ijertv7is090051
• 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
• Abdelhamid, O. 1985. “Aerodynamic Characteristics of Quasi-Slender Wing: Body Combinations at Supersonic Velocities.” International Conference on Aerospace Sciences and Aviation Technology 1 (CONFERENCE): 1–9. https://doi.org/10.21608/asat.1985.26464
• Abdulrahim, Mujahid, Helen Garcia, and Rick Lind. 2004. “Flight Testing a Micro Air Vehicle Using Morphing for Aeroservoelastic Control.” In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference. AIAA 2004-1674. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1674
• Abel, I. 1971. “A Critical Wind-Tunnel Evaluation of a Technique for Predicting Static Aerodynamic Characteristics for a Highly Flexible Supersonic Transport Configuration.” In 12th Structures, Structural Dynamics and Materials Conference. AIAA 1971-343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-343
• Aberg, R., C. Francis, J. Ryon, I. Bellavin, and C. Loughmiller. 1962. Navy Air to Air Missile Study Fire Control Requirements. Defense Technical Information Center. https://doi.org/10.21236/ad0376576
• 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
• Abramovitz, M. 1952. Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems-Effect of Method of Positioning the Radar Antenna on the Speed of Response. NACA-RM-A52E27. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19630002663
• Abramovitz, Marvin. 1953. Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Missile Configuration on the Speed of Response. NACA-RM-A52J22. NASA. https://ntrs.nasa.gov/citations/19930090424
• Abratanski, Artur, Rafał Grzejda, and Rafał Perz. 2023. “Feasibility Study of Topology Optimization of the Control System Frame for the Missile with Canard Configuration.” Aircraft Engineering and Aerospace Technology 95 (5): 814–19. https://doi.org/10.1108/aeat-04-2022-0109
• Acharya, M., M. I. Kussoy, and C. C. Horstman. 1978. “Reynolds Number and Pressure Gradient Effects on Compressible Turbulent Boundary Layers.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780036832
• Acheson, Kurt, and Mark Rothnie. 2009. “Fast and Accurate Use of Unstructured CFD Methods to Assess Performance and Aerodynamic Heating of Reusable Launch Vehicles in Hypersonic Flight.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3632
• “Acoustic Sensitivity Measurements of Injectors in a Small Liquid Propellant Rocket Engine.” 1996. In Recent Advances in Spray Combustion: Spray Combustion Measurements and Model Simulation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866432.0369.0392
• “Active Radar Missile Seekers.” 2012. In Pulse Doppler Radar: Principles, technology, applications. Institution of Engineering and Technology. https://doi.org/10.1049/sbra024e_ch18
• Acuff, Chris, and Trong Bui. 2015. “NASA Armstrong’s Approach to Store Separation Analysis.” In NASA AFRC Meeting. https://ntrs.nasa.gov/citations/20150014964
• Ada, Celâl, and Ayhan Kural. 2017. “Three-Axes Predictive Control of Autopilot for Missile.” Aircraft Engineering and Aerospace Technology 89 (1): 1–10. https://doi.org/10.1108/aeat-06-2014-0090
• Adamović, Pavle, Zlatko Petronijević, Nebojša Jovičić, Aleksandar Stefanović, and Miloš Pavić. 2022. “Lead Compensator Design for DC Motor Driven Electromechanical Fin Actuator.” Scientific Technical Review 72 (2): 44–49. https://doi.org/10.5937/str2202044a
• Adams, Gaynor J. 1951. Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings. NACA-TN-2270. NASA. https://ntrs.nasa.gov/citations/19930083072
• Adams, James L. 1962. An Investigation of the Effects of the Time Lag Due to Long Transmission Distance upon Remote Control. Phase II: Vehicle Experiments. Phase III: Conclusions. NASA-TN-D-1351. NASA. https://ntrs.nasa.gov/citations/19620001000
• Adams, Gaynor J., and Dugan W. Duane. 1952. Theoretical Damping in Roll and Rolling Moment Due to Differential Wing Incidence for Slender Cruciform Wings and Wing-Body Combinations. NACA-TR-1088. NASA. https://ntrs.nasa.gov/citations/19930091085
• 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
• “Adaptive Neural Network–Based Autopilot Design.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-12
• Adcock, J. B., A. L. Braslow, D. I. McRee, and J. B. Peterson Jr. 1966. Further Investigation of Effect of Air Injection through Slots and Porous Surfaces on Flat-Plate Turbulent Skin Friction at Mach 3. NASA-TN-D-3311. NASA. https://ntrs.nasa.gov/citations/19660011639
• Adel, Outayeb, Farid Ferguene, and R. Toumi. 2017. “Adaptive Neural Control for Bilateral Teleoperation System Using External Force Approach.” In International Conference on Informatics in Control, Automation and Robotics (ICINCO). https://doi.org/10.5220/0006419603090315
• Advanced Fuel Research INC East Hartford CT. 1957. Handbook of Supersonic Aerodynamics. Volume 3. Defense Technical Information Center. https://doi.org/10.21236/ada390317
• “Advances in Missile Guidance Theory.” 2001. Aircraft Engineering and Aerospace Technology 73 (1). https://doi.org/10.1108/aeat.2001.12773aae.003
• “Aerodynamic Heating for Gaps in Laminar and Transitional Boundary Layers.” 1981. In Aerothermodynamics and Planetary Entry. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865510.0003.0035
• “Aerodynamic Heating to the X-24C Hypersonic Research Configuration.” 1979. In Thermophysics and Thermal Control. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865398.0192.0214
• “Aerodynamic Hinge Moments on a Sealed Plain Trailing-Edge Flap at High Mach Number.” 1991. In 9th Applied Aerodynamics Conference. AIAA 1991-3244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3244
• “Aerodynamics of Arbitrary Wing Body Combinations with Vortex Latticeand Slender Body Theory.” 1976. In 14th Aerospace Sciences Meeting. AIAA 1976-198. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-198
• Aerojet-General Corp Sacramento Ca. 1963. Product Engineering Program. Coated Metallic Thrust Chambers Expandable Nozzles Combustion Instability Scaling Concepts Ablative Thrust Chambers. Weapon System 107A-2. Defense Technical Information Center. https://doi.org/10.21236/ad0423407
• Agarwal, G. C., F. Osafo-Charles, W. D. Oneill, and G. L. Gottlieb. 1982. Modeling of Human Operator Dynamics in Simple Manual Control Utilizing Time Series Analysis. Illinois Univ. https://ntrs.nasa.gov/citations/19820026162
• 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
• Aguilar, Rodolfo J., Franques Jr., and John T. 1969. Studies in the Methodology of Weapons Systems Effectiveness Analysis: Using the Techniques of Simulation, Optimization and Statistics: Phase 2. Volume 4. Formulation and Optimization of Warhead Kill Probabilities. Defense Technical Information Center. https://doi.org/10.21236/ad0875381
• 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
• Ahuja, Vivek. 2026. “Validation of Compressible-Flow Panel-Methods for the Analysis of the Transonic and Supersonic Aerodynamics of Long-Range Air-Launched Missiles.” In AIAA SCITECH 2026 Forum. AIAA 2026-1325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1325
• Ahuja, Vivek, Roy J. Hartfield, and Matthew S. Campbell. 2025. “Transonic Store-Separation Analysis Using a Compressible Surface-Vorticity Panel Method.” In AIAA SCITECH 2025 Forum. AIAA 2025-1263. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1263
• Ai, X. L., Y. C. Shen, and L. L. Wang. 2019. “Adaptive Integrated Guidance and Control for Impact Angle Constrained Interception with Actuator Saturation.” Aeronautical Journal 123 (1267): 1437–53. https://doi.org/10.1017/aer.2019.71
• Ailneni, Sanketh, Sudesh Kumar Kashyap, Amitabh Saraf, David Livingstone, and A. Kabadwal. 2023. “Airborne Separation Inertial System (ASIS) and Trajectory Computation of Aircraft Launched Stores – a Solution to Store Separation in Flight Testing.” In AIAA AVIATION 2023 Forum. AIAA 2023-3779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3779
• 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 Life Cycle Mgmt Center Armament DIR. 2013. AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). Defense Technical Information Center. https://doi.org/10.21236/ada614731
• “The Air Force Strategic Missile Program.” 2002. In Titan II. University of Arkansas Press. https://doi.org/10.2307/j.ctvvng4n.7
• “Aircraft and Missile Impact — Data and Analysis.” n.d. In Explosion-Resistant Buildings. Springer-Verlag. https://doi.org/10.1007/3-540-31289-7_7
• “Aircraft Store Separation Motion Prediction via Grid Data Trajectories.” 1980. In 11th Aerodynamic Testing Conference. AIAA 1980-462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-462
• Akbulatov, Edkham Sh., Vladimir V. Koshlakov, Sergey V. Mosolov, et al. 2026. “Design Development and Experimental Studies of Chambers of Low-Thrust Rocket Engines with Regenerative Cooling.” Siberian Aerospace Journal 27 (2): 238–57. https://doi.org/10.31772/2712-8970-2026-27-2-238-257
• Akdag, Remzi, and Turgay Altilar. 2005. “A Comparative Study on Practical Evasive Maneuvers against Proportional Navigation Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6352. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6352
• Akimov, V. N., A. A. Kostyukov, E. N. Kravchuk, and K. O. Rozantsev. 2021. “Refining the Aerodynamic Moment of the Missile Based on Flight Test Results.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 4: 47–56. https://doi.org/10.38013/2542-0542-2021-4-47-56
• Akishita, S., R. Kurosaki, K. Okada, and T. Hirata. 1984. “Theoretical Prediction of Roll Moment on Wing-Controlled Missile.” In 2nd Applied Aerodynamics Conference. AIAA 1984-2148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-2148
• Aksu, Arda. 2014. “Aerodynamic Parameter Estimation of a Missile without Wind Angle Measurements.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2557. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2557
• Al-Ashtari, Waleed Kh. 2008. “A Full Missile Homing System Design Based on Proportional Navigation Guidance Law and Electro-Optical Tracking System.” Journal of Engineering 14 (03): 2806–24. https://doi.org/10.31026/j.eng.2008.03.19
• Al-barzinji, Jamal. n.d. “A Stochastic Time-Series Model of the Human Performance in Compensatory Tracking.” PhD diss., Louisiana State University and Agricultural & Mechanical College. https://doi.org/10.31390/gradschool_disstheses.2588
• Al-Obaidi, Abdulkareem Shafiq Mahdi. 2011. “Implementation of Semi-Empirical Models to Enhance the Accuracy of Panel Methods for Drag Prediction at Supersonic Speeds.” IIUM Engineering Journal 12 (3). https://doi.org/10.31436/iiumej.v12i3.71
• Albanese, Kimberly, Mary Meyers, Kassandra Prusko, and Michael Courtney. 2012. Altitude Dependence of Rocket Motor Performance. Defense Technical Information Center. https://doi.org/10.21236/ada571357
• Alcock, Joseph, and Steven Hagar. 1989. “Transferring Jet Engine Diagnostic and Control Technology to Liquid Propellant Rocket Engines.” In 25th Joint Propulsion Conference. AIAA 1989-2851. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2851
• Aldrich, G. T., and W. B. Krabill. 1972. “A Versatile Kalman Technique for Aircraft or Missile State Estimation and Error Analysis Using Radar Tracking Data.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19720055423
• Alexander, William E. 1970. A Transducer for Controlling Simulated Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0875525
• Alexander, A., G. Aleksey, N. Igor, et al. 2011. “Development Liquid Rocket Engine of Small Thrust with Combustion Chamber from Carbon: Ceramic Composite Material.” In InTech eBooks. https://doi.org/10.5772/18160
• Alhadhrami, Esra. n.d. “An Innovative Integration of JPDA-LSTM Synergy and Explainable AI for Enhanced Multi-Target Tracking and Radar Performance.” PhD diss., Sorbonne université. https://doi.org/10.70675/e0e55678z3d11z4bb9z9e87z16b5aa408381
• Alhussan, K. 2007. “A Novel Design: Porous Boundary Condition for Drag Reduction of Three Dimensional Rotating Body of Revolution—Slender Body.” In New Trends in Fluid Mechanics Research. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-75995-9_83
• Ali, K. M., M. Abozied, I. Arafa, and Y. Elhalwagy. 2019. “Design of a Roll Autopilot for a Skid-to-Turn Guided Missile.” IOP Conference Series: Materials Science and Engineering 610 (1): 012017. https://doi.org/10.1088/1757-899x/610/1/012017
• Alksne, Alberta Y. 1957. Determination of Vortex Paths by Series Expansion Technique with Application to Cruciform Wings. NACA-TR-1311. NASA. https://ntrs.nasa.gov/citations/19930092303
• Allee, E. G., Jr. 1980. Store Separation Testing Techniques at the Arnold Engineering Development Center, Volume 4. Description of Dynamic Drop Store Separation Testing. Defense Technical Information Center. https://doi.org/10.21236/ada087490
• Allen, H. Julian. 1955. Motion of a Ballistic Missile Angularly Misaligned with the Flight Path upon Entering the Atmosphere and Its Effect upon Aerodynamic Heating, Aerodynamic Loads, and Miss Distance. NACA-RM-A56F15. NASA. https://ntrs.nasa.gov/citations/19930089312
• Allen, Julian H. 1957. Motion of a Ballistic Missile Angularly Misaligned with the Flight Path upon Entering the Atmosphere and Its Effect upon Aerodynamic Heating, Aerodynamic Loads, and Miss Distance. NACA-TN-4048. NASA. https://ntrs.nasa.gov/citations/19930084822
• Allen, J. M. 1970. Experimental Preston Tube and Law-of-the-Wall Study of Turbulent Skin Friction on Axisymmetric Bodies at Supersonic Speeds. NASA-TN-D-5660. NASA. https://ntrs.nasa.gov/citations/19700008939
• Allen, J. 1981. “Comparison of Analytical and Experimental Supersonic Aerodynamic Characteristics of a Forward Control Missile.” In 19th Aerospace Sciences Meeting. AIAA 1981-398. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-398
• Allen, Jerry M. 2005. Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and in-Line Tail Fins from Mach 0.60 to 4.63. NASA/TM-2005-213541. NASA. https://ntrs.nasa.gov/citations/20050160470
• Allen, Max J., Timothy A. Brahan, Joshua C. Coya, et al. 2026. “Roll Control of a Smooth Body Missile.” In AIAA SCITECH 2026 Forum. AIAA 2026-0506. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-0506
• Allen, J. M., and K. R. Czarnecki. 1965. Effects of Surface Emittance on Turbulent Skin Friction at Supersonic and Low Hypersonic Speeds. NASA-TN-D-2706. NASA. https://ntrs.nasa.gov/citations/19650008903
• Allen, J., and M. Dillenius. 1979. “Vortex Development on Slender Missiles at Supersonic Speeds.” In 17th Aerospace Sciences Meeting. AIAA 1979-360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-360
• Allen, J. M., and W. J. Monta. 1965. Local Turbulent Skin-Friction Measurements on a Flat Plate at Mach Numbers from 2.5 to 4.5 and Reynolds Numbers up to 69 x 106. NASA-TN-D-2896. NASA. https://ntrs.nasa.gov/citations/19650018215
• 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, C. Q., R. G. Schwind, and G. N. Malcolm. 1978. Canard-Body-Tail Missile Test at Angles of Attack to 50 Deg in the Ames 11-Foot Transonic Wind Tunnel. NASA-TM-78441. NASA. https://ntrs.nasa.gov/citations/19790003850
• Allen, Jerry, David Shaw, and Wallace Sawyer. 1989. “Analysis of Selected Data from the Triservice Missile Data Base.” In 27th Aerospace Sciences Meeting. AIAA 1989-478. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-478
• 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
• Almeida, Fabio. 2021. “Model Predictive Control and Constrained Dynamic Compensation for a Hypersonic Flight Vehicle.” In AIAA Scitech 2021 Forum. AIAA 2021-1566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1566
• Almeida, Daniel Soares de, Emerson Andrade dos Santos, and Günter Langel. 2021. “Upper Stage Liquid Propellant Rocket Engine: A Case Analysis.” Journal of Aerospace Technology and Management 13: e1221. https://doi.org/10.1590/jatm.v13.1203
• Alongi, Robert. 1966. “Strapdown System Application Studies Related to a Surface to Surface Missile of 100 to 400 Nautical Miles.” In Guidance and Control Conference. AIAA 1966-1811. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1811
• 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
• Alsaka, Y. A., L. A. Young, and M. Hamid. 1993. “Nonbiased Geometric Centroid for High Resolution Radar Angle Tracking.” IEE Proceedings F Radar and Signal Processing 140 (5): 297. https://doi.org/10.1049/ip-f-2.1993.0041
• 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
• Altınöz, Bağış, Hüsamettin Eken, Anıl Cönger, and Sultan Can. 2024. “Modelling Inertial Measurement Unit Error Parameters for an Unmanned Air Vehicle.” Communications Faculty of Sciences University of Ankara Series A2-A3 Physical Sciences and Engineering 66 (1): 64–81. https://doi.org/10.33769/aupse.1308165
• Alves Almeida, Ana Clecia, Reece Davis, and Jonathan Armbrust. 2024. “Design and Flight Vehicle Integration of a VAPAK Liquid Engine Rocket.” In 2024 Regional Student Conferences. AIAA 2024-86165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-86165
• Aman Prakash, K. A. Suraj, and Ansab Peter. 2024. “Estimation of Base Drag for a Subsonic Missile Configuration Using CFD.” ACS Journal for Science and Engineering 4 (1): 89–95. https://doi.org/10.34293/acsjse.v4i1.108
• Amirkhizi, Alireza, Fernando Campos, Fatemeh Seyhani, et al. 2024. “Variability of Mechanical Properties of Parachute Canopy Fabrics Relevant to Deployment.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4517. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4517
• Amos, R., and R. Amos. 1997. “Structural Testing of the Bonded Body for an Insensitive Munitions Air-to-Air Missile.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-3130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3130
• An, Jiguang, Ming Yan, Wenbo Zhou, Xuexiong Shan, and Zhen Yan. 1989. “Aerodynamic-Guidance-Trajectory Simulation of Tactical Missile.” In Guidance, Navigation and Control Conference. AIAA 1989-3590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3590
• “Analysis of Pressure Feasibility Limits in Regenerative Cooling of Combustion Chambers for Large-Thrust Rockets.” 1960. In Liquid Rockets And Propellants. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864759.0543.0562
• “Analysis of Proportional Navigation Guided Missile Systems in the Frequency Domain.” 2007a. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-7
• “Analysis of Proportional Navigation Guided Missile Systems in the Time Domain.” 2007b. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-6
• “Analysis of Proportional Navigation Guided Systems in the Frequency Domain.” 2011a. In Guidance of Unmanned Aerial Vehicles. CRC Press. https://doi.org/10.1201/b10807-8
• “Analysis of Proportional Navigation Guided Systems in the Time Domain.” 2011b. In Guidance of Unmanned Aerial Vehicles. CRC Press. https://doi.org/10.1201/b10807-7
• Ananthasayanam, M. R., and A. K. Sarkar. 2005. “Nonlinear Observer State Estimation from Seeker Measurements and Seeker-Radar Measurements Fusion.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6066
• Anděl, Jiří. 1974. “On evaluation of some two-dimensional normal probabilities.” Applications of Mathematics 19 (1): 28–35. https://doi.org/10.21136/am.1974.103511
• 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. 1961. Investigation of Static Stability and Aerodynamic Effects of Control Jets on a 1/3-SCALE Pye Wacket Missile at Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0322137
• 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, G. 1979a. “A Comparison of Air-to-Air Missile Guidance Laws Based on Optimal Control and Differential Game Theory.” In Guidance and Control Conference. AIAA 1979-1736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1736
• Anderson, William P. 1979b. Target Missile Airframe Costs. Defense Technical Information Center. https://doi.org/10.21236/ada073314
• Anderson, Seth B. 1986. A Look at Handling Qualities of Canard Configurations. NASA-TM-88354. NASA. https://ntrs.nasa.gov/citations/19870013196
• 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, Wesly, Stephen D. Heister, and Carl Hartsfield. 2019. “Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine.” In AIAA Scitech 2019 Forum. AIAA 2019-0474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0474
• Anderson, William E., Stephen D. Heister, and Steven S. Son. 2013. Fuel Chemistry and Combustion Distribution Effects on Rocket Engine Combustion Stability. Defense Technical Information Center. https://doi.org/10.21236/ada577052
• Anderson, William E., Stephen D. Heister, and Steven S. Son. 2015. Fuel Chemistry and Combustion Distribution Effects on Rocket Engine Combustion Stability. Defense Technical Information Center. https://doi.org/10.21236/ad1001343
• Anderson, Eric, and Jacob Lopata. 1996. “Using a Modified SR-71 Aircraft and Air-Launched Expendable Rockets to Place Small Payloads into Orbit.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2774
• Anderson, M., R. McAmis, C. Bracier, J. Drakes, D. Brown, and R. Howard. 1996. “Advanced Measurement Diagnostics for Liquid Propellant Rocket Engine Anomaly Investigation and Health Monitoring.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2613
• Anderson, William, Harry Ryan, Robert Santoro, and Ross Hewitt. 1995. “Combustion Instability Mechanisms in Liquid Rocket Engines Using Impinging Jet Injectors.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2357
• Anderson, William E., Steven F. Son, and Stephen D. Heister. 2012. Fuel Chemistry and Combustion Distribution Effects on Rocket Engine Combustion Stability. Defense Technical Information Center. https://doi.org/10.21236/ada566310
• Andon, Jerar. 1965. Nuclear Blast Vulnerability of Shelter Electrical Generating Equipment: Diesel Engine Overpressure Tolerance. Defense Technical Information Center. https://doi.org/10.21236/ad0684462
• Andrey, Belyakov. 2011. “Aerodynamic Heating at Hypersonic Speed.” In InTech eBooks. https://doi.org/10.5772/13890
• Andriievskyi, M. V., Yu. A. Mitikov, and D. A. Shamrovskyi. 2018. “Control Peculiarities of Rocket Engine Which Runs on Ecologically-Friendly Storable Propellant.” Herald of Aeroenginebuilding 0 (1). https://doi.org/10.15588/1727-0219-2018-1-2
• 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
• Androsenkov, V. A., R. M. Zaichuk, and A. T. Ponomarev. 2007. “Mathematical Modeling of Cruciform Parachute Deployment.” Russian Aeronautics (Iz VUZ) 50 (1): 89–93. https://doi.org/10.3103/s1068799807010151
• Anggara, Riswan. 2025. “Design of a Teleoperation Haptic Control System with Network Delay Compensation Using Passivity Based Control and Observers.” Journal of Electrical Engineering 2 (03): 85–94. https://doi.org/10.54209/elimensi.v2i03.415
• Angué, J. C., N. Malvache, and D. Roger. 1978. “An Attempt to Identify the Visual and Manual Phenomena for a Human Operator Submitted to Vestibular Stimulations (Pitch Motion) during Visual Detection Tasks.” In Control of Distributed Parameter Systems. Elsevier. https://doi.org/10.1016/b978-0-08-022018-5.50044-6
• Anjaly, P., and Ashwini Ratnoo. 2016. “A Beam Rider Concept for Three Point Aerial Rendezvous Guidance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-2108. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2108
• Anoop, C. R., John Bejoy, Thomas Tharian, and P. V. Venkitakrishnan. 2015. “Evaluation of Mechanical Properties of the Rocket Thrust Chamber Material under Flight Conditions.” In Materials science forum, vol. 830-831. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/msf.830-831.219
• Apostol, Silviu, Fabian Breharu, and Florin Mingireanu. 2013. “Serious Game Application in Anti-Aircraft Missile Training.” Internet Learning. https://doi.org/10.18278/il.2.1.6
• “Appendix C: Rocket Engine Materials.” 1992. In Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866197.0399.0403
• Application of Slender-Body Theory. 2025. Wiley. https://doi.org/10.1002/9781394285662.ch3
• “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
• “Application to Missile Guidance: Proportional Navigation.” 2010. In Optimal Control Theory with Aerospace Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600867347.0231.0239
• Arbic, R. G., and W. Gillespie Jr. 1952. Flight Determination of the Longitudinal Stability of a 1 10-SCALE Rocket-Powered Model of the Northrop MX-775A Missile at Low Lift Coefficients and Mach Numbers from 0.89 to 1.34. NACA-RM-SL52112. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19630038252
• 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
• Aretz, Anthony J., Joseph C. Hickox, and Susan R. Kesler. 1987. “Dynamic Function Allocation in Fighter Cockpits.” Proceedings of the Human Factors Society Annual Meeting 31 (4): 414–18. https://doi.org/10.1177/154193128703100407
• Arita, Shunsaku, and Seiya Ueno. 2013. “Optimal Feedback Guidance for Nonlinear Missile Model with Impact Time and Angle Constraints.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4785
• Armstrong, D. L. 1952. Investigation of Liquid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0009863
• Armstrong, Elizabeth. 1989. “Liquid Oxygen Cooling of Hydrocarbon Fueled Rocket Thrust Chambers.” In 25th Joint Propulsion Conference. AIAA 1989-2739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2739
• Armstrong, D. L., and S. B. Kilner. 1953. Investigation of Liquid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0009747
• Armstrong, Elizabeth, and Julie Schlumberger. 1990. “Cooling of Rocket Thrust Chambers with Liquid Oxygen.” In 26th Joint Propulsion Conference. AIAA 1990-2120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2120
• Army Aviation Board Fort Rucker Al. 1960. Helicopter-Mounted SS-11 Anti-Tank Guided Missile System. Defense Technical Information Center. https://doi.org/10.21236/ada030732
• Army Materiel Command Alexandria VA. 1975. Missile Manufacturing Technology Conference Held at Hilton Head Island, South Carolina on 22-26 September 1975. Panel Presentations: Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada017242
• 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 Missile Command Redstone Arsenal AL. 1963. Automated Cost Estimates: Ace. Defense Technical Information Center. https://doi.org/10.21236/ad0609268
• 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
• Army War Coll Carlisle Barracks Pa. 1952. Handbook of Supersonic Aerodynamics. Defense Technical Information Center. https://doi.org/10.21236/ada390507
• Arnold, W., III, N. Gates, and Arlynn Wilson. 1991. “Multivariable Stability Margins for Missile Autopilot Coupling.” In Navigation and Control Conference. AIAA 1991-2615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2615
• Arrow, A. 1982. An Analysis of Aerodynamic Requirements for Coordinated Bank-to-Turn Autopilots. NASA-CR-3644. NASA. https://ntrs.nasa.gov/citations/19830004802
• Arrow, A., and D. Williams. 1987. “Comparison of Classical and Modern Autopilot Design and Analysis Techniques for a Tactical Air-to-Air Bank-to-Turn Missile.” In Guidance, Navigation and Control Conference. AIAA 1987-2581. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2581
• Arrow, A., and D. Yost. 1976. “Large Angle-of-Attack Missile Control Concepts for Aerodynamically Controlled Missiles.” In Guidance and Control Conference. AIAA 1976-1944. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1944
• Artigas Esclusa, Jordi. n.d. “Time Domain Passivity Control for Delayed Teleoperation.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.33677
• Arunajatesan, Srinivasan, Christopher Chartrand, and Roger Birkbeck. 2009. “Analysis of Unsteady Bay Shear Layer Effects on Store Separation Characteristics.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-546. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-546
• As’ad, Faisal, Philip Avery, Charbel Farhat, Jason Rabinovitch, and Marcus Lobbia. 2022. “Validation of a High-Fidelity Supersonic Parachute Inflation Dynamics Model and Best Practice.” In AIAA SCITECH 2022 Forum. AIAA 2022-0351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0351
• As’ad, Faisal, Philip Avery, Charbel Farhat, Jason Rabinovitch, Marcus Lobbia, and Navid Ataei. 2024. “Sensitivity Analysis and Validation of a Computational Framework for Supersonic Parachute Inflation Dynamics.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4656. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4656
• Asadsangabi, Zohreh, Reza Mohseni, and Sadegh Samadi. 2024. “Optimizing the OFDM Radar Waveform for Low-Angle Target Tracking Using WAF Criteria.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4218893/v1
• Ashford, D. M. 1965. “Boost-Glide Vehicles for Long Range Transport.” Journal of the Royal Aeronautical Society 69 (655): 448–58. https://doi.org/10.1017/s000192400005908x
• 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
• “Assessment of Thrust Chamber Performance.” 2004. In Liquid Rocket Thrust Chambers. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866760.0601.0620
• Assisi, Aladin. 2001. “Analysis of the Angle Tracking Error Induced in a Radar Homing Missile by Phase-Front Distorted Jamming.” International Conference on Aerospace Sciences and Aviation Technology 9 (9): 1129–38. https://doi.org/10.21608/asat.2001.59811
• Assisi, Aladin. 2006. “Simulation of an Active Radar Homing Missile under Phase-Front Distortion Jamming.” International Conference on Electrical Engineering 5 (5): 1–10. https://doi.org/10.21608/iceeng.2006.33665
• Asthana, C., and Prahlad. 1989. “Evaluation of Missile Seeker Dwell Time for Three-Dimensional Aerialengagements.” In Guidance, Navigation and Control Conference. AIAA 1989-3484. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3484
• Astrakhov, V. V. 2016. “The Origins of Mobile Medium-Range Surface-to-Air Missile Systems.” Military Thought 25 (001): 152–61. https://doi.org/10.21557/mth.46655762
• Astrov, Igor, Svetlana Tatarly, and Svetlana Tatarly. 2007. “Simulation of Missile Autopilot with Two-Rate Hybrid Neural Network System.” Advances in Electrical and Computer Engineering 7 (1): 18–22. https://doi.org/10.4316/aece.2007.01004
• 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
• Ates, Ulas H. 2015. “Lyapunov Based Nonlinear Impact Angle Guidance Law for Stationary Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0863. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0863
• Ates, Ulas H. 2016. “Nonlinear Impact Angle Control Guidance Law for Stationary Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-2112. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2112
• Ates, Ulas H. 2018. “Impact Angle Guidance Law via Controlling Line-of-Sight Dynamics.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1321. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1321
• Ates, Ulas H. 2019. “Detailed Analysis of Nonlinear Impact Angle Guidance Law via Controlling Line-Of-Sight Dynamics.” In AIAA Scitech 2019 Forum. AIAA 2019-1929. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1929
• Athearn, Christopher B. 2015. Joint Air-to-Surface Standoff Missile (JASSM). Defense Technical Information Center. https://doi.org/10.21236/ad1019462
• Atir, Ronen, Gyorgy Hexner, Haim Weiss, and Tal Shima. 2009. “Target Maneuver Adaptive Guidance Law for a Bounded Acceleration Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6089
• Atkinson, P. 1968. “The Dynamics of a Simple Servomechanism for Angular Position Control.” In Feedback Control Theory for Engineers. Springer New York. https://doi.org/10.1007/978-1-4684-7453-4_8
• Atkinson, Christopher J. 2016. “Modeling of Inertial Control Surface Hinge Moments Using Quaternion Calculations.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2016-1185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1185
• Atwood, Christopher A. 1993. “Computation of a Controlled Store Separation from a Cavity.” In Computation of the Fluid and Optical Fields About the Stratospheric Observatory for Infrared Astronomy (SOFIA) and the Coupling of Fluids, Dynamics, and Control Laws on Parallel Computers. https://ntrs.nasa.gov/citations/19940012040
• Atwood, Christopher. 1994. “Computation of a Controlled Store Separation from a Cavity.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-31. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-31
• Atygayev, Talgat, Victor Ivel, Julia Gerasimova, and Pavel Petrov. 2022. “Onboard System for Correcting the Flight Range of an Unguided Missile.” Trudy Universiteta, no. 2: 278–83. https://doi.org/10.52209/1609-1825_2022_2_278
• 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, 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
• Autenrieb, Johannes, and Patrick Gruhn. 2025. “An Iterative Control Allocation Algorithm for Hypersonic Glide Vehicles with Asymmetric Magnitude and Rate Limits.” In AIAA SCITECH 2025 Forum. AIAA 2025-2265. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2265
• Avdieiev, V. V., and A. E. Aleksandrov. 2023. “Missile Movement Control System Stability Reserve.” System design and analysis of aerospace technique characteristics 32 (1): 3–14. https://doi.org/10.15421/472301
• Avery, D., P. Kerr, and A. Wieting. 1983. “Experimental Aerodynamic Heating to Simulated Shuttle Tiles.” In 18th Thermophysics Conference. AIAA 1983-1536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1536
• Avinash, Gunti, Saiseshu Reddy, and P. Vijaya Poojitha. 2020. “Design and Prototype Development of Quadrant Estimation Unit for Laser Beam Rider Guidance System.” International Journal of Engineering and Computer Science 9 (03): 24970–77. https://doi.org/10.18535/ijecs/v9i03.4449
• Awad, A., and H. P. Wang. 2016a. “Integrated Pitch-Yaw Acceleration Autopilot Design for Varying-Velocity Man Portable Missile.” International Journal of Modeling and Optimization 6 (1): 11–17. https://doi.org/10.7763/ijmo.2016.v6.496
• Awad, Ahmed, and Haoping Wang. 2017. “Integrated Roll-Pitch-Yaw Autopilot via Equivalent Based Sliding Mode Control for Uncertain Nonlinear Time-Varying Missile.” International Journal of Aeronautical and Space Sciences 18 (4): 688–96. https://doi.org/10.5139/ijass.2017.18.4.688
• Azuma, Nobuyuki, Daisuke Ogawa, Asuka Iijima, Kazuyuki Higashino, Tetsuo Hiraiwa, and Mitsuharu Oguma. 2016. “Material Compatibility of Bio-Ethanol Fuel with Rocket Engine Combustion Chamber Cooling Channels.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-5088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5088
• Baba, Yoriaki, and Robert Howe. 1988. “Suboptimal Guidance with Line-of-Sight Rate Only Measurements.” In Guidance, Navigation and Control Conference. AIAA 1988-4066. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4066
• 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
• Baba, Yoriaki, Tetsuya Takehira, and Hiroyuki Takano. 1994. “New Guidance Law for a Missile with Varying Velocity.” In Guidance, Navigation, and Control Conference. AIAA 1994-3565. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3565
• 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
• 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
• Babish, C., III. 1970. “A Continuous Surface of Revolution Parachute for Supersonic/hypersonic Speeds.” In 3rd Aerodynamic Deceleration Systems Conference. AIAA 1970-1173. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1173
• Babu, K., I. Sarma, and K. Swamy. 1994b. “Two Variable-Structure Homing Guidance Schemes with and without Target Maneuver Estimation.” In Guidance, Navigation, and Control Conference. AIAA 1994-3566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3566
• Bacci, David, and Alistair j. Saddington. 2022. “Exploring Angle-of-Attack Effects in the Aero-Acoustic Response of a Weapons Bay at Transonic and Supersonic Mach Number.” In 28th AIAA/CEAS Aeroacoustics 2022 Conference. AIAA 2022-3008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3008
• Bacci, David, and Alistair J. Saddington. 2024. “Angle of Attack Effects on the Induced Structural Loads of a Weapons Bay.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4353517/v1
• Backus, F. I. 1965. A Study of Various Analytical Techniques for the Inflight Compensation of Gyro Drift Rates. NASA-CR-54574. NASA. https://ntrs.nasa.gov/citations/19660010163
• Baczynski, Christopher. 2022. “Effects of Grain Geometry and Vibration on the Suppression of Combustion Instability in a Solid Rocket Motor.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14661933.v1
• Badinand, T., and T. Fransson. 2002. “Study of Radiative Heat Transfer in Film Cooled LH/LO Rocket Engines Thrust Chamber.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-920. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-920
• Bae, Ji-Yeul, Hyung Mo Bae, Jihyuk Kim, Dae Yoon Jung, and Hyung Hee Cho. 2017. “Effect of Evasive Maneuver against Air to Air Infrared Missile on Survivability of Aircraft.” Journal of the Computational Structural Engineering Institute of Korea 30 (6): 501–6. https://doi.org/10.7734/coseik.2017.30.6.501
• Baehr, E. F. 1964. New Method Used to Fabricate Light-Weight Heat Exchanger for Rocket Motor. LEW-43. NASA. https://ntrs.nasa.gov/citations/19630000059
• Baetz, Jay G. 1974. Experimental Evaluation of Coated Graphite ICBM Rocket Nozzle Throat Inserts. Defense Technical Information Center. https://doi.org/10.21236/ad0783200
• Baetz, Jay G. 1975. Characterization of Advanced Solid Rocket Nozzle Materials. Defense Technical Information Center. https://doi.org/10.21236/ada020041
• Bagley, Hubert D., and Novella S. Billions. 1963a. Atmospheric Environment for Pershing Missile 403. Defense Technical Information Center. https://doi.org/10.21236/ad0409880
• Bagley, Hubert D., and Novella S. Billions. 1963b. Atmospheric Environment for Pershing Missile 405. Defense Technical Information Center. https://doi.org/10.21236/ad0410411
• Bai, Yang. 2013. “Miss Distance Error Analysis of Strapdown Seeker Imaging System.” Advanced materials research 753-755: 1976–79. https://doi.org/10.4028/www.scientific.net/amr.753-755.1976
• 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
• Bairamov, Farit D., and Bulat F. Bairamov. 2022. “Optimal Stabilization of Operation of Liquid-Propellant Rocket Engine.” Trudy MAI, no. 125. https://doi.org/10.34759/trd-2022-125-03
• Bakeman, D. C. 1962. Missile Design for the Effects of Winds Aloft. Defense Technical Information Center. https://doi.org/10.21236/ad0609275
• Baker, R. 1967. “Inert Calibration of Deep-Throttling Bipropellant Rocket Engines.” In 3rd Propulsion Joint Specialist Conference. AIAA 1967-427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-427
• Baker, R. 1969. “Prediction of Flight Performance of a Throttling, Ablative Rocket Engine.” In 5th Propulsion Joint Specialist. AIAA 1969-452. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-452
• 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, Chris J., and Anthony Zyweck. 2010. Radar Missile Seekers. Wiley. https://doi.org/10.1002/9780470686652.eae280
• Balakrishnan, S. 1987. “A Dual Control Homing Guidance Law.” In Guidance, Navigation and Control Conference. AIAA 1987-2448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2448
• Balakrishnan, S. N., and V. Biega. 1995. “A New Neural Architecture for Homing Missile Guidance.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 3. American Autom Control Council. https://doi.org/10.1109/acc.1995.531278
• 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
• Balakrishnan, S., J. Shen, J. Grohs, S. Balakrishnan, J. Shen, and J. Grohs. 1997. “Hypersonic Vehicle Trajectory Optimization and Control.” In Guidance, Navigation, and Control Conference. AIAA 1997-3531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3531
• Balakrishnan, S., and J. Speyer. 1986. “Assumed Density Filter with Application to Homing Missile Guidance.” In Astrodynamics Conference. AIAA 1986-2262. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2262
• 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
• Baldwin, R., and J. Hanking. 1980. “Real-Time Simulator Evaluation of Interactive Control of a Supersonic Missile.” In Guidance and Control Conference. AIAA 1980-1748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1748
• Balepin, V. 2001. “Liquid Air Augmented Rocket Engine for a Small Reusable SSTO Launcher (More Rocket than Any Rocket-Based Combined Cycle).” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3236
• Balepin, Vladimir. 2006. “Concept of the Third Fluid Cooled Liquid Rocket Engine.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4695. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4695
• Ball, J. 1978. “Rolling Tail Design and Behavior as Affected by Actuator Hinge Moment Limits.” In Aircraft Systems and Technology Conference. AIAA 1978-1500. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1500
• Ballenger, John. 1998. “Enhanced Fiber-Optic Guided Missile (EFOGM): Precision Fire for Early Entry Forces.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5150
• “BALLISTIC MISSILE and AEROSPACE TECHNOLOGY.” 1961. In Design and Reliability, and Invited Addresses. Elsevier. https://doi.org/10.1016/b978-1-4832-2899-0.50001-9
• Ballistic Missile Office Norton AFB CA. 1986. Human Factors Engineering Program for Intercontinental Ballistic Missile Systems, (MIL-STD-1794(USAF)). Defense Technical Information Center. https://doi.org/10.21236/ada278185
• Balraj Sharma, Squadron Leader. 2023. “Improvements in Classical Proportional Navigation Guidance Using Fuzzy Logic.” Journal of Aerospace Sciences and Technologies: 229–38. https://doi.org/10.61653/joast.v72i4.2020.190
• Balusamy, Kathiravan, A. Vinothraj, and V. Suresh. 2024. “Aero-Spike and Aero-Disk Effects of on Wave Drag Reduction of Supersonic Flow past over Blunt Body.” Aircraft Engineering and Aerospace Technology 96 (2): 233–47. https://doi.org/10.1108/aeat-04-2023-0088
• Banani, Seyed Alireza, and Bita Imam. 2011. “3-Dimensional Maneuvering Target Tracking with Online Observed Colored Glint Noise Parameter Estimation.” In Control and Applications. ACTAPRESS. https://doi.org/10.2316/p.2011.729-088
• Bandyopadhyay, G. 1989. “Low Speed Aerodynamics of Canard Configurations.” Aeronautical Journal 93 (921): 22–28. https://doi.org/10.1017/s0001924000016651
• Banerjee, Srijan, Debolina Bhattacharjee, Software Engineer, Videonatics Technology Private Limited 49/2, Mahendra Banerjee Road, Behala, Kolkata – 700060, West Bengal, India, and Souma Banerjee. 2015. “Controller Design for a Two-Loop Missile Autopilot in Pitch Plane.” International Journal Of Engineering And Computer Science. https://doi.org/10.18535/ijecs/v4i9.36
• Banerjee, A., and L. Utreja. 1975. “Drogue Parachute Deployment Dynamics of the Space Shuttle Solid Rocket Booster.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1383
• Bang, Dao Thanh. 2026. “Improving the Accuracy of Target Coordinate Determination in the Tracking and Illumination Radar of Air Defense Missile Systems Using Statistical Signal Processing.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0526002.2
• 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
• Barber, H. T., Jr., and R. R. Lundstrom. 1956. Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined from Flight Test for a Mach Number Range of 1.1 to 1.8. NACA-RM-L55L16. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19690067240
• Barlog, S. 1979. “Practical Aspects of Reefing Cutter Designfor Full Parachute Deployment.” In 6th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1979-418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-418
• Barnett, Bruce. 1962. Trajectory Equations for a Six-Degree-of-Freedom Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0615569
• Barnhardt, Michael, Travis Drayna, Ioannis Nompelis, Graham Candler, and William Garrard. 2007. “Detached Eddy Simulations of the MSL Parachute at Supersonic Conditions.” In 19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2007-2529. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2529
• Barnwell, Richard. 1989. “A Skin Friction Law for Compressible Turbulent Flow.” In 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1989-1864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1864
• Baron, Sheldon, and William H. Levison. 1977. “Display Analysis with the Optimal Control Model of the Human Operator.” Human Factors: The Journal of the Human Factors and Ergonomics Society 19 (5): 437–57. https://doi.org/10.1177/001872087701900502
• 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
• Barrett, Ron. 1993. “Aeroservoelastic DAP Missile Fin Development.” Smart Materials and Structures 2 (2): 55–65. https://doi.org/10.1088/0964-1726/2/2/001
• Bartrand, Timothy A. 1988. “Evaluation and Improvement of Liquid Propellant Rocket Chugging Analysis Techniques. Part 2: A Study of Low Frequency Combustion Instability in Rocket Engine Preburners Using a Heterogeneous Stirred Tank Reactor Model.” PhD diss., Tennessee Univ.. https://ntrs.nasa.gov/citations/19880017841
• 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, Zarrin T., Quincy E. McKown, Karen Mae Baldonado, et al. n.d. “Pterodactyl: 6-DOF Integration of Guidance and Control Algorithms in Genesis.” In AIAA SciTech Forum and Exposition. https://ntrs.nasa.gov/citations/20240014893
• “Basics of Missile Guidance.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-4
• Bass, Steven, Thomas Thompson, and John Rutherford. 1995. “Fixed-Wing Performance Predictions of the Canard Rotor/wing Concept Based on Wind Tunnel Test Results.” In 13th Applied Aerodynamics Conference. AIAA 1995-1887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1887
• Bass, Steven, Thomas Thompson, John Rutherford, and Stephen Swanson. 1993. “Low-Speed Wind Tunnel Test Results of the Canard Rotor/Wing Concept.” In 11th Applied Aerodynamics Conference. AIAA 1993-3412. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3412
• Bastress, E. K., G. H. Harris, and I. Miller. 1967. Statistical Derivation of Design Criteria for Liquid Rocket Combustion Instability Final Report. NASA-CR-72370. NASA. https://ntrs.nasa.gov/citations/19680010275
• Baty, Daniel L. 1970. Effects of Display Gain on Human Operator Information Processing Rate in a Rate Control Tracking Task: (506132009-013). American Psychological Association (APA). https://doi.org/10.1037/e506132009-013
• Baugher, Skyler K., and Datta V. Gaitonde. 2023. “3D Effects of Doors on Cavity Bay Dynamics.” In AIAA SCITECH 2023 Forum. AIAA 2023-1003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1003
• Baum, Joseph D., and Jay N. Levine. 1982. Nonlinear Combustion Instability in Solid Rocket Motors: A Numerical Study of Longitudinal Oscillations with Pressure and Velocity Coupling. Defense Technical Information Center. https://doi.org/10.21236/ada115084
• Baum, Joseph D., and Jay N. Levine. 1984. Modeling of Nonlinear Combustion Instability in Solid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ada176271
• Bayoğlu, Tuğba, Ozan Nalci, and Ali T. Kutay. 2016. “Aerodynamic Parameter Estimation of a Supersonic Air to Air Missile with Rapid Speed Variation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2016-3856. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3856
• Baysal, Oktay. 1986. Supersonic Aerodynamic Interference Effects of Store Separation. Part 1: Computational Analysis of Cavity Flowfields. NASA-CR-180311. NASA. https://ntrs.nasa.gov/citations/19870017424
• Baysal, Oktay. 1991. Viscous Flow Simulations of Internal Store Carriage and Separation. NASA-CR-185343. NASA. https://ntrs.nasa.gov/citations/19910016809
• Baysal, Oktay. 1995. A CFD Study of Complex Missile and Store Configurations in Relative Motion. NASA-CR-197912. NASA. https://ntrs.nasa.gov/citations/19950016532
• Baysal, Oktay, Robert L. Stallings Jr., and Elizabeth B. Plentovich. 1989. “Navier-Stokes Solutions for Flows Related to Store Separation.” In NASA Computational Fluid Dynamics Conference. Volume 1: Sessions 1-6. https://ntrs.nasa.gov/citations/19910001548
• Bazarov, Vladimir. 1998. “Non-Linear Interactions in Liquid-Propellant Rocket Engine Injectors.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-4039. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4039
• Beard, Randal, Jess Curtis, Martin Eilders, Johnny Evers, and James Cloutier. 2007. “Vision Aided Proportional Navigation for Micro Air Vehicles.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6609
• Beare, A. C., and A. Kahn. 1967. Describing Functions for Compensatory Tracking of Sine Waves Plus Noise. Westinghouse Electric Corp. https://ntrs.nasa.gov/citations/19680006440
• Beck, R. A. S. 1984a. Aerodynamic Heating Computations for Projectiles. Volume 3. BRL Interactive Plotting Program (BRLINPLOT). Defense Technical Information Center. https://doi.org/10.21236/ada143254
• Beck, Robin A. 1984b. Aerodynamic Heating Computations for Projectiles: Vol. 3: BRL Interactive Plotting Program (BRLINPLOT). Defense Technical Information Center. https://doi.org/10.21236/ada328840
• 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
• Begum, Rumena, and Faisal Aqlan. 2025. “Human-Machine Teaming Function Allocation: A Systematic Review.” In IISE Annual Conference & Expo 2025. Curran Associates, Inc. https://doi.org/10.21872/annual2025_6834
• Behr, Vance. 1989. “The Development and Testing of the HISAC Parachute Recovery System.” In 10th Aerodynamic Decelerator Conference. AIAA 1989-921. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-921
• Beideman, Larry R., Frank E. Gomer, and Sheldon H. Levine. 1980. Dynamic Target Acquisition: Empirical Models of Operator Performance. Defense Technical Information Center. https://doi.org/10.21236/ada092263
• Bejczy, Antal K., Paolo Fiorini, Won Soo Kim, and Paul Schenker. 1994. Toward Integrated Operator Interface for Advanced Teleoperation under Time-Delay. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20060038557
• Bejczy, Antal K., Paolo Fiorini, Won Soo Kim, and Paul S. Schenker. 1995. “Toward Integrated Operator Interface for Advanced Teleoperation under Time-Delay.” In Intelligent Robots and Systems. Elsevier. https://doi.org/10.1016/b978-044482250-5/50023-2
• Bekey, G. A., J. M. Biddle, and A. J. Jacobson. 1967. The Effect of a Random Sampling Interval on a Sampled-Data Model of the Human Operator. NASA-CR-87263. NASA. https://ntrs.nasa.gov/citations/19680017493
• Bekey, G. A., C. Jacobs, and M. J. Merritt. 1966. Pulse Models of Human Operators Performing Compensatory Tracking with Coordinated Multiple Inputs. University of Southern California. https://ntrs.nasa.gov/citations/19670000852
• Bekey, G. A., H. F. Meissinger, and R. E. Rose. 1965. Mathematical Models of Human Operators in Simple Two-Axis Manual Control Systems. NASA. https://ntrs.nasa.gov/citations/19650052770
• Belcher. n.d. “Ballistic Missile Defense Radar.” In Principles of Modern Radar: Volume 3: Radar Applications. Institution of Engineering and Technology. https://doi.org/10.1049/sbra503e_ch7
• Bell, William, and Lon Pringle. 2000. “The Impact of Seeker Angular Resolution on the Miss Distance of Tactical Missiles.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-770. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-770
• Bell Aerospace Co Buffalo Ny. 1953. Project Rascal, Project Shrike. Defense Technical Information Center. https://doi.org/10.21236/ad0010755
• Bell Aerospace Co Buffalo Ny. 1954. RASCAL WEAPON SYSTEM (Project MX-776). Defense Technical Information Center. https://doi.org/10.21236/ad0046714
• Bell Aerospace Co Buffalo Ny. 1955. MX-2276 Reconnaissance Aircraft Weapon System. System Design. Defense Technical Information Center. https://doi.org/10.21236/ad0125726
• Bell Aerospace Co Buffalo Ny. 1956. MX-776. Defense Technical Information Center. https://doi.org/10.21236/ad0113976
• Bello, R. 1981. “Miss Distance Indicators.” In 1st Flight Test Conference. AIAA 1981-2509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2509
• Bellows, J., R. Brewster, and E. Bekir. 1984. “OTV Liquid Rocket Engine Control and Health Monitoring.” In 20th Joint Propulsion Conference. AIAA 1984-1286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1286
• Belousov, V. L., M. S. Ramm, and A. A. Schmidt. 1990. “Wave Processes Occuring in Supersonic Motion of Blunted Body through Dust Layer.” In AIP Conference Proceedings, vol. 208. AIP. https://doi.org/10.1063/1.39459
• Beltran, M., and T. Kosvic. 1966. “Parametric Study of Combustion Instability in MMHNTO Liquid Rocket Engine.” In 2nd Propulsion Joint Specialist Conference. AIAA 1966-603. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-603
• Belyakov, V. A. 2022. “The Choice of the Energy Parameters of an Oxygen-Hydrogen Propellant Expander Cycle Rocket Engine.” Siberian Aerospace Journal 23 (3): 424–36. https://doi.org/10.31772/2712-8970-2022-23-3-424-436
• Ben-Asher, Joseph Z., and Jason L. Speyer. 2016. “Games in Aerospace: Homing Missile Guidance.” In Handbook of Dynamic Game Theory. Springer International Publishing. https://doi.org/10.1007/978-3-319-27335-8_25-1
• Ben-Gida, Hadar. 2022. “Experimental Study of the Transonic Flow within a Jet-Fighter Weapons Bay with Internal Stores.” In AIAA AVIATION 2022 Forum. AIAA 2022-3448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3448
• Ben-Gida, Hadar. 2023b. “Experimental Study of an Air-to-Ground Store Release from a Jet-Fighter Weapons Bay in Transonic Flow Conditions.” In AIAA AVIATION 2023 Forum. AIAA 2023-4497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4497
• Ben-Porat, Ori, Moshe Shoham, and Joachim Meyer. 2000. “Control Design and Task Performance in Endoscopic Teleoperation.” Presence: Teleoperators and Virtual Environments 9 (3): 256–67. https://doi.org/10.1162/105474600566781
• Benavoli, Alessio, Luigi Chisci, Alfonso Farina, Sandro Immediata, and Luca Timmoneri. 2007. Knowledge-Based Radar Tracking. Wiley. https://doi.org/10.1002/9780470283158.ch8
• Benjamin, Theodore, and Paul McConnaughey. 1991. “Navier-Stokes Analysis of a Liquid Rocket Engine Disk Cavity.” In 27th Joint Propulsion Conference. AIAA 1991-2361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2361
• Bennewitz, John W., David M. Lineberry, and Robert A. Frederick. 2013. “Investigation of a Single Injector with Applied High Frequency Pressure Disturbances for Applications to Liquid Rocket Engine Combustion Instabilities.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3853
• Benson, Willard R. 1954. The Basic Method of Calculating the Lethal Area of the Warhead. Defense Technical Information Center. https://doi.org/10.21236/ad0044471
• Benstein, Eli. 1989. “An Assessment of Supersonic Gas Turbine Missile Propulsion Potential.” In 25th Joint Propulsion Conference. AIAA 1989-2471. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2471
• Benstein, Eli H. 1991. “An Assessment of Supersonic Gas Turbine Missile Propulsion Potential.” International Journal of Turbo and Jet Engines 8 (1–2). https://doi.org/10.1515/tjj.1991.8.1-2.101
• 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, Keith, Steve Tavan, and Amer Fejzic. 2011. “Accuglide: Precision Airdrop Guidance and Control via Glide Slope Control.” In 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2011-2530. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2530
• Berglind, Torsten, and Lars Tysell. 2010. “Numerical Investigation of the Impact of Maneuver on Store Separation Trajectories.” In 28th AIAA Applied Aerodynamics Conference. AIAA 2010-4241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4241
• Berglind, Torsten, and Lars Tysell. 2011. “Time-Accurate CFD Approach to Numerical Simulation of Store Separation Trajectory Prediction.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3958. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3958
• Bermudez, Alvaro. 2024. Design and Evaluation of a Small Scale Liquid Rocket Engine Using Pineapple’s Waste. https://doi.org/10.52202/078371-0180
• Bernard, James E., and Carolina Cruz Neira. 2002. Evaluating Human Operator Performance in a Fully Immersive Virtual Reality Environment. Defense Technical Information Center. https://doi.org/10.21236/ada400507
• Bernot, P. T., and R. B. Robinson. 1958. Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One with Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One with a Flared Afterbody and All-Movable Controls. NACA-RM-L58D24. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710074595
• Berque, J., and J. Georges. 1992. “Test of a CMC Liquid Propulsion Rocket Engine Turbine Stator.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3131. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3131
• Berry, P. E., S. Kodituwakku, and K. Venkataraman. 2017. “Generalised Phase Monopulse for Multi-Target DoA Estimation and Extended Target Spatial Imaging.” In International Conference on Radar Systems (Radar 2017). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2017.0484
• 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
• Bertin, J., and W. Goodrich. 1980. “Aerodynamic Heating for Gaps in Laminar and Transitional Boundary Layers.” In 18th Aerospace Sciences Meeting. AIAA 1980-287. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-287
• Bestard, Jaime, and Gregory Czarnecki. 2008. “Missile Miss Distance.” In 2008 U.S. Air Force T&E Days. AIAA 2008-1645. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-1645
• Betts, Erin, and Robert Frederick. 2010. “A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6541. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6541
• Beyer, Steffen. 2003. “Advanced CMC: Material Development for Future Liquid Rocket Engine Thrust Chamber Applications.” In 54th 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-03-s.3.03
• 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
• Bhashyam, N., and Naunihal Singh. 1967. “Stochastic Duels with Varying Single-Shot Kill Probabilities.” Operations Research 15 (2): 233–44. https://doi.org/10.1287/opre.15.2.233
• Bhattacharya, T. K. 1997. “Time Frequency Based Detection Scheme for Missile Approach Warning System (MAWS).” In Radar Systems (RADAR 97), vol. 1997. IEE. https://doi.org/10.1049/cp:19971734
• Bhattacharyya, Abhijit, and R. N. Bhattacharjee. 2002. “Performance Analysis of Nominal Scheme and Decoupling Loop Scheme for RF Seeker.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4774
• Bhattacharyya, Abhijit, and R. N. Bhattacharjee. 2003. “Seeker Based Optimal Guidance Law, a Few Issues.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5794
• Bheary, Mostafa. 2026. “GrainArtist: A Physics-Informed Multi-Engine Framework for Solid Rocket Propellant Grain Inverse Design.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-11025434/v1
• Bhowmick, Shiladitya, Hariprasanth Palanivel, V. Kalyana Chakravarthy, and Rinku Mukherjee. 2025. “Aerodynamic Design of Inverse Diamond-Back Joined Wing on a Slender Body at Subsonic and Supersonic Mach Numbers.” In AIAA SCITECH 2025 Forum. AIAA 2025-0254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0254
• 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
• Bialy, B., J. Klotz, J. Willard Curtis, and W. Dixon. 2012. “An Adaptive Backstepping Controller for a Hypersonic Air-Breathing Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4468
• 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
• 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
• Bickford, L. 1968. “Determining the Frequency Response of a Throttlable Liquid Rocket Engine Using White Noise Excitation.” In 2nd Simulation and Support Conference. AIAA 1968-247. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-247
• Bidwell, Jonathan, Alexandra Holloway, and Scott Davidoff. 2014. “Measuring Operator Anticipatory Inputs in Response to Time-Delay for Teleoperated Human-Robot Interfaces.” In Proceedings of the SIGCHI Conference on Human Factors in Computing Systems. ACM. https://doi.org/10.1145/2556288.2557174
• Biezad, D., and D. Schmidt. 1984. “Time Series Modeling of Human Operator Dynamics in Manual Control Tasks.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1899
• Bilich, Leonid Ayzikovich, Sergey Alekseyevich Lyovin, and Vladlena Vladlenovna Ostapova. 2018. “Air-to-Air Missile Guidance for Nonmaneuverable Target Interception at Maximum Distance.” TsAGI Science Journal 49 (7): 753–70. https://doi.org/10.1615/tsagiscij.2018029598
• Billingsley, J. P., R. H. Burt, and J. T. Best. 1979. Store Separation Testing Techniques at the Arnold Engineering Development Center. Volume 3. Description and Validation of Captive Trajectory Store Separation Testing in the Von Karman Facility. Defense Technical Information Center. https://doi.org/10.21236/ada068319
• Binion Jr. and T. W. R. D. Herron. 1962. Pressures and Forces on a Missile Model Resulting from Stage Separation at Very High Altitudes. Defense Technical Information Center. https://doi.org/10.21236/ad0290303
• Binkley, Brian, and Anton Vanderwyst. 2012. “Application of Statistical Techniques to Analyze and Model Trajectory Envelopes for Subscale Store Separation Testing.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3337
• Birch, Trevor, Jerry Allen, and Floyd Wilcox Jr. 2000b. “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
• Birch, Trevor, Ian Wrisdale, and Simon Prince. 2000a. “CFD Predictions of Missile Flowfields.” In 18th Applied Aerodynamics Conference. AIAA 2000-4211. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4211
• 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
• Bishop, Lee R. 1991. The Use and Misuse of Aircraft and Missile RCS Statistics. Defense Technical Information Center. https://doi.org/10.21236/ada239892
• Bittle, David, Gary Hall, and Roswell Nourse III. 1998. “Roll Isolation Bearing Design and Testing for Low Cost Precision Kill Missile System.” In AIAA Defense and Civil Space Programs Conference and Exhibit. AIAA 1998-5148. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5148
• Bittle, Charles, and Mitty Plummer. 2008. “A Ballistic Missile Search and Tracking System.” In 2008 Annual Conference & Exposition Proceedings. ASEE Conferences. https://doi.org/10.18260/1-2–3226
• Bjorklund, R. A., R. S. Rogero, and R. K. Baerwald. 1979. Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance,. Defense Technical Information Center. https://doi.org/10.21236/ada072125
• Black, R. 1968. “High-Speed Store Separation: Correlation between Wind-Tunnel and Flight-Test Data.” In 3rd Aerodynamics Testing Conference. AIAA 1968-361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-361
• Black, Christopher. 2020. “Timing Accuracy Test of Non-GPS-Based Positioning System at White Sands Missile Range.” In The Precise Time and Time Interval Systems and Applications Meeting. Institute of Navigation. https://doi.org/10.33012/2020.17316
• 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
• Black, G. R., F. V. Bracco, L. Crocco, et al. 1967. Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors Status Report, 1 Jun. 1966: 31 May 1967. NASA-CR-72270. NASA. https://ntrs.nasa.gov/citations/19670025793
• Black, R., and J. Picklesimer. 1971. “Captive Trajectory Technique Improvements of Store Separation Studiesin a Wind Tunnel.” In 6th Aerodynamics Testing Conference. AIAA 1971-282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-282
• Blackburn, C. P., and D. B. George. 1964. Air Launched Rocketsounding Study. Defense Technical Information Center. https://doi.org/10.21236/ad0600400
• Blackman, A., H. Ford, and D. Utvik. 1965. “Evaluation of Absorption Liners for Suppression of Combustion Instability in Rocket Engines.” In Propulsion Joint Specialist Conference. AIAA 1965-585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-585
• Blades, Eric, David Marcum, and Brent Mitchell. 2002. “Simulation of Spinning Missile Flow Fields Using U2NCLE.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2797. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2797
• Blaesild, P. 1979. “Conditioning with Conic Sections in the Two-Dimensional Normal Distribution.” Annals of Statistics 7 (3): 659–70. https://doi.org/10.1214/aos/1176344686
• 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, W. Dale, and Maite Brandt-Pearce. 1996. “Radar Waveform Requirements for Reliable Detection of an Aircraft-Launched Missile.” In SPIE Proceedings, vol. 2739, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.241911
• Blair, M., and D. DeGeorge. 2000. Overview of the Integrated High Payoff Rocket Propulsion Technology (IHPRPT) Program. Defense Technical Information Center. https://doi.org/10.21236/ada411290
• 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. 1977. Stability and Control Characteristics of a Monoplannar Missile Configuration with Two Low-Profile Tail Arrangements at Mach Numbers from 1.70 to 2.86. NASA-TM-X-3533. NASA. https://ntrs.nasa.gov/citations/19770022140
• 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 Mach Numbers from 1.90 to 2.86 of a Canard-Controlled Missile with Ram-Air-Jet Spoiler Roll Control. NASA-TP-1124. NASA. https://ntrs.nasa.gov/citations/19780012136
• Blair, A. B., Jr. 1978c. 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., Jr. 1981. “Remote Control Canard Missile with a Free-Rolling Tail Brake Torque System.” In 19th Aerospace Sciences Meeting. AIAA 1981-146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-146
• 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., Jr. 1990b. “Supersonic Aerodynamic Characteristics of Conformal Carriage Monoplanar Circular Missile Configurations with Low-Profile Quadriform Tail Fins.” In 28th Aerospace Sciences Meeting. AIAA 1990-620. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-620
• 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., Jr., W. Sawyer, and C. Jackson Jr. 1978. “A Ram-Air-Spoiler Roll Stabilization Device for Forward Control Cruciform Missiles.” In 16th Aerospace Sciences Meeting. AIAA 1978-24. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-24
• Blair, A. B., Jr., and R. L. Stallings Jr. 1988. Cavity Door Effects on Aerodynamic Loadings of Compressed-Carriage Store Configurations Separating from Cavities at Supersonic Speeds. AIAA PAPER 88-0333. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19880035017
• Blake, William. 1989. “Missile Datcom: Applications to Projectiles.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3370
• Blake, William, and William Blake. 1997. “Missile Datcom: 1997 Status and Future Plans.” In 15th Applied Aerodynamics Conference. AIAA 1997-2280. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2280
• Blake, William, and Etan Karni. 2005. “A Cambered Body Method for Missile Datcom.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4971. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4971
• 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
• Blakeley, Robert, and John Diamond. 1991. “Store Separation Wind Tunnel Testing with an in-Bay Strut Mechanism.” In 29th Aerospace Sciences Meeting. AIAA 1991-200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-200
• 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
• Blomshield, Fred. 2007. “Lessons Learned in Solid Rocket Combustion Instability.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5803. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5803
• Blumenthal, S., and J. Denton. 1962. Estimating Missile Reliability. Defense Technical Information Center. https://doi.org/10.21236/ad0291603
• Blundell, L., and R. H. Brashear. 1962. The Sucessful Application of a Repeated Test-to-Failure Program on Sergeant Missile Assemblies. Part i. the Design, Application, and Results of the Combined Operating Temperature Vibration Test for Missile Assemblies Reliability. Part II. Statistical Techniques Applied to the Sergeant Repeated Test-to-Failure Program. Part III. Conclusions and Recommendations. Sperry Utah Co. https://ntrs.nasa.gov/citations/19630007397
• 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
• Bo Liu and Wenge Chang. 2013. “Motion Compensation for Missile-Borne Frequency Stepped Chirp Radar.” In IET International Radar Conference 2013. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2013.0293
• Boatright, William B. 1952. Total Pressure and Schlieren Studies of the Wakes of Various Canard Control Surfaces Mounted on a Missile Body at a Mach Number of 1.93. NACA-RM-L52I29. NASA. https://ntrs.nasa.gov/citations/19930087326
• Boberg, B., J. Lundberg, J. Wiberg, et al. 1997. “Estimation of Target Lateral Acceleration for Augmented Proportional Navigation.” In Guidance, Navigation, and Control Conference. AIAA 1997-3565. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3565
• Bodin, N., and V. Zalgaller. 1967. “On the Concavity of Some Functions Connected with the Two-Dimensional Normal Distribution.” Lithuanian Mathematical Journal 7 (3): 389–93. https://doi.org/10.15388/lmj.1967.19978
• Bodnar, D. G. 1977. A Technique for Determining Radar Target Scintillation (GLINT). Defense Technical Information Center. https://doi.org/10.21236/ada041493
• Boeing Aerospace Co Seattle Wa. 1975. Computer Aided Function-Allocation Evaluation System. Defense Technical Information Center. https://doi.org/10.21236/ada537710
• Bogatyrev, Vladimir Valeryevich. 2017. “Numerical Investigations of the Effects of Shapes and Sizes of the Gap between the Lifting Surface and Control Surface with the Overhang Balance on Its Effectiveness and Hinge Moment.” TsAGI Science Journal 48 (1): 11–24. https://doi.org/10.1615/tsagiscij.2017020745
• Boia, John J., Gary L. Welter, and Martin F. Gakenheimer. 1994. “A Long-Baseline Method for HST Gyro Drift Rate Bias Calibration.” In NASA. Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium, 1994. https://ntrs.nasa.gov/citations/19940031107
• Boissevain, Alfred G. 1954. Experimental Investigation of the Damping in Roll of Cruciform Triangular Wing-Body Combinations at Mach Numbers from 1.5 to 6.0. NACA-RM-A54B15a. NASA. https://ntrs.nasa.gov/citations/19930088092
• Bole, Alan, Alan Wall, and Andy Norris. 2014. “Automatic Radar Target Tracking, Specified Facilities.” In Radar and ARPA Manual. Elsevier. https://doi.org/10.1016/b978-0-08-097752-2.00004-0
• Bolen, Scott. 1994. Monopulse Tracker Operating Characteristics Measurement Error Performance for Azimuth Tracking. Defense Technical Information Center. https://doi.org/10.21236/ada281188
• Bolender, Michael A., and David B. Doman. 2005. Flight Path Angle Dynamics of Air-Breathing Hypersonic Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ada444974
• Bolender, Michael, Michael Oppenheimer, and David Doman. 2007. “Effects of Unsteady and Viscous Aerodynamics on the Dynamics of a Flexible Air-Breathing Hypersonic Vehicle.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2007-6397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6397
• 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
• Bolster, W., and G. Googins. 1967. “The Design, Development, and Testing of a Series of Air-Launched Sounding Rockets.” In Sounding Rocket Vehicle Technology Specialist Conference. AIAA 1967-1328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-1328
• 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
• 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
• Bonilla Romacho, Adriana M., Penelope Nieves, Giovanni Oliveras, et al. 2023. “Loxodon-1: Bi-Propellant Liquid Rocket Engine.” In ASCEND 2023. AIAA 2023-4765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4765
• Bonometti, Joseph A., and Kirk F. Sorensen. 2006. “The Crossbow Air Launch Trade Space.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20070002822
• 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
• Borisov, D. M. 2025. “Mathematical Modeling of Hydrodynamic Instability of the Flows in Combustion Chambers Liquid Propellant Rocket Engines.” Известия Российской академии наук. Энергетика / Bulletin of the Russian Academy of Sciences. Energetics, no. 2: 53. https://doi.org/10.7868/s3034649525020042
• Borst, Howard L., Anita Friedman, and Michael Lynch. 1984. “Development and Operation of Real-Time Missile Flight Safety Display Systems at the Western Test Range.” In SPIE Proceedings, vol. 0457, edited by Elliott Schlam. SPIE. https://doi.org/10.1117/12.939403
• Bos, J. F. T., H. G. Stassen, and A. van Lunteren. 1993. “Aiding the Operator in the Manual Control of a Space Manipulator.” In Analysis, Design and Evaluation of Man–Machine Systems 1992. Elsevier. https://doi.org/10.1016/b978-0-08-041900-8.50037-2
• 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
• Bossard, Werner, and Thomas Pesek. 1991. “Vibration Damping Device for Improving the Hit Accuracy of a Firing Weapon.” Journal of the Acoustical Society of America 89 (3): 1484–1484. https://doi.org/10.1121/1.400588
• Bott, Richard. 1997. TWA Flight 800 Missile Impact Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada427917
• Boustani, Jonathan, Gokul Anugrah, Michael F. Barad, Cetin C. Kiris, and Christoph Brehm. 2020. “A Numerical Investigation of Parachute Deployment in Supersonic Flow.” In AIAA Scitech 2020 Forum. AIAA 2020-1050. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1050
• Boustani, Jonathan, Michael F. Barad, Cetin C. Kiris, and Christoph Brehm. 2019. “Fully-Coupled Fluid-Structure Interaction Simulations of a Supersonic Parachute.” In AIAA Aviation 2019 Forum. AIAA 2019-3279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3279
• Boustani, Jonathan, Gaetan Kenway, Francois Cadieux, Michael F. Barad, Christoph Brehm, and Cetin C. Kiris. 2022. “Fluid-Structure Interaction Simulations of the ASPIRE SR01 Supersonic Parachute.” In AIAA SCITECH 2022 Forum. AIAA 2022-0904. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0904
• 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
• Bower, Adam J., and Dale Thomas. 2018. “An Affordability Model Framework for the RS-25 Liquid Rocket Engine.” In 2018 Joint Propulsion Conference. AIAA 2018-4460. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4460
• Bowman, Craig T. 1967. Experimental Investigation of High-Frequency Longitudinal Combustion Instability in Gaseous Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0649860
• Bowman, Gregory, and Jason Speyer. 1987. “Detection Filters for Missile Tracking.” In Guidance, Navigation and Control Conference. AIAA 1987-2383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2383
• Boy, Guy. n.d. “Human-Centered Automation: A Matter of Agent Design and Cognitive Function Allocation.” In IFIP International Federation for Information Processing. Kluwer Academic Publishers. https://doi.org/10.1007/1-4020-8159-6_11
• 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
• Boylan, D., D. Carver, D. Stallings, and L. Trimmer. 1978. “Measurement and Mapping of Aerodynamic Heating Using a Remote Infrared Scanning Camera in Continuous Flow Wind Tunnels.” In 10th Aerodynamic Testing Conference. AIAA 1978-799. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-799
• Boylan, Gregory L., Bobbie L. Foote, and Roger Burk. 2005. A Preliminary Analysis of Loitering Aircraft as a Capability Added to Anti-Ballistic Missile Systems. Defense Technical Information Center. https://doi.org/10.21236/ada444769
• Bozsóki, Attila. 2014. “Developmental Trends in the SA–6 (2K12 KUB) Air Defence Missile Systems and the Finalized Developments in the Hungarian Air Force Surface–To–Air Missile System.” Academic and Applied Research in Military and Public Management Science 13 (2): 283–93. https://doi.org/10.32565/aarms.2014.2.6
• Bracco, F. V., L. Crocco, J. B. Elgin, et al. 1968. Nonlinear Aspect of Combustion Instability in Liquid Propellant Rocket Motors Status Report No. 8, 1 Jun. 1967: 31 May 1968. NASA-CR-72426. NASA. https://ntrs.nasa.gov/citations/19680020511
• Bradley, Edward. 1987. “Advanced Medium Range Air-to-Air Missile (AMRAAM) System Overview.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-462
• 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
• Braithwaite, Moyle. 1962. Extrapolation Techniques of Kill Probability Data. Defense Technical Information Center. https://doi.org/10.21236/ad0294011
• Brandeau, Erich, John C. Gallon, Allen Witkowski, and Christopher L. Tanner. 2015. “Deployment of the 30.5 Meter Parachute on the Supersonic Flight Dynamics Test.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2129
• Brandenburg, R. L. 1956. A Deception Repeater for Conical-Scan Automatic Tracking Radars. Defense Technical Information Center. https://doi.org/10.21236/ada459647
• 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
• Brearley, Mn. 1969. “The Hazard of Atmospheric Wind Shears during Parachute Recovery of Instruments.” Australian Journal of Physics 22 (2): 285–88. https://doi.org/10.1071/ph690285
• Breckenridge, W. G., and A. J. Treder. 1977. “In-Flight Gyro Drift Rate Calibration on the Viking Orbiters.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780048018
• Breitner, Michael H., Uwe Rettig, and Oskar von Stryk. 2001. “On Optimal Missile Guidance Upgrades with Dynamic Stackelberg Game Linearizations.” In Advances in Dynamic Games and Applications. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-0155-7_16
• Brennan, W. 1967. “Milestones in Cryogenic Liquid Propellant Rocket Engines.” In 4th Annual Meeting and Technical Display. AIAA 1967-978. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-978
• 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
• Briones, Robert Albert, and Ralph Frederick Wuerker. 1978. Application of Holography to the Combustion Characterization of Solid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ada061058
• 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
• 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, D. 1971. “Store Separation from High Speed Aircraft with Emphasis on Comparisons of Predictions and Flight Test Results.” In 6th Aerodynamics Testing Conference. AIAA 1971-294. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-294
• Brooks, Thurston L., Ilhan Ince, and Greg Lee. 1992. “Operator Vision Aids for Space Teleoperation Assembly and Servicing.” In Fifth Annual Workshop on Space Operations Applications and Research (SOAR 1991). https://ntrs.nasa.gov/citations/19930002793
• Brooks, E., Jr. 1970. “A Method for Predicting the Static Aerodynamic Characteristics of Typical Missile Configurations for Angles of Attack to 180 Degrees.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-981. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-981
• 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
• Broomby, Hayden, and Eduardo Trifoni. 2024. “Design, Manufacturing and Cold Flow Testing of a Liquid Rocket Engine 3D Printed Pintle Injector.” In AIAA SCITECH 2024 Forum. AIAA 2024-1214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1214
• 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, Andrew M. 2022a. “Rocket Engine System Loads.” In Synthesis Lectures on Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-18207-5_5
• Brown, Andrew M. 2022b. “Structural Dynamics Applied to Rocket Engine Turbopumps.” In Synthesis Lectures on Mechanical Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-18207-5_3
• Brown, R., and R. Muzzy. 1969. “Linear and Nonlinear Pressure Coupled Combustion Instability of Solid Propellants.” In 5th Propulsion Joint Specialist. AIAA 1969-479. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-479
• Brown, Kendall K., and Karl W. Nelson. 2005. Technology Challenges for Deep-Throttle Cryogenic Engines for Space Exploration. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20050110123
• Brown, Clinton E., and Hermon M. Parker. 1945. A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-Nose Bodies of Revolution at Supersonic Speeds. NACA-TR-808. NASA. https://ntrs.nasa.gov/citations/19930091887
• 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
• Brown, Clarence A., Jr., and Reginald R. Lundstrom. 1952. Flight Investigation from Mach Number 0.8 to 2.0 to Determine Some Effects of Wing-to-Tail Distance on the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing-Canard Missile. NACA-RM-L52C26. NASA. https://ntrs.nasa.gov/citations/19930087212
• Brownlee, W. 1963. “Experiments on Nonlinear Axial Combustion Instability in Solid Propellant Rocket Motors.” In Summer Meeting. AIAA 1963-228. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-228
• Brownlee, W., and A. Roberts. 1963. “Investigations of Nonlinear Axial Combustion Instability in Solid Propellant Rocket Motors.” In 9th Anglo-American Aeronautical Conference. AIAA 1963-474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-474
• Bruckart, James E. 1993. Analysis of Injury Severity Caused by Flight Motor Overpressure of the Javelin Antiarmor Missile. Defense Technical Information Center. https://doi.org/10.21236/ada270946
• 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
• Bryson, Joshua. 2021. Analysis of Steady-State Aerodynamic Performance and Control-Surface Effectiveness of a High-Speed Projectile. DEVCOM Army Research Laboratory. https://doi.org/10.21236/ad1146662
• Bryson, Joshua. 2022. “Analysis of Steady-State Aerodynamic Performance and Control Surface Effectiveness of a High-Speed Projectile.” In AIAA SCITECH 2022 Forum. AIAA 2022-1794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1794
• 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
• Bucco, Domenic, and Martin Weiss. 2013. “Blind Range Influence on Guidance Loop Performance: An Adjoint-Based Analysis.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4953. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4953
• Bucco, D., P. Zarchan, and M. Weiss. 2012. “On Some Issues Concerning the Adjoint Simulation of Guidance Systems.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4684. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4684
• Budd, Gerald D. 2015. Towed Glider Air-Launch System (TGALS). DFRC-E-DAA-TN25359. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20150015945
• Budd, Gerald D. 2018. System and Method for Air Launch from a Towed Aircraft. Patent Application Number: US-Patent-Appl-SN-15/046,789. NASA. https://ntrs.nasa.gov/citations/20180002683
• Budd, Jerry, and Red Jensen. 2015. “Air Launch to Orbit: Flight Testing the Towed Gilder Air Launch Concept Using a Sub-Scale Research Model.” In AMA Expo 2015. https://ntrs.nasa.gov/citations/20160008708
• Budd, Jerry, and Angie Monheim. 2015. “Towed Glider Air Launch System.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20160008707
• Budd, Gerald D., and Darryl W. Webb. 2016. “Towed Glider Air Launch System.” In SpaceTech Expo 2016. https://ntrs.nasa.gov/citations/20160006964
• Budiyono, Agus, and Harapan Rachman. 2012. “Proportional Guidance and CDM Control Synthesis for a Short-Range Homing Surface-to-Air Missile.” Journal of Aerospace Engineering 25 (2): 168–77. https://doi.org/10.1061/(asce)as.1943-5525.0000104
• 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
• Buford, James A., Jr., and Teri S. Dunavant. 1996. “U.S. Army Missile Command Imaging Infrared System Simulation (IIRSS).” In SPIE Proceedings, vol. 2741, edited by Robert Lee Murrer Jr.. SPIE. https://doi.org/10.1117/12.241130
• Buford, James A., Jr., and Scott B. Mobley. 1994. “U.S. Army Missile Command Hardware-in-the-Loop Infrared Projector Development.” In SPIE Proceedings, vol. 2223, edited by Wendell R. Watkins, Dieter Clement. SPIE. https://doi.org/10.1117/12.177948
• Bui, Trong, David Lux, Michael Stenger, Michael Munson, and George Teate. 2006. “New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-221
• Bujes, J. I. 1962. Detection and Evaluation of Interface Separations in Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0286961
• Bukovska, Diana. 2025. “Research of UAV Guidance Accuracy Using Proportional Navigation Method with Compensation of External Influences through Differential-Game Approach.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/2221-4550-2025-1-072
• Bulbeck, C., J. Morgan, and B. Fairlie. 2000. “RANS Computations of High-Incidence Missile Flow Using Hybrid Meshes.” In 18th Applied Aerodynamics Conference. AIAA 2000-4209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4209
• 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
• Bunn, Fred. 1993. Hit Probability of a High Velocity Tank Round. Defense Technical Information Center. https://doi.org/10.21236/ada262846
• 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
• Burchett, Bradley T., Justin L. Paul, Joseph D. Vasile, and Joshua Bryson. 2022. “A High Fidelity Roll Dependent Aerodynamic Model for a Long Range, High Speed Missile.” In AIAA SCITECH 2022 Forum. AIAA 2022-0420. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0420
• Burke, Kelly A., David J. Wing, and Timothy A. Lewis. 2013. “Pilot Subjective Assessments during an Investigation of Separation Function Allocation Using a Human-In-The-Loop Simulation.” In 2013 Aviation Technology, Integration, and Operations Conference. AIAA 2013-4360. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4360
• Burkhalter, John. 1996. “Grid Fins for Missile Applications in Supersonic Flow.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-194. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-194
• 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
• Burrows, M. L. 2008. Extended Radar Return from a Rocket Engine: A Thermal Model. Defense Technical Information Center. https://doi.org/10.21236/ada492443
• Burstein, S. Z. 1967. Nonlinear Combustion Instability in Liquid-Propellant Rocket Engines. the Transverse Mode. I. the Hydrodynamic Differential and Difference Equations and Computer Algorithm. NASA-CR-88763. NASA. https://ntrs.nasa.gov/citations/19670027953
• Burstein, S. Z., and W. Chinitz. 1967. Nonlinear Combustion Instability in Liquid-Propellant Rocket Motors. NASA-CR-91443. NASA. https://ntrs.nasa.gov/citations/19680003554
• Burstein, S. Z., and W. Chinitz. 1968a. Nonlinear Combustion Instability in Liquid Propellant Rocket Motors. NASA-CR-93674. NASA. https://ntrs.nasa.gov/citations/19680009979
• Burstein, S. Z., and W. Chinitz. 1968b. Nonlinear Combustion Instability in Liquid-Propellant Rocket Motors Quarterly Report. NASA-CR-96014. NASA. https://ntrs.nasa.gov/citations/19680021933
• Burstein, S. Z., W. Chinitz, and H. S. Schechter. 1970. Nonlinear Combustion Instability in Liquid-Propellant Rocket Motors Final Report. NASA-CR-119182. NASA. https://ntrs.nasa.gov/citations/19710020872
• Burstein, S., W. Chinitz, and H. Schechter. 1972. “A Nonlinear Model of Combustion Instability in Liquid Propellant Rocket Engines.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1146
• Burstein, S. Z., and H. S. Schechter. 1970. A Study of High Frequency Nonlinear Combustion Instability in Baffled Annular Liquid Propellant Rocket Motors. Volume 2: A User Manual for Computer Programs TRDL and TRDPLT Final Report, 25 Aug. 1969: 25 Sep. 1970. NASA-CR-115871. NASA. https://ntrs.nasa.gov/citations/19710005155
• Burton, Rodney, Eric Loth, and Michael Selig. 2007. “Supersonic Aircraft for Reusable Rocket Air-Launch (SARRA).” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5841. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5841
• Buschek, Harald. 1998. “Self-Scheduled Missile Autopilot Using Parameter-Varying Robust Control.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4492. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4492
• 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
• Buschek, Harald, and Raimund Dold. 2001. “Flight Test of a Scheduled Mu-Synthesis Autopilot for an Air-to-Air Missile.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4215
• 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, P. S., Jr., and J. R. Busse. 1966. Localized Overheating in Aerobee Regeneratively Cooled Thrust Chambers. NASA-TM-X-55516. NASA. https://ntrs.nasa.gov/citations/19660021049
• 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
• Butler, G., D. King, G. Abate, and M. Stephens. 1991. “Ballistic Range Tests of Store Separation at Supersonic to Hypersonic Speeds.” In 29th Aerospace Sciences Meeting. AIAA 1991-199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-199
• Butlewski, Marcin. 2017. “Taxonomy of Responsibility Allocation in Human-Machine Systems with Different Levels of Automation.” MATEC Web of Conferences 137: 01002. https://doi.org/10.1051/matecconf/201713701002
• Bużantowicz, Witold. 2016. “Computer-Aided Missile Autopilot Analysis and Synthesis.” Mechanik, no. 7: 654–56. https://doi.org/10.17814/mechanik.2016.7.111
• 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
• Bużantowicz, Witold. 2024. “An Airframe Stabilization System with State Observer and Correction Part for Terminal-Phase Missile Guidance.” Advances in Military Technology 19 (1): 91–118. https://doi.org/10.3849/aimt.01858
• Bużantowicz, Witold, and Kamil Klicki. 2026. “Integrated Simulation of Missile Guidance and Energy Effects on Warhead Effectiveness in Air-to-Air Engagements.” Journal of Engineering 2026 (1): e70210. https://doi.org/10.1049/tje2.70210
• Bużantowicz, Witold, Jakub Miernik, and Jan Pietrasieński. 2015. “Fin Actuator Transfer Function of the Anti-Aircraft Missile: Modeling and Approximation.” Mechanik, no. 7: 557/83-557/92. https://doi.org/10.17814/mechanik.2015.7.217
• Bużantowicz, Witold, and Marta Walenczykowska. 2025. “Impact of 3D Model Simplifications on the Determination of Numerical Accuracy of the Radar Cross-Section in Aerial Target Recognition Issues.” IET Radar, Sonar & Navigation 19 (1): e70003. https://doi.org/10.1049/rsn2.70003
• Byaloshitsky, I. E. 2024. “Construction of a Doppler Radar Target Tracking Zone in Conditions of Active Noise Interference.” Radioengineering. https://doi.org/10.18127/j00338486-202410-11
• Byars, D., C. Chang, and C. Woo. 1980. “Extendible Exit Cone Effects on Ballistic Missile Stability.” In 16th Joint Propulsion Conference. AIAA 1980-1302. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1302
• Cabib, Dario, Larry Davidzon, and Amir Gil. 2009. “Controllable Time Dependent and Dual Band Emission Infrared Source to Test Missile Warning Systems In-Flight: System Characterization.” In SPIE Proceedings, vol. 7300, edited by Gerald C. Holst. SPIE. https://doi.org/10.1117/12.818890
• Cabrall, Christopher D. D., Thomas B. Sheridan, Thomas Prevot, Joost C. F. de Winter, and Riender Happee. 2017. “The 4D LINT Model of Function Allocation: Spatial-Temporal Arrangement and Levels of Automation.” In Advances in Intelligent Systems and Computing. Springer International Publishing. https://doi.org/10.1007/978-3-319-73888-8_6
• Cadieux, Francois, Jordan B. Angel, Michael F. Barad, and Cetin C. Kiris. 2023. “Fluid-Structure Interaction Simulations of the ASPIRE SR03 Supersonic Parachute Flight Test.” In AIAA SCITECH 2023 Forum. AIAA 2023-1336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1336
• Cadieux, Francois, and Michael F. Barad. 2024. “Fluid-Structure Interaction Simulations of Supersonic Parachute Inflation: Model Sensitivities.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4225. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4225
• Cadieux, Francois, and Michael F. Barad. 2025. “Wall-Modeled Large-Eddy Simulation of Supersonic Parachute Inflation.” Preprint, . https://doi.org/10.2139/ssrn.5205824
• 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, Fei. 2025. “Bernoulli Filter for Low-Grazing Angle Track-before-Detect with Monopulse Radar.” Progress In Electromagnetics Research C 156: 121–30. https://doi.org/10.2528/pierc25040201
• Cai, Jiaze, Hunter Denton, and Moble Benedict. 2023. “Development of an Air-Launched Tail-Sitter Unmanned Aerial Vehicle.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0079-2023-17962
• Cain, A., R. Epstein, and E. Kerschen. 1999. “Quick Turnaround Prediction of Weapons Bay Cavity Acoustics Resonance.” In 5th AIAA/CEAS Aeroacoustics Conference and Exhibit. AIAA 1999-1899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1899
• Calculating the CEP (Circular Error Probable). 1987. NASA-CR-182996. NASA. https://ntrs.nasa.gov/citations/19890002104
• Caldwell, Barrett S., Megan Nyre-Yu, and Jordan R. Hill. 2019. “Advances in Human-Automation Collaboration, Coordination and Dynamic Function Allocation.” In Advances in Transdisciplinary Engineering. IOS Press. https://doi.org/10.3233/atde190141
• California Univ Regents Berkeley. 2007. Transmission for PATRIOT Missile Test Station. Defense Technical Information Center. https://doi.org/10.21236/ada481830
• Callaway, Lawrence C. 1963. Pacific Missile Range Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ad0405121
• Callen, T. 1979. “Guidance Law Design for Tactical Weapons with Strapdown Seekers.” In Guidance and Control Conference. AIAA 1979-1732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1732
• Callin, Grant D., James V. Devine, and Paul Garcia. 1981. Visual Compensatory Tracking Performance after Exposure to Flashblinding Pulses. I. Comparison of Human and Rhesus Monkey Subjects. Defense Technical Information Center. https://doi.org/10.21236/adb056770
• Callot, S. 1981. “The Use of Simulations for Pre-Flight Predictions in Tactical Missile Development Test Programs.” In 1st Flight Test Conference. AIAA 1981-2361. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2361
• Cameron Reed, B. 2011. “Fission Fizzles: Estimating the Yield of a Predetonated Nuclear Weapon.” American Journal of Physics 79 (7): 769–73. https://doi.org/10.1119/1.3569575
• Campbell, J. E. 1962. Steels for Large Solid-Propellant Rocket-Motor Cases. Defense Technical Information Center. https://doi.org/10.21236/ad0292258
• Campbell, P. 1970. “EOILAC Motor Development for High-Thrust, Short-Action-Time Rocket Propulsion.” In 2nd Sounding Rocket Technology Conference. AIAA 1970-1385. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1385
• Campbell, Matthew. 2024. “A Validation of FlightStream for Store-Separation Modeling.” In 2024 Regional Student Conferences. AIAA 2024-85220. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-85220
• Campbell, John, and Joseph Riccio. 1995. “High Performance Earth Storable Rocket Engine.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2399
• Candler, Graham V. 2001. Simulation of Nonequilibrium Rocket Motor Plumes. Defense Technical Information Center. https://doi.org/10.21236/ada394241
• 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
• Canellas, Marc, and Rachel Haga. 2020. “Toward Meaningful Human Control of Autonomous Weapons Systems through Function Allocation.” Preprint, . https://doi.org/10.31228/osf.io/uvwd9
• Cannizzo, Lou F. 1997. Development of New Energetic Materials for Advanced Solid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ada407949
• Cao, Rui, Chen Lin, Yang Yi, Kelin Lu, Jianzhong Qiao, and Enmei Wang. 2025b. “Research on Hinge Moment Load Reduction of High-Speed Morphing Tail Aircraft Based on Meta-Model.” Preprint, . https://doi.org/10.2139/ssrn.5375639
• Cao, Yuxi, and Jinzhi Wang. 2026. “Distance-Based Cooperative Localization for Target with Constant Velocity.” Preprint, . https://doi.org/10.2139/ssrn.7352636
• Cao, Xuemin, Zhenhai Xu, Xinghua Liu, Luoshengbin Wang, and Wei Dong. 2019. “Four-Channel Monopulse Angle Estimation for Phased Array Radar with Elliptical Plane.” Journal of Engineering 2019 (21): 8116–20. https://doi.org/10.1049/joe.2019.0660
• Cao, DongXing, YiWei Zhou, XinXing Zhou, et al. 2025a. “Comprehensive Modeling and Dynamic Stiffness Analysis of an Electromechanical Fin-Actuator System Considering Multiple Nonlinear Couplings.” Journal of Computational and Nonlinear Dynamics 20 (6): 061003. https://doi.org/10.1115/1.4068265
• Capel-Jorquera, Javier, Leo Miguel González, Eusebio Valero, Luis Torres-Ruiz, Ramón Lacruz-Alcaraz, and Rafael Gómez-Blanco. 2025. “Deployable Fins Effect on Store Separation Dynamics.” Preprint, . https://doi.org/10.2139/ssrn.5634422
• 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
• Cappellucci, D., and R. Schinnerer. 1986. “Missile Launch Windows for Avoiding Collisions with Satellites.” In Astrodynamics Conference. AIAA 1986-2218. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2218
• Capps, F. M. 1957. Survey of Propagation Characteristics of Sea Test Range in Vicinity of the Naval Air Missile Test Center, Point Mugu:: Progress Report No. 5. National Bureau of Standards. https://doi.org/10.6028/nbs.rpt.5508
• 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
• 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
• 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, David, Murray King, and Richard Patterson. 1995. “Integrated Store Separation and Ballistic Accuracy: Applying Enabling Technologies to Improve Aircraft Store Separation.” In 20th Atmospheric Flight Mechanics Conference. AIAA 1995-3431. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3431
• Carmel, M. M., K. R. Czarnecki, and J. R. Sevier Jr. 1958. Effects of Fabrication-Type Roughness on Turbulent Skin Friction at Supersonic Speeds. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19710070007
• Carpenter, R. G., and T. R. Jeffus. 1962. Segmented Rocket Motor Case Program. Defense Technical Information Center. https://doi.org/10.21236/ad0291654
• Carpenter, R. G., and T. R. Jeffus. 1963. Segmented Rocket Motor Case Program. Defense Technical Information Center. https://doi.org/10.21236/ad0296857
• Carr, Ryan W., and Richard Cobb. 2017. “An Energy Based Objective for Solving an Optimal Missile Evasion Problem.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1016. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1016
• Carr, Ryan W., Jason Torf, and Richard Cobb. 2016. “Cooperative Control for Missile Evasion.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-1862. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1862
• “Carriage and Launch Characteristics of the Pegasus Air-Launched Space Booster.” 1994. In 12th Applied Aerodynamics Conference. AIAA 1994-1910. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1910
• Carroll, G., and H. Cox. 1983. “A Missile Flight Control System Using Boundary Layer Thrust Vector Control.” In 19th Joint Propulsion Conference. AIAA 1983-1149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1149
• Carter, Ryan. 2012. “Store Separation Equations of Motion.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4957. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4957
• Carter, Ryan, and Rick Lind. 2012a. “Parametric Modeling for Store Separation Aerodynamics Using System Identification.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4510
• Carter, Ryan, and Rick Lind. 2012b. “Trajectory Optimization for Guided Store Separation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4686. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4686
• Cary, A., Jr., and J. Hefner. 1971. “An Investigation of Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow.” In 4th Fluid and Plasma Dynamics Conference. AIAA 1971-599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-599
• Casasco, Massimo, Gonzalo Saavedra Criado, Sven Weikert, et al. 2013. “Pointing Error Budgeting for High Pointing Accuracy Mission Using the Pointing Error Engineering Tool.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5251
• 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
• Casiano, Matthew, Tim Hinerman, R. Jeremy Kenny, et al. 2013. Status on the Verification of Combustion Stability for the J-2X Engine Thrust Chamber Assembly. M12-2211. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20130014078
• Casiano, Matthew, James Hulka, and Vigor Yang. 2009. “Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5135
• Cass, Elisa. n.d. “Can Situation Awareness Be Predicted?: Investigating Relationships between CogScreen-AE and Pilot Situation Awareness.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2011-08630
• Cassimatis, Nicholas L. 2011. Exploring the Effectiveness of Attention Manipulations on Operator Performance in C2 Task: Computational Modeling Approach. Defense Technical Information Center. https://doi.org/10.21236/ada564118
• Cassimatis, Nicholas L. 2012. Exploring the Effectiveness of Attention Manipulations on Operator Performance in C2 Task: Computational Modeling Approach. Defense Technical Information Center. https://doi.org/10.21236/ada567159
• Cattafesta, L., III, D. Shukla, S. Garg, and J. Ross. 1999. “Development of an Adaptive Weapons-Bay Suppression System.” In 5th AIAA/CEAS Aeroacoustics Conference and Exhibit. AIAA 1999-1901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1901
• Cavallo, Peter, Robert Lee, Ashvin Hosangadi, Timothy Baker, and Richard Kreeger. 1999. “Simulation of Weapons Bay Store Separation Flowfields Using Unstructured Grids.” In 17th Applied Aerodynamics Conference. AIAA 1999-3188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3188
• 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
• Celmins, Ilmars. 2007. Design and Evaluation of an Electromechanical Actuator for Projectile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada473694
• Cenko, A. 1994. “Analytic Investigation of Wind Tunnel Test Anomalies to Determine Flight Test Envelopes for Safe Store Release.” In 25th Plasmadynamics and Lasers Conference. AIAA 1994-2610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2610
• Cenko, Alex. 2009. “Lessons Learned in 30 Years of Store Separation Testing.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-98. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-98
• Cenko, Alexis. 2018. “Mistakes Made in Store Separation Wind Tunnel Testing during the Last 4 Decades.” In 2018 Aerodynamic Measurement Technology and Ground Testing Conference. AIAA 2018-4282. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4282
• Cenko, Alexis. 2025. “80 Years of Mistakes Made in Store Separation.” In AIAA SCITECH 2025 Forum. AIAA 2025-2450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2450
• Cenko, A., and M. Lutton. 2000. “ACFD Applications to Store Separation — Status Report.” Aeronautical Journal 104 (1040): 459–66. https://doi.org/10.1017/s0001924000091958
• Cenko, A., A. Piranian, and M. Talbot. 1995. “Utilizing Wind Tunnel Test Data and Analysis to Determine Flight Test Envelopes for Safe Store Release.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-328. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-328
• 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
• Chadwick, William R. 1995. Augmentation of High-Altitude Maneuver Performance of a Tail-Controlled Missile Using Lateral Thrust,. Defense Technical Information Center. https://doi.org/10.21236/ada328973
• Chadwick, K. M., D. J. Deturris, and J. A. Schetz. 1992. “Direct Measurements of Skin Friction in Supersonic Combustion Flow Fields.” In Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. American Society of Mechanical Engineers. https://doi.org/10.1115/92-gt-320
• Chadwick, K. M., D. J. DeTurris, and J. A. Schetz. 1993. “Direct Measurements of Skin Friction in Supersonic Combustion Flow Fields.” Journal of Engineering for Gas Turbines and Power 115 (3): 507–14. https://doi.org/10.1115/1.2906737
• Chai, Qian Long, Yu Long Bai, and Cun Hui Dong. 2012. “Radar Target Tracking Error Research Using Kalman Filter-Based Algorithms.” Applied Mechanics and Materials 239-240: 1184–87. https://doi.org/10.4028/www.scientific.net/amm.239-240.1184
• Chakoian, George. 1969. A Parachute Retrorocket Recovery System for Airdrop of Heavy Loads. Defense Technical Information Center. https://doi.org/10.21236/ad0699342
• Chakravarthy, Sukumar R., and Kuo-Yen Szema. 1991. Computational Fluid Dynamics Capability for Internally Carried Store Separation. Defense Technical Information Center. https://doi.org/10.21236/ada253671
• Chakravarty, Soumen, and V. Narayanaswamy. 2024. “Investigations of Skin Friction Drag Mitigation over Viscoelastic Surfaces in Supersonic Flows.” Physical Review Fluids 9 (5): 054609. https://doi.org/10.1103/physrevfluids.9.054609
• Chakravarty, Soumen, Dhyanam Patel, and Venkateswaran Narayanaswamy. 2024. “Analysis of Turbulent Skin Friction for Supersonic Flow over Stiff Viscoelastic Coatings.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3884
• 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
• Chan, Y., and Z. Zhu. 1999. “Neural Network Modelling of Aerodynamics and Applications to Store Separation.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-685. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-685
• Chandrasekharan, Reuben M., Nick Iarocci, Sherry Vafa, and Iyad Akel. 2015. “Tailplane with Positive Camber for Reduced Elevator Hinge Moment.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2015-01-2566
• 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
• Chao, Chin, Rich Choi, Scott Cohen, et al. 1993. Design of an Airborne Launch Vehicle for an Air Launched Space Booster. NASA-CR-195534. NASA. https://ntrs.nasa.gov/citations/19940020387
• Chaoqi, Liu, Wen LiHua, He Jiangjun, and Liu Yuxiang. 2018. “Research on Launch Dynamics Modeling and Simulating for Surface-to-Air Missile Supported by Adapter.” MATEC Web of Conferences 175: 03038. https://doi.org/10.1051/matecconf/201817503038
• 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
• Chaplin, Ross, and Trevor Birch. 2012. “The Aero-Acoustic Environment within the Weapons Bay of a Generic UCAV.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3338
• Chapman, Gary. 1998. “A Formal Approach to Aerodynamic Modeling for Store Separation.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-755
• Chappell, Sheryl L., and Kendra L. Dunlap. 2006. “Incorporating Operator Situation Awareness into the Design Process: A Key Ingredient for Future Combat Unmanned Rotorcraft.” In Vertical Flight Society Annual Forum & Technology Display (VFS Forum). https://doi.org/10.4050/vfs-f62-140
• Charczenko, N. 1962. “Parachute Performance at Supersonic Speeds.” In Compilation of Papers Presented to Meeting on Space Vehicle Landing and Recovery Res. and Technol.. https://ntrs.nasa.gov/citations/19730061713
• Charlton, Eric, and Myron Davis. 2008. “Computational Optimization of the F-35 External Fuel Tank for Store Separation.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-376
• Chaudhari, Vedant, Anjali Mistry, Vidhanshu Jadhav, Anudeep Gupta, Devabrata Sahoo, and Dinesh Kumar Bajaj. 2026. “Computational Analysis of Aerodynamic Parameters of a Supersonic Variable Sweep Wing Missile.” In AIP Conference Proceedings, vol. 3369. AIP Publishing. https://doi.org/10.1063/5.0317615
• Chaudhary, Aryan, Bismanjyot Kaur Bindra, Vedansh Singh, Prabhjeet Singh, and Rakesh Kumar. 2025. “Experimental Design, Fabrication and Validation of a Small-Scale Liquid Bi-Propellant Rocket Engine.” In AIAA SCITECH 2025 Forum. AIAA 2025-0128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0128
• Chaudhary, Ajit B., Anil Kumar D. Uttarkar, Prashant Vora, and R. N. Bhattacherjee. 2005. “Post-Flight Analysis and Design Improvement in Command Guidance System for a Short-Range Surface-to-Air Missile System.” Defence Science Journal 55 (3): 293–305. https://doi.org/10.14429/dsj.55.1993
• Chaumette, E., and P. Larzabal. 2007. “Statistical Prediction of Monopulse Angle Measurement.” IET Radar, Sonar & Navigation 1 (5): 377–87. https://doi.org/10.1049/iet-rsn:20060143
• Chawda, Vinay, and Marcia K. O’Malley. 2011. “A Lyapunov Approach for SOSM Based Velocity Estimation and Its Application to Improve Bilateral Teleoperation Performance.” In ASME 2011 Dynamic Systems and Control Conference and Bath/ASME Symposium on Fluid Power and Motion Control, Volume 1. ASMEDC. https://doi.org/10.1115/dscc2011-6181
• Chehroudi, Bruce. 2008. A Unified Approach on Combustion Instability in Cryogenic Liquid Rockets (Preprint). Defense Technical Information Center. https://doi.org/10.21236/ada502420
• Chehroudi, Bruce. 2009. “A Unified Approach on Combustion Instability in Cryogenic Liquid Rocket Engines.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-237. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-237
• Chelaru, Teodor-Viorel I., Cristian Emil Constantinescu, Valentin Pană, and Costin Ene. 2025b. “Stability of Single-Channel Rolling Aerospace Vehicle with Semi-Automatic Command to Line of Sight.” Preprint, . https://doi.org/10.20944/preprints202508.1918.v1
• Chelaru, Teodor-Viorel, Cristian Emil Constantinescu, Valentin Pană, Costin Ene, and Adrian Chelaru. 2024. “Stability of Single Channel Homing Slow-Rolling Missile.” Preprint, . https://doi.org/10.20944/preprints202405.1816.v1
• Chelner, Herbert. 2002. Embedded Sensor Technology for Solid Rocket Motor Health Monitoring. Defense Technical Information Center. https://doi.org/10.21236/ada405070
• Chelner, Herbert. 2003. Embedded Sensor Technology for Solid Rocket Motor Health Monitoring. Defense Technical Information Center. https://doi.org/10.21236/ada412607
• Chen, Mou. 2009. “Design of H∞ Flight Controller for Fighter under Tactical Data-Link Command.” Acta Automatica Sinica 34 (2): 211–14. https://doi.org/10.3724/sp.j.1004.2008.00211
• 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, Jianzhong. 2022. “Research on Abnormal Geometric Similarity Design Method of a Missile with Tail Rudder Model in High Speed Wind Tunnel.” Journal of Physics: Conference Series 2252 (1): 012018. https://doi.org/10.1088/1742-6596/2252/1/012018
• Chen, Dan Qiang, Guo Hua Cao, Hui Lin Fan, Man Yi Hou, and Jing Hua Wang. 2012a. “Hardware Design of Test System for Missile Flight Control System.” Applied Mechanics and Materials 241-244: 9–13. https://doi.org/10.4028/www.scientific.net/amm.241-244.9
• Chen, Dan Qiang, Guo Hua Cao, Hui Lin Fan, Jing Hua Wang, and Duo Qi. 2012b. “Software Design of Test System for Missile Flight Control System.” Applied Mechanics and Materials 241-244: 2764–68. https://doi.org/10.4028/www.scientific.net/amm.241-244.2764
• Chen, B. H., and T. L. Chen. 2020. “Design of Missile Mid-Course Guidance for Constrained Impact Angle.” Journal of Physics: Conference Series 1509 (1): 012007. https://doi.org/10.1088/1742-6596/1509/1/012007
• Chen, Yidan, and Tao Cui. 2025. “Novel Control of Supersonic Combustion Instability via Weakly Coupled Identical Oscillators Induced by Multi-Injector Design.” Preprint, . https://doi.org/10.2139/ssrn.5233853
• Chen, L. Y., Geoffrey Delooze, David Ritchie, and Daniel East. 2025b. Multi-Material Laser Powder Bed Fusion of Liquid Rocket Nozzle with Regenerative Cooling Channel Wall. https://doi.org/10.52202/083088-0064
• Chen, Yongchao, Xinbao Gao, Min Gao, and Dan Fang. 2018b. “An Optimal Missile Autopilot Design Model.” International Journal of Enterprise Information Systems 14 (1): 104–10. https://doi.org/10.4018/ijeis.2018010106
• Chen, Ye, Zhengyu Guo, and Yunze Cai. 2021f. “Time and Angle Constraint Guidance Law Applicable to Maneuvering Target.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_15
• Chen, Jessie Y., Ellen C. Haas, Krishna Pillalamarri, and Catherine N. Jacobson. 2006b. Human-Robot Interface: Issues in Operator Performance, Interface Design, and Technologies. Defense Technical Information Center. https://doi.org/10.21236/ada451379
• Chen, Weiyi, Fan He, and Haidi Dong. 2023e. “Optimal Predictive Guidance Law Based on Guidance Law Identification Using Variable Structure Interactive Multiple Guidance Law Model.” AIP Advances 13 (5): 055104. https://doi.org/10.1063/5.0149905
• Chen, Guoying, and Peikang Huang. 1996a. “New Model of Radar Target Glint Based on Filtered Discrete Differenced Gaussian Noise.” In SPIE Proceedings, vol. 2845, edited by William J. Miceli. SPIE. https://doi.org/10.1117/12.257238
• Chen, Guoying, and Peikang Huang. 1996b. “Wavelet Method to Suppress Angle Measurement Error in Monopulse Tracking Radar.” In SPIE Proceedings, vol. 2739, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.241937
• Chen, Guoying, and Peikang Huang. 1999. “Suppress the Radar Target Glint by an L-Filter Preprocessor.” In SPIE Proceedings, vol. 3692, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.352881
• Chen, Wei, Fancheng Kong, Di Zhang, and Zhenzhou Bai. 2017c. “Research on Target Matching of Television Guided Missile Seeker.” In Proceedings of the 2017 International Conference on Electronic Industry and Automation (EIA 2017). Atlantis Press. https://doi.org/10.2991/eia-17.2017.68
• Chen, Y.-H., and Y.-T. Lian. 1995. “2-D Multitarget Angle Tracking Algorithm Using Sensor Array.” IEE Proceedings - Radar, Sonar and Navigation 142 (4): 158–61. https://doi.org/10.1049/ip-rsn:19951984
• Chen, Zhang, Bin Liang, Tao Zhang, Xueqian Wang, and Bo Zhang. 2014a. “Adaptive Bilateral Control for Nonlinear Uncertain Teleoperation with Guaranteed Transient Performance.” Robotica 34 (10): 2205–22. https://doi.org/10.1017/s0263574714002847
• Chen, Jian Zhong, and Pei Qing Liu. 2014. “Test Technique Research for the Hinge Moment of a Grid Fin in High Speed Wind Tunnel.” Applied Mechanics and Materials 574: 480–84. https://doi.org/10.4028/www.scientific.net/amm.574.480
• Chen, Qiding, Yanwei Luo, and Yan Wang. 2025c. “Research on Line-of-Sight Angular Rate Extraction Method for Strapdown Seeker Based on AUKF.” Journal of Physics: Conference Series 3026 (1): 012060. https://doi.org/10.1088/1742-6596/3026/1/012060
• Chen, Y. S., H. M. Shang, Paul Liaw, and J. Hutt. 1993. “Liquid Propellant Rocket Engine Combustion Simulation with a Time-Accurate CFD Method.” In Eleventh Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion. https://ntrs.nasa.gov/citations/19950017025
• Chen, Jinli, Yang Song, Hua Shao, and Jiaqiang Li. 2025d. “Robust Angle Estimation in MIMO Radar under Impulsive Noise via Fast Bayesian Tensor Decomposition with Intra-Dimension Correlation​.” Preprint, . https://doi.org/10.2139/ssrn.5734123
• Chen, Robert, Jason Speyer, and Dimitrios Lianos. 2006a. “Homing Missile Guidance and Estimation under Agile Target Acceleration.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6701
• Chen, Robert, Jason Speyer, and Dimitrios Lianos. 2007a. “Game-Theoretic Homing Missile Guidance with Autopilot Lag.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6535. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6535
• Chen, Robert, Jason Speyer, and Dimitrios Lianos. 2008a. “Homing Missile Guidance and Estimation for Three-Dimensional Intercept.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7457
• Chen, Robert, Jason Speyer, and Dimitrios Lianos. 2010b. “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, Nanqian, Li Su, and Xiaoshen Yu. 1991. “Some Separation Characteristics on the Ogive Nosed Slender Body in Supersonic Flows.” In 9th Applied Aerodynamics Conference. AIAA 1991-3258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3258
• Chen, P. C., E. Sulaeman, and D. D. Liu. 2002. A Comprehensive Rapid-Assessment-Of-Flutter/Ejection-Loads (RAFEL) Software System for Aircraft/Store Compatibility. Defense Technical Information Center. https://doi.org/10.21236/ada399365
• Chen, Si, Zonghua Sun, and Liaoni Wu. 2023d. “On Predictor-Corrector Guidance of Hypersonic Vehicle in Glide Segment.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_84
• Chen, Yuhao, Bo Tang, Da Li, Yangjia Wang, and Wenjun Wu. 2026e. “Spectrally Compatible Deceptive Jamming Waveform Design for Synthetic Aperture Radar Countermeasures.” IET Radar, Sonar & Navigation 20 (1): e70110. https://doi.org/10.1049/rsn2.70110
• Chen, Jian, Yuan Tian, Hugh Ht Liu, and Zhang Ren. 2010a. “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, Jun, Fei Wang, Jianjiang Zhou, and Chenguang Shi. 2019. “Information Divergence-Based Low Probability of Intercept Waveform Detection for Multi-Antenna Intercept Receivers.” Journal of Engineering 2019 (20): 7034–38. https://doi.org/10.1049/joe.2019.0589
• Chen, Hsin-Yuan, and Ciann-Dong Yang. 1998. “Nonlinear H-Infinity Robust Guidance Law for Homing Missiles.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4212
• Chen, Hsin-Yuan, and Chi-Ching Yang. 2001. “Nonlinear H2/H-Infinity Guidance Design for Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4346
• Chen, Ming-Ghow, and Pin-Jar Yuan. 1996. “Optimal Guidance of Proportional Navigation.” In Guidance, Navigation, and Control Conference. AIAA 1996-3840. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3840
• Chen, Qian, and Wentao Zhao. 2005. “Studies of Parallel Algorithm in Liquid Rocket Engine Combustion Instability.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-3741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-3741
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020c. “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. 2020d. “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. 2020e. “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. 2020f. “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. 2020g. “Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-To-Drag Ratio Reentry Vehicle.” In Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0_10
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2020i. “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 Guoying and Huang Peikang. n.d. “Monopulse Radar Angle Measurement Error Reduction Based on Wavelet Multiresolution Analysis.” In Proceedings of International Radar Conference. Publishing House of Electron. Ind. https://doi.org/10.1109/icr.1996.574593
• Cheng, S. I. 1985. “L*-Combustion Instability in Solid Propellant Rocket Combustion.” In Recent Advances in the Aerospace Sciences. Springer US. https://doi.org/10.1007/978-1-4684-4298-4_13
• Cheng, G., and R. Farmer. 2002. “CFD Spray Combustion Model for Liquid Rocket Engine Injector Analyses.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-785. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-785
• Cheng, Haibin, and Hao Lu. 2023. “Research on Air-to-Air Missile Cooperative Navigation Technology Based on GNSS.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_18
• Cheng, Nuo, Bo Shen, Wei Li, Pinghui Jia, and Liangbo Zhao. 2025. “A Parameter Optimization Method for Non-Singular Terminal Sliding Mode Guidance Law with Falling Angle Constraint.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2204-7_22
• Cheng, Xiaohui, Haiqing Si, Yao Li, and Peihong Zhang. 2023. “Numerical Simulation about the Characteristics of the Store Released from the Internal Bay in Supersonic Flow.” Computer Modeling in Engineering & Sciences 136 (2): 1729–42. https://doi.org/10.32604/cmes.2023.022694
• 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, Chi-Hao, and James Tsui. 2022. “Missile Detection Schemes and Defense.” In An Introduction to Electronic Warfare; from the First Jamming to Machine Learning Techniques. River Publishers. https://doi.org/10.1201/9781003337171-6
• Cheng, Peng, Jiping Wu, Qinglian Li, and Zhongtao Kang. 2017b. “Dynamic Response of a Dual-Manifold Injector Rocket Engine for RBCC to Deep Throttling.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2286
• Chepurnov, Il’ya Aleksandrovich. 2023. “Professiographic Study of the Professional Activities of Operators Anti-Aircraft Missile Systems.” Психология и Психотехника, no. 3: 97–107. https://doi.org/10.7256/2454-0722.2023.3.43982
• Chepurnov, Ilya, and Vladimir Prokhorenko. 2024. “Simulation Modelling of a Radar Semi-Active Homing System for a Guided Missile at an Air Target.” Ergodesign 2024 (2): 173–79. https://doi.org/10.30987/2658-4026-2024-2-173-179
• Cherniavskyi, Oleksandr. 2026. “Specific Aspects of Mathematical Modeling of Filling of Branched Feedlines within a Reconfigurable Feed System during Liquid-Propellant Rocket Engine Start-up.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/3083-7057-2026-1-035
• Chernikoff, Rube, and Franklin V. Taylor. 1957. “Effects of Course Frequency and Aided Time Constant on Pursuit and Compensatory Tracking.” Journal of Experimental Psychology 53 (5): 285–92. https://doi.org/10.1037/h0045252
• Chevalier, OPHÉLIE, Mathilda Liennard, ANDRÉ Langlet, Yann Guilmard, Marcel Mansion, and Patrice Bailly. 2017. “Dynamic of Tubes Crossed by High Speed Projectiles, Influence of Tube and Weapon Geometry on Accuracy and Dispersion.” In 30th International Symposium on Ballistics. DEStech Publications, Inc. https://doi.org/10.12783/ballistics2017/16880
• Chew, Thomas J. 1973. Hydraulic Flip Behavior in Typical Liquid Rocket Operating Regimes. Defense Technical Information Center. https://doi.org/10.21236/ad0764730
• Chhavi, Chhavi, and Vikram Ramanan. 2023. “Modeling and Theoretical Design of Missile Launch System Utilizing Electromagnetism.” In AIAA AVIATION 2023 Forum. AIAA 2023-4125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4125
• Chien, K.-Y. 1974. “Hypersonic, Turbulent, Cold-Wall, Skin-Friction and Heat-Transfer Measurements on an Axisymmetric Sharp Cone.” In 12th Aerospace Sciences Meeting. AIAA 1974-97. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-97
• 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
• Ching-Fang Lin, J. R. Cloutier, and J. H. Evers. 1995. “Robust Bank-to-Turn Missile Autopilot Design.” In Proceedings of 1995 American Control Conference - ACC’95, vol. 3. American Autom Control Council. https://doi.org/10.1109/acc.1995.531226
• Chiou, Ying-Chwan, Chen-Yuan Kuo, Ying-Chwan Chiou, and Chen-Yuan Kuo. 1997. “Qualitative Analysis of Missile Guidance Problem.” In Guidance, Navigation, and Control Conference. AIAA 1997-3689. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3689
• Chireau, Roland F. 1966. Silver-Zinc Missile Power Supply. Defense Technical Information Center. https://doi.org/10.21236/ad0488983
• Chiu, H. 1986. “Theory of Bipropellant Combustion. II: Conjugate, Normal and Composite Combustion in Liquid Rocket Combustion Chamber.” In 24th Aerospace Sciences Meeting. AIAA 1986-221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-221
• Chiu, H. 1987. “A New Design Approach of a Compact High Performance Bipropellant Liquid Rocket Engine Combustors.” In 23rd Joint Propulsion Conference. AIAA 1987-2033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2033
• Cho, Dongsoo, Seonhyeok Kang, H. Jin Kim, and Min-Jae Tahk. 2011. “Adaptive Dynamic Surface Control Based on Neural Network for Missile Autopilot.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6251
• Cho, Byung-Lae, Jung-Soo Lee, Jongmin Lee, and Sun-Gu Sun. 2012. “Accuracy Improvement of the Estimated Angle Using Phase Averaging in Phase-Comparison Monopulse Algorithm.” Journal of Korean Institute of Electromagnetic Engineering and Science 23 (10): 1212–15. https://doi.org/10.5515/kjkiees.2012.23.10.1212
• 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
• Chong, Edwin, and Louis L. Scharf. 2006. Integrated Radar Imaging, Target Tracking and Sensor Scheduling. Defense Technical Information Center. https://doi.org/10.21236/ada448056
• Chornyi, Oleksii, Valerii Tytiuk, Victor Busher, Volodymyr Grabko, and Oleksandr Bratko. 2024. “Compensating Delay and Time Constants in Human Operator Motor Dynamics.” Electromechanical and energy saving systems 67 (4): 8–16. https://doi.org/10.32782/2072-2052.2024.4.67.1
• Chou, David C., and Theodore F. Smith. 1974. Aerodynamic Heating of Supersonic Blunt Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada001135
• Chow, Winston C. 1996. Analysis of the Probability Density Function of the Monopulse Ratio Radar Signal. Defense Technical Information Center. https://doi.org/10.21236/ada315600
• Chow, R., and F. Marconi. 1989. “A Navier-Stokes Solution to Hypersonic Store Separation Flow Fields.” In 27th Aerospace Sciences Meeting. AIAA 1989-31. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-31
• Christensen, James C., and Justin R. Estepp. 2013. Co-Adaptive Aiding and Automation Enhance Operator Performance. Defense Technical Information Center. https://doi.org/10.21236/ada586165
• Christensen, Julian M., Charles E. Hutchinson, and Frederick A. Muckler. 1981. The Human Operator in Advanced Aerospace Systems. Defense Technical Information Center. https://doi.org/10.21236/ada216046
• Chrysler Corp Detroit Mi Missile Div. 1963. Product Assurance Program Technical Report for the Radar Cross-Section Reduction of Re-Entry Vehicles. Defense Technical Information Center. https://doi.org/10.21236/ad0402807
• Chu, Min, and Xu Xu. 2014. “Time-Domain Numerical Simulation of High Frequency Combustion Instability in Liquid Propellant Rocket Engines.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3416
• Chubb, R. S. 1952. Experimental Investigation of the Stability, Control, and Induced Rolling Moments of a Canard Missile Airframe at a Mach Number of 1.7. NACA-RM-A52G29. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19710065199
• Chudej, Kurt. 1993. “Optimal Ascent of a Hypersonic Space Vehicle.” In Optimal Control. Birkhäuser Basel. https://doi.org/10.1007/978-3-0348-7539-4_23
• 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
• Chusilp, Pawat, Weerawut Charubhun, and Pattadon Koanantachai. 2014b. “Monte Carlo Simulations of Weapon Effectiveness Using Pk Matrix and Carleton Damage Function.” International Journal of Applied Physics and Mathematics 4 (4): 280–85. https://doi.org/10.7763/ijapm.2014.v4.299
• Cicolani, Luigi S. 1961. Trajectory Control in Rendezvous Problems Using Proportional Navigation. NASA-TN-D-772. NASA. https://ntrs.nasa.gov/citations/20040005909
• Cieśliński, Dawid, Michał Ranachowski, Krystian Kutnik, et al. 2024. On Development of Green Storable Liquid Rocket Engine with Thrust Variation. https://doi.org/10.52202/078371-0009
• Circular Normal Distribution. 2014. Wiley. https://doi.org/10.1002/9781118445112.stat00937
• Circular Probable Error. 2014. Wiley. https://doi.org/10.1002/9781118445112.stat00938
• Clark, D. 1967. “Activation and Initial Test Operations of Large Rocket Engine: Thrust Chamber Test Facilities.” In 3rd Propulsion Joint Specialist Conference. AIAA 1967-455. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-455
• Clark, Rodney L. 1975. Weapons Bay Turbulence Reduction Techniques. Defense Technical Information Center. https://doi.org/10.21236/ada334771
• 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
• Clark, Ian G., John C. Gallon, and Allen Witkowski. 2015a. “Parachute Decelerator System Performance during the Low Density Supersonic Decelerator Program’s First Supersonic Flight Dynamics Test.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2130. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2130
• Clark, Matthew, Zachary Kern, and Richard J. Prazenica. 2015b. “A Vision-Based Proportional Navigation Guidance Law for UAS Sense and Avoid.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0074. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0074
• Clark, S., and F. McLamb. 1983. “Eastern Space and Missile Center Capability.” In 2nd Flight Testing Conference. AIAA 1983-2710. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2710
• Clark, W., J. Peoples, and M. Briggs. 1972. “Occurrence and Inhibition of Large Yawing Moments during High-Incidence Flight of Slender Missile Configurations.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-968
• Clark, Matthew, and Richard J. Prazenica. 2017. “Proportional Navigation Based Guidance Laws for UAV Obstacle Avoidance in Complex Urban Environments.” In AIAA Information Systems-AIAA Infotech @ Aerospace. AIAA 2017-0672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0672
• Clark, Ian G., John W. Van Norman, Joseph M. Brock, and Clara”, ‘Muppidi, Suman “O’Farrell. 2017. Development of Models for Disk-Gap-Band Parachutes Deployed Supersonically in the Wake of a Slender Body. Jet Propulsion Laboratory. https://ntrs.nasa.gov/citations/20210007715
• Clark, E., Jr., and A. Hodapp Jr. 1970. “An Improved Technique for Determining Missile Roll Rate with the Epicyclic Theory.” In Propulsion and ASW Meeting. AIAA 1970-536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-536
• Clarke, J. F., and Y. L. Sinai. 1977. “The Wave System Attached to a Slender Body in a Supersonic Relaxing Gas Stream. Basic Results: The Cone.” Journal of Fluid Mechanics 79 (3): 499–524. https://doi.org/10.1017/s0022112077000299
• Clayton, B., and W. Posingies. 1965. “The Development and Flight Test of a Pure Fluid Missile Control System.” In Guidance Control Conference. AIAA 1965-1221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-1221
• Clemente, John A. 1958. “A Design and Operational Philosophy for an Ultra-Precision Tracking Mount System for a Missile Test Range.” Journal of the SMPTE 67 (4): 242–45. https://doi.org/10.5594/j11146
• 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
• Cliff, Eugene, and Henry Kelley. 1989. “3-D Air-to-Air Missile Trajectory Shaping Study.” In Guidance, Navigation and Control Conference. AIAA 1989-3637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3637
• Cloutier, James, and Donald Stansbery. 1999. “All-Aspect Acceleration-Limited Homing Guidance.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4063. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4063
• Coate, W. G. 2004. Preliminary Design Review: Kinematic Tracking for the PCA Integrated Radar-Tracker Application. Defense Technical Information Center. https://doi.org/10.21236/ada419855
• Coate, W., and M. Arakawa. 2004. Preliminary Design Review: Feature-Aided Tracking for the PCA Integrated Radar-Tracker Applications. Defense Technical Information Center. https://doi.org/10.21236/ada427295
• Cobb, H. M. 1949. “Motion Pictures in the Guided-Missile Program.” Journal of the Society of Motion Picture Engineers 53 (5): 431–39. https://doi.org/10.5594/j11685
• Coelho, André Fialho. 2023. “Whole-Body Control and Teleoperation of a Suspended Aerial Manipulator.” PhD diss.. https://doi.org/10.3990/1.9789036559584
• 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, Herbert E. 1981. Proceedings of the Meeting of the Coordinating Group on Modern Control Theory (3rd) (20-21 October 1981) US Army Missile Command, Redstone Arsenal, AL. Part I. Defense Technical Information Center. https://doi.org/10.21236/ada109124
• 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
• Colburn, Bruce K. 1978. Investigation of MRAS Identification Techniques for the Human Operator Problem. Defense Technical Information Center. https://doi.org/10.21236/ada069951
• Cole, John S., Jr. 1996. “Hardware-in-the-Loop Simulation at the U.S. Army Missile Command.” In Proceedings of SPIE, vol. 2741. SPIE. https://doi.org/10.1117/12.241103
• 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
• Coleburn, N. L., and B. E. Drimmer. 1961. The Thermal Behavior of Explosives Subjected to Simulated Aerodynamic Heating, III. Defense Technical Information Center. https://doi.org/10.21236/ad0326783
• Coleburn, N. L., and B. E. Drimmer. 1962. The Thermal Behavior of Explosives Subjected to Simulated Aerodynamic Heating, II: Datb. Defense Technical Information Center. https://doi.org/10.21236/ad0329109
• Coleman, Daniel K., Marcus Lobbia, and Jerry Rowan. 2026. “A New Methodology for Stress Analysis of Supersonic Parachute Inflation.” In 28th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2026-3855. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-3855
• Coletta, Fernando G., Leon H. Miller, Sumner John H., and N. Ray Jr. 1964. A Method for Evaluating Materiel Readiness of Surface-to-Air Missile Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0452678
• Coley, Christopher. 2024. “Artificial Neural Network Surrogate Modeling for Cavity-Released Store Separation Trajectory Prediction.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4616. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4616
• Coley, Christopher, and Andrew Lofthouse. 2012. “Correlation of Weapon Bay Resonance and Store Unsteady Force and Moment Loading.” In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2012-415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-415
• Colson, K. K., and C. T. Thomas. 1977. Fabrication and Test of Volume Scan Transmitter/Receiver Module Brassboard, an Integral Part of the Missile Attitude Measurement System. Defense Technical Information Center. https://doi.org/10.21236/adb019882
• Combs, L. 1970. “Comprehensive Analysis of Liquid Rocket Combustion.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-622. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-622
• Combs, L. P., and F. W. Hoehn. 1964. Steady-State Rocket Combustion of Gaseous Hydrogen and Liquid Oxygen. Part i. Experimental Investigation. Defense Technical Information Center. https://doi.org/10.21236/ad0615798
• Combs, L. P., and M. D. Schuman. 1965. Steady-State Rocket Combustion of Gaseous Hydrogen and Liquid Oxygen. Part 2: Analysis for Coaxial Jet Injection. Defense Technical Information Center. https://doi.org/10.21236/ad0623401
• “Combustion Instability and Transient Behavior in Hybrid Rocket Motors.” 2007. In Fundamentals of Hybrid Rocket Combustion and Propulsion. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866876.0351.0412
• “Combustion Instability in Solid Rockets Using Propellants with Reactive Additives.” 1960. In Solid Propellant Rocket Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864766.0393.0422
• Compressible Turbulent Boundary Layers. 1969. NASA-SP-216. NASA. https://ntrs.nasa.gov/citations/19700001122
• Concept Analysis Corp Plymouth Mi. 1989. Missile Geometry Package. Defense Technical Information Center. https://doi.org/10.21236/ada253181
• 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
• Coogan, Shane B., and Grant O. Musgrove. 2017. “Preliminary Analysis Method for Large Amplitude Liquid Slosh in Air-Launched Space Launch Vehicles.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-5006. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-5006
• Cook, C. 1999. “Investigating Methods of Dynamic Function Allocation for Naval Command and Control.” In International Conference on People in Control (Human Interfaces in Control Rooms, Cockpits and Command Centres), vol. 1999. IEE. https://doi.org/10.1049/cp:19990221
• Cook, C. 2000. “Function Allocation: Optimising the Automation Boundary.” In IEE One Day Seminar on Systems Dependency on Humans, vol. 2000. IEE. https://doi.org/10.1049/ic:20000101
• 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, R. T., and R. J. Quentmeyer. 1980. “Advanced Cooling Techniques for High-Pressure, Hydrocarbon-Fueled Rocket Engines.” In Joint Propulsion Conference. https://ntrs.nasa.gov/citations/19800054824
• 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, D. W., and R. James. 1979. Shuttle Orbiter Radar Cross-Sectional Analysis. NASA-TM-72870. NASA. https://ntrs.nasa.gov/citations/19800002036
• Corbridge, Colin, and Catherine A. Cook. 1999. “Future Challenges for Function Allocation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 43 (19): 1027–31. https://doi.org/10.1177/154193129904301903
• Corda, Stephen, Curt Longo, and Zachary Krevor. 2018. “Stratolaunch Air-Launched Hypersonic Testbed.” In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2018-5257. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-5257
• Corker, K., and A. K. Bejczy. 1984. “The Effect of Part-Simulation of Weightlessness on Human Control of Bilateral Teleoperation: Neuromotor Considerations.” In NASA. Ames Research Center 20th Ann. Conf. on Manual Control, Vol. 1. https://ntrs.nasa.gov/citations/19850006201
• Cormack, D. R., M. Henderson, and D. E. Clark. 2017. “An Investigation of an Alternative Coordinate Space Parameterisation for Radar Target Tracking.” In International Conference on Radar Systems (Radar 2017). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2017.0465
• Corriveau, Daniel, Nicolas Hamel, and Franklin Wong. 2006. “Side Force Generation Mechanism for a Missile with Nose-Mounted Micro-Structures.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3000
• Cosens, Doug, and Ron Newton. 1988. “Expendable Liquid Rocket Engine Status Monitoring Experience: Titanbooster Engine.” In 24th Joint Propulsion Conference. AIAA 1988-3309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-3309
• Cotting, M. Christopher, and Timothy H. Cox. 2005. A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. AIAA Paper 2005-0032. NASA Dryden Flight Research Center. https://ntrs.nasa.gov/citations/20050029394
• 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
• Cougherty, F. C., J. A. Benek, and J. L. Steger. 1985. On Applications of Chimera Grid Schemes to Store Separation. NASA-TM-88193. NASA. https://ntrs.nasa.gov/citations/19860003824
• Coulbert, Clifford. 1963. “Selecting a Thrust Chamber Cooling Technique for Spacecraft Rocket Engines.” In Summer Meeting. AIAA 1963-241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-241
• Coulter, George A. 1982. Blast Wave Loading of a Two-Dimensional Circular Cylinder. Defense Technical Information Center. https://doi.org/10.21236/ada121600
• Cox, E., and G. E. Turney. 1967. Cooldown Characteristics of Regenerative Nozzle Used in Full-Scale, Cold-Flow, Nuclear Rocket Test Facility. NASA-TN-D-3931. NASA. https://ntrs.nasa.gov/citations/19670015289
• Crabtree, D. L. 1962. Investigation of a Gas-Driven Jet Pump for Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ad0273836
• Crachi, Matteo, Marco Pizzarelli, Raffaella Sesana, and Cristiana Delprete. 2024. Life Evaluation of Liquid Rocket Engine Regenerative Cooling System: A Comparison of Hardening Models. https://doi.org/10.52202/078371-0147
• Craig, R., and R. Reich. 1981. “Flight Test Aerodynamic Drag Characteristics Development and Assessment of in-Flight Propulsion Analysis Methods for the AGM-109 Cruise Missile.” In 1st Flight Test Conference. AIAA 1981-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2423
• 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
• Craley, Jason, and Kenneth Desabrais. 2007. “An Investigation of Pilot Parachute Deployment Hesitation.” In 19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2007-2575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2575
• Cramer, W. E. 1979. Nomograms for Overpressure, Fireball Radius and Thermal Energy of Nuclear Weapons. Defense Technical Information Center. https://doi.org/10.21236/ada076489
• Cramer, Evin J., Jerre E. Bradt, and John W. Hardtla. 1990. Ascent Guidance Algorithm Using Lidar Wind Measurements. Boeing Co. https://ntrs.nasa.gov/citations/19910045426
• 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
• Crawford, R. A., P. J. Hand, and H. H. Horiuchi. 1972. Electronic Integrator for Gyro Rate Output Voltages. NPO-11499. NASA. https://ntrs.nasa.gov/citations/19720000554
• Creaser, P., B. Stacey, and B. White. 1998. “Fuzzy Missile Guidance Laws.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4306
• Crone, Chet, Carl Stechman, and Pete Woll. 1993. “Combustion Instability in Small Earth Storable Bipropellant Rocket Engines.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1960
• “Cruise Missiles.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_7
• Cuffe, J., and C. Limerick. 1983. “Propulsion for an Air Launched Space Sortie System.” In 19th Joint Propulsion Conference. AIAA 1983-1188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1188
• Cui, Yan Kai, Fu Li, Xiao Geng Liang, and Ling Luo. 2010. “Optimal Sliding-Mode Terminal Guidance Law Design of Airborne Boost-Phase Ballistic Missile Interception.” Applied Mechanics and Materials 40-41: 15–20. https://doi.org/10.4028/www.scientific.net/amm.40-41.15
• Cui, Ming, Zhiyong Wu, and Yonggang Cao. 2015. “Design of Image Tracking System for Strapdown Seeker Based on FPGA+DSP.” In Proceedings of the 5th International Conference on Advanced Design and Manufacturing Engineering. Atlantis Press. https://doi.org/10.2991/icadme-15.2015.108
• Cui, Lei, Kang Zhang, Xijing Hu, Zhe Li, Jianying Yang, and Nan Jin. 2023. “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
• Cuk, Danilo, Mostafa Abobaker, and Slobodan Mandic. 2012. “A New Guidance Law for a Tactical Surface-to-Surface Missile.” Vojnotehnicki glasnik 60 (1): 115–35. https://doi.org/10.5937/vojtehg1201115c
• Culick, F. 1971. “Research on Combustion Instability and Application to Solid Propellant Rocket Motors.” In 7th Propulsion Joint Specialist Conference. AIAA 1971-753. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-753
• Culick, F. 1972. “Research on Combustion Instability and Application to Solid Propellant Rocket Motors. II.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1049. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1049
• 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
• Culpepper, Gideon A. 1978. Statistical Analysis of Radial Error in Two Dimensions. Defense Technical Information Center. https://doi.org/10.21236/ada059117
• Cunningham, R. S. 1963. Ground Test Missile Requirements. Defense Technical Information Center. https://doi.org/10.21236/ad0401413
• Curfman, Howard J., Jr., and Carl E. Grigsby. 1952. Longitudinal Stability and Control Characteristics of a Canard Missile Configuration for Mach Numbers from 1.1 to 1.93 as Determined from Free-Flight and Wind-Tunnel Investigation. NACA-RM-L52F06. NASA. https://ntrs.nasa.gov/citations/19930087105
• Cutting, E., and C. R. Gates. 1963. Midcourse Guidance Using Radio Techniques. NASA. https://ntrs.nasa.gov/citations/19630027368
• Czarnecki, K. R., Mary W. Jackson, and William J. Monta. 1965. Turbulent Skin Friction at High Reynolds Numbers and Low Supersonic Velocities. NASA-TN-D-2687. NASA. https://ntrs.nasa.gov/citations/19650009005
• 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
• Dahal, Nimesh, Katsuyoshi Fukiba, Yusuke Itou, Kazuki Mizuta, and Yusuke Maru. 2018a. “Pressure Mode Classification of the Supersonic Flow over a Rigid Parachute Model with Suspension Lines.” In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 2018-5324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-5324
• Dahal, Nimesh, Katsuyoshi Fukiba, Kazuki Mizuta, and Yusuke Maru. 2018b. “Study of Pressure Oscillations in Supersonic Parachute.” International Journal of Aeronautical and Space Sciences 19 (1): 24–31. https://doi.org/10.1007/s42405-018-0025-3
• Dai, Encheng, Guangbin Cai, Yonghua Fan, Hui Xu, Hao Wei, and Yunfei Sun. 2026. “Physics-Informed Neural Predictor-Corrector Guidance for Time-Coordinated Reentry of Hypersonic Glide Vehicles.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9996711/v1
• Dai, Xiaowen, and Asok Ray. 1996. “Damage-Mitigating Control of a Reusable Rocket Engine: Part I—Life Prediction of the Main Thrust Chamber Wall.” Journal of Dynamic Systems, Measurement, and Control 118 (3): 401–8. https://doi.org/10.1115/1.2801159
• Dai, Jing, Ping Zhang, Xingshan Li, Canxing Liao, and Zongli Wang. 2006. “Software Design of Missile Integrated Test System.” In SPIE Proceedings, vol. 6358, edited by Jiancheng Fang, Zhongyu Wang. SPIE. https://doi.org/10.1117/12.718066
• Dalle, Derek, Scott Frendreis, James Driscoll, and Carlos Cesnik. 2010. “Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamic and Reduced-Order Propulsive Models.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7930. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7930
• Dalle, Derek, Sean Torrez, and James Driscoll. 2011. “Turn Performance of an Air-Breathing Hypersonic Vehicle.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6300. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6300
• 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
• Dana, Roger A. 2022. “Fidelity and Accuracy of Monopulse Measurement Simulation.” In Monopulse Measurement with Active Electronically Scanned Arrays (AESAs). Springer International Publishing. https://doi.org/10.1007/978-3-030-91908-5_10
• Danchick, Roy. 2016. “Connecting Gravity Turn Guidance Dynamics to near Planar Missile Motion Geometry.” IET Radar, Sonar & Navigation 10 (2): 278–84. https://doi.org/10.1049/iet-rsn.2015.0165
• Dang, Son Tung, Hai Anh Nguyen, Hai Duong Nguyen, and Tran Thi Minh Kieu. 2023. “The Mathematical Framework for Simulating an Air-To-Air Missile Operation on Fighter Aircraft.” International Journal of Computational Methods and Experimental Measurements 11 (2): 97–104. https://doi.org/10.18280/ijcmem.110204
• 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
• Daniels, H. E. 1952. “The Covering Circle of a Sample from a Circular Normal Distribution.” Biometrika 39 (1/2): 137. https://doi.org/10.2307/2332472
• Daniels, Peter, and Samuel R. Hardy. 1975. Roll-Rate Stabilization of a Missile Configuration with Wrap-Around Fins in Incompressible Flow. Defense Technical Information Center. https://doi.org/10.21236/ada019928
• Daniels, Peter, and Samuel R. Hardy. 1978. Theoretical and Experimental Methods in the Solution of Missile Nonlinear Roll Problems. Defense Technical Information Center. https://doi.org/10.21236/ada055718
• Darvekar, Sanjay, and Subrahmanyam Kanney. 2016. “Drag Reduction by Rotation of Frontal Shell in Case of Axisymmetric Slender Body.” Indian Journal of Science and Technology 9 (42). https://doi.org/10.17485/ijst/2016/v9i42/95791
• Daryabeigi, Kamran. 2001. “Thermal Analysis and Design of Multi-Layer Insulation for Re-Entry Aerodynamic Heating.” In 35th AIAA Thermophysics Conference. AIAA 2001-2834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2834
• Das, Arpan, Errol Hale, Pier Marzocca, and Michael J. Candon. 2025. “A Data-Driven Approach in Real-Time Trajectory Prediction of Store Release from Cavity.” In AIAA SCITECH 2025 Forum. AIAA 2025-1261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1261
• Das, S., P. Kumar, J. K. Prasad, M. K. Ralh, and R. Krishna Mohan Rao. 2023. “Drag Reduction of a Hemispherical Body Adopting Spike at Supersonic Speed.” Journal of Aerospace Sciences and Technologies: 315–27. https://doi.org/10.61653/joast.v65i4.2013.872
• Dasaro, Joseph A. 1970. Rapid Initialization of Inertial Navigation Systems through Parameter Estimation. Defense Technical Information Center. https://doi.org/10.21236/ad0706219
• Davenport, Esther Lee, Joanne Green, William E. Sears, and Harold F. 1981. Refinements and Validation Testing of Human Operator Performance Emulator (HOPE). Defense Technical Information Center. https://doi.org/10.21236/ada097449
• Davidian, Kenneth J. 1989. A Rocket Engine Design Expert System. NASA-TM-102373. NASA. https://ntrs.nasa.gov/citations/19900000856
• Davidian, Kenneth O. 1990. “Developments in REDES: The Rocket Engine Design Expert System.” In JANNAF Combustion Meeting. https://ntrs.nasa.gov/citations/19910000806
• Davids, S., and A. Cenko. 2001. “Grid Based Approach to Store Separation.” In 19th AIAA Applied Aerodynamics Conference. AIAA 2001-2418. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2418
• Davis, W. T. 1984. Missile Rolling Tail Brake Torque System. Patent Number: NASA-CASE-LAR-12751-1. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840008163
• Davis, Richard W. 1999. Theater Air and Missile Defense Family of Systems. 8th Annual AIAA/BMDO Technology Conference. Defense Technical Information Center. https://doi.org/10.21236/ada370455
• Davis, Myron, and Tracy Welterlen. 2003. “Minimized Domain CFD for Store Separation.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1245. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1245
• Davis, Myron, Pat Yagle, B. Smith, K. Chankaya, and R. Johnson. 2009. “Store Trajectory Response to Unsteady Weapons Bay Flowfields.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-547
• Dawson, W., and N. Parke IV. 1968. “Development Tools for a Strapdown Guidance System.” In Control and Flight Dynamics Conference. AIAA 1968-826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-826
• Day, Donald W. 2013. “Circular Error Probability (CEP) of in a De-Reefed Parachute Payload Recovery System in Stratospheric Flights.” In AIAA Balloon Systems (BAL) Conference. AIAA 2013-1375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1375
• Dayman, B., Jr., and D. Kurtz. 1968. “Forebody Effects on Drogue Drag in Supersonic Flow.” In 6th Aerospace Sciences Meeting. AIAA 1968-8. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-8
• Dazer, Martin, Alexander Grundler, Achim Benz, Marco Arndt, and Philipp Mell. 2022. Pitfalls of Zero Failure Testing for Reliability Demonstration. https://doi.org/10.3850/978-981-18-5183-4_r28-06-054
• de Almeida, Daniel Soares, and Cristiane Maria de Moraes Pagliuco. 2014. “Development Status of the L75: A Brazilian Liquid Propellant Rocket Engine.” Journal of Aerospace Technology and Management 6 (4): 475–84. https://doi.org/10.5028/jatm.v6i4.386
• de Iaco Veris, Alessandro. 2020a. “Fundamental Concepts on Liquid-Propellant Rocket Engines.” In Springer Aerospace Technology. Springer International Publishing. https://doi.org/10.1007/978-3-030-54704-2_1
• de Iaco Veris, Alessandro. 2020b. “The Thrust Chamber Assembly.” In Springer Aerospace Technology. Springer International Publishing. https://doi.org/10.1007/978-3-030-54704-2_2
• De Maio, A., A. Farina, A. Aubry, V. Carotenuto, and L. Pallotta. 2017. “Cognition in Radar Target Tracking.” In The Impact of Cognition on Radar Technology. Institution of Engineering and Technology. https://doi.org/10.1049/sbra520e_ch7
• Debasis Chakraborty. 2023. “Cfd Simulations of Store Separation: An Indian Perspective.” Journal of Aerospace Sciences and Technologies: 220–44. https://doi.org/10.61653/joast.v73i4.2021.102
• Dederra, H. 1975. “Test Results with a Regeneratively Cooled LOX/LH2 Thrust Chamber Forthe Ariane 3rd Stage Propulsion System.” In 11th Propulsion Conference. AIAA 1975-1189. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1189
• 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
• Deepak, Vijayarani Ponraj. 2004. “Fuzzy Enhanced Maneuverability Law for Tactical Missile Guidance.” In AIP Conference Proceedings, vol. 718. AIP. https://doi.org/10.1063/1.1787360
• Deets, D. A., and K. J. Szalai. 1970. “An Airborne Simulator Program to Determine If Roll-Mode Simulation Should Be a Moving Experience.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19700048086
• DeHoff, Bryan, Edgar K. Tucker, and R. McAmis. 1993. “Liquid-Propellant Rocket Engine Testing at Arnold Engineering Development Center.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/931447
• Dejarnette, F. 1983. “Aerodynamic Heating and Surface Temperatures on Vehicles for Computer-Aided Design Studies.” In 21st Aerospace Sciences Meeting. AIAA 1983-411. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-411
• Dejarnette, F., H. Hamilton, and K. Weilmuenster. 1985. “A Review of Some Approximate Methods Used in Aerodynamic Heating Analyses.” In 20th Thermophysics Conference. AIAA 1985-906. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-906
• Delangre, John P. 1959. “Motion-Picture Film Processing System for Guided Missile Research.” Journal of the SMPTE 68 (10): 686–90. https://doi.org/10.5594/j16967
• Delcher, R., A. Dergevorkian, and S. Barkhoudarian. 1989. “Fiberoptics for Liquid Propellant Rocket Engine Environments.” In 25th Joint Propulsion Conference. AIAA 1989-2416. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-2416
• Delmonte, J. 1967. A Semiconductor Combustion Pressure Transducer for Rocket-Motor Instability Studies. NASA. https://ntrs.nasa.gov/citations/19670046091
• 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
• Demir, Görkem. 2018. “Computational Fluid Dynamics Modelling of Store Separation for Transonic Generic Store.” In 2018 Fluid Dynamics Conference. AIAA 2018-3860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3860
• 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, Mingyang, Haiting Li, and Zhuang Xiong. 2026. “An FPGA-Based Laser Semi-Active Guidance Information Processing Architecture.” In Third International Conference on Optoelectronic Information and Optical Engineering (OIOE 2026), edited by Harith Bin Ahmad, Lingfeng Shi. SPIE. https://doi.org/10.1117/12.3116497
• Deng, W., B. Q. Mao, B. W. Liang, and P. Song. 2015. “Co-Simulation of Stabilization Accuracy Optimization of Overhead Weapon Station.” In Advances in Engineering Research. Atlantis Press. https://doi.org/10.2991/asei-15.2015.193
• Deng, Yuhao, Julan Xie, Zishu He, and Jun Li. 2021. “Monopulse Estimation of Unknown Polarization for Conformal Phased Array with Arbitrarily Oriented Dipoles.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-407708/v1
• Denney, Mark D. 1994. “Within-the-Beam Miss Distance Analysis.” In SPIE Proceedings, vol. 2221, edited by Michael K. Masten, Larry A. Stockum, Morris M. Birnbaum, George E. Sevaston. SPIE. https://doi.org/10.1117/12.178959
• Derkevorkian, Armen, Philip Avery, Charbel Farhat, Jason Rabinovitch, and Lee Peterson. 2019. “Effects of Structural Parameters on the FSI Simulation of Supersonic Parachute Deployments.” In AIAA Aviation 2019 Forum. AIAA 2019-3276. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3276
• Derose, C. 1971. “Surface Flow Patterns and Aerodynamic Heating on Space Shuttle Vehicles.” In 4th Fluid and Plasma Dynamics Conference. AIAA 1971-594. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-594
• Dershin, H., W. H. Gallaher, and C. A. Leonard. 1967. Direct Measurement of Compressible, Turbulent Boundary Layer Skin Friction on a Porous Flat Plate with Mass Injection. AIAA PAPER 67-194. NASA. https://ntrs.nasa.gov/citations/19670039612
• “Design of CLOS Guidance System.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-22
• “Design of Gas-Pressurized Propellant Feed Systems.” 1992. In Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866197.0135.0153
• “Design of Guidance Laws Implementing Parallel Navigation. Frequency- Domain Approach.” 2007a. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-9
• “Design of Guidance Laws Implementing Parallel Navigation. Time-Domain Approach.” 2007b. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-8
• “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
• “Design of Rocket-Engine Control and Condition-Monitoring Systems.” 1992. In Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866197.0219.0283
• “Design of Turbopump Propellant Feed Systems.” 1992. In Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866197.0155.0218
• Deslandes, R., and J. Seifert. 2000. “Improvements of Store Separation Analysis by Considering Realistic Aircraft Response.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4200. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4200
• 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. 2003b. “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
• Dethloff, R. C. 1961. Development of High Performance Rocket Motor Case. Defense Technical Information Center. https://doi.org/10.21236/ad0258305
• DeTroye, David J., and Vincent J. Ellis. 1994. Non-Intrusive Missile Control Surface Monitor System. Defense Technical Information Center. https://doi.org/10.21236/ada285356
• Deutsch, Stephen. 2006. UAV Operator Human Performance Models. Defense Technical Information Center. https://doi.org/10.21236/ada464246
• Devan, Leroy. 1987. “Inviscid, Nonaxisymmetric Body, Supersonic Aerodynamic Prediction.” In 14th Atmospheric Flight Mechanics Conference. AIAA 1987-2296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2296
• 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
• Devi, M. Rajani. 2021. “Low Probability of Intercept (LPI) Radar Signal Identification Techniques.” Bioscience Biotechnology Research Communications 14 (5): 365–73. https://doi.org/10.21786/bbrc/14.5/63
• 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
• Dhabale, Ashwin, and Debasish Ghose. 2012. “Impact Angle Constraint Guidance Law Using Cubic Splines for Intercepting Stationary Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4689. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4689
• Dharmendrabhai, Prajapati D., Akash Gholap, Nikhil K. Singh, and Sikha Hota. 2022. “Impact Angle Constrained Guidance Law for Intercepting Non-Maneuvering Targets Avoiding Obstacles.” In AIAA SCITECH 2022 Forum. AIAA 2022-0752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0752
• Dhawan, Satish. 1953. Direct Measurements of Skin Friction. NACA-TR-1121. NASA. https://ntrs.nasa.gov/citations/19930092157
• Diao, Yin, Baogang Lu, and Yingzi Guan. 2022. Research on Guidance Method of Hypersonic Vehicle Based on Reinforcement Learning and Dynamic Surface Control. https://doi.org/10.5220/0012010400003612
• Dickerson, K., H. Watkins, B. Hartle, and C. Kovesdi. 2025. “Function Allocation: Myths, Process, and Emerging Methods.” In Nuclear Plant Instrumentation and Control & Human-Machine Interface Technology (NPIC&HMIT 2025). American Nuclear Society. https://doi.org/10.13182/xyz-46654
• Dickson, Richard E. 1986. Toward a More Unified Theory of Monopulse Rhode’s Theory of Monopulse: Revisited. Defense Technical Information Center. https://doi.org/10.21236/ada180616
• 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
• “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
• Diggins, J. L. 1951. Diffuser Investigations in a Supersonic Wind Tunnel. Defense Technical Information Center. https://doi.org/10.21236/ad0895227
• 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, Marnix, Thomas Canning, Teresa Lesieutre, and Samuel McIntosh. 1992a. “Aeroelastic Tailoring Procedure to Optimize Missile Fin Center of Pressure Location.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-80. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-80
• 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, Marnix F. E., David L. Johnson, and Daniel J. Lesieutre. 1992b. Improvements to the Missile Aerodynamic Prediction Code DEMON3. NASA-CR-4432. NASA. https://ntrs.nasa.gov/citations/19920011432
• 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
• Dinesh, Kantubhukta, D. NarendraKumar, J. Vijaychandra, B. SeshaSai, K. Vedaprakash, and Koyyana Srinivasa Rao. 2021. “A Review on Cascaded Linear Quadratic Regulator Control of Roll Autopilot Missile.” Preprint, . https://doi.org/10.2139/ssrn.3768344
• 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, Chenxi, Kun Wang, Yanning Guo, Gang Zhang, and Pengyu Wang. 2026b. “Physics-Informed Trajectory Optimization for Terminal Guidance Based on Adjoint Control Transformation.” Preprint, . https://doi.org/10.2139/ssrn.6662558
• Ding Chibiao and Mao Shiyi. n.d. “Miss Distance Dynamics in Active Radar Homing Missiles.” In Proceedings of International Radar Conference. Publishing House of Electron. Ind. https://doi.org/10.1109/icr.1996.574597
• Dinh, Ian. n.d. “Design of Main Parachute Recovery System for AUSROC2.5 Rocket.” PhD diss., The University of Queensland. https://doi.org/10.14264/345519
• Dinter, H. A. 1970. “Gyro Dynamic Error Problems in a Strapdown System.” In INST. OF NAVIGATION. https://ntrs.nasa.gov/citations/19710031760
• Dipprey, D. F. 1972. Liquid Propellant Rockets. California Institute of Technology, Jet Propulsion Laboratory, Pasadena. https://ntrs.nasa.gov/citations/19730045334
• Dixon, Nolan L., and Douglas F. Hunsaker. 2023. “A Theoretical Trade-Off between Wave Drag and Sonic Boom Loudness Due to Equivalent Area Changes on a Supersonic Body.” In AIAA SCITECH 2023 Forum. AIAA 2023-1512. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1512
• Djanal-Mann, Dominique J., and Muthuvel Murugan. 2025. “Application of PID Control to Hypersonic Vehicle Control Surfaces.” In AIAA SCITECH 2025 Forum. AIAA 2025-2632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2632
• Dmitriev, I. S., O. N. Zavalishina, and M. P. Slichenko. 2024. “Potential Accuracy of Direction Finding by Non-Monopulse Detector-Direction Finder with Ring Antenna Array for Various Switching Options.” Radioengineering. https://doi.org/10.18127/j00338486-202412-02
• Doan, Larry, Patrick A. Day, and Oleg Brovko. 1995. Large Dynamic Range Radar Cross Section Parallel Tracking. Defense Technical Information Center. https://doi.org/10.21236/ada304014
• Doane, Stephanie. 2003. Relating Memory Processes to Aviation Flight Situation Awareness Abilities. Defense Technical Information Center. https://doi.org/10.21236/ada417024
• Dobyns, A., and D. McCarthy. 1990. “Analysis of Composite Helicopter Structure for Missile Launch Effects.” In 31st Structures, Structural Dynamics and Materials Conference. AIAA 1990-1122. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1122
• Dodge, C., G. Nunz, and R. Riebling. 1972. “Experimental Evolution of an Earth-Storable Bimodal Rocket Engine.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1128
• Doig, Graham, Goran Bogdan, Murray Snyder, and Ben Rowe. 2013. “Aspects of Sting Interference for Transonic Store Release Wind Tunnel Testing.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-642. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-642
• Dolgih, Dmitriy E. 2025. “Dynamic Loading Conditions of Radial Bearings of Rocket Steering Units of Liquid Rocket Engine Steering Units.” Journal of Dynamics and Vibroacoustics 11 (2): 46–55. https://doi.org/10.18287/2409-4579-2025-11-2-46-55
• Doman, David, and Mark Anderson. 1998. “Minimal Representations of Human Operator Dynamics in Compensatory Systems.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4143
• Donahue, Benjamin. 2001. “Air-Launched Mini-Shuttle.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3963
• Donatelli, G., and E. Fleeman. 1982. “Methodology for Predicting Miss Distance for Air Launched Missiles.” In 20th Aerospace Sciences Meeting. AIAA 1982-364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-364
• 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, Wei, Haiqing Li, Chunyan Wang, Jianan Wang, and Jiayuan Shan. 2021a. “Nonlinear Impact Angle Constrained Guidance Law Design via the SDRE Method.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_102
• Dong, Yizhang, Zhiwei Shi, Kun Chen, and Zengran Ge. 2023c. “Suppression of Roll Oscillations of a Canard-Configuration Model Using Fluid Effector and Reinforcement Learning.” Journal of Aerospace Engineering 36 (3): 04023005. https://doi.org/10.1061/jaeeez.aseng-4429
• Dong, Wei, Chunyan Wang, Jianan Wang, Ming Xin, and Fang Deng. 2025a. “Command-Decoupled Spatial-Temporal Cooperative Guidance.” In Spatial-Temporal Cooperative Guidance for Multiple Flight Vehicles. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-5138-2_5
• Dong, Wei, Chunyan Wang, Jianan Wang, Ming Xin, and Fang Deng. 2025b. “Varying-Gain Proportional Navigation Guidance for Time Control.” In Spatial-Temporal Cooperative Guidance for Multiple Flight Vehicles. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-5138-2_3
• Dong, Liang-ci, Tao Zhao, Wei Shang, and Jun-hui Xiong. 2018. “Variable Structure Guidance with Auto-Generated Impact Angle Constraint Based on Fuzzy Strategy.” In Global Intelligence Industry Conference (GIIC 2018), edited by Yueguang Lv. SPIE. https://doi.org/10.1117/12.2503908
• Doolan, Con. 2006. “An Air-Launched Hypersonic Vehicle Performance Study.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-222. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-222
• Doro-on, Anna M. 2022. “Missile Systems Engineering.” In CRC Press eBooks. CRC Press. https://doi.org/10.4324/9780429272233-7
• 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
• 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, Alexander B., Parham Oveissi, Jeffrey Barton, and Ankit Goel. 2026. “Swarm-Optimized Adaptive Augmentation of Missile Autopilot.” In AIAA SCITECH 2026 Forum. AIAA 2026-2164. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2164
• Doso, M., M. Khali, M. Y. Zakaria, and M. Y. Ahmed. 2023. “Assessment of Drag Prediction Techniques Based on Radar Data for Supersonic Vehicles.” Journal of Physics: Conference Series 2616 (1): 012007. https://doi.org/10.1088/1742-6596/2616/1/012007
• Dou, Libin, Qi Jiang, Wenyuan Zhang, Rui Wang, and Cheng Hu. 2024. “Analysis of Formation UAV Targets’ Angular Glint Characteristics Using Phase Gradient Method.” IET Conference Proceedings 2023 (47): 1669–75. https://doi.org/10.1049/icp.2024.1335
• Dougherty, F., and Jyh-Horng Kuan. 1989. “Transonic Store Separation Using a Three-Dimensional Chimera Grid Scheme.” In 27th Aerospace Sciences Meeting. AIAA 1989-637. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-637
• Douglass, H. W., G. Hennings, and H. G. Price Jr. 1959. Experimental Performance of Liquid Hydrogen and Liquid Fluorine in Regeneratively Cooled Rocket Engines. NASA-TM-X-87. NASA. https://ntrs.nasa.gov/citations/19660024052
• Douvillier, Joseph G., Jr., John V. Foster, and Fred J. Drinkwater III. 1956. An Airborne Simulator Investigation of the Accuracy of an Optical Track Command Missile Guidance System. NACA-RM-A56G24. NASA. https://ntrs.nasa.gov/citations/19930089453
• Dow, Stephen J. 2001. Missile Trainer Workstation Enhancement. Defense Technical Information Center. https://doi.org/10.21236/ada401149
• Dow, E., and R. Sarver. 1972. “The Effects of Protuberances and Scaling Parameters on the Aerodynamic Characteristics of an Air-to-Air Cruciform Missile.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-969
• Dowdle, J. 1985. “An Optimal Guidance Law for Supersonic Sea Skimming.” In Guidance, Navigation and Control Conference. AIAA 1985-1866. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1866
• Doyle, Josh, and Christopher C. Rosema. 2015. “Enhanced Body Vortex Modeling within Missile Datcom.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-2587. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2587
• Drake, David L. 1967. Display for a Forward-Looking Radar. Defense Technical Information Center. https://doi.org/10.21236/ad0380510
• Drakulić, Una. 2023. “Performance Comparison of Bilateral Teleoperation Control of Direct Control, PID Control, and Fuzzy Logic Control for Water Tank System.” IOP Conference Series: Materials Science and Engineering 1298 (1): 012023. https://doi.org/10.1088/1757-899x/1298/1/012023
• Drexler, Morris. 2006. Radar Transponder Antenna Systems Evaluation Handbook. Defense Technical Information Center. https://doi.org/10.21236/ada630611
• Dreyfus, Stuart E., and Jarrell R. Elliott. 1963. An Optimal Linear Feedback Guidance Scheme. RAND-RM-3604-PR. RAND Corporation. https://ntrs.nasa.gov/citations/19630010297
• Driels, Morris R., and Young S. Shin. 2004. Determining the Number of Iterations for Monte Carlo Simulations of Weapon Effectiveness. Defense Technical Information Center. https://doi.org/10.21236/ada423541
• Driftmyer, Richard. 1988. “Skin Friction Measurement Problems: Mach = 10.” In 15th Aerodynamic Testing Conference. AIAA 1988-2023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2023
• 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, Cornelius, and Clyde V. Hamilton. 1956. Wind-Tunnel Investigation of a Ram-Jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges: Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01. NACA-RM-L56B21. NASA. https://ntrs.nasa.gov/citations/19930089240
• Drougge, G. 1990. “30th Lanchester Memorial Lecture: The Wave Drag of Delta Wings at Supersonic Speeds: A Recent Study.” Aeronautical Journal 94 (937): 225–30. https://doi.org/10.1017/s000192400002296x
• Drury, Colin G. 1976. “Human Performance in Manual Process Control.” In Monitoring Behavior and Supervisory Control. Springer US. https://doi.org/10.1007/978-1-4684-2523-9_30
• 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
• Drynan, David. n.d. “The Parachute Recovery System Design for the AUSROC 2.5 Rocket.” PhD diss., The University of Queensland. https://doi.org/10.14264/299127
• Du, Feiping. 2017. “Choi-Williams Ditribution Analysis for Fault Detection of the Liquid Propellant Rocket Engine.” Preprint, . https://doi.org/10.26226/morressier.59c106e9d462b80292389e5d
• Du, He, Ming Yang, Songyan Wang, and Tao Chao. 2026. “Impact Angle Control with Field-of-View Constrained Guidance Law against a Various Motion of Target.” Aeronautical Journal 130 (1344): 639–56. https://doi.org/10.1017/aer.2025.10122
• Duan, Lian, and Meelan M. Choudhari. 2012. “Effects of Riblets on Skin Friction in High-Speed Turbulent Boundary Layers.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20120001342
• Duan, Lian, and Meelan, M. Choudhari. 2014. “Direct Numerical Simulations of High-Speed Turbulent Boundary Layers over Riblets.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140011906
• Duan, Hongyao, and Jing Wang. 2024. “Optimization and Simulation Study of Strapdown Seeker Line of Sight Angular Rate Estimation Algorithm.” In Fourth International Conference on Telecommunications, Optics, and Computer Science (TOCS 2023), edited by Jinfeng Wang. SPIE. https://doi.org/10.1117/12.3025742
• Dubben, James, and Charles Denegri. 2007. “Underwing Missile Aerodynamic Effects on Flight-Measured Limit Cycle Oscillations.” In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2007-1801. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1801
• Dubois, I., M. Habiballah, and R. Lecourt. 1995. “Numerical Analysis of Liquid Rocket Engine Combustion Instability.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-607. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-607
• Duffy, Robert. 1989. “Experimental Measurements of the Aerodynamic Hinge Moment on a Plaintrailing-Edge Flap at M = 10.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3383. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3383
• Dugger, P. H. 1982. Range Instrumentation Development. Defense Technical Information Center. https://doi.org/10.21236/ada118436
• Dukes, Wilfred H. 1962. “Progress Report on the Development of Protected Construction for Hypersonic Vehicles.” In Proceedings of the National Meeting on Manned Space Flight (Unclassified Portion). https://ntrs.nasa.gov/citations/19620004480
• Dumper, K. 1997. “Spaceborne Synthetic Aperture Radar and Noise Jamming.” In Radar Systems (RADAR 97), vol. 1997. IEE. https://doi.org/10.1049/cp:19971707
• Dunbar, William G., and Sidney W. Silverman. 1986. Cruise Missile Power System. Defense Technical Information Center. https://doi.org/10.21236/ada174324
• Duncan, W. J. 1950. “Note on the Dependence of Flap Hinge Moment Derivatives on Hinge Position.” Aeronautical Quarterly 2 (2): 143–45. https://doi.org/10.1017/s0001925900000378
• Duncan, Donald B. 1958. “Inertial Guidance and Space Navigation.” Navigation 6 (1): 30–33. https://doi.org/10.1002/j.2161-4296.1958.tb01031.x
• Dung, Do Quang. 2025. “Integrated Kalman-Filter-Based Algorithm for Parameter Estimation of Air-Launched Missiles in Warning and Combat Systems.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate1125018.014
• Dung, Kieu Tien. 2026. “An Adaptive Terminal Guidance Law with Target Maneuver Compensation for Surface-to-Air Missile Interception of High-Agility UAVs.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0726038.32
• Dungate, D. 1999. “Higher-Order Kalman Filter to Support Fast Target Tracking in a Multi-Function Radar System.” In IEE Colloquium. Target Tracking: Algorithms and Applications, vol. 1999. IEE. https://doi.org/10.1049/ic:19990515
• Dunlop, A. J. 1981. “AGC Response and Target Glint.” IEE Proceedings F Communications, Radar and Signal Processing 128 (2): 83. https://doi.org/10.1049/ip-f-1.1981.0013
• Dunn, Glenn. 1990. Test Plan Pressure Fed Thrust Chamber Technology. NASA-CR-184083. NASA. https://ntrs.nasa.gov/citations/19910007822
• Dunworth, Kevin, Donald Atkins, and Jae Lee. 2005. “Incorporation of CFD Generated Aerodynamic Data in Store Separation Predictions.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-846. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-846
• Durga, Naveen. n.d. “Situation Awareness in Multiple UAV Control.” PhD diss., San Jose State University. https://doi.org/10.31979/etd.v2em-nbfx
• Durgun, Behice. 2017. “The Human Nervous System as a Model for Function Allocation in Human-Automation Interaction.” In Advances in Intelligent Systems and Computing. Springer International Publishing. https://doi.org/10.1007/978-3-319-60642-2_38
• Durston, D., and J. Schreiner. 1983. “High Angle-of-Attack Aerodynamics of a Strake-Canard-Wing V/STOL Fighter Configuration.” In Aircraft Design, Systems and Technology Meeting. AIAA 1983-2510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2510
• Durston, Donald A., and Ronald K. Stonum. 1987. “Wave Drag and High-Speed Performance of Supersonic STOVL Fighter Configurations.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/872311
• Dutzmann, R., and N. Ludtke. 1969. “An Integrated Sensor Controller for Missile Directional Control.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-837. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-837
• Dwivedi, P. N., Prashant G. Bhale, Abhijit Bhattacharyya, and Radhakant Padhi. 2013. “Lead Angle Constrained Optimal Midcourse Guidance.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4786
• Dwyer, H., E. Hopkins, and E. Keener. 1971. “Turbulent Skin Friction and Boundary-Layer Profiles Measured on Nonadiabatic Flat Plates at Hypersonic Mach Numbers.” In 9th Aerospace Sciences Meeting. AIAA 1971-167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-167
• “Dynamic Design Technology of Missile Launch System.” 2011. In International Symposium on Information Engineering and Electronic Commerce, 3rd (IEEC 2011). ASME Press. https://doi.org/10.1115/1.859759.paper25
• “Dynamic Function Allocation.” 2006. In International Encyclopedia of Ergonomics and Human Factors - 3 Volume Set. CRC Press. https://doi.org/10.1201/9780849375477-235
• 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. 1992. “Comparison of Missile Flight Test Data with Aerodynamic Predictions.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-76. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-76
• Eberhart, Chad, David Lineberry, and Robert Frederick. 2012. “Propellant Throttling Effects on Self-Pulsation of Liquid Rocket Swirl-Coaxial Injection.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-4204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4204
• Ebrahimi, Mohsen, and Saeed Nasrollahi. 2023. “Fractional Guidance Law with Impact Angle Constraint and Seeker’s Look Angle Limits.” Unmanned Systems 13 (01): 261–77. https://doi.org/10.1142/s2301385025500189
• 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
• Edefur, Henrik, Fredrik Haglind, and Stefan Olsson. 2007. “Design of an Air-Launched Tactical Missile for Three Different Propulsion Systems: ATR, Rocket and Turbojet.” In Volume 1: Turbo Expo 2007. ASMEDC. https://doi.org/10.1115/gt2007-27844
• Edge, Harris, Jubaraj Sahu, and Karen Heavey. 1999. “Computational Fluid Dynamics Modeling of Submunition Separation from Missile.” In 17th Applied Aerodynamics Conference. AIAA 1999-3129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3129
• 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, Sherman, and Katsumi Hikido. 1953. A Method for Estimating the Rolling Moments Caused by Wing-Tail Interference for Missiles at Supersonic Speeds. NACA-RM-A53H18. NASA. https://ntrs.nasa.gov/citations/19930087843
• “Effects of Aerodynamic Heating and TPS Thermal Performance Uncertainties on the Shuttle Orbiter.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0247.0268
• “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
• Eggers, A. J., Jr. 1965. Nonslender Bodies of Revolution Having Minimum Pressure Drag. NASA. https://ntrs.nasa.gov/citations/19660043224
• Eggers, A. J., Jr., Meyer M. Resnikoff, and David H. Dennis. 1957. Bodies of Revolution Having Minimum Drag at High Supersonic Airspeeds. NACA-TR-1306. NASA. https://ntrs.nasa.gov/citations/19930092299
• Eggleston, John M., and Robert S. Dunning. 1961. Analytical Evaluation of a Method of Midcourse Guidance for Rendezvous with Earth Satellites. NASA-TN-D-883. NASA. https://ntrs.nasa.gov/citations/19980227200
• Eguchi, Hirofumi, Hidehiko Kubo, and Tadashi Yamashita. 1991. “Robust Stability of Guidance and Control System for Homing Missiles.” In 29th Aerospace Sciences Meeting. AIAA 1991-585. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-585
• 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
• Ehrenfeld, Sylvain. 1959. Variability of Lethal Area. Defense Technical Information Center. https://doi.org/10.21236/ad0305166
• Ehricke, Krafft A. 1955. MX-2276 Advanced Strategic Weapon System. Preliminary Global System Study. Defense Technical Information Center. https://doi.org/10.21236/ad0073756
• Ehrsam, E. E., S. A. Cresswell, G. R. McKelvey, and F. L. Matthews. 1978. “Precise Terrestrial Time: A Means for Improved Ballistic Missile Guidance Analysis.” In NASA. Goddard Space Flight Center Proc. of the Tenth Ann. Precise Time and Time Interval (PTTI) Appl. and Planning Meeting. https://ntrs.nasa.gov/citations/19790016565
• 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
• 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
• Ekimogloy, Vasilios, Lucian Stelk, and Luke Raque. 2026. “Managing Safety Hazards for a Liquid Rocket Engine Test System.” In 2026 Regional Student Conferences. AIAA 2026-112651. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-112651
• El mahdi, Loai A., Mahmoud Y. Ahmed, Osama Mahmoud, and Omar Abdel Hameed. 2017. “A Comparative Study of Prediction Techniques for Supersonic Missile Aerodynamic Coefficients at Incidence.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-1205. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1205
• 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-Madany, M. M., and S. I. Alswailem. 1995. “Classical versus Modern Guidance Laws for Homing Missiles.” In Current Advances in Mechanical Design and Production VI. Elsevier. https://doi.org/10.1016/b978-008042140-7/50040-8
• El-Mahdy, L., M. Ahmed, O. Mahmoud, and O. Abdel-Hameed. 2016. “Experimental, Computational, and Empirical Evaluation of Supersonic Missile Aerodynamic Coefficients.” International Conference on Applied Mechanics and Mechanical Engineering 17 (17): 1–15. https://doi.org/10.21608/amme.2016.35168
• 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
• 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
• Elfstrom, G., C. Kostopoulos, D. Peake, and D. Fisher. 1982. “The Obstacle Block as a Device to Measure Turbulent Skin Friction Incompressible Flow.” In 12th Aerodynamic Testing Conference. AIAA 1982-589. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-589
• Elkind, J. I., and D. C. Miller. 1967. The Adaptive Response of the Human Controller to Sudden Changes in Controlled Process Dynamics. NASA. https://ntrs.nasa.gov/citations/19680094916
• Elliott, R. D. 1966. Methods for Predicting Aerodynamic Heating Rates to High-Velocity Bodies in the Upper Atmosphere. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4564563
• Elliott, D. G., and R. K. Rose. 1957. Experimental Rocket Motor Performance and Heat Transfer of the Wfna- Ammonia and the Rfna-Ammonia Propellant Systems at Combustion Pressures of 1000 Psia and 1500 Psia. Defense Technical Information Center. https://doi.org/10.21236/ad0139275
• 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
• Ellis, William. 2013. Joint Air-to-Surface Standoff Missile (JASSM). Defense Technical Information Center. https://doi.org/10.21236/ada613368
• 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
• Elston, R. A. 1963. Description of a Control System for Rocket-Motor Mass Measurement. Defense Technical Information Center. https://doi.org/10.21236/ad0407325
• Ema, Tetsuro. 1990. “Manual Control Behaviors in the Two-Axis Tracking Systems. Effects of the Coupling Factor and Study of Human Operator Models.” Japanese Journal of Ergonomics 26 (2): 59–66. https://doi.org/10.5100/jje.26.59
• 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
• Engler, Harold F., Esther L. Davenport, Joanne Green, and William E. Sears III. 1980. Human Operator Control Strategy Model. Defense Technical Information Center. https://doi.org/10.21236/ada084695
• Englisch, W., and M. Endemann. 1984. “Conical Scan-Tracking-Technik mit kohärentem optischen Empfang bei 10 μm.” In Optoelektronik in der Technik / Optoelectronics in Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-82121-9_85
• 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
• Erdos, David, Tal Shima, Evgeny Kharisov, and Naira Hovakimyan. 2012. “L1 Adaptive Control Integrated Missile Autopilot and Guidance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4465. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4465
• Eremeitsev, I. G., and N. N. Pilyugin. 1984. “Friction and Heat Transfer in Laminar and Turbulent Boundary Layers on Axisymmetric Bodies in Nonuniform Supersonic Flows.” Fluid Dynamics 19 (2): 227–34. https://doi.org/10.1007/bf01091244
• Eremeitsev, I. G., and N. N. Pilyugin. 1986. “Heat Transfer and Drag of a Body in a Far Supersonic Wake.” Fluid Dynamics 21 (2): 218–24. https://doi.org/10.1007/bf01050172
• 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
• Erer, Koray S., and M. Kemal Ozgoren. 2013. “Control of Impact Angle Using Biased Proportional Navigation.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5113
• Erer, Koray S., Raziye Tekin, and M. Kemal Ozgoren. 2015. “Look Angle Constrained Impact Angle Control Based on Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0091. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0091
• Ericksen, R., J. Guiteras, and J. Larrivee. 1966. “A Parachute Recovery System Dynamic Analysis.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-25. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-25
• Ericksen, R., W. Pepper, and L. Whinery. 1984. “Preliminary Results of the Effects of Sewing, Packing and Parachute Deployment on Material Strength.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-813
• Erickson, C. M. 1992. Orbit Transfer Rocket Engine Technology Program: Advanced Engine Study. NASA-CR-187215. NASA. https://ntrs.nasa.gov/citations/19920013349
• 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
• Ernst, Katie M., Emilie Roth, Scott Scheff, et al. 2019. “A Strategy for Determining Optimal Crewing in Future Vertical Lift: Human-Automation Function Allocation.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0075-2019-14558
• “Error Budget.” 2018. In Mechanics of Accuracy in Engineering Design of Machines and Robots Volume I: Nominal Functioning and Geometric Accuracy. ASME Press. https://doi.org/10.1115/1.861615_ch8
• Escher, W., D. Pryor, and E. Hyde. 1999. “Development of a 12-Thrust Chamber Kerosene/oxygen Primary Rocket Subsystem for an Early (1964) Air-Augmented Rocket Ground Test System.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4896
• “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
• Eslinger, Robert C. 1964. “Elimination of Steering Rate Gyro Bias in a Missile Autopilot.” SIMULATION 2 (1): 5–12. https://doi.org/10.1177/003754976400200101
• Esten, Randall D. 1953. Radar Relief Displacement and Radar Parallax. Defense Technical Information Center. https://doi.org/10.21236/ad0018579
• Etzkorn, Letha. 2001. CORBA Support for Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada401028
• Eugene, L. Tu. 1996. Numerical Study of Steady and Unsteady Canard-Wing-Body Aerodynamics. NASA-TM-110394. NASA. https://ntrs.nasa.gov/citations/19960047050
• 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, G., and P. Smith. 1978. “The Suppression of Combustion Instability in Smokeless Solid Propellant Rocket Motors.” In 14th Joint Propulsion Conference. AIAA 1978-1568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1568
• 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
• Evcimen, Çagdas, and Kemal Leblebicioglu. 2013. “An Adaptive, Optimal Proportional-Integral Guidance for Missiles.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4784. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4784
• Evduzen, Rasit. 2026. “Strapdown Seeker Line-of-Sight Rate Estimation via Pixel-Plane Kalman Filtering and Gyro Fusion.” Preprint, . https://doi.org/10.31224/7642
• Ewing, C. 1994. “Advanced Missile Concept Evaluation Toolset (AMCET).” In Flight Simualtion Technologies Conference. AIAA 1994-3417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3417
• Excelco Developments INC Silver Creek NY. 1963. Investigation and Evaluation of High Strength Steels in Heavy Gauges for Large Diameter Solid Propellant Rocket Engine Cases. Defense Technical Information Center. https://doi.org/10.21236/ad0424490
• 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
• Falkiewicz, Nathan, Carlos Cesnik, Michael Bolender, and David Doman. 2009. “Thermoelastic Formulation of a Hypersonic Vehicle Control Surface for Control-Oriented Simulation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6284
• Falkiewicz, Nathan, Scott Frendreis, and Carlos Cesnik. 2011. “Effect of Control Surface-Fuselage Inertial Coupling on Hypersonic Vehicle Flight Dynamics.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2011-6378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6378
• Fan, Jianpeng, Shijie Fan, Hongqi Fan, and Huaitie Xiao. 2013. “An Analytic Expression for near-Field Angular Glint Prediction of Radar Sensor Using Far-Field Scattering Centers Models.” Progress In Electromagnetics Research M 30: 225–38. https://doi.org/10.2528/pierm13032105
• 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, Xiangrui, Jingyong Lin, Jiarun Liu, and Chunmei Zhou. 2017b. “An Intelligent Anti-Jamming Network System of Data Link.” In AOPC 2017: Space Optics and Earth Imaging and Space Navigation, edited by Carl Nardell, Suijian Xue, Huaidong Yang. SPIE. https://doi.org/10.1117/12.2283059
• Fan, Wenfeng, Wei Quan, Feng Liu, Lihong Duan, and Gang Liu. 2019. “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
• Fang, J. 1984. “Application of Combustion Time-Lag Theory to Combustion Stability Analysis of Liquid and Gaseous Propellant Rocket Engines.” In 22nd Aerospace Sciences Meeting. AIAA 1984-510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-510
• Fang, Feng, and Yuan-Li Cai. 2016. “Optimal Cooperative Guidance with Guaranteed Miss Distance in Three-Body Engagement.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232 (3): 492–504. https://doi.org/10.1177/0954410016683416
• Fang, Feng, Qingwei Li, Jiafan He, Yiming Mao, Feng Ding, and Aiguo Fei. 2023. “Air-to-Air Missile Launch Envelope Computation Based on Neural Network.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-99-0479-2_355
• Fang, Yichuan, William Liou, and Sushuan Xu. 2003. “Skin Friction Prediction for High-Speed Turbulent Boundary Layers with Ablation.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1250. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1250
• Fanggidae, Diva Dana, and Wahyu Kusumahardi. 2025. “Analisis Karakteristik Aerodinamika Sayap Pesawat F-16 Fighting Falcon Sebagai Air-Launched Rocket Platform Menggunakan Metode Computational Fluid Dynamics (CFD).” Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) 7: 131–40. https://doi.org/10.54706/senastindo.v7.2025.435
• Fano, Devon, Jonathan Poggie, and Gregory A. Blaisdell. 2020. “Aerodynamic Heating in Missile-Fin Interaction Region.” In AIAA Scitech 2020 Forum. AIAA 2020-0583. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0583
• 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
• Farmer, Richard C., and Gary C. Cheng. 2000. Quantifying Instability Sources in Liquid Rocket Engines. SECA-FR-00-04. SECA, Inc. https://ntrs.nasa.gov/citations/20000059224
• 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
• 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
• Fashbaugh, R. H., and V. L. Streeter. 1965. “Resonance in Liquid Rocket Engine Systems.” Journal of Basic Engineering 87 (4): 1011–17. https://doi.org/10.1115/1.3650792
• Fatuev, Igor Y. 2006. “Analysis of Peculiarities of Liquid Propellant Rocket Engine Startup.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-c4.p.1.05
• 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
• Feaux, Karl, William Jordan, Graham Killough, Robert Miller, and Vonn Plunk. 1989. Low Earth Orbit Raider (LER) Winged Air Launch Vehicle Concept. NASA-CR-186057. NASA. https://ntrs.nasa.gov/citations/19900003274
• Fedaravičius, Algimantas, Karolis Jasas, Egidijus SliŽYs, and Arvydas Survila. 2022. “Modeling of the Missile Launch Dynamic Processes in Short-Range Air Defense System.” Mechanika 28 (1): 32–37. https://doi.org/10.5755/j02.mech.29266
• Fedele, G., M. Orsini, and S. Strappaveccia. 1985. “Monopulse Angular Accuracy for Fluctuating Targets.” Electronics Letters 21 (6): 229–31. https://doi.org/10.1049/el:19850163
• Fedorov, A. V., N. D. Malmuth, and V. G. Soudakov. 2007. “Supersonic Scattering of a Wing-Induced Incident Shock by a Slender Body of Revolution.” Journal of Fluid Mechanics 585: 305–22. https://doi.org/10.1017/s0022112007006714
• Fei, Liu. 2022. “Optimization Method of Air Defense Missile Launch Type.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-3927-3_81
• Feigh, Karen, and Amy Pritchett. 2016. Function Allocation between Human and Automation and between Air and Ground. Wiley. https://doi.org/10.1002/9780470686652.eae1128
• Feldman, J., S. Kazel, R. Standley, and P. Toulios. 1962. Evaluation and Improvement of Radar Beacon Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0404455
• Feng, Dinghua, Zhengyu Tian, Feng Liu, and Hua Li. 2010. “Study of Missile Aerodynamic Characteristics in the Process of Crossing the Carrier’s Shock Wave.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8251
• Feng, Shulin, Wei Wang, and Huanshui Zhang. 2013a. “Implementation of Three-Dimensional Line of Sight Guidance with a Moving Target.” Control and Intelligent Systems 41 (1). https://doi.org/10.2316/journal.201.2013.1.201-2402
• Feng, Dingwei, Siliang Wu, Guo-hua Wei, and Xu Wang. 2013b. “Research of Miss Distance Parameters Estimation Based on Data Fusion of Doppler Frequency and Range.” JOURNAL OF ELECTRONICS INFORMATION TECHNOLOGY 34 (11): 2615–20. https://doi.org/10.3724/sp.j.1146.2012.00582
• Feng, De Long, Suo Chang Yang, and Ying Xi Liu. 2013d. “Research on Missile System with Strapdown Guidance Technology.” Advanced materials research 785-786: 1560–63. https://doi.org/10.4028/www.scientific.net/amr.785-786.1560
• Feng, De Long, Suo Chang Yang, Yun Zhi Yao, and Ying Xi Liu. 2013c. “Research on Improved Extended Proportional Navigation Guidance.” Applied Mechanics and Materials 347-350: 980–84. https://doi.org/10.4028/www.scientific.net/amm.347-350.980
• 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
• Fernando, E., J. Donovan, D. Smith, and A. Smits. 1989. “Conventional Skin Friction Measurement Techniques for Strongly Perturbed Supersonic Turbulent Boundary Layers.” In 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1989-1861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1861
• Ferreira, Daniel Roberto, and Wladimyr Dourado. 2018. “Design of Typical Cooling Jacket for Liquid Propellant Rocket Engine by Computational Fluid Dynamics.” In 17th Brazilian Congress of Thermal Sciences and Engineering. ABCM. https://doi.org/10.26678/abcm.encit2018.cit18-0121
• Ferrer, Eduardo Seiji Suguimoto Miyazato, and Jhonatan Ribeiro dos Santos. 2023. “Simulation of a Liquid Propellant Rocket Engine Manufacturing Assembly Line Utilizing the PFS/PN Methodology.” Mecatrone 6 (1): 1–18. https://doi.org/10.11606/issn.2526-8260.mecatrone.2023.220823
• 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
• Ferris, K. D. 1981. “Fiber-Optic Communication Link for Missile Guidance.” In Integrated Optics and Optical Fiber Communication. OSA. https://doi.org/10.1364/ofc.1981.tue2
• 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
• Fidler, Owen, Jack Jenkins, and Kurt Rouser. 2025. “Evaluating Liquid Rocket Engine Fuel Pressures and Mass Flow Rates.” In 2025 Regional Student Conferences. AIAA 2025-99401. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-99401
• Fifth Annual NASA-University Conference on Manual Control. 1970. NASA-SP-215. NASA. https://ntrs.nasa.gov/citations/19700021566
• Fikes, D. H. 1977. Aerodynamic Characteristics and Fin Loads of a Bank-to-Turn, Air-to-Air Missile Concept at Supersonic Mach Numbers. Defense Technical Information Center. https://doi.org/10.21236/adb019652
• 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
• Fine, T., R. Nock, and R. Sansom. 1965. “A Statistical Technique for the Design of Missile Flight Test Programs to Measure Accuracy Information.” In Flight Testing Conference. AIAA 1965-222. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-222
• Fink, M. 1966. “Hypersonic Minimum-Drag Slender Bodies of Revolution.” In 3rd and 4th Aerospace Sciences Meeting. AIAA 1966-129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-129
• 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
• Finney, Luke P. 2010. Investigation of Cavity Flow Effects on Store Separation Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ada549052
• Fint, Jeffry, Fritz Kuck, and Frank Sciorelli. 2005. “Development of Channel Wall Nozzles for Use on Liquid Propellant Rocket Engine.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4371
• Fiore, Matteo, Francesco Nasuti, Marco Pizzarelli, and Nicola Ierardo. 2022. “HEM Modeling for Subcritical Flows in Liquid Rocket Engine Cooling Systems.” In AIAA AVIATION 2022 Forum. AIAA 2022-3273. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-3273
• Fiorini, Paolo, Blake Hannaford, Bruno Jau, Edwin Kan, and Antal Bejczy. 1987. “Hand Trigger System for Bi-Lateral Gripping Control in Teleoperation.” In 1987 IEEE International Conference on Robotics and Automation. https://ntrs.nasa.gov/citations/19880055451
• First U.S. Missile Intercepts. 2015. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624103506.0255.0264
• Fitz-Coy, Norman, and Ming-Cheng Liu. 1995. “A Modified Proportional Navigation Scheme for Rendezvous and Docking with Tumbling Targets: The Planar Case.” In NASA. Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium 1995. https://ntrs.nasa.gov/citations/19950021363
• Fitzgerald, Robert. 1988. “Reduction of Missile Navigation Errors by Roll Programming.” In Guidance, Navigation and Control Conference. AIAA 1988-4090. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4090
• 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
• Flanagan, M., Jr. 1993. “Aerodynamic Heating in the Vicinity of Hypersonic, Axisymmetric, Shock-Wave Boundary-Layer Interactions.” In 28th Thermophysics Conference. AIAA 1993-2766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2766
• Flandro, Gary, Joseph Sims, and Joseph Majdalani. 2004a. “Nonlinear Longitudinal Mode Instability in Liquid Propellant Rocket Engine Preburners.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-4162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4162
• Flandro, Gary, Joseph Sims, and Joseph Majdalani. 2004b. “On Nonlinear Combustion Instability in Liquid Propellant Rocket Engines.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3516. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3516
• 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
• Fleeman, E., and G. Donatelli. 1981. “Conceptual Design Procedure Applied to a Typical Air-Launched Missile.” In Aircraft Systems and Technology Conference. AIAA 1981-1688. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1688
• “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
• Flora, Thomas, Mark Reeder, Andrew Lofthouse, and Neal Kraft. 2013. “Dynamic Store Release of Ice Models from a Cavity into Mach 2.9 Flow.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-236. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-236
• Flowe, Robert T., and Duane C. Bright. 1963. Lightweight Gyro Azimuth Theodolite (Lear North Seeking Gyro Model No. 11NG530A). Defense Technical Information Center. https://doi.org/10.21236/ad0409872
• Fluhr, F. R. 1963. Four-Frequency Radar Master Console. Defense Technical Information Center. https://doi.org/10.21236/ad0409128
• 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
• Follé, M. I. 1998. “A Slender Chisel-Like Body in a Supersonic Stream.” Fluid Dynamics 33 (5): 761–67. https://doi.org/10.1007/bf02698627
• Fomin, V. M., S. G. Mironov, and K. M. Serdyuk. 2009. “Reducing the Wave Drag of Bodies in Supersonic Flows Using Porous Materials.” Technical Physics Letters 35 (2): 117–19. https://doi.org/10.1134/s1063785009020060
• Fong, L. 1964. “Propellant Surface Flame Propagation in Rocket Motors.” In Solid Propellant Rocket Conference. AIAA 1964-125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-125
• Fontaine, R. 1965. “Sensitivity of Rocket Engine Stability to Propellant Feed Systems Dynamics.” In Propulsion Joint Specialist Conference. AIAA 1965-558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-558
• Fontaine, R. J., R. S. Levine, and L. P. Combs. 1968. “Secondary Nondestructive Instability in Medium Size Liquid Fuel Rocket Engines.” In Advances in Tactical Rocket Propulsion Conference Proceedings. https://ntrs.nasa.gov/citations/19690030801
• Fortenbaugh, R. 1983. “The Maneuver Acceleration Parameter: A Figure of Merit for Evaluating Missile Miss Distance Performance.” In Guidance and Control Conference. AIAA 1983-2199. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2199
• Fortescue, P. W. 1982. “Pitch/Yaw Coupling Due to Roll of an Axisymmetric Missile with Autopilot.” Aeronautical Quarterly 33 (2): 124–39. https://doi.org/10.1017/s0001925900009367
• 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, G. V., and R. B. Robinson. 1961. Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-Movable Wing and Tail Surfaces. NASA-TM-X-516. NASA. https://ntrs.nasa.gov/citations/19650014316
• Fougnie, Alexandre. n.d. “Low Order Modeling of High-Frequency Combustion Instabilities in Liquid Rocket Engines.” PhD diss., université Paris-Saclay. https://doi.org/10.70675/31761767z3506z4985z9474zf30b4ff89686
• 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
• Fowdur, Jaya Shradha. 2022. “Multiple Extended Target Tracking in Maritime Environment Using Marine Radar Data.” PhD diss.. https://doi.org/10.53846/goediss-9486
• Fowler, Kenneth J. 1990. Inertial Navigation System Simulator Program: Top-Level Design. Defense Technical Information Center. https://doi.org/10.21236/ada223762
• Fradenburgh, Evan A., and Robert C. Campbell. 1953. Characteristics of a Canard-Type Missile Configuration with an Underslung Scoop Inlet at Mach Numbers from 1.5 to 2.0. NACA-RM-E52J22. NASA. https://ntrs.nasa.gov/citations/19930087538
• Fradenburgh, Evan A., and Emil J. Kremzier. 1953. Performance Comparison of Three Canard-Type Ram-Jet Missile Configurations at Mach Numbers from 1.5 to 2.0. NACA-RM-E53F11. NASA. https://ntrs.nasa.gov/citations/19930087603
• Fraenkel, L. E. 1958. “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
• “France’s Liquid Propellant Rocket-Engine History.” 2006. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0785.0814
• Freese, Colin E., Donald M. Neal, and Edward M. Lenoe. 1978. Proof Test Procedures for Ceramic Missile Radomes. Defense Technical Information Center. https://doi.org/10.21236/ada056436
• French, K. 1979. “A First-Order Theory for the Effects of Line Ties on Parachute Deployment.” In 6th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1979-450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-450
• French, K. 1988. “Flight Test Experience with an RPV Emergency (Parachute) Recovery System.” In 4th Flight Test Conference. AIAA 1988-2139. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-2139
• Fresconi, Frank. 2011. Guidance and Control of a Fin-Stabilized Projectile Based on Flight Dynamics with Reduced Sensor and Actuator Requirements. Defense Technical Information Center. https://doi.org/10.21236/ada539868
• 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
• Fresconi, Frank, Benjamin Greunwald, and Tansel Yucelen. 2017. “Adaptive Missile Flight Control for Complex Aerodynamic Phenomena.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2017-4207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4207
• Frey, M., B. Kniesner, and O. Knab. 2011. “Consideration of Real Gas Effects and Condensation in a Spray-Combustion Rocket-Thrust-Chamber Design Tool.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/201102285
• 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
• Frick, Charles W. 1948. Application of the Linearized Theory of Supersonic Flow to the Estimation of Control-Surface Characteristics. NACA-TN-1554. NASA. https://ntrs.nasa.gov/citations/19930082357
• Fricker, H. S. 1996. “A Simple Aerodynamic Balance.” Physics Education 31 (4): 207–10. https://doi.org/10.1088/0031-9120/31/4/016
• Friedland, E. 1965. “Liquid Rocket Engine Cost Estimating Relationships.” In 2nd Annual Meeting. AIAA 1965-533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-533
• Friedman, Morris D. 1951. Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag. NACA-RM-A51I20. NASA. https://ntrs.nasa.gov/citations/19930093733
• 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
• Fu, K. S., and E. E. Gould. 1966. Adaptive Model of the Human Operator in a Time-Varying Control Task. Purdue Univ. https://ntrs.nasa.gov/citations/19670006528
• Fu, Zhumu, Dongfeng Wan, Zhikai Wang, and Fazhan Tao. 2024. “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, Xiu Hui, Jingyue Wang, Shu Li Ouyang, and Wei Bo Song. 2011. “Characteristics of Human Operator in Manual Tracking Control System.” Advanced materials research 328-330: 1788–91. https://doi.org/10.4028/www.scientific.net/amr.328-330.1788
• Fujii, Keisuke, and Yasutoshi Inoue. 1998b. “Aerodynamic Heating Measurement on Ceramic Tile Region of Hypersonic Flight Experiment (HYFLEX).” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-605
• Fujii, Keisuke, Shigeya Watanabe, Takuji Kurotaki, and Masao Shirouzu. 2000. “Aerodynamic Heating Measurements on Nose and Elevon of Hypersonic Flight Experiment Vehicle.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-267. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-267
• Fujita, Kazuhisa, and Takashi Abe. 2000. “Assessment of Rotational Nonequilibrium Impact on the Aerodynamic Heating Rate.” In 34th Thermophysics Conference. AIAA 2000-2588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2588
• Fukiba, Katsuyoshi, Yuma Ueno, and Yusuke Maru. 2023. “Suppression of Pressure Oscillation in Supersonic Parachute Model Using a Ring.” International Journal of Aeronautical and Space Sciences 25 (1): 36–45. https://doi.org/10.1007/s42405-023-00654-9
• Fulbright, J. 1977. “Stress Relieving Liners for Air-Launched Tactical Solid Rocket Motors.” In 13th Propulsion Conference. AIAA 1977-827. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-827
• Fuld, Robert B. 1993. “The Fiction of Function Allocation.” Ergonomics in Design: The Quarterly of Human Factors Applications 1 (1): 20–24. https://doi.org/10.1177/106480469300100107
• “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 Mechanisms of Combustion Instabilities: Liquid-Propellant Droplet Vaporization: A Rate-Controlling Process for Combustion Instability.” 1995. In Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866371.0307.0343
• Furukawa, Hiroshi, Toshiyuki Inagaki, and Yuji Niwa. 2004. “Optimization of Task Allocation through Human Cognitive Simulation: Levels of Automation and Human Behaviors.” In Probabilistic Safety Assessment and Management. Springer London. https://doi.org/10.1007/978-0-85729-410-4_42
• 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
• Gagne, G. A., and W. W. Wierwille. 1966a. Characterization of Time-Varying Human Operator Dynamics. NASA-CR-539. NASA. https://ntrs.nasa.gov/citations/19660023669
• Gagne, G. A., and W. W. Wierwille. 1966b. Time Varying and Nonlinear Models of Human Operator Dynamics. NASA. https://ntrs.nasa.gov/citations/19670006530
• Gaiddon, Arnaud, Jean-Noel Greard, and Didier Pagan. 2003. “Automated Optimization of Supersonic Missile Performances Taking into Account Design Uncertainties.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3879
• 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
• Gajera, Viraj. 2026. “Computational Multiphysics Modeling of Instability Staged Combustion Propulsion, Radiative Convective Ablative/TPS Interfacial Heat Transfer, Supersonic Retro Propulsive Landing Dynamics for Reusable Heavy Lift Architectures and Subcooled Liquid Management in High Pressure Rocket Engine and Booster Return Trajectories.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-11332943/v1
• Gal, Shmuel. 1974. “Optimal Test Design for Reliability Demonstration.” Operations Research 22 (6): 1236–42. https://doi.org/10.1287/opre.22.6.1236
• Galante, Joseph M., and Robert M. Sanner. 2012. “A Nonlinear Adaptive Filter for Gyro Thermal Bias Error Cancellation.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20120008277
• Gale, Harold W., and Philip C. Moedt. 1962. Design and Testing of a Pyrogen Igniter for a LO2-LH2 Rocket Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0295670
• 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
• Galli, Federica. n.d. “Offline State of Health Estimation and Prediction of a Reusable Liquid Propellant Rocket Engine to Guide Maintenance Planning.” PhD diss., Normandie. https://doi.org/10.70675/97c77627zc51bz4cb0za02bzf5547129624d
• Gallo, Giuseppe, Hiroki Kojima, Landon Kamps, and Harunori Nagata. 2024a. “Experimental Advancements in the Development of a Regenerative Cooling System for Hybrid Rocket Applications.” In AIAA SCITECH 2024 Forum. AIAA 2024-1609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1609
• 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
• Gallon, John, Allen Witkowski, Ian G. Clark, Tommaso Rivellini, and Douglas S. Adams. 2013. “Low Density Supersonic Decelerator Parachute Decelerator System.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1329
• Gammal, Abraham A., and Thomas L. Kennedy. 1954. Flight Investigation to Determine Lift and Drag Characteristics of a Canard Ram-Jet Missile Configuration in the Mach Number Range of 0.8 to 2.0. NACA-RM-L54D28. NASA. https://ntrs.nasa.gov/citations/19930088289
• Gan, Xu, Xue Qin Tang, and Jian Guo Gao. 2013. “Missile Autopilot Design Based on Fuzzy Self-Tuning Immune PID Control.” Advanced materials research 739: 550–54. https://doi.org/10.4028/www.scientific.net/amr.739.550
• Gao, C., J. Li, T. Feng, and W. Jing. 2017a. “Adaptive Terminal Guidance Law with Impact-Angle Constraint.” Aeronautical Journal 122 (1249): 369–89. https://doi.org/10.1017/aer.2017.124
• Gao, Bo, Shuo Tang, and Zhi Xu. 2017b. “Separation Modeling of the Internal Air-Launch Rocket from a Cargo Aircraft.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2253. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2253
• Gao, Wei, and Weitao Tie. 2017. “Evaluation of Electronic Jamming Effect Based on Seeker Captive Flight Test and Missile Flight Simulation.” In SPIE Proceedings, vol. 10322, edited by Xiyuan Chen. SPIE. https://doi.org/10.1117/12.2265314
• Gao, Yushan, Ping Zhang, and Shihui Huo. 2023. “An Investigation on the Cyclic Deformation and Service Life of a Reusable Liquid Rocket Engine Thrust Chamber Wall.” Multidiscipline Modeling in Materials and Structures 19 (3): 522–43. https://doi.org/10.1108/mmms-02-2023-0044
• Gaonkar, Ashwini Anand, Poornima Menon, and G. Srinivas. 2019. “Aerodynamic Performance Enhancement of Supersonic 2D Missile Using ANSYS.” Universal Journal of Mechanical Engineering 7 (6A): 1–11. https://doi.org/10.13189/ujme.2019.071401
• Garcia, Eloy, David Casbeer, and Meir Pachter. 2017. “Optimal Guidance for Active Aircraft Defense against Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1017
• Garcia, Eloy, David Casbeer, Khanh D. Pham, and Meir Pachter. 2015a. “Cooperative Aircraft Defense from an Attacking Missile Using Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0337
• Garcia, C. P., P. Gradl, J. Wood, C. S. Protz, and S. E. Greene. 2018. Characterizing Performance of Additively Manufacturing Regenerative Cooled Combustion Chambers through Hot Fire Testing. M18-6482. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20180005155
• Gardiner, Robert A., Jacob Zarovsky, and H. O. Ankenbruck. 1950. An Investigation of the Stability of a System Composed of a Subsonic Canard Airframe and a Canted-Axis Gyroscope Automatic Pilot. NACA-TN-2004. NASA. https://ntrs.nasa.gov/citations/19930082667
• Garner, H. D., and H. E. Poole. 1974. Development and Flight Tests of a Gyro-Less Wing Leveler and Directional Autopilot. NASA-TN-D-7460. NASA. https://ntrs.nasa.gov/citations/19740011169
• Gates, Roger, Gerald Winchenbach, John Cipolla, and Mark Fischer. 1989. “Aerodynamic Test and Analysis of a Slender Generic Missile Configuration.” In 16th Atmospheric Flight Mechanics Conference. AIAA 1989-3368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3368
• 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
• Gaudet, Brian, and Roberto Furfaro. 2012. “Missile Homing-Phase Guidance Law Design Using Reinforcement Learning.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4470. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4470
• Gaudet, Brian, and Roberto Furfaro. 2023. “Line of Sight Curvature for Missile Guidance Using Reinforcement Meta-Learning.” In AIAA SCITECH 2023 Forum. AIAA 2023-1627. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1627
• 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, Hang, Yixiang Xu, Donglei Sun, Xinmin Chen, and Boyang Chen. 2025. “Design and Flight Test of a Compact and Rapidly-Deployable Air-Launched Inflatable-Winged Aircraft.” In AIAA SCITECH 2025 Forum. AIAA 2025-1824. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1824
• 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. 1973. Terminal Guidance System. Patent Application Number: US-PATENT-APPL-SN-232021. NASA Flight Research Center. https://ntrs.nasa.gov/citations/19740005307
• 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
• General Dynamics/Astronautics San Diego Ca. 1961. WS 107A-1 Flight Test Working Group, Flight Test Report, Atlas Missile 32E. Defense Technical Information Center. https://doi.org/10.21236/ad0843200
• 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 Diego Ca. 1964. Re-Entry Physics Research. United States Army Missile Command. Defense Technical Information Center. https://doi.org/10.21236/ad0441930
• 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
• “The Generalized Missile Equations of Motion.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_2
• Geng, Z., Roger Xu, and Claire McCullough. 1995. “Missile Control Using the Fuzzy CMAC Neural Networks.” In Guidance, Navigation, and Control Conference. AIAA 1995-3271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3271
• Genova, James J. 2005. Coherent Seeker Guided Antiship Missile Performance Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada430023
• Georgievskiy, P., and V. Levin. 2019. “Thermal Spike Conception for Wave Drag Reduction of Blunt Bodies at Different Supersonic Speeds.” In 31st International Symposium on Shock Waves 2. Springer International Publishing. https://doi.org/10.1007/978-3-319-91017-8_138
• Georgievskiy, P. Yu., and V. A. Levin. 2022. “Equivalence Criterion for a Problem of Wave Drag Reduction of Bodies in Supersonic Flow by “Thermal Spike”.” In International Conference on the Methods of Aerophysical Research (ICMAR). https://doi.org/10.53954/9785604788967_56
• Gerber, John William. n.d. “Logic Design of a Line of Sight Guidance System.” PhD diss., Drexel University. https://doi.org/10.17918/00003304
• Gerisch, Hans, Gerhard Staude, Werner Wolf, and Gerhard Bauch. 2013. “A Three-Component Model of the Control Error in Manual Tracking of Continuous Random Signals.” Human Factors: The Journal of the Human Factors and Ergonomics Society 55 (5): 985–1000. https://doi.org/10.1177/0018720813480387
• Gerstley, J. G., and R. D. Tobin. 1975. Regenerative Cooling Design and Analysis Computer Program. LEW-12110. Rockwell Intern. Corp. https://ntrs.nasa.gov/citations/19750000015
• Ghaffar, Zulkifli Abdul, Salmiah Kasolang, and Ahmad Hussein Abdul Hamid. 2017. “Jet-Swirl Injector Spray Characteristics in Combustion Waste of a Liquid Propellant Rocket Thrust Chamber.” In Engineering and Technical Development for a Sustainable Environment. Apple Academic Press. https://doi.org/10.1201/9781315207322-13
• Ghose, Debasish, and Nobin Paul. 2024. “Qualitative Analysis of Variable Speed Proportional Navigation Guidance Law.” In AIAA SCITECH 2024 Forum. AIAA 2024-1988. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1988
• Ghosh, A. K., Girish Sagoo, and Ankur Singhal. 2023. “Wind Tunnel Investigation of Typical Strategic Missile Configuration at High Angle of Attack.” Journal of Aerospace Sciences and Technologies: 75–81. https://doi.org/10.61653/joast.v58i1.2006.672
• Gibart, Jules. n.d. “Non-Linear Stability of a Liquid Propelled Rocket Engine in Closed Loop Regulation.” PhD diss., université Paris-Saclay. https://doi.org/10.70675/a3daf536z34f7z4ce1zab60z57865f27ae3b
• 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
• Gillespie, W., Jr. 1956. Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration. NACA-RM-L56G24. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19690093428
• 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
• Giragosian, P. 1982. “Aerodynamic Consideration in the Design of a Vertically Launched Advanced Interdiction Missile /VLAIM/.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1340. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1340
• Giragosian, Pakrad. 1992. “Rapid Synthesis for Evaluating Missile Maneuverability Parameters.” In 10th Applied Aerodynamics Conference. AIAA 1992-2615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2615
• Giuliano, Victor J., Timothy G. Leonard, Walter M. Adamski, and Tony S. Kim. 2007. “CECE: A Deep Throttling Demonstrator Cryogenic Engine for NASA’s Lunar Lander.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090028814
• Giuliano, Victor, Timothy Leonard, Randy Lyda, and Tony Kim. 2010a. “CECE: Expanding the Envelope of Deep Throttling in Liquid Oxygen/Liquid Hydrogen Rocket Engines for NASA Exploration Missions.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6724
• Giuliano, Victor J., Timothy G. Leonard, Randy T. Lyda, and Tony S. Kim. 2010b. “CECE: Expanding the Envelope of Deep Throttling Technology in Liquid Oxygen/Liquid Hydrogen Rocket Engines for NASA Exploration Missions.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20100032918
• Giurgiutiu, Victor, and Radu Pomirleanu. 2000. Smart-Material Actuated Missile Flight Control Surfaces Feasibility Study. Defense Technical Information Center. https://doi.org/10.21236/ada384331
• Glenn, Floyd. 1988. “A Human Operator Model Management Environment.” Proceedings of the Human Factors Society Annual Meeting 32 (16): 1046–50. https://doi.org/10.1177/154193128803201611
• Glushko, V. P. 1976. “Development of Liquid-Propellant Rocket Engine Engineering and Its Influence on Science and Technology in the USSR.” In Space Activity Impact on Science and Technology. Elsevier. https://doi.org/10.1016/b978-0-08-020365-2.50007-x
• Gnemmi, Patrick, Reza Adeli, and José Longo. 2008. “Computational Comparisons of the Interaction of a Lateral Jet on a Supersonic Generic Missile.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6883
• Goddard, F. E., Jr. 1957. Effect of Uniformly Distributed Roughness on Turbulent Skin-Friction Drag at Supersonic Speeds. AD-152714. Jet Propulsion Lab., California Inst. of Tech. https://ntrs.nasa.gov/citations/19660084259
• Goertz, Christoph. 1995. “A Modular Method for the Analysis of Liquid Rocket Engine Cycles.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-2966. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2966
• Goertzen, L. L. 1972. Altitude-Aided Radar Tracking. Defense Technical Information Center. https://doi.org/10.21236/ad0756655
• 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
• Goldbeck, Robert A., and Felice M. Ferrante. 1981. An Information Processing Model for Predicting Error Detection and Correction: An Analysis of Operator Performance. Defense Technical Information Center. https://doi.org/10.21236/ada105079
• Goldberg, Louis. 1967a. “The Application of Parameter Management to Roll Rate Control in the Ballistic Missile Target System.” In Sounding Rocket Vehicle Technology Specialist Conference. AIAA 1967-1326. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-1326
• 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
• Golodjaev, Aleksandar. 2014. “10.5937/vojtehg62-4806 = Improving the Efficiency of Portable Anti-Aircraft Missile Systems and Air-to-Air Missiles and Newcombat Use of These Missiles.” Vojnotehnicki glasnik 62 (3): 121–27. https://doi.org/10.5937/vojtehg62-4806
• Golovitchev, V. I., and G. Krulle. 1997. “Real Gas Effects Simulation in a Model GH2/O2 Rocket Thrust Chamber.” International Journal of Energetic Materials and Chemical Propulsion: 734–42. https://doi.org/10.1615/intjenergeticmaterialschemprop.v4.i1-6.680
• Gomez, T., V. Flutet, and P. Sagaut. 2009. “Contribution of Reynolds Stress Distribution to the Skin Friction in Compressible Turbulent Channel Flows.” Physical Review E 79 (3): 035301. https://doi.org/10.1103/physreve.79.035301
• Gong, Junfeng, and Fang Wang. 2019. “Simulation of the Store Separation from Internal Weapons Bay Using M_SST DES Model.” Journal of Physics: Conference Series 1215 (1): 012001. https://doi.org/10.1088/1742-6596/1215/1/012001
• Gong, Chen, Wen Chong Xie, and Yong Liang Wang. 2014. “Angle Estimation with Knowledge-Aided Constraint-Based Space-Time Adaptive Monopulse.” Advanced materials research 998-999: 966–70. https://doi.org/10.4028/www.scientific.net/amr.998-999.966
• Gong, Xiaopeng, Qian Zhang, Hao Zhou, Wanchun Chen, and Zhaohui Qi. 2023. “Agile Turn Guidance for Air-to-Air Missile with Linear Gauss Pseudospectral Method.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_197
• Gonzalez, J., and J. Elias. 1978. “Full Scale Correlation of an Effective Thermal Model for Air Launched Supersonic Missile Applications.” In 2nd Thermophysics and Heat Transfer Conference. AIAA 1978-842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-842
• Gonzalez-Martino, Ignacio, Netanel Viner, and Hadar Ben-Gida. 2023. “Very-Large Eddy Simulations of Transonic Flows within a Jet-Fighter Weapon Bay with Internal Store.” In AIAA SCITECH 2023 Forum. AIAA 2023-0057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0057
• 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
• Goodrick, Thomas F. 1969. Wind Effect on Gliding Parachute Systems with Non-Proportional Automatic Homing Control. Defense Technical Information Center. https://doi.org/10.21236/ad0698456
• Goodwin, Frederick K., Marnix F. Dillenius, and Jack N. Nielsen. 1972. Prediction of Six-Degree-of-Freedom Store Separation Trajectories at Speeds up to the Critical Speed. Volume 1. Theoretical Methods and Comparisons with Experiment. Defense Technical Information Center. https://doi.org/10.21236/ada004413
• Goodwin, Frederick K., Jack N. Nielsen, and Marnix F. Dillenius. 1971. A Method for Predicting Three-Degree-of-Freedom Store Separation Trajectories at Speeds up to the Critical Speed. Defense Technical Information Center. https://doi.org/10.21236/ada004771
• 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
• Gordon, Gerald M., and David A. Brown. 1963. Tungsten and Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0296147
• Goswami, Mrinal, Somnath Mahato, Rowdra Ghatak, and Anindya Bose. 2020. “Potential of Multi Constellation Global Navigation Satellite System in Indian Missile Test Range Applications.” Defence Science Journal 70 (6): 682–91. https://doi.org/10.14429/dsj.70.15570
• Goto, Keita, Katsuyuki Nakayama, Motohiro Oshima, and Yoshitaka Sakamura. 2021. “On the Accuracy of Wave Drag Acting on a Supersonic Moving Body Predicted by the Overset Grid Method Implemented in OpenFOAM.” Proceedings of Conference of Hokuriku-Shinetsu Branch 2021.58 (0): G011. https://doi.org/10.1299/jsmehs.2021.58.g011
• 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
• Gour, Saroj K., Debasish Ghose, and Vengadarajan Aki. 2015. “A Novel IEG Strategy for Realistically Modeled Seeker-Less Interceptors.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0343
• Govindaraj, T., and C. M. Mitchell. 1994. Operator Modeling in Commerical Aviation: Cognitive Models, Intelligent Displays, and Pilot’s Assistants. NASA-CR-198609. NASA. https://ntrs.nasa.gov/citations/19950021782
• Goyne, C., R. Stalker, and A. Paull. 1998. “Shock Tunnel Skin Friction Measurement in a Supersonic Combustor.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-943
• Gözde, Haluk, and Semih Ozden. 2021. “Adaptive True Proportional Navigation Guidance Based on Heuristic Optimization Algorithms.” Defence Science Journal 71 (2): 271–81. https://doi.org/10.14429/dsj.71.16218
• Graefe, A. F., and L. J. Gordon. 1957. Investigation of Liquid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0139048
• 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
• Graham, D. 1967. Effect of Some Control System Nonlinearities on Single Loop Compensatory Tracking. Systems Technology, Inc. https://ntrs.nasa.gov/citations/19680006448
• Graham, Kenneth J. 2010. Mitigation of Fuel Fire Threat to Large Rocket Motors by Venting. Defense Technical Information Center. https://doi.org/10.21236/ada532243
• 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
• Graves, E. B. 1972. Supersonic Aerodynamic Characteristics of a Low-Aspect-Ratio Missile Model with Wing and Tail Controls and with Tails in Line and Interdigitated. NASA-TM-X-2531. NASA. https://ntrs.nasa.gov/citations/19720013321
• Graves, E. B., and R. H. Fournier. 1974. Stability and Control Characteristics at Mach Numbers from 0.20 to 4.63 of a Cruciform Air-to-Air Missile with Triangular Canard Controls and a Trapezoidal Wing. NASA-TM-X-3070. NASA. https://ntrs.nasa.gov/citations/19740025319
• Graves, E., and A. Robins. 1979. “Supersonic Aerodynamic Trade Data for a Low-Profile Monoplanar Missile Conceptair Launched Maneuvering Missile Design.” In 17th Aerospace Sciences Meeting. AIAA 1979-222. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-222
• Gray, J. D. 1965. Laminar Boundary-Layer Separation on Flared Bodies at Supersonic and Hypersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0609841
• 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
• Greatrix, David. 2009. “Parametric Evaluation of Solid Rocket Combustion Instability Behavior.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5251. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5251
• Greatrix, David R. 2013a. “Nonuniform Particle Regression and Solid Rocket Combustion Instability Suppression.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-4082. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4082
• Greatrix, David R. 2013b. “Uniform Particle Regression and Solid Rocket Combustion Instability Suppression.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-4081. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4081
• Greatrix, David R. 2014. “Use of Reactive Particles for Solid Rocket Combustion Instability Suppression.” In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2014-3493. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-3493
• Greatrix, David R. 2018. “LF and HF Combustion Instability in Hybrid Rocket Engines.” In 2018 Joint Propulsion Conference. AIAA 2018-4527. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4527
• Greatrix, David R. 2021. “Scale Effects on Solid Rocket Combustion Instability Behaviour.” Preprint, Ryerson University. https://doi.org/10.32920/14638521.v1
• Green, Brian, Theresa Buchanan, and Amy D’Agostino. 2025. “Assessing Independence from Human Performance: Considerations for Functional Requirements Analysis and Function Allocation.” In Nuclear Plant Instrumentation and Control & Human-Machine Interface Technology (NPIC&HMIT 2025). American Nuclear Society. https://doi.org/10.13182/xyz-46591
• Greenwood, T., R. Prozan, A. Ratliff, and D. Seymour. 1970. “Analysis of Liquid Rocket Propellant Engine Exhaust Plumes.” In 5th Thermophysics Conference. AIAA 1970-844. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-844
• Gregoire, J. 1983. “Pan Air versus S/HABP: An Evaluation of Two Diverse Approaches to Supersonic Missile Aerodynamic Analysis.” In 21st Aerospace Sciences Meeting. AIAA 1983-8. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-8
• Gregoire, J., and R. Krieger. 1980. “Aerodynamic Trades Leading to the Development of an Advanced Airbreathing Missile Concept.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1577
• 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
• Grenda, J., S. Venkateswaran, and C. Merkle. 1991. “Liquid Rocket Combustion Instability Analysis by CFD Methods.” In 27th Joint Propulsion Conference. AIAA 1991-2085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2085
• Grey, Jerry. 1953. Combustion Instability in Liquid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0036007
• 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
• Grigsby, Carl E. 1952a. Tests at Mach Number 1.62 of a Series of Missile Configurations Having Tandem Cruciform Lifting Surfaces. NACA-RM-L51J15. NASA. https://ntrs.nasa.gov/citations/19930087120
• Grigsby, Carl E. 1952b. The Use of the Rolled-up Vortex Concept for Predicting Wing-Tail Interference and Comparison with Experiment at Mach Number of 1.62 for a Series of Missile Configurations Having Tandem Cruciform Lifting Surfaces. NACA-RM-L52H05. NASA. https://ntrs.nasa.gov/citations/19930087562
• 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
• Grimm, W. 1993. “On Ascent Guidance of a Hypersonic Vehicle.” In Automatic Control in Aerospace 1992. Elsevier. https://doi.org/10.1016/b978-0-08-041715-8.50072-9
• Grismer, Matthew, Don Kinsey, and Deborah Grismer. 2000. “Hinge Moment Predictions Using CFD.” In 18th Applied Aerodynamics Conference. AIAA 2000-4325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4325
• Gros, Charles G. 1963. Aerodynamic Heating and Other Parameters Affecting Space Vehicle Operations: An Annotated Bibliography. Defense Technical Information Center. https://doi.org/10.21236/ad0436090
• Grosdemange, Herve, and Guy Schaeffer. 1990. “The SEPR 844 Reusable Liquid Rocket Engine for Mirage Combat Aircraft.” In 26th Joint Propulsion Conference. AIAA 1990-1835. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-1835
• Gross, Klaus W. 1987. “Liquid Engine Jet Atomization Workshop Report.” In Johns Hopkins Univ., The 24th JANNAF Combustion Meeting, Volume 2. https://ntrs.nasa.gov/citations/19880016200
• Grossman, A., and A. Kul. 2005. Evolution of Fuel-Air and Contaminant Clouds Resulting from a Cruise Missile Explosion Scenario. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/877894
• “Ground Target Tracking with STAP Radar: Selected Tracking Aspects.” 2004a. In Applications of Space-Time Adaptive Processing. Institution of Engineering and Technology. https://doi.org/10.1049/pbra014e_ch15
• “Ground Target Tracking with STAP Radar: The Sensor.” 2004b. In Applications of Space-Time Adaptive Processing. Institution of Engineering and Technology. https://doi.org/10.1049/pbra014e_ch14
• Groutage, F. D. 1977. Radome Development for a Broadband RF Missile Sensor (Multilayered Power Series Radome with Integrated Lens Provides Excellent Drag Characteristics and Electrical Boresight Error Performance). Defense Technical Information Center. https://doi.org/10.21236/ada038262
• Groves, Arthur D. 1975. A Kill Probability Model for a Multiple-Burst Attack of a Vehicle, Where the Probability of Igniting Spilled Fuel Is Time Dependent. Defense Technical Information Center. https://doi.org/10.21236/ada024793
• Grubin, C., P. Shultz, and R. Soufl. 1964. “A Boost Guidance Scheme for Following a Trajectory Profile and Satisfying Injection Constraints.” In Astrodynamics Guidance and Control Conference. AIAA 1964-639. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-639
• Grundler, Alexander, and Martin Dazer. 2023. “Consideration of Uncertainty in Reliability Demonstration Test Planning.” In European Safety and Reliability Conference (ESREL). https://doi.org/10.3850/978-981-18-8071-1_p166-cd
• Grundler, Alexander, Martin Dazer, Thomas Herzig, and Bernd Bertsche. 2021. “Efficient System Reliability Demonstration Tests Using the Probability of Test Success.” In European Safety and Reliability Conference (ESREL). https://doi.org/10.3850/978-981-18-2016-8_317-cd
• Gschwind, Robert T. 1976. Control Dynamics of Human Tracking with a Viscously Damped Tracking Aid. Defense Technical Information Center. https://doi.org/10.21236/ada035455
• Gu, H. 2002. “Radar Angle-Tracking System for Multiple Moving Targets.” IEE Proceedings - Radar, Sonar and Navigation 149 (1): 23–28. https://doi.org/10.1049/ip-rsn:20020223
• Gu, Guohua, Gang Cheng, Chenjun Zhang, and Lei Zhou. 2017. “Study on Miss Distance Based on Projectile Shock Wave Sensor.” In AIP Conference Proceedings, vol. 1839. Author(s). https://doi.org/10.1063/1.4982480
• Gu, Jihong, Jiaxuan Wang, Jie Kang, Jiamin Shi, Zhaoyuan Wang, and Dazhi Ding. 2025. “A CM-Based Fast Computation Method for the Angular Glint Feature of Multiple Objects.” Radio Science 60 (6): e2025RS008245. https://doi.org/10.1029/2025rs008245
• 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. 2014a. “Supersonic Wing-Body Wave Drag Co-Ordinated Optimisation Based on FCE Methodology.” Aeronautical Journal 118 (1209): 1359–72. https://doi.org/10.1017/s0001924000010010
• Guédon, Olivier, Jean-Louis Vercher, and Gabriel M. Gauthier. 1995. “Human Operator Adaptation to a New Visuo-Manual Relationship.” In Analysis, Design and Evaluation of Man–Machine Systems 1995. Elsevier. https://doi.org/10.1016/b978-0-08-042370-8.50015-x
• Guelman, Mauricio. 1974. The Closed Form Solution of True Proportional Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada048008
• Guelman, M. 1990. “The Stability of Proportional Navigation Systems.” In Guidance, Navigation and Control Conference. AIAA 1990-3380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3380
• Guercio, Joseph G., and Robert L. Wall. 1972. “Congruent and Spurious Motion in the Learning and Performance of a Compensatory Tracking Task.” Human Factors: The Journal of the Human Factors and Ergonomics Society 14 (3): 259–69. https://doi.org/10.1177/001872087201400307
• Guesalaga, Andres, and Sebastian Tepper. 1999. “Improved AGC Design for Scan Tracking Radar Using H-∞.” In SPIE Proceedings, vol. 3692, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.352883
• “Guidance Law Performance Analysis under Stochastic Inputs.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-10
• “Guidance Laws for Boost-Phase Interceptors Launched from UAVs.” 2011. In Guidance of Unmanned Aerial Vehicles. CRC Press. https://doi.org/10.1201/b10807-14
• 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
• Gulko, Vladimir L., and Alexander A. Mescheryakov. 2026. “Monopulse Polarization-Amplitude Method for Estimating an Aircraft’s Pitch Angle.” Radioelectronics. Nanosystems. Information Technologies. 18 (5): 541. https://doi.org/10.17725/j.rensit.2026.18.541
• 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, Xiao-chuan, Gui-ming Cheng, Lei-lei Chang, Qi Xiong, and Xiao-mei Shi. 2017. “Operational Effectiveness Evaluation of Missile Weapon Based on Information Entropy.” In Artificial Intelligence Science and Technology. WORLD SCIENTIFIC. https://doi.org/10.1142/9789813206823_0058
• Guo, Dong, Min Gong, Feng Gao, Xiwang Dong, and Zhang Ren. 2021b. “Attitude/Parameter Coupling Modeling and Sliding Mode Control System Design for Hyper-Glide Vehicle.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_430
• Guo, Bin, Yafei Lu, Bo Wang, Qingyang Chen, and Peng Wang. 2024. “Launch Trajectory Simulation and Flight Experiment of Small Air-Launched UAV.” In First Aerospace Frontiers Conference (AFC 2024), edited by Han Zhang. SPIE. https://doi.org/10.1117/12.3032413
• Guo, Qi, Yuxiang Nan, Baokui Geng, Zijian Ni, and Wei Wang. 2025c. “Event-Triggered Predefined-Time Cooperative Guidance Law with Impact Angle Constraint.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2224-5_36
• Guo, Zichun, Le Wang, Jianxiang Xi, Miao Zhao, and Mingxing Qin. 2025d. “Impact Time Proportional Navigation Guidance for Hypersonic Flight Vehicles Based on DFNN.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2232-0_40
• Guo, Yuchao, Chaofeng Zhang, Xiangyan Xu, Liang Chang, and Xiaohua Nie. 2025b. “Development of Software for Coupling Analysis of Aerodynamic Heating and Transient Heat Transfer.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-3007-6_39
• Guodong, Qi, Yu Jianqiao, Ai Xiaolin, and Jiang Jun. 2019. “Multi-Missile Coordination High Precision Guidance and Control Method for Beam-Riding Guidance.” Journal of Physics: Conference Series 1215 (1): 012013. https://doi.org/10.1088/1742-6596/1215/1/012013
• 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, 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
• Gupta, N., B. Sridhar, and J. Fuller. 1979. “Development and Implementation of Missile Guidance Laws Based on Command Constraint Concepts.” In Guidance and Control Conference. AIAA 1979-1737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1737
• Gur, I., J. Shinar, and J. Rom. 1978. “Prediction of Roll-Controllability of Slender Cruciform Canard Configurations.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1338
• Gurfil, Pini. 2001c. “Zero-Miss-Distance Guidance Law Based on Line-of-Sight Rate Measurement Only.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4277
• Gurfil, Pini. 2012. “Neoclassical Missile Guidance.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-8
• Gutman, Shaul. 2011. “Nose Jet Guidance and Control for Exoatmospheric Kill-Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6568. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6568
• Gutman, Shaul, and Orly Ben-Aharon. 2006. “Agility vs. Stability in Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6433
• Gutman, Shaul, and Orly Goldan. 2011. “Adjoint Stability and Miss-Distance in Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6417. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6417
• Gutman, Shaul, and Orly Goldan Ben-Aharon. 2009. “Optimal Guidance: A Guaranteed Miss Approach.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5894
• Gutman, Oren, and Zalman Palmor. 2010. “Proportional Navigation against Multiple Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8183
• 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
• Głębocki, Robert, and Mariusz Jacewicz. 2018. “Simulation Study of a Missile Cold Launch System.” Journal of Theoretical and Applied Mechanics: 901. https://doi.org/10.15632/jtam-pl.56.4.901
• Haber, Jerold M. 1995. “Risk Acceptability: Space and Missile Launch Hazards.” In Risk and Safety Assessments: Building Viable Solutions. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0445
• Habiballah, M., I. Dubois, L. Vingert, D. Lourme, and D. Scherrer. 1992. “High Frequency Combustion Instability in Liquid Propellant Rocket Engines: A Review of Studies Carried out at ONERA for the Ariane Launcher.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-774. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-774
• Hablani, Hari. 1998. “Gaussian Second-Order Filter for Proportional Navigation of Exoatmospheric Interceptors with Angles-Only Measurements.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4217
• Hacısalihzade, Selim S. 2013. “The Human Operator.” In Lecture Notes in Control and Information Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-37279-7_3
• Haga, Takanori. 2024. Liquid Rocket Engine Combustor Simulations by Flamelet-Based Model and Flux-Reconstruction Method. https://doi.org/10.52843/cassyni.t07j48
• Hagemann, Gerald, Dieter Preclik, Ludwig Brummer, et al. 2006. “TEKAN 2010: Thrust Chamber Technologies for Liquid Rocket Propulsion.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4362. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4362
• Haglind, Fredrik, Henrik Edefur, and Stefan Olsson. 2007. “Design of a Solid Propellant Air Turbo Rocket for a Tactical Air-Launched Missile.” In Volume 1: Turbo Expo 2007. ASMEDC. https://doi.org/10.1115/gt2007-27826
• Haglund, Nils, Torre Jr., and James P. 1978. Prediction of Target Travel during Missile Time of Flight. a Computer Simulation. Defense Technical Information Center. https://doi.org/10.21236/ada059032
• Hahn, Jerry S. 1969. Experimental Investigation of Turbulent Step-Induced Boundary-Layer Separation at Mach Numbers 2.5, 3, and 4. Defense Technical Information Center. https://doi.org/10.21236/ad0683767
• Hahn, P. 1974. “On Some Anomalies Involving Structural Dynamics in the Design of theSAM-D Flight Vehicle Autopilot.” In Mechanics and Control of Flight Conference. AIAA 1974-912. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-912
• Haines, A. B., and Marylyn E. Wood. 1987. “Experience with Prediction Techniques for Store Installed Drag and Store Release Characteristics.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/871795
• Hald, Hermann. 2003. “CMC Rocket Combustion Chamber with Effusion Cooling.” In 54th 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-03-s.p.22
• Hale, Amory D. 1978. “Optical Data Conversion Program 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/10.1117/12.956105
• Hale, Errol, Michael J. Candon, Andrea Da Ronch, Vincenzo Muscarello, and Pier Marzocca. 2026. “Identification of Low-Order Unsteady Aerodynamic Models for Store Release in Transonic Flow.” In AIAA SCITECH 2026 Forum. AIAA 2026-2704. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2704
• Hale, J. P., II. 1992. Anthropomorphic Teleoperation: Controlling Remote Manipulators with the DataGlove. NASA-TM-103588. NASA. https://ntrs.nasa.gov/citations/19920019278
• 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, 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, Stephen L. 2003. “Multisensor Target and Missile Tracking for a Point Defense Missile System.” In SPIE Proceedings, vol. 5082, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.487070
• Hall, Les. 2004. “Simulation of Missile with Spinning Tail Fin Using Chimera Moving Body Methodology.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1249. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1249
• 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
• Hallberg, Eric, and William Godiksen. 2007. “MATLAB Based Telemetry Integration Utility for Store Separation Analysis.” In 2007 U.S. Air Force T&E Days. AIAA 2007-1643. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1643
• Haller, Piroska, Lőrinc Márton, Zoltán Szántó, and Tamás Vajda. 2015. “Bilateral Teleoperation in the Presence of Jitter: Communication Performance Evaluation and Control.” In Studies in Systems, Decision and Control. Springer International Publishing. https://doi.org/10.1007/978-3-319-26327-4_12
• Halter, Megaera, and Eugene Cliff. 1991. “Optimal Energy-Heading Transients for an Airbreathing Hypersonic Vehicle.” In Navigation and Control Conference. AIAA 1991-2713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2713
• Hampsten, Kenneth R. 1996. “An Air Launched, Highly Responsive Military Transatmospheric Vehicle (TAV), Based on Existing Aerospace Systems.” In AIP Conference Proceedings, vol. 361. AIP. https://doi.org/10.1063/1.49958
• Han, Lit S. 1960. “An Approximate Analysis of the Influence of Aerodynamic Heating and Initial Twist on the Torsional Stiffness of Thin Wings.” Journal of Applied Mechanics 27 (2): 332–34. https://doi.org/10.1115/1.3643961
• Han, Poong-Gyoo. 2004. “Evaluation on the Regenerative Cooling Characteristics in Liquid Rocket Engine of 10tf-Thrust Using Kerosene and Liquid Oxygen as a Propellant.” Journal of the Korean Society for Aeronautical & Space Sciences 32 (4): 111–17. https://doi.org/10.5139/jksas.2004.32.4.111
• Han, Junhao, Lin He, and Zhengbang Wu. 2022. “Experimental Investigation on Evolution Characteristics of High- and Low-Speed Streaks in Supersonic Turbulent Boundary Layer.” AIP Advances 12 (11): 115204. https://doi.org/10.1063/5.0121259
• Han, Poong-Gyoo, Seong-Woong Lee, Kyoung-Ho Kim, and Youngbin Yoon. 2004. “Performance Analysis of the Thrust Chamber in Liquid Rocket Engine Using Liquefied Natural Gas as a Fuel.” In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2004-3860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-3860
• Han, Yinghong, Su Meng, Zeyu Xu, et al. 2021a. “Analysis of Missile-Born Cooperative Data Link.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-6324-6_34
• Han, Seoeum, Yoonsik Park, Seulki Hong, and Bok-Jik Lee. 2023. “A Comparison Study of Aerodynamics Calculation Methods with Deformation of the Missile Nose.” Journal of Computational Fluids Engineering 28 (1): 44–52. https://doi.org/10.6112/kscfe.2023.28.1.044
• Han, Seul-Ki, Won-Sang Ra, Ick-Ho Whang, and Jin Bae Park. 2016a. “Geometric Joint Probabilistic Data Association Approach to Ballistic Missile Warhead Tracking Using FMCW Radar Seeker.” IET Radar, Sonar & Navigation 10 (8): 1422–30. https://doi.org/10.1049/iet-rsn.2015.0510
• 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
• Han, Ding, Xiao-liang Wang, Ming Zhao, and Deng-ping Duan. 2016b. “An Improved Proportional Navigation Guidance Law for Waypoint Navigation of Airships.” In Advances in Intelligent Systems and Computing. Springer International Publishing. https://doi.org/10.1007/978-3-319-38789-5_46
• Han, Sook Hyun, Won Young Yun, and Sun Keun Seo. 2021b. “Economic Design of a Zero-Failure Reliability Demonstration Test Considering Capacity Limitation of Test Equipment.” Journal of Korean Society for Quality Management 49 (3): 341–58. https://doi.org/10.7469/jksqm.2021.49.3.341
• Hancock, P. A., and S. F. Scallen. 1996. “The Future of Function Allocation.” Ergonomics in Design: The Quarterly of Human Factors Applications 4 (4): 24–29. https://doi.org/10.1177/106480469600400406
• 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
• Hankins, R. 1986. “Development Status of the Transtar Pump-Fed Storable Propellant Rocket Engine.” In 22nd Joint Propulsion Conference. AIAA 1986-1572. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-1572
• Hanson, Charles A. 1963. Flight Article Mass Properties Report for Minuteman Wing II Components for Missile 739-786. Defense Technical Information Center. https://doi.org/10.21236/ad0408958
• Hanson, Curtis E. 2012. An Ad-Hoc Adaptive Pilot Model for Pitch Axis Gross Acquisition Tasks. NASA/TM-2012-216031. NASA. https://ntrs.nasa.gov/citations/20150000179
• Hanson, P. W., D. J. Martin, and A. G. Rainey. 1966. Investigation of the Divergence Characteristics of Delta-Planform Canard Controls. NASA-TR-R-235. NASA. https://ntrs.nasa.gov/citations/19660011754
• 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
• Hardesty, Donald R. 1970. Unsteady Combustion in Gaseous Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0726118
• Hardgrove, J., and H. Krieg Jr. 1984. “High Performance Throttling and Pulsing Rocket Engine.” In 20th Joint Propulsion Conference. AIAA 1984-1254. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1254
• Harding, Gregory, and Kyle Barton. 2007. “Predicting Aircraft Flowfield Induced Water Vapor Condensation for Store Separation Flight Tests.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4169
• Hardtla, John, Kevin Milligan, and Evin Cramer. 1987. “Design and Implementation of a Missile Guidance Law Derived from Modern Control Theory.” In Guidance, Navigation and Control Conference. AIAA 1987-2447. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2447
• Hardy, G. 1969. “Man’s Role in Launch Vehicle Guidance and Control.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-876. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-876
• 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
• Harish, G., M. Pavanakumar, and K. Anandhanarayanan. 2006. “Store Separation Dynamics Using Grid-Free Euler Solver.” In 24th AIAA Applied Aerodynamics Conference. AIAA 2006-3650. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-3650
• 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
• Harmon, Bruce, and Lisa Ward. 1990. “Schedule Estimating Relationships for Air-Launched Missiles.” In Cost Analysis and Estimating. Springer New York. https://doi.org/10.1007/978-1-4612-0995-9_6
• Harper, Brent, L. Renea Ellison, and Marlow D. Moser. 2004. Combustion Instability Analysis and the Effects of Drop Size on Acoustic Driving Rocket Flow. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20040075603
• 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
• Harris, Thomas A. 1935. Reduction of Hinge Moments of Airplane Control Surfaces by Tabs. NACA-TR-528. Langley Memorial Aeronautical Laboratory. https://ntrs.nasa.gov/citations/19930091601
• Harris, Charles. 1963. Development of Nondestructive Testing Techniques for Large Solid-Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0402393
• Harris, Steven D. 1978. Human Performance in Concurrent Verbal and Tracking Tasks: A Review of the Literature. Defense Technical Information Center. https://doi.org/10.21236/ada060493
• Harris, Steven D., Jerry M. Owens, and Robert A. North. 1979. Human Performance in Time-Shared Verbal and Tracking Tasks. Defense Technical Information Center. https://doi.org/10.21236/ada070275
• Harris, Robert S., Jr., and John R. Davidson. 1961. An Analysis of Exact and Approximate Equations for the Temperature Distribution in an Insulated Thick Skin Subjected to Aerodynamic Heating. L-721. NASA Langley Research Center. https://ntrs.nasa.gov/citations/20010125633
• Harris, Robert S., Jr., and John R. Davidson. 1962. Methods for Determining the Optimum Design of Structures Protected from Aerodynamic Heating and Application to Typical Boost-Glide or Reentry Flight Paths. NASA-TN-D-990. NASA. https://ntrs.nasa.gov/citations/19980227826
• Harrison, Michael D. n.d. “Scenarios, Function Allocation and Human Reliability.” In Lecture Notes in Control and Information Sciences. Springer London. https://doi.org/10.1007/bfb0110454
• Harrje, David T. 1959. Combustion Instability in Liquid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0212816
• Harrje, D. T. 1972. Liquid Propellant Rocket Combustion Instability. NASA-SP-194. NASA. https://ntrs.nasa.gov/citations/19720026079
• Harrje, David T., and William A. Sirignano. 1966. Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors Sixth Yearly Progress Report, 1 Jun. 1965: 31 May 1966. NASA-CR-77672. NASA. https://ntrs.nasa.gov/citations/19660026500
• Harrje, D. T., W. A. Sirignano, and W. C. Strahle. 1962. Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors. Second Yearly Progress Report for the Period 1 June 1961 to 31 May 1962. AERONAUTICAL ENG. REPT.-533B. Princeton Univ. https://ntrs.nasa.gov/citations/19620003967
• Hartman, Edward R., and Patrick J. Johnston. 1987. Mach 6 Experimental and Theoretical Stability and Performance of a Cruciform Missile at Angles of Attack up to 65 Degrees. NASA-TP-2733. NASA. https://ntrs.nasa.gov/citations/19870014159
• Hartman, Richard D., Frederick H. Lutze, and Eugene M. Cliff. 1991. “Time-Optimal Maneuver Guidance Design with Sensor Line-of-Sight Constraint.” In SPIE Proceedings, vol. 1478, edited by Jack F. Wade, Avi Tuchman. SPIE. https://doi.org/10.1117/12.45623
• Harvazinski, Matthew E., and Tomas Houba. 2022. “Conjugate Heat Transfer Analysis of the Wall Heat Flux in a Liquid Rocket Engine.” In AIAA SCITECH 2022 Forum. AIAA 2022-0069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0069
• Harvazinski, Matthew E., Cheng Huang, Venkateswaran Sankaran, et al. 2013. “Combustion Instability Mechanisms in a Pressure-Coupled Gas-Gas Coaxial Rocket Injector.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3990. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3990
• Harvazinski, Matthew E., Ranjan Mehta, and Vinod Venugopalan. 2024. “Liquid Rocket Engine Combustion Simulations with Radiation Heat Transfer.” In AIAA SCITECH 2024 Forum. AIAA 2024-0149. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0149
• Harvazinski, Matthew E., Venkateswaran Sankaran, and Douglas G. Talley. 2014. Effect of Swirl on an Unstable Single-Element Gas-Gas Rocket Engine. Defense Technical Information Center. https://doi.org/10.21236/ada611028
• Harvey, D. 1970. “Throttling Venturi Valves for Liquid Rocket Engines.” In 6th Propulsion Joint Specialist Conference. AIAA 1970-703. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-703
• Hashtrudi-Zaad, Keyvan, and Septimiu E. Salcudean. 1999. “Bilateral Parallel Force/Position Teleoperation Control.” In Dynamic Systems and Control. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1999-0046
• 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
• Hauser, H. A., and W. E. Helfrich. 1963. Research and Development of Titanium Rocket Motor Case. Defense Technical Information Center. https://doi.org/10.21236/ad0406781
• Hausl, Κ. 1990. “Stabilität Und Treffergenauigkeit Eines Digitalen Lenksystems Mit Kaiman-Filter / Stability and Miss Distance of a Digital Guidance System with Kaiman Filter.” auto 38 (1–12): 161–67. https://doi.org/10.1524/auto.1990.38.112.161
• Hawley, John K., and Anna L. Mares. 2006. Developing Effective Human Supervisory Control for Air and Missile Defense Systems. Defense Technical Information Center. https://doi.org/10.21236/ada444786
• Hayashi, Kentaro, and Shigeru Aso. 2003. “Effect of Pressure Ratio on Aerodynamic Heating Reduction Due to Opposing Jet.” In 36th AIAA Thermophysics Conference. AIAA 2003-4041. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4041
• Haykin, S., and J. P. Reilly. 1982. “Maximum-Likelihood Receiver for Low-Angle Tracking Radar. Part 1: The Symmetric Case.” IEE Proceedings F Communications, Radar and Signal Processing 129 (4): 261. https://doi.org/10.1049/ip-f-1.1982.0039
• Haykin, S., J. Reilly, and D. Taylor. 1980. “New Realisation of Maximum Likelihood Receiver for Low-Angle Tracking Radar.” Electronics Letters 16 (8): 288–89. https://doi.org/10.1049/el:19800210
• Haynes, Anthony. 2008. Low Cost Zinc Sulfide Missile Dome Manufacturing. Defense Technical Information Center. https://doi.org/10.21236/ada480194
• 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
• Hazelton, David, Rodney Bowersox, and Joseph Schetz. 1996. “Directional Skin Friction Measurements in a High Enthalpy Supersonic Flow about a Sharp Fin.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-4503. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-4503
• He, Xiaoliang. 2015. “Target Tracking Algorithm of Ballistic Missile in Boost Phase Based on Ground-Based Radar Systems.” Journal of Information and Computational Science 12 (2): 855–64. https://doi.org/10.12733/jics20105682
• He, Shaoming, Chang-Hun Lee, Hyo-Sang Shin, and Antonios Tsourdos. 2020a. “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, S., and D. Lin. 2016. “Sliding Mode-Based Continuous Guidance Law with Terminal Angle Constraint.” Aeronautical Journal 120 (1229): 1175–95. https://doi.org/10.1017/aer.2016.50
• 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, Zheng, Zaicheng Wang, Yubiao Wei, and Hui Kang. 2024a. “Evaluation of Multi-Munition Joint Damage Effects on Command Vehicle of Missile Position.” Journal of Physics: Conference Series 2891 (14): 142018. https://doi.org/10.1088/1742-6596/2891/14/142018
• He, Jia, Hua Zhou, Wengang Xu, Bo Ji, and Xiaoli Chen. 2024b. “Infrared Polarization Imaging Test of Typical Background in Missile Range.” In Sixth Conference on Frontiers in Optical Imaging and Technology: Imaging Detection and Target Recognition, edited by Jiangtao Xu, Chao Zuo. SPIE. https://doi.org/10.1117/12.3016149
• Headrick, J. M., E. W. Ward, and D. L. Lucas. 1966. Information on over-the-Horizon Radar. Part 9. Missile Detection at Altitude. Defense Technical Information Center. https://doi.org/10.21236/ada472351
• Headrick, J. M., E. W. Ward, and D. L. Lucas. 1967. Information on over-the-Horizon Radar. Part 12. Missile Detection at Altitude for a Medium Distance. Defense Technical Information Center. https://doi.org/10.21236/ada472379
• Heat Transfer in Rocket Engine Combustion Chambers and Regeneratively Cooled Nozzles. 1993. NASA-CR-193949. NASA. https://ntrs.nasa.gov/citations/19940019998
• Hecht, C. 1991. “Homing Guidance Using Angular Acceleration of the Line of Sight.” In Navigation and Control Conference. AIAA 1991-2701. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2701
• Heilig, Paul T. 1979. Navy Air-Launched Missile Operating and Support Cost Estimating Model. Defense Technical Information Center. https://doi.org/10.21236/ada069527
• 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
• Heister, Stephen. 2008. Modeling Liquid Rocket Engine Atomization and Swirl/Coaxial Injectors. Defense Technical Information Center. https://doi.org/10.21236/ada494724
• Helfman, Richard A., John C. Saccenti, Richard E. Kinsler, and J. R. Suckling. 1985. An Expert System for Predicting Component Kill Probabilities. Defense Technical Information Center. https://doi.org/10.21236/ada161827
• Heller, Carmit, Isaac Yaesh, Joseph Ben-Asher, and Iian Rusnak. 2009. “Lq-Optimal Missile Guidance and Its Relation to Mixed L2/Lq Laws.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5895. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5895
• 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, M., and J. Nielsen. 1982. “The Equivalent Angle-of-Attack Method for Estimating the Nonlinear Aerodynamic Characteristics of Missile Wings and Control Surfaces.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1338. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1338
• Hemsch, M., and J. Nielsen. 1983. “Aerodynamic Characteristics of Missile Control Fins in Nonlinear Flow Fields.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2083
• Hemsch, Michael J., and Jack N. Nielsen. 1986. Tactical Missile Aerodynamics. PRC Kentron, Inc. https://ntrs.nasa.gov/citations/19870035652
• Hemsch, M., J. Nielsen, C. Smith, and S. Perkins Jr. 1977. “Component Aerodynamic Characteristics of Banked Cruciform Missiles with Arbitrary Control Deflections.” In Guidance and Control Conference. AIAA 1977-1153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-1153
• Hender, D. 1982. “Elastomer Thermal Response in an Aerodynamic Heating Environment.” In 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference. AIAA 1982-860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-860
• Hender, D., and C. Okabe. 1983. “Expanded Uses of Infrared Scanning Data in Aerodynamic Heating Materials Tests.” In 18th Thermophysics Conference. AIAA 1983-1542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1542
• Hendrick, P., and M. Saint-Mard. 1999. “Subsonic in-Flight LOX Collection for an All-Rocket Air-Launched Orbiter.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2351
• Henke, D., and R. Nerem. 1968. “Theoretical and Experimental Studies of Supersonic Turbulent Wakes and Parachute Performance.” In 2nd Aerodynamic Deceleration Systems Conference. AIAA 1968-947. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-947
• Henning, Allen B. 1959. Stability Characteristics of Two Missiles of Fineness Ratios 12 and 18 with Six Rectangular Fins of Very Low Aspect Ratio over a Mach Number Range of 1.4 to 3.2. NASA-MEMO-12-2-58L. NASA. https://ntrs.nasa.gov/citations/19980228138
• Herbertz, Armin, Markus Ortelt, Ilja Müller, and Hermann Hald. 2012. “Transpiration Cooled Ceramic Thrust Chamber Applicability for High-Thrust Rocket Engines.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-3990. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3990
• Herbertz, Armin, and Markus Selzer. 2012. “Systems Analysis of a LOX/LH2 Rocket Engine with a Transpiration-Cooled Ceramic Thrust-Chamber.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-3989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3989
• Herman, Ronald, and Joseph Butler. 1992. “Subsystems for the Extended Range Interceptor (ERINT-1) Missile.” In Annual Interceptor Technology Conference. AIAA 1992-2750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2750
• Hermance, Clarke E. 1961. Comparison of Solid Propellant Burning Rates in Strands and Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0261589
• 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
• Hershey, A. V., and G. E. Vibrane. 1961. Review of Data on Induced Mass and Drag of the Finner Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0724292
• Hessman, F. 1979. “Induced Roll Technology for Missile Configurations with Forward Surfaces.” In 17th Aerospace Sciences Meeting. AIAA 1979-223. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-223
• Hessman, F. 1982. “High Angle of Attack Aerodynamic Characteristics for a Finless TVC Missile Configuration.” In 9th Atmospheric Flight Mechanics Conference. AIAA 1982-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1337
• Hexner, Gyorgy, and Aaron Pila. 2010. “A Practical Stochastic Optimal Guidance Law for a Bounded Acceleration Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8054. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8054
• Hickey, James R. 1975. Development of a Low Cost Molded Plastic Missile/RPV Control Surface Actuator. Defense Technical Information Center. https://doi.org/10.21236/ada026700
• Hicks, W., and E. Greenberg. 1981. “Flight Testing of the AIM/RIM-7M Missile, Preflight Analysis.” In 1st Flight Test Conference. AIAA 1981-2385. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2385
• Hicks, Jamison, Michael Lewis, and Katia Sycara. 2023. Report on Human Factors Issues Likely to Affect Air-Launched Effects/Autonomous Loitering Effects (ALE). DEVCOM Analysis Center. https://doi.org/10.21236/ad1215148
• Hiền, Vũ Anh, Huu Phuong Tran, Van Tuan Bui, and Dang Hung Nguyen. 2022. “A method for measure command coefficient from ground control station of close-range guided anti-tank missile with intergrated circuit.” Journal of Military Science and Technology, no. FEE2022: 17. https://doi.org/10.54939/1859-1043.j.mst.fee.2022.17-24
• Higgins, Robert W., and Constantine C. Pappas. 1951. An Experimental Investigation of the Effect of Surface Heating on Boundary-Layer Transition on a Flat Plate in Supersonic Flow. NACA-TN-2351. NASA. https://ntrs.nasa.gov/citations/19930083026
• Higgins, M., and R. Speelman III. 1973. “A Stability Analysis of Tandem Parachute Mid-Air Recovery Systems.” In 4th Aerodynamic Deceleration Systems Conference. AIAA 1973-461. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-461
• 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 Video System for Store Separation Testing.” 2019. Aerospace Testing International 2019 (4): 78–78. https://doi.org/10.12968/s1478-2774(22)50436-6
• “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
• Hildebrandt, Michael, and Michael Harrison. 2003. “Putting Time (Back) into Dynamic Function Allocation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 47 (3): 488–92. https://doi.org/10.1177/154193120304700350
• Hill, J. W., and J. C. Bliss. 1972. “A Computer Assisted Teleoperator Control Station with Tactile Feedback.” In NASA, Washington 7th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19730001416
• Hill, S., Jr. 1978. “Wind Tunnel Determination of the Drag of an Advanced Air Breathing Missile.” In 16th Aerospace Sciences Meeting. AIAA 1978-118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-118
• Hinada, Motoki, Yoshifumi Inatani, Takashi Nakajima, and Masahisa Honda. 1991. “Parachute Deployment Experiment in Transonic and Supersonic Wind Tunnels.” In 11th Aerodynamic Decelerator Systems Technology Conference. AIAA 1991-859. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-859
• Hingst, W. R., and C. E. Towne. 1974. Comparison of Theoretical and Experimental Boundary-Layer Development in a Mach 2.5 Mixed-Compression Inlet. NASA-TM-X-3026. NASA. https://ntrs.nasa.gov/citations/19740011800
• Hiraki, Koju, Motoki Hinada, Hiroshi Higuchi, Koju Hiraki, Motoki Hinada, and Hiroshi Higuchi. 1997. “Flow Measurement around Rigid Parachute-like Bodies in Supersonic Free Stream.” In 14th Aerodynamic Decelerator Systems Technology Conference. AIAA 1997-1529. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1529
• 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
• Hirwani, Vijay, and Ashwini Ratnoo. 2018a. “Field-of-View Constrained Polynomial Guidance Law for Dual-Seeker Interceptors.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1325. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1325
• Hirwani, Vijay, and Ashwini Ratnoo. 2018b. “Three-Stage Switched PN Guidance Law for Air-Launched Dual-Seeker Interceptor with Physical Constraints.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1324
• Hitt, Matthew A., Lucas Kalathas, John Coogan, and Nathan Slegers. 2013. “UAH Tactical Missile System Design of a Surface to Air Missile for Missile Defense.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3834. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3834
• 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
• Hoberg, O. A., and J. E. Rorex. 1962. Telemetry Development for Large Guided Missiles and Space Carrier Vehicles. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19630006122
• Hoch, Saul. 1960. Wspacs (Weapon System Programming and Control System) Mod Zero: A Demonstration Model. Defense Technical Information Center. https://doi.org/10.21236/ad0296546
• Hodžić, Mirza, and Naser Prljača. 2024. “Missile Guidance Using Proportional Navigation and Machine Learning.” Journal of Engineering Research and Sciences 3 (3): 19–26. https://doi.org/10.55708/js0303003
• Hoefener, C., and J. Stone. 1981. “Missile Tracking with Global Positioning System /GPS/ Satellites.” In 1st Flight Test Conference. AIAA 1981-2518. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2518
• Hoertel, F. W. 1961. Vapor Deposition of Tungsten on Rocket Nozzle Inserts. Defense Technical Information Center. https://doi.org/10.21236/ad0259441
• Hoff, R. 1967. Time Response Test of Thrust Chamber Thermocouples in Simulated Rocket Firing. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4228957
• Hoffman, William. 1987. “Development Status of the Transtar Pump-Fed Storable Propellant Rocket Engine.” In 23rd Joint Propulsion Conference. AIAA 1987-1937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-1937
• Hoffman, Robert R., and Matthew Johnson. 2019. “The Quest for Alternatives to “Levels of Automation” and “Task Allocation”.” In Human Performance in Automated and Autonomous Systems. CRC Press. https://doi.org/10.1201/9780429458330-3
• Hoffman, J. R., and R. P. S. Mahler. 2002. “Multitarget Miss Distance and Its Applications.” 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.2002.1021144
• Hoffren, Jaakko, and Esa Salminen. 1999. “Affordable Hybrid Simulation for Predicting Store Separation.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4107
• Holden, M. 1984. “Experimental Studies of Surface Roughness Shape and Spacing Effects on Heat Transfer and Skin Friction in Supersonic and Hypersonic Flows.” In 22nd Aerospace Sciences Meeting. AIAA 1984-16. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-16
• Holden, F. M., and S. M. Shinners. 1973. “Identification of Human Operator Performance Models Utilizing Time Series Analysis.” In MIT Proc. of the 9th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19750011078
• 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
• Holley, B., P. Render, and R. Pratt. 1996. “Missile Trajectory Modelling Using the Method of Apparent Masses to Generate Aerodynamic Coefficients.” In 21st Atmospheric Flight Mechanics Conference. AIAA 1996-3394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3394
• Holliday, Mary R. 1989. Methodology of an Event-Driven Monte Carlo Missile Simulation. Defense Technical Information Center. https://doi.org/10.21236/ada601300
• Hollnagel, Erik. 2018. “From Function Allocation to Function Congruence.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9780429460609-3
• Holm-Hansen, Brian, Howard Lee, and Hussein Youssef. 2010. “Neuro-Fuzzy Dynamic Inversion Control for a Hypersonic Cruise Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7868. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7868
• Holst, R., and J. Rogers. 1983. “Pacific Missile Test Center Flight Safety Decision Techniques.” In 2nd Flight Testing Conference. AIAA 1983-2709. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2709
• Holster, J. 1973. “Liquid Rocket Propellant Feedline Dynamics.” In 9th Propulsion Conference. AIAA 1973-1286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1286
• Holzmann, Wilfried A., and Warren R. Hayden. 1988. Integrated Control and Health Management. Orbit Transfer Rocket Engine Technology Program. NASA-CR-182122. NASA. https://ntrs.nasa.gov/citations/19890002434
• “Homing Guidance.” 2014. In Fundamentals of Aerospace Navigation and Guidance. Cambridge University Press. https://doi.org/10.1017/cbo9781107741751.006
• Hong, Ju-Hyeon, and Chang-Kyung Ryoo. 2014. “Compensation of Parasitic Effect in Homing Loop with Strapdown Seeker via PID Control.” In International Conference on Informatics in Control, Automation and Robotics (ICINCO). https://doi.org/10.5220/0005055907110717
• 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, E. 1969. “Use of Preston Tubes for Measuring Hypersonic Turbulent Skin Friction.” In 4th Aerodynamic Testing Conference. AIAA 1969-345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-345
• Hopkins, E. J., and E. R. Keener. 1966. Study of Surface Pitots for Measuring Turbulent Skin Friction at Supersonic Mach Numbers: Adiabatic Wall. NASA-TN-D-3478. NASA. https://ntrs.nasa.gov/citations/19660019925
• Hopkins, E., and E. Keener. 1972. “Pressure-Gradient Effects on Hypersonic Turbulent Skin Friction and Boundary-Layer Profiles.” In 10th Aerospace Sciences Meeting. AIAA 1972-215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-215
• Hopko, Russell N. 1951. A Flight Investigation of the Damping in Roll and Rolling Effectiveness Including Aeroelastic Effects of Rocket Propelled Missile Models Having Cruciform, Triangular, Interdigitated Wings and Tails. NACA-RM-L51D16. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/19680068649
• Horiuchi, S., and N. Yuhara. 1989. “Detection of System Failure by Human Operator — Mathematical Model and Experiments.” In Analysis, Design and Evaluation of Man–Machine Systems 1988. Elsevier. https://doi.org/10.1016/b978-0-08-036226-7.50049-1
• Hornstein, B. 1965. Research Study of Light Emission Caused by Pressure Fluctuations in Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ad0622524
• Horstman, C. C., M. I. Kussoy, and M. J. Lanfranco. 1978. “An Evaluation of Several Compressible Turbulent Boundary-Layer Models Effects of Pressure Gradient and Reynolds Number.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19780057950
• 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
• Hossein, Mohammad, and Hamidreza R. Amindavar. 2012. “Doppler Radar Tracking Using Moments.” In InTech eBooks. https://doi.org/10.5772/37307
• 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
• Hou, Yongjun. n.d. “Stabilization and Control of Teleoperation Systems with Time Delays.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180813-13212
• Hou, Xiaoling. 2024. “Study on Spatial Anti-Jamming of Link-16 Based on Power Inversion.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-4126753/v1
• Houck, Roger D., Brian D. Kelly, and John Wiedemann. 1986. “An Integrated Display for Vertical Situation Awareness in Commercial Transport Airplanes.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/861770
• Houhou, Hatem, Hemza Layachi, and Abd Elmajid Boudjemai. 2020. “Design of the Thrust Chamber: Dimensional Analysis of the Combustion Chamber and the Nozzle of Rocket Engine Using LOX/LCH4 Propellants.” IOP Conference Series: Materials Science and Engineering 715 (1): 012085. https://doi.org/10.1088/1757-899x/715/1/012085
• Houser, Thomas. 1972. Rates and Mechanisms of Reactions of Fluorine Containing Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0752564
• 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
• Howard, Richard, M. Rabang, and Donald Roane Jr. 1989. “Aerodynamic Effects of a Turbulent Flowfield on a Vertically-Launched Missile.” In 27th Aerospace Sciences Meeting. AIAA 1989-329. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-329
• Howe, S. H., and P. W. McCree Jr. 1962. Model and Computer Program for Calculating the Kill Probabilities for Certain Asw Tactics. Defense Technical Information Center. https://doi.org/10.21236/ad0402265
• Howerton, Layton W., Gregory Blaisdell, and Jonathan Poggie. 2024. “Aerodynamic Heating of a Cylinder between Flat Plates.” In AIAA SCITECH 2024 Forum. AIAA 2024-2381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2381
• Howerton, Walter, and Wayne Hathaway. 1994. “Aerodynamic Test and Analysis of a Slender Grooved-Body, Generic Missile Configuration.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3498. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3498
• Howitt, Sara, and Jon Platts. 2002. “Real-Time Deep Strike Mission Simulation Using Air-Launched UAVs.” In 1st UAV Conference. AIAA 2002-3480. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3480
• Howland, P. F. 1999. “Target Tracking Using Television-Based Bistatic Radar.” IEE Proceedings - Radar, Sonar and Navigation 146 (3): 166–74. https://doi.org/10.1049/ip-rsn:19990322
• 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
• Hoyt, Robert. 2006. “Responsive Launch of Small Spacecraft Using Reusable in-Space Tether and Air-Launch Technologies.” In Space 2006. AIAA 2006-7278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7278
• Hozumi, Koichi, Yukimitsu Yamamoto, Alain Masson, Jacques Soutade, Patric Wagner, and Joelle Fontaine. 2001. “A Study for Prediction of Flight Aerodynamic Heating Using HYFLEX Flight and Wind Tunnel Data.” In 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2001-1826. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-1826
• Hsieh, Paul Y. 1961. A Study of the Encapsulation Applicable to Liquid Rocket Fuel. Defense Technical Information Center. https://doi.org/10.21236/ad0265894
• Hu, Patrick, Marc Bodson, and Marty Brenner. 2008. “Towards Real-Time Simulation of Aeroservoelastic Dynamics for a Flight Vehicle from Subsonic to Hypersonic Regime.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2008-6375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6375
• Hu, Rongji, Zhikang Huang, Geng Zhao, et al. 2026a. “Analysis of Instantaneous Skin Friction in a Supersonic Turbulent Boundary Layer.” Physical Review E 113 (4): 045102. https://doi.org/10.1103/bcpw-w9db
• Hu, Bingtao, and Feng Li. 2019. “Monopulse SAR Angle Measurement Based on Total Variation and Monotonic Iterative Algorithm.” Journal of Engineering 2019 (19): 5763–65. https://doi.org/10.1049/joe.2019.0436
• Hu, Yu-Long, Ke-Bo Li, Lei Bao, and Haibo Liu. 2025a. “Capturability Analysis of Three-Dimensional True Proportional Navigation Guidance Law against Arbitrarily Maneuvering Target under Maneuverability Limitation.” Preprint, . https://doi.org/10.2139/ssrn.5433516
• Hu, Qindong, Jiang Wang, Hongyan Li, and Zirui Zhang. 2024a. “Impact Angle Constraint Guidance Law with Field-of-View Limitation.” In First Aerospace Frontiers Conference (AFC 2024), edited by Han Zhang. SPIE. https://doi.org/10.1117/12.3032645
• Hu, K., Y. Zhang, X. Cai, Z. Ma, and P. Zhang. 1994. “Study of High Thrust Ratio Approaches for Single-Chamber Dual-Thrust Solid Rocket Motors.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-3333. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3333
• Hua, Changchun, Yana Yang, Xian Yang, and Xinping Guan. 2019. “Constrained Control Design for Bilateral Teleoperation System.” In Analysis and Design for Networked Teleoperation System. Springer Singapore. https://doi.org/10.1007/978-981-13-7936-9_9
• Huang, C. 1985. “A Practical Approach to the Boundary Layer of the Thrust Chamber of a Rocket Engine.” In 21st Joint Propulsion Conference. AIAA 1985-1389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1389
• Huang, Gangqiang. 1990. “The Application of CCD Frame-Transfer Sensor to the Performance Test of Angle Tracking System of Radar.” In International Conference on Optoelectronic Science and Engineering ‘90. SPIE. https://doi.org/10.1117/12.2294675
• Huang, W. 2000. “An Object-Oriented Analysis Method for Liquid Rocket Engine System.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3770. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3770
• Huang, Minchao, Yuqiang Cheng, Jia Dai, and Jian Li. 2024c. “Mathematical Model of the Operation of a Pump-Fed Liquid Rocket Engine.” In Performance Analysis of a Liquid/Gel Rocket Engine During Operation. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-6485-3_7
• Huang, Minchao, Yuqiang Cheng, Jia Dai, and Jian Li. 2024d. “Simulation Analysis of the Starting Process of the Pump-Fed Liquid Rocket Engine.” In Performance Analysis of a Liquid/Gel Rocket Engine During Operation. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-6485-3_8
• Huang, Haimin, and Matteo Giacobello. 2022. “Uncertainty Quantification in Store Separation Analysis Using Kestrel, Design of Experiments and Surrogate Modelling.” In AIAA SCITECH 2022 Forum. AIAA 2022-1318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1318
• Huang, Junfeng, Erming He, Jinxiang Yi, Dahua Du, and Hongjian Wang. 2022b. “Research on Thermomechanical Fatigue Life Prediction of Regenerative Cooling Thrust Chamber.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 40 (4): 723–31. https://doi.org/10.1051/jnwpu/20224040723
• Huang, Yong, and Yang Li. 2022. “On the Anti-Missile Interception Technique of Unpowered Phase Based on Data-Driven Theory.” Mechanics & Industry 23: 26. https://doi.org/10.1051/meca/2022024
• Huang, Juan-Chen, Herng Lin, and Ching-Chang Chieng. 2002. “Computations of Roll-Damping Stability Derivative for Body/Cruciform-Tail Configuration.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2721. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2721
• Huang, Yanrong, Manrong She, Chunhui Wang, Chao Zhu, Shanguang Chen, and Zhizhong Li. 2024b. “A Generalized Framework for Human-Machine Function Allocation.” AHFE international 131. https://doi.org/10.54941/ahfe1004860
• Huang, Hai Bo, Wei Hua Wang, and Tao Zuo. 2011. “Influence Analysis of CCD Miss-Distance and Corresponding Research of τ Compensatory Technology Based on Finite Memory.” In Key engineering materials, vol. 474-476. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.474-476.309
• Huang, Z. C., Y. S. Zhang, and Yao Liu. 2018. “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, Yuhui, Jin Zhou, and Zhenguo Wang. 2000. “Numeric Simulation for Combustion Instability of Liquid Propellant Rocket Engine.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3297. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3297
• Huang, Liang, GuoQing Zhou, and XianFeng Zhang. 2022a. “Miss Distance Evaluation Based on UAV Video Image.” In International Symposium on Artificial Intelligence Control and Application Technology (AICAT 2022), edited by Wei Wei. SPIE. https://doi.org/10.1117/12.2645723
• Hubbard, Robert. 1983. Digital Microwave Transmission Tests at the Pacific Missile Test Center, Pt. Mugu, California. Institute for Telecommunication Sciences. https://doi.org/10.70220/942sw3mn
• Hudson, Gary C. 2005. “An Air-Launched Low-Cost Launch Vehicle.” In AIP Conference Proceedings, vol. 746. AIP. https://doi.org/10.1063/1.1867137
• 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
• 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
• Hughes, E. J., and M. Leyland. 1998. “Target Manoeuvre Detection Using Radar Glint.” Electronics Letters 34 (17): 1695–96. https://doi.org/10.1049/el:19981188
• Hughes, Taylor, and Michael McFarland. 2000. “Integrated Missile Guidance Law and Autopilot Design Using Linear Optimal Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4163
• Hughes, Hunter, and Fen Wu. 2010. “H-Infinity LPV State Feedback Control for Flexible Hypersonic Vehicle Longitudinal Dynamics.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8281
• Hughson, Montgomery, and Edward Luke. 2008. “Unsteady Simulations of Missile Exhaust Plume Interactions.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6744. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6744
• Hulka, James. 2008. “Scaling of Performance in Liquid Propellant Rocket Engine Combustion Devices.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-5113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-5113
• Hull, David, and Rodney Mack. 1988. “Prediction of Time-to-Go for a Homing Missile Using Bang-Bang Control.” In Guidance, Navigation and Control Conference. AIAA 1988-4065. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4065
• 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, David, and David Salguero. 1994. “Missile Sizing for Ascent-Phase Intercept.” In 19th Atmospheric Flight Mechanics Conference. AIAA 1994-3450. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3450
• Hull, David, and Jean-Marie Seguin. 1993. “Guidance Law Based on Piecewise Constant Control for Hypersonic Gliders.” In Guidance, Navigation and Control Conference. AIAA 1993-3888. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3888
• Hull, D., and J. Speyer. 1981. “Maximum Information Trajectories for Homing Missiles.” In Guidance and Control Conference. AIAA 1981-1757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1757
• Hull, D., J. Speyer, and D. Burris. 1987. “A Linear-Quadratic Guidance Law for Dual Control of Homing Missiles.” In Guidance, Navigation and Control Conference. AIAA 1987-2381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2381
• 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
• Hull, D., J. Speyer, and C. Tseng. 1984. “Maximum-Information Guidance for Homing Missiles.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1887. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1887
• Human, Mel. 2001. “A Missile Flight Simulation Using Interdisciplinary Coupling.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2001-4421. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4421
• 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
• Hung, Bui Quoc. 2026. “Adaptive Command-to-Line-of-Sight Guidance Using Feedback Linearization.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0626110.114
• Hung, F., and C. Scottoline. 1975. “Aerodynamic Heating in Gaps in the Presence of Protuberances and Shock Wave Impingement.” In 10th Thermophysics Conference. AIAA 1975-670. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-670
• Hunley, J. D. 2008. “From Eaton Canyon to the Sergeant Missile: Solid-Propellant Rocket Developments, 1940–1962.” In University Press of Florida eBooks. https://doi.org/10.5744/florida/9780813031774.003.0006
• 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
• Hussein, Mennatallah M., Lilly Etzenbach, and Olivier de Weck. 2026. “Sensor and Actuator Evaluation for Liquid Rocket Engines Combustion Instability.” In AIAA SCITECH 2026 Forum. AIAA 2026-1001. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-1001
• Huston, Wilber B., Calvin N. Warfield, and Anna Z. Stone. 1948. A Study of Skin Temperatures of Conical Bodies in Supersonic Flight. NACA-TN-1724. NASA. https://ntrs.nasa.gov/citations/19930082417
• Hutchins, Charles W. 1974. “A Computer Aided Function Allocation and Evaluation System (CAFES).” Proceedings of the Human Factors Society Annual Meeting 18 (3): 350–53. https://doi.org/10.1177/154193127401800322
• Hwang, Yuchung. n.d. “Optimal Target/missile Tracking under Reduced Order Ideal Models.” PhD diss., Drexel University. https://doi.org/10.17918/00007109
• Hwang, Danny P. 1999. An Experimental Study of Turbulent Skin Friction Reduction in Supersonic Flow Using a Microblowing Technique. NASA/TM-1999-209632. NASA. https://ntrs.nasa.gov/citations/20000023178
• Hwang, Danny. 2000. “An Experimental Study of Turbulent Skin Friction Reduction in Supersonic Flow Using a Microblowing Technique.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-545
• Hwang, W., W. Chen, and P. Tasi. 1991. “Measuring Flight Hinge Moment.” In 27th Joint Propulsion Conference. AIAA 1991-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2423
• Hwang, Ki-Young, and Hwanil Huh. 2020. “Research and Development Trends of a Hypersonic Glide Vehicle (HGV).” Journal of the Korean Society for Aeronautical & Space Sciences 48 (9): 731–43. https://doi.org/10.5139/jksas.2020.48.9.731
• Hyde, R. S. 2002. A Solid Rocket Motor Manufacturer’s View of Sensors and Aging Surveillance. Defense Technical Information Center. https://doi.org/10.21236/ada406078
• Hyde, Stephen, and Victor Argueta. 2025. “Evaluating Performance of Simple Gas-on-Liquid Injector Designs in a Small Bipropellant Rocket Engine.” In AIAA SCITECH 2025 Forum. AIAA 2025-0109. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0109
• 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
• “Hydrodynamic and Thermal Analysis of Additively Manufactured Thrust Chamber Cooling Channels.” 2025. South African Journal of Industrial Engineering 36 (3). https://doi.org/10.7166/36-3-3349
• Hypersonic Aerodynamics (Slender Bodies). 2025. Wiley. https://doi.org/10.1002/9781394285662.ch2
• Ibarrondo Hernández, Francisco de Borja. n.d. “Optimization of the Integrated Guidance and Control for a Dual Aerodynamic Control Missile.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.38301
• 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
• Iida, Reo, Yasunori Nagata, Kazuhiko Yamada, and Akira Oyama. 2026. “Effect of Gas Permeability on the Aerodynamic Heating Characteristics of a Textile-Based Flexible Deployable Aeroshell.” In 28th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2026-3805. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-3805
• Imado, Fumiaki, and Takeshi Kuroda. 1992. “Optimal Missile Guidance System against a Hypersonic Target.” In Astrodynamics Conference. AIAA 1992-4531. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4531
• Imado, Fumiaki, Takeshi Kuroda, and Akira Ichikawa. 1996. “A Trade-off Study between Conventional and Augmented Proportional Navigation.” In Guidance, Navigation, and Control Conference. AIAA 1996-3882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3882
• Imado, Fumiaki, Takeshi Kuroda, and Susumu Miwa. 1989. “Optimal Thrust Design of a Missile with a Pulse Motor.” In Guidance, Navigation and Control Conference. AIAA 1989-3479. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3479
• Imado, Fumiaki, Takeshi Kuroda, and Min-Jea Tahk. 1998. “A New Missile Guidance Algorithm against a Maneuvering Target.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4114
• Imado, F., and S. Miwa. 1985. “A Comparative Study of Evasive Maneuvers of a Fighter against a Proportional Navigation Missile.” In Guidance, Navigation and Control Conference. AIAA 1985-1870. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1870
• Imado, Fumiaki, and Sachio Uehara. 1996. “Proportional Navigation versus High-g Barrel Roll Maneuvers from Optimal Control of View.” In Guidance, Navigation, and Control Conference. AIAA 1996-3839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3839
• Immich, H., J. Kretschmer, and D. Preclik. 2001. “Thrust Chamber Technology Developments for Future Launch Vehicle Liquid Rocket Engines.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3544
• “Impact Angle and Field-of-View Constrained Guidance Law against Non-Maneuvering Moving Tank Using Nonlinear Virtual Relative Model and Optimal Error Dynamics.” 2025. International Journal of Mechanical Engineering and Robotics Research 14 (1): 26–38. https://doi.org/10.18178/ijmerr.14.1.26-38
• Inaba, Takeshi, and Yoshiki Matsuo. 1995. “Loop-Shaping Characteristics of a Human Operator in a Compensatory Manual Control System.” In Analysis, Design and Evaluation of Man–Machine Systems 1995. Elsevier. https://doi.org/10.1016/b978-0-08-042370-8.50052-5
• Inbar, Gideon F. 1991. “Human Operator Tracking Performance with a Vibrotactile Display.” In NASA. Ames Research Center, Human Machine Interfaces for Teleoperators and Virtual Environments. https://ntrs.nasa.gov/citations/19950007636
• “Influence of Corrugation-Roughness Shape on Aerodynamic Heating in Thick Turbulent Boundary Layers.” 1980. In Entry Heating and Thermal Protection. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865435.0332.0359
• Inger, George. 1991. “Nonequilibrium Effects on the Aerodynamic Heating of Lifting Hypersonic Vehicles.” In 9th Applied Aerodynamics Conference. AIAA 1991-3324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-3324
• Innocenti, Mario, and Ajay Thukral. 1993. “Simultaneous Reaction Jet and Aerodynamic Control of Missile Systems.” In Guidance, Navigation and Control Conference. AIAA 1993-3739. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3739
• “Innovative Flight Deck Function Allocation Concepts for NextGen.” 2012. In Advances in Human Aspects of Aviation. CRC Press. https://doi.org/10.1201/b12321-36
• “Instability Phenomenology and Case Studies: Instability Phenomena in Earth Storable Bipropellant Rocket Engines.” 1995a. In Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866371.0113.0142
• “Instability Phenomenology and Case Studies: Instability Phenomena in Liquid Oxygen/Hydrocarbon Rocket Engines.” 1995b. In Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866371.0073.0088
• “Instability Phenomenology and Case Studies: Overview of Combustion Instabilities in Liquid-Propellant Rocket Engines.” 1995c. In Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866371.0003.0037
• “Instrumentation for Research on Combustion Instability in Solid-Propellant Rocket Motors.” 1960. In Liquid Rockets And Propellants. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864759.0119.0143
• “Integrated Design of Estimator and Guidance Law.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-19
• “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 Missile Design.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-12
• “Introduction to Liquid-Propellant Rocket Engines.” 1992. In Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866197.0001.0022
• Irfan, Irfan Fadilla Nursamsi, Nanang Burhan, Reza Setiawan, and Siswadi. 2026. “Analisis Pengaruh Modifikasi Geometri Rudder Terhadap Koefisien Hinge Moment Dan Karakteristik Aerodinamis Pesawat n-Xxx Menggunakan Computational Fluid Dynamics.” Barometer 11 (2): 58–66. https://doi.org/10.35261/barometer.v11i2.13201
• Irons, Fred H., and Melvin M. Landesberg. 1981. Precision Standoff Guidance Antenna Accuracy Evaluation. Defense Technical Information Center. https://doi.org/10.21236/ada103063
• Ishimoto, Shinji. 1995. “Guidance Algorithm for Suborbital Flight Experiment of Unmanned Lifting Entry Vehicle.” In Guidance, Navigation, and Control Conference. AIAA 1995-3286. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3286
• Ismail, Shaik, P. C. Jain, and P. S. R. Anjaneyulu. 2023. “Effect of Flexibility and Aircraft Flow Field on Rail Launch Simulation of a Missile.” Journal of Aerospace Sciences and Technologies: 81–88. https://doi.org/10.61653/joast.v68i2.2016.249
• Istepanian, R. Sh. H. 1998. “Finite Word Length Stability Issues of a Teleoperation Motion-Scaling Control System.” In UKACC International Conference on Control (CONTROL ‘98), vol. 1998. IEE. https://doi.org/10.1049/cp:19980481
• Istiqomah, A., Suma’inna, A. Riyadl, R. A. Duhri, and I. E. Putro. 2021. “Lateral Stability Control of LAPAN Missile Using Incremental-Based Model Reference Adaptive Control.” In AIP Conference Proceedings, vol. 2366. AIP Publishing. https://doi.org/10.1063/5.0059991
• Ito, Koji, Haruo Hayami, and Masami Ito. 1973. “A Model for Precognitive Control Behavior of Human Operator in Manual Control Systems.” Transactions of the Society of Instrument and Control Engineers 9 (1): 37–44. https://doi.org/10.9746/sicetr1965.9.37
• Ito, K., and M. Ito. 1975. “On Tracking Behaviors of the Human Operator in Preview Control Systems.” Kybernetes 4 (1): 33–38. https://doi.org/10.1108/eb005380
• Itohara, Hiroyuki, and Susumu Miwa. 1992. “Non-Gaussian Clutter Effect on the Miss Distance of a Radar Homing Missile.” In Astrodynamics Conference. AIAA 1992-4536. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4536
• Iwakawa, Akira, Naoki Hasegawa, Takeshi Osuka, Ryosuke Majima, Takeharu Sakai, and Akihiro Sasoh. 2013. “Supersonic Drag Reduction Performance of Blunt-Body with Conical Spike Using with Energy Depositions.” In 44th AIAA Plasmadynamics and Lasers Conference. AIAA 2013-3127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3127
• 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
• Jabbar, Muhammad Rifki Abdul, Reza Setiawan, and Farradina Choria Suci. 2026. “Pengaruh Penambahan 10% Plat Pada Rudder Pesawat N2XX Terhadap Hinge Moment Berbasis Metode Computational Fluid Dynamics.” Barometer 11 (2): 67–73. https://doi.org/10.35261/barometer.v11i2.13206
• Jabbour, Elio. n.d. “Shared-Autonomy Control for Improving Human-Robot Collaboration in Haptic Teleoperation.” PhD diss., Bordeaux. https://doi.org/10.70675/53c62ad1z37cbz4f1fz9b0cz76870058cc4f
• Jack, John R., and Warren C. Burgess. 1951. Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6): Body of Revolution with near-Parabolic Forebody and Cylindrical Afterbody. NACA-RM-E51H13. NASA. https://ntrs.nasa.gov/citations/19930086849
• Jackson, G. A. 1967. Measuring Human Performance with a Parameter Tracking Version of the Crossover Model. NASA-CR-910. NASA. https://ntrs.nasa.gov/citations/19670030767
• Jackson, G. A. 1969. A Method for the Direct Measurement of Crossover Model Parameters. NASA. https://ntrs.nasa.gov/citations/19690047941
• 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
• Jacob, Eric, Gary Flandro, Paul Gloyer, and Jonathan French. 2010. “Nonlinear Liquid Rocket Combustion Instability Behavior Using UCDS Process.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6800. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6800
• Jaeger, Robert J., Gyan C. Agarwal, and Gerald L. Gottlieb. 1980. “Predictor Operator in Pursuit and Compensatory Tracking.” Human Factors: The Journal of the Human Factors and Ergonomics Society 22 (4): 497–506. https://doi.org/10.1177/001872088002200410
• 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
• 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
• Jagacinski, Richard J., Walter W. Johnson, E. James Hartzell, Sharon Ward, and Kaile Bishop. 1978. Process Model of How the Human Operator Tracks Discontinuous Inputs. Defense Technical Information Center. https://doi.org/10.21236/ada069001
• Jaggers, R. F. 1977. An Explicit Solution to the Exoatmospheric Powered Flight Guidance and Trajectory Optimization Problem for Rocket Propelled Vehicles. AIAA PAPER 77-1051. McDonnell Douglas Technical Services Co. https://ntrs.nasa.gov/citations/19770059962
• Jahangir, E., and R. Howe. 1990. “A Two-Pulse Scheme for the Time-Optimal Attitude Control of a Spinning Missile.” In Guidance, Navigation and Control Conference. AIAA 1990-3377. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3377
• Jain, Sambhav Kumar, Tapan K. Jain, Saumya Shanker, and Srikant Srivastava. 2023. “Rapid and Accurate INS Transfer Alignment for Air Launched Tactical Missile Using Kalman Filter.” Defence Science Journal 73 (4): 496–502. https://doi.org/10.14429/dsj.73.18435
• Jain, Sambhav Kumar, Tapan K. Jain, Srikant Srivastava, and Saumya Shanker. 2024. “Comparison of Filtering Techniques for Transfer Alignment of Air Launched Tactical Guided Weapons.” Defence Science Journal 74 (4): 560–66. https://doi.org/10.14429/dsj.74.19303
• Jalali-Naieni, S. Hamid, and Ali Arabian Arani. 2020. “Proportional Navigation Guidance with Variable Navigation Ratio in terms of the angle of relative velocity with respect to Line-of-Sight and its Rate.” Journal of Space Science and Technology 13 (2): 1–12. https://doi.org/10.30699/jsst.2020.1180
• Jalali-Naini, S. H., and S. H. Sajjadi. 2016. “First-Order Optimal Line-of-Sight Guidance for Stationary Targets.” Scientia Iranica 23 (2): 588–99. https://doi.org/10.24200/sci.2016.3846
• James, D. A. 1986a. “Principles of Doppler Homing Guidance.” In Radar Homing Guidance for Tactical Missiles. Macmillan Education UK. https://doi.org/10.1007/978-1-349-08602-3_5
• James, D. A. 1986c. “Radar Homing on Surface Targets.” In Radar Homing Guidance for Tactical Missiles. Macmillan Education UK. https://doi.org/10.1007/978-1-349-08602-3_8
• Jamison, Lelan. 1966. “A Method for Calculating Parachute Opening Forces for General Deployment Conditions.” In Aerodynamic Deceleration Systems Conference. AIAA 1966-1501. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1501
• Janda, Mathew D., Robert J. Sinclair, and Debra Gardinier. 2013. “Tailoring a Parachute Recovery System for Commercial Space.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1261
• Jann, Thomas. 2015. “Implementation of a Flight Dynamic Simulation for Cargo Airdrop with Complex Parachute Deployment Sequences.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2144. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2144
• “Japan’s Liquid Propellant Rocket-Engine History.” 2006. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0815.0842
• 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
• Jarrett, T. W. 1971. Space Shuttle: Static Longitudinal, Directional and Lateral Characteristics and Control Surface Effectiveness of the MDAC-STS Canard Booster. NASA-CR-119978. NASA. https://ntrs.nasa.gov/citations/19710029204
• Jasher, Neeraj. 2012. “Impact of Shock Wave on a Body Moving at Supersonic Speed.” IOSR Journal of Applied Physics 2 (2): 37–42. https://doi.org/10.9790/4861-0223742
• Jassim, Esam. 2017. “Numerical Study on Skin Friction and Shock Inception in Various Geometries of Supersonic Nozzle.” International Journal of Vehicle Structures and Systems 9 (3). https://doi.org/10.4273/ijvss.9.3.01
• Jasztal, Michał, and Artur Kłosiński. 2024. “Design and Application of a Parachute Deployment Mechanism for Sounding Rockets Based on Commonly Available and Affordable Components.” Journal of Konbin 54 (1): 21–32. https://doi.org/10.5604/01.3001.0054.4460
• Jay, Shinde A., Ghariya Rutika, Chatterjee Dipayan, and Jani Grishma. 2024. “Design and Analysis of Ku Band Planar Monopulse Tracking Antenna.” Preprint, . https://doi.org/10.2139/ssrn.4495948
• Jayan, N., and B. N. Raghunandan. 2003. “A Technique for Drop Size Control during Throttling of a Rocket Engine.” Atomization and Sprays 13 (4): 345–56. https://doi.org/10.1615/atomizspr.v13.i4.10
• Jeler, Eduard Grigore. 2025. “Use and Adaptation of Classic Anti-Aircraft Missile Systems against Drones.” Review of the Air Force Academy 23 (2): 5–11. https://doi.org/10.19062/1842-9238.2025.23.2.1
• Jeng, San-Mou, and Ron Litchford. 1991. “Nonlinear Analysis of Longitudinal-Mode Liquid Propellant Rocket Combustion Instability.” In 27th Joint Propulsion Conference. AIAA 1991-1985. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1985
• Jenke, Leroy M. 1976. Experimental Roll-Damping, Magnus, and Static-Stability Characteristics of Two Slender Missile Configurations at High Angles of Attack (0 to 90 Deg) and Mach Numbers 0.2 through 2.5. Defense Technical Information Center. https://doi.org/10.21236/ada027027
• Jenkins, R. 1982. “Development of the High Capability Air Launched Test Vehicle.” In 6th Sounding Rocket Conference. AIAA 1982-1748. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1748
• Jenn, A., and H. Nelson. 1988a. “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, Dale. 2005. “Advanced Performance, Liquid Propellant, Rocket Engine.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4566. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4566
• Jensen, A. V., B. B. Goshgarian, and N. E. Dane. 1962. Mass Spectral Analysis of Rocket Engine Combustion Products Containing Boron Nitride. Defense Technical Information Center. https://doi.org/10.21236/ad0295656
• Jeon, In Soo, and Mark Karpenko. 2019. “Off-Target Look Angle Control Guidance Law for Moving Targets.” In AIAA Scitech 2019 Forum. AIAA 2019-1926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1926
• Jernell, L. S. 1970. Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-Finned Missile Configuration at Mach 1.50 to 2.86. NASA-TM-X-2031. NASA. https://ntrs.nasa.gov/citations/19700022495
• Jernell, L. S. 1974. Stability and Control Characteristics of a Monoplane Missile with Large Delta Wings and Various Tail Controls at Mach 1.90 to 2.86. NASA-TM-X-71984. NASA. https://ntrs.nasa.gov/citations/19740021178
• Jex, H. R., J. D. McDonnell, and A. V. Phatak. 1966a. A ‘‘Critical’’ Tracking Task for Man-Machine Research Related to the Operator’s Effective Delay Time. Part I: Theory and Experiments with a First-Order Divergent Controlled Element. NASA-CR-616. NASA. https://ntrs.nasa.gov/citations/19660030603
• Jha, Ishayyu. 2024. “A Comparative Analysis of the Rotation Detonation Engine and Liquid Rocket Engine in Thrust, Impulse, and Flow Rate.” Preprint, . https://doi.org/10.2139/ssrn.4889182
• Ji, Jialong, and Bing Sun. 2015. “Research on Structural Optimization for Regenerative-Cooling Thrust Chamber.” In Volume 1A: Symposia, Part 2. American Society of Mechanical Engineers. https://doi.org/10.1115/ajkfluids2015-09332
• Jialong Ji and Bing Sun. 2014. “Life Analysis of Regenerative-Cooling Thrust Chamber.” In 2014 ISFMFE - 6th International Symposium on Fluid Machinery and Fluid Engineering. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2014.1217
• Jiang, Qiuxi. 2015. “Target Tracking of Network Radar Countermeasure Systems.” In Network Radar Countermeasure Systems. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-48471-5_4
• Jiang, Hailin. 2021. “Analysis on Coordinated Anti-Jamming of Anti-Missile Early Warning Radar System Based on Intelligent Optimization Algorithm.” In Seventh Symposium on Novel Photoelectronic Detection Technology and Applications, edited by Junhao Chu, Qifeng Yu, Huilin Jiang, Junhong Su. SPIE. https://doi.org/10.1117/12.2587394
• Jiang, Shan. 2024. “Research on the Effectiveness of Tactical Missile Weapon Systems Based on Energy Big Data.” Applied Mathematics and Nonlinear Sciences 9 (1): 20241059. https://doi.org/10.2478/amns-2024-1059
• Jiang, Panke, Pengcheng Gong, Yuntao Wu, and Xiong Deng. 2022b. “Multiple-Input Multiple-Output with Frequency Diverse Array Radar Transmit Beamforming Design for Low-Probability-of-Intercept in Cluttered Environments.” IET Signal Processing 16 (7): 811–20. https://doi.org/10.1049/sil2.12112
• 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
• Jianmei, Song, Cai Gaohua, Kong Lixia, and Fan Jianhua. 2012. “Precision Analysis of the Semi-Strapdown Homing Guided System.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4687. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4687
• JianQi, Wang, Wang DongMei, and Yan Liang. 2021. “Research on the Stability of an Air-to-Air Missile Compound Control System with a Pulse Modulator.” Journal of Physics: Conference Series 1884 (1): 012027. https://doi.org/10.1088/1742-6596/1884/1/012027
• Jiao, Renlei, Xiaobin Pan, Qiang Zhou, and Fang Di. 2024. “Simulation and Analysis of Firing Accuracy of Remote Control Weapon Station.” Journal of Physics: Conference Series 2862 (1): 012037. https://doi.org/10.1088/1742-6596/2862/1/012037
• Jin, Yu Qiang, and Qiang Ma. 2011. “Overload Control of Supersonic Missile System.” Advanced materials research 295-297: 1761–63. https://doi.org/10.4028/www.scientific.net/amr.295-297.1761
• Jin, Zhen, 良贵 谢, and Wen Shu-liang. 2014. “Distributed MIMO Radar Monopulse Angular Estimation.” JOURNAL OF RADARS 3 (4): 474–79. https://doi.org/10.3724/sp.j.1300.2014.13077
• Jo, Han-Sang. 2007. “A Study on the Accuracy Analysis for Air-to-Ground Weapon Delivery.” Journal of the Korean Society for Aeronautical & Space Sciences 35 (8): 741–46. https://doi.org/10.5139/jksas.2007.35.8.741
• Jo, Eric. 2026. “Aerodynamic Heating from Compression Corner Interactions in Hypersonic Flow.” In 2026 Regional Student Conferences. AIAA 2026-115448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-115448
• Johann, Ulrich A., Klaus Pribil, and Heinz Sontag. 1991. “Novel Optical-Fiber-Based Conical Scan Tracking Device.” In SPIE Proceedings, vol. 1522, edited by Juergen Franz. SPIE. https://doi.org/10.1117/12.46079
• Johnson, A. 1995. “Achieving the Balance between Automation and Manual Control.” In IEE Colloquium on `The Role of the Operator in the Safety of the Nuclear Industry’, vol. 1995. IEE. https://doi.org/10.1049/ic:19950888
• Johnson, Mark. 2015. Tactical Tomahawk RGM-109E/UGM-109E Missile (TACTOM). Defense Technical Information Center. https://doi.org/10.21236/ad1019558
• Johnson, Mary D., and Gary B. Matthews. 1978. “Range Instrumentation for the Measurement of the Effects of a Marine Environment on Electro-Optical Radiation.” In SPIE Proceedings, vol. 0133, edited by Stephen A. Benton, Geoffery Knight. SPIE. https://doi.org/10.1117/12.956070
• Johnson, Breanna J., Daniela Rocca-Bejar, Ping Lu, et al. 2020. “Pterodactyl: The Development and Performance of Guidance Algorithms for a Mechanically Deployed Entry Vehicle.” In American Institute of Aeronautics and Astronautics (AIAA). https://ntrs.nasa.gov/citations/20200000239
• Johnson, Rudy, Michael Stanek, and James Grove. 2008. “Store Separation Trajectory Deviations Due to Unsteady Weapons Bay Aerodynamics.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-188. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-188
• Johnson, P., P. Wright, and M. Harrison. 2001. “An Evaluation of Two Function Allocation Methods.” In People in Control. Human Factors in Control Room Design. Institution of Engineering and Technology. https://doi.org/10.1049/cp:20010458
• Jolly, Bruce A., and Christopher Coley. 2026. “Monte-Carlo 6-DoF with Weapons Bay Cavity Acoustic Influence.” In AIAA AVIATION 2026 Forum. AIAA 2026-4278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-4278
• Jonas, Julius. 1953. “Effect of Aerodynamic Heating on Fuel Systems.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/530236
• Jones, Robert T. 1959a. “Aerodynamic Design for Supersonic Speeds.” In Advances in Aeronautical Sciences. Elsevier. https://doi.org/10.1016/b978-1-4831-9832-3.50006-1
• Jones, Lynette A., and Ian W. Hunter. 1991. “Analysis of the Human Operator Subsystems.” In NASA. Ames Research Center, Human Machine Interfaces for Teleoperators and Virtual Environments. https://ntrs.nasa.gov/citations/19950007606
• Jones, Robert T., and Kenneth Margolis. 1946. Flow over a Slender Body of Revolution at Supersonic Velocities. NACA-TN-1081. NASA. https://ntrs.nasa.gov/citations/19930084662
• 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, Malcolm E., and Kim Eric Moore. 1987. Dual Laser Gyro Test Program. AIAA PAPER 87-2542. NASA Johnson Space Center. https://ntrs.nasa.gov/citations/19870063268
• Jong Yil, Park, Lee Sung Uk, and Kim Ho Soo. 2014. “Framework of Weapon Effectiveness Tool for Hardened Targets.” Journal of the Computational Structural Engineering Institute of Korea 27 (6): 551–55. https://doi.org/10.7734/coseik.2014.27.6.551
• Jordan, J., A. Denny, J. Jordan, and A. Denny. 1997. “Approximation Methods for Computational Trajectory Predictions of a Store Released from a Bay.” In 15th Applied Aerodynamics Conference. AIAA 1997-2201. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2201
• Josey, Timothy, Kishore Pamadi, and Brett A. Newman. 2019. “Spinning Projectile Navigation and Guidance Using Strapdown Seeker.” In AIAA Scitech 2019 Forum. AIAA 2019-2342. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2342
• Joshi, Harshal V., Salahudden Salahudden, and Ajoy K. Ghosh. 2023. “Conceptualization and Analysis of Various Mid-Air Launch Technique for Parasite Aircraft.” In AIAA SCITECH 2023 Forum. AIAA 2023-1556. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1556
• Joshi, Hemant, Peter Thomas, Christabel Tan, and Hongwei Wu. 2024b. “Improved Vortex Lattice Method for Drag Prediction of Supersonic Wings Using Shock Cone Modelling.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-5418595/v1
• Joshi, Hemant, Peter Thomas, Hongwei Wu, and Christabel Tan. 2024a. “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
• Joyce, Eric R., Krishna B. Kidambi, and Markus P. Rumpfkeil. 2025. “Missile Flight Simulation with Surrogate Aerodynamic Models and Robust Control Autopilot.” In AIAA SCITECH 2025 Forum. AIAA 2025-1158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1158
• Jun, Zhao, Feng Li, Liang Wang, and Liu Wei Jian. 2013. “Adaptive Monopulse Angle Measurement for Meter-Wave Radar Based on Differential Constraints Technique.” Advanced materials research 846-847: 812–17. https://doi.org/10.4028/www.scientific.net/amr.846-847.812
• Juncosa, M. L., and D. M. Young. 1953. A Mathematical Formulation for ORDVAC Computation of the Probability of Kill of an Airplane by a Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0017267
• 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, Yunyoung, and Jong-Hwan Kim. 2023. “Combat Effectiveness and Efficiency Evaluation of Firearm Weapon Systems in Different Projectile Guidance Simulations.” Journal of Advances in Military Studies 6 (1): 119–43. https://doi.org/10.37944/jams.v6i1.196
• Jung, Ki-Wook, Hyeonjae Kim, Min-Jea Tahk, and Chang-Hun Lee. 2025. “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
• Jurado, E., J. Shade, and M. Weise. 1990. “Selection of Monitoring Techniques for a Liquid Propellant Rocket Engine.” In 26th Joint Propulsion Conference. AIAA 1990-2698. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2698
• Just, Herbert. 1991. “Ariane-5 Booster Recovery System: Description of the Parachute Assembly and the Test Philosophy.” In 11th Aerodynamic Decelerator Systems Technology Conference. AIAA 1991-839. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-839
• Kaber, David B., Jennifer M. Riley, Rong Zhou, and John Draper. 2000b. “Effects of Visual Interface Design, and Control Mode and Latency on Performance, Telepresence and Workload in a Teleoperation Task.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 44 (5): 503–6. https://doi.org/10.1177/154193120004400505
• Kachelmyer, Alan L. 1990. “Laser Radar Angular Tracking.” In SPIE Proceedings, vol. 1222, edited by Richard J. Becherer. SPIE. https://doi.org/10.1117/12.18366
• Kaczmarek, Paweł, and Piotr Serafin. 2019. “Analysis of Main Beam Adaptive Beamforming Effect on Accuracy of Monopulse Angle Estimation in Jammed Environment.” In XII Conference on Reconnaissance and Electronic Warfare Systems, edited by Piotr Kaniewski. SPIE. https://doi.org/10.1117/12.2525043
• Kada, B. 2015b. “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
• 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
• 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
• Kai-Bor Yu, Kai-Bor Yu. 2015. “Enhanced Monopulse Angle Estimation Using 4-Channel Radar System.” In IET International Radar Conference 2015. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2015.1109
• Kain, J. 1981. “Application of Directed-Miss Guidance for Roll-Pointing of Unidirectional Warheads.” In Guidance and Control Conference. AIAA 1981-1759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1759
• 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
• Kain, J., and D. Yost. 1976. “Command to Line-of-Sight Guidance: A Stochastic Optimal Control Problem.” In Guidance and Control Conference. AIAA 1976-1956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1956
• Kalam, A. P. J. Abdul. 1995. “Future Operational Scenario for Antitank Guided Missile Systems.” Defence Science Journal 45 (3): 183–86. https://doi.org/10.14429/dsj.45.4117
• 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
• Kam, Moshe. n.d. “The Power Spectral Density at the Output of the Gaussian Nonlinearity in Conical Scan Laser Target Tracking.” PhD diss., Drexel University. https://doi.org/10.17918/00003483
• 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
• Kamijo, K. 1983. “Dynamic Response of the LE-5 Rocket Engine Liquid Oxygen Pump.” In 19th Joint Propulsion Conference. AIAA 1983-1385. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1385
• Kamijo, K., E. Sogame, and A. Okayasu. 1981. “The Development of Small Liquid Oxygen and Liquid Hydrogen Turbopumps of a LE-5 Rocket Engine.” In 17th Joint Propulsion Conference. AIAA 1981-1375. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1375
• Kamran, Danial. 2023. “Reduced Human Effort in Optical Tracking of Anti-Tank Guided Missile Targets Due to Integrated Tracking System Design.” Preprint, . https://doi.org/10.31219/osf.io/mxcjb
• Kanda, Takeshi. 2019. “Off-Design Combustion in Liquid-Propellant Rocket Engine with High-Frequency Instability.” Transactions of the Japan Society for Aeronautical and Space Sciences 62 (6): 331–33. https://doi.org/10.2322/tjsass.62.331
• Kang, Seonhyeok, H. Jin Kim, Daeyeon Won, Min-Jae Tahk, Jinik Lee, and Byoungeul Jun. 2008. “Robust Roll-Pitch-Yaw Integrated Autopilot for a High Angle-of-Attack Missile.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7001. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7001
• Kang, Honglong, and Shenmin Song. 2024. “Analytical Solution for Impact-Angle-Constrained Guidance with Flight Speed and Trajectory Length Prediction.” In International Symposium on Project Management (ISPM). https://doi.org/10.52202/076061-0132
• Kang, Si-Yoon, Bu-Kyeng Sung, Jaeeun Kim, Soo Seok Yang, and JeongYeol Choi. 2025. “Coupled Analysis of Regenerative Cooling and CFD for a Nuclear Thermal Rocket Engine.” In AIAA SCITECH 2025 Forum. AIAA 2025-2703. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2703
• Kanter, Irving, and Robert R. Boothe. 1978. Exact Probability Density Function of the Monopulse Ratio. Defense Technical Information Center. https://doi.org/10.21236/ada058459
• Kao, Henry S. R. 1977. “Effects of Delay of Feedback and Intermittency of Feedback in Compensatory Tracking.” Perceptual and Motor Skills 44 (3_suppl): 1079–85. https://doi.org/10.2466/pms.1977.44.3c.1079
• Kapela, Aleksandra. 2026. “Manual Control, Automation, and Technology.” In Human Factors for Pilots and Aviation Specialists. CRC Press. https://doi.org/10.1201/9781003515418-10
• Kaplan, Joseph A., Alan R. Chappell, and John W. McManus. 1994. The Analysis of a Generic Air-to-Air Missile Simulation Model. NASA-TM-109057. NASA. https://ntrs.nasa.gov/citations/19940031931
• Karahan, Mehmet, and Unver Kaynak. 2026. “Kalman Filter Design and Flutter Suppression Control for an Aeroelastic Fin System.” International Journal of Science and Research Archive 19 (2): 489–500. https://doi.org/10.30574/ijsra.2026.19.2.0957
• Karelahti, Janne, Kai Virtanen, and Tuomas Raivio. 2006b. “Near-Optimal Missile Avoidance Trajectories via Receding Horizon Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6312
• Karlgaard, Chris D., Jake Tynis, and Clara O’Farrell. 2018. “Reconstruction of the Advanced Supersonic Parachute Inflation Research Experiment Sounding Rocket Flight Test.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-3624. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3624
• Karlgaard, Chris D., Jake Tynis, Clara O’Farrell, and Bryan Sonneveldt. 2019. “Reconstruction of the Advanced Supersonic Parachute Inflation Research Experiment Sounding Rocket Flight Tests with Strengthened Disk-Gap-Band Parachute.” In AIAA Scitech 2019 Forum. AIAA 2019-0014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0014
• Karnesky, A., and S. Colucci. 1973. “Recent Occurrences of Combustion Instability in Solid Rocket Motors: An Overview.” In 9th Propulsion Conference. AIAA 1973-1296. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-1296
• Kartchner, Kenneth A. 1963. Service Life Test of Cartridge Shackle Ejector for the GAM-72 Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0407548
• Kasdorf, F. W. 1952. Fuzing System for XSAM-N-4, Guided Missile Dove. Defense Technical Information Center. https://doi.org/10.21236/ad0007646
• Kasdorf, F. W. 1953. Fuzing System for XSAM-N-4, Guided Missile Dove; Steel Plate Impact Tests. Defense Technical Information Center. https://doi.org/10.21236/ad0013175
• Kashiwagi, Yasutada. 1968. Prediction of Ballistic Missile Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ad0728502
• Kashler, Richard C. 1961. The Effects of Transverse Accelerations and Exponential Time-Lag Constants on Compensatory Tracking Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0268185
• Kassner, D. L., and B. Wettlaufer. 1977a. Aerodynamic Characteristics of a Canard-Controlled Missile at Mach Numbers of 0.8, 1.3, and 1.75. NASA-TM-X-73218. NASA. https://ntrs.nasa.gov/citations/19770021127
• Kassner, D. L., and B. Wettlaufer. 1977b. Aerodynamic Characteristics of a Canard-Controlled Missile at Mach Numbers of 1.5 and 2.0. NASA-TM-X-73219. NASA. https://ntrs.nasa.gov/citations/19770023138
• Kassner, D. L., and B. Wettlaufer. 1977c. Effects of Canard Location on the Aerodynamic Characteristics of a Blunt-Nosed Missile at Mach Numbers of 1.5 and 2.0. NASA-TM-X-73220. NASA. https://ntrs.nasa.gov/citations/19770023139
• Kassner, D. L., and B. Wettlaufer. 1977d. Effects of Canard Location on the Aerodynamic Characteristics of a Sharp-Nosed Missile at Mach Numbers of 1.5 and 2.0. NASA-TM-73221. NASA. https://ntrs.nasa.gov/citations/19780002082
• Kassoy, D. R. 1997. Nonlinear, Rotational-Acoustic Processes in Solid Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ada329605
• Kassoy, David. 2013. “Mechanical Disturbances Arising from Thermal Power Deposition in a Gas with Application to Supercritical Liquid Rocket Engine Combustion Instability.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-567
• Katsionov, Oleg. 2026. “Laboratory Complex of Missile Control Systems.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/3083-7057-2026-1-084
• 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
• Kawamura, Ryuma, and Keiichi Karashima. 1957. “On the Wave Drag of Wing-Body Combination Moving at Supersonic Speeds.” Journal of the Japan Society of Aeronautical Engineering 5 (39): 93–99. https://doi.org/10.2322/jjsass1953.5.93
• Kawatsu, Kaname, Seiji Tsutsumi, Miki Hirabayashi, and Daiwa Sato. 2020. “Model-Based Fault Diagnostics in an Electromechanical Actuator of Reusable Liquid Rocket Engine.” In AIAA Scitech 2020 Forum. AIAA 2020-1624. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1624
• Kawiecki, Grzegorz, and Winthrop Smith. 1994. “Piezoelectric Actuator Capable of Inducing Torsional and Bending Control Loads with No Structural Coupling.” In Adaptive Structures Forum. AIAA 1994-1736. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-1736
• 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
• Kaykayoglu, C. 1996. “Application of the Vortex Lattice CFD Method to Obtaining Unsteady Aerodynamic Predictions about Wing/fuselage/pylon/store Configuration Including Store Separation.” In 34th Aerospace Sciences Meeting and Exhibit. AIAA 1996-168. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-168
• Kayran, Altan, and Mehmet O. Nalci. 2014. “Aeroservoelastic Modeling and Analysis of a Missile Control Surface with a Nonlinear Electromechanical Actuator.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-2055. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2055
• Kazaroff, John, and Albert Pavli. 1990. “Advanced Tube-Bundle Rocket Thrust Chamber.” In 26th Joint Propulsion Conference. AIAA 1990-2726. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2726
• Keche, M., A. Ouamri, I. Harrison, and M. S. Woolfson. 1997. “Performance Evaluation of an Algorithm for Multiple Target Angle Tracking.” IEE Proceedings - Radar, Sonar and Navigation 144 (5): 252–58. https://doi.org/10.1049/ip-rsn:19971321
• Keel, A., Jr. 1977. “Influence of Surface Roughness on Skin Friction and Heat Transfer for Compressible Turbulent Boundary Layers.” In 15th Aerospace Sciences Meeting. AIAA 1977-178. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-178
• Kehoe, Michael W., Lisa J. Bjarke, and Edward J. Laurie. 1990. “An in-Flight Interaction of the X-29A Canard and Flight Control System.” In AIAA Dynamics Specialists Meeting. https://ntrs.nasa.gov/citations/19900016657
• Keihl, Daria. 2025. “Prospects for the Use of Unmanned Aerial Vehicles Equipped with Liquid-Propellant Rocket Engines.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/2221-4550-2025-1-095
• 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
• Keith, M. W., and B. P. Selberg. 1984. Aerodynamic Canard/wing Parametric Analysis for General Aviation Applications. AIAA PAPER 84-0560. Gates Learjet. https://ntrs.nasa.gov/citations/19840035377
• Keller, Donald C. 1982a. 12823A Lance Missile Number 5356 Round Number 375-MCT. Defense Technical Information Center. https://doi.org/10.21236/ada116924
• Keller, Donald C. 1982b. 14823A LANCE Missile Number 5358, Round Number 378-AST.. Defense Technical Information Center. https://doi.org/10.21236/ada117137
• Kelley, T. L. 1923. “Further Note on the Probable Error of the Mean.” Journal of Educational Psychology 14 (8): 497–98. https://doi.org/10.1037/h0072890
• Kelley, H., E. Cliff, and F. Lutze. 1981. “Boost-Glide Range-Optimal Guidance.” In Guidance and Control Conference. AIAA 1981-1781. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1781
• Kelly, Joy, and W. Arnold, I. 1995. “Tolerance Analysis of an Air-to-Air Missile: A Comparison between Mu and the RSS Method.” In Guidance, Navigation, and Control Conference. AIAA 1995-3319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3319
• Kelly, John W., Charles E. Rogers, Gregory T. Brierly, J. Campbell Martin, and Marshall G. Murphy. 2017. “Motivation for Air-Launch: Past, Present, and Future.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20170007919
• Kemmner, Markus. n.d. “Reliability Demonstration of a Multi-Component Weibull System under Zero-Failure Assumption.” PhD diss., University of Louisville. https://doi.org/10.18297/etd/735
• Kennelly, Robert A., Jr., Aga M. Goodsell, and Lawrence E. Olsen. 2000. Skin Friction and Transition Location Measurement on Supersonic Transport Models. NASA Ames Research Center. https://ntrs.nasa.gov/citations/20010083466
• Kenny, Robert, Marlow Moser, James Hulka, and Gregg Jones. 2006. “Cold Flow Testing for Liquid Propellant Rocket Injector Scaling and Throttling.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4705. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4705
• Kenyon, Robert V. 1981. The Effects of Enhanced Disparity on Manual Control Stereopsis and Tracking Performance. Defense Technical Information Center. https://doi.org/10.21236/ada105447
• 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
• Khan, Umar Ali, Ahmad Ilyas, and Ekram Khan. 2026. “Advanced Frameworks for Low-Latency Teleoperation and LLMdriven Autonomous Exploration in Omnidirectional Mobile Robotics.” Journal of Undergraduate Research International 2 (3A): 38–43. https://doi.org/10.64589/juri/231349
• 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
• Kianvashrad, Nadia, Doyle D. Knight, Stephen P. Wilkinson, Amanda Chou, George B. Beeler, and Moazzam Jangda. 2018. “Effect of off-Body Laser Discharge on Drag Reduction of Hemisphere Cylinder in Supersonic Flow-Part II.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1433. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1433
• Kibbe, Marion P., and Jan S. Stiff. 1993. Operator Performance in Pattern Matching as a Function of Reference Material Structure. Defense Technical Information Center. https://doi.org/10.21236/ada269889
• Kibbe, Marion P., and Scott A. Weisgerber. 1990. Targeting Decisions Using Multiple Imaging Sensors: Operator Performance and Calibration. Defense Technical Information Center. https://doi.org/10.21236/ada224277
• Kidwell, Brian D., William D. Miller, and Raja Parasuraman. 2014. “Automation Complacency: Using Non-Invasive Brain Stimulation to Change Attention Allocation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 58 (1): 240–44. https://doi.org/10.1177/1541931214581050
• Kikumoto, Kousuke, Etsuroh Sentoh, Shinichiro Takanashi, Akihiko Yoshida, Tatsuo Takahashi, and Tsutomu Yamanaka. 1998. “Sidejet Aerodynamic Interaction Effect of the Missile. III: Flight Test Results.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4347. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4347
• Kim, Eunil. 2014. “Measurement and Analysis for Radar Glint Effect of Maritime Target.” Journal of the Korea Institute of Military Science and Technology 17 (4): 521–30. https://doi.org/10.9766/kimst.2014.17.4.521
• Kim, Seihwan. 2026. “Shock Wave Interaction and Drag Reduction by Laser Energy Deposition on a Blunt Body in Supersonic Flow.” Journal of the Korea Academia-Industrial cooperation Society 27 (6): 113–21. https://doi.org/10.5762/kais.2026.27.6.113
• Kim, Byoung Soo, Anthony Calise, and Ramachandra Sattigeri. 2006. “Adaptive, Integrated Guidance and Control Design for Line-of-Sight Based Formation Flight.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6716. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6716
• Kim, Y. M., C. P. Chen, and J. P. Ziebarth. 1992a. “Combustion Instability Analysis for Liquid Propellant Rocket Engines.” In NASA. Goddard Space Flight Center, Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1. https://ntrs.nasa.gov/citations/19920023053
• Kim, Y., C. Chen, J. Ziebarth, and Y. Chen. 1992b. “Prediction of High Frequency Combustion Instability in Liquid Propellant Rocket Engines.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3763. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3763
• Kim, Jinrae, Namhoon Cho, and Youdan Kim. 2019. “Field-of-View Constrained Impact Angle Control Guidance Guaranteeing Error Convergence before Interception.” In AIAA Scitech 2019 Forum. AIAA 2019-1927. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1927
• Kim, Junhong, S. Chung, and Jong Kim. 2004a. “Modeling of Lifted Turbulent Flame by the Flame Edge Theory and Its Implication in Liquid Rocket Combustion Instability.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1337. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1337
• Kim, Jinho, and Jungsoon Jang. 1995. “Nonlinear Model Inversion Control for Bank-to-Turn Missile.” In Guidance, Navigation, and Control Conference. AIAA 1995-3318. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3318
• Kim, Tae-Hun, Jaehyun Jin, Tae-Young Kang, Chang-Kyung Ryoo, and Jeong-Hun Kim. 2023b. “Composite Guidance Law for Homing Missiles Considering Nonlinear Field-of-View of a Strapdown Semi-Active Laser Seeker.” Journal of the Korean Society for Aeronautical & Space Sciences 51 (11): 779–88. https://doi.org/10.5139/jksas.2023.51.11.779
• Kim, Philsung, Byung-eul Jun, and Hangju Cho. 2002. “An Approximate Target Adaptive Guidance for IR Homing.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4842. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4842
• 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, K. Up, Seonhyeok Kang, H. Jin Kim, Chang-Hun Lee, and Min-Jea Tahk. 2010c. “Realtime Agile-Turn Guidance and Control for an Air-to-Air Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7745. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7745
• Kim, Hyeonggeun, and H. Jin Kim. 2015. “Missile Guidance Law Considering Constraints on Impact Angle and Terminal Angle of Attack.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0861
• Kim, Tae-Hun, Jong-Han Kim, and Philsung Kim. 2017a. “New Guidance Filter Structure for Homing Missiles with Strapdown IIR Seeker.” International Journal of Aeronautical and Space Sciences 18 (4): 757–66. https://doi.org/10.5139/ijass.2017.18.4.757
• Kim, Taeil, Taehwan Kim, Hwanseong Lee, Ji-Yeul Bae, Dae Yoon Jung, and Hyung Hee Cho. 2017b. “Susceptibility Analysis of Supersonic Aircraft Considering Drag Force of Infrared Guided Missile.” Journal of the Korea Institute of Military Science and Technology 20 (2): 255–63. https://doi.org/10.9766/kimst.2017.20.2.255
• Kim, Yehyun, Sejin Kwon, and Sang-Hyun Lee. 2023c. “Experimental Analysis in Hydrogen Peroxide Monopropellant Thruster with Different Injector Pressure Drop.” In AIAA SCITECH 2023 Forum. AIAA 2023-0719. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0719
• Kim, Sun Hoon, and Seunghoon Lee. 2024. “Iterative Self-Learning Framework for Dynamic Assignment of Multiple Targets to Aircraft with Variable Kill Probability.” Preprint, . https://doi.org/10.2139/ssrn.5030358
• Kim, Byung, Jang Lee, Hyung Han, et al. 1997. “Homing Guidance with Terminal Angular Constraint against Nonmaneuvering and Maneuvering Targets.” In Guidance, Navigation, and Control Conference. AIAA 1997-3474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-3474
• Kim, So-Young, Seung Man Lee, and Eric Johnson. 2008. “Analysis of Dynamic Function Allocation between Human Operators and Automation Systems.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2008-6673. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6673
• Kim, Mingu, Yongwoo Lee, Seokwon Lee, and Youdan Kim. 2015b. “Lyapunov-Based Three-Dimensional Terminal Angle Constrained Guidance Laws.” In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing. https://doi.org/10.1007/978-3-319-17518-8_3
• Kim, Boseok, Chang-Hun Lee, Min-Jea Tahk, and Shaoming He. 2021. “A New Biased Proportional Navigation Guidance for Decelerating Targets.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-8155-7_209
• Kim, Do-Hyung, Hyun-Shik Oh, and Seong Wook Hwang. 2016a. “A DDS-Based Distributed Simulation for Anti-Air Missile Systems.” In International Conference on Simulation and Modeling Methodologies, Technologies and Applications. https://doi.org/10.5220/0005980402700276
• Kim, Tae-Hun, and Bong-Gyun Park. 2019. “New Composite Guidance Law with Look Angle Rate Constraint.” Transactions of The Korean Institute of Electrical Engineers 68 (4): 566–72. https://doi.org/10.5370/kiee.2019.68.4.566
• Kim, Dowan, Woosung Park, and Chang-Kyung Ryoo. 2013b. “Look-Angle-Control Guidance for Missiles with Strapdown Seeker.” Journal of Institute of Control Robotics and Systems 19 (3): 275–80. https://doi.org/10.5302/j.icros.2013.12.1809
• Kim, Jinwhan, Monish Tandale, Padmanabhan Menon, and Ernest Ohlmeyer. 2010b. “Particle Filter for Ballistic Target Tracking with Glint Noise.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7881. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7881
• Kimata, Hiroyuki, Masato Taguchi, Xiaopeng Xue, and Koichi Mori. 2015. “Unsteady Aerodynamic Simulation of Supersonic Flexible Parachute Including Fluid-Structure Interaction.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2186. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2186
• 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, 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
• Kimura, Toshiya, Masaki Sato, Tadashi Masuoka, Takeshi Kanda, and Atsushi Osada. 2010. “Effects of Deep Throttling on Rocket Engine Systems.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-6727. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-6727
• King, E. J., and John Salvaggi. 1975. Analysis of Liquid Rocket Tankage for Model LR58-RM-4 Liquid Propellant. Defense Technical Information Center. https://doi.org/10.21236/ada022573
• Kinsler, Martin R. 1958. Effects of Aerodynamic Heating on X-15 Temperatures. NASA. https://ntrs.nasa.gov/citations/19930092395
• Kleckner, Harold F. 1946. Flight Tests of an All-Movable Horizontal Tail with Geared Unbalancing Tabs on the Curtiss XP-42 Airplane. NACA-TN-1139. NASA. https://ntrs.nasa.gov/citations/19930081790
• Kleinhenz, Julie E., Matthew C. Deans, Benjamin R. Stiegemeier, and Peter M. Psaras. 2013. “Thermal Stability of RP-2 for Hydrocarbon Boost Regenerative Cooling.” In Department of the Navy. https://ntrs.nasa.gov/citations/20130014379
• Kleinman, D. L. 1981. “Modeling Human Tracking Error in Several Different Anti-Tank Systems.” In JPL Proc. of the 17th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19820005826
• Klem, Mark D. 1990. “JANNAF Liquid Rocket Combustion Instability Panel Research Recommendations.” In JANNAF Combustion Meeting. https://ntrs.nasa.gov/citations/19910004178
• 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
• Klenke, D. J., and M. J. Hemsch. 1980. Consolidation of Data Base for Army Generalized Missile Model. NASA-CR-166273. NASA. https://ntrs.nasa.gov/citations/19820005173
• Klimas, Mindaugas, and Sigitas Kilikevičius. 2025. “Missile Launch-Induced Dynamics of a Vehicle-Integrated Air Defense System.” Preprint, . https://doi.org/10.20944/preprints202506.1432.v1
• Klimov, Anatoly, Sergey Leonov, Anatoly Pashina, Vladimir Skvortsov, Terrence Cain, and Boris Timofeev. 1999. “Influence of a Corona Discharge on the Supersonic Drag of an Axisymmetric Body.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4856. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4856
• Klopfer, G. H. 1985. High Mach Number Predictive Methods for Missile Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada158358
• 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
• Knaack, Marcelle Size. 1978. Encyclopedia of US Air Force Aircraft and Missile Systems. Volume 1. Post-World War II Fighters 1945-1973,. Defense Technical Information Center. https://doi.org/10.21236/ada057002
• Knaack, Marcelle S. 1988. Encyclopedia of U.S. Air Force Aircraft and Missile Systems. Volume 2. Post-World War II Bombers, 1945-1973. Defense Technical Information Center. https://doi.org/10.21236/ada209273
• Knab, Oliver, Manuel Frey, Josef Görgen, Katharina Quering, Dietmar Wiedmann, and Chris Mäding. 2009. “Progress in Combustion and Heat Transfer Modelling in Rocket Thrust Chamber Applied Engineering.” In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2009-5477. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5477
• Knab, Oliver, Anton Fröhlich, Dag Wennerberg, and Wolfgang Haslinger. 2002. “Advanced Cooling Circuit Layout for the VINCI Expander Cycle Thrust Chamber.” In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2002-4005. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4005
• Knab, O., D. Preclik, and D. Estublier. 1998. “Flow Field Prediction within Liquid Film Cooled Combustion Chambers of Storable Bi-Propellant Rocket Engines.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3370
• Knab, O., H. Riedmann, B. Ivancic, C. Höglauer, M. Frey, and T. Aichner. 2019. “Consequences of Modeling Demands on Numerical Rocket Thrust Chamber Flow Simulation Tools.” In Progress in Propulsion Physics – Volume 11. EDP Sciences. https://doi.org/10.1051/eucass/201911317
• Knacke, T. W. 1985. Parachute Recovery Systems Design Manual, Chapters 1 through 4 Offprint. Defense Technical Information Center. https://doi.org/10.21236/ada157839
• Knapp, H. A. 1965. Magnitude and Distribution of Weapon Effects for the Design of Shelters for Protection against Fallout. Defense Technical Information Center. https://doi.org/10.21236/ad0624370
• Knauber, R. N. 1982. Computer Program for Post-Flight Evaluation of the Control Surface Response for an Attitude Controlled Missile. NASA-CR-166032. NASA. https://ntrs.nasa.gov/citations/19860004451
• Knight, Doyle D. 2023. “Flight Control of the Kinzhal Missile Using Energy Deposition.” In AIAA AVIATION 2023 Forum. AIAA 2023-4493. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4493
• Knight, Michael R., Kyle Adriany, Stephen Guerin, Andrew Kieatiwong, and Elyce Bayat. 2015. “Thermo-Structural Enhancement of Liquid-Propellant Rocket Engine Thrust Chambers Using Functionally Graded Alloys.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-4069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4069
• 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
• 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
• Knutzon, Jared Scott. n.d. “Tracking and Control Design for a Virtual Reality Aided Teleoperation System.” PhD diss., Iowa State University. https://doi.org/10.31274/rtd-20200716-25
• Ko, William L., and Leslie Gong. 2001. Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission. NASA/TP-2001-210398. NASA. https://ntrs.nasa.gov/citations/20010098879
• Kobayashi, Kan, Yu Daimon, Nobuyuki Iizuka, HIroshi Tamura, Tohru Mitani, and Takuo Onodera. 2011. “Studies on Combustion Instability for Liquid Propellant Rocket Engines.” In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2011-6028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6028
• Koch, W., and R. Klemm. 2001. “Ground Target Tracking with STAP Radar.” IEE Proceedings - Radar, Sonar and Navigation 148 (3): 173–85. https://doi.org/10.1049/ip-rsn:20010381
• Kochenderfer, Mykel, J. Griffith, and James Kuchar. 2008. “Hazard Alerting Using Line-of-Sight Rate.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6630
• Kochi, K., and H. Dibble. 1963. “Stellar Techniques for Midcourse Navigation-Guidance.” In Guidance and Control Conference. AIAA 1963-357. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-357
• Kohiyar, F., M. Tremblay, and C. Gauthier. 1992. “Store Separation Model for Ripple Release.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-652. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-652
• Koike, Taiki, Yusuke Takahashi, Nobuyuki Oshima, and Kazuhiko Yamada. 2018. “Aerodynamic Heating Prediction of Flare-Type Membrane Inflatable Reentry Vehicle from Low Earth Orbit.” In 2018 AIAA Atmospheric Flight Mechanics Conference. AIAA 2018-0289. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-0289
• Kolesovas, J., and D. Svitra. 1976. “Mathematical Modeling of the Combustion Process in the Chamber of a Liquid Propellant Rocket Engine.” Lithuanian Mathematical Journal 15 (4): 632–42. https://doi.org/10.1007/bf00969794
• Kolodchak, I. L., A. Y. Semeniuk, and O. Y. Chudiak. 2012. “The Direction-Finding Characteristic Formation Approach in the Two Channel Radar Locator of a Missile Homing Device with Conical Scan.” Military Technical Collection 0 (7): 44–47. https://doi.org/10.33577/2312-4458.7.2012.44-47
• Korn, J., and D. L. Kleinman. 1978. “Modeling the Effects of High-G Stress on Pilots in a Tracking Task.” In NASA. Ames Res. Center The 14th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19790007422
• 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
• Koruba, Zbigniew, and Łukasz Nocoń. 2015. “Automatic Control of an Anti-Tank Guided Missile Based on Polynomial Functions.” Journal of Theoretical and Applied Mechanics: 139. https://doi.org/10.15632/jtam-pl.53.1.139
• Kostis, Theodoros G., Konstantinos G. Galanis, and Sokratis K. Katsikas. 2009. “Angular Glint Effects Generation for False Naval Target Verisimility Requirements.” Measurement Science and Technology 20 (10): 104016. https://doi.org/10.1088/0957-0233/20/10/104016
• Kou, Zp, and Hr Zhan. 2022. “Effects of Forebody on Supersonic Parachute Aerodynamic Performance.” Journal of Physics: Conference Series 2228 (1): 012013. https://doi.org/10.1088/1742-6596/2228/1/012013
• Koubek, F. J. 1963. High Temperature Resistant Materials for Missile Propulsion Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0408362
• Kovesdi, Casey, Paul Hunton, Jeremy Mohon, et al. 2022. Demonstration and Evaluation of the Human-Technology Integration Function Allocation Methodology. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/1881859
• Kowaleczko, Grzegorz. 2016. “Evaluation of the Jet Damping Effect on Flight Dynamics of a Homing Guided Missile.” Journal of Theoretical and Applied Mechanics: 893. https://doi.org/10.15632/jtam-pl.54.3.893
• Kozlov, Alexander, Jose Hinckel, and Adalberto Comiran. 1996. “Investigation of a Nozzle Tap-off Liquid Rocket Engine Scheme.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3118
• Kraft, Neal, and Andrew Lofthouse. 2011. “Non-Repeatability of Store Separation Trajectories from Internal Weapon Bays Due to Unsteady Cavity Flow Effects: Lessons Learned from a 2D Investigation.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-1238. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1238
• Krahmann, Elke. 2017. “United Kingdom: The Tactical Air-to-Surface Missile.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781315197197-5
• Kraiko, A. N., and R. A. Tkalenko. 1967. “Thin Flat Bodies of Minimum Wave Drag in Nonequilibrium Supersonic Flow.” Fluid Dynamics 2 (4): 37–41. https://doi.org/10.1007/bf01019533
• Krasich, Milena. 2004. “Test Design and Acceleration for Product Lifetime Reliability Demonstration.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/2004-01-1640
• Krause, James, and Gunter Stein. 1988. A General Adaptive Control Structure with a Missile Application. Defense Technical Information Center. https://doi.org/10.21236/ada206760
• 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
• Kreifeldt, J. G. 1965. A Sampled-Data Pursuit Tracking Model. NASA-CR-57221. NASA. https://ntrs.nasa.gov/citations/19650010148
• 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
• Kremzier, Emil J., and Joseph Davids. 1952. Performance Characteristics of Canard-Type Missile with Wing-Mounted Nacelle Engines at Mach Numbers 1.5 to 2.0. NACA-RM-E52J08. NASA. https://ntrs.nasa.gov/citations/19930087396
• 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. 1982a. “An Aerodynamic and Signature Shaping Technique for Developing Advanced Supersonic Missile Concepts.” In 20th Aerospace Sciences Meeting. AIAA 1982-373. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-373
• Krieger, R. 1982b. “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., R. Hood, and D. Gillies. 1980. “Correlation of Oil Flow and Aerodynamic Characteristics of Arbitrarily Shaped Advanced Missile Concepts.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1560. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1560
• 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
• Kriel, Marelize, and Herman le Roux. 2016. “Target Tracking Using a 2D Radar.” In Mobile Intelligent Autonomous Systems. CRC Press. https://doi.org/10.1201/b12690-33
• Krishna Paik, Hari, N. N. Sastry, and I. Santi Prabha. 2014. “Effectiveness of External Noise Jamming in Missile Borne Monopulse Radar Receivers.” International Journal of Engineering and Technology: 269–72. https://doi.org/10.7763/ijet.2014.v6.711
• Krishnabrahmam, V., N. Bharadwaj, K. N. Swamy, and V. V. S. Sarma. 2000. “Guided Missile with an Intelligent Agent.” Defence Science Journal 50 (1): 25–30. https://doi.org/10.14429/dsj.50.3319
• Kruczynski, L., B. Parkinson, and M. Wynne. 1971. “Sight Line Autopilot: A New Concept in Air Weapons.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-960. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-960
• Kruger, J. J., and I. S. Shaw. 1990. “A Fuzzy Learning System Emulating a Human Tracking Operator.” In [1990] Proceedings. First International Symposium on Uncertainty Modeling and Analysis. IEEE Comput. Soc. Press. https://doi.org/10.1109/isuma.1990.151216
• Krukowski, Danielle. n.d. “The Effect of Object Selection and Operator Movement on Situation Awareness in Virtual Reality.” PhD diss., Carleton University. https://doi.org/10.22215/etd/2019-13473
• Kubicki, Stephen W., Wesly Anderson, and Stephen D. Heister. 2020. “Further Experimental Study of a Hypergolically-Ignited Liquid-Liquid Rotating Detonation Rocket Engine.” In AIAA Scitech 2020 Forum. AIAA 2020-0196. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0196
• Kucuk, Mustafa, Mustafa Atahan Nuhoglu, Lutfiye Durak-Ata, and Hakan Ali Cirpan. 2024. “Defeating Angle Tracking: A Comprehensive Analysis of Scan Rate Modulation Jamming against Sequential Lobing Radars.” IET Radar, Sonar & Navigation 18 (11): 2122–33. https://doi.org/10.1049/rsn2.12617
• 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
• Kuehne, B. 1980. “An Assessment of Radome and Aero/control Models for Simulating Boresight Errors in Homing Missiles.” In Guidance and Control Conference. AIAA 1980-1750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1750
• Kugler, Justin. 2007. “Weapons Bay Flow and Tone Classification by Sequential Function Approximation.” In AIAA Infotech@Aerospace 2007 Conference and Exhibit. AIAA 2007-2974. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-2974
• Kukushkin, V., and A. Ivanchenko. 1993. “The Pasty Propellant Rocket Engine Development.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1754
• 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
• Kulkarni, V., and K. P. J. Reddy. 2009. “Drag Reduction by Counterflow Supersonic Jet for a Blunt Cone in High Enthalpy Flows.” In Shock Waves. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-85168-4_91
• Kumar, Prem, Abhijit Bhattacharya, and Radhakant Padhi. 2018b. “Minimum Drag Optimal Guidance with Final Flight Path Angle Constraint against Re-Entry Targets.” In 2018 AIAA Guidance, Navigation, and Control Conference. AIAA 2018-1320. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1320
• 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, M. Bharat, and P. Rajesh Kumar. 2022. “A Missile Jamming Design for Aircraft Defence Using Infrared Automated Counter Measures.” Journal of scientific research 66 (02): 163–71. https://doi.org/10.37398/jsr.2022.660222
• Kumar, G. Naresh, Ak Sarkar, and Se Talole. 2018a. “Dynamic Pressure Based Mid-Course Guidance Scheme for Hypersonic Boost-Glide Vehicle.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (9): 3211–22. https://doi.org/10.1177/0954410018795265
• Kumar, Amit, Nikhil K. Singh, and Sikha Hota. 2022. “Impact Angle Constrained Time-Optimal Guidance Law for Stationary Target Interception in 3D.” In AIAA SCITECH 2022 Forum. AIAA 2022-1391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1391
• Kumar, Amit, Nikhil K. Singh, and Sikha Hota. 2023a. “Look Angle Constrained Guidance Law for Stationary Target Interception in 3D.” In AIAA SCITECH 2023 Forum. AIAA 2023-1629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1629
• Kumar, Manoj, G. Kadam Sunil, V. Shanmugam, and G. Balu. 2021. “Hinge Moment Characterization of All Movable Control Surface.” In Lecture Notes in Mechanical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-15-9601-8_13
• 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
• 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, and Fumiaki Imado. 1989. “Advanced Missile Guidance System against a Very High Speed Maneuvering Target.” In Guidance, Navigation and Control Conference. AIAA 1989-3445. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3445
• Kuroda, Takeshi, and Fumiaki Imado. 1990. “Improved Advanced Missile Guidance System against a Hypersonic Target with Short Maneuvering Time.” In Guidance, Navigation and Control Conference. AIAA 1990-3379. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3379
• 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
• Kuti-Mensah, Ramshiv, and Williams Kyei. 2026. “Beyond the T-Distribution: Robust Confidence Interval Estimation in Small-Sample Inference Using Bootstrap and Bayesian Techniques.” International Journal of Applied Research in Social Sciences 8 (1): 25–41. https://doi.org/10.51594/ijarss.v8i1.2169
• Kuznetsov, N. 1993. “Closed-Cycle Liquid Propellant Rocket Engines.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1956. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1956
• Kwak, Dochan, and Cetin C. Kiris. 2010. “Simulation of a Liquid-Propellant Rocket Engine Subsystem.” In Scientific Computation. Springer Netherlands. https://doi.org/10.1007/978-94-007-0193-9_6
• Kwon, Hyeokmin. 2020. “Study on Internal Ballistic Performance Analysis for Single-Chamber Dual-Thrust Rocket Motors.” Journal of the Korean Society of Propulsion Engineers 24 (4): 1. https://doi.org/10.6108/kspe.2020.24.4.001
• Kwon, Boseong. 2026. “Experimental Identification and Phase-Bsed Correction of Missile Fin Actuator Dynamic Stiffness.” Journal of the Korea Institute of Military Science and Technology 29 (4): 283–92. https://doi.org/10.9766/kimst.2026.29.4.283
• Kyriakides, Ioannis. 2019. “Cognitive Fusion for Target Tracking with Foveal and Radar Nodes.” In Synthesis Lectures on Algorithms and Software in Engineering. Springer International Publishing. https://doi.org/10.1007/978-3-031-01528-1_3
• LaBotz, R. J., and R. L. Ewen. 1982. “Thrust Chamber Technology for Advanced Earth-to-Orbit Rocket Engines.” In Space Mankind’s Fourth Environment. Elsevier. https://doi.org/10.1016/b978-0-08-028708-9.50040-3
• Lacefield, T., and W. Sprow. 1994. “High Performance Russian NK-33 LOX/kerosene Liquid Rocket Engine.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-3397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3397
• Lackey, Shane, Robert Tramel, and D. Brian Landrum. 2011. “Weapons Bay Acoustic Suppression Using a Novel Rod in Crossflow Configuration.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-1239. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1239
• Ladner, Michael. 2016. Standard Missile-6 (SM-6). Defense Technical Information Center. https://doi.org/10.21236/ad1019541
• Lai, Chien Liang, and Pau Lo Hsu. 2011. “Design of Multi-Rate Remote Control Systems with Online Estimation of the Delay Time.” International Journal of Systems, Control and Communications 3 (2): 124. https://doi.org/10.1504/ijscc.2011.039864
• Lakshmi, Edury Vijaya, N. N. Sastry, and B. Prabhakar Rao. 2019. “Effect of Errors on Miss Distance of Missile Trackers in Active Decoy Environment.” International Journal of Electrical and Computer Engineering (IJECE) 9 (6): 4696. https://doi.org/10.11591/ijece.v9i6.pp4696-4702
• 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, Vincent. 2006. “Acceleration-Compensated Zero-Effort-Miss Guidance Law.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6083. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6083
• Lamb, M., W. C. Sawyer, D. L. Wassum, and C. D. Babb. 1979a. Pressure Distributions on Three Different Cruciform Aft-Control Surfaces of a Wingless Missile at Mach 1.60, 2.36, and 3.70. Volume 2: Clipped Delta Tail. NASA-TM-80097-VOL-2. NASA. https://ntrs.nasa.gov/citations/19790019968
• Lamb, M., W. C. Sawyer, D. L. Wassum, and C. D. Babb. 1979b. Pressure Distributions on Three Different Cruciform Aft-Tail Control Surfaces of a Wingless Missile at Mach 1.60, 2.36, and 3.70 Volume 1: Trapezoidal Tail. NASA-TM-80097-VOL-1. NASA. https://ntrs.nasa.gov/citations/19790018928
• Lamb, M., and C. D. Trescot Jr. 1980. A Study of Panel Loads and Centers of Pressure of Three Different Cruciform Aft-Tail Control Surfaces of a Wingless Missile from Mach 1.60 to 3.70. NASA-TM-81787. NASA. https://ntrs.nasa.gov/citations/19800014762
• Lambert, Warren George. n.d. “Optimization of the Range of an Unpowered Space Vehicle Subjected to an Aerodynamic Heating Constraint.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180817-4276
• 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
• 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
• Landry, Steven. 2010. “An Approach to Function Allocation for the Next Generation Air Transport System.” In Advances in Human Factors and Ergonomics Series. CRC Press. https://doi.org/10.1201/ebk1439834916-c53
• Lane, F. 1967. “Frequency Effects in the Radar Return from Turbulent Weakly Ionized Missile Wakes.” In 5th Aerospace Sciences Meeting. AIAA 1967-23. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-23
• Langley, Frank J., and John Demetrick. 1978. Modular Digital Missile Guidance. Defense Technical Information Center. https://doi.org/10.21236/ada072544
• Lapshina, T. V., and N. A. Ostapenko. 2009. “A Criterion for Minimum Wave Drag of a Body.” Doklady Physics 54 (1): 37–42. https://doi.org/10.1134/s1028335809010108
• “Large Eddy Simulation of Combustion Instability in a Subcritical Hydrogen Peroxide/kerosene Liquid Rocket Engine: Intermittency Route to Period-2 Thermoacoustic Instability.” 2023. Physics of Fluids 35 (6): 065145. https://doi.org/10.1063/5.0151462
• Laroche, E., M. Habibbalah, and P. Kuentzmann. 2000. “Numerical Analysis of Liquid Rocket Combustion Instability: Preliminary 3D Acoustic Calculations.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3497. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3497
• Lasek, M., and K. Sibilski. 2002. “Modelling of External Store Separation.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-687. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-687
• Latonov, V. V. 2018. “Programmed Strategies to Test the Quality of Line-of-Sight Guidance Control Using Video Images.” Moscow University Mechanics Bulletin 73 (6): 135–40. https://doi.org/10.3103/s002713301806002x
• Latonov, V. V., and V. V. Tikhomirov. 2018. “Line-of-Sight Guidance Control Using Video Images.” Moscow University Mechanics Bulletin 73 (1): 11–17. https://doi.org/10.3103/s002713301801003x
• Latto, W. T., Jr. 1967. Small Rocket Engine Patent. Patent Number: NASA-CASE-XLE-00685. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19700032676
• Lawhead, R. B., and L. P. Combs. 1963. “Modeling Techniques for Liquid Propellant Rocket Combustion Processes.” In Ninth Symposium (International) on Combustion. Elsevier. https://doi.org/10.1016/b978-1-4832-2759-7.50105-9
• Lawn, C. A., and B. Hannaford. 1993. “Performance Testing of Passive Communication and Control in Teleoperation with Time Delay.” In [1993] Proceedings IEEE International Conference on Robotics and Automation. IEEE Comput. Soc. Press. https://doi.org/10.1109/robot.1993.292239
• 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, Timothy J. 2005. Nuclear Thermal Rocket Propulsion Systems. Defense Technical Information Center. https://doi.org/10.21236/ada430931
• Lawrence, F., and Connie Fensky. 1996. “Grid Graphical Analysis Package (GridGAP) for Store Separation Testing at AEDC.” In Advanced Measurement and Ground Testing Conference. AIAA 1996-2277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2277
• 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
• Lawton, John A., and Craig A. Martell. 1997. Hybrid Neighboring-Optimal-Control and Lambert-Based Interceptor Boost-Phase Guidance,. Defense Technical Information Center. https://doi.org/10.21236/ada329043
• Lazur, Andrew, J. Sawyer, Brian Sullivan, and Larry Hudson. 1999. “Hypersonic Vehicle Control Surface Development.” In 9th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1999-4864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4864
• Le, Minh-Quyen. n.d. “Development of Bilateral Control for Pneumatic Actuated Teleoperation System.” PhD diss., Lyon, INSA. https://doi.org/10.70675/07f84928zc241z4629z9bfdz6a03fd1a82b0
• Le, Thien-Hiep, Ivan Mary, and Marc Terracol. 2005. “LES of Pressure Loads Suppression in Weapons Bay Flow.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-794. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-794
• Lebak, J. M. 2002. Preliminary Design Review: PCA Integrated Radar-Tracker Application. Defense Technical Information Center. https://doi.org/10.21236/ada419901
• Lechevin, Nicolas, and Camille Alain Rabbath. 2011. “Passivity-Based Robust Design of Proportional-Derivative Navigation Guidance Law.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6711. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6711
• Lee, Roland E. 1963. Heat Transfer to the Throat Region of a Solid Propellant Rocket Nozzle. Defense Technical Information Center. https://doi.org/10.21236/ad0406455
• Lee, Roland E. 1964. Measurements and Correlation of Heat Transfer in a Solid Propellant Rocket Nozzle. Defense Technical Information Center. https://doi.org/10.21236/ad0614626
• 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, S. 1993. “Initial Transient Analysis of Missile Launch-Tube Gas Flow and Its Interactions with Structures.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2455. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2455
• Lee, Yeon-Seok Liu. 2007a. “Performance Comparisons between Command to Line-of-Sight Guidance Law and Proportional Navigation Guidance Law in Short Range Surface-to-Air Missile.” Journal of Control Automation and Systems Engineering 13 (3): 273–78. https://doi.org/10.5302/j.icros.2007.13.3.273
• Lee, Sung-Mhan. 2007b. “Test and Evaluation of Onboard Equipments for Guided Missile via Captive Flight Test.” Journal of the Korean Society for Aeronautical & Space Sciences 35 (1): 73–78. https://doi.org/10.5139/jksas.2007.35.1.073
• Lee, Jin-Ik. 2013. “Shaping Guidance Law with Impact Angle Constraint for Alleviating Guidance Command at Terminal Phase.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4951. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4951
• Lee, Seung-Phil, Byung-Lae Cho, and Young-Soo Kim. 2016. “Two Unresolved Target Angle Estimation in Phase Comparison Monopulse Radar.” Journal of Korean Institute of Electromagnetic Engineering and Science 27 (6): 539–44. https://doi.org/10.5515/kjkiees.2016.27.6.539
• Lee, Jae, Kevin Dunworth, Magdi Rizk, William Westmoreland, and Donald Atkins. 2004b. “Studies of Combined Use of CFD and Wind Tunnel Test Approaches to Simulate a Store Separation from F-15E Using Efficient CFD Database Generation.” In 22nd Applied Aerodynamics Conference and Exhibit. AIAA 2004-4724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4724
• Lee, Kwang-Jin, Yeoung-Min Han, Jong-Gyu Kim, and Hwan-Seok Choi. 2012. “A Study on the Ignition Characteristics of Liquid Rocket Engine Thrust Chamber with Regenerative Cooling.” Journal of the Korean Society of Propulsion Engineers 16 (6): 73–78. https://doi.org/10.6108/kspe.2012.16.6.073
• Lee, Chae Heun, Chul Hyun, Jang Gyu Lee, Jin Yung Choi, and Sangkyung Sung. 2013a. “A Hybrid Guidance Law for a Strapdown Seeker to Maintain Lock-on Conditions against High Speed Targets.” Journal of Electrical Engineering and Technology 8 (1): 190–96. https://doi.org/10.5370/jeet.2013.8.1.190
• Lee, Bohyung, and Seokjae Jeong. 2025. “Simulation-based analysis of operational effectiveness using army weapon effectiveness analysis model of attack helicopter through manned–unmanned teaming (MUM-T) in plain, urban, and mountainous terrains environments.” Journal of Advances in Military Studies 8 (2): 43–66. https://doi.org/10.37944/jams.v8i2.284
• Lee, Seokwon, Jinrae Kim, Youdan Kim, and Namhoon Cho. 2024a. “Analytic Approach to Impact Time Guidance with Look Angle Constraint Using Exact Time-to-Go Solution.” Journal of Aerospace Engineering 37 (2): 04023118. https://doi.org/10.1061/jaeeez.aseng-5250
• Lee, Choong Hee, Gwang Tae Kim, Byung Ho Lee, and Young Ki Cho. 2019b. “Optimization of Voice Coil Motors for a Small Guided Missile Fin Actuator.” Journal of the Korean Society for Aeronautical & Space Sciences 47 (1): 59–65. https://doi.org/10.5139/jksas.2019.47.1.59
• 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, Seong-Hyeon, Seung-Jae Lee, In-O. Choi, and Kyung-Tae Kim. 2018a. “ICA-Based Phase-Comparison Monopulse Technique for Accurate Angle Estimation of Multiple Targets.” IET Radar, Sonar & Navigation 12 (3): 323–31. https://doi.org/10.1049/iet-rsn.2017.0156
• Lee, Sangbok, and Tae-Seong Roh. 2013. “Software for Design and Analysis of Liquid Rocket Engine System.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-4165. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4165
• Lee, Yong-In, Chang-Kyung Ryoo, and Eulgon Kim. 2003. “Optimal Guidance with Constraints on Impact Angle and Terminal Acceleration.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5795
• Lee, Keumoh, Chulsung Ryu, Seongchan Heo, and Hwanseok Choi. 2017. “Predictions of Fatigue Life of Copper Alloy for Regenerative Cooling Channel of Thrust Chamber.” Journal of the Korean Society of Propulsion Engineers 21 (6): 73–82. https://doi.org/10.6108/kspe.2017.21.6.073
• 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, Roland E., William J. Yanta, and Annette C. Leonas. 1969. Velocity Profile, Skin-Friction Balance and Heat-Transfer Measurements of the Turbulent Boundary Layer at Mach 5 and Zero-Pressure Gradient. Defense Technical Information Center. https://doi.org/10.21236/ad0697929
• 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
• Leese, Grady W. 1966. Rocket-Blast-Resistant Materials: Rocket Engine Blast Tests on Expedient Surfacing Materials. Defense Technical Information Center. https://doi.org/10.21236/ad0633264
• Lefebvre, Maëlis. n.d. “Impact of Dynamic Environments and View Perspective on Teleoperation Performance: From Laboratory to Real-Life Settings.” PhD diss., Toulouse, ISAE. https://doi.org/10.70675/f57ea4bfz3b38z4666zb052z9095b9b56759
• Leger, J. 1975. “C-5A Air Launch of Minuteman I Missile.” In Aircraft Systems and Technology Meeting. AIAA 1975-969. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-969
• Legkiy, N. М., and I. V. Unchenko. 2024. “Mathematical Modeling of Microwave Channels of a Semi-Active Radar Homing Head.” Russian Technological Journal 12 (2): 48–56. https://doi.org/10.32362/2500-316x-2024-12-2-48-56
• Lei, Junwei, Chao Dong, and Lei Meng. 2025a. “An Optimal Guidance Law Design for Aircraft with Fall Angle Constraint.” In International Conference on Electrical Engineering and Intelligent Systems (IC2EIS 2025), edited by Mohan Kolhe, Bin Gou. SPIE. https://doi.org/10.1117/12.3069190
• Lei, Yu, Wei Zhi Jiang, Bo Gao, and Zhu Wei. 2015. “Modeling of Anti-Aircraft Weapon Systems Cooperative Guidance for Anti-Aircraft Missile.” Applied Mechanics and Materials 719-720: 504–13. https://doi.org/10.4028/www.scientific.net/amm.719-720.504
• Lei, Jun Wei, Jing Shen Tang, and Hua Li Wu. 2011. “Research on the Relationship between Stabilization Problem and Tracking Problem of Missile Control System.” Applied Mechanics and Materials 66-68: 199–202. https://doi.org/10.4028/www.scientific.net/amm.66-68.199
• Leighton, Russell A. 1982. Quick-Look Structural Analysis Techniques for Solid Rocket Propellant Grains. Defense Technical Information Center. https://doi.org/10.21236/ada119841
• Lempert, Mark. 1975. Air Launch Characteristics of the MQM-74C Target Drone from DC-130A Airplane. Defense Technical Information Center. https://doi.org/10.21236/ada004190
• Lengyel, J., and Patrick Sosa. 2021. “Air Launched Effects Payload and Air Vehicle Integration.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0077-2021-16823
• Lenhard Jr., Doody Robert W., and Margaret P. 1963. Accuracy of Meteorological Data Obtained by Tracking the Robin with MPS-19 Radar. Defense Technical Information Center. https://doi.org/10.21236/ad0434379
• Leopold, Tobias. 2023. Determination of Sample Size and Test Duration of Reliability Demonstration Tests – Challenges and Opportunities. https://doi.org/10.46720/eb2023-tst-003
• Lesage, F., J. Nicolle, and M.-A. Boulianne. 2000. “Navier-Stokes Computations of High Angle of Attack Missile Flowfields.” In 18th Applied Aerodynamics Conference. AIAA 2000-4212. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4212
• 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, D., M. Dillenius, and J. Gjestvang. 2002. “Store Separation Simulation of Penguin Missile from Helicopters.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-278
• 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
• Lesieutre, Daniel J., Michael R. Mendenhall, Susana M. Nazario, and Michael J. Hemsch. 1987. Aerodynamic Characteristics of Cruciform Missiles at High Angles of Attack. AIAA PAPER 87-0212. Nielsen Engineering and Research, Inc. https://ntrs.nasa.gov/citations/19870035215
• Leslie, D. C. M., and J. D. Perry. 1954. “Wave Drag of Wings at Supersonic Speeds.” Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences 225 (1161): 213–25. https://doi.org/10.1098/rspa.1954.0198
• 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
• Levi, R., and P. H. Stahlhuth. 1977. Low Cost Servo Actuator for Tactical Missile Thrust Vector Control (TVC). Defense Technical Information Center. https://doi.org/10.21236/adb019655
• 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
• 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, Hao. 2010. “Improved Hybrid Robust Control Method for the Electromechanical Actuator in Aircrafts.” Chinese Journal of Mechanical Engineering 23 (04): 443. https://doi.org/10.3901/cjme.2010.04.443
• Li, Feng. 2014. “Investigation of Aerodynamics and Flight Mechanics Characteristics of Ground Effect Missile.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0215. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0215
• Li, Hao. 2015. “Cooperative Attack of Multiple Missiles with Ideal-Line-of-Sight-Guidance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0618. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0618
• Li, Xiangxiang, Wanchun Chen, Zhongyuan Chen, and Shen Zhang. 2023b. “An Impact Angle Control Guidance via Self-Restrained Look Angle Shaping.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_583
• Li, Yuanchang, Guiming Chen, and Lingliang Xu. 2025h. “A Review of Research on Evaluation Methods for Missile Weapon System Effectiveness.” Journal of innovation and development 11 (1): 1–3. https://doi.org/10.54097/z8256026
• Li, Hang, and Wusheng Chou. 2025. “Dynamic Surface Control for Nonlinear Bilateral Teleoperation Manipulators with Guaranteed Transient Performance.” Tsinghua Science and Technology 30 (6): 2505–21. https://doi.org/10.26599/tst.2024.9010096
• Li, Yu, Naigang Cui, and Siyuan Rong. 2009. “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, 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, Yinghao, and Rong Fan. 2018. “The Solution and Simulation of Air-to-Air Missile Launch Envelope Based on Cooperative Air Combat of Manned/Unmanned Formation.” In Proceedings of the 2018 International Conference on Network, Communication, Computer Engineering (NCCE 2018). Atlantis Press. https://doi.org/10.2991/ncce-18.2018.32
• Li, Zhengda, Lionel Ganippa, and Thanos Megaritis. 2026d. “Literature Review of Liquid Rocket Engine Injector Design and Technology.” Preprint, . https://doi.org/10.20944/preprints202601.1002.v1
• Li, Xuan, Rui Mao, Sheng Luo, and Jiang Lou. 2025c. “Cooperative Guidance of Glide Bombs Based on Gaussian Pseudo-Spectral Method.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2216-0_19
• Li, Huiyang, Nadine Sarter, Christopher Wickens, and Angelia Sebok. 2013a. “Supporting Human-Automation Collaboration through Dynamic Function Allocation: The Case of Space Teleoperation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 57 (1): 359–63. https://doi.org/10.1177/1541931213571078
• Li, Xinbin, Zhihan Tian, Miao Liu, Song Han, and Shunshun Chen. 2024a. “Adaptive Fast Integral Sliding Mode Control of Teleoperation Manipulator System Based on Prescribed Performance.” Preprint, . https://doi.org/10.22541/au.171922338.86861450/v1
• Li, H.-W., and J. Wang. 2012. “Particle Filter for Manoeuvring Target Tracking via Passive Radar Measurements with Glint Noise.” IET Radar, Sonar & Navigation 6 (3): 180–89. https://doi.org/10.1049/iet-rsn.2011.0075
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015b. “Model Reference Bilateral Teleoperation Control.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_5
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015c. “Model-Based Bilateral Teleoperation Control.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_4
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015d. “Modeling of Teleoperation System.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_3
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015e. “Multilateral Cooperative Teleoperation.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_8
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015g. “Single-Master-Multi-Slaves Teleoperation.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_6
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015h. “Trilateral Teleoperation.” In Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2_7
• Li, Zhaohui, and Hai-xia Xu. 2011. “Measurement for Missile-Target Miss Distance Based on 3D Rectilinear Motion with Constant Acceleration.” JOURNAL OF ELECTRONICS INFORMATION TECHNOLOGY 30 (10): 2329–32. https://doi.org/10.3724/sp.j.1146.2007.00251
• Li, Peng Cheng, Suo Chang Yang, and De Long Feng. 2014d. “Research on the Improved Proportional Navigation Guidance Law Using CADET.” Applied Mechanics and Materials 488-489: 1061–63. https://doi.org/10.4028/www.scientific.net/amm.488-489.1061
• 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, Ke, and Xing Zhao. 2025. “Highly Accurate Radar Cross-Section Measurement without Reference Target.” Journal of Physics: Conference Series 2967 (1): 012001. https://doi.org/10.1088/1742-6596/2967/1/012001
• Li, Weiyi, Jisong Zhao, and Jiahong Deng. 2026f. “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, Haoxing, Di Zhu, Ruiheng Lv, et al. 2019b. “Angular Glint Compensation for Seekers Based on Multicarrier Techniques.” Journal of Engineering 2019 (21): 7705–8. https://doi.org/10.1049/joe.2019.0760
• 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
• Lianos, D., Y. Shtessel, and I. Shkolnikov. 2001. “Integrated Guidance-Control System of a Homing Interceptor: Sliding Mode Approach.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4218. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4218
• 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
• “Lift/Drag Ratios of Optimised Slewed Wings at Supersonic Speeds.” 1962. Aeronautical Quarterly 13 (1): 91–92. https://doi.org/10.1017/s0001925900002274
• Lighthill, M. J. 1956. “The Wave Drag at Zero Lift of Slender Delta Wings and Similar Configurations.” Journal of Fluid Mechanics 1 (3): 337–48. https://doi.org/10.1017/s0022112056000196
• 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
• Lijewski, Lawrence, and Lawrence Lijewski. 1997. “Comparison of Transonic Store Separation Trajectory Predictions Using the Pegasus/DXEAGLE and Beggar Codes.” In 15th Applied Aerodynamics Conference. AIAA 1997-2202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2202
• Lijewski, Lawrence, and Norman Suhs. 1992. “Chimera-EAGLE Store Separation.” In Astrodynamics Conference. AIAA 1992-4569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4569
• Lilliefors, H. W. 1957. “A Hand-Computation Determination of Kill Probability for Weapons Having Spherical Lethal Volume.” Operations Research 5 (3): 416–21. https://doi.org/10.1287/opre.5.3.416
• Lim, Samuel. 1992. “Impact of Jammer Side Information on the Performance of Anti-Jam Systems.” In 14th International Communication Satellite Systems Conference and Exhibit. AIAA 1992-1807. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-1807
• Lim, Kair-Chuan, and Paul E. George II. 1987. Combustion Stability Analysis of Preburners in Liquid Propellant Rocket Engines during Shutdown. AIAA PAPER 87-1776. Tennessee Univ. https://ntrs.nasa.gov/citations/19870057923
• Lim, Byoungjik, Keejoo Lee, Junseong Lee, and Jaesung Park. 2025. “An Additively Manufactured Thrust Chamber with Alternating Cooling Channels for Cyrogenic Fuel and Oxidizer.” In AIAA SCITECH 2025 Forum. AIAA 2025-0759. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0759
• Limerick, C. 1991. “Component Design Concerns for Deep Throttling H2/O2 Rocket Engines.” In 27th Joint Propulsion Conference. AIAA 1991-2209. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2209
• Lin, K. 1986. “The Gun-Launched Test for a Supersonic Parachute.” In 9th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1986-2474. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2474
• Lin, Ching-Fang, John Bibel, Ernest Ohlmeyer, and Steve Malyevac. 1998. “Optimal Design of Integrated Missile Guidance and Control.” In AIAA and SAE, 1998 World Aviation Conference. AIAA 1998-5519. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-5519
• Lin, Guohuai, Xun Chen, Jiecai Long, Jianfeng Sun, and Renquan Lu. 2025. “NN-Based Fixed-Time Human-in-the-Loop Formation Control for Nonlinear MASs with Time-Varying Delay.” Preprint, . https://doi.org/10.2139/ssrn.5499588
• 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., J. Juang, Q. Wang, J. Cloutier, and J. Evers. 1991. “High Performance, Adaptive, Robust Bank-to-Turn Missile Autopilot Design.” In Navigation and Control Conference. AIAA 1991-2614. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-2614
• 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, T., L. Sproul, and R. Muskat. 1995. “Persistent Roll Resonance Induced by missile/RV Aeroelastic Behavior.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-65. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-65
• Lind, Rick, James Buffington, and Andrew Sparks. 1999. “Multi-Loop Aeroservoelastic Control of a Hypersonic Vehicle.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4123. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4123
• Lindberg, Robert E. 1989. “Overview of the Pegasus Air-Launched Space Booster.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/892308
• Lindsay, E. Earl, and J. L. Jordan. 1975. Experimental Static Stability Studies of Several Tactical Missile Configurations at Mach Numbers from 1.76 to 3.01. Defense Technical Information Center. https://doi.org/10.21236/ada009137
• “Linear Acoustic Gains and Losses in Solid Propellant Rocket Motors.” 1964. In Solid Propellant Rocket Conference. AIAA 1964-134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-134
• Lingard, John, and Matt Darley. 2005. “Simulation of Parachute Fluid Structure Interaction in Supersonic Flow.” In 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2005-1607. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1607
• Lingard, J. S., Arrun Saunders, John C. Underwood, Steven Rogers, James Merrifield, and Luca Ferracina. 2017. “Supersonic Parachute Testing Using a MAXUS Sounding Rocket Piggy-Back Payload.” In 24th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2017-3724. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3724
• Lingard, J. Stephen, John C. Underwood, Matthew G. Darley, Lionel Marraffa, and Luca Ferracina. 2013. “Supersonic Parachute Aerodynamic Testing and Fluid Structure Interaction Simulation.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1365. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1365
• “Liquid Propellant Rocket Engines.” n.d. In Rocket and Spacecraft Propulsion. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-69203-4_3
• “Liquid Propellant Rocket Engines in Germany.” 2006a. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0737.0784
• “Liquid Propellant Rocket Engines in India.” 2006b. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0881.0886
• “Liquid Propellant Rocket Engines in Russia, Ukraine, and the Former Soviet Union.” 2006c. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0531.0736
• “Liquid Propellant Rocket Engines in the People’s Republic of China.” 2006d. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0865.0880
• “Liquid Propellant Rocket Engines in the United Kingdom or Britain.” 2006e. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0843.0864
• “Liquid Propellant Rocket Engines in the United States (Summary).” 2006f. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0303.0530
• “Liquid Propellant Rocket-Engine Organizations Worldwide, 1932 to 2003.” 2006. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0293.0302
• Liquid Rocket Engine Combustion Stabilization Devices. 1974. NASA-SP-8113. NASA. https://ntrs.nasa.gov/citations/19750020175
• Liquid Rocket Engine Fluid-Cooled Combustion Chambers. 1972. NASA-SP-8087. NASA. https://ntrs.nasa.gov/citations/19730022965
• Liquid Rocket Engine Self-Cooled Combustion Chambers. 1977. NASA-SP-8124. NASA. https://ntrs.nasa.gov/citations/19780013268
• Litaker, Harry L., Jr., Kara H. Beaton, Zu Qun Li, and John F. Lewis. 2025. “Lunar Terrain Vehicle (LTV) Remote Teleoperation Studies under Four Lunar Communication Latencies.” In 46th International IEEE Aerospace Conference. https://ntrs.nasa.gov/citations/20240011392
• Litaker, Harry L., Jr., Zu Qun Li, Kara H. Beaton, and John F. Lewis. 2024. Lunar Terrain Vehicle (LTV) Remote Teleoperation Studies under Four Lunar Communication Latencies. NASA/TM-20240001217. NASA. https://ntrs.nasa.gov/citations/20240001217
• Litchford, R. J. 2005. Baseline Computational Fluid Dynamics Methodology for Longitudinal-Mode Liquid-Propellant Rocket Combustion Instability. NASA/TP-2005-214188. NASA. https://ntrs.nasa.gov/citations/20060024984
• Litchford, Ron, and San-Mou Jeng. 1992. “Liquid Rocket Spray Combustion Stability Analysis.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3227
• Liu, Yue-Huan. 2007. “Performance Comparison between True Proportional Navigation Guidance Law and Pure Proportional Navigation Guidance Law.” Journal of Control Automation and Systems Engineering 13 (6): 525–30. https://doi.org/10.5302/j.icros.2007.13.6.525
• Liu, Fang, and Wan Chun Chen. 2011. “Controller Design for Spinning Missile with the Actuator Limit.” Advanced materials research 383-390: 45–51. https://doi.org/10.4028/www.scientific.net/amr.383-390.45
• Liu, Weiqiang, Qizhi Chen, and Baoyuan Wu. 1998. “Transpiration Cooling of Rocket Thrust Chamber with Liquid Oxygen.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-890
• Liu, Rui, Fan Ding, Jindong Zhang, and Huangrong Zhou. 2024b. “Generalized Monopulse Angle Measurement for Conformal Antenna Arrays.” In Fifteenth International Conference on Signal Processing Systems (ICSPS 2023), edited by Zhenkai Zhang, Cheng Li. SPIE. https://doi.org/10.1117/12.3023186
• Liu, Yating, Jingbo Duan, Buqing Xu, and Jiaqi Wu. 2024g. “Transient Aerodynamic Heating Effects on Aeroelastic Dynamic Response of Curved Fiber-Reinforced Composite Panel in Supersonic Airflow.” International Journal of Structural Stability and Dynamics 25 (05): 2550052. https://doi.org/10.1142/s021945542550052x
• Liu, Yuwen, Ming Jiang, Zhiyuan Zhang, and Yanan Duan. 2019d. “Study on the Impact of Altitude on the Hitting Accuracy of Laser Terminal Guided Projectile and Its Improvement.” Journal of Physics: Conference Series 1325 (1): 012130. https://doi.org/10.1088/1742-6596/1325/1/012130
• Liu, Liguo, Mo Jin-Jun, Yunqi Fu, and Naichang Yuan. 2014. “Study on near Field Angular Glint Computation Based on GRECO.” JOURNAL OF ELECTRONICS INFORMATION TECHNOLOGY 35 (4): 865–70. https://doi.org/10.3724/sp.j.1146.2012.01573
• Liu, Shuyu, Shu Liang, Jie Wang, and Yiguang Hong. 2026a. “Cascaded Model Predictive Control for Coordinated Formation of Hypersonic Glide Vehicle Swarms.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-8435-2_9
• Liu, Xinyi, Qiang Liu, Zhenbing Luo, Mingbo Sun, and Junqiang Song. 2026b. “Conditionally Averaged Skin-Friction Decomposition on the Wall-Attached Reynolds Stress Structure in Supersonic Turbulent Boundary Layers.” Journal of Fluid Mechanics 1030: A33. https://doi.org/10.1017/jfm.2026.11173
• Liu, Jiaxun, Gangyi Liu, Wenyuan Zhou, Xueqing He, Qingchun Yang, and Xu Xu. 2023d. “Numerical Investigation of Liquid Oxygen Filling Process in Liquid Rocket Engine by a Multi-Dimensional Co-Simulation Method.” Preprint, . https://doi.org/10.2139/ssrn.4590657
• Liu, Jiaxun, Gangyi Liu, Wenyuan Zhou, Xueqing He, Qingchun Yang, and Xu Xu. 2024e. “Numerical Investigation of Liquid Oxygen Filling Process in Liquid Rocket Engine by a Multi-Dimensional Co-Simulation Method.” Preprint, . https://doi.org/10.2139/ssrn.4792547
• Liu, Yanfang, Naiming Qi, and Jinjun Shan. 2013a. “Cooperative Interception with Double-Line-of-Sight-Measuring.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-5112. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-5112
• Liu, Weiqiang, and Chen Qizhi. 1996. “Recession Analysis for Carbon-Carbon Composite Nozzle of Liquid Propellant Rocket Engine.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3214
• Liu, YongShan, Li Song, and JingLong Li. 2018. “Extraction and Filter Algorithm of Guidance Information for Full-Strapdown Seeker on Rotation Missile.” MATEC Web of Conferences 214: 03008. https://doi.org/10.1051/matecconf/201821403008
• Liu, Zhiming, Shaoqian Song, Zhiguo Song, Tian Dong, and Xinmin Chen. 2024f. “Terminal Guidance Law Design Considering Seeker SAR Imaging and Field of View Constraint.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-8658-9_32
• Liu, Ying, Wei Feng Tian, Jian Zhao, Shi Qing Zhu, and Ge Wen Yang. 2013c. “Line-of-Sight Angle Rate Reconstruction for Phased Array Strapdown Seeker.” Advanced materials research 645: 196–201. https://doi.org/10.4028/www.scientific.net/amr.645.196
• Liu, Xiaoming, Jiandong Wang, and Xudong Wang. 2010a. “Anti-Radiation-Missile Detection Based on Parameterized Time-Frequency Analysis.” Journal of Computer Applications 30 (11): 3108–10. https://doi.org/10.3724/sp.j.1087.2010.03108
• Liu, Xuancen, Bin Wang, Houyuan Xiao, Jiayi Tian, and Shifeng Zhang. 2023a. “Biased Proportional Navigation Guidance for Autonomous Landing of Unmanned Seaplane Considering Look Angle Constraint.” In Proceedings of the 2023 International Joint Conference on Robotics and Artificial Intelligence. ACM. https://doi.org/10.1145/3632971.3633003
• Liu, Weidong, Zhenguo Wang, Jin Zhou, and Fengchen Zhuang. 1996. “Numerical Simulation of Unsteady Flow in Liquid Propellant Rocket Engine with PISO Algorithm.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3124. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3124
• Liu, Weidong, Zhenguo Wang, Fen Zhuang, and Cheng Zhuang. 1995. “Numerical Analysis of Combustion Instability in Liquid Propellant Rocket Engine.” In 31st Joint Propulsion Conference and Exhibit. AIAA 1995-3117. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3117
• Liu, Xiaodong, Yunjie Wu, Yong Deng, and Song Xiao. 2013b. “A Global Sliding Mode Controller for Missile Electromechanical Actuator Servo System.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228 (7): 1095–1104. https://doi.org/10.1177/0954410013485522
• Liu, Kun, and Yulin Zhang. 2000. “A Study on Versatile Simulation of Liquid Propellant Rocket Engine Systems Transients.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3771. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3771
• Liu Jinrong, Wang Jun, and Yu Yuan Meng. 2009. “Detection and Recognition of Anti-Ridiation Missile Based on External Illuminator.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0437
• Lo, Hsu. 1948. Determination of Transient Skin Temperature of Conical Bodies during Short-Time, High-Speed Flight. NACA-TN-1725. NASA. https://ntrs.nasa.gov/citations/19930082418
• Lo, T., T. Wong, and J. Litva. 1991. “New Technique for Low-Angle Radar Tracking.” Electronics Letters 27 (6): 529–31. https://doi.org/10.1049/el:19910333
• 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, 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, A. S. 1950. Some Tactical Limitations of Beam-Rider, Command, and Semi-Active Homing Guidance Systems. Defense Technical Information Center. https://doi.org/10.21236/adc954460
• 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
• Logan, William, Roger Davis, Nesrin Sarigul-Klijn, and Marti Sarigul-Klijn. 2006. “Engine Thrust Effects on Air-Launched Rocket Aerodynamic Characteristics at High Angle of Attack.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4963. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4963
• Lohner, Rainald, and Joseph Baum. 1991. “Three-Dimensional Store Separation Using a Finite Element Solver Andadaptive Remeshing.” In 29th Aerospace Sciences Meeting. AIAA 1991-602. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-602
• Long, G. A. 1950. “MISSILE GUIDANCE.” Navigation 2 (8): 290–94. https://doi.org/10.1002/j.2161-4296.1950.tb00580.x
• Long, Matthew R. 2014. “Design-to-Cost and Robust Liquid Rocket Engine Design Using PMDA/PMDO and MBSE.” In AIAA SPACE 2014 Conference and Exposition. AIAA 2014-4408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-4408
• 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
• López, D., D. Domínguez, and J. Gonzalo. 2014. “Optimization of Air-Ejected Rocket/missile Geometries under Validated Supersonic Flow Field Simulations.” In AIP Conference Proceedings, vol. 1637. AIP Publishing LLC. https://doi.org/10.1063/1.4904629
• Lorenz, Sven, and Andreas Bierig. 2013. “Robustness Analysis Related to the Control Design of the SHEFEX-II Hypersonic Canard Control Experiment.” In AIAA Guidance, Navigation, and Control (GNC) Conference. AIAA 2013-4857. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4857
• 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
• Lorenz, Sydney R., and Jennifer Lam. 2026. “Small-Scale Supersonic Parachute Design and Fabrication.” In 28th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2026-3830. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-3830
• Lorenzetto, J. H., and L. Crocco. 1971. Theoretical Investigation on Transverse Mode Combustion Instability for Liquid Propellant Rockets. NASA-CR-120781. NASA. https://ntrs.nasa.gov/citations/19710029270
• Lores, M., and B. Zinn. 1973. “Nonlinear Longitudinal Combustion Instability in Rocket Motors.” In 11th Aerospace Sciences Meeting. AIAA 1973-217. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-217
• Lovtsov, D. A., and D. S. Karpov. 2011. “Dynamic Planning of Navigation Determinations of Airspace and Missile Objects in an Automated Flight Test Control System.” Solar System Research 45 (7): 645–51. https://doi.org/10.1134/s003809461107015x
• “Low Angle Tracking with Symmetric Beam Pattern Monopulse Based on Uniform Circular Array.” 2017. In 2017 6th International Conference on Advanced Materials and Computer Science (ICAMCS 2017). Clausius Scientific Press Inc. https://doi.org/10.23977/icamcs.2017.1027
• “Low Frequency Oscillations in Liquid Rocket Combustion Chambers.” 2008. In Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866913.0001.0042
• Lu, Ping. 1994. “A General Nonlinear Guidance Law: Application to a Launch Vehicle.” In Guidance, Navigation, and Control Conference. AIAA 1994-3632. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3632
• Lu, Haibo, Deyou Xu, and Weiqiang Liu. 2024b. “Research on Aerodynamic Drag Optimization Design of Base Cavity for Slender Body.” In Third International Conference on Mechatronics and Mechanical Engineering (ICMME 2024), edited by Yucheng Jiang. SPIE. https://doi.org/10.1117/12.3039168
• Lu, Haibo, and Qunfang Zhang. 2022. “Numerical Investigation on Aerodynamic Drag Reducing of Slender Body with Non-Cylindrical Base Cavity.” In Advances in Transdisciplinary Engineering. IOS Press. https://doi.org/10.3233/atde220838
• Lu, Qin, Ping Zhang, Longfei Hu, and Guiqing Jiang. 2016. “Analytical Solution on Transient Aerodynamic Heating of Hypersonic Vehicle Hot Structure.” In Proceedings of the 2016 International Conference on Innovative Material Science and Technology (IMST 2016). Atlantis Press. https://doi.org/10.2991/imst-16.2016.15
• Lu, Haoran, Wei Zheng, Xiaohua Chang, and Wei Dai. 2022. “Research on Cooperative Target Assignment and Guidance Method of Hypersonic Glide Vehicle.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-9492-9_258
• Luce, Richard W., Jr. 1949. Deflections of a Supersonic Wing Due to Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ada278113
• 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
• Lum, Kai-Yew. 2003. “Infinite-Dimensional Linearization and Extended Adjoint Method for Nonlinear Homing Loop Analysis.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5449
• Lumb, S., and Robert Cayse. 1992. “Transient Aerodynamics of a High Dynamic Pressure Shroud Separation for a Ground-Based Interceptor Missile.” In Annual Interceptor Technology Conference. AIAA 1992-2820. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2820
• Lundstrom, Reginald R., and Ruth I. Whitman. 1959. Analytical Investigation of a Flicker-Type Roll Control for a Mach Number 6 Missile with Aerodynamic Controls over an Altitude Range of 82,000 to 282,000 Feet. NASA-MEMO-4-23-59L. NASA. https://ntrs.nasa.gov/citations/19980228475
• Luo, Shi Jie. 2014. “Asymmetrical Lateral Jet Interaction on a Slender Body in Supersonic Flow.” Applied Mechanics and Materials 565: 107–12. https://doi.org/10.4028/www.scientific.net/amm.565.107
• Luo, Haowen, and Shaoming He. 2026. “Parallel-Curriculum Reinforcement Learning Guidance for Low-Maneuverability-Ratio Interception with Active-Seeker Measurements.” Preprint, . https://doi.org/10.2139/ssrn.7524430
• Luo, Shi Jie, Yao Feng Liu, and Ning Cao. 2013. “Numerical Simulation of Lateral Jet Interaction a Slender Body in Supersonic Flow.” Applied Mechanics and Materials 404: 296–301. https://doi.org/10.4028/www.scientific.net/amm.404.296
• Luo, Shi-Jie, Yao-Feng Liu, and Yu-Wei Liu. 2020b. “Visualization of Asymmetric Separation Induced by Lateral Jet Interaction on a Slender Body in Supersonic Flow.” International Journal of Modern Physics B 34 (14n16): 2040081. https://doi.org/10.1142/s0217979220400810
• Luo, Jianjun, and Erlong Su. 2016. “Hypersonic Entry Guidance Design Based on Three-Dimensional Equilibrium Glide Space.” SCIENTIA SINICA Informationis 46 (9): 1339–56. https://doi.org/10.1360/n112015-00172
• Lusser, Robert. 1952. Planning and Conducting Reliability Test Programs for Guided Missiles. Defense Technical Information Center. https://doi.org/10.21236/ad0007061
• Lv, Maolong, and Chuhan Zhou. 2023. “Adaptive Performance-Constrained Synchronization Control for Hypersonic Flight Vehicle Swarms: A Novel Finite-Time Convergence Protocol Methodology.” Guidance, Navigation and Control 03 (02): 2350011. https://doi.org/10.1142/s2737480723500115
• Lyalin, Victor, and Victor Morozov. 2005. “Comparative Analysis of the Recovery Parachute Systems Efficiency.” In 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2005-1682. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-1682
• Lyon INC Detroit MI. 1963. Deep Drawn Ausforming Development Program, 12 Dia. Rocket Motor Chambers. Defense Technical Information Center. https://doi.org/10.21236/ad0401194
• Lysaght, Robert J., Susan G. Hill, A. O. Dick, Brian D. Plamondon, and Paul M. Linton. 1989. Operator Workload: Comprehensive Review and Evaluation of Operator Workload Methodologies. Defense Technical Information Center. https://doi.org/10.21236/ada212879
• Lyu, Yan, and Xiaowei Wang. 2024. Two New Launch Platforms for Air-Launched Rockets. https://doi.org/10.52202/078373-0094
• Ma, MingSheng, Youqi Deng, Ming Zheng, and Naichun Zhou. 2005. “Navier-Stokes Computations for a Grid Fin Missile.” In 23rd AIAA Applied Aerodynamics Conference. AIAA 2005-4973. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4973
• Ma, Jian, Yongsheng Hao, Jian Miao, and Jianmao Zhang. 2007. “A Design Proposal of a Certain Missile Tactical Command System Based on Beidou Satellite Communication and GPS Positioning Techniques.” In SPIE Proceedings, vol. 6795, edited by Cheng Wang, Shan Zhong, Jiaolong Wei. SPIE. https://doi.org/10.1117/12.775034
• Ma, Jirong, Zhi Jiang, Zheming Zhang, Yuanbo Liu, and Shujun Yang. 2026. “A Hit Accuracy Analysis Method for Weapon System.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-6557-3_23
• Ma, Qiang, and Yu Qiang Jin. 2011. “Supersonic Missile Control with PI Sliding Mode Method.” Advanced materials research 295-297: 1773–76. https://doi.org/10.4028/www.scientific.net/amr.295-297.1773
• Ma Zhen-qiu and Cui Wei. 2009. “Angle Measurement Performance Analysis and Simulation of Sum and Difference Phase-Comparison Monopulse Radar.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0369
• Mabey, D. G. 1979. “Influence of the Wake Component on Turbulent Skin Friction at Subsonic and Supersonic Speeds.” Aeronautical Quarterly 30 (4): 590–606. https://doi.org/10.1017/s000192590000874x
• MacCarthy, R. W. 1954. Textiles for Parachutes in Aircraft Deceleration and Missile Recovery. Defense Technical Information Center. https://doi.org/10.21236/ada451760
• Macek, Andrej, and J. M. Semple. 1972. Composition and Combustion Characteristics of Condensed Exhaust from Boron-Containing Fuel-Rich Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0753105
• Machado, Humberto. 2008. “Two-Dimensional Simulation of Ablation Due to Aerodynamic Heating in a Sounding Rocket.” In 40th Thermophysics Conference. AIAA 2008-4248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4248
• Machado, Humberto. 2018. “Aerodynamic Heating of SARA Sub-Orbital Platform Considering Chemical Equilibrium.” In Anais do X Congresso Nacional de Engenharia Mecânica. ABCM. https://doi.org/10.26678/abcm.conem2018.con18-1561
• MacLaren, M. D., and David W. Walkup. 1964. A Missile Targeting Problem. Defense Technical Information Center. https://doi.org/10.21236/ad0603583
• Maddux, Gary A. 1999. Research and Evaluation of Advanced Missile Component Technologies. Defense Technical Information Center. https://doi.org/10.21236/ada374350
• Maeding, C., D. Wiedmann, K. Quering, and O. Knab. 2011. “Improved Heat Transfer Prediction Engineering Capabilities for Rocket Thrust Chamber Layout.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/201102239
• Magalhães, Giorgio M. 2021. “Radar Aerial Target-Tracking on Lie Groups.” PhD diss.. https://doi.org/10.47749/t/unicamp.2021.1165418
• Magill, J., and S. Wehe. 2002. “Initial Test of a Wire Suspension Mount for Missile Virtual Flight Testing.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-169
• Magis, S. F. 1960. A Review of Metallurgical Factors in Development of the Warhead MK 19 MOD 0 for ASM-N-7A Bullpup Guided Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0321180
• Maheskumar, Pon., R. Girimurugan, G. Sivaraman, S. Purushothaman, and M. Vairavel. 2021. “Thermal Analysis on Regenerative Cooled Liquid Propellant Rocket Thrust Chamber Using ANSYS.” IOP Conference Series: Materials Science and Engineering 1059 (1): 012068. https://doi.org/10.1088/1757-899x/1059/1/012068
• Mahire, Arifin, Sheikh Mohammad Rafi, Shahrear Jahan Santho, and Tariq Mahbub. 2026. “Effect of Relative Orientation of Body Fin and Tail Fin on the Aerodynamic Characteristics of a Missile in Subsonic Flight – an Experimental Study.” Preprint, . https://doi.org/10.2139/ssrn.6203298
• Mahmud, Zakaria, and Rodney Bowersox. 2001. “Experimental Investigation of Low Blow Ratio Blended Missile Body Supersonic Jet Interaction Flowfields.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-886
• Mahmud, Zakaria, and Rodney Bowersox. 2003. “Supersonic Missile Body Jet Interaction Flowfields at Low Momentum-Parameter-Ratio.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-1244. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-1244
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2023a. “Impact Time Constrained Sliding Mode Guidance with Prescribed Performance.” In AIAA SCITECH 2023 Forum. AIAA 2023-2157. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2157
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2023b. “Prescribed Performance Terminal Sliding Mode Based Guidance with Impact Angle Constraints.” In AIAA SCITECH 2023 Forum. AIAA 2023-2158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2158
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2024b. “True-Proportional-Navigation Based Impact Time Guidance with Predefined Convergence Time.” In AIAA SCITECH 2024 Forum. AIAA 2024-1987. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1987
• Majumder, Kakoli, and Shashi Ranjan Kumar. 2025. “Input-to-State Stability Based Impact Time Constrained Nonlinear Guidance.” In AIAA SCITECH 2025 Forum. AIAA 2025-1713. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-1713
• Makena, Jacqueline, and Solomon Omwoma. 2017. “Nonlinear H∞ Guidance Design for Missile against Maneuvering Target.” Advances in Research 9 (4): 1–21. https://doi.org/10.9734/air/2017/33186
• Maklakov, D. V. 2001. “Steady Waves Generated by a Moving Body and Wave Drag.” Doklady Physics 46 (8): 572–75. https://doi.org/10.1134/1.1401226
• Maley, James M. 2015. “Line of Sight Rate Estimation for Guided Projectiles with Strapdown Seekers.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0344. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0344
• 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. 1976a. Storage Reliability of Missile Materiel Program. Igniters and Safe and Arm Device Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada026938
• Malik, Dennis F. 1976b. Storage Reliability of Missile Materiel Program. Storage Reliability Summary Report. Volume IV. Ordnance Devices. Defense Technical Information Center. https://doi.org/10.21236/ada026478
• Malmuth, Norman, and Vladimir Shalaev. 2004. “Theoretical Modeling of Slender Bodies Interaction in Supersonic Flows.” In 42nd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2004-1127. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-1127
• Maloney, Michael S. 2007. Cruise Missile Attack Are We Prepared. Defense Technical Information Center. https://doi.org/10.21236/ada469582
• Manchester, Ian, and Andrey Savkin. 2003. “Circular Navigation Missile Guidance with Incomplete Information and Uncertain Autopilot Model.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5448. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5448
• Mandt, G., and T. Neighbor. 1982. “Air-to-Air Missile Avoidance.” In Guidance and Control Conference. AIAA 1982-1516. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1516
• Mani, M., A. Cary, and W. W. Bower. 2004. “Accurate Flow Prediction for Store Separation from Internal Bay.” In Computational Fluid Dynamics 2004. Springer Berlin Heidelberg. https://doi.org/10.1007/3-540-31801-1_38
• Mani, Mahmood, M. Dadkhah, and A. Gili. 2000. “A Simple Code for Calculation of Mixture Ratio in Liquid Propellant Rocket Engine, and Its Evaluation.” In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3765. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3765
• “Manual Control Devices.” 2006. In International Encyclopedia of Ergonomics and Human Factors - 3 Volume Set. CRC Press. https://doi.org/10.1201/9780849375477-306
• 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
• Marcum, David L. 2001. Computational Simulation of Unsteady, Viscous, Hypersonic Flow about Flight Vehicles with Store Separation. Defense Technical Information Center. https://doi.org/10.21236/ada387492
• 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
• “Marshall Selected to Convert L1011 Tristar to Become Carrier of Air-Launched Space Booster.” 1992. Aircraft Engineering and Aerospace Technology 64 (7): 14–15. https://doi.org/10.1108/eb037260
• Martin, Wayne A. 1962. Development of Deep Drawn: One Piece High Performance Rocket Motorcase. Defense Technical Information Center. https://doi.org/10.21236/ad0273826
• Martin, Edward A., Bryan E. Brett, and David G. Hoagland. 1999. Tools for Including Realistic Representations of Operator Performance in DOD Constructive Simulations. Defense Technical Information Center. https://doi.org/10.21236/ada430277
• Martín Barrio, Andrés. n.d. “Design, Modelling, Control and Teleoperation of Hyper-Redundant Robots.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.65161
• Martineau, P., A. Tomasino, and B. Light. 1990. “Structural Analysis and Testing of the Pegasus Air-Launched Space Booster.” In 26th Joint Propulsion Conference. AIAA 1990-2204. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2204
• Martinovsky, Bilyana, and David Traum. 2006. The Error Is the Clue: Breakdown in Human-Machine Interaction. Defense Technical Information Center. https://doi.org/10.21236/ada459168
• Martz, H. F. Jr., and R. A. Waller. 1976. Bayesian Zero-Failure (BAZE) Reliability Demonstration Testing Procedure and Its Application to a Rankine Dynamic Radioisotope Power Conversion System. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/7140632
• 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
• Marzat, Julien. 2017. “A Missile Guidance Law Tolerant to Unestimated Evasive Maneuvers.” Aircraft Engineering and Aerospace Technology 89 (2): 314–19. https://doi.org/10.1108/aeat-04-2014-0044
• Masek, R., D. Hender, and J. Forney. 1973. “Evaluation of Aerodynamic Heating Uncertainties for Space Shuttle.” In 8th Thermophysics Conference. AIAA 1973-737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-737
• Mashburn, James H. 1969. Turbulent Boundary Layer Separation Ahead of Cylindrical Protuberances in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0690947
• 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, David M. 2009. Directed Energy Weapon System for Ballistic Missile Defense. Defense Technical Information Center. https://doi.org/10.21236/ada540023
• Mason, Keith, Catherine Howard, Jeff Sturm, and Craig Keogh. 2007. “An Assessment of the Impact of ELEXSA Visualizations on Operator Situation Awareness.” In Proceedings of the 19th Australasian conference on Computer-Human Interaction: Entertaining User Interfaces. ACM. https://doi.org/10.1145/1324892.1324916
• 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
• Masters, A. I. 1968. Investigation of Light Hydrocarbon Fuels with Fluorine Oxygen Mixtures as Liquid Rocket Propellants Final Report. NASA-CR-72425. NASA. https://ntrs.nasa.gov/citations/19690001016
• Masyagin, V. S. 2026. “Using a Predictive Model to Control the Thrust Vector of a Multi-Chamber Liquid Rocket Engine with a Central Body.” Journal of Instrument Engineering 69 (3): 211–24. https://doi.org/10.17586/0021-3454-2026-69-3-211-224
• 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
• Matmurodov, Farkhod Matkurbonovich, and Kamol Qaxramonovich Toshtemirov. 2025. “Mathematical Modeling of the Vertical Launch and Operation of an Aircraft Missile Gyroscope.” Innovative International Multidisciplinary Journal of Applied Technology (2995-486X) 3 (12): 91–95. https://doi.org/10.51699/dj7bex24
• Mattei, Giovanni, and Salvatore Monaco. 2012. “Nonlinear Robust Autopilot for Rolling and Lateral Motions of an Aerodynamic Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4467. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4467
• Matthews, George B. 1957. Combustion Instability in Liquid Propellant Rocket Motors: Determination of Combustion Time Lag Parameters in a Liquid Bipropellant Rocket Motor. Defense Technical Information Center. https://doi.org/10.21236/ad0127419
• Matthews, H. F., and S. F. Schmidt. 1955. A Comparison of the Maneuvering Performance of a Monowing versus a Cruciform Missile. NACA-RM-A55D13. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19710064940
• Matthews, Howard F., and Elwood C. Stewart. 1951. A Comparison of the Calculated Maximum-Maneuver Response Characteristics of Three Air-to-Air, Beam-Rider, Guided Missiles Having Different Lift Ratios. NACA-RM-A51F18. NASA. https://ntrs.nasa.gov/citations/19930086711
• Matthews, J., and G. Taylor. 1969. “Development Program for a General Purpose Computer and Strapdown Inertial Measurement Unit.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-850. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-850
• Matting, Fred W., and Dean R. Chapman. 1958. Turbulent Skin Friction at High Mach Numbers and Reynolds Numbers. NACA-RM-A58D28. National Advisory Committee for Aeronautics. Ames Aeronautical Lab. https://ntrs.nasa.gov/citations/20040034083
• “Maximum Likelihood Estimation of Radial Error PDF.” 2009. In Spatial Error Analysis. IEEE. https://doi.org/10.1109/9780470546468.ch6
• Mayer, Wolfgang, and Gerd Kruelle. 1992. “Rocket Engine Coaxial Injector Liquid/gas Interface Flow Phenomena.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3389. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3389
• McAmis, R., D. Lankford, and W. Phares. 1992. “Theoretical Liquid Rocket Engine Nozzle Flow Fields.” In 28th Joint Propulsion Conference and Exhibit. AIAA 1992-3730. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3730
• McAmis, R., D. Lankford, and R. Torick Jr. 1991. “Application of a Chemically Reacting Navier-Stokes Code for Predicting Nozzle Performance of a High Area Ratio Liquid-Propellant Rocket Engine.” In 29th Aerospace Sciences Meeting. AIAA 1991-307. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-307
• McAnally, J., and C. Engel. 1979. “Reentry Aerodynamic Heating Methods for Sounding Rocket Payloads.” In 5th Sounding Rocket Technology Conference. AIAA 1979-508. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-508
• McCabe, Linda. 2011. Operator-in-the-Loop Experimentation: Providing Combat Utility Measures. Defense Technical Information Center. https://doi.org/10.21236/ada573494
• McCandlish, S. G. 1966. “A Computer Simulation Experiment of Supervisory Control of Remote Manipulation.” PhD diss., Massachusetts Inst. of Tech.. https://ntrs.nasa.gov/citations/19720017325
• McCormack, P. D. 1964. “A Driving Mechanism for High Frequency Combustion Instability in Liquid Fuel Rocket Engines.” Journal of the Royal Aeronautical Society 68 (645): 633–37. https://doi.org/10.1017/s0368393100080433
• McCracken, J. H., and T. B. Aldrich. 1984. Analyses of Selected LHX Mission Functions: Implications for Operator Workload and System Automation Goals. Defense Technical Information Center. https://doi.org/10.21236/ada232330
• 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
• McDonald, M. W., L. B. Malone, and E. H. Gleason. 1985. Consideration of Radar Target Glint from ST during OMV Rendezvous. NASA-TM-86533. NASA. https://ntrs.nasa.gov/citations/19860006986
• McDowell, D., G. Irwin, and G. McConnell. 1995. “Online Neural Control Applied to a Bank-to-Turn Missile Autopilot.” In Guidance, Navigation, and Control Conference. AIAA 1995-3316. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3316
• 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
• McFarland, Michael, and Shaheen Hoque. 2000. “Robustness of a Nonlinear Missile Autopilot Designed Using Dynamic Inversion.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-3970. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3970
• McGehee, R. 1979. “Bank-to-Turn /BTT/ Technologyfor Enhancement of Short Range Air-to-Air Missile Maneuverability.” In Guidance and Control Conference. AIAA 1979-1752. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1752
• McGowan, Gregory, Matthew Kurzen, Robert Nance, James Carpenter, and Frankie Moore. 2012. “Computational Investigation of Pitch Damping on Missile Geometries at High Angles of Attack.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-2903. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2903
• 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
• McKee, Larry. 1998. Air-to-Air Missile T&E Using Live Aircraft Linked to a Missile HWIL Simulation. Defense Technical Information Center. https://doi.org/10.21236/ada359504
• McKillip, Robert, and Todd R. Quackenbush. 2015. “Store Separation Modeling for Rotorcraft Applications.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0071-2015-10207
• McKinney, L. W., and E. C. Polhamus. 1966. A Summary of NASA Data Relative to External-Store Separation Characteristics. NASA-TN-D-3582. NASA. https://ntrs.nasa.gov/citations/19670002016
• 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
• McLaughlin, J. S., and B. D. Staunton. 1989. “Performance Constraints and Compensation for Teleoperation with Delay.” In JPL, California Inst. of Tech., Proceedings of the NASA Conference on Space Telerobotics, Volume 5. https://ntrs.nasa.gov/citations/19900020565
• McLaughlin, Ryan, Jacob L. Yancosek, and Mario G. Perhinschi. 2026. “Effects of Actuator and Sensor Abnormal Conditions on Missile Performance.” In AIAA SCITECH 2026 Forum. AIAA 2026-2402. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2402
• McLendon, J., and F. Baumann III. 1983. “High Speed Anti-Radiation Missile (HARM) Test and Evaluation Program.” In 2nd Flight Testing Conference. AIAA 1983-2728. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2728
• McLeod, Ronald W. 2025. “The Proactive Operator Monitoring Assessment Tool for Supervisory Control (POMATsc).” In Transitioning to Autonomy. CRC Press. https://doi.org/10.1201/9781003679479-15
• McNeill, W. E., G. A. Smith Jr., and R. M. Gerdes. 1982. “Evaluation of a Trajectory Command Concept for Manual Control of Carrier Approaches and Landings.” In 16th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19820026184
• McNellis, J., W. Ruland, and D. Woods. 1971. “A Computerized Test System for Strapdown Guidance Systems.” In Guidance, Control and Flight Mechanics Conference. AIAA 1971-967. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1971-967
• McNicholl, D., S. Cohen, and C. Palmer. 1988a. Common Ada (Tradename) Missile Package (CAMP) Project. Missile Software Parts. Volume 2. Version Description Document. Defense Technical Information Center. https://doi.org/10.21236/adb120249
• McNicholl, D., S. Cohen, and C. Palmer. 1988b. Common Ada (Tradename) Missile Package (CAMP) Project. Missile Software Parts. Volume 5. Top-Level Design Document. Defense Technical Information Center. https://doi.org/10.21236/adb120252
• McNolty, Frank. 1962. “Kill Probability When the Weapon Bias Is Randomly Distributed.” Operations Research 10 (5): 693–701. https://doi.org/10.1287/opre.10.5.693
• McNolty, Frank. 1965. “Letter to the Editor—Kill Probability When the Lethal Effect Is Variable.” Operations Research 13 (3): 478–82. https://doi.org/10.1287/opre.13.3.478
• McNolty, Frank. 1967. “Letter to the Editor—Kill Probability for Multiple Shots.” Operations Research 15 (1): 165–69. https://doi.org/10.1287/opre.15.1.165
• Mead, Merrill H. 1953. Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9. NACA-RM-A52K14. NASA. https://ntrs.nasa.gov/citations/19930087422
• Meakin, Robert L., and Tor A. Nygaard. 2003. An Aerodynamic Analysis of a Spinning Missile with Dithering Canards. Army Aviation and Missile Command. https://ntrs.nasa.gov/citations/20030071145
• Mebarki, Youssef, Sador Brhane, and Suart Rutherford. 2020. “Real-Time Optical Tracking for Store Separation Testing in Wind Tunnel.” In AIAA Scitech 2020 Forum. AIAA 2020-1397. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1397
• 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
• Meiry, J. L., and L. R. Young. 1965. Bang-Bang Aspects of Manual Control in High Order Systems. NASA. https://ntrs.nasa.gov/citations/19650046064
• 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
• Melchiorri, Claudio. 2015. “Robot Teleoperation.” In Encyclopedia of Systems and Control. Springer London. https://doi.org/10.1007/978-1-4471-5058-9_172
• Melville, Maelyn, and Dennis Helmich. 2021. “Common Hypersonic Boost Glide R&D.” In Proposed for presentation at the Military Hypersonic Weapons System Conference held October 18-19, 2021 in Virtual, Virtual United States. US DOE. https://doi.org/10.2172/1892153
• Menees, Gene P., and John W. Boyd. 1959. An Experimental Investigation of the Effect of a Canard Control on the Lift, Drag, and Pitching Moment of an Aspect-Ratio 2.0 Triangular Wing Incorporating a Form of Conical Camber. NASA-MEMO-5-20-59A. NASA. https://ntrs.nasa.gov/citations/19980228046
• Meng, Xiangrui, chong Li, and Xiaomin Li. 2026. “Novel Bias Drift Mechanism of Whole-Angle Mode Gyroscopes: Oscillatory Rectification Errors.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-8837107/v1
• Menon, P., and V. Iragavarapu. 1998. “Blended Homing Guidance Law Using Fuzzy Logic.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4304. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4304
• 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
• Menon, P. K., G. D. Sweriduk, and E. J. Ohlmeyer. 2003. Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-to-Kill Missiles. Defense Technical Information Center. https://doi.org/10.21236/ada436322
• Menssen, Jacob. 2026. “Trajectory Analysis for Manned Spaceflight: Aerodynamic Heating of a Two-Person Lunar-Return Vehicle.” In 2026 Regional Student Conferences. AIAA 2026-111626. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-111626
• Merchant, Clifton. 1961. Electromagnetic Coupling Due to Apertures in Missile Bodies. Defense Technical Information Center. https://doi.org/10.21236/ad0257304
• Merhav, S. 1979. Low-Cost Inertial Navigation for Moderate-g Missions. NASA-TM-78611. NASA. https://ntrs.nasa.gov/citations/19790024034
• Merhav, S. 1989. “Effects of Biodynamic Coupling on the Human Operator Model.” In Guidance, Navigation and Control Conference. AIAA 1989-3518. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3518
• “Merits of Liquid Propellant Rocket Engines and Their Applications.” 2006. In History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600868870.0005.0022
• Mermagen, W. H. 1964. High ‘g’ Telemetry for Ballistic Range Instrumentation. Defense Technical Information Center. https://doi.org/10.21236/ad0444246
• Mermagen, William, Sr., and Charles Murphy. 2001. “Flight Motion of a Continuously Elastic Finned Missile.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2001-4327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4327
• Merrick, Justin, and Mark F. Reeder. 2015. “Cavity-Store Interaction under Supersonic Freestream Conditions.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-3017. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3017
• Merritt, J., and G. Gocal. 1979. “Radar Signal Processor for Tactical Missile.” In 2nd Computers in Aerospace Conference. AIAA 1979-1938. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1938
• Mesalles Ripoll, Pol, Nicholas S. Campbell, and Brian Argrow. 2021. “Aerothermodynamic Uncertainty in Lifting and Boost-Glide Entry Trajectories.” In AIAA Scitech 2021 Forum. AIAA 2021-0934. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0934
• Meyer, Rudolf X. 1938. Magnetohydrodynamics and Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ad0608024
• Meyer, R. A. 1958. Wind Tunnel Investigation of Conventional Types of Parachute Canopies in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0208856
• Meyer, J. 1992. “Effects of the Roll Angle on Cruciform Wing-Body Configurations at High Incidences.” In Guidance, Navigation and Control Conference. AIAA 1992-4356. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4356
• Meyer, Michael L., and James E. Giuliani. 1993. Flow Visualization Study in High Aspect Ratio Cooling Channels for Rocket Engines. NASA Lewis Research Center. https://ntrs.nasa.gov/citations/19940018576
• Meyer, Robert, Jr., Robert Curry, and Gerald Budd. 1992. “Aerodynamic Flight Research Using the Pegasus Air-Launched Space Booster.” In 17th Aerospace Ground Testing Conference. AIAA 1992-3990. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-3990
• 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
• Micci, Michael M. 1997. Contributions of Atomization, Vaporization and Combustion to Liquid Rocket Acoustic Energy. Defense Technical Information Center. https://doi.org/10.21236/ada329776
• Michigan Univ Ann Arbor. 1963. The Feasibility of a Rotating Detonation Wave Rocket Motor. Defense Technical Information Center. https://doi.org/10.21236/ad0410035
• Mickle, M. C., and J. J. Zhu. n.d.-c. “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
• Middlebrooks, Sam E., Beverly G. Knapp, B. Diane Barnette, Cheryl A. Bird, and Joyce M. Johnson. 1999. CoHOST (Computer Modeling of Human Operator System Tasks) Computer Simulation Models to Investigate Human Performance Task and Workload Conditions in a U.S. Army Heavy Maneuver Battalion Tactical Operations Center. Defense Technical Information Center. https://doi.org/10.21236/ada368587
• Miele, Angelo. 1958. “Optimum Burning Program as Related to Aerodynamic Heating for a Missile Traversing the Earth’s Atmosphere.” In VIIIth International Astronautical Congress Barcelona 1957 / VIII. Internationaler Astronautischer Kongress / VIIIe Congrès International D’Astronautique. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-39990-3_21
• Miele, Angelo, and David G. Hull. 1963. Slender Bodies of Revolution Having Minimum Total Drag at Hypersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ad0404858
• Mihelj, Matjaž, and Janez Podobnik. 2012. “Teleoperation.” In Intelligent Systems, Control and Automation: Science and Engineering. Springer Netherlands. https://doi.org/10.1007/978-94-007-5718-9_9
• Milanovic, Bojan. 2008. “Monopulse Homing Missile Jamming with the Amplitude Modulated Cross Eye Method.” Vojnotehnicki glasnik 56 (3): 44–60. https://doi.org/10.5937/vojtehg0803044m
• 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
• Miles, Richard B., and Sergey Macheret. 2004. Microwave-Driven Air Plasma Studies for Drag Reduction and Power Extraction in Supersonic Air. Defense Technical Information Center. https://doi.org/10.21236/ada427662
• 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
• Miller, George S. 1952. Antijamming Performance of Radar Set AN/APS-23(XA-2) (Tunable Radar System). Defense Technical Information Center. https://doi.org/10.21236/ad0004521
• Miller, M. 1987. “An Investigation of the Aerodynamic Characteristics of a Cruciform Missile in Subsonic Flow.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-143. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-143
• Miller, Eric J., Josue Cruz, Shun-fat Lung, et al. 2016. “Evaluation of the Hinge Moment and Normal Force Aerodynamic Loads from a Seamless Adaptive Compliant Trailing Edge Flap in Flight.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0038. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0038
• Miller, Richard A., Ingjaldur Hannibalsson, and Samuel C. McNamee. 1977. Identification of Finite State Models of a Human Operator. Defense Technical Information Center. https://doi.org/10.21236/ada053017
• Miller, R. A., and R. J. Jagacinski. 1986. Twenty-First Annual Conference on Manual Control. NASA-CP-2428. NASA. https://ntrs.nasa.gov/citations/19860023504
• Miller, Eric J., Chris R. Miller, David Moseley, et al. 2018. “Captive-Carry Flight Demonstration of an Inert Test Rocket Using a Business Jet as an Air Launch Platform.” In Annual National Space and Missile Materials Symposium (NSMMS) and Commercial and Government Responsive Access to Space Technology Exchange (CRASTE) Joint Symposium. https://ntrs.nasa.gov/citations/20180004443
• Miller, Matthew J., Bradley A. Steinfeldt, and Robert D. Braun. 2014. “Supersonic Inflatable Aerodynamic Decelerators for Use on Sounding Rocket Payloads.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2014-1092. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1092
• Mills, A., G. Raman, and V. Kibens. 2002. “Optimization of High Frequency Actuators for Weapons Bay Noise Suppression.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-660. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-660
• Milstein, Laurence B. 1991. “An Introduction to Anti-Jam Performance of Spread Spectrum Communications.” In Space Communication and Nuclear Scintillation. Springer Netherlands. https://doi.org/10.1007/978-94-017-5418-7_5
• Min, Byung-Young, Jae-Woo Lee, and Yung-Hwan Byun. 2003. “Investigation of the Shock Interaction Effect on the Lateral Jet Controlled Missile.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3932
• Minato, Ryojiro, Kazuyuki Higashino, Masatoshi Sugioka, and Y. Sasayam. 2012. “Control of LNG Pyrolysis and Application to Regenerative Cooling Rocket Engine.” In InTech eBooks. https://doi.org/10.5772/34146
• Miner, E. W., and C. H. Lewis. 1972. A Finite Difference Method for Predicting Supersonic Turbulent Boundary Layer Flows with Tangential Slot Injection. NASA-CR-2124. NASA. https://ntrs.nasa.gov/citations/19720025621
• Miner, E. W., and C. H. Lewis. 1973. “Supersonic Turbulent Boundary-Layer Flows with Tangential Slot Injection.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19730051443
• Mironov, S. G., and K. M. Serdyuk. 2012. “Effect of Mesh Screens on the Wave Drag of a Blunt Body in Supersonic Flow.” Thermophysics and Aeromechanics 19 (2): 201–8. https://doi.org/10.1134/s0869864312020047
• Mirzaei, Amirhossein, S. Hamid Jalali-Naini, and Ali Arabian Arani. 2022. “Miss Distance Analysis of First-Order Explicit Guidance Law With/without Radome Effect.” Journal of Space Science and Technology 15 (4): 1–18. https://doi.org/10.30699/jsst.2022.1385
• Mirzamoghadam, A. 1991. “Advanced Liquid Rocket Chamber Wall Cooling Design Criteria.” In 27th Joint Propulsion Conference. AIAA 1991-1982. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1982
• Mishina, Yuki, Ryoya Umeoka, and Takeshi Kanda. 2020. “Study of Liquid-Propellant Rocket Engine High-Frequency Combustion Instability.” Proceedings of Mechanical Engineering Congress, Japan 2020 (0): J19104. https://doi.org/10.1299/jsmemecj.2020.j19104
• Mishley, Adi, and Vitaly Shaferman. 2022. “Optimal Guidance with an Intercept Angle Constraint for Varying Speed Adversaries.” In AIAA SCITECH 2022 Forum. AIAA 2022-1598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1598
• Mishley, Adi, and Vitaly Shaferman. 2023. “Linear Quadratic Differential Games Guidance Law with an Intercept Angle Constraint and Varying Speed Adversaries.” In AIAA SCITECH 2023 Forum. AIAA 2023-2495. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2495
• Mishra, D. P. 2017a. “Hybrid Propellant Rocket Engine.” In Fundamentals of Rocket Propulsion. CRC Press. https://doi.org/10.1201/9781315175997-9
• Mishra, D. P. 2017b. “Liquid-Propellant Rocket Engines.” In Fundamentals of Rocket Propulsion. CRC Press. https://doi.org/10.1201/9781315175997-8
• “Missile Attack Warning.” 2007. In Advances in Bistatic Radar. Institution of Engineering and Technology. https://doi.org/10.1049/sbra001e_ch4
• “Missile Attitude Control.” 2013. In LMIs in Control Systems. CRC Press. https://doi.org/10.1201/b15060-23
• “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 Defense Problem.” 2016. In Air and Missile Defense Systems Engineering. CRC Press. https://doi.org/10.1201/b19671-8
• “Missile Defense Radar Design Considerations.” 2009. In Phased-Array Radar Design: Application of radar fundamentals. Institution of Engineering and Technology. https://doi.org/10.1049/sbra018e_ch12
• “Missile Guidance Software.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-13
• Mitchell, Meredith B. 1964. A SURVEY OF HUMAN OPERATOR MODELS FOR MANUAL CONTROL. Appendix. Defense Technical Information Center. https://doi.org/10.21236/ad0449587
• Mitchell, C. E. 1967. Axial Mode Shock Wave Combustion Instability in Liquid Propellant Rocket Engines. NASA-CR-72259. NASA. https://ntrs.nasa.gov/citations/19670025271
• Mitchell, J. P. 1968. Space Storable Regenerative Cooling Investigation Interim Report, 1 Jul.: 30 Sep. 1967. NASA-CR-72341. NASA. https://ntrs.nasa.gov/citations/19680019986
• Mitchell, C. 1969. “Stability Limits for a Liquid Rocket Engine Using a Droplet Vaporization Model.” In 5th Propulsion Joint Specialist. AIAA 1969-483. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-483
• Mitchell, Joe C. 1976. Storage Reliability of Missile Materiel Program. Missile Hydraulic and Pneumatic Systems Actuator Analysis. Defense Technical Information Center. https://doi.org/10.21236/ada026353
• Mitchell, Royce E. 1993. NASA’s Advanced Solid Rocket Motor. NASA-CR-191950. NASA. https://ntrs.nasa.gov/citations/19930010636
• Mitchell, J., and G. C. Kinney. 1966. Specification for a Display Console with Electronic and Projected Displays. Defense Technical Information Center. https://doi.org/10.21236/ad0649756
• Mitchell, J. P., and J. W. Neal. 1969. “Space Storable Regenerative Cooling Investigation.” In AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS. https://ntrs.nasa.gov/citations/19690054729
• 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
• Miwa, Susumu, Fumiaki Imado, and Takeshi Kuroda. 1987. “Clutter Effect on the Miss Distance of a Radar Homing Missile.” In Guidance, Navigation and Control Conference. AIAA 1987-2449. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2449
• Miwa, Susumu, and Satoshi Kouya. 1995. “Radome Effect on the Miss Distance of a Radar Homing Missile.” In Guidance, Navigation, and Control Conference. AIAA 1995-3285. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3285
• Mizrahi, Izhak, and Daniella E. Raveh. 2018. “An Investigation of Wing Elasticity Effects on Store Separation Based on Computational Fluid Dynamics.” In 2018 Atmospheric Flight Mechanics Conference. AIAA 2018-2831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-2831
• Mizukaki, Toshiharu, Anna Kono, and Kazuhiko Yamada. 2019. “Quantification and Visualization of Acoustic Disturbance inside a Supersonic Forward-Facing Cavity: A Simplified Supersonic-Parachute Model.” In AIAA Scitech 2019 Forum. AIAA 2019-2110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2110
• Mkrtchyan, Mger, and Yury Kochetkov. 2021. “Gas Dynamic Characteristics Computing of a Liquid Propellant Rocket Engine for Laminar Flows.” Vestnik Moskovskogo aviatsionnogo instituta 28 (2): 166–76. https://doi.org/10.34759/vst-2021-2-166-176
• Mobley, Scott B. 1994. “U.S. Army Missile Command Dual-Mode Millimeter Wave/infrared Simulator Development.” In SPIE Proceedings, vol. 2223, edited by Wendell R. Watkins, Dieter Clement. SPIE. https://doi.org/10.1117/12.177947
• Mobley, Scott B., Vicki Vanderford, and John B. Cooper. 1995. “U.S. Army Missile Command Dual-Mode Millimeter Wave/infrared Simulator Development.” In SPIE Proceedings, vol. 2469, edited by Wendell R. Watkins, Dieter Clement. SPIE. https://doi.org/10.1117/12.210587
• “Model Assignments and the Function Allocation Diagram.” n.d. In ARIS Design Platform. Springer London. https://doi.org/10.1007/978-1-84628-613-1_12
• “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
• “Modified Guidance Law Based on a Sliding Mode Controller for a Missile Guidance System.” 2016. Tehnicki vjesnik - Technical Gazette 23 (3). https://doi.org/10.17559/tv-20130625173047
• 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
• Mohenski, D. D. 1998. “Guided Anti-Tank Missile Control Training Simulator Design via Object-Oriented Modelling.” In UKACC International Conference on Control (CONTROL ‘98), vol. 1998. IEE. https://doi.org/10.1049/cp:19980246
• Moiseev, Sergey N. 2022. “Simulation of the Difference Error in Target Tracking by Airborne Radar and Optoelectronic Stations.” Trudy MAI, no. 124. https://doi.org/10.34759/trd-2022-124-16
• 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
• “Monopulse Direction Estimation.” 2001. In Radar Techniques Using Array Antennas. Institution of Engineering and Technology. https://doi.org/10.1049/pbra010e_ch11
• “Monopulse Direction Estimation.” 2013. In Radar Techniques Using Array Antennas. Institution of Engineering and Technology. https://doi.org/10.1049/pbra026e_ch11
• Monta, W. J., and J. B. Peterson Jr. 1966. Considerations Regarding the Evaluation and Reduction of Supersonic Skin Friction. NASA-TN-D-3588. NASA. https://ntrs.nasa.gov/citations/19660027862
• Montanez, Roberto, and Carlos Pantano. 2026. “Fluid-Structure Interaction Simulation of the Effect of Speed in the Deployment of a Parachute with High-Speed Dynamic Reefing.” In 28th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2026-3823. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-3823
• Montgomery, Douglas C., and Robert G. Conard. 1980. “Comparison of Simulation and Flight-Test Data for Missile Systems.” SIMULATION 34 (2): 63–72. https://doi.org/10.1177/003754978003400206
• Monty, Richard A., and William J. Ruby. 1965. “Effects of Added Work Load on Compensatory Tracking for Maximum Terrain Following.” Human Factors: The Journal of the Human Factors and Ergonomics Society 7 (3): 207–14. https://doi.org/10.1177/001872086500700302
• Moog, R. 1975. “Aerodynamic Line Bowing during Parachute Deployment.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1381
• Moon, J. R. 2002a. “Effects of Birds on Radar Tracking Systems.” In RADAR 2002. IEE. https://doi.org/10.1109/radar.2002.1174701
• Moon, J. R. 2002b. “Effects of Birds on Radar Tracking Systems.” In 2002 International Radar Conference (Radar 2002), vol. 2002. IEE. https://doi.org/10.1049/cp:20020296
• 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
• Moon, Jongki, and Youdan Kim. 2000. “Design of Missile Guidance Law via Variable Structure Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4068. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4068
• Moon, Gwanyoung, and Youdan Kim. 2011. “Non-Affine Waypoint Guidance Law Using Distance Information.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6595. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6595
• Mooney, F. J. 1962. Application of Encoders in Missile Azimuth Alignment Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0295597
• 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, 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, 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, Thomas, and Thomas Moore. 2011. “Solid Propulsion Enabling Technologies and Milestones for Navy Air-Launched Tactical Missiles.” In AIAA Centennial of Naval Aviation Forum “100 Years of Achievement and Progress”. AIAA 2011-6941. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6941
• Moran, Inanc, and Turgay Altilar. 2005. “Three Plane Approach for 3D True Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6457. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6457
• 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
• Moray, Neville, Toshiuki Inagaki, and Makoto Itoh. 1998. “Allocation of Function, Adaptive Automation, and Fault Management.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 42 (3): 277–79. https://doi.org/10.1177/154193129804200320
• Morgan, C. J. 2015. The Effect of Resistance on Rocket Injector Acoustics. M15-4797. Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA). https://ntrs.nasa.gov/citations/20150021411
• Mori, Takashige, Takeshi Tsuchiya, and Ko Ogasawara. 2002. “Glide-Back Flying Test Bed Concept for Hypersonic Flight Test.” In AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2002-5221. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5221
• Morita, Takakazu, Koki Kitagawa, Saburo Yuasa, Shigeru Yamaguchi, and Toru Shimada. 2012. “Low-Frequency Combustion Instability Induced by the Combustion Time Lag of Liquid Oxidizer in Hybrid Rocket Motors.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 10 (ists28): Pa_37-Pa_41. https://doi.org/10.2322/tastj.10.pa_37
• Morote, Jesus. 2009. “Control of Roll Lock-In and Catastrophic Yaw for Cruciform Finned Missiles.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5717. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5717
• Morton, Harold S. 1966. Scaling the Effects of Air Blast on Typical Targets. Defense Technical Information Center. https://doi.org/10.21236/ad0481144
• Moruzzi, Michael J., Jan Fessl, Paul Prochnicki, and John A. Targonski. 2018. “Liquid Rocket Engine Component Water-Flow Test Stand.” In 2018 Joint Propulsion Conference. AIAA 2018-4599. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4599
• Mosier, Daniel, and Malur K. Sundareshan. 2001. “Multiple-Model Algorithm for Passive Ranging and Air-to-Air Missile Guidance Systems.” In SPIE Proceedings, vol. 4473, edited by Oliver E. Drummond. SPIE. https://doi.org/10.1117/12.492790
• Moskowitz, H. 1965. “Blast Effects Resulting from Fragmentation of an Atlas Missile.” In Flight Testing Conference. AIAA 1965-195. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1965-195
• 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
• Mouloua, Mustapha, Raja Parasuraman, and Robert Molloy. 1993. “Monitoring Automation Failures: Effects of Single and Multi-Adaptive Function Allocation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 37 (1): 1–5. https://doi.org/10.1177/154193129303700102
• 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
• Moustfa, K., Y. Elhalwagy, and H. Salem. 2008. “CW Radio Seeker Performance Analysis in Presence of Uncertainties for Semi-Active Homing Guidance System.” International Conference on Electrical Engineering 6 (6): 1–17. https://doi.org/10.21608/iceeng.2008.34631
• Moyer, R. 1963. Scientific Passenger Pod, Addendum to Annex Flight Test Directive Missile N-24. Defense Technical Information Center. https://doi.org/10.21236/ad0408760
• Moyer, Seth, and Alex Cenko. 1994. “Navy Applications of Integrated Store Separation Analysis and Flight Testing.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-32. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-32
• Moyer, Seth, Phil Richardson, Alex Cenko, and Margus Susi. 1995. “Flight Test Incident Investigation via Computational Aerodynamics and Store Separation Analysis.” In 33rd Aerospace Sciences Meeting and Exhibit. AIAA 1995-67. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-67
• Mracek, Curtis. 2006. “A Miss Distance Study for Homing Missiles: Tail vs Canard Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6082. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6082
• Mracek, Curtis P. 2014. “Tactical Missile Autopilots.” In Encyclopedia of Systems and Control. Springer London. https://doi.org/10.1007/978-1-4471-5102-9_19-1
• Mracek, Curtis P. 2024. “Optimal Guidance for an Ideal Missile.” In AIAA SCITECH 2024 Forum. AIAA 2024-1989. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1989
• 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
• Mracek, Curtis, and D. Ridgely. 2005. “Missile Longitudinal Autopilots: Connections between Optimal Control and Classical Topologies.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6381
• Mracek, Curtis, and D. Ridgely. 2006. “Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6569
• Muckler, Frederick A. 1961. The Design of Operator Controls: A Selected Bibliography. Defense Technical Information Center. https://doi.org/10.21236/ad0267055
• Muehlner, Joachim W. 1962. Trends in Missile and Space Radio Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ad0407379
• Mueller, D. C., T. E. Bratkovich, K. Lupkes, S. Henderson, and J. T. Williams. 1999. Recent ASI Progress in Pulse Detonation Rocket Engine (PDRE) Hardware Development. Defense Technical Information Center. https://doi.org/10.21236/ada405512
• Muhury, Ankita, Smita Sadhu, and Tapan Kumar Ghoshal. 2023. “Alternative Scheme for Guidance Signal Filtering in a Strapdown Seeker.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 238 (2): 169–81. https://doi.org/10.1177/09544100231219951
• Mukambetov, R. Ya., and I. N. Borovik. 2022. “Ensuring Reliable Cooling of the Combustion Chamber of an Oxygen-Hydrogen Liquid Rocket Engine of the First Stage Launcher with Deep Thrust Throttling.” Engineering Journal: Science and Innovation, no. 1 (121). https://doi.org/10.18698/2308-6033-2022-1-2146
• Mukherjee, Dwaipayan, and Debasish Ghose. 2012. “Zero Miss Distance Guidance Using Feedforward and Periodic Control.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4710. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4710
• Mulanax, Virgil E. 1967. ‘Hornet’ Anti-Tank Missile Warhead Study.. Defense Technical Information Center. https://doi.org/10.21236/ad0387102
• Mulder, Max, Barend Lubbers, Peter Zaal, Marinus van Paassen, and Jan Mulder. 2009. “Aerodynamic Hinge Moment Coefficient Estimation Using Automatic Fly-by-Wire Control Inputs.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2009-5692. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5692
• 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, Ilja, Markus Kuhn, and Ivaylo Petkov. 2017. “Liquid Rocket Engine Concept for SMILE Launcher.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2349. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2349
• Multifractal Detrended Fluctuation Analysis for Onset of Combustion Instability in Liquid Rocket Engines. 2023. https://doi.org/10.37285/bsp.sasat2023.19
• Mungall, Robert C. 1948. Flight Investigation of a Combined Geared Unbalancing-Tab and Servotab Control System as Used with an All-Movable Horizontal Tail. NACA-TN-1763. NASA. https://ntrs.nasa.gov/citations/19930082436
• Mungas, Greg, David J. Fisher, Adam Pollok London, and Jack Merrill Fryer. 2013. Regeneratively Cooled Porous Media Jacket. Patent Number: US-Patent-8,413,419. NASA. https://ntrs.nasa.gov/citations/20140001874
• Munusamy, Raja, and Sai Avikshith Kadam Sai Avikshith Kadam. 2026. “Robust UAV Interception Using Hybrid Guidance Laws: A Comparative Study with Pure Pursuit and Proportional Navigation.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-9755937/v1
• 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
• Muralidharan, Ramal, Sheldon Baron, and Carl Feehrer. 1979. A Decision, Monitoring and Control Model of the Human Operator Applied to an RPV Control Problem. Defense Technical Information Center. https://doi.org/10.21236/ada069880
• 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
• Murphy, B. F. 1952. Operation Buster Some Measurements of Overpressure Time versus Distance for Airburst Bombs,. Defense Technical Information Center. https://doi.org/10.21236/ada296534
• Murphy, J. D. 1967. Flight Test Aerodynamic Heating Data for the Afterbody of the Project Mercury Spacecraft with Comparisons to Available Prediction Methods. NASA-CR-649. NASA. https://ntrs.nasa.gov/citations/19670020040
• Murphy, C. 1970. “Gravity-Induced Angular Motion of a Spinning Missile.” In Guidance, Control and Flight Mechanics Conference. AIAA 1970-968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-968
• Murphy, Charles H. 1971. Gravity-Induced Angular Motion of a Spinning Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0730641
• Murphy, C. 1972. “Generalized Subharmonic Response of a Missile with Slight Configurational Asymmetries.” In 2nd Atmospheric Flight Mechanics Conference. AIAA 1972-972. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-972
• Murphy, Charles, and William Mermagen Sr. 2000. “Flight Mechanics of an Elastic Symmetric Missile.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4202. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4202
• Murphy, Terry, and Norbert Voss. 1996. “Liquid Rocket Engine Acceptance Testing: Improved System Reliability without Hotfire.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3277. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3277
• Murray, A. L., and C. H. Lewis. 1975. Supersonic Turbulent Boundary-Layer Flows with Mass Injection through Slots And/or Porous Walls. NASA-CR-2587. NASA. https://ntrs.nasa.gov/citations/19750022408
• Mushtaq, Muhammad, Wenbin Yu, and Wanchun Chen. 2026. “Field-of-View Constrained Optimal Guidance Law for Impact-Time and Angle Control.” International Journal of Aeronautical and Space Sciences 27 (4): 3333–49. https://doi.org/10.1007/s42405-026-01148-0
• Muthaiah, M., Suraj Saini, and S. Varunkumar. 2023. “Whistling Potential of Throttling Orifices and Its Connection to Liquid Rocket Combustion Instability.” Preprint, . https://doi.org/10.2139/ssrn.4559948
• 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, K. A. 1963. Lethal Area Description. Defense Technical Information Center. https://doi.org/10.21236/ad0612041
• 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
• Nabaa, Nassib, Roland Longchamp, and Marc-Andre Eggimann. 1993. “Linear Programming Control of an Air to Air Missile Using a Model Obtained by Non-Linear Identification.” In Guidance, Navigation and Control Conference. AIAA 1993-3706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3706
• Nagler, Jacob. 2025. “Development of a Stealth-Enabled Supersonic Interceptor Missile: Design, Propulsion, and Guidance.” Mechanical Engineering Advances 3 (3): 3077. https://doi.org/10.59400/mea3077
• 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
• Nam, Vu Hoai. 2025. “Synthesis of Adaptive Proportional Navigation Guidance Laws for Air-to-Air Missiles Intercepting Maneuvering Targets in Modern Aerial Combat.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate1125033.024
• 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
• Naraghi, Mohammad, Stu Dunn, and Doug Coats. 2006a. “Dual Regenerative Cooling Circuits for Liquid Rocket Engines.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4367
• Naraghi, M. H., S. Dunn, and D. Coats. 2006b. Dual Regenerative Cooling Circuits for Liquid Rocket Engines (Preprint). Defense Technical Information Center. https://doi.org/10.21236/ada454591
• Naraghi, Mohammad, David Mohr, and Richard Quentmeyer. 2001. “Effect of a Blocked Channel on the Wall Temperature of a Regeneratively Cooled Rocket Thrust Chamber.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3406. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3406
• Narain, J. 1991. “High Angle of Attack Aerodynamics of a Glide Vehicle.” In 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. AIAA 1991-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1813
• Narayanan, A. 2014. “Cryogenic Rocket Engine Thrust Chamber Test Facility.” Indian Journal of Cryogenics 39 (1): 86–91. https://doi.org/10.5958/2349-2120.2014.00806.1
• NASA Orbit Transfer Rocket Engine Technology Program. 1984. NASA-CR-168156. NASA. https://ntrs.nasa.gov/citations/19840020832
• Nash, J. 1981. “The Advanced Range Instrumentation Aircraft Improvement and Modernization Program.” In 1st Flight Test Conference. AIAA 1981-2368. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2368
• Nason, Martin L., Clarence A. Brown Jr., and Rupert S. Rock. 1955. An Evaluation of the Roll-Rate Stabilization System of the Sidewinder Missile at Mach Numbers from 0.9 to 2.3. NACA-RM-SL55C22. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090023599
• Nath, Suryadeep, and Debasish Ghose. 2020. “Path Length Constrained Interception of Higher Speed Targets Using Retro-Proportional Navigation Guidance Law.” In AIAA Scitech 2020 Forum. AIAA 2020-0611. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0611
• National Renewable Energy Laboratory (NREL), Golden, CO. 2000. Total Solutions Approach at White Sands Missile Range. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/897720
• Naval Ordnance Lab White Oak MD. 1963. Guided Missile Propulsion System, Hazards of Electromagnetic Radiation to Ordnance (Hero);aracteristics of Electro-Explosive Devices.. Defense Technical Information Center. https://doi.org/10.21236/ad0409952
• Naval Weapons Center China Lake CA. 1963. Purchase Description: Igniter, Rocket Motor, Mark 264 Mod O. Defense Technical Information Center. https://doi.org/10.21236/ad0846594
• Naval Weapons Center China Lake CA. 1964. Purchase Description: Igniter, Rocket Motor, Mark 264. Defense Technical Information Center. https://doi.org/10.21236/ad0848200
• Navaneethan, Mansu, T. Sundararajan, K. Srinivasan, and T. Jayachandran. 2024. “Simulations with Compressible Multiphase Formulation on Heat Transfer Studies in a Rocket Thrust Chamber with Experimental Validation.” Journal of Thermal Science and Engineering Applications 16 (9): 091011. https://doi.org/10.1115/1.4065855
• Naylor, P. W. 1961. Development of the EX 25 Mod 0 Continuous Rod Warhead for the Sparrow 1 Air-to-Air Missile. Defense Technical Information Center. https://doi.org/10.21236/ad0323370
• Neelans, W. 1986. “Calculating the Top Ten Risks Prior to the Next Missile Flight Test.” In 3rd Flight Testing Conference and Technical Display. AIAA 1986-9750. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-9750
• 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
• Negaard, Gordon R. 1979. Analysis of a Pyroceram Radome Subjected to Aerodynamic Heating. Defense Technical Information Center. https://doi.org/10.21236/ada363019
• Negishi, Hideyo, Yu Daimon, Nobuki Negoro, and Akihide Kurosu. 2015. “Regenerative Cooling Performance Analysis of the LE-X Engine Combustion Chamber.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3760. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3760
• Nelsen, James. 1995. “Computational Fluid Dynamic Studies of a Solid and Ribbon 12-Gore Parachute Canopy in Subsonic and Supersonic Flow.” In 13th Aerodynamic Decelerator Systems Technology Conference. AIAA 1995-1558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1558
• 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, 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
• “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
• Nesline, F., and P. Zarchan. 1983b. “Line of Sight Reconstruction for Faster Homing Guidance.” In Guidance and Control Conference. AIAA 1983-2170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2170
• Nesline, F., and P. Zarchan. 1984a. “Miss Distance Dynamics in Homing Missiles.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1844. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1844
• Nesline, F., and P. Zarchan. 1984b. “Radome Induced Miss Distance in Aerodynamically Controlled Homing Missiles.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1845. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1845
• Nesline, F., Jr., and M. Nesline. 1985. “Wing Size versus Radome Compensation in Aerodynamically Controlled Radar Homing Missiles.” In Guidance, Navigation and Control Conference. AIAA 1985-1869. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1869
• Nesline, F., Jr., and P. Zarchan. 1983a. “Digital Homing Guidance: Stability vs. Performance Trade-Offs.” In Guidance and Control Conference. AIAA 1983-2167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2167
• Neuman, Frank. 1988. “Methodology for Determination and Use of the No-Escape Envelope of an Air-to-Air-Missile.” In Guidance, Navigation and Control Conference. AIAA 1988-4137. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4137
• 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
• Neurodynamics-Based Teleoperation. 2026. Wiley. https://doi.org/10.1002/9781394402762.ch11
• “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
• Newberry, Conrad, and Peter Badzey. 1990. “An Undergraduate Design for a Long-Range Air Launched Weapon (LAW) Propulsion System.” In 26th Joint Propulsion Conference. AIAA 1990-2391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2391
• Newell, J. F., and K. R. Rajagopal. 1993. “Application of Probabilistic Methods to the Structural Analysis of Liquid Rocket Engine Components.” In Volume 3A: General. American Society of Mechanical Engineers. https://doi.org/10.1115/93-gt-238
• Newirth, D. M., and C. J. Bosco. 1980. “Flight Test Reliability Demonstration of Electronic Engine Controls.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/801201
• Newman, Gary, Karen Fulcher, Robert Ray, and Mark Pinney. 1992. “On the Aerodynamics/dynamics of Store Separation from Hypersonic Aircraft.” In 10th Applied Aerodynamics Conference. AIAA 1992-2722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-2722
• Nguyễn, Thanh Tùng. 2019. “Evaluating Effectiveness of Extending Engagement Zone of Surface-to-Air Missile Using the Combinational Guidance Law CV-2DGOC.” Journal of Science and Technique 14 (1). https://doi.org/10.56651/lqdtu.jst.v14.n01.497
• Nguyen, Minh Phu. 2020. “Contour Design for Solid-Propellant Rocket-Engine Nozzle.” Journal of Science and Technique 15 (1). https://doi.org/10.56651/lqdtu.jst.v15.n01.105
• Nguyen, Dung The. 2021. “Internal Ballistics Calculations of the Solid Propellant Rocket Engine with Two Combustion Chambers.” Journal of Science and Technique 16 (3). https://doi.org/10.56651/lqdtu.jst.v16.n03.282
• Nguyen, Duc Thang. 2026. “Gravity Turn-Assisted Optimal Guidance Law for Short-Range Missile Interception.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0426086.066
• Nguyen, Thanh Chung, and Huu Tinh Cao. 2024. “Design of Robust H∞ Combined with PID Controller Using Fuzzy Logic for a Missile Autopilot.” Advances in Military Technology 19 (1): 41–53. https://doi.org/10.3849/aimt.01831
• Nguyen, V., C. Dang, and V. Luong. 2021. “Application of Learning Feed-Forward Controller Based on Model Reference Adaptive System for Missile Stabilization.” East European Scientific Journal 1 (4(68)): 34–39. https://doi.org/10.31618/essa.2782-1994.2021.1.68.11
• Nguyen, Tuan M., Pavel P. Popov, and William A. Sirignano. 2017. “Driving Mechanisms of Liquid-Propellant Rocket Longitudinal Combustion Instability.” In 55th AIAA Aerospace Sciences Meeting. AIAA 2017-0822. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-0822
• Nguyen, Tuan M., and William A. Sirignano. 2018. “Spontaneous and Triggered Longitudinal Combustion Instability in a Single-Injector Rocket Engine.” In 2018 Joint Propulsion Conference. AIAA 2018-4948. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4948
• Nguyen-Tat, Thang, Nhat-Minh Le-Phan, and Nga Thi-Thuy Vu. 2026. “Data-Driven Q-Learning Based Robust Longitudinal Missile Autopilot Design without Angle-of-Attack Measurement.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01203-w
• Ni, Weilin, Jianying Wang, Fuxiang Wu, Zhigang Wu, and Yonghai Wang. 2025b. “Cooperative Maneuvering Guidance for Glide Vehicles in Unknown Multiplayer Scenario via Meta-Reinforcement Learning.” Preprint, . https://doi.org/10.2139/ssrn.5370682
• 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
• Nicholls, J. A. 1969. Two Phase Detonation as Related to Rocket Motor Combustion Instability. NASA-CR-72532. NASA. https://ntrs.nasa.gov/citations/19690012792
• Nicholls, Robert E. 1982. Monopulse Angle Estimation from Coherently Integrated Radar Signals. Defense Technical Information Center. https://doi.org/10.21236/ada120427
• Nichols, Robert. 2008. “A Comparison of Hybrid RANS/LES Turbulence Models for a Generic Weapons Bay with and without a Spoiler.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6229. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6229
• Nichols, Robert, and William Westmoreland. 2006. “Comparison of CFD Approaches for Simulating Flow inside a Weapons Bay.” In 44th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2006-455. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-455
• Nickel, U. 1993. “Monopulse Estimation with Adaptive Arrays.” IEE Proceedings F Radar and Signal Processing 140 (5): 303. https://doi.org/10.1049/ip-f-2.1993.0042
• Nie, Tao, and Wei Qiang Liu. 2011a. “Numerical Study on 3D Coupled Heat Transfer of Thrust Chamber with Regenerative Cooling.” Applied Mechanics and Materials 52-54: 1057–61. https://doi.org/10.4028/www.scientific.net/amm.52-54.1057
• Nie, Tao, and Wei Qiang Liu. 2011b. “Research on Cooling Effect with Cooling Groove Structure Parameters of Liquid Rocket Engine Thrust Chamber.” Applied Mechanics and Materials 108: 7–11. https://doi.org/10.4028/www.scientific.net/amm.108.7
• Nie, Shunchen, Li Yu, Yanjun Li, Zhihong Sun, and Bowen Qiu. 2023b. “Influence of Fabric Permeability on Breathing Phenomenon of Supersonic Parachute.” Journal of Industrial Textiles 53: 15280837231171733. https://doi.org/10.1177/15280837231171733
• Nie, Cong, Ke Zhang, Pei Wang, and Meibo Lv. 2014. “A Method for Line of Sight Angle Rate Reconstruction Based on Strapdown Seeker.” In Advances in Engineering Research. Atlantis Press. https://doi.org/10.2991/meic-14.2014.147
• Nielsen, F. B. 1966. Combustion Termination System for 120-INCH-DIAMETER Solid Rocket Motor (Titan Iii-c). Defense Technical Information Center. https://doi.org/10.21236/ad0804269
• 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, Jack N. 1988b. The Present Status and the Future of Missile Aerodynamics. NASA-TM-100063. NASA. https://ntrs.nasa.gov/citations/19880020389
• Nielsen, Jack N. 1989. “The Present Status and the Future of Missile Aerodynamics.” In AGARD, Stability and Control of Tactical Missile Systems. https://ntrs.nasa.gov/citations/19900000735
• Nielsen, J., F. Goodwin, M. Dillenius, and M. Hemsch. 1984. “Prediction of Cruciform All-Movable Control Characteristics at Transonic Speeds.” In 22nd Aerospace Sciences Meeting. AIAA 1984-312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-312
• Nietubicz, Charles J. 1975. Some Aerodynamic Characteristics of Supersonic Lifting Bodies. Defense Technical Information Center. https://doi.org/10.21236/ada009704
• 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
• Niino, M., A. Kumakawa, N. Yatsuyanagi, and A. Suzuki. 1982. “Heat Transfer Characteristics of Liquid Hydrogen as a Coolant for the LO2/LH2 Rocket Thrust Chamber with the Channel Wall Construction.” In 18th Joint Propulsion Conference. AIAA 1982-1107. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1107
• 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
• 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, Hongru, and Yongzhi Sheng. 2025. “Three-Dimensional Prescribed-Time Cooperative Guidance Law with Impact Angle Constraint.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2264-1_41
• Ninh, Nguyen The. 2026. “Synthesis Study of Air-to-Air Missile Guidance Methods for Long-Range Interception of Separating Targets.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate0226015.013
• Niu, Kang, Xu Bai, Li Jiaxun, and Jian-Qiao Yu. 2024. “Three-Dimensional Impact Angle Constraint Guidance Law Design via Appointed-Time Convergence Theory and Back-Stepping Method.” Preprint, . https://doi.org/10.2139/ssrn.4916519
• 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
• Noel, Milton B., and Paul F. Massier. 1962. Development of a Light-Weight Regeneratively Cooled Thrust Chamber with Brazed Ribs and Brazed Outer Wire Trap. JPL-TR-32-219. Jet Propulsion Lab. https://ntrs.nasa.gov/citations/19620002673
• Noetscher, Gregory, Terence M. Rose, and Keith Bergeron. 2019. “Modeling and Experimental Efforts towards Robust Low-Cost Cruciform Canopy Control.” In AIAA Aviation 2019 Forum. AIAA 2019-3371. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3371
• Noffz, Gregory, and Robert Curry. 1991. “Summary of Aerothermal Test Results from the First Flight of the Pegasus Air-Launched Space Booster.” In 3rd International Aerospace Planes Conference. AIAA 1991-5046. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-5046
• Noh, Eunyoung. 2024. “Design of Emergency Destruction System for Long-Range Surface-to-Air Missile Flight Test.” Journal of the Korea Institute of Military Science and Technology 27 (4): 466–73. https://doi.org/10.9766/kimst.2024.27.4.466
• Nonaka, Satoshi, Tomotaro Muto, Takahiro Nakamura, and Hiroyuki Nishida. 2022. “Aerodynamic Characteristics of a Slender-Body Ejecting a Supersonic Jet.” Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 20 (0): 59–63. https://doi.org/10.2322/tastj.20.59
• “Nonequilibrium Stagnation Region Aerodynamic Heating of Hypersonic Glide Vehicles.” 1975. In Heat Transfer with Thermal Control Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600865138.0415.0435
• “Nonlinear Effects in Instability of Solid- Propellant Rocket Motors.” 1964. In Solid Propellant Rocket Conference. AIAA 1964-140. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-140
• North, Robert A., and Victor A. Riley. 1989. “W/INDEX: A Predictive Model of Operator Workload.” In Applications of Human Performance Models to System Design. Springer US. https://doi.org/10.1007/978-1-4757-9244-7_6
• 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
• Novean, M., J. Schetz, R. Bowersox, M. Novean, J. Schetz, and R. Bowersox. 1997. “Direct Measurements of Skin Friction in Complex Supersonic Flows.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-394
• “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
• Novikov, V. S. 2023. “Prospects for Developing Medium-Range Surface-to-Air Missile Systems.” Military Thought 32 (002): 157–60. https://doi.org/10.21557/mth.85716320
• Novozhilov, Boris, Vladimir Marshakov, and Vasily Novozhilov. 2018. “Solution of Inverse Problem of the Theory of Nonsteady Solid Propellant Combustion under the Pressure Drop in Rocket Engine.” In AIP Conference Proceedings, vol. 2046. Author(s). https://doi.org/10.1063/1.5081588
• Nulk, R., H. Pastrick, and P. Morrison. 1978. “Copperhead Semi-Active Laser Guidance System Development.” In Guidance and Control Conference. AIAA 1978-1261. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1261
• “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 Investigation of Impinging Planar Shock Wave Interaction with Axisymmetric Slender Body.” 2025. Journal of Applied Fluid Mechanics 18 (3). https://doi.org/10.47176/jafm.18.3.2768
• Numerical Method and Simulations of Liquid Rocket Engine Combustion Process. 2016. Wiley. https://doi.org/10.1002/9781118890035.ch8
• “Numerical Simulation of High-Frequency Combustion Instabilities in Liquid Rocket Engines.” 1996. In Recent Advances in Spray Combustion: Spray Combustion Measurements and Model Simulation. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866432.0331.0347
• “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
• Nurohman, Chandra, Ony Arifianto, and Agra Barecasco. 2018. “Hinge Moment Coefficient Prediction Tool and Control Force Analysis of Extra-300 Aerobatic Aircraft.” Journal of Physics: Conference Series 1005: 012020. https://doi.org/10.1088/1742-6596/1005/1/012020
• Nusca, Michael. 2007. “Utility of Computational Modeling for the Study of Combustion Instability in Small MMH-NTO Liquid Rocket Engines.” In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2007-5562. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5562
• Nusca, Michael. 2008. “Investigation of Combustion Instability in Small MMH-NTO Liquid Rocket Engines Using CFD.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-4545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4545
• Nusca, Michael. 2010. “Modeling Combustion Instability in Small MMH-NTO Liquid Rocket Engines Using CFD: Injector-Chamber Coupling.” In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2010-1518. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1518
• Nygaard, Tor. 2003. “Aeromechanic Analysis of a Missile with Freely Spinning Tailfins.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3672
• 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’Connor, John J. 1975. Transformations Applicable to Missile and Satellite Trajectory Computations. Defense Technical Information Center. https://doi.org/10.21236/ada013969
• Obery, Leonard J., and Howard S. Krasnow. 1952. Performance Characteristics of Canard-Type Missile with Vertically Mounted Nacelle Engines at Mach Numbers 1.5 to 2.0. NACA-RM-E52H08. NASA. https://ntrs.nasa.gov/citations/19930087279
• Obrien, Charles J. 1989. Transpiration and Regenerative Cooling of Rocket Engine. MFS-28251. Aerojet TechSystems Co. https://ntrs.nasa.gov/citations/19890000415
• Ochi, Yoshimasa. 2003. “Missile Guidance Law Design Based on Two-Degree-of-Freedom Bearing Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2003-5578. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-5578
• Ognjanovic, Ognjen, Stevan Maksimovic, Nenad Vidanovic, Stevo Segan, and Gordana Kastratovic. 2017. “Numerical Aerodynamic-Thermal-Structural Analyses of Missile Fin Configuration during Supersonic Flight Conditions.” Thermal Science 21 (6 Part B): 3037–49. https://doi.org/10.2298/tsci160919318o
• 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, Jae-Hyuk. 2001. “Zero Miss Distance of Pure PNG.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4278
• Ohashi, Hideo. 1968. “Turbopumps of Liquid Propellant Rocket Engine.” Journal of the Society of Mechanical Engineers 71 (591): 527–34. https://doi.org/10.1299/jsmemag.71.591_527
• Ohlmeyer, Ernest. 1996. “Root-Mean-Square Miss Distance of Proportional Navigation Missile against Sinusoidal Target.” In Guidance, Navigation, and Control Conference. AIAA 1996-3838. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3838
• Ohlmeyer, Ernest, and P. Menon. 2001. “Nonlinear Integrated Guidance-Control Laws for Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4160
• Okano, Seiko. 2015. Air and Missile Defense Radar (AMDR). Defense Technical Information Center. https://doi.org/10.21236/ad1018973
• Oktay, E., and C. Asma. 2000. “Drag Prediction with a Euler Solver at Supersonic Speeds.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-392. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-392
• Okuno, Yoshinori, and Shigeya Watanabe. 1992. “Optimal Launch Trajectory of a Hypersonic Research Vehicle.” In Guidance, Navigation and Control Conference. AIAA 1992-4302. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4302
• Olejnik, Aleksander, and Piotr Zalewski. 2020. “Su-22 and MiG-29 Aircraft as Air-Launch Platforms for Space Rockets.” Bulletin of the Military University of Technology 69 (3): 89–103. https://doi.org/10.5604/01.3001.0014.8874
• Olsen, Susan R. 2011. Mission Assurance Analysis of Theater Ballistic Missile Defense Systems. Defense Technical Information Center. https://doi.org/10.21236/ada547967
• Omar, Hanafy. 2008. “Optimal Integrated Fuzzy Guidance Law for Short Range Homing Missiles.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-875. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-875
• Omori, S. 1973a. Calculation of Eddy Viscosity in a Compressible Turbulent Boundary Layer with Mass Injection and Chemical Reaction, Volume 2. NASA-CR-129019-VOL-2. NASA. https://ntrs.nasa.gov/citations/19740008905
• Omori, S., K. W. Gross, and A. Krebsbach. 1972. Wall Temperature Distribution Calculation for a Rocket Nozzle Contour. NASA-TN-D-6825. NASA. https://ntrs.nasa.gov/citations/19720023123
• Ong, Shaw, and Bion Pierson. 1992. “Optimal Evasive Aircraft Maneuvers against a SAM Guided by Proportional Navigation.” In Guidance, Navigation and Control Conference. AIAA 1992-4348. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-4348
• Ooi, Hong Yee Julian. 2024. “Aerodynamic Challenges and Innovations in Wing Designs for Supersonic Flight: A Comprehensive Review.” International Journal of Science and Healthcare Research 9 (4): 454–63. https://doi.org/10.52403/ijshr.20240450
• “Operational Base Missile Test Programs.” 2021. In Minuteman. University of Arkansas Press. https://doi.org/10.2307/j.ctv19wx7k1.23
• “Optimal Guidance for Intercept.” 2024. In Optimal Trajectory Estimation for Missile Defense Applications. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624107092.0307.0328
• “Optimal Guidance Laws with Impact Angle Control.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-18
• 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
• Orr, Jeb S., and Colter W. Russell. n.d. “A Modern Load Relief Guidance Scheme for Space Launch Vehicles.” In 44th Annual AAS Guidance, Navigation and Control (GN&C) Conference. https://ntrs.nasa.gov/citations/20220000587
• Osborn, J. R., and L. R. Davis. 1961. Effects of Injection Location on Combustion Instability in Premixed Gaseous Bipropellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0253633
• Osborn, J. R., and R. M. Schiewe. 1958. An Experimental Investigation of High Frequency Combustion Pressure Oscillations in a Gaseous Bipropellant Rocket Motor. Defense Technical Information Center. https://doi.org/10.21236/ad0161563
• Osherov, A., and B. Natan. 1999. “Combustion Instability in a Small Liquid Rocket Motor.” Aeronautical Journal 103 (1023): 245–52. https://doi.org/10.1017/s0001924000027913
• Oshman, Yaakov, and David Arad. 2001. “Enhanced Air-to-Air Missile Tracking Using Target Orientation Observations.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4110. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4110
• 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
• Otto, Jim. 1993. AMC-SWMO Countermeasures Study; Volume 4: Guide to Army Smart Weapon Testing Issues. Defense Technical Information Center. https://doi.org/10.21236/ada363807
• Otto, Edward W., and Richard A. Flage. 1960. “Experimental Studies of Combustion Chamber and Feed System Stability during Throttling of a Regeneratively Cooled Liquid Hydrogen: Fluorine Rocket Engine.” In SAE Technical Paper Series, vol. 1. SAE International. https://doi.org/10.4271/600403
• Oza, Harshal, and Radhakant Padhi. 2010. “A Nonlinear Suboptimal Guidance Law with 3D Impact Angle Constraints for Ground Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8185. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8185
• 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
• Özgür, Onur, Abdullah E. Çetiner, Bedri Yagiz, and Goktan Guzel. 2016. “Store Separation Analyses by Means of Response Surface Modeling.” In 34th AIAA Applied Aerodynamics Conference. AIAA 2016-4335. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4335
• ÖZkan, Bülent. 2021. “Investigation of the Performance Characteristics of the Angle-Based Proportional Navigation Guidance Law.” European Journal of Science and Technology. https://doi.org/10.31590/ejosat.1006720
• Ozkan, Bulent, M. Kemal Ozgoren, and Gokmen Mahmutyazicioglu. 2008. “Guidance and Control of Two-Part Homing Missiles Using the Proportional Navigation Guidance Law.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6499
• Ożóg, Rafał, Mariusz Jacewicz, and Robert Głębocki. 2020. “Use of Wind Tunnel Measurements Data in Cold Launched Missile Flight Simulations.” Pomiary Automatyka Robotyka 24 (1): 49–60. https://doi.org/10.14313/par_235/49
• 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
• Pachikara, Abraham, and Rick Lind. 2012. “Flight Dynamics of a Micro Air Vehicle with Aeroservoelastic Interactions across a Range of Wing Stiffness.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2012-4577. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4577
• Pachter, Meir N., Phillip R. Chandler, and Dharba Swaroop. 2008. “Optimal Control of an ATR Module: Equipped MAV/Human Operator Team.” In Edward Elgar Publishing eBooks. Edward Elgar Publishing. https://doi.org/10.4337/9781035305520.00016
• Pacis, E. B., H. R. Everett, N. Farrington, and S. Khurana. 2004. Towards a Warfighter’s Associate: Eliminating the Operator Control Unit. Defense Technical Information Center. https://doi.org/10.21236/ada457986
• Packard, James, and Mark Miller. 2000. “Assessment of Engineering-Level Codes for Missile Aerodynamic Design and Analysis.” In Atmospheric Flight Mechanics Conference. AIAA 2000-4590. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4590
• Pagan, Didier, and Pascal Molton. 1991. “Basic Experiment on a Supersonic Vortex Flow around a Missile Body.” In 29th Aerospace Sciences Meeting. AIAA 1991-287. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-287
• Pages, Chris, and Ethan Achipa. 2026. “Development of a Propane-Oxygen Torch Igniter for a Small Liquid Rocket Engine Test Stand.” In 2026 Regional Student Conferences. AIAA 2026-114634. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-114634
• Paine, A. S. 2023. “Adaptive Monopulse Error Estimation for Radar Track Updates.” IET Conference Proceedings 2022 (17): 266–71. https://doi.org/10.1049/icp.2022.2328
• Pakulak Jr., Kuletz Jack M., and Edward. 1982. Thermal Stability of Six Candidate Propellants for an Air-Launched Tactical Missile. Defense Technical Information Center. https://doi.org/10.21236/ada116682
• Palej, Patryk, and Tomasz Palacz. 2018. “Preliminary Design Analysis of Regenerative Cooling for N 2 O/Alcohol Small Scale Liquid Rocket Engine.” Transactions on Aerospace Research 2018 (3): 87–102. https://doi.org/10.2478/tar-2018-0024
• Pan, Jiaxing, Jiajia Ma, Junhua Huang, and Chong Sun. 2025. “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
• 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
• Pandya, S., and M. Aftosmis. 2001. “Computation of External Aerodynamics for a Canard Rotor/wing Aircraft.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-997
• 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
• Panzirsch, Michael. n.d. “Passivity-Based Multilateral Control for Delayed Teleoperation.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.52592
• 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
• Pappas, C. C. 1954. Measurement of Heat Transfer in the Turbulent Boundary Layer on a Flat Plate in a Supersonic Flow and Comparison with Skin Friction Results. NACA-TN-3222. NASA. https://ntrs.nasa.gov/citations/19930084126
• Paradise, J. J. 1971. A Release Mechanism with Mechanical Redundancy. Lockheed Missiles and Space Co. https://ntrs.nasa.gov/citations/19720005757
• Park, Hee-Ho. 2005. “A Study on Regenerative Cooling System for Thrust Chamber Protection.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (3): 78–85. https://doi.org/10.5139/jksas.2005.33.3.078
• Park, Bong-Gyun. 2015. “Optimal Impact Angle Constrained Guidance with the Seeker’s Lock-on Condition.” Journal of the Korea Society for Industrial and Applied Mathematics 19 (3): 289–303. https://doi.org/10.12941/jksiam.2015.19.289
• 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, G., and M. Abla. 1982. “Determination of Learjet Longhorn Airplane Horizontal Tail Load and Hinge Moment Characteristics from Flight Data.” In 20th Aerospace Sciences Meeting. AIAA 1982-183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-183
• Park, Jongmin, and Sang-Joon Chung. 2012. “The Study on Experimental Measurement Method of Hinge Moment Acting on Control Surface of Air Vehicle.” Journal of the Korean Society for Aeronautical & Space Sciences 40 (2): 165–70. https://doi.org/10.5139/jksas.2012.40.2.165
• Park, Young-Ha, Sang-Eon Je, and Soo-Yong Cho. 2013. “Aerodynamics Characteristics on a Canard-Controlled Projectile.” Journal of the Korean Society of Propulsion Engineers 17 (1): 42–51. https://doi.org/10.6108/kspe.2013.17.1.042
• Park, Tae Seon, and Tae Jun Jeon. 2024. “Thermal Recycling Analysis in Regenerative Cooling Channels Based on Liquid Rocket Engine Cycles.” Preprint, . https://doi.org/10.2139/ssrn.4801252
• Park, Myung-Hoon, Jeong Kim, Jae-Deok Jang, Se-Woong Kwon, and Sun-Hyeok Hwang. 2026a. “Analysis of Monopulse Angle Estimation Errors in Electronically Scanned AESA Radars.” Journal of the Korea Institute of Information and Communication Engineering 30 (9): 1655–65. https://doi.org/10.6109/jkiice.2026.30.9.1655
• Park, Myung-Hoon, Jeong Kim, Jae-Deok Jang, Se-Woong Kwon, and So-Yeong Lee. 2026b. “Measurement Quality Based Terminal Guidance Method for Active Radar Seeker.” Journal of the Korea Institute of Information and Communication Engineering 30 (6): 1032–41. https://doi.org/10.6109/jkiice.2026.30.6.1032
• Park, Jang-Seong, Yun-Young Kim, Sanghyuk Park, and Yoon-Hwan Kim. 2020. “Asynchronous Guidance Filter Design Based on Strapdown Seeker and INS Information.” Journal of the Korean Society for Aeronautical & Space Sciences 48 (11): 873–80. https://doi.org/10.5139/jksas.2020.48.11.873
• Park, Kyung-Su, Yang Na, and Changjin Lee. 2016a. “Internal Flow Characteristics and Low-Frequency Instability in Hybrid Rocket Combustion.” In Springer Aerospace Technology. Springer International Publishing. https://doi.org/10.1007/978-3-319-27748-6_23
• Park, Jinwoo, Byunggil Yu, Euntae Jung, Ilhyun Park, Jongwoo Seo, and Jaesoo Jung. 2021. “A Study on Antenna of Low-Probability of Intercept for LOS Datalink System.” Journal of the Korea Institute of Military Science and Technology 24 (5): 519–26. https://doi.org/10.9766/kimst.2021.24.5.519
• Parker, Hermon M. 1955. Minimum-Drag Ducted and Pointed Bodies of Revolution Based on Linearized Supersonic Theory. NACA-TR-1213. NASA. https://ntrs.nasa.gov/citations/19930092224
• 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
• Parraud, Pascal. 2006. “Smooth Attitude Guidance Laws for Homing Maneuvers.” In SpaceOps 2006 Conference. AIAA 2006-5621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-5621
• Parris, Daniel K., and D. Brian Landrum. 2005. Effect of Tube Geometry on Regenerative Cooling Performance. AlAA Paper 2005-4301. Alabama Univ. https://ntrs.nasa.gov/citations/20050209950
• 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
• Pasqual, Mack, and Daniel DeLaurentis. 2012. “Measurement Fusion via Covariance Intersection for Ballistic Missile Tracking.” In Infotech@Aerospace 2012. AIAA 2012-2564. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-2564
• 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, Dimal. 2016a. “Antares Liquid Rocket Engine Convective Base Heating: AJ-26 to RD-181.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2016-4415. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4415
• Patel, Dimal. 2016b. “Antares Liquid Rocket Engine IOP and Transient Flow Entertainment: AJ-26 to RD-181.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2016-4414. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-4414
• Patel, Mehul, Jack DiCocco, Troy Prince, and Terry Ng. 2003a. “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
• Patel, Anant, Alex Forbes, and Narayanan Komerath. 2011. “Drag Prediction for Supersonic Hydrogen-Fueled Airliners.” In 29th AIAA Applied Aerodynamics Conference. AIAA 2011-3968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-3968
• Patel, Mehul, Terry Ng, and Alan Cain. 2003b. “A CFD Study of a Missile Aero Control Fin by near-Wall Flow Modifications.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-547
• Patterson, Douglas M., and Richard A. Ashley. 2000. “Glint Tracking Errors in Radar.” In Dynamic Modeling and Econometrics in Economics and Finance. Springer US. https://doi.org/10.1007/978-1-4419-8688-7_7
• Pauckert, R. P. 1968. Space Storable Regenerative Cooling Investigation Interim Report, Jul.: Dec. 1967. NASA-CR-72360. NASA. https://ntrs.nasa.gov/citations/19690009327
• Pauckert, R. P. 1970. Space Storable Regenerative Cooling Investigation Final Report, Jul. 1967: May 1970. NASA-CR-72705. NASA. https://ntrs.nasa.gov/citations/19710016325
• Pauckert, R. P., and R. D. Tobin. 1975. Space Shuttle Orbit Maneuvering Engine Reusable Thrust Chamber Program. NASA-CR-144441. NASA. https://ntrs.nasa.gov/citations/19750024091
• Paus, Michael, and Klaus Well. 1996. “Optimal Ascent Guidance for a Hypersonic Vehicle.” In Guidance, Navigation, and Control Conference. AIAA 1996-3901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3901
• Pavacic, Andrew. 2013. “2DZAP: A Program for Simulating Air-Launched Missiles.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-4015. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-4015
• Pavlenko, Olga V., and Evgeny A. Pigusov. 2018. “Numerical Investigation of the Aerodynamic Loads and Hinge Moments of the Flap with Boundary Layer Control.” In AIP Conference Proceedings, vol. 1959. Author(s). https://doi.org/10.1063/1.5034652
• Pavlenko, Olga V., and Mustafa G. Reslan. 2022. “Influence of Interference of the Airscrew and the High-Aspect-Ratio Wing on the Hinge Moment Deflect Control Surfaces of the Wing.” Vestnik Moskovskogo aviatsionnogo instituta 29 (3): 17–28. https://doi.org/10.34759/vst-2022-3-17-28
• Pearl, Raymond. 1908a. “On Certain Points Concerning the Probable Error of the Standard Deviation.” Biometrika 6 (1): 112. https://doi.org/10.2307/2331564
• Pearl, R. 1908b. “VII. on Certain Points Concerning the Probable Error of the Standard Deviation.” Biometrika 6 (1): 112–16. https://doi.org/10.1093/biomet/6.1.112
• Pearson, David, and Hari Hablani. 2001. “Determination of Guidance Parameters of Exo-Atmospheric Interceptors via Miss Distance Error Analysis.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4279. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4279
• Pedersen, Paul E. 1961. Study of Parachute Performance at Low Supersonic Deployment Speeds: Effects of Changing Scale and Clustering. Defense Technical Information Center. https://doi.org/10.21236/ad0267502
• Peebles, Curtis. 2006. “The X-43A Fin Actuator System Controversy: Reliability in Shades of Grey.” In Space 2006. AIAA 2006-7469. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-7469
• Peery, H. Rodney. 1960. A Self-Adaptive Missile Guidance System for Statistical Inputs. NASA-TN-D-343. NASA. https://ntrs.nasa.gov/citations/19980227306
• Pelevin, F. V., and A. V. Ponomarev. 2018. “To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber.” Russian Aeronautics 61 (1): 71–77. https://doi.org/10.3103/s1068799818010117
• Pelevin, Fedor V., and Aleksey V. Ponomarev. 2021. “A REGENERATIVE COOLING SYSTEM FOR THE CHAMBER OF A LIQUID-PROPELLANT ROCKET ENGINE WITH INTERCHANNEL COOLANT FLOW THROUGH A METAL MESH.” Space engineering and technology: 65–77. https://doi.org/10.33950/spacetech-2308-7625-2020-4-65-77
• Pell, K., A. Presson, R. Conard, and D. Brown. 1977. Status of the Laser Automated Missile Position and Attitude Measurement System. Defense Technical Information Center. https://doi.org/10.21236/ada048348
• Pempie, Pascal, and Hilda Vernin. 2001. “Liquid Rocket Engine Test Plan Comparison.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3256. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3256
• Penev, Borislav G. 2018. “An Expanded Two-Dimensional Proportional–Derivative Command to Line-of-Sight Guidance Law.” Gyroscopy and Navigation 9 (4): 344–51. https://doi.org/10.1134/s2075108718040132
• Peng, Zhi Ling. 2011. “Analysis of Aerodynamics Characteristic of High Length-to-Diameter Ratio Missile.” Advanced materials research 327: 153–58. https://doi.org/10.4028/www.scientific.net/amr.327.153
• Peng, Jun, Jun Wei Lei, and Di Liu. 2014. “The PID Control Stability Analysis and Simulation of Missile Posture Inner Loop Based on Simulink.” Applied Mechanics and Materials 644-650: 150–53. https://doi.org/10.4028/www.scientific.net/amm.644-650.150
• 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, W. 1977. Development of a Parachute Recovery System for a Reentry Nose Cone (NRV). Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/5306498
• Pepper, W. 1984. “Development of the Parachute Recovery System for the LBRV-2 Reentry Vehicle.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-802. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-802
• Pepper, W., H. Lucero, P. Klimas, R. Klein, and H. Antkowiak. 1984. “Adaptation of a 15-Ft-Dia Ribbon Parachute and a 73-Ft Cross Main Recovery Parachute for Cargo Delivery from High Altitude.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-790. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-790
• Pepper, W., Jr. 1979. “Preliminary Report on Development of an Interim Parachute Recovery System /IRS/ for a Reentry Vehicle.” In 6th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1979-468. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-468
• Pereira, Jennifer, and Melissa Richardson. 2023. “Uncertainty Analysis of Store Separation Aerodynamic Data at the NRC 1.5 m Trisonic Wind Tunnel.” In AIAA SCITECH 2023 Forum. AIAA 2023-2520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-2520
• Perelman, Andrey, Tal Shima, and Ilan Rusnak. 2010. “Cooperative Differential Games Strategies for Active Aircraft Protection from a Homing Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7878. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7878
• Pérez Roca, Sergio. n.d. “Model-Based Robust Transient Control of Reusable Liquid-Propellant Rocket Engines.” PhD diss., université Paris-Saclay. https://doi.org/10.70675/8da63282z9e21z49c0z9f67z0156f62140d8
• Peri, Lakshmi Narayana Phaneendra, Ingenito Antonella, and Paolo Teofilatto. 2023. “Large-Eddy Simulations of a Hypersonic Re-Entry Capsule Coupled with the Supersonic Disk-Gap-Band Parachute.” Preprint, . https://doi.org/10.20944/preprints202305.0350.v1
• Perkins, Thomas. n.d. “A Math Model of a Well Trained Human Operator Performing a Tracking Task.” PhD diss., Louisiana State University and Agricultural & Mechanical College. https://doi.org/10.31390/gradschool_disstheses.2628
• Perlmutter, Isaac, and Vincent DePierre. 1965. Steels for Solid-Propellant Rocket-Motor Cases. Defense Technical Information Center. https://doi.org/10.21236/ad0612646
• Persico, A. R., C. Clemente, and J. Soraghan. 2017. “CubeSAT Based Bistatic Passive Radar for Ballistic Missile Defence: Feasibility Study.” In International Conference on Radar Systems (Radar 2017). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2017.0444
• Peschka, Walter. 1992. “Liquid Hydrogen as a Rocket Propellant.” In Liquid Hydrogen. Springer Vienna. https://doi.org/10.1007/978-3-7091-9126-2_5
• 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
• Peter, Florian, Florian Holzapfel, Enric Xargay, and Naira Hovakimyan. 2012. “L1 Adaptive Augmentation of a Missile Autopilot.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4832. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4832
• Peters, Nicholas, John Ekaterinaris, and Andrew Wissink. 2021. “A Mode Based Reduced Order Model for Supersonic Store Separation.” In AIAA Aviation 2021 Forum. AIAA 2021-2548. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2548
• Peters, Nicholas, John A. Ekaterinaris, and Andrew M. Wissink. 2023. “A Data-Driven Modeling Approach for Rotorcraft Store Separation.” In AIAA SCITECH 2023 Forum. AIAA 2023-0233. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-0233
• Peters, Nicholas, Andrew M. Wissink, and John A. Ekaterinaris. 2022. “A Mode Based Reduced Order Model for Rotorcraft Store Separation.” In AIAA SCITECH 2022 Forum. AIAA 2022-0312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0312
• 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, C., D. Waye, L. Rollstin, and I. Holt. 1986. “Design and Performance of a Parachute for Supersonic and Subsonic Recovery of an 800-Lb Payload.” In 9th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1986-2435. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2435
• Petkosek, Michael A., Lamar Warfield, and Thomas R. Carretta. 2005. Development of a Human Performance Model of a UAV Sensor Operator: Lessons Learned. Defense Technical Information Center. https://doi.org/10.21236/ada437815
• Petters, J. R. 1952. Fuzing System for XSAM-N-4, Guided Missile Dove; Testing Of. Defense Technical Information Center. https://doi.org/10.21236/ad0015014
• Pew, R. W. 1966. Performance of Human Operators in a Three-State Relay Control System with Velocity-Augmented Displays. NASA. https://ntrs.nasa.gov/citations/19660051980
• 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
• Pharokhipanah, Tolou, and Sebastian Bouckenooghe. 2024. Development of Atlas: A Liquid Rocket Engine Cryogenic Feed System. https://doi.org/10.52202/078371-0178
• Philco Corp Palo Alto Ca. 1963. Life Test on WDL-RT-5A Radar Beacon Transponder with 6-COMMAND Decoder. Defense Technical Information Center. https://doi.org/10.21236/ad0296907
• Philipchuk, V. 1952. Warheads for Air Target Guided Missiles; Testing of. Investment Cast Steel Tube for Air Target Guided Missiles; Fragmentation Test Of. Defense Technical Information Center. https://doi.org/10.21236/ad0499509
• Philipchuk, V. 1953. Aap Rod Warhead and Slotted Rocket Motor Assembly No. 366. Defense Technical Information Center. https://doi.org/10.21236/ad0009072
• Philipson, Lloyd L. 1995. “Risk Assessments for Space and Missile Launch Hazards.” In Risk and Safety Assessments: Building Viable Solutions. American Society of Mechanical Engineers. https://doi.org/10.1115/imece1995-0453
• Phillips, Craig. 1993. “Preliminary Pulse Motor Optimization for a Surface-to-Air Missile.” In Guidance, Navigation and Control Conference. AIAA 1993-3741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3741
• Phillips, Craig. 1994. “Terminal Homing Performance of Semi-Active Missiles against Multi-Target Raids.” In Guidance, Navigation, and Control Conference. AIAA 1994-3605. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3605
• 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
• Piersol, Allan G. 1977. Evaluation of the Harpoon Missile Shock Environment during Ejection Launch by Aircraft Launchers. Defense Technical Information Center. https://doi.org/10.21236/ada037067
• Pilette, Sterling, Bill Biggs, and Harold Martinek. 1978. The Value of Special Training and Job Aids for Improving Unattended Ground Sensor Operator Performance. Defense Technical Information Center. https://doi.org/10.21236/ada061046
• 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
• Placco, L. 2023. “High-Fidelity Simulation of the Interaction between the Wake of a Descent Capsule and a Supersonic Parachute.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-42
• Plane, V. C. 1963. Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase I Report. Defense Technical Information Center. https://doi.org/10.21236/ad0605853
• Plane, V. C. 1964a. Total Impulse Measuring System for Solid Propellant Rocket Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0605491
• Plane, V. C. 1964b. Total Impulse Measuring System for Solid Propellant Rocket Engine: Installation and Operation Handbook. Defense Technical Information Center. https://doi.org/10.21236/ad0606515
• Plane, V. C. 1964c. Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase II Report. Defense Technical Information Center. https://doi.org/10.21236/ad0606557
• Platanitis, George, and Sergey Shkarayev. 2005. Integration of an Autopilot for a Micro Air Vehicle. FRS-340080. Arizona Univ. https://ntrs.nasa.gov/citations/20050185598
• Platus, D. H. 1998. Missile and Spacecraft Coning Instabilities. Defense Technical Information Center. https://doi.org/10.21236/ada349546
• Platzer, Max F. 2010. Missile Aerodynamics. Wiley. https://doi.org/10.1002/9780470686652.eae017
• Pleasants, J. 1975. “Flight Qualification of Mortar-Actuated Parachute Deployment Systems.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1403. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1403
• Podoprelov, Pavel, Nikolay Knapp, Khomidzhon Muratov, Dmitry Kolmykov, Roman Ledenev, and Pavel Skorodumov. 2021. TU-22M Soviet Long-Range Supersonic Missile-Bomber. Science and Innovation Center Publishing House. https://doi.org/10.12731/gorbachev.0414.15042021
• 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
• “Polynomial Approach for Design and Robust Analysis of Lateral Missile Control.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-10
• Poole, Harmon A. 1965. “A Stored Gas Actuator Unit for the TOW Missile.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/650338
• Popov, Pavel, Athanasios Sideris, and William A. Sirignano. 2013. “Stochastic Modeling of Transverse Wave Instability in a Liquid Propellant Rocket Engine.” In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2013-3777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-3777
• Popov, Pavel P., Athanasios Sideris, and William A. Sirignano. 2014a. “Propellant Feed System Influence on Rocket Engine Combustion Instability.” In 52nd Aerospace Sciences Meeting. AIAA 2014-0134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-0134
• Popov, Pavel P., Athanasios Sideris, and William A. Sirignano. 2014b. “Stochastic Modelling of Transverse Wave Instability in a Liquid-Propellant Rocket Engine.” Journal of Fluid Mechanics 745: 62–91. https://doi.org/10.1017/jfm.2014.96
• Popov, Pavel P., Athanasios Sideris, and William A. Sirignano. 2016. “Low-Probability Events Leading to Rocket Engine Combustion Instability.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-1932. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-1932
• Popov, Pavel P., and William A. Sirignano. 2015. “Transverse Combustion Instability in a Rectangular Rocket Motor.” In 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-4210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-4210
• Popovici, Alexandru, Petrus M. T. Zaal, Daan M. Pool, Max Mulder, and Marinus M. Van Paassen. 2017. “Effects of Eye Measures on Human Controller Remnant and Control Behavior.” In AIAA SciTech Forum. https://ntrs.nasa.gov/citations/20190027682
• Porter, H. K. 1968. Disposal Tests for AIR-2A ‘Genie’ Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0833638
• Poth, Stefan, Jr., Michael Fisher, David Levy, and Joe Eisley. 1993. “Design of an Airborne Launch Vehicle and an Air Launched Space Booster.” In Aircraft Design, Systems, and Operations Meeting. AIAA 1993-3955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3955
• Potter, J. 1964. “A Guidance-Navigation Separation Theorem.” In Astrodynamics Guidance and Control Conference. AIAA 1964-653. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-653
• Potter, J. E., and J. C. Deckert. 1972. Gyro and Accelerometer Failure Detection and Identification in Redundant Sensor Systems. NASA-CR-115749. NASA. https://ntrs.nasa.gov/citations/19720021024
• Potvin, Jean, Roberto Montanez, G. Peek, Jean Potvin, Roberto Montanez, and G. Peek. 1997. “The Parks College Ram-Air Parachute Deployment Study: A Status Report.” In 14th Aerodynamic Decelerator Systems Technology Conference. AIAA 1997-1426. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1426
• Potvin, Jean, and Jean Potvin. 1997. “Theoretical and Experimental Studies of Ram-Air Parachute Deployment Observable Variance.” In 14th Aerodynamic Decelerator Systems Technology Conference. AIAA 1997-1544. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1544
• Poulain, François, Hélène Piet-Lahanie, and Laurent Serre. 2009. “Nonlinear Control of a Airbreathing Hypersonic Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7290. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7290
• 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
• Poveda, Jorge, Nicolás Ochoa-Lleras, and Carlos Rodriguez. 2012. “Guidance of an Autonomous Glider Based on Proportional Navigation and Virtual Targets: A Hybrid Dynamical Systems Approach.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4905. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4905
• Powell, Thomas H. n.d. “Angular Accuracy of Monopulse Radar.” PhD diss., Drexel University. https://doi.org/10.17918/00007178
• Powell, R. B., D. W. Holder, and J. H. Wright. 1982. “Optical Fiber Data Link for Missile Guidance.” In SPIE Proceedings, vol. 0317, edited by Bob D. Guenther, William Pittman. SPIE. https://doi.org/10.1117/12.933096
• Powell, E. A., and B. T. Zinn. 1970. “Nonlinear Combustion Instability in Liquid- Propellant Rocket Engines.” In COMBUSTION INST., INTERNATIONAL SYMPOSIUM ON COMBUSTION, 13TH, U. OF UTAH. https://ntrs.nasa.gov/citations/19700068309
• Powell, E. A., and B. T. Zinn. 1973. The Prediction of Nonlinear Three Dimensional Combustion Instability in Liquid Rockets with Conventional Nozzles. NASA-CR-121279. NASA. https://ntrs.nasa.gov/citations/19740002748
• “Practical Considerations in Robust Control of Missiles.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-23
• Practical Issues for Radar Tracking. 1998. Wiley. https://doi.org/10.1002/0471224197.ch3
• “Practical Techniques for the Design of Multirate Digital Guidance Laws and Autopilots.” 2016. In Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503-21
• Prakash, Jose, K. E. Reby Roy, T.s Krishnakumar, et al. 2012. “Numerical Studies on Combustion in a Film Cooled Semi-Cryogenic Rocket Thrust Chamber.” In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2012-4167. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4167
• Prakash, Om, and Ritesh Singh. 2021. “Flight Dynamics Analysis Using High Altitude & Mach Number for Generic Air-Breathing Hypersonic Vehicle.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3271
• Prasad, M. V. K. S., Patri Sreehari Rao, and Jagannath Nayak. 2021. “Aeroload Simulation of Interceptor Missile Using Fin Load Simulator.” Defence Science Journal 71 (1): 102–7. https://doi.org/10.14429/dsj.71.16045
• Pratt, Patrick D. 1976. “Optical Heterodyne Radar (Ladar) for Precision Missile Tracking and Guidance.” In Conference on Laser and Electrooptical Systems. Optica Publishing Group. https://doi.org/10.1364/cleos.1976.tuc3
• 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
• “Pressurization of Liquid Propellant Rocket Engine Tanks.” 2019. In Chemical Kinetics in Combustion and Reactive Flows. Cambridge University Press. https://doi.org/10.1017/9781108581714.009
• Price, E. 1964. “Axial Mode, Intermediate Frequency Combustion Instability in Solid Propellant Rocket Motors.” In Solid Propellant Rocket Conference. AIAA 1964-146. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1964-146
• Price, Dennis L. 1970. “Operator-Mounted Controllers for Precision Tracking.” Human Factors: The Journal of the Human Factors and Ergonomics Society 12 (5): 485–91. https://doi.org/10.1177/001872087001200509
• Price, H. 1980. “Cooling of High Pressure Rocket Thrust Chambers with Liquid Oxygen.” In 16th Joint Propulsion Conference. AIAA 1980-1260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1260
• Price, E., and G. Dehority. 1967. “Velocity Coupled Axial Mode Combustion Instability in Solid Propellant Rocket Motors.” In 2nd Solid Propulsion Conference. AIAA 1967-1523. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1967-1523
• Price, William A., and Ernest H. Ehling. 1955. “Motion-Picture Photography in Guided-Missile Research.” SMPTE Journal 1955 64 (6): 310–14. https://doi.org/10.5594/j12159
• Price, E. W., and G. A. Flandro. 1987. Combustion Instability in Solid Propellant Rockets. Defense Technical Information Center. https://doi.org/10.21236/ada179701
• Price, Charles F., and Ronald S. Warren. 1973. Performance Evaluation of Homing Guidance Laws for Tactical Missiles. Defense Technical Information Center. https://doi.org/10.21236/ad0761626
• Priedhorsky, William, and James Wells. 2026. “Space-Based Missile Defense with Early Interceptor Launch Strategies.” Space & Defense. https://doi.org/10.32873/uno.dc.sd.17.01.1337
• Princeton Univ Nj. 1952. Combustion Instability in Liquid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0036008
• Priolo, F., and A. Wardlaw Jr. 1988. “Supersonic Non-Circular Missile Computations.” In 26th Aerospace Sciences Meeting. AIAA 1988-278. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-278
• Priolo, F., A. Wardlaw Jr., F. Baltakis, and J. Solomon. 1985. “Inviscid Multiple Zone Strategy Applied to Complicated Supersonic Tactical Missile Configurations.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1813. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1813
• 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
• Pritchett, Amy R., So Young Kim, and Karen M. Feigh. 2013a. “Measuring Human-Automation Function Allocation.” Journal of Cognitive Engineering and Decision Making 8 (1): 52–77. https://doi.org/10.1177/1555343413490166
• Pritchett, Amy R., So Young Kim, and Karen M. Feigh. 2013b. “Modeling Human–Automation Function Allocation.” Journal of Cognitive Engineering and Decision Making 8 (1): 33–51. https://doi.org/10.1177/1555343413490944
• Pritz, W., and R. Schoner. 1972. “Verification of a Comprehensive Thrust Chamber Compatibility Model for Liquid Rocket Engines.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1078. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1078
• Prizirembel, C. E., and D. T. Wen. 1978. Boundary Layer Separation from a Slender Body at High Angles of Attack. Defense Technical Information Center. https://doi.org/10.21236/ada064583
• Proceedings of the Seventeenth Annual Conference on Manual Control. 1981. NASA-CR-165005. NASA. https://ntrs.nasa.gov/citations/19820005792
• 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
• Prokopenko, Bohdan. 2026. “Method of Producing Clean Reducing Generator Gas for a Liquid Rocket Engine Turbopump Unit.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/3083-7057-2026-1-030
• Pruett, Stanley. 2008. “Urban Operator in the Loop Simulation.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6312. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6312
• Pshenychka, Yevhenii. 2026. “Cooling of Low-Thrust Liquid Rocket Engines with Liquid and Alkali Metals.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/3083-7057-2026-1-032
• Purvis, J. 1984. “Improved Prediction of Parachute Line Sail during Lines-First Deployment.” In 8th Aerodynamic Decelerator and Balloon Technology Conference. AIAA 1984-786. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-786
• Purwadi, Arif Rahmadhi Hidayat, Ilham Hariz, et al. 2023. “Designing of Hinge Moment Balance for Hinge Rudder Performance Measurement in Indonesian Low Speed Tunnel (ILST).” In AIP Conference Proceedings, vol. 2981. AIP Publishing. https://doi.org/10.1063/5.0181422
• Pustovyi, Roman. 2026. “Features of the Implementation of Additive Manufacturing for the Production of Liquid Rocket Engine Combustion Chamber Components.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/3083-7057-2026-1-031
• Qamar, Shabahat Hasnain, and Adrian David Cheok. 2023. “Numerical Simulation and Computational Fluid Dynamics Analysis of Two-Dimensional Lid-Driven Cavity Flow within the Weapon Bay of an Autonomous Fighter Drone.” Qeios. https://doi.org/10.32388/8a6rct
• Qi, Chen, and Ai Jianliang. 2017. “NDI-Based L1 Adaptive Control Design for a Generic Hypersonic Vehicle Model.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1248. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1248
• Qian, Zhang, Zhi Xu, Hong Bei, and Bao F. Yan. 2017. “A Guidance Scheme for Air-Launched Solid Launch Vehicle.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2141. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2141
• Qiao, Qing Qing, and Wan Chun Chen. 2013. “A near Optimal Midcourse Guidance Law for Air-to-Air Missile.” Applied Mechanics and Materials 336-338: 833–38. https://doi.org/10.4028/www.scientific.net/amm.336-338.833
• Qin, Yu-liang, and Yong-qiang Cheng. 2012. “Dynamic Multipath Model of Low Angle Passive Radar Tracking with Experimental Evaluation.” Defence Science Journal 62 (5): 331–37. https://doi.org/10.14429/dsj.62.1000
• Qin, Wutao, Xiaogang Wang, and Naigang Cui. 2017. “Maximum Correntropy Sparse Gauss–Hermite Quadrature Filter and Its Application in Tracking Ballistic Missile.” IET Radar, Sonar & Navigation 11 (9): 1388–96. https://doi.org/10.1049/iet-rsn.2016.0594
• Qin, Jianxiu, Huiqiang Zhang, and Bing Wang. 2016. “Numerical Investigation on Combustion Instability in a Small MMH/NTO Liquid Rocket Engine.” In 52nd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2016-5087. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5087
• Qing, KaiXin, Lingpeng Zhang, and Xunbin Yi. 2024. “Overview of Laser Semi-Active Guidance Jamming Technology.” In 2024 International Conference on Optoelectronic Information and Optical Engineering (OIOE 2024), edited by Harith Bin Ahmad, Ming Jiang. SPIE. https://doi.org/10.1117/12.3030720
• Qiu, Wenjie, Qingzhong Jia, Xiuyun Meng, and Yibo Sun. 2016. “Maximum Range Trajectory Optimization for a Boost-Glide Vehicle Using Adaptive Mesh Refinement Pseudospectral Methods.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231 (7): 1171–82. https://doi.org/10.1177/0954410016649208
• Qiu, Wenjie, Xiuyun Meng, and Youwei Kang. 2017. “Three-Dimensional Robust Guidance Law with Impact Angle Constraint and Compensation of Channels Coupling.” DEStech Transactions on Materials Science and Engineering, no. icmsme. https://doi.org/10.12783/dtmse/icmsme2016/7509
• Qiuqiu, Wen, Xia Qunli, and Su Weixia. 2016. “Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint.” Journal of Aerospace Engineering 29 (3): 04015067. https://doi.org/10.1061/(asce)as.1943-5525.0000552
• Qu, Jian-Ming, Chen-yang Yang, and Shiyi Mao. 1999. “Missile Angle Acquisition Based on Total Least Square Estimation with Phased Array Radar.” In SPIE Proceedings, vol. 3692, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.352879
• Qu, Pingping, Di Zhou, and Sheng Sun. 2017. “Observer-Based Guidance Law with Impact Angle Constraint.” Journal of Dynamic Systems, Measurement, and Control 139 (11): 114504. https://doi.org/10.1115/1.4036664
• Quam, D. 1978. “Missile Aerodynamic Sensitivity Analysis.” In 16th Aerospace Sciences Meeting. AIAA 1978-113. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-113
• Quentmeyer, R., H. Kasper, and J. Kazaroff. 1978. “Investigation of the Effect of Ceramic Coatings on Rocket Thrust Chamber Life.” In 14th Joint Propulsion Conference. AIAA 1978-1034. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1034
• Quillin, R. H., and E. M. Parry. 1962. Investigation of Stowage Hazards in Air Launched Missile Magazines: The Compatibility of Prepackaged Liquid- and Solid-Propellant Bullpup Missiles in a Common Shipboard Magazine. Defense Technical Information Center. https://doi.org/10.21236/ad0333070
• 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
• Rabinovitch, Jason, Gregory S. Griffin, William Seto, Clara O’Farrell, Christopher L. Tanner, and Ian G. Clark. 2019a. “ASPIRE Supersonic Parachute Shape Reconstruction.” In AIAA Scitech 2019 Forum. AIAA 2019-1629. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1629
• Rabinovitch, Jason, Zhengyu Huang, Philip Avery, Charbel Farhat, Armen Derkevorkian, and Lee D. Peterson. 2018. “Preliminary Verification and Validation Test Suite for the CFD Component of Supersonic Parachute Deployment FSI Simulations.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1542
• Rabinovitch, Jason, Daniel Z. Huang, Raunak Borker, et al. 2019b. “Towards a Validated FSI Computational Framework for Supersonic Parachute Deployments.” In AIAA Aviation 2019 Forum. AIAA 2019-3275. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3275
• “Radar Angle-of-Arrival Estimation.” 2013. In Angle-of-Arrival Estimation Using Radar Interferometry: Methods and Applications. Institution of Engineering and Technology. https://doi.org/10.1049/sbra508e_ch4
• “Radar Measurements and Target Tracking.” n.d. In Radar and Electronic Warfare Principles for the Non-specialist. Institution of Engineering and Technology. https://doi.org/10.1049/sbra502e_ch5
• Radar Resource Management for Target Tracking—a Stochastic Control Approach. 2014. Wiley. https://doi.org/10.1002/9781118450550.ch11
• “Radar Target Tracking Algorithm Based on Association Rules.” 2021. Machine Learning Theory and Practice 2 (3). https://doi.org/10.38007/ml.2021.020304
• “Radar Tracking Algorithms.” 2010. In Principles of Modern Radar: Basic principles. Institution of Engineering and Technology. https://doi.org/10.1049/sbra021e_ch19
• 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
• Rafique, Amer, and He LinShu. 2009. “Effect of Aerodynamic Enhancements on Flight Performance of Air Launched Satellite Launch Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7246. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7246
• Rafique, Amer, He LinShu, Ma Ying, Ali Kamran, and Qasim Zeeshan. 2010b. “Performance Enhancement of Air Launched Satellite Launch Vehicle Using Composite Motors.” In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th. AIAA 2010-2986. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-2986
• Rafique, Amer, He LinShu, and Qasim Zeeshan. 2009a. “Comparison of Heuristic Optimization Methods for Multidisciplinary Design of Air-Launched Space Launch Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7442. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7442
• Rafique, Amer, He LinShu, Qasim Zeeshan, and Ali Kamran. 2009b. “Design and Optimization of Air Launched Satellite Launch Vehicle Using Hybrid Heuristic Search Algorithm.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7394. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7394
• Rafique, Amer Farhan, Qasim Zeeshan, and Ali Kamran. 2014. “Design of Experiments Based Variation Mode and Effect Analysis of a Conceptual Air Launched SLV.” In AIP Conference Proceedings, vol. 1637. AIP Publishing LLC. https://doi.org/10.1063/1.4904657
• Rafla, Farid K. 2019. “Aerodynamic Heating Coupled with Structural Temperature Response Analysis for Hypersonic Flight Vehicles.” In AIAA Aviation 2019 Forum. AIAA 2019-3132. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3132
• Ragnoli, Giona, Raffaele Savino, Anselmo Cecere, and Marco Rigamonti. 2024. “Hypersonic Boost-Glide Systems: Flight Mechanics and Plasma Parameters Evaluation through Aero-Thermo-Chemical Cfd.” Preprint, . https://doi.org/10.2139/ssrn.4687892
• Rahaim, Christopher, Shawn Grage, William Margopoulos, and Robert Stachow. 2000. “A Design Tool for Missile System Rocket Motor Scaling.” In 18th Applied Aerodynamics Conference. AIAA 2000-4525. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4525
• Rahal, Rahaf. n.d. “Shared Control and Authority Distribution for Robotic Teleoperation.” PhD diss., Rennes 1. https://doi.org/10.70675/faa0a309z8a93z4a80zbfadz5bf5a34e52a0
• Rahn, Daniel, Hendrik Riedmann, and Oskar Haidn. 2019. “Conjugate Heat Transfer Simulation of a Subscale Rocket Thrust Chamber Using a Timescale Based Frozen Non-Adiabatic Flamelet Combustion Model.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-3864. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3864
• Rainey, Robert W. 1951. Langley 9-Inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces: Three-Component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to and Less than 1 and Some Static. NACA-RM-L50G07. NASA. https://ntrs.nasa.gov/citations/19930086355
• Raisinghani, S. C., and S. Rao. 1983. “Perturbed Motion of Airplane and Safe Store Separation.” Defence Science Journal 33 (3): 221–34. https://doi.org/10.14429/dsj.33.7684
• Raisinghani, S. C., and S. Rao. 1984. “Perturbed Motion of Airplane and Safe Store Separation.” Defence Science Journal 34 (3): 221–34. https://doi.org/10.14429/dsj.34.7685
• Raivio, Tuomas, and Jukka Ranta. 2002. “Optimal Missile Avoidance Trajectory Synthesis in the Endgame.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4947. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4947
• Rajagopal, Manikanda. 2015. “Numerical Modeling of Regenerative Cooling System for Large Expansion Ratio Rocket Engines.” Journal of Thermal Science and Engineering Applications 7 (1): 011012. https://doi.org/10.1115/1.4028979
• Rajagopal, Karthikeyan, and S. Balakrishnan. 2012. “Adaptive Neural Network– Based Autopilot Design.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-5
• Rajan, K. M., and K. Narasimhan. 2005. “Design and Structural Analysis of a Thrust Chamber for a Spinning Supersonic Rocket – a Case Study.” Aeronautical Journal 109 (1094): I-VI. https://doi.org/10.1017/s0001924000000701
• Rakita, Daniel, Bilge Mutlu, and Michael Gleicher. 2020. “Effects of Onset Latency and Robot Speed Delays on Mimicry-Control Teleoperation.” In Proceedings of the 2020 ACM/IEEE International Conference on Human-Robot Interaction. ACM. https://doi.org/10.1145/3319502.3374838
• 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
• Rand, James L. 1963. The Aerodynamic Heating of a Composite Flat Plate. Defense Technical Information Center. https://doi.org/10.21236/ad0419249
• Raney, David, John McMinn, Anthony Pototzky, and Christine Wooley. 1993. “Impact of Aeroelasticitu on Propulsion and Longitudinal Flight Dynamics of an Air-Breathing Hypersonic Vehicle.” In 34th Structures, Structural Dynamics and Materials Conference. AIAA 1993-1367. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1367
• Rao, G. Kumaraswamy, Sreehari Rao, and Sudhir Kumar Chaudhuri. 2017. “Networking of Tracking Radars of Two Different SAM Weapons to Protect the Missile in Intensive Jamming Environment.” Defence Science Journal 68 (1): 70. https://doi.org/10.14429/dsj.68.10993
• Rao, C. R., L. Zhang, and L. C. Zhao. 1993. “New Algorithm for Multitarget Angle Tracking.” IEE Proceedings F Radar and Signal Processing 140 (5): 335. https://doi.org/10.1049/ip-f-2.1993.0047
• Rapp, Douglas. 1993. “Reliability Assessment of Thrust Chamber Cooling Concepts Using Probabilistic Analysis Techniques.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-2163. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2163
• Raspopov, V. Ya. 2018. “The Technology Level of Promising Gyroscope-Based Angular Rate Sensors.” Spravochnik. Inzhenernyi zhurnal: 27–35. https://doi.org/10.14489/hb.2018.12.pp.027-035
• 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
• Ratnoo, Ashwini. 2015. “Analysis of Two-Stage Proportional Navigation with Impact Angle and Field-of-View Constraints.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0615
• Ratnoo, Ashwini, and Debasish Ghose. 2007. “SDRE Based Guidance Law for Impact Angle Constrained Trajectories.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6539
• Ratnoo, Ashwini, and Debasish Ghose. 2008b. “Pure Proportional Navigation for Impact Angle Constrained Interception of Stationary Targets.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7306. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7306
• Ratnoo, Ashwini, and Debasish Ghose. 2009a. “Satisfying Terminal Angular Constraint Using Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-6088. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6088
• Ratnoo, Ashwini, and Tal Shima. 2010. “Line of Sight Guidance for Defending an Aircraft.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7877. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7877
• Ray, E. 2000. “Comparison of AEDC 4T and CALSPAN 8-Ft Wind Tunnels for F/A-18C/JDAM Store Separation.” In 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-793. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-793
• Rea, Jeremy R., and Zachary R. Putnam. 2007. “A Comparison of Two Skip Entry Guidance Algorithms.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20070023643
• 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 Unilateral Teleoperation System for Arm Movement Performance.” 2011. In International Conference on Informatics in Control, Automation and Robotics (ICINCO). https://doi.org/10.5220/0003537703040307
• Rebeiz, Gabriel M. 2000. W-Band Polarimetric Monopulse Tracking Receiver. Defense Technical Information Center. https://doi.org/10.21236/ada379069
• Reches, Mark. 1980. “Weapon Effectiveness and Casualty Reduction Analysis.” In Methods and Phenomena. Elsevier. https://doi.org/10.1016/b978-0-444-41928-6.50013-2
• “Recording Store Separation Safe and Sound.” 2022. Aerospace Testing International 2022 (2): 72–72. https://doi.org/10.12968/s1478-2774(23)50022-3
• 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
• Reda, D. 1978. “Boundary-Layer Transition Experiments on Sharp, Slender Cones in Supersonic Freeflight.” In 11th Fluid and PlasmaDynamics Conference. AIAA 1978-1129. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1129
• Reda, D., F. Ketter Jr., and C. Fan. 1974. “Compressible Turbulent Skin Friction on Rough and Rough/wavy Walls in Adiabatic Flow.” In 7th Fluid and PlasmaDynamics Conference. AIAA 1974-574. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-574
• Rehman, Obaid Ur, Baris Fidan, and Ian Petersen. 2009. “Minimax LQR Control Design for a Hypersonic Flight Vehicle.” In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2009-7291. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-7291
• 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, J. P., and S. Haykin. 1982. “Maximum-Likelihood Receiver for Low-Angle Tracking Radar. Part 2: The Nonsymmetric Case.” IEE Proceedings F Communications, Radar and Signal Processing 129 (5): 331. https://doi.org/10.1049/ip-f-1.1982.0050
• Reilly, J., J. Litva, and P. Bauman. 1988. “New Angle-of-Arrival Estimator: Comparative Evaluation Applied to the Low-Angle Tracking Radar Problem.” IEE Proceedings F Communications, Radar and Signal Processing 135 (5): 408. https://doi.org/10.1049/ip-f-1.1988.0048
• Reinhard, David, Jean Vergnolle, David Reinhard, and Jean Vergnolle. 1997. “Atmospheric Re-Entry Demonstrator (ARD): Its Parachute Recovery Assembly.” In 14th Aerodynamic Decelerator Systems Technology Conference. AIAA 1997-1438. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1438
• Reis, Ronaldo C., Lucas d. Silva, Cristiane M. Pagliuco, Daniel S. Almeida, and Daniel Bourdon. 2019. “Design and Testing of Centrifugal Fuel Pump for Liquid Propellant Rocket Engine L75.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-4432. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-4432
• Reising, John. 2005. Uninhabited Systems and Operator Control. Defense Technical Information Center. https://doi.org/10.21236/ada444046
• Reisner, Daniel, and Tal Shima. 2011. “Optimal Guidance-to-Collision for an Accelerating Exo-Atmospheric Interceptor Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6567. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6567
• Ren, Gaofeng, Chunxiao Feng, Jinyu Dong, Yitao Qiao, and Xucheng Chang. 2026. “Velocity Consistency Based Multi-Missile Cooperative State Estimation of a Maneuvering Target against Velocity Gate Pull-Off Jamming.” Preprint, . https://doi.org/10.2139/ssrn.7238583
• Ren, Yongjie, KangKang Guo, Songjiang Feng, Yiheng Tong, Wei Lin, and Wansheng Nie. 2023. “Experimental and Numerical Investigation of Transverse Combustion Instability in 2d Multi-Injector Rocket Combustor.” Preprint, . https://doi.org/10.2139/ssrn.4435489
• Ren, Leliang, Yong Xian, Zhenyu Liu, Daqiao Zhang, and Weilin Guo. 2024a. “Deep Reinforcement Learning Compensation Guidance Law for Intercepting Maneuvering Targets Using Only Line-of-Sight Rate Measurement.” Preprint, . https://doi.org/10.2139/ssrn.4783502
• “Research on Anti-Jamming Transmission Mechanism and Intelligent Modulation Recognition Algorithm of Data Link for Complex Battlefield Environment.” 2025. Advances in Computer, Signals and Systems 9 (3). https://doi.org/10.23977/acss.2025.090306
• “Research on Target Tracking Technologies to a Guidance Radar of Anti-Missile Weapon System.” 2013. In Information Technology and Computer Application Engineering. CRC Press. https://doi.org/10.1201/b15936-90
• “Research on the Integrated Design of Missile Guidance Control Considering the Angle of Attack Constraint.” 2023. Academic Journal of Engineering and Technology Science 6 (2). https://doi.org/10.25236/ajets.2023.060202
• “Review of Experimental Research on Combustion Instability of Solid Propellants.” 1960. In Solid Propellant Rocket Research. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600864766.0561.0602
• “Review on Effectiveness Evaluation of Missile Weapon System.” 2021. International Journal of Frontiers in Engineering Technology 3 (9). https://doi.org/10.25236/ijfet.2021.030905
• Rezaee, Alireza. 2026. “Fuzzy Proportional Navigation Guidance for a Complete 3-DOF Model.” Preprint, . https://doi.org/10.20944/preprints202608.1127.v1
• Rezaei, Habib, Mohammad Ali Sebt, Nadali Zarei, and Goudarz Saadati Moghadam. 2023. “Closed-Form Angle Estimation of Unresolved Targets in Monopulse Radar to Counter the Angular Electronic Attack.” IET Signal Processing 17 (4): e12203. https://doi.org/10.1049/sil2.12203
• Rezende, Rene N. 2021. “The Literature behind a Liquid Rocket Engine Design Methodology.” In AIAA Propulsion and Energy 2021 Forum. AIAA 2021-3358. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-3358
• Ribner, Herbert S. 1951. Damping in Roll of Cruciform and Some Related Delta Wings at Supersonic Speeds. NACA-TN-2285. NASA. https://ntrs.nasa.gov/citations/19930082942
• Rice, Michael. 1999. A Comprehensive Investigation of Advanced Range Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ada389435
• Rice, Michael. 2013. The Challenges of C-Band Missile Telemetry. Defense Technical Information Center. https://doi.org/10.21236/ada578383
• Rice, Eric E., Edward Bangsund, Martin J. Chiaverini, and Daniel J. Gramer. 1998. ORBITEC Advanced Cryogenic Solid Hybrid Rocket Engine and Propellant Developments: A 1998 Status Report. Defense Technical Information Center. https://doi.org/10.21236/ada409805
• Rice, Tina, Gary Flandro, and Paul Gloyer. 2010. “Effects of Unsteady Heat Release on Liquid Rocket Combustion Instability.” In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2010-7153. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7153
• 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
• Ridgely, D., Yung Lee, and Todd Fanciullo. 2006. “Dual Aero/Propulsive Missile Control: Optimal Control and Control Allocation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6570
• Riggins, David, H. Nelson, and Eric Johnson. 1998. “Blunt Body Wave Drag Reduction Using Focused Energy Deposition.” In 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 1998-1647. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-1647
• Riley, Christopher, and Fred Dejarnette. 1992. “An Engineering Aerodynamic Heating Method for Hypersonic Flow.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-499. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-499
• Rinat, Keren, and Joseph Ben-Asher. 1999. “Determination of Time-to-Go Distributions with Maximal Average Miss Distances.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1999-4142. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4142
• Ringas, Nicolas. 2022. “Propellant Feed Assembly Design for a Pressure-Fed 1 kN Liquid Propellant Rocket Engine Test Platform.” In Southern Space Studies. Springer International Publishing. https://doi.org/10.1007/978-3-030-89887-8_2
• Riou, Jacques, Eric Garnier, and Claude Basdevant. 2009. “Dynamic Control of the Separated Flow over a Stalled Missile Fin.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3623. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3623
• rish.M, Ha, Keerthi Varman.N, Muthu Kumar R, Ka vin R, and Renu ga.R. 2018. “Numerical Investigation of Flow over a Canard Controlled Missile Configuration in Subsonic and Transonic Flow Regimes.” International Journal of Mechanical Engineering 5 (10): 5–9. https://doi.org/10.14445/23488360/ijme-v5i10p102
• 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
• Rizk, Magdi, Steven Ellison, and Nathan Prewitt. 2002. “Beggar: A Store Separation Predictive Tool.” In 32nd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2002-3190. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3190
• 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
• Robbins, William H., Daniel Bachkin, and Arthur A. Medeiros. 1960. An Analysis of Nuclear-Rocket Nozzle Cooling. NASA-TN-D-482. NASA. https://ntrs.nasa.gov/citations/19980227310
• Roberts, Quentin W. 2023. “Investigation of Pre-Ignition Propellant Mixing in Rotating Detonation Rocket Engine.” In 2023 Regional Student Conferences. AIAA 2023-71901. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-71901
• Roberts, David P., and Valerie J. Gawron. 1986. “Operator/Manager Classification as a Precursor to Function Allocation.” Proceedings of the Human Factors Society Annual Meeting 30 (9): 857–60. https://doi.org/10.1177/154193128603000901
• Robillard, P. E., and W. E. Blore. 1964. CW Radar for Measuring Head-on Radar Cross Section of Free-Flight Projectiles. 1. Antenna for Simultaneous 35 and 70GC Operation. Defense Technical Information Center. https://doi.org/10.21236/ad0444070
• Robins, A. Warner. 1953. Preliminary Investigation of the Effects of Several Seeker-Nose Configurations on the Longitudinal Characteristics of a Canard-Type Missile at a Mach Number of 1.60. NACA-RM-L53I18. NASA. https://ntrs.nasa.gov/citations/19930087897
• 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, M. 1970. “The Estimation of Pitch Damping Derivatives of Missile Configurations at Subsonic Speeds.” In Propulsion and ASW Meeting. AIAA 1970-537. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-537
• Robison, Delbert E. 1953. Experimental Rocket Motor Performance with White Fuming Nitric Acid and JP-4 at 1000 PSIA Combustion Pressure. Defense Technical Information Center. https://doi.org/10.21236/ad0013096
• “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
• Rochowicz, Robert. 2021. “The First Polish Antitank Guided Missile.” Problemy Techniki Uzbrojenia 157 (2): 81–98. https://doi.org/10.5604/01.3001.0015.5048
• Rocker, Marvin. 1999. Simulation of Non-Acoustic Combustion Instability in a Hybrid Rocket Motor. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/19990064113
• “Rocket Engine Nozzle Concepts.” 2004. In Liquid Rocket Thrust Chambers. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866760.0437.0467
• Rocketdyne Canoga Park Ca. 1961. Research on the Hazard Classification of New Liquid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0257300
• Rodi, Patrick E. 2020. “Combined Capsule/Waverider Configurations for Boost Glide Missions.” In 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2020-2423. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2423
• Rodi, Patrick E. 2021. “Effects of Viscosity on Capsule/Waverider Shape Optimization for Boost-Glide Missions.” In AIAA Aviation 2021 Forum. AIAA 2021-2542. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-2542
• Rodi, Patrick E. 2022. “Effects of Finite Radius Leading Edges on the Performance of Capsule/Waveriders for Boost-Glide Missions.” In AIAA AVIATION 2022 Forum. AIAA 2022-4050. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-4050
• Rodriguez, Armando A. 1999. Missile Guidance. Wiley. https://doi.org/10.1002/047134608x.w1122
• 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
• Roelke, Evan, Justin S. Green, and Soumyo Dutta. 2025. “Advanced Supersonic Parachute Inflation Research Experiment-2 (ASPIRE2) Parachute Modeling and Flight Mechanics Performance.” In AIAA SCITECH 2025 Forum. AIAA 2025-2422. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-2422
• 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
• Rojas-Ramirez, Belem Isabel. n.d. “Modeling and Control of Aerial Vehicles Using Teleoperation with Input Delay.” PhD diss., Compiègne. https://doi.org/10.70675/a88f8992z0e02z40cezb5abzb31535a2fffd
• Rokita, Tomer, Rimon Arieli, and Yuval Levy. 2012. “Different Approaches for Simulating the Flow inside and near a Weapons Bay.” In 30th AIAA Applied Aerodynamics Conference. AIAA 2012-3339. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3339
• Roland, Jorden, David Edwards, and Adam Harris. 2016. “Electronic Nose Cone Separation Ring (eNSR) for Deployment of Rocket Recovery Parachute.” In AIAA Space 2016. AIAA 2016-5364. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-5364
• Rollstin, L. 1986. “A Rocket System for Development Testing of a Retardation Parachute for a Supersonic Store.” In 7th Conference on Sounding Rockets, Balloons and Related Space Systems. AIAA 1986-2558. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2558
• 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
• Romero, James. 2015. Joint Air-to-Ground Missile (JAGM). Defense Technical Information Center. https://doi.org/10.21236/ad1019455
• Rose, Robert K. 1958. Experimental Determination of the Heat Flux Distribution in a Rocket Nozzle. Defense Technical Information Center. https://doi.org/10.21236/ad0218493
• Rose, R. E., L. G. Summers, and E. P. Todosiev. 1966. Human Performance in Single-Axis and Two-Axis Tracking Systems. NASA. https://ntrs.nasa.gov/citations/19670006533
• Rose, R. E., L. G. Summers, and E. P. Todosiev. 1967. Human Performance in Single and Two-Axis Tracking Systems. NASA. https://ntrs.nasa.gov/citations/19670054449
• 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
• Rosema, Christopher, and Joshua Doyle. 2011. “Fin-Shed Vortex Modeling within Missile Datcom.” In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2011-1240. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-1240
• Rosema, Christopher, Joshua Doyle, and William B. Blake. 2014. MISSILE DATA COMPENDIUM (DATCOM) User Manual 2014 Revision. Defense Technical Information Center. https://doi.org/10.21236/ad1000581
• Rosema, Christopher, Josh Doyle, Brett Wilks, and Lamar Auman. 2009. “Improvements in Fin-Shed Vortex Treatment for Missile Datcom.” In 27th AIAA Applied Aerodynamics Conference. AIAA 2009-3853. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-3853
• Rosema, Christopher, Mark Underwood, and Lamar Auman. 2007. “Recent Fin Related Improvements for Missile DATCOM.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-3937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3937
• Rosner, D., and R. Cibrian. 1974. “Non-Equilibrium Stagnation Region Aerodynamic Heating of Hypersonic Glide Vehicles.” In Thermophysics and Heat Transfer Conference. AIAA 1974-755. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-755
• Roth, Bryce, and Dimitri Mavris. 1999. Evaluation and Selection of Technology Concepts for a Hypersonic High Speed Standoff Missile. Defense Technical Information Center. https://doi.org/10.21236/ada396843
• Rousar, D. C. 1971. Heat Pipe Technology for Advanced Rocket Thrust Chambers. NASA-CR-123117. NASA. https://ntrs.nasa.gov/citations/19710029269
• Rovner, Daniel M. 1991. “GN&C for Pegasus® Air-Launched Space Booster: Design and First Flight Results.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/911105
• 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
• Rubesin, Morris W., Randall C. Maydew, and Steven A. Varga. 1951. An Analytical and Experimental Investigation of the Skin Friction of the Turbulent Boundary Layer on a Flat Plate at Supersonic Speeds. NACA-TN-2305. NASA. https://ntrs.nasa.gov/citations/19930082975
• Ruhlin, Charles L., and W. J. Tuovila. 1961. Transonic and Supersonic Flutter Investigation of 1/2-Size Models of All-Movable Canard Surface of an Expendable Powered Target. NASA-TM-SX-616. NASA. https://ntrs.nasa.gov/citations/19980227183
• 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
• Ruscio, Daniele, Adrien Metge, Marvin Schopp, Daniel Dreyer, and Benedikt Petermeier. 2024. “The General Automation Level Allocation (GALA) Framework, Or: Why Do We Need Another Level of Automation Framework?” AHFE international. https://doi.org/10.54941/ahfe1005372
• Rush, Ray. 1973. Missile, Guided, Antitank. Defense Technical Information Center. https://doi.org/10.21236/ad0757809
• Rusnak, Ilan. 1993. “Guidance Law Based on an Exponential Criterion for Acceleration Constrained Missile and a Maneuvering Target.” In Guidance, Navigation and Control Conference. AIAA 1993-3782. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3782
• Rusnak, Ilan. 2010c. “Guidance Laws in Defense against Missile Attack with Acceleration Constrained Players.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-8057. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8057
• Russell, Philip W. 1962. “Estimates of the Kill Probability in Target Area Family Shelters.” JAMA 180 (1): 25. https://doi.org/10.1001/jama.1962.03050140027006
• 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
• Ruth, Michael. 1990. “Robust Control of a Bank-to-Turn Missile.” In Guidance, Navigation and Control Conference. AIAA 1990-3341. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3341
• Ruth, E., H. Ahn, R. Baker, and M. Brosmer. 1990. “Advanced Liquid Rocket Engine Transient Model.” In 26th Joint Propulsion Conference. AIAA 1990-2299. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-2299
• Ruther, Philippe, Michael Strohal, and Peter Stütz. 2022. “Conceptual Approach for Optimizing Air-to-Air Missile Guidance to Enable Valid Decision-Making.” In International Conference on Simulation and Modeling Methodologies, Technologies and Applications. https://doi.org/10.5220/0011302800003274
• Ryan, James. 1966. “Aerodynamic Deceleration from as High as Mach 4.0 for the Alarr (Air Launched Air Recoverable Rocket) Project.” In Aerodynamic Deceleration Systems Conference. AIAA 1966-1520. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1966-1520
• Ryu, Chul-Sung. 2009. “Formability Evaluation of a Copper Alloy for Regenerative Cooling Thrust Chamber.” Journal of the Korean Society for Aeronautical & Space Sciences 37 (9): 939–45. https://doi.org/10.5139/jksas.2009.37.9.939
• Ryu, Chul-Sung, Hwan-Seok Choi, and Dong-Ju Lee. 2005. “Structure Design of Regenerative Cooling Chamber of Liquid Rocket Thrust Chamber.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (12): 109–16. https://doi.org/10.5139/jksas.2005.33.12.109
• Saboktakin, Abbasali, and Mohammad Monjezi. 2024. “Reusable and Low Cost Space Rocket Engine with High Efficient Propellant Pump.” Aerospace Research in Bulgaria 36: 157–68. https://doi.org/10.3897/arb.v36.e14
• Sackheim, Robert L., John J. Hutt, William E. Anderson, and Gordon A. Dressler. 2005. Axisymmetric, Throttleable Non-Gimballed Rocket Engine. Patent Number: NASA-Case-MSF-31689. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20060009006
• Sadat Hosseini, Seyed M. R., Farid Amoozegar, and Ali Notash. 1995. “Noise Effect on the Miss Distance of a Closed-Loop Neural-Network-Based Radar Homing Missile for a Tail-Chase Engagement.” In SPIE Proceedings, vol. 2466, edited by Walter J. Fowski, Morris M. Birnbaum. SPIE. https://doi.org/10.1117/12.211504
• 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
• Sahbon, Nezar, Maciej Michałów, Siddharth Murpani, Paulina Żurawka, and Kacper Kaczmarek. 2023. “CFD Study of Base Drag of the Grot Rocket.” Transactions on Aerospace Research 2023 (2): 1–16. https://doi.org/10.2478/tar-2023-0007
• Sahingil, Mehmet C. 2019. “Optimization of the Jamming Signal Parameters for Conical-Scan Systems.” In Pattern Recognition and Tracking XXX, edited by Mohammad S. Alam. SPIE. https://doi.org/10.1117/12.2522497
• 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. 1986. Drag Predictions for Projectiles at Transonic and Supersonic Speeds. Defense Technical Information Center. https://doi.org/10.21236/ada171462
• 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
• Sahu, Jubaraj, Karen Heavey, and Surya Dinavahi. 2000. “Application of CFD to High Angle of Attack Missile Flowfields.” In 18th Applied Aerodynamics Conference. AIAA 2000-4210. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4210
• Sailaranta, Timo, Ari Siltavuori, and Antti Pankkonen. 2011. “Simple Missile Models against High-g Barrel Roll Maneuver.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6570
• Sainio, W. C., and B. A. Krandel. 1993. “YF-23 Leading Edge Flap and Weapons Bay Door Hydromechanical Drive Systems.” In Aerospace Design Conference. AIAA 1993-1162. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1162
• Sakarya, Doğan Uğur. 2017. “Four and Eight Faceted Domes Effects on Drag Force and Image in Missile Application.” In Optifab 2017, edited by Julie L. Bentley, Sebastian Stoebenau. SPIE. https://doi.org/10.1117/12.2282368
• Sakarya, Dogan Ugur, and Alican Bayram. 2019. “Compact Seeker Design by Using Piezo Actuator in Missile Application.” In Physics and Simulation of Optoelectronic Devices XXVII, edited by Marek Osiński, Yasuhiko Arakawa, Bernd Witzigmann. SPIE. https://doi.org/10.1117/12.2510335
• Sakarya, Dogan Ugur, and Hüseyin Sari. 2019. “Stabilization Effects on Seeker Performance in Missile Applications.” In Optomechanical Engineering 2019, edited by Keith B. Doyle, Jonathan D. Ellis. SPIE. https://doi.org/10.1117/12.2534752
• Salazar, J., and P. Kintner. 1981. “Air Force Western Space and Missile Center Data Processing Modernization for the 1980’s.” In 1st Flight Test Conference. AIAA 1981-2391. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2391
• Salcudean, Septimiu E. n.d. “Control for Teleoperation and Haptic Interfaces.” In Lecture Notes in Control and Information Sciences. Springer-Verlag. https://doi.org/10.1007/bfb0015076
• Sale, D. H. 1964. Elastomeric Insulation for Solid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0609001
• Salih, Adham, and Amiram Moshaiov. 2023. “Neuro-Evolution-Based Generic Missile Guidance Law for Many-Scenarios.” Preprint, . https://doi.org/10.2139/ssrn.4333419
• Saliy, Oleksandr, Vladyslav Hol, Andrii Divitskyi, and Oleksiy Khakhlyuk. 2023. “A Complete Solution for Anti-Jaming Radio Data-Link of an Unmanned Aerial Vehicle.” Collection “Information Technology and Security” 11 (2): 251–65. https://doi.org/10.20535/2411-1031.2023.11.2.293939
• Salt, David J. 2014. “Could a Subsonic Air-Launched RLV Enable a Paradigm Shift in Space Operations?” In SpaceOps 2014 Conference. AIAA 2014-1897. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1897
• Salt, David J. 2015. “Could a Subsonic Air-Launched Reusable Launch Vehicle (RLV) Enable a Paradigm Shift in Space Operations?” In Space Operations: Innovations, Inventions, and Discoveries. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/5.9781624101991.0185.0218
• Sambamurthi, Jay, John Warmbrod, and Mark Seaford. 1989. “Engineering Methodology to Estimate the Aerodynamic Heating to the Base of the Aeroassist Flight Experiment Vehicle.” In 24th Thermophysics Conference. AIAA 1989-1732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-1732
• Sandia Corp., Albuquerque, N. Mex. 1953. Approximations to the Circular Normal Distribution. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4360350
• Sankar, Vigneshwaran, A. Aravind, D. Giridharan, Pavithra Murugesh, and Vr Sanal Kumar. 2017. “Wall Heat Flux Mapping of Liquid Rocket Thrust Chamber with Dual Impinging GH2/GO2 Jets.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-4766. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4766
• Sankar, Ram B., Ajit B. Chaudhary, and Anil Kumar. 2013. “Euler Angle Error Computation and Thrust Vector Control Scheme for Initial Turning Phase of a Vertical Launch Surface to Air Missile.” International Journal of Applied Research in Mechanical Engineering: 269–73. https://doi.org/10.47893/ijarme.2013.1098
• Santhini S Lal, A. K. Asraff, and Shobha Elizebath Thomas. 2015. “Thermostructural Analysis of Rocket Engine Thrust Chamber.” International Journal of Engineering Research and V4 (08). https://doi.org/10.17577/ijertv4is080439
• Santhosh, Thomas, and Biju T. Kuzhiveli. 2019. “Heat Transfer Aspects and Analysis of Regenerative Cooling in Semi-Cryogenic Thrust Chamber with Fixed and Variable Aspect Ratio Coolant Channels.” IOP Conference Series: Materials Science and Engineering 502: 012066. https://doi.org/10.1088/1757-899x/502/1/012066
• Santiago, Jorge. 1996. “Evolution of the RL10 Liquid Rocket Engine for a New Upperstage Application.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-3013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3013
• Santos, Jhonatan Ribeiro dos, and Eduardo Seiji Suguimoto Miyazato Ferrer. 2024. “Simulation of a Liquid Propellant Rocket Engine Manufacturing Assembly Line Utilizing the PFS/PN Methodology.” Mecatrone 6 (1): 1–18. https://doi.org/10.11606/issn.2526-8260.mecatrone.2023.221035
• Santos, Wilson, and Mark Lewis. 2003. “Aerodynamic Heating Performance of Power Law Leading Edges in Rarefied Hypersonic Flow.” In 36th AIAA Thermophysics Conference. AIAA 2003-3894. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3894
• 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
• Sarigul-Klijn, Marti, Nesrin Sarigul-Klijn, Gary Hudson, Bevin McKinney, Lyle Menzel, and Eric Grabow. 2005. “Trade Studies for Air Launching a Small Launch Vehicle from a Cargo Aircraft.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-621. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-621
• Sarigulklijn, Martinus, Nesrin Sarigul-Klijn, Gary Hudson, and Carlie Brown. 2012. “A New Air Launch Concept: Vertical Air Launch Sled (VALS).” In AIAA SPACE 2012 Conference & Exposition. AIAA 2012-5156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5156
• Sarma, I., and K. Swamy. 1989. “MAMS: An Approach to Optimal Terminal Homing Guidance for Aerial Engagements.” In Guidance, Navigation and Control Conference. AIAA 1989-3588. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3588
• Sarotte, Camille. n.d. “Improvement of Monitoring and Reconfiguration Processes for Liquid Propellant Rocket Engine.” PhD diss., Université Paris-Saclay (ComUE). https://doi.org/10.70675/7e4e5805z21f6z4e0bz8874z44abf9aa6d38
• Sarwar, Gulam, Lavala Srinivasa Rao, Syed Shoaib Mohd, and Saista Tabssum. 2024. “A Study of Different Techniques for Reducing Drag and Heating Problems on a Blunt Body at Supersonic and Hypersonic Speed.” In Advances in Aerospace Technologies. River Publishers. https://doi.org/10.1201/9788770046299-5
• Sasoh, Akihiro, Takeharu Sakai, Yohei Sekiya, Atsushi Matsuda, and Jae Hyung Kim. 2009b. “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, Yohei Sekiya, Takeharu Sakai, Jae Hyung Kim, and Atsushi Matsuda. 2009a. “Drag Reduction of Blunt Body in a Supersonic Flow with Laser Energy Depositions.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-1533. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-1533
• 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
• 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
• Savage, P. 1969. “A Strapdown Phased Array Radar Tracker Loop Concept for a Radar Homing Missile.” In AIAA Guidance, Control, and Flight Mechanics Conference. AIAA 1969-873. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1969-873
• Savery, Ryan, and James G. Coder. 2024. “The Computational Analysis of a Generic Hypersonic Store Separation.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4150. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4150
• Savvas Sadiq Ali, Farhad Nawaz, Pranav Tekade, and Ashwini Ratnoo. 2020. “On Obstacle Avoidance Characteristics of Proportional Navigation Guidance.” In AIAA Scitech 2020 Forum. AIAA 2020-1093. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1093
• Sawyer, J. W. 1977. Pressure and Heating-Rate Distributions on a Corrugated Surface in a Supersonic Turbulent Boundary Layer. NASA-TP-1024. NASA. https://ntrs.nasa.gov/citations/19840002436
• Sawyer, W. C., and C. Hayes. 1976. Stability and Control Characteristics of an Air-Breathing Missile Configuration Having a Forward Located Inlet. NASA-TM-X-3391. NASA. https://ntrs.nasa.gov/citations/19760022078
• Sawyer, W. C., and C. M. Jackson Jr. 1982. “An Overview of NASA’s Role in Maneuvering Missile Aerodynamic Technology.” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19820038540
• Sawyer, Wallace C., Robert L. Stallings Jr., Floyd J. Wilcox Jr., A. B. Blair Jr., William J. Monta, and Elizabeth B. Plentovich. 1989. “New Test Techniques to Evaluate near Field Effects for Supersonic Store Carriage and Separation.” In AGARD, Stability and Control of Tactical Missile Systems. https://ntrs.nasa.gov/citations/19900000746
• Scala, Sinclaire M. 1957. Transverse Wave and Entropy Wave Combustion Instability in Liquid Propellant Rockets. Defense Technical Information Center. https://doi.org/10.21236/ad0130408
• 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
• Schade, N. 2013. “Simulation of Store Separation Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations.” In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-35680-3_3
• Schadt, G. 1968. “Aerodynamic Heating Problems and Their Influence on Earth Orbit Lifting Entry Spacecraft.” In 5th Annual Meeting and Technical Display. AIAA 1968-1126. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-1126
• Schappell, R. T., and R. L. Knickerbocker. 1975. “Experimental and Simulation Study Results of an Adaptive Video Guidance System (AVGS).” In American Institute of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/19750057587
• Scherrer, Richard, and David H. Dennis. 1951. Damping in a Roll of a Missile Configuration with a Modified Triangular Wing and a Cruciform Tail at a Mach Number of 1.52. NACA-RM-A51A03. NASA. https://ntrs.nasa.gov/citations/19930086518
• Schick, Michael O. 1977. Missile Vulnerability (MV) Code Simplification. Defense Technical Information Center. https://doi.org/10.21236/ada035318
• Schindel, Leon, and Lisa Lam. 1995. “Payoffs of Improved Missile Control Effectiveness.” In 13th Applied Aerodynamics Conference. AIAA 1995-1898. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1898
• Schipani, Salvatore P., and Elena R. Messina. 2007. Maze Hypothesis Development in Assessing Robot Performance during Teleoperation. National Institute of Standards and Technology. https://doi.org/10.6028/nist.ir.7443
• Schleich, W. 1982. “Shuttle Vehicle Configuration Impact on Ascent Guidance and Control.” In Guidance and Control Conference. AIAA 1982-1552. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1552
• Schmidt, Bryan E., Neal Bitter, Hans Hornung, and Joseph Shepherd. 2014. “Experimental Investigation of Gas Injection into the Boundary Layer on a Slender Body in Supersonic Flow.” In 7th AIAA Theoretical Fluid Mechanics Conference. AIAA 2014-2496. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-2496
• Schmit, Ryan F., and Ganesh Raman. 2006. “High and Low Frequency Actuation Comparison for a Weapons Bay Cavity.” International Journal of Aeroacoustics 5 (4): 395–414. https://doi.org/10.1260/147547206779379903
• Schmit, Ryan, David Schwartz, Valdis Kibens, Ganesh Raman, and John Ross. 2005. “High and Low Frequency Actuation Comparison for a Weapons Bay Cavity.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-795. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-795
• Schmitt, Harry A. 2001. Advanced Mathematics for Optimizing Missile Seeker Signal Processing. Defense Technical Information Center. https://doi.org/10.21236/ada398610
• Schmitt, Harry A. 2004. Integrated Sensing and Processing in Missile Systems. Defense Technical Information Center. https://doi.org/10.21236/ada429425
• Schmitt, D. J., J. L. Novak, and G. P. Starr. 1994. “Real-Time Seam Tracking for Rocket Thrust Chamber Manufacturing.” In Proceedings of the 1994 IEEE International Conference on Robotics and Automation. IEEE Comput. Soc. Press. https://doi.org/10.1109/robot.1994.350949
• Schoeler, H. 1987. Kinetic Energy Finned Projectile Aerodynamic Heating Measurements. Defense Technical Information Center. https://doi.org/10.21236/ada195832
• Scholcover, Federico, and Douglas J. Gillan. 2017. “Using Temporal Sensitivity to Predict Performance under Latency in Teleoperation.” Human Factors: The Journal of the Human Factors and Ergonomics Society 60 (1): 80–91. https://doi.org/10.1177/0018720817734727
• Schroeder, Jeffery. 1993. “Simulation Motion Effect on Single Axis Compensatory Tracking.” In Flight Simulation and Technologies. AIAA 1993-3579. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3579
• 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
• Schutte, Paul C. 2000. “Distance: A Metric for Flight Deck Design and Function Allocation.” Proceedings of the Human Factors and Ergonomics Society Annual Meeting 44 (1): 85–88. https://doi.org/10.1177/154193120004400123
• Schwab, Harry. 1999. “Vibration Testing a Large Guided Missile on Air-Spring Supports.” Journal of the IEST 42 (4): 35–40. https://doi.org/10.17764/jiet.42.4.p56174w22v3rnu15
• Schwarz, Klaus-Peter. 1981. Gravity Induced Position Errors in Airborne Inertial Navigation,. Defense Technical Information Center. https://doi.org/10.21236/ada113823
• Schwind, R. G. 1978. High Angle Canard Missile Test in the Ames 11-Foot Transonic Wind Tunnel. NASA-CR-2993. NASA. https://ntrs.nasa.gov/citations/19780017114
• 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, G. W. 1966. Digital Hydraulic Actuator Study. Defense Technical Information Center. https://doi.org/10.21236/ad0647709
• 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
• Scott, C., L. Murray, and J. Milhoan. 1977. “Shuttle Elevon Cove Aerodynamic Heating by Internal Flow.” In 12th Thermophysics Conference. AIAA 1977-757. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1977-757
• 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
• Seader, J. D., and W. R. Wagner. 1964. Regenerative Cooling of Rocket Engines. University of Utah. https://ntrs.nasa.gov/citations/19650032919
• Sebastia, Carlos, and Mirko Hornung. 2023. “Numerical Analysis of Aerodynamic Flap Hinge Moment under Unsteady Flow Conditions Considering Laminar-Turbulent Transition.” In AIAA AVIATION 2023 Forum. AIAA 2023-3528. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-3528
• Sebastia, Carlos, Werner Würz, Ulrich Deck, and Mirko Hornung. 2024. “Experimental and Numerical Analysis of Aerodynamic Flap Hinge Moment under Unsteady Flow Conditions on a NLF Airfoil.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-3997. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-3997
• Seidel, Hans H. 1965. Transient Chamber Pressure and Thrust in Solid Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ad0613962
• Seidel, A. 1974. “A Completely Electroformed Lightweight Regenerative Thrust Chamber for Cryogenic Rocket Engines.” In 10th Propulsion Conference. AIAA 1974-1183. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-1183
• Seiner, John, Bernard Jansen, and Nathan Murray. 2008. “Weapons Bay Acoustic Suppression at Mach 2.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-60. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-60
• Seiner, John, Bernard Jansen, Michael Ponton, Christopher Bruner, and Jere Singleton. 2000. “Acoustics Associated with Fluid/structural Coupling for Interceptor Missile Flow Fields.” In 6th Aeroacoustics Conference and Exhibit. AIAA 2000-2035. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-2035
• Seiple, E. L. 1960. Production Engineering Test of Guided Missile XM5E3 Warhead. Defense Technical Information Center. https://doi.org/10.21236/ad0315737
• 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
• Sells, Ray. 1992. “Derivation of an Universal Guidance Performance Relationship for a Homing Missile.” In 30th Aerospace Sciences Meeting and Exhibit. AIAA 1992-208. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1992-208
• Semenov, Aleksandr N., Vladimir I. Krainy, and Ivan A. Rodichev. 2019. “Monopulse Angle Estimation with MIMO Radar.” ITM Web of Conferences 30: 15018. https://doi.org/10.1051/itmconf/20193015018
• Senchev, Maxim, Ivan Zubrilin, Artem Yurtaev, and Yuliya Komisar. 2022. “Analysis of the Kerosene Combustion Simulation for a Liquid-Propellant Rocket Engine.” Thermal processes in engineering 14 (1): 42–48. https://doi.org/10.34759/tpt-2022-14-1-42-48
• Seo, Miran, Yeon Chae, and Youngjib Ham. 2024. “Exploring Latency during Long-Distance Robot-Assisted Teleoperation and Construction.” In Computing in Civil Engineering 2023. American Society of Civil Engineers. https://doi.org/10.1061/9780784485224.094
• Seo, Kyugnwon, Do-Kwan Lee, Sung-Cheol Kim, Eunhye Choi, Sanghyun Han, and Jong-Geon Lee. 2023. “Development of the Store Separation Test Equipment and Grid Test in the Transonic Wind Tunnel.” Journal of the Korean Society for Aeronautical & Space Sciences 51 (10): 669–75. https://doi.org/10.5139/jksas.2023.51.10.669
• Seshime, Takahiro, Takanori Haga, Hiroshi Gotoda, Yusuke Nabae, and Ryoichi Kurose. 2026. “Spatiotemporal Dynamics of High-Frequency Combustion Instability in a Single-Element Liquid Rocket Engine Combustor.” Journal of the Acoustical Society of America 159 (4_Supplement): A315-A315. https://doi.org/10.1121/10.0045842
• 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
• Settles, G. S. 1986. Recent Skin Friction Techniques for Compressible Flows. AIAA PAPER 86-1099. Pennsylvania State University. https://ntrs.nasa.gov/citations/19860053722
• Sevier, John R., Jr., Clyde V. Hamilton, and Cornelius Driver. 1953. Wind-Tunnel Investigation of a Ram-Jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges: Force and Moment Characteristics of Various Combinations of Components at a Mach Number of 1.6. NACA-RM-L53A14. NASA. https://ntrs.nasa.gov/citations/19930087490
• Sforza, Pasquale M. 2017. “Liquid Propellant Rocket Motors.” In Theory of Aerospace Propulsion. Elsevier. https://doi.org/10.1016/b978-0-12-809326-9.00011-7
• Sforza, Pasquale M. 2020. “Bluntness Effects on the Lift to Drag Ratio of Slender Bodies in Hypersonic Flight.” In AIAA Scitech 2020 Forum. AIAA 2020-0281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0281
• Shadram, Zeinab, Tuan M. Nguyen, Athanasios Sideris, and William A. Sirignano. 2019. “Neural Network Closure Models for Estimating Flame Variables in a Liquid-Propellant Rocket Engine.” In AIAA Scitech 2019 Forum. AIAA 2019-2008. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2008
• Shaferman, Vitaly. 2017. “Optimal Guidance with an in Route Look-Angle Constraint.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1507
• 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
• 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
• Shakiba, Mohammad, and Andrea Serrani. 2011. “Control Oriented Modeling of 6-DOF Hypersonic Vehicle Dynamics.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6227. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6227
• Shalaev, Vladimir, Norman Malmuth, and Alexander Fedorov. 2003. “Analytical Modeling of Transonic Store Separation from a Cavity.” In 41st Aerospace Sciences Meeting and Exhibit. AIAA 2003-4. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-4
• Shandling, J., and D. Platus. 1985. “Control of Missile Dispersion via Roll Rate Modulation.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1778. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1778
• Shang She and Xu Yinghe. n.d. “Investigation on Low-Angle Tracking Technique for Tactical Radar.” In Proceedings of International Radar Conference. Publishing House of Electron. Ind. https://doi.org/10.1109/icr.1996.574558
• 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
• Shao, Mao-sen, Cheng Xu, Bin Zhao, and Jun Zhou. 2021. “Integrated Guidance and Control Design Considering Angle of View Constraint of Strap-down Optical Seeker and Input Constraint.” Optics and Precision Engineering 29 (6): 1291–1300. https://doi.org/10.37188/ope.20212906.1291
• 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
• 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
• Shaw, Leonard, Rodney Clark, and Dick Talmadge. 1987. “F-111 Generic Weapons Bay Acoustic Environment.” In 25th AIAA Aerospace Sciences Meeting. AIAA 1987-168. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-168
• Shaw, L. L., and S. McGrath. 1996. “Weapons Bay Acoustics: Passive or Active Control.” In Space Plane and Hypersonic Systems and Technology Conference. AIAA 1996-5000. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-5000
• Shaw, L. L., and D. L. Smith. 1977. Aeroacoustic Environment of a Store in an Aircraft Weapons Bay. Defense Technical Information Center. https://doi.org/10.21236/ada041263
• 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
• Sheiko, Zakhar. 2025. “Analysis and Comparison of Liquid-Propellant Rocket Engines and Solid-Propellant Rocket Motors as Propulsion Systems for Aerial Attack Vehicles Based on the Example of Soviet Air-to-Surface Missiles.” In Human and Space. О.М. Makarov National youth aerospace education center. https://doi.org/10.62717/2221-4550-2025-1-039
• Shekhawat, Kavita, and Nandan Kumar Sinha. 2026. “Bifurcation-Based Analysis of the Longitudinal Flight Dynamics of an Air-Breathing Hypersonic Vehicle.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01263-y
• 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
• Shelley, J. S., R. LeClaire, and J. Nichols. 2001. Metal Matrix Composites for Liquid Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ada410056
• Shen, Shaobo, Aiguo Song, Tao Li, and Huijun Li. 2019. “Time Delay Compensation for Nonlinear Bilateral Teleoperation: A Motion Prediction Approach.” Transactions of the Institute of Measurement and Control 41 (16): 4488–98. https://doi.org/10.1177/0142331219860928
• 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
• Sheng-bing, Shi, Wang Chang-an, and Wang Guang-wei. 2016. “Test Technology Research on Missile Infrared System Range.” DEStech Transactions on Engineering and Technology Research, no. ICMITE2016. https://doi.org/10.12783/dtetr/icmite20162016/4600
• Shepherd, William L. 1963. Derivation of Exact Formulas for Correcting Radar Angle Data for Errors Caused by Nonper Pendicularity of the Radar Axes. Defense Technical Information Center. https://doi.org/10.21236/ad0403489
• 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
• Sheridan, T. B. 1984. “Review of Teleoperator Research.” In NASA. Ames Research Lab 20th Ann. Conf. on Manual Control, Vol. 1. https://ntrs.nasa.gov/citations/19850006202
• Sheta, Essam F., Robert E. Harris, Edward A. Luke, Benjamin George, and Lawrence S. Ukeiley. 2015. “Loads and Acoustics Prediction on Deployed Weapons Bay Doors.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-3018. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3018
• Shewale, Shantanu S., Aniket D. Tompe, Bharat R. Yenurkar, and Shiva U. Prasad. 2022. “Investigation of Canard Missile with Planar and Grid Fins by Using CFD Tool.” Graduate Research in Engineering and Technology: 5–9. https://doi.org/10.47893/gret.2022.1104
• Shi, Heng, Zheng Chen, Jihong Zhu, and Minchi Kuang. 2021b. “Model Predictive Guidance for Active Aircraft Protection from a Homing Missile.” IET Control Theory & Applications 16 (2): 208–18. https://doi.org/10.1049/cth2.12218
• Shi, C. G., F. Wang, S. Salous, and J. J. Zhou. 2019a. “Adaptive Jamming Waveform Design for Distributed Multiple-Radar Architectures Based on Low Probability of Intercept.” Radio Science 54 (1): 72–90. https://doi.org/10.1029/2018rs006668
• Shi, Chenguang, Fei Wang, Mathini Sellathurai, and Jianjiang Zhou. 2019b. “Low Probability of Intercept-Based Distributed MIMO Radar Waveform Design against Barrage Jamming in Signal-Dependent Clutter and Coloured Noise.” IET Signal Processing 13 (4): 415–23. https://doi.org/10.1049/iet-spr.2018.5212
• 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
• Shibata, Naoki, Goro Obinata, and Yasuhiro Kajiwara. 2005. Estimation of Load to Human-Operator by Model-Based Approach~Effect of Visual Distractions. https://doi.org/10.4271/2005-08-0243
• Shih, W. 1976. “Ballistics Range Measurements of Aerodynamic Heating in Erosion Environments.” In 9th Fluid and PlasmaDynamics Conference. AIAA 1976-319. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-319
• 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, Moshe Idan, and Oded Golan. 2004. “Sliding Mode Control for Integrated Missile Autopilot-Guidance.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4884. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4884
• 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
• Shimshi, Jason, and Gerald Walberg. 1993. “An Investigation of Aerodynamic Heating to Spherically Blunted Conesat Angle of Attack.” In 28th Thermophysics Conference. AIAA 1993-2764. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-2764
• Shin, Won-Ho. 2005. “Nonlinear Flutter Analysis of Missile Fin Considering Dynamic Stiffness of Actuator.” Journal of the Korean Society for Aeronautical & Space Sciences 33 (2): 54–59. https://doi.org/10.5139/jksas.2005.33.2.054
• Shin, Hyo-Sang, Jin-Ik Lee, Antonios Tsourdos, and Min-jea Tahk. 2012. “Homing Guidance Law for Reducing Sensitivity on Heading Error.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4473. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4473
• 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
• Shinar, Josef, and Vladimir Turetsky. 2005. “Further Improved Homing Accuracy in Ballistic Missile Defense against Randomly Maneuvering Targets.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6160
• Shinar, Josef, Vladimir Turetsky, and Yaakov Oshman. 2004. “New Logic-Based Estimation/Guidance Algorithm for Improved Homing against Randomly Maneuvering Targets.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4886
• Shinar, J., and P. Zarchan. 1976. “Miss Distance Calculation for Rolling Missiles.” In Guidance and Control Conference. AIAA 1976-1955. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1955
• Shinbrot, Marvin, and Grace C. Carpenter. 1958. An Analysis of the Optimization of a Beam Rider Missile System. NACA-TN-4145. NASA. https://ntrs.nasa.gov/citations/19930085004
• Shinichi, Taguchi, Ohnishi Naofumi, Michiko Furudate, and Sawada Keisuke. 2007. “Numerical Analysis of Drag Reduction for Supersonic Blunt Body by Pulse Energy Deposition.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-1235. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-1235
• 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, Hiroyuki Takano, Takeshi Yamasaki, and Isao Yamaguchi. 2019. “A Study on the Improvement of Modified Proportional Navigation Guidance.” In AIAA Scitech 2019 Forum. AIAA 2019-2346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-2346
• Shiraishi, Yohei, Hiroyuki Takano, Takeshi Yamasaki, and Isao Yamaguchi. 2020. “A Improvement Method of Modified Proportional Navigation under Noise and Time Lag for a Missile Guidance.” In AIAA Scitech 2020 Forum. AIAA 2020-1871. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-1871
• Shirley, R. S. 1978. “Some Modern Control Techniques for Human Operator Modeling and Identification.” In NASA, Washington Fourth Inter-Center Control Systems Conf.. https://ntrs.nasa.gov/citations/19780015079
• 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
• Shkolnikov, I., Y. Shtessel, D. Lianos, and P. Zarchan. 2001. “Simulation Study of the Homing Interceptor Guidance Loop with Sliding Mode Observers versus Kalman Filter.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4216. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4216
• Shneydor, N. A. 1998a. “Guidance Laws Related to Prop. Navigation.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.165
• Shneydor, N. A. 1998b. “Line-of-Sight Guidance.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.11
• Shneydor, N. A. 1998c. “Mechanization of Proportional Navigation.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.129
• Shneydor, N. A. 1998e. “Modern Guidance Laws.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.181
• Shneydor, N. A. 1998f. “Proportional Navigation.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.101
• Shneydor, N. A. 1998g. “Pure Pursuit.” In Missile Guidance and Pursuit. Elsevier. https://doi.org/10.1533/9781782420590.47
• Shnidman, David A. 1975. Evaluation of Probability of Detection for Several Target Fluctuation Models. Defense Technical Information Center. https://doi.org/10.21236/ada013733
• Shoji, J. M. 1981. Low-Thrust Chemical Rocket Engine Study. NASA-CR-165275. NASA. https://ntrs.nasa.gov/citations/19810012596
• 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
• Shoyama, Tadayoshi, and Kazuaki Hirakawa. 2024. Development of Tri-Propellant Rocket Engine for Reusable SSTO. https://doi.org/10.52202/078371-0065
• Shrivastava, Sachin, and P. M. Mohite. 2015. “Redesigning of a Canard Control Surface of an Advanced Fighter Aircraft: Effect on Buckling and Aerodynamic Behavior.” Curved and Layered Structures 2 (1). https://doi.org/10.1515/cls-2015-0010
• 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, 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
• Shuang, Xu. 2024. “Research on Missile Guidance Based on Three-Loop Autopilot Device.” Highlights in Science Engineering and Technology 111: 533–43. https://doi.org/10.54097/arrkn390
• 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
• “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
• Shyu, Lih Shyng, and Yung Chia Hsiao. 2014. “Mini UAV Design and Manufacture with Bungee Launched / Parachute Recovery.” Applied Mechanics and Materials 610: 97–100. https://doi.org/10.4028/www.scientific.net/amm.610.97
• Si, Hai-Qing, and Tong-Guang Wang. 2010. “Numerical Understanding of the Self-Induced Oscillation of Flow past the Open Cavity with a Store.” International Journal of Modern Physics B 24 (27): 5295–5307. https://doi.org/10.1142/s0217979210056839
• Siapkaras, A. 1977. “Multi-Attribute Subjective Evaluations of Manual Tracking Tasks vs. Objective Performance of the Human Operator.” In Proc, 13th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19790009315
• Sibol, Jerome L. 1979. “Super Recording Automatic Digital Optical Tracker (RADOT) Field-Test Results at Kwajalein Missile Range (KMR).” In SPIE Proceedings, vol. 0187, edited by Harold B. Jeffreys. SPIE. https://doi.org/10.1117/12.965578
• Sickles, W., T. Hand, C. Morgret, J. Masters, and A. Denny. 2008. “High-Fidelity, Time-Accurate CFD Store Separation Simulations from a B-1B Bay with Comparisons to Quasi-Steady Engineering Methods.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-186. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-186
• Sickles, William, Greg Power, Joshua Calahan, and A. Denny. 2007. “Application of a CFD Moving-Body System to Multicomponent Store Separation.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-4073. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4073
• Siddarth, Anshu, Florian Peter, Florian Holzapfel, and John Valasek. 2014. “Autopilot for a Nonlinear Non-Minimum Phase Tail-Controlled Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-1293. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1293
• Siebenhaar, Adam, and William Campbell. 1987. “XLR-132A Storable Propellant Rocket Engine Turbopump Development Status.” In 23rd Joint Propulsion Conference. AIAA 1987-2116. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2116
• Siegel, Arthur I., J. J. Wolf, and Kenneth Crain. 1961. Techniques for Evaluating Operator Loading in Man-Machine Systems. a ‘Model’ for Digital Simulation of One and Two-Operator Man-Machine Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0255518
• Sieradzki, Adam. 2016. “Gurney Flap and t-Strip Influence on Stabilizer Aerodynamic Effectiveness and Hinge Moment Characteristics.” Transactions of the Institute of Aviation 245 (4): 199–208. https://doi.org/10.5604/05096669.1226890
• Sierra, Pablo, Juan M. Tizón, Javier Vilas, and José F. Moral. 2017. “Efficient Simulation of Liquid Propellant Rocket Engine Cycle.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-5007. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-5007
• 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
• Silbert, M., A. Moltedo, and E. Bedy Sr. 1986. “Parachute Recovery Location Aids.” In 7th Conference on Sounding Rockets, Balloons and Related Space Systems. AIAA 1986-2545. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2545
• 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
• Silton, Sidra I., and Craig J. Coyle. 2016. “Effect of Canard Deflection for Roll Control on Fin Performance of a Fin-Stabilized Projectile.” In 54th AIAA Aerospace Sciences Meeting. AIAA 2016-0309. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-0309
• Silver, Jordan, Michael J. Brooks, and Glen Snedden. 2024. “Design Simulation of Gas Generator and Electrically Pumped Rocket Engine Cycles under Ablative and Regenerative Cooling.” In AIAA SCITECH 2024 Forum. AIAA 2024-0351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0351
• Silvius, Jack M., and Eugene A. Sherrill. 1978. Digital Electrohydraulic Stepper Actuator for Advanced Missile Systems. Defense Technical Information Center. https://doi.org/10.21236/ada061693
• Simon, James, and William Blake. 1999. “Missile Datcom: High Angle of Attack Capabilities.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4258. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4258
• Sims, L. W. 1963. Analytical and Experimental Investigation of Supersonic Parachute Phenomena. Defense Technical Information Center. https://doi.org/10.21236/ad0334868
• Sims, J. D., Gary A. Flandro, Joseph Majdalani, and Joseph D. Sims. 2004. On Nonlinear Combustion Instability in Liquid Propellant Rocket Motors. AIAA Paper 2004-3516. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20040085915
• Sims, Robert J., and Edward R. Graf. 1969. The Determination of Glint for a Complex Radar Target. Volume 2. Defense Technical Information Center. https://doi.org/10.21236/ad0857647
• 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
• “Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic Propellant Rockets.” 2004a. In Liquid Rocket Thrust Chambers. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866760.0527.0551
• “Simulation and Analysis of Thrust Chamber Flowfields: Storable Propellant Rockets.” 2004b. In Liquid Rocket Thrust Chambers. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866760.0493.0525
• “Simulation of Store Separation Using Low-Cost CFD with Dynamic Meshing.” 2014. International Journal of Engineering 27 (5 (B)). https://doi.org/10.5829/idosi.ije.2014.27.05b.14
• Sinai, Y. L., and J. F. Clarke. 1978. “The Wave System Attached to a Finite Slender Body in a Supersonic Relaxing Gas Stream.” Journal of Fluid Mechanics 84 (4): 717–41. https://doi.org/10.1017/s0022112078000440
• Singelmann, Dietrich, and Heinz Mueller. 1948. BMW Rocket Engine Development. Defense Technical Information Center. https://doi.org/10.21236/ada402594
• Singh, Naunihal. 1962. “Spherical Probable Error.” Nature 193 (4815): 605–605. https://doi.org/10.1038/193605a0
• Singh, Leena. 2004. “Autonomous Missile Avoidance Using Nonlinear Model Predictive Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4910. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4910
• 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, Sanjay, and Ajoy Ghosh. 2006. “Parameter Estimation from Flight Data of a Missile Using Maximum Likelihood and Neural Network Method.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2006-6284. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6284
• Singh, S., and A. K. Ghosh. 2023. “Longitudinal Parameter Estimation Using Wind Tunnel and Simulated Flight Data of Missile Configuration.” Journal of Aerospace Sciences and Technologies: 102–20. https://doi.org/10.61653/joast.v59i2.2007.567
• Singh, Nikhil K., and Sikha Hota. 2021. “Moving Target Interception Guidance Law for Any Impact Angle with Field-of-View Constraint.” In AIAA Scitech 2021 Forum. AIAA 2021-1462. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-1462
• Singh, R. N., and S. S. Negi. 1995. “Target Acquisition System for Antitank Guided Missile Systems.” Defence Science Journal 45 (3): 199–205. https://doi.org/10.14429/dsj.45.4119
• Singh, Nikhil K., Sayantan Pal, Aswin D. Menon, and Sikha Hota. 2026. “Impact Angle Constrained Guidance Laws for Stationary Target Interception in 3D Space.” In AIAA SCITECH 2026 Forum. AIAA 2026-2348. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2348
• Singh, Ritesh, Om Prakash, Sudhir Joshi, and Yogananda Jeppu. 2022. “Bifurcation Analysis of Longitudinal Dynamics of Generic Air-Breathing Hypersonic Vehicle for Different Operating Flight Conditions.” In Springer Proceedings in Complexity. Springer International Publishing. https://doi.org/10.1007/978-3-030-99792-2_97
• Singh, L. P., V. D. Sharma, and R. Ram. 1989. “Radiating Gas Flow past a Slender Body with an Attached Shock Wave.” In Zeitschrift für Angewandte Mathematik und Mechanik Volume 69, Number 9. De Gruyter. https://doi.org/10.1515/9783112570562-005
• Singh, Netra, and Manoranjan Prasad Sinha. 2011. “Suboptimal Guidance and Control Design for a Missile with Onboard Strapdown Seeker.” Applied Mechanics and Materials 110-116: 2513–20. https://doi.org/10.4028/www.scientific.net/amm.110-116.2513
• Sinha, N., S. Arunajatesan, J. Shipman, and J. Seiner. 2001. “High Fidelity Simulation and Measurements of Aircraft Weapons Bay Dynamics.” In 7th AIAA/CEAS Aeroacoustics Conference and Exhibit. AIAA 2001-2125. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2125
• Sinha, N., S. Arunajatesan, and L. Ukeiley. 2000. “High Fidelity Simulation of Weapons Bay Aeroacoustics and Active Flow Control.” In 6th Aeroacoustics Conference and Exhibit. AIAA 2000-1968. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-1968
• Sinha, Aniruddha, and Sparsh Garg. 2018. “Reduced-Order Modeling of Steady Aerodynamics for 2D Store Separation Analysis.” In 2018 Applied Aerodynamics Conference. AIAA 2018-3168. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-3168
• Sinha, Abhinav, and Shashi Ranjan Kumar. 2020. “Super-Twisting Control Based Impact Time Constrained Guidance.” In AIAA Scitech 2020 Forum. AIAA 2020-0610. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-0610
• Sinha, A., R. Kumar, and J. Umakant. 2022. “Reduced-Order Model for Efficient Generation of a Subsonic Missile’s Aerodynamic Database.” Aeronautical Journal 126 (1303): 1546–67. https://doi.org/10.1017/aer.2022.4
• 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
• Sitton, R. L. 1982. “Optical Command and Beamrider Missile Guidance.” In SPIE Proceedings, vol. 0317, edited by Bob D. Guenther, William Pittman. SPIE. https://doi.org/10.1117/12.933136
• Sivasubramanian, Jayahar, Ananth Padmanabha, and Bhoomika Prasad. 2026. “Analysis of Aerodynamic Characteristics for a Missile Geometry in the Supersonic and Hypersonic Flow Regimes.” Advanced International Journal for Research 7 (2): 4955. https://doi.org/10.63363/aijfr.2026.v07i02.4955
• Sivrioglu, Selim, and Sinan Basaran. 2024. “A Vertical Take-off and Landing (VTOL) Unmanned Aircraft Vehicle Trajectory Control Model with Air-Launched Missiles.” Aircraft Engineering and Aerospace Technology 96 (10): 1302–10. https://doi.org/10.1108/aeat-04-2024-0118
• Sixteenth Annual Conference on Manual Control. 1982. NASA-TM-84273. NASA. https://ntrs.nasa.gov/citations/19820026161
• 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
• 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
• Sklar, Aaron E., and Nadine B. Sarter. 1999. “Good Vibrations: Tactile Feedback in Support of Attention Allocation and Human-Automation Coordination in Event-Driven Domains.” Human Factors: The Journal of the Human Factors and Ergonomics Society 41 (4): 543–52. https://doi.org/10.1518/001872099779656716
• Slater, J. M. 1956. Measurement and Integration of Acceleration in Inertial Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada284483
• 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, Sandra, Shirl Breitling, Kenneth Hodgdon, and Joseph Nedeau. 1995. “Missile Technology Demonstration Flight Test.” In Space Programs and Technologies Conference. AIAA 1995-3539. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-3539
• Smallwood, William L. 1966. Beryllium Erosion Corrosion Investigation for Solid Rocket Nozzles. Defense Technical Information Center. https://doi.org/10.21236/ad0372384
• Smallwood, W. L. 1967. Beryllium Erosion Corrosion Investigation for Solid Rocket Nozzles. Defense Technical Information Center. https://doi.org/10.21236/ad0382136
• Smeltzer, D., D. Durston, and V. Stewart. 1983. “Experimental Wing and Canard Jet-Flap Aerodynamics.” In 21st Aerospace Sciences Meeting. AIAA 1983-81. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-81
• 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, Turner L. 1953. Balance System for the Aberdeen 13 x 15” Supersonic Wind Tunnel”. Defense Technical Information Center. https://doi.org/10.21236/ad0007625
• Smith, Gerald L. 1960. A Homing Missile Control System to Reduce the Effects of Radome Diffraction. NASA-TM-X-395. NASA. https://ntrs.nasa.gov/citations/19980228347
• Smith, J. H. B. 1961. “Lift/Drag Ratios of Optimised Slewed Elliptic Wings at Supersonic Speeds.” Aeronautical Quarterly 12 (3): 201–18. https://doi.org/10.1017/s0001925900002067
• Smith, I. E. 1964. “Thrust Throttling of Large Liquid Propellant Rocket Engines.” Journal of the Royal Aeronautical Society 68 (647): 751–58. https://doi.org/10.1017/s0368393100080871
• Smith, Russell L. 1971. “The Human Operator in Optical Tracking Systems.” In SPIE Proceedings, vol. 0023, edited by J. G. Muhlberger, Ernie D. Miller. SPIE. https://doi.org/10.1117/12.953467
• Smith, Austin. 2007. “Proportional Navigation with Adaptive Terminal Guidance for Aircraft Rendezvous.” In AIAA Modeling and Simulation Technologies Conference and Exhibit. AIAA 2007-6712. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6712
• 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, D. D., and A. S. Keys. 2018. Prospects for the Development of Fast-Light Inertial Sensors. NASA/TM-2018-219867. NASA. https://ntrs.nasa.gov/citations/20180006415
• Smith, Dg, and R. Kinslow. 1977. “Simulating Rain Impact Damage to Supersonic Missile Radomes.” Journal of Testing and Evaluation 5 (2): 75–83. https://doi.org/10.1520/jte10665j
• Smith, C. A., J. N. Nielsen, and M. J. Hemsch. 1979. “Prediction of Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack.” In American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting. https://ntrs.nasa.gov/citations/19790035471
• Smith, Tamara, Albert Pavli, and Kenneth Kacynski. 1987. “Comparison of Theoretical and Experimental Thrust Performance of a 1030:1 Area Ratio Rocket Nozzle at a Chamber Pressure of 2413 kN/sq m (350 Psia).” In 23rd Joint Propulsion Conference. AIAA 1987-2069. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2069
• Smith, Theodore, Joseph Schetz, and Trong Bui. 2002a. “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, B., T. Welterlen, B. Maines, L. Shaw, M. Stanek, and J. Grove. 2002b. “Weapons Bay Acoustic Suppression from Rod Spoilers.” In 40th AIAA Aerospace Sciences Meeting & Exhibit. AIAA 2002-662. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-662
• Smith (e H) and Associates INC Sebastopol CA. 1961. Nuclear Weapon Casualties: Effects on Personnel. Defense Technical Information Center. https://doi.org/10.21236/ad0261739
• Smits, A. J. 1988. Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers. Defense Technical Information Center. https://doi.org/10.21236/ada191494
• Smoot, L., J. Simonsen, and G. Williams. 1972. “Exhaust Plume Prediction Model for a Low-Altitude Supersonic Missile.” In 8th Joint Propulsion Specialist Conference. AIAA 1972-1170. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-1170
• Smyth, R. 1972. “Weapon Delivery System Development.” In Guidance and Control Conference. AIAA 1972-896. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1972-896
• Snider, Shelley R. 2019. “Optimal Guidance Solutions for Tactical Missiles by Maximizing Impact Angle.” In AIAA Scitech 2019 Forum. AIAA 2019-1928. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1928
• Snyder, Murray, Eric Hallberg, and Alexis Cenko. 2010. “USNA/NAVAIR Cooperative Program in Store Separation.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-8118. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-8118
• Snyder, Deryl, Evangelos Koutsavdis, and John Anttonen. 2003. “Transonic Store Separation Using Unstructured CFD with Dynamic Meshing.” In 33rd AIAA Fluid Dynamics Conference and Exhibit. AIAA 2003-3919. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3919
• Snyder, Mark G., Richard J. Prazenica, and Richard A. Hull. 2015. “A New Impact Time Control Guidance Law for Precise Time-on-Target Missile Strike.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0613
• Sobel, S. A. 1963. Economics of Increasing Knowledge about Missile Reliability. Defense Technical Information Center. https://doi.org/10.21236/ad0422474
• Sobel, Jeffrey. 2015. AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). Defense Technical Information Center. https://doi.org/10.21236/ad1018985
• Soeda, M. 1998. “Human-Computer Cooperative Teleoperation with Time Delay.” In UKACC International Conference on Control (CONTROL ‘98), vol. 1998. IEE. https://doi.org/10.1049/cp:19980442
• Sokolov, Oleg A. 2016. “Air Launched Space Transportation Systems.” In Proceedings of the 12th Reinventing Space Conference. Springer International Publishing. https://doi.org/10.1007/978-3-319-34024-1_17
• Sol Acero, Enrique del. n.d. “Proprioceptive Force Estimation and Control for Teleoperation in Radioactive Environments.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.39021
• Solberg, Jason B. 1993. TOW Missile Pallet MIL-STD-1660 Tests. Defense Technical Information Center. https://doi.org/10.21236/ada275329
• “Solid Rocket Combustion Instability-An American Historical Account.” 1992. In Nonsteady Burning and Combustion Stability of Solid Propellants. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866159.0001.0016
• Solis, R. 1983. “An Analysis of the Vertical Launch Phase of a Missile Concept.” In 21st Aerospace Sciences Meeting. AIAA 1983-569. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-569
• 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, V., V. Krivtsov, A. Konchakov, and N. Malmuth. 2001. “Simulation of Supersonic Body Drag Reduction Produced by Forebody Filamentary Plasmas.” In 32nd AIAA Plasmadynamics and Lasers Conference. AIAA 2001-2727. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-2727
• Soms, Andrew P. 1988. Exact Lower Confidence Limits for the Reliability of k of n Systems for Zero Failures and Nonconservativeness of the Maximus Method. Defense Technical Information Center. https://doi.org/10.21236/ada194299
• Son, Chang-Hyeon, Sang-Hun Kim, and Heekyu Woo. 2021. “Application of Store Separation Wind Tunnel Test Technique into CFD.” Journal of the Korean Society for Aeronautical & Space Sciences 49 (4): 263–72. https://doi.org/10.5139/jksas.2021.49.4.263
• Son, Chang-Hyeon, and Sung-Eun Seo. 2017. “Store Separation Analysis of Flow Angularity Wind Tunnel Test Technique Using CFD (1).” Journal of the Korean Society for Aeronautical & Space Sciences 45 (1): 10–20. https://doi.org/10.5139/jksas.2017.45.1.10
• Song, Wei. 2021. “Investigation on Aircraft-Store Compatibility Criteria of External Store Separation.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-515674/v1
• Song, Tao, Defu Lin, and Jiang Wang. 2016. “Disturbance Observer–based Control for Missile Non-Strapdown Seeker Disturbance Rejection.” Advances in Mechanical Engineering 8 (4): 1687814016644577. https://doi.org/10.1177/1687814016644577
• Song, Taek Lyul, and Sang Jin Shin. 2004. “Active Homing Performance Enhancement with Multiple Model Radome Slope Estimation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-4899. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4899
• Sonneveldt, Bryan S., Ian G. Clark, and Clara O’Farrell. 2019. “Summary of the Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) Sounding Rocket Tests with a Disk-Gap-Band Parachute.” In AIAA Aviation 2019 Forum. AIAA 2019-3482. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3482
• Sorensen, Kirk, and Charles Schafer. 2001. Air Launch and LOX Collection as Enabling Technologies for Future Launch Systems. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20020023257
• Sorrells, Russell B., Matthew C. Towne, Charles F. Anderson, and Ronald H. Tolbert. 1985. Effects of Inlet Spillage on Store Carriage Loads and Launch Trajectories. Defense Technical Information Center. https://doi.org/10.21236/ada531358
• Soumekh, Mehrdad. 1997. Moving Target Detection and Motion Estimation in Foliage Using along Track Monopulse Synthetic Aperture Radar Imaging and Signal Subspace Processing of Uncalibrated MTD-SARs. Defense Technical Information Center. https://doi.org/10.21236/ada329234
• Sozen, Mehmet, Philip Davis, and Philip Davis. 2008. “Transpiration Cooling of a Liquid Rocket Thrust Chamber Wall.” In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2008-4559. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-4559
• Sozinov, P. A., and Б. Н. Горевич. 2021. “Dependence between the Accuracy of Target Designation to an Onboard Missile Radar Station and Errors Related to Determination of the Target and Missile Coordinates by a Ground Radar System.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 1: 22–41. https://doi.org/10.38013/2542-0542-2021-1-22-41
• Space Shuttle Orbit Maneuvering Engine Reusable Thrust Chamber. 1972. NASA-CR-128675. NASA. https://ntrs.nasa.gov/citations/19730005057
• Space Storable Regenerative Cooling Investigation. 1971. NASA-CR-72704. NASA. https://ntrs.nasa.gov/citations/19710028084
• “Spacecraft Intercept Guidance Using Zero Effort Miss Steering.” 1993. In Guidance, Navigation and Control Conference. AIAA 1993-3890. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3890
• Spahr, J. R. 1954. Longitudinal Aerodynamic Characteristics to Large Angles of Attack of a Cruciform Missile Configuration at a Mach Number of 2. NACA-RM-A54H27. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19710065192
• Spahr, H. 1974. “Theoretical Store Separation Analyses of a Prototype Store and Comparison with a Flight Drop Test.” In Mechanics and Control of Flight Conference. AIAA 1974-776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-776
• Spahr, Harold R. 1987. “Store Separation of Nuclear Weapons.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/871796
• Spahr, J. Richard, and Robert R. Dickey. 1951. Effect of Tail Surfaces on the Base Drag of a Body of Revolution at Mach Numbers of 1.5 and 2.0. NACA-TN-2360. NASA. https://ntrs.nasa.gov/citations/19930083086
• Spahr, J. Richard, and Robert A. Robinson. 1951. Wind-Tunnel Investigation at Mach Numbers of 1.5 and 2.0 of a Canard Missile Configuration. NACA-RM-A51C08. NASA. https://ntrs.nasa.gov/citations/19930086621
• Spalding, D. Brian. 1979. “LIQUID-PROPELLANT ROCKET.” In Combustion and Mass Transfer. Elsevier. https://doi.org/10.1016/b978-0-08-022106-9.50012-7
• Sparta INC Huntsville AL. 1992. Missile Interface Definition. Defense Technical Information Center. https://doi.org/10.21236/ada285637
• Spearman, M. Leroy. 1953. Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01. NACA-RM-L53K03. NASA. https://ntrs.nasa.gov/citations/19930087997
• 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. 1979. “Aerodynamic Characteristics of Missile Configurations Based on Soviet Design Concepts.” In 5th Atmospheric Flight Mechanics Conference for Future Space Systems. AIAA 1979-1657. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-1657
• Spearman, M. L. 1983. Supersonic Aerodynamic Characteristics of a Tail-Control Cruciform Maneuverable Missile with and without Wings. NASA-TM-84600. NASA. https://ntrs.nasa.gov/citations/19830009235
• Spearman, M. L. 1984. An Overview of Some Monoplanar Missile Programs. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19840059493
• Spearman, M. 1986a. “Effects of Some Geometric Variations on Missile Aerodynamic Characteristics at Supersonic Speeds.” In 24th Aerospace Sciences Meeting. AIAA 1986-570. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-570
• Spearman, M. L. 1986b. 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. L. 1992. Historical Review of Tactical Missile Airframe Developments. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920057203
• Spearman, M. Leroy, and Dorothy O. Braswell. 1994. An Experimental and Theoretical Study of the Aerodynamic Characteristics of Some Generic Missile Concepts at Mach Numbers from 2 to 6.8. NASA-TM-109110. NASA. https://ntrs.nasa.gov/citations/19940024970
• Spearman, M. Leroy, and Cornelius Driver. 1958. Effects of Canard Surface Size on Stability and Control Characteristics of Two Canard Airplane Configurations at Mach Numbers of 1.41 and 2.01. NACA-RM-L57L17a. NASA. https://ntrs.nasa.gov/citations/19930089965
• 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, M., and R. Fournier. 1978. “Supersonic Aerodynamic Characteristics of a Tail-Control Cruciform Maneuverable Missile with and without Wings.” In 4th Atmospheric Flight Mechanics Conference. AIAA 1978-1351. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1978-1351
• Spearman, M. Leroy, and Ross B. Robinson. 1952. Wind-Tunnel Investigation of a Ram-Jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges: Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.60. NACA-RM-L52E15. NASA. https://ntrs.nasa.gov/citations/19930087863
• Spearman, M. Leroy, and Ross B. Robinson. 1954. Aerodynamic Characteristics of a Cruciform-Wing Missile with Canard Control Surfaces and of Some Very Small Span Wing-Body Missiles at a Mach Number of 1.41. NACA-RM-L54B11. NASA. https://ntrs.nasa.gov/citations/19930088117
• Spearman, M. L., and W. W. Sawyer. 1977. Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-Span Missile with Three Wing Planforms. NASA-TM-74088. NASA. https://ntrs.nasa.gov/citations/19780004089
• Speelman, R., III. 1975. “Parachute Deployment Process Evaluation Using a Simple Dynamic Testing Technique.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1384. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1384
• 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
• Spencer, Bernard, Jr. 1981. Effects of Horizontal-Control Planform and Wing-Leading-Edge Modification on Low-Speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration. NASA-TM-X-549. NASA. https://ntrs.nasa.gov/citations/19980235628
• 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 Gyroscope Co Great Neck Ny. 1963c. Research in Predictive Instrumentation for Manual Control. Defense Technical Information Center. https://doi.org/10.21236/ad0602863
• Sperry Phoenix Co Az. 1962. Operational Analysis Report of the Microwave Command Guidance System. Defense Technical Information Center. https://doi.org/10.21236/ad0405722
• Speyer, Jason L. 1997. A Disturbance Attenuation Approach to Missile Guidance and Control. Defense Technical Information Center. https://doi.org/10.21236/ada329598
• Speyer, J., D. Dannemiller, and D. Walker. 1980. “Periodic Optimal Cruise of a Hypersonic Vehicle.” In Guidance and Control Conference. AIAA 1980-1777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1777
• Speyer, J., W. Greenwell, and D. Hull. 1982. “Adaptive Noise Estimation and Guidance for Homing Missiles.” In Guidance and Control Conference. AIAA 1982-1507. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1507
• Speyer, Jason L., and David G. Hull. 1986. Advanced Guidance Algorithms for Homing Missiles with Bearing-Only Measurements. Defense Technical Information Center. https://doi.org/10.21236/ada170833
• Speyer, Jason, Kevin Kim, and Minjea Tahk. 1990a. “A Passive Homing Missile Guidance Law Based on New Target Maneuver Models.” In Guidance, Navigation and Control Conference. AIAA 1990-3378. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3378
• Spinetti, Robert, and Bruce Jolly. 2008. “Time-Accurate Numerical Simulation of GBU-38s Separating from the B-1B Aircraft with Various Ejector Forces, Store Properties, and Load-Out Configurations: IHAAA Store Separation Cavity (SSC) Project -.” In 46th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2008-187. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-187
• 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
• Spratlin, Kenneth Milton. 1987. “An Adaptive Numeric Predictor-Corrector Guidance Algorithm for Atmospheric Entry Vehicles.” PhD diss., Draper (Charles Stark) Lab., Inc.. https://ntrs.nasa.gov/citations/19870017501
• Squire, L. C. 2000. “The Accuracy of Flat Plate, Turbulent Skin Friction at Supersonic Speeds.” Aeronautical Journal 104 (1036): 257–63. https://doi.org/10.1017/s0001924000091570
• Sreekumar, K., and A. T. Ramchandani. 2005. “Launch Stabilisation System for Vertical Launch of a Missile.” Defence Science Journal 55 (3): 223–30. https://doi.org/10.14429/dsj.55.1984
• Srinivasan, G., and R. Chamberlain. 2004. “Drag Reduction of Spiked Missile by Heat Addition.” In AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA 2004-4714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-4714
• Srinivasan, Navneeth, S. Varunkumar, and Preeti Aghalayam. 2021. “Supercritical Injection, Combustion and Acoustic Interactions in a Semi-Cryogenic Liquid Propellant Rocket Engine Injector.” International Conference on Liquid Atomization and Spray Systems (ICLASS) 1 (1). https://doi.org/10.2218/iclass.2021.5850
• Srinivasu, Neon, and Ashwini Ratnoo. 2022. “Guidance Design Using Line-of-Sight Angle Bifurcation.” In AIAA SCITECH 2022 Forum. AIAA 2022-1434. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1434
• Srivastava, B. 1998b. “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. 1997a. “Lateral Jet Control of a Supersonic Missile: CFD Predictions and Comparison to Force and Moment Measurements.” In 35th Aerospace Sciences Meeting and Exhibit. AIAA 1997-639. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-639
• Srivastava, B., and B. Srivastava. 1997b. “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
• Srokowski, A., F. Howard, and W. Feller. 1976. “Direct Measurements at Mach 6 of Turbulent Skin-Friction Reduction by Injection from Single and Multiple Flush Slots.” In 14th Aerospace Sciences Meeting. AIAA 1976-178. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-178
• Srour, Kutaibah, and Sohayb Abdulkerim. 2026. “Passive Fault-Tolerant Control for Supersonic Missile.” International Journal of Aeronautical and Space Sciences. https://doi.org/10.1007/s42405-026-01219-2
• “Stability Testing Methodology: Scaling Techniques for Liquid Rocket Combustion Stability Testing.” 1995. In Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866371.0545.0564
• Stallard, D. 1976. “Decoupling the Flight Control System of a Cruciform Missile.” In Guidance and Control Conference. AIAA 1976-1943. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1943
• 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
• Stallard, D. 1980. “An Approach to Optimal Guidance for a Bank-to-Turn Missile.” In Guidance and Control Conference. AIAA 1980-1747. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1747
• Stallard, D. 1984. “Discrete Optimal Control Solutions, with Application to Missile Guidance.” In 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference. AIAA 1984-1886. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1984-1886
• Stallard, D. 1985. “Analysis of the Parasitic Radome Loop in a Bank-to-Turn Homing Missile.” In Guidance, Navigation and Control Conference. AIAA 1985-1868. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1868
• 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
• Stallings, R. L., Jr. 1983. Store Separation from Cavities at Supersonic Flight Speeds. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19830043664
• Stallings, R. L., Jr. 1984. Aerodynamic Characteristics of a Sparrow 3 Missile Model in the Flow Field of a Generalized Parent Body at Mach 2.86. NASA-TM-85713. NASA. https://ntrs.nasa.gov/citations/19840009066
• Stanek, Michael J. 2002. “Aircraft Weapons Bay Acoustic Suppression Apparatus.” Journal of the Acoustical Society of America 111 (6): 2535. https://doi.org/10.1121/1.1492934
• Stanek, Michael J. 2003. “Aircraft Weapons Bay High Frequency Acoustic Suppression Appartus.” Journal of the Acoustical Society of America 113 (4): 1788. https://doi.org/10.1121/1.1572348
• Stanek, Michael J. 2007. “Aircraft Weapons Bay Acoustic Resonance Suppression System.” Journal of the Acoustical Society of America 122 (6): 3151. https://doi.org/10.1121/1.2822955
• Stanley, J. K. 1969. The Deterioration of Stainless Steel Regeneratively Cooled Thrust Chambers. Defense Technical Information Center. https://doi.org/10.21236/ad0862109
• Stanley, James. 1970. “The Deterioration of Stainless Steel Regeneratively Cooled Thrust Chambers.” In 11th Structures, Structural Dynamics, and Materials Conference. AIAA 1970-1510. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1510
• Stansbery, Donald, and James Cloutier. 2001. “Nonlinear, Hybrid Bank-to-Turn/skid-to-Turn Missile Autopilot Design.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4158
• Stechman, R., and C. Drenning. 1981. “Qualification Test Results, 5 Lb/f/ /22 Newton/ Earth Storable Bipropellant Rocket Engine.” In 17th Joint Propulsion Conference. AIAA 1981-1408. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1408
• Stefanski, Konrad. 2019. “The Analysis of the Anti-Aircraft Missile Flight Controlled with Gyroscopic System.” In AIP Conference Proceedings, vol. 2077. Author(s). https://doi.org/10.1063/1.5091915
• Steinfeldt, Bradley, Grant Rossman, Robert Braun, and Gregg Barton. 2013. “Rapid Robust Design of a Deployable System for Boost-Glide Vehicles.” In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. AIAA 2013-31. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-31
• Steinicke, Armin, and Gunther Michalka. 2002. “Improving Transient Performance of Dynamic Inversion Missile Autopilot by Use of Backstepping.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4658. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4658
• Steltzner, Adam, Robin Bruno, Robert Mitcheltree, and Juan Cruz. 2003. “Opportunities and Limitations in Low-Earth Subsonic Testing and Qualification of Extraterrestrial Supersonic Parachute Designs.” In 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2003-2135. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2135
• Stephen, Eric J., Drew Q. Broadbent, Brent A. Matherne, and Thomas E. McLaughlin. 2018. “Investigation of Reshaping Pin Protuberance for Missile Flight Control in Supersonic Flow.” In 2018 AIAA Aerospace Sciences Meeting. AIAA 2018-1515. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1515
• 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
• Stepp, Nigel, and Michael T. Turvey. 2017. “Anticipation in Manual Tracking with Multiple Delays.” Journal of Experimental Psychology: Human Perception and Performance 43 (5): 914–25. https://doi.org/10.1037/xhp0000393
• Stevens, F., T. On, and T. Clare. 1974. “Wrap-around vs. Cruciform Fins: Effects on Rocket Flight Performance.” In Mechanics and Control of Flight Conference. AIAA 1974-777. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1974-777
• Stewart, Elwood C. 1955. Application of Statistical Theory to Beam-Rider Guidance in the Presence of Noise I: Wiener Filter Theory. NACA-RM-A55E11. NASA. https://ntrs.nasa.gov/citations/19930088776
• Stewart, Elwood C. 1958. Application of Statistical Theory to Beam-Rider Guidance in the Presence of Noise II: Modified Wiener Filter Theory. NACA-TN-4278. NASA. https://ntrs.nasa.gov/citations/19930085069
• Stewart, Elwood C. 1961. An Explicit Linear Filtering Solution for the Optimization of Guidance Systems with Statistical Inputs. NASA-TN-D-685. NASA. https://ntrs.nasa.gov/citations/20040006352
• Stewart, V. R. 1981. “An Investigation of the Use of a Propulsive Wing/canard Concept for Improved Maneuvering.” In V/STOL Conference. https://ntrs.nasa.gov/citations/19820033370
• 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, Christine E. 2013. “Spacecraft Parachute Recovery System Testing from a Failure Rate Perspective.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1308. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1308
• Stewart, Mark G. 2021. “Simplified Reliability-Based Load Design Factors for Explosive Blast Loading, Weapons Effects, and Its Application to Collateral Damage Estimation.” Journal of Defense Modeling and Simulation: Applications, Methodology, Technology 19 (3): 385–401. https://doi.org/10.1177/1548512920977737
• Stewart, Reuben-Wayne, Moble Benedict, and Jack Dooher. 2024. “Nonlinear Flight Dynamics Modeling of an Air-Launched Tailsitter UAS.” In Vertical Flight Society Annual Forum and Technology Display. https://doi.org/10.4050/f-0080-2024-0006
• Stewart, Elwood C., Frank Druding, and Togo Nishiura. 1958. The Effects of Target and Missile Characteristics on Theoretical Minimum Miss Distance for a Beam-Rider Guidance System in the Presence of Noise. NACA-RM-A57F26. NASA. https://ntrs.nasa.gov/citations/19930089891
• Stewart, Elwood C., Frank Druding, and Togo Nishiura. 1959. The Effects of Target and Missile Characteristics on Theoretical Minimum Miss Distance for a Beam-Rider Guidance System in the Presence of Noise. NASA-MEMO-2-12-59A. NASA. https://ntrs.nasa.gov/citations/19980230603
• Stewart, Elwood C., and Gerald L. Smith. 1959. The Synthesis of Optimum Homing Missile Guidance Systems with Statistical Inputs. NASA-MEMO-2-13-59A. NASA. https://ntrs.nasa.gov/citations/19980228243
• Stiegler, Anthony D. 1960. A Mathematical Formulation for ORDVAC Computation of the Single-Shot Kill Probabilities of a General Missile versus a General Aircraft. Defense Technical Information Center. https://doi.org/10.21236/ad0249957
• Stippes, M. 1962. Analysis of Missile Launchers. Part r. Approximate Formulas for Pitch Velocity at Tip-off. Defense Technical Information Center. https://doi.org/10.21236/ad0285042
• 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
• Stojanović, Marijana, Aleksandar Stefanović, Nebojša Jovičić, and Ivan Marić. 2024. “Testing the Roll Stabilization of a Supersonic Surface-to-Air Guided Missile.” In 11th International Scientific Conference on Defensive Technologies - OTEX 2024 - zbornik radova. Military Technical Institute, Belgrade. https://doi.org/10.5937/oteh24053s
• Stokes, Joshua T., and Thomas Lombaerts. 2023. “Control System Design for a Hypersonic Re-Entry Vehicle.” In AIAA SCITECH 2023 Forum. AIAA 2023-1638. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1638
• Stoll, F., and D. G. Koenig. 1983. Large-Scale Wind-Tunnel Investigation of a Close-Coupled Canard-Delta-Wing Fighter Model through High Angles of Attack. AIAA PAPER 83-2554. NASA Ames Research Center. https://ntrs.nasa.gov/citations/19830067155
• Stone, A. H. 1945. The Aerodynamics of a Slightly Yawing Supersonic Cone. Defense Technical Information Center. https://doi.org/10.21236/ada801302
• Storey, Callum. 2023. “The Effect of Frame Shape on the Aerodynamic Properties of a Missile Grid Fin.” In 2023 Regional Student Conferences. AIAA 2023-77003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-77003
• Stoykov, Stoyko. 2022. “Comparative Analysis of the Accuracy of Bomb Release and the Probability Characteristics of the Error of Bombing of Different Methods Solving the Problem of Aiming.” Aerospace Research in Bulgaria 34: 149–56. https://doi.org/10.3897/arb.v34.e13
• Stoykov, Stoyko, and Milen Atanasov. 2016. “Determination Bombing Accuracy from Level Delivery Using the Ejection Practical Bomb.” Scientific Research and Education in the AIR Force 18 (1): 361–66. https://doi.org/10.19062/2247-3173.2016.18.1.49
• Strahle, W. C. 1970a. New Considerations on Causes for Combustion Instability in Liquid Propellant Rockets. NASA. https://ntrs.nasa.gov/citations/19700063964
• Strahle, W. C. 1970b. A Note on the Forgotten Velocity Effect in Combustion Instability of Liquid Rockets. NASA. https://ntrs.nasa.gov/citations/19700063963
• “Strategic Missiles.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_6
• Strauss, Robert F. 1964. Monitoring of Rocket Engine Performance by Spectroscopic Techniques. Defense Technical Information Center. https://doi.org/10.21236/ad0609492
• 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
• Strohm, Luke S. 2013. An Introduction to the Sources of Delivery Error for Direct-Fire Ballistic Projectiles. Defense Technical Information Center. https://doi.org/10.21236/ada588846
• Strope, Kristopher, and Richard Kretzschmar. 1998. “Aerodynamic Prediction Accuracy for a Missile Configuration with Elliptical Cross Section.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4271
• Strydom, Reuben, and Mandyam V. Srinivasan. 2017. “UAS Stealth: Target Pursuit at Constant Distance Using a Bio-Inspired Motion Camouflage Guidance Law.” Bioinspiration & Biomimetics 12 (5): 055002. https://doi.org/10.1088/1748-3190/aa7d65
• Stuber, Eric, Nishant Prasadh, Stephen Edwards, and Dimitri Mavris. 2012. “Hydrocarbon Liquid Rocket Engine Technology Impact Forecasting.” In AIAA SPACE 2012 Conference & Exposition. AIAA 2012-5155. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5155
• Student. 1908. “The Probable Error of a Mean.” Biometrika 6 (1): 1. https://doi.org/10.2307/2331554
• Studhalter, W. R. 1964. “The J-2 Liquid Hydrogen Rocket Engine.” SAE technical papers on CD-ROM/SAE technical paper series 1. https://doi.org/10.4271/640040
• Sturek, W. B., L. D. Kayser, and P. Weinacht. 1983. Computational Study of Swept-Fin Aerodynamic Heating for the 105mm M774. Defense Technical Information Center. https://doi.org/10.21236/ada134992
• Sturek, Walter B., and Malcolm S. 2001. Statistical Analysis of CFD Results for Missile Surface Pressures. Defense Technical Information Center. https://doi.org/10.21236/ada394691
• Sturek, W., and L. Schiff. 1980. “Computations of the Magnus Effect for Slender Bodies in Supersonic Flow.” In 6th Atmospheric Flight Mechanics Conference. AIAA 1980-1586. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-1586
• Sturek, Walter B., and Lewis B. Schiff. 1981. Computations of the Magnus Effect for Slender Bodies in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ada110016
• Sturek, Walter, Sr., and Malcolm Taylor. 2000. “Statistical Analysis of CFD Results for Missile Surface Pressures.” In 18th Applied Aerodynamics Conference. AIAA 2000-4214. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4214
• Su, Pei Ran, Qitai Eri, and Xi Xi Li. 2013. “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, Shaoying, Mingfeng Shi, Meilin He, Zhirui Hu, and Wei Feng. 2026. “Adaptive Forgetting Factor Probabilistic Data Association Filtering for Radar Target Tracking in Cluttered Environments with Unknown and Varying Measurement Noise Covariance.” IET Radar, Sonar & Navigation 20 (1): e70250. https://doi.org/10.1049/rsn2.70250
• 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
• 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
• Suenaga, Osamu. 1996. “Study on Control Characteristics of Human Operator in Pursuit Manual Tacking Control Systems.” Japanese Journal of Ergonomics 32 (Supplement): 372–73. https://doi.org/10.5100/jje.32.supplement_372
• Suenaga, Osamu, and Motozo Ihara. 1991. “A Consideration on Manual Preview Control of Human Operator.” Japanese Journal of Ergonomics 27 (6): 283–89. https://doi.org/10.5100/jje.27.283
• Suenaga, Osamu, Motozo Ihara, and Tooru Nogai. 1983. “An Analysis of Individual Difference of Human Operator in Manual Tracking Control: Individual Difference in Relation to Learning Characteristics.” TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series C 49 (447): 1991–98. https://doi.org/10.1299/kikaic.49.1991
• Summerfield, Martin. 1951a. Project SQUID: A Theory of Unstable Combustion in Liquid Propellant Rocket Systems. Defense Technical Information Center. https://doi.org/10.21236/ada952489
• Summerfield, Martin. 1960. “G. the Liquid Propellant Rocket Engine.” In Liquid Propellant Rockets. Princeton University Press. https://doi.org/10.1515/9781400879953-005
• Summerfield, Martin, and Herman Krier. 1968. Role of Aluminum in Suppressing Instability in Solid Propellant Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ada952099
• 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, 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, Jun, Peng Cheng, Qinglian Li, Jie Song, Lanwei Chen, and Peng Cui. 2022. “Gas Film/Regenerative Composite Cooling Characteristics of the Lox/Lch4 Rocket Engine.” Preprint, . https://doi.org/10.2139/ssrn.4113765
• 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, Lei, Pu Lian, and Xiaofei Chang. 2017. “Capturability of Retro-Augmented Proportional Navigation Guidance Law against Higher Speed Maneuvering Target.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2203. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2203
• Sun, Rui Sheng, Peng Yun Liu, and Jian Shen. 2012a. “Integrated Guidance and Control of Missile Using Subspace Stabilization Method.” Advanced materials research 490-495: 1161–65. https://doi.org/10.4028/www.scientific.net/amr.490-495.1161
• Sun, Jin, Dengyin Zhang, Xiaoye Shi, and Fei Ding. 2020. “Fast Compass Alignment for Strapdown Inertial Navigation System.” Computers, Materials & Continua 65 (2): 1349–60. https://doi.org/10.32604/cmc.2020.011459
• Sundberg, W. 1975. “Finite-Element Modeling of Parachute Deployment and Inflation.” In 5th Aerodynamic Deceleration Systems Conference. AIAA 1975-1380. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1380
• Sundén, Bengt, and Juan Fu. 2017. “Aerodynamic Heating.” In Heat Transfer in Aerospace Applications. Elsevier. https://doi.org/10.1016/b978-0-12-809760-1.00003-x
• Sung, D. K. 2004. “Combustion Instability of Liquid Rocket Engines.” Journal of the Korean Society for Aeronautical & Space Sciences 32 (9): 153–61. https://doi.org/10.5139/jksas.2004.32.9.153
• Suraweera, Milinda, David Mee, and Raymond Stalker. 2005. “Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion.” In 43rd AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2005-613. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-613
• Surve, Prajakta S., Arnab Maity, and Shashi Ranjan Kumar. 2023. “Impact Angle Constrained Guidance against Non-Maneuvering Target with Bounded Input.” In AIAA SCITECH 2023 Forum. AIAA 2023-1630. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-1630
• Surzhikov, S. 1999. “Blast Wave Stage of Explosion of Launch Vehicle in Flight.” In 30th Fluid Dynamics Conference. AIAA 1999-3776. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-3776
• Sutton, George P. 1968. “Rocket Classifications, Liquid Propellant Rockets, Engine Selection, and Heat Transfer.” In Applied Physics and Engineering. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-46109-5_5
• Sutton, R. D. 1970. Propellant Spray Combustion Processes during Stable and Unstable Liquid Rocket Combustion. Defense Technical Information Center. https://doi.org/10.21236/ad0722473
• Sutton, George. 2007. “The Effect of Laser-Induced Upstream Cylindrical Shock Waves on the Drag, Weight, and Performance of a High Velocity Missile.” In 38th Plasmadynamics and Lasers Conference. AIAA 2007-4010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-4010
• Sutton, George, James Troiler, Dale Carlson, and Ronald Hinrichsen. 1995. “Thermal Stresses and Radiation of an Uncooled Optical Dome Due to Transient Aerodynamic Heating.” In 30th Thermophysics Conference. AIAA 1995-2014. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-2014
• Svob, G., and K. W. Bills Jr. 1982. “A Predictive Surveillance Technique for Air-Launched Motors.” In 18th Joint Propulsion Conference. AIAA 1982-1097. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-1097
• 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
• Sweet, Barbara Townsend. 2013. “A Model of Manual Control with Perspective Scene Viewing.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20140009117
• Szajnecki, Logan, Dhiman Roy, Lian Duan, and Nicholas J. Bisek. 2025. “Effect of Reynolds Number on a High-Speed Cold-Wall Turbulent Boundary Layer.” Journal of Fluid Mechanics 1016: A49. https://doi.org/10.1017/jfm.2025.10296
• Szakaly, Z., W. S. Kim, and A. K. Bejczy. 1989. “Force-Reflective Teleoperated System with Shared and Compliant Control Capabilities.” In Proceedings of the NASA Conference on Space Telerobotics, Volume 4. https://ntrs.nasa.gov/citations/19900020529
• 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
• 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
• “Tactical Missile Guidance Laws.” n.d. In Missile Guidance and Control Systems. Springer-Verlag. https://doi.org/10.1007/0-387-21816-5_4
• Taguchi, Masato, Koichi Mori, and Masashi Kashitani. 2021. “Frequency Analysis on Canopy Motion and Shock Wave Oscillation around a Hemispherical Wind Tunnel Model of Supersonic Parachute.” In AIAA Scitech 2021 Forum. AIAA 2021-0612. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2021-0612
• Taguchi, Masato, Naoki Semba, and Koichi Mori. 2015. “Effects of Flexibility and Gas Permeability of Fabric to Supersonic Performance of Flexible Parachute.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2133. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2133
• Taha, A., and J. E. Hudson. 1986. “Symmetric Two-Target Monopulse Angle Estimator.” Electronics Letters 22 (21): 1116–17. https://doi.org/10.1049/el:19860764
• 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
• Tahk, Min-Jea, Han-Lim Choi, Hun-Gu Lee, and Yonmook Park. 2001. “A Three-Dimensional Diffrential Game Missile Guidance Law Using Neural Networks.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4343. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4343
• Tahk, Minjea, and Jason Speyer. 1989. “Use of Intermittent Maneuvers for Miss Distance Reduction in Exoatmospheric Engagements.” In Guidance, Navigation and Control Conference. AIAA 1989-3547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1989-3547
• Tajima, Y. A. 1965. Mechanism of Catalytic Ignition and Combustion of Solid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0472135
• Takabayashi, K., K. Fukumoto, and K. Kitamura. 2019. “Computational Study on Rigid Disk-Gap-Band Supersonic Parachute Aerodynamics.” In 31st International Symposium on Shock Waves 2. Springer International Publishing. https://doi.org/10.1007/978-3-319-91017-8_129
• Takahashi, Yusuke, Kazuhiko Yamada, Takashi Abe, and Kojiro Suzuki. 2013. “Aerodynamic Heating around an Inflatable Vehicle during a Reentry Demonstration Flight by a Sounding Rocket.” In AIAA Aerodynamic Decelerator Systems (ADS) Conference. AIAA 2013-1303. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-1303
• Takanashi, Shinichiro, Etsuroh Sentoh, Akihiko Yoshida, Kousuke Kikumoto, Tatsuo Takahashi, and Hidenori Tokunaga. 1998. “Sidejet Aerodynamic Interaction Effect of the Missile. II: Prediction of Interaction Effect by the Force Measurement.” In 23rd Atmospheric Flight Mechanics Conference. AIAA 1998-4346. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4346
• Takano, Satoru, Hikaru Inooka, and Xiangjie Lu. 2000. “309 Manual Control System Providing a Performance Index to a Human Operator.” Proceedings of Conference of Tohoku Branch 2000.35 (0): 96–97. https://doi.org/10.1299/jsmeth.2000.35.96
• Takano, Hiroyuki, Youhei Shiraishi, and Takeshi Yamasaki. 2026. “New Modified Proportional Navigation Guidance with Several Constraints.” In AIAA SCITECH 2026 Forum. AIAA 2026-2347. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-2347
• Takano, Hiroyuki, Youhei Shiraishi, Takeshi Yamasaki, and Isao Yamaguchi. 2022. “A Note on the Singularity of Modified Proportional Navigation Guidance.” In AIAA SCITECH 2022 Forum. AIAA 2022-1430. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-1430
• Takano, Hiroyuki, Takeshi Yamasaki, and Isao Yamaguchi. 2024. “The Optimal Trajectories and Modified Proportional Navigation Guidance.” In AIAA SCITECH 2024 Forum. AIAA 2024-1015. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-1015
• Takeda, Shodai, Ibuki Sato, Hiroshi Katanoda, and Hiroshi Kouguchi. 2022. “Effect of the Ratio of Fuel to Aft-Combustion Chamber Length on Thrust Characteristics of Hybrid Rocket Engine.” Proceedings of Mechanical Engineering Congress, Japan 2022 (0): J191-08. https://doi.org/10.1299/jsmemecj.2022.j191-08
• Talbot, Matthew, and Seth Moyer. 1993. “A Refinement of the Preliminary Store Separation Analysis Process.” In 31st Aerospace Sciences Meeting. AIAA 1993-857. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-857
• Talley, Doug. 2002. Progress in Pulsed Detonation Rocket Engines at AFRL-West. Defense Technical Information Center. https://doi.org/10.21236/ada410766
• Talole, Sanjay, and Srivijay Phadke. 2002. “Nonlinear Target State Estimation in Homing Guidance.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-4772. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-4772
• Talole, S., S. Phadke, and R. Singh. 2005. “Predictive Homing Guidance Using Time Delay Control.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6159. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6159
• 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
• 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, Toshiyuki, and Hirofumi Eguchi. 1990. “Hyperstable Range in Homing Missiles.” In Guidance, Navigation and Control Conference. AIAA 1990-3381. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1990-3381
• Tang, Chun Y., Suman Muppidi, John W. Van Norman, Rebekah Tanimoto, Deepak Bose, and Ian G. Clark. 2015. “Post-Flight Aerodynamic and Aerothermal Model Validation of a Supersonic Inflatable Aerodynamic Decelerator.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2136. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2136
• Tang, M. H., and G. P. E. Pearson. 1971. Flight-Measured HL-10 Lifting Body Center Fin Loads and Control Surface Hinge Moments and Correlation with Wind-Tunnel Predictions. NASA-TM-X-2419. NASA. https://ntrs.nasa.gov/citations/19710029224
• Tang, Mingzhang, Liwu Wang, Yu Liu, and Sijun Zhang. 2021. “Effects of Aerodynamics on Line Sail during Parachute Deployment.” In Volume 1: Aerospace Engineering Division Joint Track; Computational Fluid Dynamics. American Society of Mechanical Engineers. https://doi.org/10.1115/fedsm2021-65585
• Tanner, Christopher L., Clara O’Farrell, John C. Gallon, et al. 2015. “Pilot Deployment of the LDSD Parachute via a Supersonic Ballute.” In 23rd AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2015-2128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2128
• 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
• Tao, Yang, Zhaolin Fan, Jifei Wu, and Wenhua Wu. 2010. “Investigation on Stability in Roll of Square Section Missile at High Angle of Attack.” Modern Physics Letters B 24 (13): 1385–88. https://doi.org/10.1142/s0217984910023682
• Tao, Yujing, Wu Jiping, and Wang Zhenguo. 2006. “Design and Application of Throttling Venturi for Cryogenic Propellants in Tripropellant Rocket Engine.” In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2006-4883. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4883
• Taraborrelli, A. 2023. “Development of an FBG-Based Hinge Moment Measuring System for Wind Tunnel Testing.” In Materials Research Proceedings, vol. 37. Materials Research Forum LLC. https://doi.org/10.21741/9781644902813-92
• Tardioli, Luca, Giovanni Franzini, Lorenzo Pollini, and Mario Innocenti. 2017. “Visibility Augmentation of the Proportional Navigation Guidance.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1013. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1013
• 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
• Taub, Ilan, and Tal Shima. 2012. “Intercept Angle Missile Guidance under Time-Varying Acceleration Bounds.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2012-4472. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4472
• 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. 2009. “Robust Optimal Sliding Mode Guidance Law with Path Constraint for Passive Homing.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2009-5898. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5898
• Taur, Der-ren. 2010. “A Sliding Mode Nonlinear Guidance with Navigation Loop Dynamics of Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2010-7746. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7746
• 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
• Taur, Der-Ren, and Jeng-Shing Chern. 1999. “Rolleron Dynamics in Missile Applications.” In 24th Atmospheric Flight Mechanics Conference. AIAA 1999-4260. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-4260
• Taur, Der-Ren, and Jeng-Shing Chern. 2000. “A Modified Proportional Navigation Guidance Law for IR Homing Missiles.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4160
• Taylor, R. E. 1956. Fuze, Guided Missile, Proximity, T3008E5, Design and Performance. Defense Technical Information Center. https://doi.org/10.21236/ad0307706
• Taylor, Nigel J. 2022. “AVT-316 Missile Facet: Lessons Learned Concerning the Prediction of Vortex Flow Interactions about Generic Missile Configurations.” In AIAA SCITECH 2022 Forum. AIAA 2022-0002. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-0002
• Tekin, Raziye, Özgür Atesoglu, and Kemal Leblebicioglu. 2010. “Modeling and Vertical Launch Analysis of an Aero- and Thrust Vector Controlled Surface to Air Missile.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2010-7639. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-7639
• Tekin, Raziye, Ozgur Atesoglu, and Kemal Leblebicioglu. 2013. “Flight Control Algorithms for a Vertical Launch Air Defense Missile.” In Advances in Aerospace Guidance, Navigation and Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-642-38253-6_6
• Tekin, Raziye, and Koray S. Erer. 2015a. “Considerations on Boost Phase Modeling and Guidance Command Generation.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-0862. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0862
• Tekin, Raziye, Koray S. Erer, and Florian Holzapfel. 2019. “Impact Time Control with Generalized Look Angle Formulation under Constraint.” In AIAA Scitech 2019 Forum. AIAA 2019-1924. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1924
• Tekin, Raziye, and Florian Holzapfel. 2017. “Impact Angle Control Based on Feedback Linearization.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1509. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1509
• Teleoperator Human Factors Study. 1986. NASA-CR-178930. NASA. https://ntrs.nasa.gov/citations/19880014778
• Tellier, G. F. 1964. Rocket Engine Valve Poppet and Seat Design Data. Defense Technical Information Center. https://doi.org/10.21236/ad0600420
• Templeton, J., J. Bosley, S. Ohanian, and K. Dannenberg. 1976. “Autopilot Design for Microcomputer Applications to Terminal Homing.” In Guidance and Control Conference. AIAA 1976-1978. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1976-1978
• Teng, Guest Editor Yuantao. 2016. “A Study on Function Allocation Application in Human-Machine System.” International Journal of Simulation Systems Science & Technology. https://doi.org/10.5013/ijssst.a.17.01.12
• Teng, Hsien-Hao, and Zhong-Xin Yu. 2023. “Analysis of Trajectory of the Projectile Released from Fighter-Aircraft Weapons Bay.” In AIAA AVIATION 2023 Forum. AIAA 2023-4547. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2023-4547
• “Test Range Instrumentation.” 1996. In Global Positioning System: Theory and Applications, Volume II. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/5.9781600866395.0593.0623
• “Testing Guidance Laws Performance.” 2007. In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781420062281-11
• Tetervin, Neal. 1963. Approximate Analysis of Effect on Drag of Truncating the Conical Nose of a Body of Revolution in Supersonic Flow. Defense Technical Information Center. https://doi.org/10.21236/ad0400708
• Thang, Le Quyet. 2025. “A Synthesis of Stabilization Algorithms for Long-Range Surface-to-Air Missile Systems.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate1125015.009
• Thapa, Rabin. 2023. “Evolution in Propellant of the Rocket Engine.” Journal of Materials Physics and Chemistry 11 (1): 8–21. https://doi.org/10.12691/jmpc-11-1-2
• Theerthamalai, P., R. Mukesh, M. Praveenkumar, et al. 2025. “Advanced Aerodynamic Prediction Software for Versatile Canard-Controlled Missile Configurations.” Physics of Fluids 37 (2): 023626. https://doi.org/10.1063/5.0256726
• 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
• “The Thermal Rocket Engine.” n.d. In Rocket and Spacecraft Propulsion. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-69203-4_2
• Thibodeaux, J. J. 1977. Effect of Gyro Verticality Error on Lateral Autoland Tracking Performance for an Inertially Smoothed Control Law. NASA-TM-X-3545. NASA. https://ntrs.nasa.gov/citations/19770020186
• Thiet, Dang Van. 2025. “Accuracy Improvement of Target Angle Tracking in Long-Range SAM Control Radars via Optimized Filtering.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate1125021.016
• Third Annual NASA University Conference on Manual Control. 1967. NASA-SP-144. NASA. https://ntrs.nasa.gov/citations/19680006432
• 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, Randy, and David Thomas. 2008. “Design Analysis of an Aircraft Parachute Recovery System for Very Light Jets.” In The 26th Congress of ICAS and 8th AIAA ATIO. AIAA 2008-8949. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-8949
• Thompson, Milton J. 1970. Skin Friction and Heat Transfer in Turbulent Boundary Layers as Influenced by Roughness. Defense Technical Information Center. https://doi.org/10.21236/ad0734152
• Thompson, George J., and Spiro Pappas. 1973. Optical Radar Angle Tracking Mount. Defense Technical Information Center. https://doi.org/10.21236/ad0765213
• Thompson, George J., Spiro Pappas, and Andrew S. Zvilna. 1974. Optical Radar Angle Tracking Mount. Defense Technical Information Center. https://doi.org/10.21236/ada001638
• Thongchua, Nat, and Michael Kaczmarek. 1994. Theater Missile Defense Targets for Interceptor Test and Evaluation,. Defense Technical Information Center. https://doi.org/10.21236/ada288602
• Thornburg, Jeff. 2002. Air Force Research Laboratory’s Rocket Engine Program Enters Fast-Paced Test Phase. Defense Technical Information Center. https://doi.org/10.21236/ada411890
• Thornton, A. L. 1981. LOVEL: A Low-Velocity Aerodynamic Heating Code for Flat-Plates, Wedges, and Cones. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/6611421
• Thurston, Paul A. 1965. Accuracy and Dispersion of Unguided, Air-Launched Rockets. Defense Technical Information Center. https://doi.org/10.21236/ad0474776
• Thynell, S. T., J. H. Adair, Goddard III, et al. 2014. Spray and Combustion of Gelled Hypergolic Propellants for Future Rocket and Missile Engines. Defense Technical Information Center. https://doi.org/10.21236/ada614447
• Tiaden, Ryan, and Oleg Yakimenko. 2008. “Development of a Payload Derived Position Acquisition System for Parachute Recovery Systems.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-7487. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-7487
• Tian, Jiahao, Zhanling Wang, Jianxiong Zhou, et al. 2025. “Angle Estimation of a Second Target in Monopulse Radar via Separation-Confirmation Method Given the DOA of the Other Target.” Preprint, . https://doi.org/10.36227/techrxiv.176403059.98656708/v1
• Timenes, N. 1964. The Firepower of a Surface-to-Air Missile System against Crossing Raids. Defense Technical Information Center. https://doi.org/10.21236/ad0450163
• Tischler, Adelbert O., and Jack C. Humphrey. 1956. Regenerative-Cooling Studies in a 5000-Pound-Thrust Liquid-Oxygen: JP-4 Rocket Engine Operated at 600-Pounds-per-Square-Inch Combustion-Chamber Pressure. NACA-RM-E56B02. NASA. https://ntrs.nasa.gov/citations/19930089246
• Tishchenko, Yu. E., and B. E. Fedunov. 2006. “Optimal Instants for Missile Launching Missiles and Application of Jamming in a Duel Situation of Fighters.” Journal of Computer and Systems Sciences International 45 (5): 772–83. https://doi.org/10.1134/s1064230706050091
• Tishkoff, J. M., M. A. Birkan, G. S. Roy, and S. G. Lekoudis. 1989. AFOSR/ONR Contractors’ Meeting on Combustion Rocket Propulsion Diagnostics of Reacting Flow Held in Ann Arbor, Michigan on 19-23 June 1989. Defense Technical Information Center. https://doi.org/10.21236/ada224411
• Tiszauer, Detlev H. 1989. “Fourier Theory of Conical Scan Demodulation.” In SPIE Proceedings, vol. 1167, edited by Daniel Vukobratovich. SPIE. https://doi.org/10.1117/12.962960
• Tiwari, Vidhu, Rajamohan Kalluru, Fang-Yu Yueh, and Jagdish Singh. 2005. “Measurement of Liquid Nitrogen in a Liquid Oxygen Feed Line during Rocket Engine Testing.” In 35th AIAA Fluid Dynamics Conference and Exhibit. AIAA 2005-5274. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-5274
• 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
• To, Tuan A. n.d. “AUSROC 2.5 Drogue Parachute Recovery System.” PhD diss., The University of Queensland. https://doi.org/10.14264/345621
• Tobey, Aubrey C., and E. Karl Bastress. 1966. Flame-Piloting Mechanisms in Liquid Propellant Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ad0655792
• Todosiev, E. P. 1967. Human Performance in a Cross-Coupled Tracking System. NAS 1-4419. NASA. https://ntrs.nasa.gov/citations/19680094917
• Tofani, A. 1989. “Analysis of the Infrared Emission Due to Aerodynamic Heating of Missile Domes.” In SPIE Proceedings, vol. 1112, edited by Paul Klocek. SPIE. https://doi.org/10.1117/12.960792
• Token, K. H. 1974. Heat Transfer Due to Shock Wave Turbulent Boundary Layer Interactions on High Speed Weapon Systems. Defense Technical Information Center. https://doi.org/10.21236/ada002685
• Tomazic, William A. 1955. Rocket-Engine Throttling. NACA-RM-E55J20. NASA. https://ntrs.nasa.gov/citations/19930088927
• Tomczak, Steven P. 1976. Diffuse Target Scintillation in 10.6-Micrometer Laser Radar. Defense Technical Information Center. https://doi.org/10.21236/ada024310
• Tomizuka, M., and D. E. Whitney. 1976. “The Human Operator in Manual Preview Tracking (an Experiment and Its Modeling via Optimal Control).” Journal of Dynamic Systems, Measurement, and Control 98 (4): 407–13. https://doi.org/10.1115/1.3427058
• Tong, Xindi, Jia Song, Wenling Li, and Yang Liu. 2026b. “Learning-Based Artificial Potential Field Guidance for Hypersonic Glide Vehicle Penetration.” Aeronautical Journal: 1–25. https://doi.org/10.1017/aer.2026.10218
• Tongmual, Noppakun, and Wannatida Yonwilad. 2025. “Bayesian Bootstrap Confidence Interval for Mean Based on Small Sample Sizes.” Malaysian Journal of Fundamental and Applied Sciences 21 (6): 2937–44. https://doi.org/10.11113/mjfas.v21n6.3479
• Toni, R. 1968. “Theory on the Dynamics of Bag Strip for a Parachute Deployment Aidedby a Pilot Chute.” In 2nd Aerodynamic Deceleration Systems Conference. AIAA 1968-925. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1968-925
• Toomey, R. 1983. “Modernization of the Western Space and Missile Center.” In 2nd Flight Testing Conference. AIAA 1983-2706. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2706
• Torres, Y., L. Stefanini, and D. Suslov. 2009. “Influence of Curvature in Regenerative Cooling System of Rocket Engine.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/200901171
• Toumodge, S. S. 1990. “Target Tracking by a Human Operator.” In Signal and Data Processing of Small Targets 1990. SPIE. https://doi.org/10.1117/12.2321778
• Townsend, Brad. 2020. “Missile Warning.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781003001843-7
• “Tracking Radar.” 1999. In Understanding Radar Systems. Institution of Engineering and Technology. https://doi.org/10.1049/sbra034e_ch3
• Training Camp and Surface-to-Air Firing Range, Romania, Viorel-Eugen Bitan, Valeriu CĂLin, and Romania Training Camp and Surface-to-Air Firing Range. 2017. “Aspects Regarding Safety System in Surface-to-Air Missile Firings.” Scientific Research and Education in the AIR Force 19 (1): 65–70. https://doi.org/10.19062/2247-3173.2017.19.1.6
• Tran, Dinh Hung. 2025. “Synthesis Optimal Guidance Law for Missile in Cruise Phases with Terminal Additional Requires.” International Journal of Advanced Engineering Research and Science 12 (3): 07–15. https://doi.org/10.22161/ijaers.123.2
• “Transition Aerodynamics for Close-Coupled Wing-Canard configurationV/STOL Operations.” 1979. In 17th Aerospace Sciences Meeting. AIAA 1979-336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-336
• Traudt, Tobias. 2024. LUMEN: Liquid Upper Stage Demonstrator Engine: A Versatile Test Bed for Rocket Engine Components: Hot-Fire Test Results. https://doi.org/10.52202/078371-0005
• Treece, Sarah M., Wali Aziz, Bruce A. Jolly, and Christopher Coley. 2024. “Repeatability of Aircraft Store Separation from Unsteady Environments.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4617. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4617
• Trescot, C. D., Jr. 1971. Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control. NASA-TM-X-2367. NASA. https://ntrs.nasa.gov/citations/19710026939
• Trescot, C. D., Jr., G. V. Foster, and C. D. Babb. 1973. Effect of Fin Planform on the Aerodynamic Characteristics of a Wingless Missile with AFT Cruciform Controls at Mach 1.60, 2.36, and 2.86. NASA-TM-X-2774. NASA. https://ntrs.nasa.gov/citations/19730018268
• 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
• Triplet, W. 1983. “Wind Tunnel Correlation Study of Aerodynamic Modeling for F/A-18 Wing-Store Tip-Missile Flutter.” In 24th Structures, Structural Dynamics and Materials Conference. AIAA 1983-1028. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-1028
• 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, 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
• Tsai, Tommy, James Tosh, and Alfred Little. 1999. “Application of Plasma Spray Process in Liquid Propellant Rocket Engine Tip Seals.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2895. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2895
• Tso, G., and R. Lobbia. 1986. “Multimode Guidance in Advanced Air-to-Air Missile Applications.” In Astrodynamics Conference. AIAA 1986-2040. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1986-2040
• 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. 2012. “Robust Autopilot Design for Quasilinear Parameter- Varying Missile Model.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-2
• Tsourdos, Antonios, Brian White, and L. Bruyere. 2012. “Polynomial Approach for Design and Robust Analysis of Lateral Missile Control.” In Control Series. CRC Press. https://doi.org/10.1201/b12503-3
• Tu, Eugene. 1992. “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. 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, 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
• Tucker, Warren A. 1948a. Characteristics of Thin Triangular Wings with Constant-Chord Full-Span Control Surfaces at Supersonic Speeds. NACA-TN-1601. NASA. https://ntrs.nasa.gov/citations/19930082249
• Tucker, Warren A. 1948b. Characteristics of Thin Triangular Wings with Triangular-Tip Control Surfaces at Supersonic Speeds with Mach Lines behind the Leading Edge. NACA-TN-1600. NASA. https://ntrs.nasa.gov/citations/19930082247
• Tucker, Maurice. 1950. Approximate Turbulent Boundary-Layer Development in Plane Compressible Flow along Thermally Insulated Surfaces with Application to Supersonic-Tunnel Contour Correction. NACA-TN-2045. National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. https://ntrs.nasa.gov/citations/19930082700
• Tucker, E., B. Dehoff, and R. McAmis. 1993. “Liquid-Propellant Rocket Engine Testing and Analysis Capabilities.” In 29th Joint Propulsion Conference and Exhibit. AIAA 1993-1861. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-1861
• Tucker, Kevin, Steve Gentz, and Mindy Nettles. 2015a. Advanced Booster Liquid Engine Combustion Stability. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20160008013
• Tucker, P. K., R. J. Kenny, B. R. Richardson, et al. 2015b. Advancing the State-of-the-Practice for Liquid Rocket Engine Injector Design. M15-4313. NASA Marshall Space Flight Center. https://ntrs.nasa.gov/citations/20150016316
• Tucker, Warren A., and Robert L. Nelson. 1948. Theoretical Characteristics in Supersonic Flow of Constant-Chord Partial-Span Control Surfaces on Rectangular Wings Having Finite Thickness. NACA-TN-1708. NASA. https://ntrs.nasa.gov/citations/19930082397
• 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
• Tuyen, Le Dinh. 2025. “Evaluation of Blind-Speed Mitigation and Moving Target Filtering in Surface-to-Air Missile Control Radars.” International Journal of Science Architecture Technology and Environment. https://doi.org/10.63680/ijsate1125012.008
• Tuzlukov, Vyacheslav. 2026a. “Design and Operation of Airborne Radar System Azimuthal Channels and Radar Homing Head.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-12
• Tuzlukov, Vyacheslav. 2026b. “Guidance on Aircraft and Missile. Trajectory Control Algorithms.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-6
• Tuzlukov, Vyacheslav. 2026c. “Multitarget Tracking by Airborne Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408826-2
• Tuzlukov, Vyacheslav. 2026d. “Multitarget Tracking by Multistatic Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408826-6
• Tuzlukov, Vyacheslav. 2026e. “New Generation of Airborne Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-7
• Tuzlukov, Vyacheslav. 2026f. “Noise Immunity under Single-Target Tracking by Airborne Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-15
• Tuzlukov, Vyacheslav. 2026g. “Operational Modes of Airborne Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-8
• Tuzlukov, Vyacheslav. 2026h. “Optimization of Multitarget Tracking Stages by Airborne Radar Systems.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408826-3
• Tuzlukov, Vyacheslav. 2026i. “Optimization of Tactical and Information Airborne Radar System Modes Owing to Trajectory Control by Observation.” In Target Tracking by Airborne Radar Systems. CRC Press. https://doi.org/10.1201/9781003408802-16
• Tvaryanas, Anthony P. 2006. Human Factors Considerations in Migration of Unmanned Aircraft System (UAS) Operator Control. Defense Technical Information Center. https://doi.org/10.21236/ada444925
• Twinting, W., and J. Sponable. 1981. “Spacecraft and Missile Test Discipline.” In 1st Flight Test Conference. AIAA 1981-2376. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-2376
• Úbeda Medina, Luis Antonio. n.d. “Robust Techniques for Multiple Target Tracking and Fully Adaptive Radar = Técnicas Robustas Para Seguimiento De Múltiples Blancos y Radar Adaptativo.” PhD diss., Universidad Politécnica de Madrid. https://doi.org/10.20868/upm.thesis.53209
• Uhlemann, H., and G. Geiser. 1975. “Multivariable Manual Control with Simultaneous Visual and Auditory Presentation of Information.” In NASA. Ames Res. Center 11th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19750025603
• Umholtz, Philip D. 1999. The History of Solid Rocket Propulsion and Aerojet. Defense Technical Information Center. https://doi.org/10.21236/ada406104
• Ünal, A. 2024. “Dual Mode, Imaging Infrared and Semi-Active Laser, Seeker Design with Squinted Combined Diffractive Optical Element.” Journal of Optics 53 (5): 4594–4615. https://doi.org/10.1007/s12596-024-01657-9
• Underwood, Mark, Christopher Rosema, Brett Wilks, James Keenan, and Lamar Auman. 2007. “Recent Improvements to Missile DATCOM.” In 25th AIAA Applied Aerodynamics Conference. AIAA 2007-3936. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-3936
• Unnikrishnan, Nishant, and S. N. Balakrishnan. 2004. “Missile Longitudinal Autopilot Design Using a New Model Following Robust Neuro-Adaptive Controller.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2004-5327. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2004-5327
• Unnikrishnan, Nishant, and S. N. Balakrishnan. 2005. “Dynamic Reoptimization of a Missile Autopilot Controller in Presence of Unmodeled Uncertainties.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2005-6387. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-6387
• Uselton, Bob L., and James C. Uselton. 1975. Test Mechanism for Measuring Pitch-Damping Derivatives of Missile Configurations at High Angles of Attack. Defense Technical Information Center. https://doi.org/10.21236/ada009865
• Vaddi, Sesha. 2006. “Moving Mass Actuated Missile Control Using Convex Optimization Techniques.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6575. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6575
• Vaddi, Sesha, Padmanabhan Menon, and Ernest Ohlmeyer. 2007. “Numerical SDRE Approach for Missile Integrated Guidance: Control.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2007-6672. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-6672
• Vaddi, Sesha, Jimmy Nguyen, Padmanabhan Menon, R. Carter, and S. Perillo. 2009. “Data Mining and Knowledge Discovery from Store Separation Trajectories.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2009-5732. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-5732
• Vadera, Atticus J. 2019. “Liquid Rocket Engine Torch Igniter Feed System.” In AIAA Propulsion and Energy 2019 Forum. AIAA 2019-3860. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-3860
• Vaeth, James Edward. n.d. “Guidance and Control Design Guides and Nonlinearity Considerations for High Performance Boost Vehicles.” PhD diss., Drexel University. https://doi.org/10.17918/00003723
• Vairavan, A., and Ashwini Ratnoo. 2017. “A Non-Switching Guidance Law for Impact Angle Constrained Interception of Moving Targets.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2017-1508. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1508
• Valenzuela, René, Pierre Dersin, and Carole Saint-Ellier. 2019. “New Method for Reliability Demonstration Test.” In Proceedings of the 29th European Safety and Reliability Conference (ESREL). Research Publishing Services. https://doi.org/10.3850/978-981-11-2724-3_0619-cd
• Valler, H. W. 1979. Performance of a Transpiration-Regenerative Cooled Rocket Thrust Chamber. NASA-CR-159742. NASA. https://ntrs.nasa.gov/citations/19800005932
• van de Merwe, Koen, Steven Mallam, and Salman Nazir. 2022. “Agent Transparency, Situation Awareness, Mental Workload, and Operator Performance: A Systematic Literature Review.” Human Factors: The Journal of the Human Factors and Ergonomics Society 66 (1): 180–208. https://doi.org/10.1177/00187208221077804
• Van Der Maas, C. J. 1962. High Altitude Wind Response of Missile Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0408258
• Van Dierendonck, Albert John. n.d. “Modeling Nonstationary Random Processes with an Application to Gyro Drift Rate.” PhD diss., Iowa State University, Digital Repository. https://doi.org/10.31274/rtd-180816-774
• Van Kesteren, Menno W., Marc Naeije, Barry T. Zandbergen, and Arnaud J. Van Kleef. 2014. “Cost and Peformance Advantages of a Dedicated Air Launched Vehicle for Nanosatellites.” In AIAA SPACE 2014 Conference and Exposition. AIAA 2014-4271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-4271
• Van Orden, K. F. 2001. Monitoring Moment-to-Moment Operator Workload Using Task Load and System-State Information. Defense Technical Information Center. https://doi.org/10.21236/ada390275
• Vanlunteren, A. 1977. “Parameter Estimation in a Human Operator Describing Function Model for a Two-Dimensional Tracking Task.” In MIT Proc., 13th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19790009310
• Vareille, Jean, Philippe Le Parc, and Lionel Marcé. 2007. “Web Remote Control of Mechanical Systems: Delay Problems and Experimental Measurements of Round Trip Time.” In Lecture Notes in Control and Information Sciences. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-49556-7_7
• Varma, S. Aditya, and Mangal Kothari. 2018. “A 3D Pitch and Impact-Angle Constrained Guidance Scheme.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233 (5): 1571–84. https://doi.org/10.1177/0954410018757239
• Varma, S. Aditya, Hardik Parwana, and Mangal Kothari. 2016. “A Pitch Controlled Impact-Angle-Constrained Guidance Law for Surface-to-Surface Missiles.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2016-2114. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-2114
• Vasile, Joseph D. 2019. “Effect of Tail Fin Geometry on the Induced Roll of a Canard-Controlled, Subsonic Projectile.” In AIAA Scitech 2019 Forum. AIAA 2019-0598. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0598
• 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
• Vaughn, R. S. 1960. Report on Test Methods for the Single Degree of Freedom Integrating Rate Gyro, Phase 1: Gyro Characteristics. Defense Technical Information Center. https://doi.org/10.21236/ad0283244
• 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
• Vaughn, Milton, and Lamar Auman. 2002. “A Productivity-Oriented Application of Computational Fluid Dynamics to the Design of a Hypervelocity Missile.” In 20th AIAA Applied Aerodynamics Conference. AIAA 2002-2937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-2937
• Vaughn, Milton, and Lamar Auman. 2003. “Assessment of a Productivity-Oriented CFD Methodology for Designing a Hypervelocity Missile.” In 21st AIAA Applied Aerodynamics Conference. AIAA 2003-3937. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-3937
• Vaughn Jr. and Milton E. 2008. The Aerodynamic Influence of a Helicopter on a Jettisoned Missile. Defense Technical Information Center. https://doi.org/10.21236/ada476434
• 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
• Venkatachari, Balaji Shankar, Michael Mullane, Gary Cheng, and Chau-Lyan Chang. 2015. “Numerical Study of Counterflowing Jet Effects on Supersonic Slender-Body Configurations.” In 33rd AIAA Applied Aerodynamics Conference. AIAA 2015-3010. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-3010
• Venkateswaran, Sankaran, Jeffrey Grenda, and Charles Merkle. 1991. “Computational Fluid Dynamic Analysis of Liquid Rocket Combustion Instability.” In 10th Computational Fluid Dynamics Conference. AIAA 1991-1609. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-1609
• Venkateswaran, S., and C. L. Merkle. 1996. “Combustion Processes in Hybrid Rocket Engines.” In Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology. https://ntrs.nasa.gov/citations/19960029278
• Ventrice, M., J. Fang, and K. Purdy. 1979b. “Simulation of Liquid Propellant Rocket Engine Combustion Instabilities.” In 17th Aerospace Sciences Meeting. AIAA 1979-156. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-156
• Venukumar, Balla, G. Jagadeesh, and K. P. J. Reddy. 2006. “Counterflow Drag Reduction by Supersonic Jet for a Blunt Body in Hypersonic Flow.” Physics of Fluids 18 (11): 118104. https://doi.org/10.1063/1.2401623
• Veres, Joseph P. 1992. “A Survey of Instabilities within Centrifugal Pumps and Concepts for Improving the Flow Range of Pumps in Rocket Engines.” In 1992 JANNAF Propulsion Meeting. https://ntrs.nasa.gov/citations/19920009038
• Vergez, P. 1982. “Target Acceleration Modeling for Tactical Missile Guidance.” In 20th Aerospace Sciences Meeting. AIAA 1982-370. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-370
• Verma, Akash, Abhishek Kanaskar, and Kiran Akella. 2019. “Launch Dynamics of a Canisterised Missile.” In 31st International Symposium on Ballistics. DEStech Publications, Inc. https://doi.org/10.12783/ballistics2019/33141
• Verstraete, D., D. Bizzarri, and P. Hendrick. 2009. “In-Flight Oxygen Collection for a Two-Stage Air-Launch Vehicle: Integration of Vehicle and Separation Cycle Design.” In Progress in Propulsion Physics. EDP Sciences. https://doi.org/10.1051/eucass/20091551
• Vertes, M. A., J. E. Oxley, and S. Cohen. 1966. High Rate (5 Minute) Missile Battery Program. Defense Technical Information Center. https://doi.org/10.21236/ad0484265
• Vertut, Jean, and Philippe Coiffet. 1985. “Performance Evaluation of Teleoperation Systems.” In Teleoperation and Robotics. Springer Netherlands. https://doi.org/10.1007/978-94-011-6103-9_4
• Veselic, Sebastijan, Claudio Zito, and Dario Farina. 2020. “Human-Robot Interaction with Robust Prediction of Movement Intention Surpasses Manual Control.” Preprint, bioRxiv. https://doi.org/10.1101/2020.12.09.416735
• Vetter, Ronald F. 1977. Reduction of Fuel Fire Cook-Off Hazard of Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/adb020024
• Vichnyakova, L., and V. Kukhtenko. 1998. “Concept Definition of Surface-to-Air Missile Systems and Their Subsystems on the Basis of Mathematical Modeling.” In Guidance, Navigation, and Control Conference and Exhibit. AIAA 1998-4419. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-4419
• Vickers, William W., and Manuel E. López. 1975. “Low-Angle Radar Tracking Errors Induced by Nonstratified Atmospheric Anomalies.” Radio Science 10 (5): 491–505. https://doi.org/10.1029/rs010i005p00491
• Vigdorovich, Igor. 2025. “Supersonic Turbulent Boundary Layer on a Plate. Universal Velocity and Temperature Defect Laws and Skin-Friction Law at Moderate Free-Stream Mach Numbers.” Journal of Fluid Mechanics 1020: A17. https://doi.org/10.1017/jfm.2025.10634
• Vishnyak, A. 1995. “Parachute Simulations for ARIANE-5 Booster Recovery System Design.” In 13th Aerodynamic Decelerator Systems Technology Conference. AIAA 1995-1593. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1593
• Vishnyakova, L., and V. Kukhtenko. 1996. “Systems Analysis Methods Development in Surface-to-Air Missile System Design Problem with Uncertain Conditions of Its Application.” In Guidance, Navigation, and Control Conference. AIAA 1996-3804. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3804
• Vishwanath, Manish. 2023. “Embedded Tracking System Design Reduces Human Effort in Optical Tracking of Anti-Tank Guided Missile Targets.” Preprint, . https://doi.org/10.31219/osf.io/b2nwp
• Viventi, R. E. 1961. Fabrication of Pyrolytic Graphite Rocket Nozzle Components. Defense Technical Information Center. https://doi.org/10.21236/ad0263599
• Viviani, Paolo, Paola Campadelli, and Pierre Mounoud. 1987. “Visuo-Manual Pursuit Tracking of Human Two-Dimensional Movements.” Journal of Experimental Psychology: Human Perception and Performance 13 (1): 62–78. https://doi.org/10.1037/0096-1523.13.1.62
• Voisinet, R. 1979. “Combined Influence of Roughness and Mass Transfer on Turbulent Skin Friction at Mach 2.9.” In 17th Aerospace Sciences Meeting. AIAA 1979-3. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1979-3
• Von Eckartsberg, Nico, Gabriel Goldman, and Jesus Sanchez. 2025. Validation of Regenerative Cooling Design Tool through Development and Test of a Liquid Rocket Engine. https://doi.org/10.52202/083090-0116
• Voronin, V. I., and A. I. Shvets. 1984. “Optimizing the Aerodynamic Characteristics of Λ-Shaped Wings at Supersonic Flight Velocities.” Fluid Dynamics 19 (5): 787–91. https://doi.org/10.1007/bf01093549
• Vujcic, Doug, and Kerry Kachejian. 2000. Combat Cueing: Geolocation System for Low Probability of Intercept Signals. Defense Technical Information Center. https://doi.org/10.21236/ada383452
• Vukelich, S., and J. Jenkins. 1981. “Evaluation of the State-of-the-Art in Missile Aerodynamic Prediction.” In 7th Atmospheric Flight Mechanics Conference. AIAA 1981-1893. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1893
• Vukelich, S., and J. Jenkins. 1983. “Missile Datcom Status Report: Body and Fin Alone Methodology.” In 21st Aerospace Sciences Meeting. AIAA 1983-181. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-181
• Waddell, M. C. 1961. Surface-to-Air Guided Missile Systems Methods of Tactical Analysis. Defense Technical Information Center. https://doi.org/10.21236/ad0258634
• Wadel, Mary, and Mary Wadel. 1997. “Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber.” In 33rd Joint Propulsion Conference and Exhibit. AIAA 1997-2913. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2913
• Wadia, A., and D. Wilson. 1981. “Component Design and Performance Evaluation of a Liquid Propellant Rocket Engine for Earth Orbital Satellite Launching.” In 17th Joint Propulsion Conference. AIAA 1981-1372. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1981-1372
• Waesche, R. H. Woodward, and Martin Summerfield. 1965. Solid Propellant Combustion Instability: Oscillatory Burning of Solid Rocket Propellants. Defense Technical Information Center. https://doi.org/10.21236/ad0634278
• Wagner, W. R., and J. M. Shoji. 1975. “Advanced Regenerative-Cooling Techniques for Future Space Transportation Systems.” In Propulsion Conference. https://ntrs.nasa.gov/citations/19760027303
• Wagner, W. R., and B. J. Waldman. 1973. Regeneratively Cooled Rocket Engine for Space Storable Propellants. NASA-CR-133915. NASA. https://ntrs.nasa.gov/citations/19730022956
• Walker, P. B. 1955. “The Structural Effects of Kinetic Heating in Supersonic Flight.” Journal of the Royal Aeronautical Society 59 (537): 581–86. https://doi.org/10.1017/s036839310011689x
• Waller, R. A. 1977. Bayesian Zero-Failure (BAZE) Reliability Demonstration Testing Procedure for Components of Nuclear Reactor Safety Systems. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/7309479
• 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
• 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
• Wan, Jing, Qian Wang, and Jianliang Ai. 2012. “Dynamic Inversion-Based Control System of a Hypersonic Vehicle with Model Uncertainty.” In 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2012-5965. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-5965
• Wang, Chunpeng. n.d. “Low Impedance Robotic Manipulator Control and Stable Teleoperation for Robot Learning.” PhD diss., Northeastern University. https://doi.org/10.17760/d20669671
• Wang, Chi-Rong. 1993. “Supersonic Boundary-Layer Flow Turbulence Modeling.” In International Conference on Near-Wall Turbulence Flows. https://ntrs.nasa.gov/citations/19930005569
• Wang, Zhongwen. 1999. “Investigation of Parachute Deployment Assembly for Drones.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1722. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1722
• Wang, Ten-See. 2008. “Transient Three-Dimensional Startup Side Load Analysis of a Regeneratively Cooled Nozzle.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20080033098
• Wang, Hongbin. 2010. Exploring the Effectiveness of Attention Manipulations on Operator Performance in C2 Tasks: Empirical Investigations. Defense Technical Information Center. https://doi.org/10.21236/ada563621
• Wang, Xinyu. 2015b. “Backstepping Synchronous Control of Simplified Supersonic Missile.” International Journal of Hybrid Information Technology 8 (12): 327–48. https://doi.org/10.14257/ijhit.2015.8.12.25
• Wang, Zhenbo. 2019. “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, 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, Ziwei. 2026. “Constraint Control of Teleoperation with Prescribed Performance.” In Human-Machine Interfaces in Medical Robotics. Elsevier. https://doi.org/10.1016/b978-0-44-313723-5.00012-5
• Wang, Sen, Qinglong Bao, and Jiameng Pan. 2021e. “Improved Probability Hypothesis Density Filter for Multi-Target Tracking of Non-Cooperative Bistatic Radar.” IET Radar, Sonar & Navigation 16 (3): 426–36. https://doi.org/10.1049/rsn2.12193
• Wang, Shuliang, Daping Bi, Huailin Ruan, and Shiwa Chen. 2019a. “Cognitive Structure Adaptive Particle Filter for Radar Manoeuvring Target Tracking.” IET Radar, Sonar & Navigation 13 (1): 23–30. https://doi.org/10.1049/iet-rsn.2018.5043
• Wang, Ten-See, Francisco Canabal, Yen-Sen Chen, Gary Cheng, and Yasushi Ito. 2013b. “Thermal Hydraulics Design and Analysis Methodology for a Solid-Core Nuclear Thermal Rocket Engine Thrust Chamber.” In InTech eBooks. https://doi.org/10.5772/52569
• Wang, Xichen, Huiliang Cao, and Xiaomin Duan. 2021a. “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, Dong, and Yun Chen. 2021. “Systematic Approach of Guidance Information Reconstruction of Laser Strapdown Guidance Air-to-Ground Missile.” Journal of Physics: Conference Series 1721 (1): 012066. https://doi.org/10.1088/1742-6596/1721/1/012066
• Wang, Chen, Xiaobo Feng, Wentao Zhang, and Xiaoxiong Zhou. 2019e. “Research on Pulse Compression Radar Angular Glint Modelling and Suppression.” Journal of Engineering 2019 (21): 7658–61. https://doi.org/10.1049/joe.2019.0618
• Wang, Hao, and Xiao Guang Gao. 2012. “A Midcourse Guidance Method of Long Range Air-to-Air Anti-Radiation Missile.” Advanced materials research 433-440: 7106–11. https://doi.org/10.4028/www.scientific.net/amr.433-440.7106
• Wang, Xin, Junjie Gong, and Yuxin Wang. 2023f. “Research on Optimal Guidance Law with Landing Angle Constraint, 79-85.” Mechatronic Systems and Control 51 (2). https://doi.org/10.2316/j.2023.201-0281
• Wang, Shuai, Guoqiang He, and Fei Qin. 2019f. “Research on Skin-Friction Drag Reduction by Hydrogen Injection in Supersonic Boundary Layer.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37 (3): 449–56. https://doi.org/10.1051/jnwpu/20193730449
• Wang, Shuai, Guo-qiang He, Fei Qin, Xiang-geng Wei, and Zhiwei Huang. 2017b. “Numerical Investigation of Skin-Friction Reduction in a Supersonic Channel.” In 21st AIAA International Space Planes and Hypersonics Technologies Conference. AIAA 2017-2324. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-2324
• Wang, Haibo, Wenhua Huang, Tao Ba, Yuchuan Zhang, and Haichuan Zhang. 2025a. “Hierarchical Matching Maximum Likelihood Estimation for Digital-Array Monopulse Tracking Radar.” Progress In Electromagnetics Research C 156: 195–200. https://doi.org/10.2528/pierc25031004
• Wang, Haibo, Wenhua Huang, Yue Jiang, and Tao Ba. 2018b. “Maximum Likelihood Method and Cramer-Rao Low Bound of Angle Estimation for Wide-Band Monopulse Radar.” Progress In Electromagnetics Research C 85: 209–19. https://doi.org/10.2528/pierc18042510
• Wang, Jiaxuan, Xiaoduo Li, Liang Han, Haoyang Yu, and Zhang Ren. 2024e. “Guidance Strategy for Hypersonic Glide Vehicle with Additional Angular Error Approach.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-3340-8_50
• Wang, Xinchun, Yongqiang Li, He Qi, and Kaiwei Chen. 2024c. “Decoupling Control Method for Roll Missile Based on Active Disturbance Rejection Technology.” In Proceedings of the 2024 4th International Conference on Artificial Intelligence, Automation and Algorithms. ACM. https://doi.org/10.1145/3700523.3700552
• Wang, Qi, Zhizhong Liao, and Fei Yan. 2021d. “Guidance Information Estimation for Strapdown Imaging Seeker of Tactical Missile Guided by Optimal Guidance Law.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-7423-5_89
• 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, Shuo, Yu Liu, Xuan Wang, Zechen Liu, Xuqun You, and Yuan Li. 2024j. “Where Is the Function Allocation Boundary? The Effect of Degree of Automation on Attention Allocation and Human Performance under Different Reliabilities.” Human Factors: The Journal of the Human Factors and Ergonomics Society 67 (8): 757–75. https://doi.org/10.1177/00187208241311808
• Wang, Jianan, Xiaole Peng, and Zhihao Wang. 2022i. “Research on Line of Sight Angular Rate Estimation of Strapdown Seeker.” In Fifth International Conference on Mechatronics and Computer Technology Engineering (MCTE 2022), edited by Dalin Zhang. SPIE. https://doi.org/10.1117/12.2660853
• 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, Xu Gang, and Jing Qin. 2011. “Motion Coupling Analysis for the Nose and Body of the Deflectable Nose Missile.” Applied Mechanics and Materials 66-68: 260–63. https://doi.org/10.4028/www.scientific.net/amm.66-68.260
• Wang, Wangzhi, Manrong She, Shanguang Chen, and Zhizhong Li. 2024f. “Identification of Factors for Dynamic Function Allocation from the Perspective of Human Information Processing.” AHFE international. https://doi.org/10.54941/ahfe1004859
• Wang, Bu-Yun, Wei-Dong Sun, Shi-Fan Wu, and Rui Guo. 2020. “Intelligent Safety Control Assistant Decision-Making System of Missile Flight Test.” DEStech Transactions on Computer Science and Engineering, no. cmso. https://doi.org/10.12783/dtcse/cmso2019/33614
• Wang, Liwu, Mingzhang Tang, Yu Liu, and Sijun Zhang. 2021c. “Fluid-Structure Interaction Simulations of Parachute Deployment and Inflation.” In Volume 1: Aerospace Engineering Division Joint Track; Computational Fluid Dynamics. American Society of Mechanical Engineers. https://doi.org/10.1115/fedsm2021-65583
• Wang, Jianan, Xizi Tao, Wei Dong, Huixia Wang, and Chunyan Wang. 2023c. “A Modified Finite-Time Guidance Law with Impact Angle Constraint.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_682
• 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, Xianghua, and Jinzhi Wang. 2014b. “Partial Integrated Guidance and Control with Input Constraints and Impact Angle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2014-1473. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2014-1473
• Wang, Jie, Dinghua Wang, Ting Wang, and Yanpeng Hu. 2024b. “Collision Avoidance and Formation Control of Hypersonic Glide Vehicles within Predefined Time.” SCIENTIA SINICA Informationis 54 (10): 2326. https://doi.org/10.1360/ssi-2024-0128
• Wang, Jianquan, Long Wang, Jinwei Zhao, Xinlu Guo, and Kai Liu. 2023d. “An Online Proportional Guidance Midcourse Guidance Method for near Space Targets Based on Air-Breathing Hypersonic Platform.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_587
• Wang, Zhuo, Shen-Peng Wu, Tao Wang, and Bo Zhang. 2019g. “Stability Analysis and Experimental Study of Portable Missile Control Device Test.” Journal of Physics: Conference Series 1314 (1): 012036. https://doi.org/10.1088/1742-6596/1314/1/012036
• Wang, Qiuwang, Feng Wu, Min Zeng, Laiqin Luo, and Jiguo Sun. 2006b. “Numerical Simulation and Optimization on Heat Transfer and Fluid Flow in Cooling Channel of Liquid Rocket Engine Thrust Chamber.” Engineering Computations 23 (8): 907–21. https://doi.org/10.1108/02644400610707793
• Wang, Hongguang, Zhensen Wu, and Qinglin Zhu. 2013a. “Influence Analysis of Atmospheric Refraction on Low-Angle Radar Tracking Errors.” JOURNAL OF ELECTRONICS INFORMATION TECHNOLOGY 34 (8): 1893–96. https://doi.org/10.3724/sp.j.1146.2011.01186
• Wang, Qingquan, Hang Yu, and Carlos Pantano. 2022k. “Structural Simulations of Conical Ribbon Parachute Deployment with a New Detailed Fabric Contact Algorithm, Reefing Line Interactions and Suspension Line Dynamics.” In 26th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2022-2702. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2702
• Wang, Pei, Ke Zhang, and Cong Nie. 2014b. “Research on Line-of-Sight Rate Estimation of Strapdown Seeker.” Applied Mechanics and Materials 556-562: 3739–44. https://doi.org/10.4028/www.scientific.net/amm.556-562.3739
• Wang, Liang, Weihua Zhang, Donghui Wang, Ke Peng, and Huabo Yang. 2017a. “Command Filtered Back-Stepping Missile Integrated Guidance and Autopilot Based on Extended State Observer.” Advances in Mechanical Engineering 9 (11): 168781401773325. https://doi.org/10.1177/1687814017733251
• Wang, Jie, Shu-lun Zhao, Fu-tao Zhu, Jia-xu Chen, En-yi Guan, and Zhu-shun Ding. 2016g. “WSN Data Link Based Cooperative Combat Model of Multi-Missile Formation.” In Wireless Communication and Sensor Network. WORLD SCIENTIFIC. https://doi.org/10.1142/9789813140011_0065
• Wang, Ting, Dekun Zheng, Liang Li, and Kurosh Madani. 2022h. “A Novel Grasping Teleoperation Control for Dual-Handed Teleoperation System.” Preprint, . https://doi.org/10.2139/ssrn.4312455
• Wang Jun, Yao Jian, and Qiao Xiaolin. 2009. “A Practical Approach of Monopulse DOA Estimation for Multiple Unresolved Targets.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0427
• Ward, G. N. 1950. “The Supersonic Flow past a Slender Ducted Body of Revolution with an Annular Intake.” Aeronautical Quarterly 1 (4): 305–18. https://doi.org/10.1017/s0001925900000214
• 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
• Wardlaw, A., Jr., F. Baltakis, F. Martin, F. Priolo, and R. Jettmar. 1985. “Godunov’s Method for Supersonic Tactical Missile Computations.” In 12th Atmospheric Flight Mechanics Conference. AIAA 1985-1812. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1985-1812
• Wardlaw, A., Jr., J. Solomon, and F. Baltakis. 1980. “Supersonic Inviscid Flow Field Computations of Missile Type Bodies.” In 18th Aerospace Sciences Meeting. AIAA 1980-271. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1980-271
• Ware, J. R. 1972. “An Input Adaptive, Pursuit Tracking Model of the Human Opertor.” In NASA, Washington 7th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19730001381
• Warsi, Z. U. 1986. Generation of Surface Grids through Elliptic Partial Differential Equations for Aircraft and Missile Configurations. Defense Technical Information Center. https://doi.org/10.21236/ada172867
• Washington, W. 1983. “Experimental Investigation of Rolling Moment for a Body-Wing-Tail Missile Configuration with Wrap around Wings and Straight Tails at Supersonic Speeds.” In 10th Atmospheric Flight Mechanics Conference. AIAA 1983-2081. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2081
• Washington, William, and Mark Miller. 1993. “Grid Fins: A New Concept for Missile Stability and Control.” In 31st Aerospace Sciences Meeting. AIAA 1993-35. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-35
• 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
• Washizu, K., K. Tanaka, and T. Osawa. 1978. “A Study of the Effect of Forcing Function Characteristics on Human Operator Dynamics in Manual Control.” In NASA. Ames Res. Center The 14th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19790007419
• Wasilewski, A., A. Rogala, and M. Magier. 2025. “Application of Tracking Doppler Radar in Missile Fragments Velocity Measurement after Mid-Air Detonation.” In Ballistics 2025. Destech Publications, Inc. https://doi.org/10.12783/ballistics25/37103
• Waters, Eric D., Dennis M. Creech, and Alan Philips. 2013. Air Launch: Examining Performance Potential of Various Configurations and Growth Options. M13-2553. Jacobs Technology, Inc. https://ntrs.nasa.gov/citations/20140003196
• Watkins, Charles E. 1946. Paths of Target Seeking Missiles in Two Dimensions. ATI No. 4831. National Advisory Committee for Aeronautics. Langley Aeronautical Lab. https://ntrs.nasa.gov/citations/20090033671
• 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
• 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
• Waye, Donald. 1991. “Design and Performance of a Parachute for the Recovery of a 760-Lb Payload.” In 11th Aerodynamic Decelerator Systems Technology Conference. AIAA 1991-882. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-882
• Webb, William. 1979. Sources of Tracking Error in Millimeter Wavelength Missile Guidance Systems. Defense Technical Information Center. https://doi.org/10.21236/ada078226
• Wei, R., B-H. Che, C-B. Sun, J. Zhang, and Y-Q. Lu. 2018. “A Three Degree of Freedom Manipulator Used for Store Separation Wind Tunnel Test.” IOP Conference Series: Materials Science and Engineering 372: 012035. https://doi.org/10.1088/1757-899x/372/1/012035
• Wei, Fu-Shang, and Jens Gjestvang. 2001. “Store Separation Analysis of the Penguin Missile from the SH-2G Helicopter.” In 39th Aerospace Sciences Meeting and Exhibit. AIAA 2001-992. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-992
• Wei, Qiushuo, Feng Zha, and Lubin Chang. 2022. “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, Shijun, Guang Zhai, and Yiyong Sun. 2026. “Tracking Hypersonic Glide Vehicles Using an Adaptive Latent Force Model.” Preprint, . https://doi.org/10.2139/ssrn.6944778
• Weibing, Hu, and Zhu Kuisheng. 2006. “Semi-Active Control Wind Tunnel Tests of Wing/Store System Flutter with an Electro-Magnetic Damper.” Multidiscipline Modeling in Materials and Structures 2 (2): 221–26. https://doi.org/10.1163/157361106776240833
• Weidlinger, Paul. 1962. “The Lethal Radius of a Salvo.” Operations Research 10 (4): 547–58. https://doi.org/10.1287/opre.10.4.547
• Weiss, Martin, and David Beld. 2006. “Higher Order Statistics and the Adjoint Method for Guidance Loop Analysis.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6439. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6439
• Wells, Lawrence L. 1981. “Real-Time Missile Tracking with GPS.” Navigation 28 (3): 224–30. https://doi.org/10.1002/j.2161-4296.1981.tb00770.x
• 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
• Welsh, C. J. 1985. Test Fixture Effects in Vibration Tests of Rocket Motors. Defense Technical Information Center. https://doi.org/10.21236/ada161403
• Welterlen, Tracy. 1999. “Store Release Simulation on the F/A-18C Using Splitflow.” In 37th Aerospace Sciences Meeting and Exhibit. AIAA 1999-124. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-124
• Welterlen, Tracy. 2000. “Weapons Bay Flow Field Simulation.” In 18th Applied Aerodynamics Conference. AIAA 2000-3926. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-3926
• Welton, D., M. Bensky, and J. Hiland. 1963. “Variable-Thrust Liquid Propellant Rocket Engines.” In Summer Meeting. AIAA 1963-268. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1963-268
• Wempe, T. E. 1976. Twelfth Annual Conference on Manual Control. NASA-TM-X-73170. NASA. https://ntrs.nasa.gov/citations/19770007802
• Wernet, Mark, Randy Locke, Adam Wroblewski, and Anita Sengupta. 2009. “Application of Stereo PIV on a Supersonic Parachute Model.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-70. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-70
• Werrell, Kenneth P. 1985b. The Evolution of the Cruise Missile. Defense Technical Information Center. https://doi.org/10.21236/ada162646
• Wexler, Omer, and Moshe Idan. 2026. “A Pointwise Minimum Norm Control Scheme for a Generic Air-Breathing Hypersonic Vehicle with State Constraints.” In 27th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2026-5048. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2026-5048
• 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
• Whalley, Ian A. 2024. “Reliability Estimation for Explosive Devices, with Zero Failures, in Series and Parallel Systems – a Comparison of Methods.” In AIAA SCITECH 2024 Forum. AIAA 2024-2160. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2160
• Wherry, Robert J. 1976. “The Human Operator Simulator — HOS.” In Monitoring Behavior and Supervisory Control. Springer US. https://doi.org/10.1007/978-1-4684-2523-9_23
• 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, Frank M., and George H. Christoph. 1972. Rapid Engineering Calculation of Two-Dimensional Turbulent Skin Friction. Defense Technical Information Center. https://doi.org/10.21236/ad0757872
• 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 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
• White Sands Missile Range Nm. 2002. Test Operations Procedure (TOP) 5-2-582. Temperature-Altitude Tests for Missile System and Missile Subsystem Equipment. Defense Technical Information Center. https://doi.org/10.21236/ada399178
• Whiteman, Leopold A. 2003. “Integrating Commercial off the Shelf Packages (COTS) into Guided Missile Systems: The EMMA Program.” SMTA International 5 (1): 337–51. https://doi.org/10.37665/smjzvxe69592
• 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
• Wickens, Christopher D., Justin G. Hollands, Simon. Banbury, and Raja. Parasuraman. 2015. “Spatial Cognition, Navigation, and Manual Control.” In Psychology Press eBooks. https://doi.org/10.4324/9781315665177-11
• Wideman, Jeffrey, John Miles, James Brown, and Oktay Ozcan. 1994. “Skin-Friction Measurements in a 3-D, Supersonic Shock-Wave/boundary-Layer Interaction.” In 32nd Aerospace Sciences Meeting and Exhibit. AIAA 1994-314. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-314
• Widgery, M. P. 2017. “Development of a Ballistic Missile Defence Capability for the SAMPSON Multi-Function Radar on UK Type 45.” In International Conference on Radar Systems (Radar 2017). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2017.0445
• Wiegand, James H. 1961. Study of Mechanical Properties of Solid Rocket Propellant. Defense Technical Information Center. https://doi.org/10.21236/ad0258883
• Wierwille, W. W. 1965. A Theory for Optimal Deterministic Characterization of Time-Varying Human Operator Dynamics. NASA. https://ntrs.nasa.gov/citations/19650039329
• Wieseneck, H. C. 1970. Regenerative Cooling of the Space Shuttle Engine. Rockwell International Corp. https://ntrs.nasa.gov/citations/19700030313
• Wightman, D. C., and G. Lintern. 1983. Part-Task Training of Tracking in Manual Control. Defense Technical Information Center. https://doi.org/10.21236/ada138346
• Wightman, Dennis C., and Gavan Lintern. 1985. “Part-Task Training for Tracking and Manual Control.” Human Factors: The Journal of the Human Factors and Ergonomics Society 27 (3): 267–83. https://doi.org/10.1177/001872088502700304
• Wightman, Dennis C., and Gavan Lintern. 2017. “Part-Task Training for Tracking and Manual Control.” In Routledge eBooks. Routledge. https://doi.org/10.4324/9781315243092-14
• Wijlens, Rowenna, Peter Zaal, and Daan M. Pool. 2020. “Retention of Manual Control Skills in Multi-Axis Tracking Tasks.” In AIAA Scitech 2020 Forum. AIAA 2020-2264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2020-2264
• Wilcox, Brian. 2001. “Miniature Ascent Vehicles Derived from the Navy’s Air-Launched Satellite Developed in 1958.” In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3879. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-3879
• Wilcox, Floyd J., Jr. 1990. “Experimental Measurements of Internal Store Separation Characteristics at Supersonic Speeds.” In Royal Aeronautical Society. https://ntrs.nasa.gov/citations/19930062818
• Wilcox, Floyd, Jr. 1991. “Tangential, Semisubmerged, and Internal Store Carriage and Separation at Supersonic Speeds.” In 29th Aerospace Sciences Meeting. AIAA 1991-198. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1991-198
• Wilcox, Floyd J., Jr., Oktay Baysal, and Robert L. Stallings Jr. 1992. Tangential, Semisubmerged, and Internal Store Carriage and Separation. NASA Langley Research Center. https://ntrs.nasa.gov/citations/19920057216
• Wilkin, D. J., I. Harrison, and M. S. Woolfson. 1991. “Target Tracking Algorithms for Phased Array Radar.” IEE Proceedings F Radar and Signal Processing 138 (3): 255. https://doi.org/10.1049/ip-f-2.1991.0033
• William Ruffles and Sam M. Dakka. 2016. “Aerodynamic Flow Characteristics of Utilizing Delta Wing Configurations in Supersonic and Subsonic Flight Regimes.” Journal of Communication and Computer 13 (6). https://doi.org/10.17265/1548-7709/2016.06.004
• Williams, M. L. 1968. The Chemistry and Mechanics of Combustion with Applications to Rocket Engine Systems. Defense Technical Information Center. https://doi.org/10.21236/ad0847204
• Williams, J. 1982. “Evaluation of Supersonic Missile Aerodynamic Prediction Techniques.” In 20th Aerospace Sciences Meeting. AIAA 1982-390. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1982-390
• Williams, Douglas. 1987. “A Computer-Aided Autopilot Design Procedure for a High Performance Bank-to-Turn Controlled Tactical Missile.” In Guidance, Navigation and Control Conference. AIAA 1987-2580. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1987-2580
• Williams, Forman A. 2004a. Combustion Processes and Instabilities in Liquid-Propellant Rocket Engines. Defense Technical Information Center. https://doi.org/10.21236/ada420091
• Williams, Forman A. 2004b. Fundamental Studies of Liquid-Propellant Rocket Combustion. Defense Technical Information Center. https://doi.org/10.21236/ada425218
• 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, Darryl, Diganta Bhattacharjee, Travis W. Drayna, Matt Bartkowicz, Maziar Hemati, and Graham V. Candler. 2025. “Integrated Guidance and Control of Generic Hypersonic Glide Vehicles Using Computational Fluid Dynamics.” In AIAA SCITECH 2025 Forum. AIAA 2025-0264. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0264
• Williams, D., J. Richman, and B. Friedland. 1983. “Design of an Integrated Strapdown Guidance and Control System for a Tactical Missile.” In Guidance and Control Conference. AIAA 1983-2169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1983-2169
• 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
• Wills, C. F. 1963. Command Systems Department CRT Oscilloscope Display. Defense Technical Information Center. https://doi.org/10.21236/ad0404701
• Willwerth, D. E. 1962. Missile Tumbling Turns. Defense Technical Information Center. https://doi.org/10.21236/ad0847353
• Wilson, D. R. 1970. “Basic Servomechanism Theory.” In Modern Practice in Servo Design. Elsevier. https://doi.org/10.1016/b978-0-08-015812-9.50006-9
• Wilson, K. J., and M. Farrow. 2018. “Assurance for Sample Size Determination in Binomial Reliability Demonstration Testing.” In Proceedings of the 10th IMA International Conference on Modelling in Industrial Maintenance and Reliability. Institute of Mathematics and its Applications. https://doi.org/10.19124/ima.2018.001.30
• 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
• Wing, L. 1970. “Practical Methods for Predicting Aerodynamic Heating Effects on Sounding Rockets.” In 2nd Sounding Rocket Technology Conference. AIAA 1970-1399. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1970-1399
• Wing, L. 1973. “A Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses.” In 3rd Sounding Rocket Technology Conference. AIAA 1973-281. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1973-281
• 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. 1988a. “A Bank-to-Turn Missile Autopilot Design Approach Using LQG/LTR Control Theory.” In 26th Aerospace Sciences Meeting. AIAA 1988-336. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-336
• Wise, Kevin. 1988b. “Optimizing Singular Value Robustness Measures in a Conventional Bank-to-Turn Missile Autopilot Design.” In Guidance, Navigation and Control Conference. AIAA 1988-4089. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-4089
• 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. 2008. “Robust Stability Analysis of Adaptive Missile Autopilots.” In AIAA Guidance, Navigation and Control Conference and Exhibit. AIAA 2008-6999. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6999
• Wise, Kevin, and David Broy. 1996. “Agile Missile Dynamics and Control.” In Guidance, Navigation, and Control Conference. AIAA 1996-3912. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-3912
• 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, Kevin, and Sridhar Kundur. 1993. “Missile Autopilot Robustness to Real and Complex Uncertainties Usinga Parameter Space Robustness Test.” In Guidance, Navigation and Control Conference. AIAA 1993-3738. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3738
• 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
• Witkowski, Allen. 1999. “The Stardust Sample Return Capsule Parachute Recovery System.” In 15th Aerodynamic Decelerator Systems Technology Conference. AIAA 1999-1741. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-1741
• Witkowski, Allen, Mike Kandis, James Reuter, Walter Machalick, Richard Kelsch, and Anita Sengupta. 2009. “Design of Subscale Parachute Models for MSL Supersonic Wind Tunnel Testing.” In 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2009-2999. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2999
• Witkowski, Allen, Larry Williams, and Daniel Hinson. 2022. “Spin Recovery Parachute System for General Aviation Aircraft.” In 26th AIAA Aerodynamic Decelerator Systems Technology Conference. AIAA 2022-2737. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2022-2737
• Witmer, Robert G. 1986. Using the Tank Gunnery and Missile Tracking System (TGMTS) for Measuring Tank Gunnery Performance. Defense Technical Information Center. https://doi.org/10.21236/ada170895
• Wolf, James D. 1978. Crew Workload Assessment. Development of a Measure of Operator Workload. Defense Technical Information Center. https://doi.org/10.21236/ada068616
• Wolf, Dean, and Edward Fallon. 2011. “Development of Parachute Opening Factor (Ck) Models for the Ares I First Stage Parachute Recovery System.” In 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2011-2555. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2555
• Wolfe, Timothy, Kidambi Sreenivas, and James Newman. 2024. “Advances in the Computational Simulation of Weapons Bay Cavities with a Dynamically Opening Door in High-Speed Flow.” In AIAA Aviation Forum and Ascend 2024. AIAA 2024-4615. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-4615
• Wong, K. W. 1979. “Analysis of Combustion Instability in Liquid Fuel Rocket Motors.” PhD diss., Tennessee Technological Univ.. https://ntrs.nasa.gov/citations/19790021057
• Wong, Anthony K., and James Brown. 1965. Malfunction of Igniters in the Amra Variable Parameter Rocket Engine. Defense Technical Information Center. https://doi.org/10.21236/ad0626273
• Wong, Anthony K., and James Brown. 1968. Titanium Carbide Content Effect on Erosion in Cermet Rocket Nozzles. Defense Technical Information Center. https://doi.org/10.21236/ad0681920
• Wong, T., T. Lo, H. Leung, J. Litva, and E. Bosse. 1993. “Low-Angle Radar Tracking Using Radial Basis Function Neural Network.” IEE Proceedings F Radar and Signal Processing 140 (5): 323. https://doi.org/10.1049/ip-f-2.1993.0045
• Wood, John D. 1961. Survey on Missile Structural Dynamics,. Defense Technical Information Center. https://doi.org/10.21236/ad0421632
• Wooden, Perry, W. Brooks, and Jubaraj Sahu. 1998. “Calibrating CFD Predictions for Use in Multiple Store Separation Analysis.” In 36th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 1998-754. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-754
• Woodward, Kenneth E. 1961. Lower Cost Packaging for Guided Missile Electronics. Defense Technical Information Center. https://doi.org/10.21236/ad0255658
• Woodward, R. H., and Martin Summerfield. 1966. Research on Solid Propellant Combustion Instability. Defense Technical Information Center. https://doi.org/10.21236/ad0629585
• Wozney, Clayton Edward. 2021. “Comparison of Solid Rocket Motor Thrust Modulation Technique.” Preprint, Toronto Metropolitan University. https://doi.org/10.32920/ryerson.14646417.v1
• Wrestler Jr. and Clifton G. 1965. Analytic Study of Aircraft Agility in the Turnaround Maneuver. Defense Technical Information Center. https://doi.org/10.21236/ad0622404
• Wright, T. W. 1882. “On the Computation of Probable Error.” Analyst 9 (3): 74. https://doi.org/10.2307/2636012
• Wu, Tongde. n.d. “Missile Guidance Law Design with Impact Angle Constraint Based on SDRE Scheme.” PhD diss., University of Missouri–Columbia. https://doi.org/10.32469/10355/67744
• Wu, S. L., and S. J. Hou. 2009. “Detection and Tracking Method of Echo Signal for Miss-Distance Measurement.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0439
• Wu, Chunjiang, Qinglei Hu, and Tuo Han. 2025a. “Hyperbola-Like Impact Angle Guidance Law with Reduced Look Angle Variation.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2232-0_7
• Wu, Zhaodong, Shengliang Hu, Yasong Luo, and Xiang Li. 2021. “Optimal Distributed Cooperative Jamming Resource Allocation for Multi-Missile Threat Scenario.” IET Radar, Sonar & Navigation 16 (1): 113–28. https://doi.org/10.1049/rsn2.12168
• Wu, Jianjun, Yuwei Liu, Yuqiang Cheng, Shuming Yang, and Yang Li. 2026b. “Liquid-Propellant Rocket Engine Health Monitoring Technologies: A Survey, Insights, and Prospects.” Progress in Aerospace Sciences 166: 101251. https://doi.org/10.1016/j.paerosci.2026.101251
• Wu, Feng, Qiuwang Wang, Laiqin Luo, Hiroyuki Ozoe, and Jiguo Sun. 2003. “303 Numerical Simulation on Heat Transfer and Fluid Flow in Cooling Channel of Liquid Rocket Engine Thrust Chamber.” Proceedings of The Computational Mechanics Conference 2003.16 (0): 177–78. https://doi.org/10.1299/jsmecmd.2003.16.177
• Wu, Xiao-tian, Xing Wang, Jin-heng Yang, and Xiang Zhang. 2018a. “Air-to-Air Missile Tracking and Guidance Law Identification Based on CKF.” In Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017). Atlantis Press. https://doi.org/10.2991/macmc-17.2018.64
• Wu, Da Fang, Shuang Wu, Yuewu Wang, Zhen Tong Gao, and Jia Ling Yang. 2013b. “Rapid High-Precision Non-Linear Calibration for Temperature Sensors in Transient Aerodynamic Heating Simulation Systems.” Applied Mechanics and Materials 321-324: 618–23. https://doi.org/10.4028/www.scientific.net/amm.321-324.618
• Wu, Dafang, Shuang Wu, Yuewu Wang, Zhentong Gao, and Jialing Yang. 2014b. “High-Speed and Accurate Non-Linear Calibration of Temperature Sensors for Transient Aerodynamic Heating Experiments.” Transactions of the Institute of Measurement and Control 36 (6): 845–52. https://doi.org/10.1177/0142331214525073
• Wu, Xiangpeng, Shuwen Yue, and Xuyuan Deng. 2025b. “Jamming Missile Deployment Strategy Based on Simulated Annealing Algorithm and Exhaustive Search Method.” Mathematical Modeling and Algorithm Application 6 (3): 68–71. https://doi.org/10.54097/h5fpjp24
• Wu, Jianjun, Yulin Zhang, and Qizhi Chen. 1996a. “Real-Time Fault Detection Algorithm Based on Neural Networks for Liquid Propellant Rocket Engine.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2591. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2591
• Wu, Jianjun, Yulin Zhang, and Qizhi Chen. 1996b. “A Real-Time Verification System on Fault Diagnosis Methods for Liquid Propellant Rocket Engine.” In 32nd Joint Propulsion Conference and Exhibit. AIAA 1996-2831. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1996-2831
• Wu Qiang, Chen He, and Wu Jie. 2009. “The Implement of Millimeter Wave Active Homing Guidance Based on Embedded System.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0103
• Wu Qiongzhi. 2002. “Velocity Compensation Methods for the Conical Scan Step-Frequency Waveform.” In 2002 International Radar Conference (Radar 2002), vol. 2002. IEE. https://doi.org/10.1049/cp:20020334
• Wu Qiongzhi, Wang Fei, and Long Teng. 2002. “Velocity Compensation Methods for the Conical Scan Step-Frequency Waveform.” In RADAR 2002. IEE. https://doi.org/10.1109/radar.2002.1174762
• Wunderlin, Nino, Duran J. Martin, Ryan W. Cooper, Jean Pitot, and Michael J. Brooks. 2024. “Ablative Thrust Chamber Development for the SAFFIRE ABLE Liquid Rocket Engine.” In AIAA SCITECH 2024 Forum. AIAA 2024-0347. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-0347
• Wyllie, Tim. 2001. “Parachute Recovery for UAV Systems.” Aircraft Engineering and Aerospace Technology 73 (6): 542–51. https://doi.org/10.1108/00022660110696696
• Xia, Xlang-Gen. 1999. Two-Dimensional Malvar Wavelets and Their Applications in Jamming Resistance Communication and Navigation. Defense Technical Information Center. https://doi.org/10.21236/ada378885
• Xiang, Shengwen, Hongqi Fan, and Qiang Fu. 2017. “Distribution of Miss Distance in Discrete-Time Controlled System with Noise-Corrupted State Information.” World Journal of Engineering and Technology 05 (04): 69–77. https://doi.org/10.4236/wjet.2017.54b008
• Xiao, Qin, Si-Yuan He, Yunhua Zhang, Hong-Cheng Yin, and Guo-Qiang Zhu. 2015. “Angular Glint Analysis of the 2-D Target above a Rough Surface Based on Extraction of the Coupling Currents.” Progress In Electromagnetics Research M 41: 199–207. https://doi.org/10.2528/pierm15012901
• Xiao, Xiao, Tao Li, Yong Qiang Ren, and Liu Tao. 2012. “Research on TV-Command-Guided Air-to-Ground Missile Simulation Training System Based on SIMBox.” Advanced materials research 630: 253–59. https://doi.org/10.4028/www.scientific.net/amr.630.253
• Xiaowen, Zhang, Wang Qiang, and Tao Yihang. 2025. “An Identification Algorithm of Coherent Jamming for Monopulse Angle Measurement.” In Sixteenth International Conference on Signal Processing Systems (ICSPS 2024), edited by Robert Minasian, Li Chai. SPIE. https://doi.org/10.1117/12.3061999
• Xin, Ming, and S. Balakrishnan. 2002. “A New Optimal Nonlinear Control Method and Its Application to Missile Guidance Law Design.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2002-5023. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-5023
• 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
• Xin, Ming, Sivasubramanya Balakrishnan, and Ernest Ohlmeyer. 2006. “Guidance Law Design for Missiles with Reduced Seeker Field-of-View.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2006-6085. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-6085
• Xiong, Juntao. 2018. “Nonlinear Combustion Instability in a Multi-Injector Rocket Engine.” In 2018 Joint Propulsion Conference. AIAA 2018-4676. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-4676
• Xu, Kunmei, Guobiao Cai, and Yuntao Zheng. 2006. “Flow Field Numerical Study within Thrust Chamber of Aerospace Small Liquid Propellant Rocket Engine.” In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.iac-06-c4.p.1.06
• Xu, Jintao, Yuanyuan Jiang, Junying Zhang, Zilong Guo, and yan Kong. 2024c. “Research on the Initial Roll Angle Algorithm of Guided Missile Bodies Based on Adaptive Complementary Filtering.” In Speckle 2023: VIII International Conference on Speckle Metrology, edited by Yechuan Zhu, Wei Wang, Weiguo Liu. SPIE. https://doi.org/10.1117/12.3016607
• Xu, X., and Y. Liang. 2015. “Biased Optimal Guidance Law with Specified Velocity Rendezvous Angle Constraint.” Aeronautical Journal 119 (1220): 1287–99. https://doi.org/10.1017/s0001924000011258
• Xu, Hongshuang, Guopin Liu, Xian Yang, and Changchun Hua. 2024a. “Adaptive Synchronization Control for Bilateral Teleoperation Systems with Global Prescribed Performance.” In Proceedings of the 2024 2nd International Conference on Frontiers of Intelligent Manufacturing and Automation. ACM. https://doi.org/10.1145/3704558.3705535
• Xu, B., G. Liu, J. D. Yang, and W. Zhang. 2012. “Investigation on Ejection Dynamics of Air Launched Missile.” In 2012 International Conference on System Simulation (ICUSS 2012). IET. https://doi.org/10.1049/cp.2012.0543
• Xu, Lei, Shuang Ma, Lifu Du, and Yingzi Guan. 2026b. “Intelligent Online Identification of Aerodynamic Parameters for Hypersonic Glide Vehicle.” In Lecture Notes in Mechanical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-95-3034-2_36
• Xu, Yue, and Jun Wen Qiu. 2011. “Research on Influence of Contact Stress on the Hinge Moment Balance Measures.” Applied Mechanics and Materials 148-149: 833–36. https://doi.org/10.4028/www.scientific.net/amm.148-149.833
• Xu, Dehao, Jianchun Wang, and Shiyi Chen. 2022a. “Skin-Friction and Heat-Transfer Decompositions in Hypersonic Transitional and Turbulent Boundary Layers.” Journal of Fluid Mechanics 941: A4. https://doi.org/10.1017/jfm.2022.269
• Xue, Yang. 2021. “Effect of Air Permeability on Stability of Supersonic Parachute.” Aviation 25 (2): 123–28. https://doi.org/10.3846/aviation.2021.15131
• Xue, X., S. Luo, and C. Y. Wen. 2019c. “Numerical Simulation of Effect of Angle of Attack on a Supersonic Parachute System.” In 31st International Symposium on Shock Waves 2. Springer International Publishing. https://doi.org/10.1007/978-3-319-91017-8_114
• Xue, Xiaopeng, and Yoshiaki Nakamura. 2011. “Computational Analysis of Supersonic Flexible Parachute Using Immersed Boundary Method.” International Journal of Aerospace and Lightweight Structures (IJALS) - 01 (02): 283. https://doi.org/10.3850/s2010428611000122
• Xue, Fei, Han Qin, Yuchao Wang, Zenghui Jiang, Xin Jin, and Peng Bai. 2019b. “Free Flight Wind Tunnel Test Similarity Law Derivation for Light Store Separation from Aircraft.” Advances in Mechanical Engineering 11 (5): 1687814019853062. https://doi.org/10.1177/1687814019853062
• 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
• Yamasaki, Takeshi, Sivasubramanya Balakrishnan, and Hiroyuki Takano. 2011. “Modified CLOS Intercept Guidance for Aircraft Defense against a Guided Missile.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6421. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6421
• Yamasaki, Takeshi, Yuhei Kikukawa, Hiroyuki Takano, and Isao Yamaguchi. 2024. “Terminal Impact Angle Control Guidance Taking Account of Field-of-View Constraint Using a Time-Shifting Sliding Surface.” In AIAA SCITECH 2024 Forum. AIAA 2024-2207. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2024-2207
• 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
• Yang, Vigor. 2004. Liquid-Propellant Rocket Engine Injector Dynamics and Combustion Processes at Supercritical Conditions. Defense Technical Information Center. https://doi.org/10.21236/ada428947
• Yang, Young-Rok, Tae-Hwan Cho, and Rho-Shin Myong. 2011b. “Range Sensitivity Analysis of a Canard Controlled Missile.” Journal of the Korea Institute of Military Science and Technology 14 (1): 39–48. https://doi.org/10.9766/kimst.2011.14.1.039
• Yang, Christopher S., Noah J. Cowan, and Adrian M. Haith. 2020a. “De Novo Learning versus Adaptation of Continuous Control in a Manual Tracking Task.” Preprint, bioRxiv. https://doi.org/10.1101/2020.01.15.906545
• Yang, Christopher S., Noah J. Cowan, and Adrian M. Haith. 2021. “De Novo Learning versus Adaptation of Continuous Control in a Manual Tracking Task.” eLife 10: e62578. https://doi.org/10.7554/elife.62578
• Yang, 陈阳 Chen, 储海荣 Chu Hai-rong, and 郭立红 Guo Li-hong. 2016. “Precision of Integral Proportion Navigation Guidance with Strapdown Seeker.” Infrared and Laser Engineering 45 (6): 0631001. https://doi.org/10.3788/irla201645.0631001
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023a. “Human–robot Interaction in Teleoperation Systems.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00010-3
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023b. “Shared Control for Teleoperation.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00009-7
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023c. “Software Systems and Platforms for Teleoperation.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00006-1
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023d. “Task Learning of Teleoperation Robot Systems.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00011-5
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023e. “Uncertainties Compensation-Based Teleoperation Control.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00007-3
• Yang, Chenguang, Jing Luo, and Ning Wang. 2023f. “User Experience-Enhanced Teleoperation Control.” In Human-In-the-loop Learning and Control for Robot Teleoperation. Elsevier. https://doi.org/10.1016/b978-0-32-395143-2.00008-5
• Yang, Shanchao, Kangsheng Tian, and Renzheng Liu. 2019b. “Task Scheduling Algorithm Based on Value Optimisation for Anti-Missile Phased Array Radar.” IET Radar, Sonar & Navigation 13 (11): 1883–89. https://doi.org/10.1049/iet-rsn.2019.0163
• Yang, Tao, and Gang Wang. 2019. “Electric Actuator Controller Design for Guided Missile Based on FPGA.” DEStech Transactions on Computer Science and Engineering, no. msota. https://doi.org/10.12783/dtcse/msota2018/27528
• Yang, Xue, Li Yu, Shunchen Nie, and Siyu Zhang. 2019a. “Aerodynamic Performance of the Supersonic Parachute with Material Permeability.” Journal of Industrial Textiles 50 (6): 812–29. https://doi.org/10.1177/1528083719844605
• Yang, Xue, Li Yu, and Xiao-Shun Zhao. 2018b. “Fluid-Structure Interaction Study of the Supersonic Parachute Using Large-Eddy Simulation.” Engineering Computations 35 (1): 157–68. https://doi.org/10.1108/ec-06-2016-0195
• Yang, Huabo, Lijun Zhang, and Yuan Cao. 2011a. “Error Separation Techniques Based on Telemetry and Tracking Data for Ballistic Missile.” In InTech eBooks. https://doi.org/10.5772/24761
• Yang, Si, Hangbin Zhao, Nailiang Zhuang, and Xiaobin Tang. 2024. “Thermal Protection of the Nuclear Rocket Engine Nozzle Based on Regenerative Cooling Method.” Preprint, . https://doi.org/10.2139/ssrn.4713390
• 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. “Design of Guidance Laws Implementing Parallel Navigation.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-6
• Yanushevsky, Rafael T. 2018e. “Design of Guidance Laws Implementing Parallel Navigation: A Time Domain Approach.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-5
• Yanushevsky, Rafael T. 2018f. “Guidance Law Performance Analysis under Stochastic Inputs.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-7
• Yanushevsky, Rafael T. 2018g. “Integrated Missile Design.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-10
• Yanushevsky, Rafael T. 2018h. “Missile Guidance Software.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-12
• Yanushevsky, Rafael T. 2018j. “New Generation of Intercept Systems for National Missile Defense.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-11
• Yanushevsky, Rafael T. 2018k. “Testing Guidance Laws Performance.” In Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954-9
• Yanushevsky, Rafael. 2026a. “Analysis of Proportional Navigation Guided Systems in the Frequency Domain.” In Guidance and Control of Unmanned Vehicles. CRC Press. https://doi.org/10.1201/9781003675921-5
• Yanushevsky, Rafael. 2026b. “Analysis of Proportional Navigation Guided Systems in the Time Domain.” In Guidance and Control of Unmanned Vehicles. CRC Press. https://doi.org/10.1201/9781003675921-4
• Yanushevsky, Rafael. 2026c. “Guidance Laws for Boost-Phase Interceptors Launched from UAVs.” In Guidance and Control of Unmanned Vehicles. CRC Press. https://doi.org/10.1201/9781003675921-11
• Yao, Xuan, Qingyang Chen, and Hongbo Xin. 2025. “Multi-Target Cooperative Strike Path Planning Method for Air-Launched Loitering Vehicle.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-3552-8_14
• 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, Haitao, and Liang Ma. 2017. “The Air Defense Missile Weapon System Based on Queuing Theory Mixed Deployment Effectiveness Evaluation.” In Proceedings of the 7th International Conference on Management, Education, Information and Control (MEICI 2017). Atlantis Press. https://doi.org/10.2991/meici-17.2017.174
• Yao, Yu, Xing Dan Wang, Bao Qing Yang, and Jian Chun Guo. 2011. “The Analysis of Miss Distance Sensitivity to Target Maneuvers for the Terminal Guidance System.” Applied Mechanics and Materials 128-129: 710–13. https://doi.org/10.4028/www.scientific.net/amm.128-129.710
• Yasumura, Yuya, and Keiichi Kitamura. 2021. “Aerodynamic Calculation of Supersonic Parachute at Initial Stage of Opening:: Effects of Gap and Clearance.” Proceedings of Mechanical Engineering Congress, Japan 2021 (0): S191-01. https://doi.org/10.1299/jsmemecj.2021.s191-01
• Yi, C., and D. Carlson. 1975. “A New Approach in Generating Missile Launch Opportunity.” In Guidance and Control Conference. AIAA 1975-1120. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1975-1120
• Yi, Lin, Yu Li, Liangzheng Ma, Yuntu Ao, and Ying Wang. 2021b. “Analysis of Aerodynamic Characteristics of Missile with Different Sweep Angle under Supersonic Condition.” Journal of Physics: Conference Series 1802 (4): 042003. https://doi.org/10.1088/1742-6596/1802/4/042003
• Yifei, He, Liu Yongshan, and Zhu Xingshuai. 2019. “Application of Improved SRCKF for Strapdown Seeker.” In Proceedings of the 2019 4th International Conference on Automation, Control and Robotics Engineering. ACM. https://doi.org/10.1145/3351917.3351948
• Yin, Y. K., and R. F. Berg. 1981. “Computer Aided Manual Tracking.” In JPL Proc. of the 17th Ann. Conf. on Manual Control. https://ntrs.nasa.gov/citations/19820005832
• Yin, Liang, Zichuan Zeng, Yubin Zhou, and Mehdi Khan. 2024. “A Numerical Study of Flow Distribution and Thermal Analyses in Regenerative Cooling Channels for Liquid Rocket Engine.” Preprint, . https://doi.org/10.2139/ssrn.4930788
• Yinghua Han, Jinkuan Wang, Qiang Zhao, and Xin Song. 2009. “A Blind Central DOA Esimation Algorithm in Radar Low-Angle Tracking Environment.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0370
• 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 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
• Yoganandam, Y., and R. Jitendra Das. 1991. “Performance Analysis of a Noncoherent Monopulse Processor in the Presence of Target Glint and Receiver Imbalances.” IEE Proceedings F Radar and Signal Processing 138 (5): 445. https://doi.org/10.1049/ip-f-2.1991.0058
• Yogaswara, Y. H., Alvin Ardiansyah, Rianto Adhy Sasongko, and Taufiq Mulyanto. 2025. “Guidance and Control System Design of a Surface-to-Air Missile Based on 122 Mm Rocket.” Indonesian Journal of Aerospace 23 (1): 23–44. https://doi.org/10.55981/ijoa.2025.9041
• Yonghua Tian, Yong Huang, and Yanling Jia. 2013. “Batch Initiation Using Weighted Least Square Algorithm for Tactical Ballistic Missile Tracking.” In IET International Radar Conference 2013. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2013.0287
• 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
• Yoo, Jeong, and Andrew Meade. 2005. “Scattered Data Approximation of Weapons Bay Flow Classification.” In Infotech@Aerospace. AIAA 2005-7169. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-7169
• Yoon, J.-K., K. Kang, and K. Kim. 1994. “Combustion Instability in Minimum Smoke Propellant Rocket Motor.” In 30th Joint Propulsion Conference and Exhibit. AIAA 1994-3192. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-3192
• Yoon, Sungboo, Moonseo Park, and Changbum Ahn. 2025b. “Learning Viewpoint Control from Human-Initiated Transitions for Teleoperation in Construction.” Preprint, . https://doi.org/10.2139/ssrn.5129658
• 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
• Yoshizawa, Makoto, and Hiroshi Takeda. 1983. “Compensation Mechanism for Time-Delay of the Human Operator in a Manual Control System.” Transactions of the Society of Instrument and Control Engineers 19 (8): 665–72. https://doi.org/10.9746/sicetr1965.19.665
• You, H., and F.-J. Zhao. 2020. “Distributed Synergetic Guidance Law for Multiple Missiles with Angle-of-Attack Constraint.” Aeronautical Journal 124 (1274): 533–48. https://doi.org/10.1017/aer.2019.122
• Youmans, B. R., R. K. Bartman, P. M. Salomon, W. J. Minford, and F. T. Stone. 1990. “Design and Performance of a Fiber Optic Gyroscope Using Integrated Optics.” In JPL. https://ntrs.nasa.gov/citations/19910034956
• Young, Frank L. 1965. Experimental Investigation of the Effects of Surface Roughness on Compressible Turbulent Boundary Layer Skin Friction and Heat Transfer. Defense Technical Information Center. https://doi.org/10.21236/ad0621085
• Youngs, Mitch, and Edmund Bitinas. 2010. Close Combat Missile Methodology Study. Defense Technical Information Center. https://doi.org/10.21236/ada535396
• 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, K.-B. 1994. “Recursive Super-Resolution Algorithm for Low-Elevation Target Angle Tracking in Multipath.” IEE Proceedings - Radar, Sonar and Navigation 141 (4): 223–29. https://doi.org/10.1049/ip-rsn:19941232
• Yu, Wenbin, and Wanchun Chen. 2011. “Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2011-6714. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-6714
• Yu, Tianpeng, Yongbo Chen, and Jinlinag Li. 2015b. “The Communication Design of the Optical Fiber Reflective Memory Network in the Semi-Physical Simulation System of the Laser Beam Rider Guidance Missile.” In Proceedings of the 2015 International Conference on Advances in Mechanical Engineering and Industrial Informatics. Atlantis Press. https://doi.org/10.2991/ameii-15.2015.91
• Yu, Polk, Yuri B. Shtessel, and Christopher Edwards. 2015a. “Adaptive Continuous Higher Order Sliding Mode Control of Air Breathing Hypersonic Missile for Maximum Target Penetration.” In AIAA Guidance, Navigation, and Control Conference. AIAA 2015-2003. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-2003
• Yu, Gang, Xugang Wang, Xuepeng Hu, et al. 2025a. “The Effects of Deployment Posture on the Inflation Process Characteristics of a Light Aircraft Recovery Parachute.” Preprint, . https://doi.org/10.2139/ssrn.5605078
• Yu, Qian, Xiao Jun Xiang, and Jun Li Yang. 2012. “Design and Simulation of Guidance Law for a Kind of Flight Test Missile.” Advanced materials research 538-541: 2887–91. https://doi.org/10.4028/www.scientific.net/amr.538-541.2887
• Yu, Han, Yao Yang, Baoe Yang, Shangrong Yang, and Shuai Shang. 2025b. “Tangential Combustion Instability and Flame Dynamics of a Shear Injector in a Model Rocket Engine Combustor.” Physics of Fluids 37 (10): 107106. https://doi.org/10.1063/5.0290649
• Yu WeiHua, Liu Xiao, Wang Lei, and Sun Houjun. 2009. “A Novel MMW Active Monopulse Antenna for Angle Measurement.” In IET Conference Publications. IET. https://doi.org/10.1049/cp.2009.0342
• Yuan, Pin-Jar. 1996. “Optimal Guidance of Proportional Navigation.” In SPIE Proceedings, vol. 2739, edited by Michael K. Masten, Larry A. Stockum. SPIE. https://doi.org/10.1117/12.241942
• Yuan, K., Ryan Avenall, Jacob Chung, Bruce Carroll, and Gregg Jones. 2005. “Enhancement of Thrust Chamber Cooling with Porous Metal Inserts.” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2005-4128. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2005-4128
• Yuan, Pin-Jar, Ming-Ghow Chen, and Jeng-Shing Chern. 2000. “Extended Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2000-4161. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2000-4161
• Yuan, Pin-Jar, Ming-Ghow Chen, and Men-Jyue Leu. 2001. “Optimal Guidance of Extended Proportional Navigation.” In AIAA Guidance, Navigation, and Control Conference and Exhibit. AIAA 2001-4345. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2001-4345
• Yuan, Pin-Jar, Shih-Che Hsu, and Ching-Yew Yang. 1993. “The Exact Closed-Form Solution of Generalized Proportional Navigation.” In Guidance, Navigation and Control Conference. AIAA 1993-3780. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1993-3780
• Yuan, Tao, Manish Kothawade, and Yuan Chen. 2021. “11 a Bayesian Design of Zero-Failure Reliability Demonstration Tests for Multicomponent Systems.” In Mathematics for Reliability Engineering. De Gruyter. https://doi.org/10.1515/9783110725599-011
• Yuhui, Huang, and Wang Zhenguo. 2002. “Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics.” In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA 2002-3992. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2002-3992
• Yun, Joongsup, Chang-Kyung Ryoo, and Taek-Lyul Song. 2009. “Guidance Filter Design Based on Strapdown Seeker and MEMS Sensors.” Journal of the Korean Society for Aeronautical & Space Sciences 37 (10): 1002–9. https://doi.org/10.5139/jksas.2009.37.10.1002
• Yuxiang Zhou, Haibo Liu, and Xiaoying Deng. 2013. “Research on Measurement Algorithm of Vector Miss Distance Based on Impulse Radar.” In IET International Radar Conference 2013. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2013.0295
• 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
• Zaikang, Qi, and Lin Defu. 2019a. “The Basics of Missile Guidance Control.” In Design of Guidance and Control Systems for Tactical Missiles. CRC Press. https://doi.org/10.1201/9780429291203-1
• Zaikang, Qi, and Lin Defu. 2019b. “Line of Sight Guidance.” In Design of Guidance and Control Systems for Tactical Missiles. CRC Press. https://doi.org/10.1201/9780429291203-6
• Zaikang, Qi, and Lin Defu. 2019c. “Missile Trajectory Models, Aerodynamic Derivatives, Dynamic Coefficients and Missile Transfer Functions.” In Design of Guidance and Control Systems for Tactical Missiles. CRC Press. https://doi.org/10.1201/9780429291203-2
• Zaikang, Qi, and Lin Defu. 2019d. “Proportional Navigation and Extended Proportional Navigation Guidance Laws.” In Design of Guidance and Control Systems for Tactical Missiles. CRC Press. https://doi.org/10.1201/9780429291203-8
• Zamani, Ali, Mohamadreza Moniri Hamadani, and Reza fatemi Mofrad. 2017. “Error-Based Adaptive Update Rate in Multi-Function Phased-Array Radar Using IMM Target-Tracking Algorithm.” International Journal Of Engineering And Computer Science. https://doi.org/10.18535/ijecs/v6i4.25
• 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
• Zavodskikh, K. Yu., and I. F. Kupryashkin. 2021. “Modelling of the Anti-Tank Guided Missile Scattering Field and Radar Performance Evaluation in Terms of Missile Detection.” Journal of «Almaz – Antey» Air and Defence Corporation, no. 3: 79–89. https://doi.org/10.38013/2542-0542-2021-3-79-89
• Zaychik, Kirill, and Frank Cardullo. 2009. “Discriminating between Individuals Based on the Parameters of the Enhanced Model of the Human Operator.” In AIAA Modeling and Simulation Technologies Conference. AIAA 2009-6033. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-6033
• Zaychik, Kirill, Frank Cardullo, Gary George, and Lon C. Kelly. 2009. “Evaluating Effectiveness of Modeling Motion System Feedback in the Enhanced Hess Structural Model of the Human Operator.” In American Inst. of Aeronautics and Astronautics. https://ntrs.nasa.gov/citations/20090029958
• Zeiger, Florian, Nikolaus Kraemer, and Klaus Schilling. 2008. Parameter Tuning of Routing Protocols to Improve the Performance of Mobile Robot Teleoperation via Wireless Ad-Hoc Networks. https://doi.org/10.5220/0001488800530060
• Zeng, Fanyu, Yunlong Qiu, Zhongzheng Jiang, Chuan Tong, Chenhao Hu, and Weifang Chen. 2024. “Direct Numerical Simulation of Skin Friction Drag Reduction on Supersonic Turbulent Boundary Layers with Micro-Blowing.” Physics of Fluids 36 (9): 095165. https://doi.org/10.1063/5.0222859
• Zengliang Li, Zengliang Li, Xin Zhao Xin Zhao, and Huadong Zhang Huadong Zhang. 2015. “Research on Angle Measurement Method of Monopulse SAR.” In IET International Radar Conference 2015. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2015.1208
• Zero-Failure Reliability Demonstration. 2022. Wiley. https://doi.org/10.1002/9781119988342.ch4
• Zhai, Guangyao. 2018. “Target Tracking Based on Millimeter Wave Radar in Complex Scenes.” International Journal of Performability Engineering. https://doi.org/10.23940/ijpe.18.02.p5.232244
• Zhai, Di-Hua, and Yuanqing Xia. 2023a. “Adaptive Control of Bilateral Teleoperation.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-3
• Zhai, Di-Hua, and Yuanqing Xia. 2023b. “Adaptive Finite-Time Teleoperation Control.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-8
• Zhai, Di-Hua, and Yuanqing Xia. 2023c. “Adaptive Semi-Autonomous Control of Heterogeneous Teleoperation Systems.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-7
• Zhai, Di-Hua, and Yuanqing Xia. 2023d. “Anti-Saturation Teleoperation Control.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-4
• Zhai, Di-Hua, and Yuanqing Xia. 2023e. “Finite-Time Adaptive Anti-Windup Teleoperation Control.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-9
• Zhai, Di-Hua, and Yuanqing Xia. 2023f. “Preliminaries of Teleoperation Control.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-2
• Zhai, Di-Hua, and Yuanqing Xia. 2023g. “Prescribed Performance Task-Space Teleoperation Control.” In High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058-10
• Zhang, Bo. n.d. “New Control Schemes for Bilateral Teleoperation under Asymmetric Communication Channels: Stabilization and Performance under Variable Time Delays.” PhD diss., Ecole centrale de Lille. https://doi.org/10.70675/4ae181d4z00f6z46ffz9a94z0e564732fd03
• Zhang, Qingbin. 2003. “A New Parachute Deployment Model by Multibody Dynamics.” In 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. AIAA 2003-2134. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2003-2134
• Zhang, Lei. 2007. “Fuzzy Controllers Based on Optimal Fuzzy Reasoning for Missile Terminal Guidance.” In 45th AIAA Aerospace Sciences Meeting and Exhibit. AIAA 2007-464. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-464
• Zhang, Lei. 2009. “Adaptive Fuzzy-PID Controllers Based on Optimal Fuzzy Reasoning for Missile Terminal Guidance.” In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. AIAA 2009-427. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-427
• Zhang, Wei. 2016. “Fault Prediction Methods of Liquid Rocket Engine (LRE).” In Failure Characteristics Analysis and Fault Diagnosis for Liquid Rocket Engines. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-49254-3_11
• Zhang, Yunbo. 2026. “The History of Liquid Rocket Fuel Engine.” Highlights in Science, Engineering and Technology 160: 654–60. https://doi.org/10.54097/5ebdm421
• Zhang, Jianling, Jinwen An, and Mina Wang. 2005. “Strategy Missile Control System Design Using Adaptive Fuzzy Control Based on Popov Stability Criterion.” In SPIE Proceedings, vol. 5985, edited by Cheng Wang, Shan Zhong, Xiulin Hu. SPIE. https://doi.org/10.1117/12.658262
• Zhang, Xue, and Jiancheng Chen. 2022. “Distributed Time Cooperative Control of Multi-Missile Systems via Second-Order Sliding Mode.” Transactions of the Institute of Measurement and Control 48 (15): 4329–35. https://doi.org/10.1177/01423312221122567
• Zhang, Yixin, Hengyu Chen, Jiazhi Ma, and Yukai Kong. 2026c. “Monopulse Angle Estimation with Adaptive Dual Sum-and-Difference Beamforming.” Electronics Letters 62 (1): e70686. https://doi.org/10.1049/ell2.70686
• Zhang, Mingyang, Zhishi Chen, Songyan Wang, Tao Chao, and Ming Yang. 2023d. “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, Haoyue, and Shihong Ding. 2023. “Numerical Algorithm for Hypersonic Vehicle Optimal Flight Control.” Measurement and Control 56 (7–8): 1308–20. https://doi.org/10.1177/00202940231154856
• Zhang, Ming-Liang, and Pu-Yun Gao. 2018. “Numerical Analysis of the Influence of the Wake Flow Field in the Process of Parachute Deployment.” DEStech Transactions on Computer Science and Engineering, no. cmsms. https://doi.org/10.12783/dtcse/cmsms2018/25203
• Zhang, Zetian, and Min Gao. 2025. “Spatio-Temporal Cooperative Guidance Law for Loitering Munitions Based on Adaptive Sliding Mode Control.” Applied Mathematical Sciences 19 (6): 249–69. https://doi.org/10.12988/ams.2025.919261
• Zhang, Jian, Xiaoquan Gong, Peihong Zhang, Jie Liu, and Yaobing Zhang. 2023a. “Analysis of Uncertainty Factors in the Prediction of Missile Pitch Damping Derivatives by Unstructured CFD Solver.” Journal of Physics: Conference Series 2599 (1): 012009. https://doi.org/10.1088/1742-6596/2599/1/012009
• Zhang, Li Jia, Yi Huang, Yu Zhang, and Zhao Ying Li. 2014b. “Study of Proportional Navigation Guidance of Reentry Vehicle Considering Wind Disturbance.” Applied Mechanics and Materials 490-491: 368–74. https://doi.org/10.4028/www.scientific.net/amm.490-491.368
• Zhang, Jiaqi, and Qinglian Li. 2017. “Development of an Oxygen-Hydrocarbon Torch for Liquid Rocket Engine Ignition.” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2017-4669. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-4669
• Zhang, Ou, Haiying Lu, Shishun Wei, and Lingnan Liu. 2025d. “Research on Missile Stability Control Based on Model-Free Adaptive Control.” In Advances in Transdisciplinary Engineering. IOS Press. https://doi.org/10.3233/atde241367
• Zhang, Minghuan, Wanchao Ma, Yunhe Guo, and Shengli Xu. 2019d. “A New Compound Control Method for Missile with Canard and Tail Rudders.” Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 37 (5): 962–67. https://doi.org/10.1051/jnwpu/20193750962
• Zhang, Sijun, A. Meganathan, K. Jain, and T. Fuchiwaki. 2008. “Effects of Store Separation on the Aeroelastic Behavior of Wings.” In 26th AIAA Applied Aerodynamics Conference. AIAA 2008-6241. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2008-6241
• Zhang, Jin, and Jungang Miao. 2012. “The Verification of Chaotic Characteristics of Radar Angular Glint.” Progress In Electromagnetics Research B 43: 295–311. https://doi.org/10.2528/pierb12062601
• Zhang, Sen, Gen-Feng Shang, Cui-Sheng Wu, and Yuan-Heng Zhang. 2015b. “Optimal Guidance Law of Air to Surface Missile with Terminal Impact Angle Constraint.” In Design, Manufacturing and Mechatronics. WORLD SCIENTIFIC. https://doi.org/10.1142/9789814730518_0053
• Zhang, Tingting, and Haoping She. 2015. “Elliptical Trajectory Guidance Law with Terminal Impact Angle Constraint.” In AIAA Atmospheric Flight Mechanics Conference. AIAA 2015-1021. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-1021
• Zhang, Dai Yu, Bao Wei Song, and Zhou Zhu. 2012a. “The Accuracy Assessment of Weapon System Using Grey Linear Regression Method.” Applied Mechanics and Materials 268-270: 1809–13. https://doi.org/10.4028/www.scientific.net/amm.268-270.1809
• Zhang, D., and R. G. Wang. 2015. “Impact-Angle-Constrained Guidance against Moving Targets.” In WIT Transactions on Engineering Sciences, vol. 1. WIT Press. https://doi.org/10.2495/acar140431
• Zhang, Jing, Bo Wang, and Haowei Zhang. 2026a. “Frequency Diverse Array-Based Angle Deception against Conical-Scan Automatic Direction Finding Systems.” IET Radar, Sonar & Navigation 20 (1): e70204. https://doi.org/10.1049/rsn2.70204
• Zhang, Tianxu, Yuehuan Wang, and Sheng Zhong. 2019c. “Information Processing Simulation and Performance Evaluation for Optical Imaging Seeker.” In Unmanned System Technologies. Springer Singapore. https://doi.org/10.1007/978-981-13-6994-0_8
• Zhang, Zilun, Jiasheng Xu, and Zhiwei Mei. 2026f. “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, Kuanqiao, and Suochang Yang. 2015. “Adaptive Sliding Mode Guidance Law with Terminal Angle Constraint.” In Advances in Intelligent Systems Research. Atlantis Press. https://doi.org/10.2991/lemcs-15.2015.155
• Zhang, J., Y. F. Yu, P. P. Yan, Y. H. Fan, and X. W. Guo. 2017d. “Global Sliding Mode Control for the Bank-to-Turn of Hypersonic Glide Vehicle.” IOP Conference Series: Materials Science and Engineering 187: 012004. https://doi.org/10.1088/1757-899x/187/1/012004
• 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, Nan, and Yue Zhang. 2013. “The Hinge Moment Optimization of Rudder Base on CFD Numerical Simulation.” Applied Mechanics and Materials 397-400: 218–21. https://doi.org/10.4028/www.scientific.net/amm.397-400.218
• Zhang Gang, Li Xiang-ping, Zhu Ming-bo, and Zhou Qiang. 2012. “Missile Terminal Guidance Trajectory Optimization with Radar Imaging Constraints.” In International Conference on Automatic Control and Artificial Intelligence (ACAI 2012). Institution of Engineering and Technology. https://doi.org/10.1049/cp.2012.1229
• Zhao, He-wei. 2023. “Barrier Lyapunov Function-Based Adaptive Neural Control for Hypersonic Vehicle with Full State Constraints.” Preprint, Research Square. https://doi.org/10.21203/rs.3.rs-2486979/v1
• Zhao, Yue, Kun Guo, Cheng Xu, et al. 2025b. “A Deep Learning Predictor-Proportional Guidance Corrector Method for Rocket Deceleration Guidance.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-96-2200-9_1
• Zhao, Z. Q., J. X. Hao, and L. J. Li. 2017. “Study on Combat Effectiveness of Air Defense Missile Weapon System Based on Queuing Theory.” In SPIE Proceedings, vol. 10322, edited by Xiyuan Chen. SPIE. https://doi.org/10.1117/12.2266077
• Zhao, Yong Tao, and Yun An Hu. 2011. “Design of the Scheme Flight Trajectory Command for the Tactical Missile.” In Key engineering materials, vol. 480-481. Trans Tech Publications. https://doi.org/10.4028/www.scientific.net/kem.480-481.1426
• Zhao, Hong Chao, Xian Jun Shi, and Ting Wang. 2013. “Sliding Mode Observer and Controller Design for Nonlinear Supersonic Missile.” Advanced materials research 718-720: 1228–33. https://doi.org/10.4028/www.scientific.net/amr.718-720.1228
• 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, Chengyu, Feng Yang, Ziheng Cheng, and Kai Liu. 2026a. “Deep Reinforcement Learning Guidance Law with Impact Angle and Time Constraints.” Preprint, . https://doi.org/10.2139/ssrn.6096170
• Zhao, X. H., S. H. Yi, Q. Mi, Y. F. Hu, and H. L. Ding. 2022. “Skin Friction Reduction of Hypersonic Body by Supersonic Layer.” Fluid Dynamics 57 (5): 686–96. https://doi.org/10.1134/s0015462822050123
• Zhao, Zhongwen, Xu Zhang, and Guodong Li. 2020. “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, Fang, Xiao Zhang, and Xin Zhang. 2023. “Technology Research of Micro Air-Launched Decoy.” In Third International Seminar on Artificial Intelligence, Networking, and Information Technology (AINIT 2022), edited by Naijing Hu, Guanglin Zhang. SPIE. https://doi.org/10.1117/12.2667665
• Zheng, Xiao Long, Bang Jie Li, and Zhi Fu Shi. 2013. “Research on Guide and Control Method of Air Launched Ballistic Missile.” Applied Mechanics and Materials 389: 583–89. https://doi.org/10.4028/www.scientific.net/amm.389.583
• Zheng, Zonggui, Chongchong Wang, Xiangdong Sun, Liang Yang, and Wanchun Chen. 2022. “Entry Guidance with No-Fly Zone Avoidance for Hypersonic Glide Vehicle.” In Lecture Notes in Electrical Engineering. Springer Singapore. https://doi.org/10.1007/978-981-16-9492-9_136
• Zheng Lu, Feng Li, and Tao Zeng. 2013. “Monopulse Radar Angle Extractor of Multiple Unresolved Targets via Matching Pursuits.” In IET International Radar Conference 2013. Institution of Engineering and Technology. https://doi.org/10.1049/cp.2013.0426
• Zhiming, Zhou, and Xiaoxian Yao. 2019. “Polynomial Guidance Law for Impact Angle Control with a Seeker Look Angle Limit.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234 (3): 857–70. https://doi.org/10.1177/0954410019890808
• Zhou, Rui. 2003. “Optimal Feedback Missile Guidance Law Using Neural Networks.” In SPIE Proceedings, vol. 5253, edited by Guangjun Zhang, Huijie Zhao, Zhongyu Wang. SPIE. https://doi.org/10.1117/12.522330
• Zhou, Xiangfa. 2018. “Porous Ceramic Matrix Phase Change Composites for Thermal Control Purposes of Hypersonic Vehicle.” In Advances in Some Hypersonic Vehicles Technologies. InTech. https://doi.org/10.5772/intechopen.70863
• Zhou, Jun, Hanqiao Huang, and Jianguo Guo. 2010a. “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, Chijun, Mingjie Li, Lei Shao, Humin Lei, and Changxin Luo. 2023a. “An Improved Predictor-Corrector Guidance Algorithm for Reentry Glide Vehicle Based on Fast Landing Points Position Prediction.” In Lecture Notes in Electrical Engineering. Springer Nature Singapore. https://doi.org/10.1007/978-981-19-6613-2_64
• Zhou, Shaobo, Delin Luo, and Jinpeng Zhang. 2019e. “Terminal Angle Constraint Guidance Law Based on SDRE Method.” IOP Conference Series: Earth and Environmental Science 242: 032060. https://doi.org/10.1088/1755-1315/242/3/032060
• Zhou, Di, Pingping Qu, and Sheng Sun. 2013b. “A Guidance Law with Terminal Impact Angle Constraint Accounting for Missile Autopilot.” Journal of Dynamic Systems, Measurement, and Control 135 (5): 051009. https://doi.org/10.1115/1.4024202
• Zhou, Hao, Tawfiqur Rahman, and Wanchun Chen. 2015. “Impact Angle and Impact Velocity Constrained Terminal Guidance for Stationary Target.” Aircraft Engineering and Aerospace Technology 87 (5): 454–64. https://doi.org/10.1108/aeat-09-2013-0164
• Zhu, Guixin, Yunlong Gao, and Tong Zhao. 2024. “Attitude Control of Hypersonic Vehicle Based on Adaptive Active Disturbance Rejection Control.” Preprint, . https://doi.org/10.2139/ssrn.4675586
• Zhu, Shiquan, Zongyao Hu, Chuanxiao Cheng, et al. 2021. “Effect of a Jet Control Device on the Process of Missile and Internal Weapons Bay Separation.” Defence Science Journal 71 (5): 691–98. https://doi.org/10.14429/dsj.71.16819
• Zhu, Jing Ju, Zeng Liang Jiang, and Xian Jie Wei. 2014. “Research on Image Guided Missile Attack Mode.” Applied Mechanics and Materials 552: 200–203. https://doi.org/10.4028/www.scientific.net/amm.552.200
• Zhu, Yalu, Feng Liu, and William A. Sirignano. 2025b. “Simulation of Multi-Injector H2-O2Rocket Combustion Instability.” In AIAA SCITECH 2025 Forum. AIAA 2025-0158. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2025-0158
• 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, Xuke, Xiaoshuo Yang, Yongchao Ji, Shiyi Chen, and Zhenhua Xia. 2026a. “Reformulating and Unifying Van Driest’s Theory for Skin-Friction Transformation and Prediction in Compressible Turbulent Boundary Layers.” Preprint, . https://doi.org/10.2139/ssrn.6764142
• Zhuang, Fengchen, Wansheng Nie, Wentao Zhao, and Weidong Liu. 1998. “Liquid Rocket Combustion Instability Analysis Methodology: Methods and Representative Examples.” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 1998-3690. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1998-3690
• Zhuang, Fengchen, Wansheng Nie, and Qin Zou. 1999. “Numerical Simulation of MMH/NTO Rocket Engine Combustion Instability.” In 35th Joint Propulsion Conference and Exhibit. AIAA 1999-2779. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1999-2779
• Zien, T. F., and W. C. Ragsdale. 1979. Predictions of Aerodynamic Heating on Tactical Missile Domes. Defense Technical Information Center. https://doi.org/10.21236/ada073217
• Zinn, B. T. 1966a. A Theoretical Study of Nonlinear Combustion Instability in Liquid Propellant Rocket Engines. NASA. https://ntrs.nasa.gov/citations/19670032683
• Zinn, B. T. 1966b. A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors. NASA-CR-75894. NASA. https://ntrs.nasa.gov/citations/19660020175
• Zinn, B. T., E. A. Powell, and M. S. Padmanabhan. 1974. Determination of the Effects of Nozzle Nonlinearities upon Nonlinear Stability of Liquid Propellant Rocket Motors. NASA-CR-139634. NASA. https://ntrs.nasa.gov/citations/19740024101
• Zinsou, Bertin. 2024. “Stability of a Flexible Missile and Asymptotics of the Eigenvalues of Fourth Order Boundary Value Problems.” Preprint, . https://doi.org/10.22541/au.170670776.63942925/v1
• Zoltowski, Michael D. 2000. NWV Topic 20 Jam-Proof Area Deniable Propagation: Anti-Jam Protection for GPS via Robust Efficient Space-Time Adaptive Processing. Defense Technical Information Center. https://doi.org/10.21236/ada384716
• Zook, Connor. 2024. Closed-Loop Thrust Throttling Capabilities on Kero-Lox Liquid Rocket Engine. https://doi.org/10.52202/078371-0154
• 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
• Zumwalt, G. W., and R. J. Damkevala. 1965. Predicted Shock Wave Patterns for a Supersonic Conical Missile Passing through a Blast Wave. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4637851
• Zumwalt, G. W., and H. H. Tang. 1964. Transient Base Pressure Study of an Axisymmetric Supersonic Missile Flying Head-on through a Blast Wave. Office of Scientific and Technical Information (OSTI). https://doi.org/10.2172/4671308
• 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
• Левихин, А. А., and A. I. Musteikis. 2025. “Computational Study of Regenerative Cooling for a Low-Thrust Rocket Engine Chamber Using Gaseous Propellants.” Aèrokosmičeskaâ tehnika i tehnologii. 3 (3): 443–57. https://doi.org/10.52467/2949-401x-2025-3-3-443-457
• МГТУ им. Н.Э. Баумана and В.П. Александренков. 2017. “Influence of Heat Exchange Intensity in the Rocket Thrust Chamber on the Cooling Channel Efficiency.” Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, no. 100. https://doi.org/10.18698/0236-3941-2017-4-4-10
• МГТУ им. Н.Э. Баумана, В.Д. Баскаков, В.А. Тарасов, and МГТУ им. Н.Э. Баумана. 2013. “Methodological Justification for Rocket Weapon Design Parameters Accuracy.” Engineering Journal: Science and Innovation, no. 16. https://doi.org/10.18698/2308-6033-2013-3-637
• 殷, 红成, 超 王, and 培康 黄. 2014. “Inherent Relations among the Three Representations of Radar Target Angular Glint (in English).” JOURNAL OF RADARS 3 (2): 119–28. https://doi.org/10.3724/sp.j.1300.2014.14025

Secondary Sources

• Anderson, John. 2002. Modern Compressible Flow: With Historical Perspective. McGraw-Hill Science/Engineering/Math. https://openlibrary.org/works/OL1993329W
• Anderson, William E., and Vigor Yang, eds. 1995. Liquid Rocket Engine Combustion Instability. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866371
• Balakrishnan, S. N., A. Tsourdos, and B. A. White, eds. 2016. Advances in Missile Guidance, Control, and Estimation. CRC Press. https://doi.org/10.1201/b12503
• Ball, Robert E., The fundamentals of aircraft combat survivability analysis, and design. 2003. The Fundamentals of Aircraft Combat Survivability: Analysis and Design (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast. https://openlibrary.org/works/OL5099643W
• Barton, David Knox. 2004. Radar System Analysis and Modeling. Artech House. https://openlibrary.org/works/OL13634896W
• Blakelock, John H., Automatic Control of Aircraft, and Missiles. 1965. Automatic Control of Aircraft and Missiles. Wiley. https://openlibrary.org/works/OL4449715W
• Bruhn, E. F. 1973. Analysis and Design of Flight Vehicle Structures. Jacobs Pub. https://openlibrary.org/works/OL8796483W
• Bryson, A. E., and Ho. 1975. Applied Optimal Control: Optimization, Estimation and Control. Wiley. https://openlibrary.org/works/OL12859817W
• Chen, Wanchun, Hao Zhou, Wenbin Yu, and Liang Yang. 2021d. Steady Glide Dynamics and Guidance of Hypersonic Vehicle. Springer Singapore. https://doi.org/10.1007/978-981-15-8901-0
• Clark, John D. 1972. Ignition!: An Informal History of Liquid Rocket Propellants. Rutgers University Press. https://openlibrary.org/works/OL7159231W
• Cover, Thomas M., and Joy A. Thomas. 2006. Elements of Information Theory. Wiley & Sons Canada, Limited, John. https://openlibrary.org/works/OL21500808W
• Dornberger, Walter. 1954. V-2. Viking Press. https://openlibrary.org/works/OL6160912W
• Dranovsky, Mark L. 2007. Combustion Instabilities in Liquid Rocket Engines: Testing and Development Practices in Russia. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866906
• Driels, Morris R. 2013. Weaponeering: Conventional Weapon System Effectiveness. American Institute of Aeronautics and Astronautics, Inc. https://openlibrary.org/works/OL3471401W
• Estimated CEP of Weapon Delivery for Attacks against Aircraft Shelters. 1970. RAND Corporation. https://doi.org/10.7249/d20250
• 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
• Fletcher, Leroy S., ed. 1978. Aerodynamic Heating and Thermal Protection Systems. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.865336
• Franklin, Gene F., Powell, and Emami-Naeini. 2019. Feedback Control of Dynamic Systems. Pearson. https://openlibrary.org/works/OL18666743W
• Garnell, P. 1980. Guided Weapon Control Systems. Pergamon Press. https://openlibrary.org/works/OL6338950W
• Glasstone, Samuel. 1962. The Effects of Nuclear Weapons. U.S. Department of Defense and U.S. Atomic Energy Commission. https://archive.org/details/TheEffectsOfNuclearWeapons
• Glasstone, Samuel, and Philip J. Dolan. 1977. Effects of Nuclear Weapons. United States Government Printing. https://openlibrary.org/works/OL37590915W
• 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
• Hammer, J., and W. Elswick. 1966. Conventional Missile Attacks against Aircraft on Airfields and Aircraft Carriers. RAND Corporation. https://doi.org/10.7249/rm4718
• Hill, Philip G., and Peterson. 1991. Mechanics and Thermodynamics of Propulsion [by] Philip G. Hill [and] Carl R. Peterson. https://openlibrary.org/works/OL8229940W
• Huang, Minchao, Yuqiang Cheng, Jia Dai, and Jian Li. 2025. Performance Analysis of a Liquid/Gel Rocket Engine during Operation. Springer Nature Singapore. https://doi.org/10.1007/978-981-97-6485-3
• Human-In-the-Loop Learning and Control for Robot Teleoperation. 2023. Elsevier. https://doi.org/10.1016/c2021-0-02620-1
• Huzel, Dieter K., and David H. Huang. 1992. Modern Engineering for Design of Liquid-Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL27313820W
• Incropera, Frank P., David P. DeWitt, Fundamentals of Heat, and Mass Transfer. 1985. Fundamentals of Heat and Mass Transfer. Wiley. https://openlibrary.org/works/OL2975219W
• James, D. A. 1986b. Radar Homing Guidance for Tactical Missiles. Macmillan Education UK. https://doi.org/10.1007/978-1-349-08602-3
• 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
• Knacke, T. W., and Parachute recovery systems design manual. 1992. Parachute Recovery Systems: Design Manual. Para Pub. https://openlibrary.org/works/OL4121303W
• Li, Zhijun, Yuanqing Xia, and Chun-Yi Su. 2015a. Intelligent Networked Teleoperation Control. Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-662-46898-2
• McRuer, Duane T., Krendel, and Mathematical Models of Human Pilot Behavior. 1973. Mathematical Models of Human Pilot Behavior. Systems Technology, Inc. https://openlibrary.org/works/OL6476637W
• 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
• A Missile Jamming and Engagement Model. 2025. RAND Corporation. https://doi.org/10.7249/rra3150-2
• Neufeld, Michael J. 1995. The Rocket and the Reich: Peenemünde and the Coming of the Ballistic Missile Era. Free Press. https://openlibrary.org/works/OL3501503W
• Nielsen, Jack Norman. 1960. Missile Aerodynamics. McGraw-Hill. https://openlibrary.org/works/OL4626547W
• Nielsen, Jack. 1988a. Missile Aerodynamics. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.062902
• Ordway and Wakeford. 1960. International Missile and Spacecraft Guide [by] Frederick I. Ordway [and] Ronald C. Wakeford. McGraw-Hill. https://openlibrary.org/works/OL5900152W
• Papoulis, Athanasios. 2002. Probability, Random Variables, and Stochastic Processes. McGraw-Hill. https://openlibrary.org/works/OL4455624W
• Przemieniecki, J. S., and Mathematical methods in defense analyses. 1994. Mathematical Methods in Defense Analyses. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL3494463W
• Rathakrishnan, Ethirajan. 2025. Hypersonic Slender Body Aerodynamics. Wiley. https://doi.org/10.1002/9781394285662
• Rezende, Rene Nardi. 2018a. Liquid Rocket Engine Thrust Chamber Parametric Modeling. SAE International eBooks. https://doi.org/10.4271/0768093333
• Rezende, Rene Nardi. 2018b. Liquid Rocket Engine Thrust Chamber: Parametrical Modeling. SAE International eBooks. https://doi.org/10.4271/r-465
• Rigby, Keith A. 2013. Aircraft Systems Integration of Air-Launched Weapons. Wiley. https://doi.org/10.1002/9781118519165
• Sheridan, Thomas B., and William R. Ferrell. 1974. Man-Machine Systems: Information, Control, and Decision Models of Human Performance. The MIT Press. https://openlibrary.org/works/OL39139905W
• Sherman, Samuel M., and Barton. 2011. Monopulse Principles and Techniques. Artech House. https://openlibrary.org/works/OL2417266W
• Shneydor, N. A. 1998d. Missile Guidance and Pursuit. Woodhead Publishing Limited. https://doi.org/10.1533/9781782420590
• Siouris, George M. 2004. Missile Guidance and Control Systems. Springer. https://openlibrary.org/works/OL3746989W
• Sklar, Bernard. 2001. Digital Communications: Fundamentals and Applications. Prentice-Hall. https://openlibrary.org/works/OL10516432W
• Skolnik, Merrill I. 2008. Radar Handbook. McGraw-Hill Education. https://openlibrary.org/works/OL11286925W
• Sutton, George P. 2006. History of Liquid Propellant Rocket Engines. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.868870
• Sutton, George P., and Oscar Biblarz. 2016. Rocket Propulsion Elements. Wiley & Sons, Incorporated, John. https://openlibrary.org/works/OL21470530W
• Tuzlukov, Vyacheslav. 2026j. Target Tracking by Airborne Radar Systems: Airborne Radar Systems and Single Target Tracking. CRC Press. https://doi.org/10.1201/9781003408802
• Van Trees, Harry L., and Harry L. Van Trees. 2001. Detection, Estimation, and Modulation Theory. Wiley. https://openlibrary.org/works/OL4282773W
• Vulnerability of Quick-Reacting Sheltered Missiles and Aircraft during Launch. 1959. RAND Corporation. https://doi.org/10.7249/d6625
• Wang, Zhen-Guo. 2016. Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical Simulations. Wiley. https://doi.org/10.1002/9781118890035
• 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. 2018i. Modern Missile Guidance. CRC Press. https://doi.org/10.1201/9781351202954
• Zarchan, Paul. 2012a. Tactical and Strategic Missile Guidance. American Institute of Aeronautics and Astronautics. https://openlibrary.org/works/OL19905556W
• Zarchan, Paul. 2012b. Tactical and Strategic Missile Guidance, Sixth Edition. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.868948
• Zarchan, Paul, ed. 2019a. Advanced Tactical and Strategic Missile Guidance, Seventh Edition, Volume 2. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.105388
• Zarchan, Paul, ed. 2019b. Tactical and Strategic Missile Guidance, Seventh Edition: SET. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.105845
• Zarchan, Paul, ed. 2019c. Tactical and Strategic Missile Guidance: An Introduction, Seventh Edition, Volume 1. American Institute of Aeronautics and Astronautics, Inc. https://doi.org/10.2514/4.105371
• Zhai, Di-Hua, Yuanqing Xia, and Shan Guo. 2023. High-Performance Adaptive Control of Teleoperation Systems. CRC Press. https://doi.org/10.1201/9781003382058
• Zhang, Tianxu, Yuehuan Wang, and Sheng Zhong. 2019b. Guidance Information Processing Methods in Airborne Optical Imaging Seeker. Springer Singapore. https://doi.org/10.1007/978-981-13-6994-0

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
• Smith, Charles R. 2021. “Aerodynamic Heating in Hypersonic Flows.” Physics Today 74 (11): 66–67. https://doi.org/10.1063/pt.3.4888

Tertiary Sources

• “Aerojet.” 2026. Wikipedia. Last modified July 25, at 14:11 (UTC). https://en.wikipedia.org/w/index.php?title=Aerojet&oldid=1365973953
• “AGM-28 Hound Dog.” 2026. Wikipedia. Last modified May 15, at 05:26 (UTC). https://en.wikipedia.org/w/index.php?title=AGM-28_Hound_Dog&oldid=1354244353
• “Air-Launched Ballistic Missile.” 2026. Wikipedia. Last modified July 27, at 15:57 (UTC). https://en.wikipedia.org/w/index.php?title=Air-launched_ballistic_missile&oldid=1366363605
• “Atomic Bombings of Hiroshima and Nagasaki.” 2026. Wikipedia. Last modified October 13, at 14:49 (UTC). https://en.wikipedia.org/w/index.php?title=Atomic_bombings_of_Hiroshima_and_Nagasaki&oldid=1380059296
• “Beam Diameter.” 2026. Wikipedia. Last modified April 30, at 21:52 (UTC). https://en.wikipedia.org/w/index.php?title=Beam_diameter&oldid=1351910430
• “Bell X-9 Shrike.” 2024. Wikipedia. Last modified February 27, at 13:16 (UTC). https://en.wikipedia.org/w/index.php?title=Bell_X-9_Shrike&oldid=1210610675
• “Boeing B-29 Superfortress.” 2026. Wikipedia. Last modified August 5, at 00:27 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_B-29_Superfortress&oldid=1367752051
• “Boeing B-50 Superfortress.” 2026. Wikipedia. Last modified July 25, at 07:17 (UTC). https://en.wikipedia.org/w/index.php?title=Boeing_B-50_Superfortress&oldid=1365930238
• “Canard (Aeronautics).” 2026. Wikipedia. Last modified March 23, at 06:51 (UTC). https://en.wikipedia.org/w/index.php?title=Canard_(aeronautics)&oldid=1344913002
• “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
• “Command Guidance.” 2026. Wikipedia. Last modified April 30, at 08:46 (UTC). https://en.wikipedia.org/w/index.php?title=Command_guidance&oldid=1351816149
• “Convair B-36 Peacemaker.” 2026. Wikipedia. Last modified July 21, at 01:46 (UTC). https://en.wikipedia.org/w/index.php?title=Convair_B-36_Peacemaker&oldid=1365219731
• “GAM-63 RASCAL.” 2026. Wikipedia. Last modified July 30, at 04:24 (UTC). https://en.wikipedia.org/w/index.php?title=GAM-63_RASCAL&oldid=1366779380
• “Holloman Air Force Base.” 2026. Wikipedia. Last modified July 19, at 17:57 (UTC). https://en.wikipedia.org/w/index.php?title=Holloman_Air_Force_Base&oldid=1364990290
• “Monopulse Radar.” 2025. Wikipedia. Last modified October 17, at 17:48 (UTC). https://en.wikipedia.org/w/index.php?title=Monopulse_radar&oldid=1317352002
• “Nuclear Weapon Yield.” 2026. Wikipedia. Last modified April 11, at 22:58 (UTC). https://en.wikipedia.org/w/index.php?title=Nuclear_weapon_yield&oldid=1348306123
• “Operation Paperclip.” 2026. Wikipedia. Last modified July 24, at 20:35 (UTC). https://en.wikipedia.org/w/index.php?title=Operation_Paperclip&oldid=1365851700
• Parsch, Andreas. 2002. “Bell RTV-A-4/X-9 Shrike.” Directory of U.S. Military Rockets and Missiles, Appendix 1: Early Missiles and Drones. https://designation-systems.net/dusrm/app1/x-9.html
• “Peenemünde Army Research Center.” 2026. Wikipedia. Last modified July 19, at 22:01 (UTC). https://en.wikipedia.org/w/index.php?title=Peenem%C3%BCnde_Army_Research_Center&oldid=1365034417
• “Proportional Navigation.” 2026. Wikipedia. Last modified January 7, at 15:51 (UTC). https://en.wikipedia.org/w/index.php?title=Proportional_navigation&oldid=1331673719
• “Rayleigh Distribution.” 2026. Wikipedia. Last modified July 3, at 17:35 (UTC). https://en.wikipedia.org/w/index.php?title=Rayleigh_distribution&oldid=1362392172
• “RCA.” 2026. Wikipedia. Last modified May 12, at 22:48 (UTC). https://en.wikipedia.org/w/index.php?title=RCA&oldid=1353876949
• “Republic-Ford JB-2.” 2026. Wikipedia. Last modified July 9, at 22:40 (UTC). https://en.wikipedia.org/w/index.php?title=Republic-Ford_JB-2&oldid=1363391220
• “SM-62 Snark.” 2026. Wikipedia. Last modified January 26, at 14:10 (UTC). https://en.wikipedia.org/w/index.php?title=SM-62_Snark&oldid=1334946107
• “Solar Turbines.” 2026. Wikipedia. Last modified June 15, at 17:05 (UTC). https://en.wikipedia.org/w/index.php?title=Solar_Turbines&oldid=1359501428
• “Standoff Weapon.” 2026. Wikipedia. Last modified July 17, at 14:46 (UTC). https://en.wikipedia.org/w/index.php?title=Standoff_weapon&oldid=1364611509
• “Terminal Ballistics.” 2026. Wikipedia. Last modified August 2, at 10:07 (UTC). https://en.wikipedia.org/w/index.php?title=Terminal_ballistics&oldid=1367315781
• “Trinity (Nuclear Test).” 2026. Wikipedia. Last modified October 9, at 23:04 (UTC). https://en.wikipedia.org/w/index.php?title=Trinity_(nuclear_test)&oldid=1379426945
• “V-1 Flying Bomb.” 2026. Wikipedia. Last modified July 31, at 19:30 (UTC). https://en.wikipedia.org/w/index.php?title=V-1_flying_bomb&oldid=1367066637
• “Walter Dornberger.” 2026. Wikipedia. Last modified July 22, at 23:45 (UTC). https://en.wikipedia.org/w/index.php?title=Walter_Dornberger&oldid=1365518356

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