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Aerospace Science and Technology, ISSN 1270-9638, 10/2013, Volume 30, Issue 1, pp. 239 - 245
In the flight trials of a spinning missile, it was observed that an unexpected and unstable coning motion occurred after burnout. The missile was still in the... 
Stability conditions | Hinge moment | Coning motion | Spinning missile | AUTOPILOT | STABILITY LIMITS | UNGUIDED ROCKETS | FLIGHT | FINS | ENGINEERING, AEROSPACE | YAW LOCK-IN | SYMMETRIC MISSILE | Air-to-surface missiles | Aerospace engineering
Journal Article
Aerospace Science and Technology, ISSN 1270-9638, 03/2013, Volume 25, Issue 1, pp. 40 - 44
Missile safety takes a more and more important place in the design and the evaluation of a missile. For that purpose, missile performance collateral damages... 
Missile performances | Monte Carlo methods | Complex system engineering | Importance splitting | Rare event simulation | GLOBAL SENSITIVITY-ANALYSIS | RARE | ENGINEERING, AEROSPACE | SIMULATION | Air-to-surface missiles | Monte Carlo method | Algorithms | Probability | Mathematics
Journal Article
Journal of the Franklin Institute, ISSN 0016-0032, 03/2012, Volume 349, Issue 2, pp. 622 - 637
An exo-atmospheric interception scenario between an accelerating missile and its target is investigated. It is assumed that the maneuvering acceleration is... 
MATHEMATICS, INTERDISCIPLINARY APPLICATIONS | ENGINEERING, MULTIDISCIPLINARY | SLIDING MODES | AUTOMATION & CONTROL SYSTEMS | ENGINEERING, ELECTRICAL & ELECTRONIC | Air-to-surface missiles | Analysis
Journal Article
Signal Processing, ISSN 0165-1684, 09/2012, Volume 92, Issue 9, pp. 2018 - 2028
Journal Article
Aerospace Science and Technology, ISSN 1270-9638, 01/2013, Volume 24, Issue 1, pp. 221 - 225
This paper presents an aerodynamic study of “×−+” finned configurations for theater ballistic missile target (TBMT) which plays a key role to evaluate the... 
CFD | Aerodynamic configuration | Theater ballistic missile target | Wind tunnel experiment | ENGINEERING, AEROSPACE | Ballistic missiles | Aerodynamics | Theaters | Air-to-surface missiles | Analysis
Journal Article
International Journal of Automation and Computing, ISSN 1476-8186, 2/2011, Volume 8, Issue 1, pp. 122 - 127
Journal Article
IEEE Transactions on Aerospace and Electronic Systems, ISSN 0018-9251, 10/2008, Volume 44, Issue 4, pp. 1599 - 1608
Journal Article
Air Power History, ISSN 1044-016X, 10/2010, Volume 57, Issue 3, pp. 22 - 33
[...] the persistent presence of ICBM mobility represents a significant piece of American military and technological history. [...] the foundational work done... 
Missiles | Ballistic missiles | Intercontinental ballistic missiles | Weapons | Cost estimates | Railroad trains | Military air facilities | Military strategy | Air forces | Features | Automobiles | Military aspects | Air-to-surface missiles | Aerospace industry | Nuclear weapons | Engineering research | Research & development--R&D | Technological change | Military history | Armed forces
Journal Article
Journal Article
Digital Signal Processing, ISSN 1051-2004, 2012, Volume 22, Issue 1, pp. 87 - 95
The spinning motion of a ballistic missile (BM), which is a kind of micro-Doppler motion, induces additional frequency modulation on the returned radar signal.... 
Radar target recognition | Micro-Doppler | Time–frequency analysis | Ballistic missile | Time-frequency analysis | EXTRACTION | ENGINEERING, ELECTRICAL & ELECTRONIC | Radar systems | Ballistic missiles | Frequency modulation | Air-to-surface missiles | Analysis | Target recognition | Modulation | Digital signal processing | Images | Radar | Feature extraction | Spinning
Journal Article
International Journal of Aerospace Engineering, ISSN 1687-5966, 2016, Volume 2016, pp. 1 - 7
A guidance law for attacking ground target based on motion camouflage strategy is proposed in this paper. According to the relative position between missile... 
IMPACT | SLIDING MODE CONTROL | TARGETS | ANGLE | ENGINEERING, AEROSPACE | CONSTRAINT | PROPORTIONAL NAVIGATION | Design | Unmanned aerial vehicles | Control theory | Bias | Aerospace engineering | Missiles | Terminal guidance | Simulation | Camouflage | Missile control | Derivation | Strategy | Guidance (motion)
Journal Article
The Journal of Engineering, ISSN 2051-3305, 10/2019, Volume 2019, Issue 20, pp. 6718 - 6722
Journal Article
Control Engineering Practice, ISSN 0967-0661, 2006, Volume 14, Issue 7, pp. 811 - 818
In this paper, a robust control scheme based on the quaternion feedback for attitude control of missiles employing thrust vector control is proposed. The... 
Quaternion feedback | Uncertainty | Stability analysis | Attitude control | quaternion feedback | stability analysis | attitude control | SYSTEMS | uncertainty | AUTOMATION & CONTROL SYSTEMS | ENGINEERING, ELECTRICAL & ELECTRONIC | Computer-generated environments | Computer simulation | Air-to-surface missiles | Analysis
Journal Article
eBook
Journal Article
Russian Aeronautics, ISSN 1068-7998, 10/2018, Volume 61, Issue 4, pp. 555 - 560
The matters of conceptual formation and design of a small-size guided air-to-surface missiles with paste-like propellant rocket engine are considered. 
Engineering | Automotive Engineering | small-size missile | rocket engine | paste-like propellant | Air-to-surface missiles | Rockets | Rocket engines | Air to surface missiles | Missile control
Journal Article
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