kw.\*:("Missile guidance")
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Impact time control guidance law with field of view constraintYOUAN ZHANG; XINGLIANG WANG; HUALI WU et al.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 361-369, issn 1270-9638, 9 p.Article
Can Lead-Lag Guidance Compensator Guarantee Zero Miss Distance?GUTMAN, Shaul.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 3, pp 779-782, issn 0731-5090, 4 p.Article
Impact Angle Constrained Interception of Stationary TargetsRATNOO, Ashwini; GHOSE, Debasish.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 6, pp 1817-1822, issn 0731-5090, 6 p.Article
Bound on Root-Mean-Square Miss of Radar-Guided Missiles for Short Terminal Phase PeriodRUSNAK, Ilan.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 2, pp 665-669, issn 0731-5090, 5 p.Article
Circular-navigation-guidance law for precision missile/target engagementsMANCHESTER, Ian R; SAVKIN, Andrey V.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 314-320, issn 0731-5090, 7 p.Article
Terminal guidance law based on proportional navigationULYBYSHEV, Yuri.Journal of guidance, control, and dynamics. 2005, Vol 28, Num 4, pp 821-824, issn 0731-5090, 4 p.Article
An online-implementable differential evolution tuned all-aspect guidance lawRAGHUNATHAN, T; GHOSE, D.Control engineering practice. 2010, Vol 18, Num 10, pp 1197-1210, issn 0967-0661, 14 p.Article
Simplified Projectile Swerve Solution for General Control InputsOLLERENSHAW, Douglas; COSTELLO, Mark.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 5, pp 1259-1265, issn 0731-5090, 7 p.Article
Robust Discrete-Time Proportional-Derivative Navigation GuidanceLECHEVIN, N; RABBATH, C. A.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 3, pp 1007-1013, issn 0731-5090, 7 p.Article
Development of three-dimensional aiming point guidance lawLIN, Yu-Ping; TSAO, Lu-Ping; LIN, Chun-Liang et al.International journal of systems science. 2010, Vol 41, Num 11, pp 1353-1362, issn 0020-7721, 10 p.Article
Simulation of infrared imaging seeking missilesMORIN, A.SPIE proceedings series. 2001, pp 46-57, isbn 0-8194-4060-4Conference Paper
Kill Vehicle Guidance and Control Sizing for Boost-Phase InterceptZARCHAN, Paul.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 2, pp 513-521, issn 0731-5090, 9 p.Article
Dither-based compensating strategy for radome boresight error and gimbal frictionLIN, Y.-C; LIN, C.-L; SHI, W.-C et al.Aeronautical Journal. 2008, Vol 112, Num 1138, pp 715-723, issn 0001-9240, 9 p.Article
Generalized vector explicit guidanceOHLMEYER, Ernest J; PHILLIPS, Craig A.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 261-268, issn 0731-5090, 8 p.Article
Fuzzy terminal attitude guidance controller with angle only measurementsPATHIRANA, P. N; FARUQI, F. A.Control and intelligent systems. 2007, Vol 35, Num 1, pp 52-59, issn 1480-1752, 8 p.Article
A rapid and high precise calibration method for long-distance cruise missilesWANG XINLONG; WANG BIN; WU XIAOJUAN et al.Aerospace science and technology (Imprimé). 2013, Vol 27, Num 1, pp 1-9, issn 1270-9638, 9 p.Article
Indirect Impact-Angle-Control Against Stationary Targets Using Biased Pure Proportional NavigationERER, Koray S; MERTTOPCUOGLU, Osman.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 2, pp 700-704, issn 0731-5090, 5 p.Article
Optimal guidance law for cooperative attack of multiple missiles based on optimal control theoryXIAO SUN; YUANQING XIA.International journal of control. 2012, Vol 85, Num 7-9, pp 1063-1070, issn 0020-7179, 8 p.Article
Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraintZHENXING ZHANG; SHIHUA LI; SHENG LUO et al.Aerospace science and technology (Imprimé). 2013, Vol 31, Num 1, pp 30-41, issn 1270-9638, 12 p.Article
A study on a missile guidance system against a randomely maneuvering air-to-surface missileIMADO, Fumiaki.IEEE International Conference on Control Applications. 2004, isbn 0-7803-8633-7, 2Vol, Vol1, 430-435Conference Paper
Multi-mode signal processor for imaging infrared seekerRONDA, V; SHUE, Louis.SPIE proceedings series. 2000, pp 142-150, isbn 0-8194-3651-8Conference Paper
Optimal path planning for unmanned combat : Aerial vehicles to defeat radar trackingKABAMBA, Pierre T; MEERKOV, Semyon M; ZEITZ, Frederick H et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 279-288, issn 0731-5090, 10 p.Article
New criterion for aircraft susceptibility to infrared guided missilesARVIND RAO, G; MAHULIKAR, Shripad P.Aerospace science and technology. 2005, Vol 9, Num 8, pp 701-712, issn 1270-9638, 12 p.Article
Differential geometric guidance based on the involute of the target's trajectory : 2-D aspectsARIFF, O; ZBIKOWSKI, R; TSOURDOS, A et al.American Control Conference. 2004, pp 3640-3645, isbn 0-7803-8335-4, 6 p.Conference Paper
The design of an IR/video imaging feature-based Autotracker for the macintosh-hosted G4 processorMILLS, Samuel T; HALL, Robert L.SPIE proceedings series. 2001, pp 58-62, isbn 0-8194-4060-4Conference Paper