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Results 1 to 25 of 54

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Multistepping approach to finite-interval missile integrated controlVADDI, S. S; MENON, P. K; SWERIDUK, G. D et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 4, pp 1015-1018, issn 0731-5090, 4 p.Article

Adaptive critic-based neural networks for agile missile controlDONGCHEN HAN; BALAKRISHNAN, S. N.Journal of guidance, control, and dynamics. 2002, Vol 25, Num 2, pp 404-407, issn 0731-5090Conference Paper

Comparison of Inverse Optimal and Tuning Functions Designs for Adaptive Missile ControlSONNEVELDT, L; VAN OORT, E. R; CHU, Q. P et al.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 4, pp 1176-1182, issn 0731-5090, 7 p.Article

Optimal dual-rate digital redesign with application to missile controlRABBATH, C. A; LECHEVIN, N; HORI, N et al.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 6, pp 1083-1087, issn 0731-5090, 5 p.Article

Modeling and H∞ control for switched linear parameter-varying missile autopilotLIM, Sungyung; HOW, Jonathan P.IEEE transactions on control systems technology. 2003, Vol 11, Num 6, pp 830-838, issn 1063-6536, 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

Adaptive fuzzy gain scheduling in guidance system designLIN, Chun-Liang; SU, Huai-Wen.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 4, pp 683-692, issn 0731-5090Article

Structured multivariable phase margin analysis with applications to a missile autopilotBAR-ON, Jonathan R; ADAMS, Robert J.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 2, pp 363-366, issn 0731-5090, 4 p.Article

Design of missile guidance law via variable structure controlMOON, Jongki; KIM, Kiseok; KIM, Youdan et al.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 4, pp 659-664, issn 0731-5090Article

Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance ControlVADDI, S. S; MENON, P. K; OHLMEYER, E. J et al.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 2, pp 699-703, issn 0731-5090, 5 p.Article

Capture set computation of an optimally guided missileRAIVIO, Tuomas.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 6, pp 1167-1175, issn 0731-5090Article

Navy theater ballistic missile defense boost multispectral discrimination requirements for low resolution detection, classification and high resolution aimpoint selectionPAIVA, C. A.SPIE proceedings series. 1998, pp 532-550, isbn 0-8194-2839-6Conference Paper

A sliding mode missile pitch autopilot synthesis for high angle of attack maneuveringTHUKRAL, A; INNOCENTI, M.IEEE transactions on control systems technology. 1998, Vol 6, Num 3, pp 359-371, issn 1063-6536Article

Nonlinear missile autopilot design with θ-D techniqueMING XIN; BALAKRISHNAN, S. N; STANSBERY, Donald T et al.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 3, pp 406-417, issn 0731-5090, 12 p.Article

Real-time computational methods for SDRE nonlinear control of missilesMENON, P. K; LAM, T; CRAWFORD, L. S et al.Proceedings of the American Control Conference. 2002, pp 232-237, issn 0743-1619, isbn 0-7803-7298-0, 6Vol, 6 p.Conference Paper

Using a multiple-model adaptive estimator in a random evasion missile/aircraft encounterOSHMAN, Y; SHINAR, J; WEIZMAN, S. Avrashi et al.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 6, pp 1176-1186, issn 0731-5090Article

Design of proportional parallel distributed compensators for non-linear systems : Fuzzy control applicationsMENG JOO ER; YI ZHOU; LIN CHEN et al.International journal of computer applications in technology. 2006, Vol 27, Num 2-3, pp 204-211, issn 0952-8091, 8 p.Article

Solving a nonlinear output regulation problem: Zero miss distance of pure PNGOH, Jae-Hyuk.IEEE transactions on automatic control. 2002, Vol 47, Num 1, pp 169-173, issn 0018-9286Article

Fuzzy side force control for missile against hypersonic targetLIN, C.-L; WANG, T.-L.IET control theory & applications (Print). 2007, Vol 1, Num 1, pp 33-43, issn 1751-8644, 11 p.Article

Improving conventional longitudinal missile autopilot using cerebellar model articulation controller neural networksLIN, C. C; CHEN, F. C.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 5, pp 711-718, issn 0731-5090, 8 p.Article

Multirate LPV synthesis: A loop-shaping approach for missile controlFARRET, D; DUC, G; HARCAUT, J. P et al.Proceedings of the American Control Conference. 2002, pp 4092-4097, issn 0743-1619, isbn 0-7803-7298-0, 6Vol, 6 p.Conference Paper

Commande de systèmes instationnaires : Séquencement de compensateurs et commande LPV = Non stationary system control: gain scheduling and LPV controlPELLANDA, Paulo César; APKARIAN, Pierre.Journal européen des systèmes automatisés. 2003, Vol 37, Num 10, pp 1311-1315, issn 1269-6935, 5 p.Article

Characterization of the WISP array performance in ambient and cryogenic operating environmentsKIRCHER, J. R; OLSON, E. M; BERGIN, T. P et al.SPIE proceedings series. 2001, pp 158-167, isbn 0-8194-4061-2Conference Paper

Solutions for high performance HWIL motion systemsAVORY, Mark; TAN, Ai-Leng; PAGE, Jeff et al.SPIE proceedings series. 2001, pp 239-268, isbn 0-8194-4061-2Conference Paper

Attitude Control of Missile Via Fliess ExpansionYU YAO; BAOQING YANG; FENGHUA HE et al.IEEE transactions on control systems technology. 2008, Vol 16, Num 5, pp 959-970, issn 1063-6536, 12 p.Article

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