Noncertainty-Equivalent Adaptive Missile Control via Immersion and Invariance
暂无分享,去创建一个
[1] J.R. Cloutier,et al. Assessment of air-to-air missile guidance and control technology , 1988, IEEE Control Systems Magazine.
[2] Alessandro Astolfi,et al. Nonlinear adaptive control of systems in feedback form: An alternative to adaptive backstepping , 2004, Syst. Control. Lett..
[3] James R. Cloutier,et al. Nonlinear, Hybrid Bank-to-Turn/Skid-to-Turn Missile Autopilot Design , 2001 .
[4] Bernard Friedland,et al. Modern Control Theory for Design of Autopilots for Bank-to-Turn Missiles , 1986, 1986 American Control Conference.
[5] Ming Xin,et al. Nonlinear Missile Autopilot Design with theta - D Technique , 2004 .
[6] E. J. Ohlmeyer,et al. Integrated Design of Agile Missile Guidance and Autopilot Systems , 2001 .
[7] Sahjendra N. Singh,et al. I-O map inversion, zero dynamics and flight control , 1990 .
[8] Mario Innocenti,et al. A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering , 1998, IEEE Trans. Control. Syst. Technol..
[9] Ernest J. Ohlmeyer,et al. Software Tools for Nonlinear Missile Autopilot Design , 1999 .
[10] Ming Xin,et al. Missile longitudinal autopilot design using a new suboptimal nonlinear control method , 2003 .
[11] Spilios Theodoulis,et al. Missile Autopilot Design: Gain-Scheduling and the Gap Metric , 2007 .
[12] Stephen P. Banks,et al. Sliding Mode Control with Optimal Sliding Surfaces for Missile Autopilot Design , 2000 .
[13] Pramod P. Khargonekar,et al. Stability Analysis of a Missile Control System with a Dynamic Inversion Controller , 1998 .
[14] J. H. Evers,et al. Assessment of air-to-air missile guidance and control technology , 1989 .
[15] Alessandro Astolfi,et al. Nonlinear and adaptive control with applications , 2008 .
[16] Debasish Ghose,et al. Variable Structure Controller Design with Application to Missile Tracking , 2001 .
[17] Chih-Min Lin,et al. Improving Conventional Longitudinal Missile Autopilot Using Cerebellar Model Articulation Controller Neural Networks , 2003 .
[18] Ching-Fang Lin,et al. Advanced Control Systems Design , 1993 .
[19] Gunter Stein,et al. A General Adaptive Control Structure with a Missile Application , 1988, 1988 American Control Conference.
[20] Naira Hovakimyan,et al. L1 Adaptive Output-Feedback Controller for Non-Strictly-Positive-Real Reference Systems: Missile Longitudinal Autopilot Design , 2009 .
[21] Song Chong,et al. Design of a CLOS guidance law via feedback linearization , 1992 .
[22] J. R. Cloutier,et al. Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method , 1994 .
[23] Jeff S. Shamma,et al. Gain-Scheduled Missile Autopilot Design Using Linear Parameter Varying Transformations , 1993 .
[24] Alessandro Astolfi,et al. Immersion and invariance: a new tool for stabilization and adaptive control of nonlinear systems , 2001, IEEE Trans. Autom. Control..
[25] Maruthi R. Akella,et al. High-Performance Spacecraft Adaptive Attitude-Tracking Control Through Attracting-Manifold Design , 2008 .
[26] E.W. Kamen,et al. Adaptive Control Applied to Missile Autopilots , 1988, 1988 American Control Conference.
[27] Moshe Idan,et al. Sliding-Mode Control for Integrated Missile Autopilot Guidance , 2004 .
[28] Li-Chen Fu,et al. Adaptive Robust Bank-to-Turn Missile Autopilot Design Using Neural Networks , 1997 .
[29] Keum W. Lee,et al. Immersion- and Invariance-Based Adaptive Control of a Nonlinear Aeroelastic System , 2009 .
[30] Petros A. Ioannou,et al. Robust Adaptive Control , 2012 .