Bounded Linear-Quadratic Differential Game Guidance Law for Dual-Thruster Controlled Missiles

Author:

LIU Yanfang,QI Naiming,LÜ Rui,ZHOU Qihang

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference21 articles.

1. 1) Tournes, C., Shtessel, Y. and Shkolnikov, I.: Autopilot for Missiles Steered by Aerodynamic Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds, AIAA Guidance, Navigation, and Control Conference, 2005, San Francisco, California, pp. 5191–5206.

2. 2) Innocenti, M. and Thukral, A.: Simultaneous Reaction Jet and Aerodynamic Control of Missile Systems, AIAA Guidance, Navigation, and Control Conference, August 1993, Monterey, CA, pp. 347–354.

3. 3) Weil, R. D. and Wise, K. A.: Blended Aero & Reaction Jet Missile Autopilot Design Using VSS Techniques, 30th Conference on Decision and Control, December 1991, Brighton, England, pp. 2828–2829.

4. Variable Structure Controller Design with Application to Missile Tracking

5. 5) Menon, P. K. and Iragavarapu, V. R.: Adaptive Techniques for Multiple Actuator Blending, AIAA Guidance, Navigation, and Control Conf., Aug. 1998, Boston, CP-1998-4494.

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1. Capture condition for endo-atmospheric interceptors steered by ALCS and ARCS;Control Theory and Technology;2014-01-18

2. Effects of Divert-Thrusters on Homing Performance of Endo-atmospheric Interceptors;Journal of Optimization Theory and Applications;2012-07-19

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