Satellite attitude control by integrator back-stepping with internal stabilization
暂无分享,去创建一个
[1] G. Ma,et al. Spacecraft attitude tracking control based on nonlinear H/sub /spl infin// control , 2006, 2006 1st International Symposium on Systems and Control in Aerospace and Astronautics.
[2] Ceren Kaplan,et al. LEO SATELLITES: ATTITUDE DETERMINATION AND CONTROL COMPONENTS ; SOME LINEAR ATTITUDE CONTROL TECHNIQUES , 2006 .
[3] A. Loria,et al. An extension of Matrosov's theorem with application to stabilization of nonholonomic control systems , 2002, Proceedings of the 41st IEEE Conference on Decision and Control, 2002..
[4] P. Hughes. Spacecraft Attitude Dynamics , 1986 .
[5] R. O. Doruk,et al. A Robustness Analysis Procedure for Realistic Missiles , 2005 .
[6] Andrew Turner. An Open-Source, Extensible Spacecraft Simulation And Modeling Environment Framework , 2003 .
[7] James R. Wertz,et al. Spacecraft attitude determination and control , 1978 .
[8] V. Matrosov. On the stability of motion , 1962 .
[9] Ciann-Dong Yang,et al. Nonlinear H/sub /spl infin// robust control for satellite large angle attitude maneuvers , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).
[10] Thor I. Fossen,et al. Nonlinear vectorial backstepping design for global exponential tracking of marine vessels in the presence of actuator dynamics , 1997, Proceedings of the 36th IEEE Conference on Decision and Control.
[11] Kevin J. Walchko. ROBUST NONLINEAR ATTITUDE CONTROL WITH DISTURBANCE COMPENSATION , 2003 .
[12] Per Johan Nicklasson,et al. Satellite attitude control by quaternion-based backstepping , 2005 .