Title :
Nonlinear H∞ robust control for satellite large angle attitude maneuvers
Author :
Show, Long-Life ; Juang, Jyh-Ching ; Yang, Ciann-Dong
Author_Institution :
Dept. of Electr. Eng., Nat. Cheng Kung Univ., Tainan, Taiwan
Abstract :
The paper presents a nonlinear H∞ state feedback for large angle attitude control of satellite. The dynamic equations of satellite with full-coupled body fixed canted attitude thruster control are derived. A nonlinear H∞ controller is designed to achieve stability and disturbance rejection for large angle maneuvers. The simulation results based on spacecraft system are presented to demonstrate the effectiveness of the proposed design method
Keywords :
H∞ control; Lyapunov methods; artificial satellites; attitude control; dynamics; nonlinear control systems; robust control; state feedback; H∞ control; Lapunov function; artificial satellite; attitude control; disturbance rejection; dynamics; nonlinear control systems; robust control; spacecraft; stability; state feedback; Aerodynamics; Attitude control; Control design; Equations; Quaternions; Robust control; Satellites; Sliding mode control; Space vehicles; State feedback;
Conference_Titel :
American Control Conference, 2001. Proceedings of the 2001
Conference_Location :
Arlington, VA
Print_ISBN :
0-7803-6495-3
DOI :
10.1109/ACC.2001.945913
