DocumentCode
3418452
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
Volume
2
fYear
2001
fDate
2001
Firstpage
1357
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.945913
Filename
945913
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