Paper Info
Title
Nonlinear H∞ robust control for satellite large angle attitude maneuvers
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
Year
DOI
Venue
2001
10.1109/ACC.2001.945913
American Control Conference, 2001. Proceedings of the 2001
Keywords
DocType
Volume
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
Conference
2
ISSN
ISBN
Citations 
0743-1619
0-7803-6495-3
0
PageRank 
References 
Authors
0.34
0
3
Name
Order
Citations
PageRank
Show, L.-L.121.12
Jyh-Ching Juang212026.23
Ciann-Dong Yang311.10