DocumentCode
3266977
Title
A satellite attitude controller using nonlinear H∞ approach
Author
AliAbbasi, M. ; Talebi, H.A. ; Karrari, M.
Author_Institution
Dept. of Electr. Eng., Amirkabir Univ. of Technol., Tehran, Iran
Volume
4
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
4078
Abstract
This paper presents a state feedback H∞ sub-optimal controller for satellite attitude system with three control torques and disturbances. A global solution to the associated Hamilton-Jacobi-Issac (HJI) equation is found. The stability properties of the closed loop system are studied and simulation results are presented to evaluate the performance of the proposed control strategy.
Keywords
H∞ control; Jacobian matrices; artificial satellites; attitude control; closed loop systems; nonlinear control systems; stability; state feedback; suboptimal control; H∞ control; Hamilton-Jacobi-Issac equation; artificial satellites; attitude control; closed loop system; control torques; nonlinear control; stability; state feedback; suboptimal controller; Angular velocity; Attitude control; Closed loop systems; Control systems; Erbium; Nonlinear control systems; Nonlinear systems; Satellites; State feedback; State-space methods;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1185005
Filename
1185005
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