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
Link To Document :
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