DocumentCode :
176517
Title :
A fault-tolerant control method for satellite with uncertainties and saturation
Author :
Duan Wenjie ; Wang Dayi
Author_Institution :
Beijing Inst. of Control Eng., Beijing, China
fYear :
2014
fDate :
May 31 2014-June 2 2014
Firstpage :
3223
Lastpage :
3228
Abstract :
A fault-tolerant control scheme including integral sliding mode, control allocation and parameter identification is introduced to deal with faults together with uncertainties and saturation. The Lyapunov stability is guaranteed by stability conditions respectively for uncertainties and saturations. Faults are tolerated by control allocation scheme based on the efficiency parameters, which call for a special requirement of parameter identification. The method is applied to a six-wheel spacecraft and simulation shows its effectiveness.
Keywords :
Lyapunov methods; artificial satellites; fault tolerant control; parameter estimation; stability; variable structure systems; Lyapunov stability; control allocation; fault-tolerant control method; integral sliding mode; parameter identification; satellite; six-wheel spacecraft; Control engineering; Fault tolerance; Fault tolerant systems; Orbits; Parameter estimation; Resource management; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
Type :
conf
DOI :
10.1109/CCDC.2014.6852730
Filename :
6852730
Link To Document :
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