DocumentCode :
3448186
Title :
Application of H robust fault-tolerant control in satellite attitude control system
Author :
Chen, X.Q. ; Wang, F. ; Chen, W. ; Zhang, Y. Ch
Author_Institution :
Harbin Inst. of Technol., Harbin
fYear :
2007
fDate :
23-25 May 2007
Firstpage :
2094
Lastpage :
2097
Abstract :
The robust Fault-Tolerant H Control problem of uncertain linear system is studied in this paper. It is shown that a solution of this problem can be obtained from a system of a linear matrix inequality (LMI). This method possesses integrity against sensors and actuators faults, have robustness to parameter uncertainty and satisfy disturbance attenuation index. At last, the simulation of a satellite attitude control system with actuator and sensor faults validates that this solution is effective and more suitable in on-board real-time computation.
Keywords :
H control; artificial satellites; attitude control; fault tolerance; linear matrix inequalities; linear systems; robust control; uncertain systems; H robust fault-tolerant control; LMI; actuators faults; disturbance attenuation index; linear matrix inequality; parameter uncertainty; satellite attitude control system; uncertain linear system; Actuators; Attenuation; Computational modeling; Control systems; Fault tolerant systems; Linear matrix inequalities; Linear systems; Robust control; Robustness; Uncertain systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Industrial Electronics and Applications, 2007. ICIEA 2007. 2nd IEEE Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-0736-1
Electronic_ISBN :
978-1-4244-0737-8
Type :
conf
DOI :
10.1109/ICIEA.2007.4318779
Filename :
4318779
Link To Document :
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