DocumentCode :
582459
Title :
Reconfigurability analysis for satellite attitude control system
Author :
Wen, Fan ; Yuehua, Cheng ; Bin, Jiang ; Wenjing, Liu
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2012
fDate :
25-27 July 2012
Firstpage :
5285
Lastpage :
5289
Abstract :
Reconfigurability represents the potential of the system to tolerate faults under resources constraints. This paper provides an approach to evaluate and analyze the reconfigurability of satellite attitude control system (ACS) with respect to actuator faults under a certain configuration. The common configurations of ACS are presented. And the controllability and energy consumption of control are analyzed. Then the smallest eigenvalue of controllability Gramian is utilized to measure the level of reconfigurability. Simulation results are given to demonstrate the effectiveness of the proposed approach.
Keywords :
actuators; artificial satellites; attitude control; controllability; eigenvalues and eigenfunctions; fault tolerance; ACS configurations; Gramian; actuator faults; controllability; eigenvalue; energy consumption; fault tolerance; reconfigurability analysis; resource constraints; satellite attitude control system; Actuators; Attitude control; Controllability; Fault tolerance; Satellites; Wheels; Actuator faults; Fault tolerant control; Reconfigurability; Satellite attitude control system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
ISSN :
1934-1768
Print_ISBN :
978-1-4673-2581-3
Type :
conf
Filename :
6390861
Link To Document :
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