DocumentCode :
28889
Title :
Finite-Time Attitude Tracking of Spacecraft With Fault-Tolerant Capability
Author :
Bing Xiao ; Qinglei Hu ; Youmin Zhang
Author_Institution :
Coll. of Eng., Bohai Univ., Jinzhou, China
Volume :
23
Issue :
4
fYear :
2015
fDate :
Jul-15
Firstpage :
1338
Lastpage :
1350
Abstract :
A finite-time attitude tracking control scheme is presented for rigid spacecraft subject to constant but unknown inertia and external disturbances. The controller, developed using sliding mode control technique, has great fault-tolerant capability to accommodate four types of actuator faults. Different from most of the existing works on attitude fault-tolerant control (FTC), the developed controller guarantees the desired attitude to be followed in finite time, which is critical for FTC systems. Moreover, the convergence time is an explicit parameter for designer´s choice. Thus, the controller design simply meets the finite-time requirement. The attitude-tracking performance is evaluated through a numerical example.
Keywords :
attitude control; control system synthesis; fault tolerant control; space vehicles; variable structure systems; FTC; controller design; fault-tolerant capability; fault-tolerant control; finite-time attitude tracking control; sliding mode control; spacecraft; Actuators; Attitude control; Fault tolerance; Fault tolerant systems; Space vehicles; Torque; Wheels; Attitude tracking; fault-tolerant control (FTC); finite-time; sliding mode control (SMC); spacecraft; spacecraft.;
fLanguage :
English
Journal_Title :
Control Systems Technology, IEEE Transactions on
Publisher :
ieee
ISSN :
1063-6536
Type :
jour
DOI :
10.1109/TCST.2014.2364124
Filename :
6948343
Link To Document :
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