Adaptive integral-type sliding mode control for spacecraft attitude maneuvering under actuator stuck failures

Chinese Journal of Aeronautics

Volumn 24, Issue 1, 2011, Pages 32-45

  Hu, Qinglei ^a,b   Zhang, Youmin ^b   Huo, Xing ^a   Xiao, Bing ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b Dept of Electrical and Computer Engineering   (Canada)

Author keywords

adaptive control; attitude maneuvering; integral sliding mode control; spacecraft; stuck failure

Indexed keywords

ACTUATOR STUCK FAULTS; ADAPTIVE CONTROL; ADAPTIVE LAWS; ATTITUDE CONTROLLER; ATTITUDE MANEUVERING; BOUNDEDNESS; COMPLETE STABILITY; CONSTANT COMPONENTS; DESIGN TECHNIQUE; EXTERNAL DISTURBANCES; FAULT TIME; FAULT TOLERANT CONTROL; HIGH-PRECISE; INTEGRAL SLIDING MODE CONTROL; MANEUVERING CONTROL; ON-LINE PARAMETER; PERFORMANCE ANALYSIS; PRIOR KNOWLEDGE; SIMULATION RESULT; SLIDING MODES; SPACECRAFT ATTITUDE; SPACECRAFT CONTROL; STUCK FAILURE;

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AIRCRAFT LANDING; ATTITUDE CONTROL; SLIDING MODE CONTROL; SPACECRAFT;

CONTROLLERS;

EID: 79952405346     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(11)60005-8     Document Type: Article

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