Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness

Nonlinear Dynamics

Volumn 64, Issue 1-2, 2011, Pages 13-23

  Hu, Qinglei ^a   Xiao, Bing ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Attitude stabilization; Fault tolerant; Input constraint; Loss of actuator effectiveness; Sliding mode control

Indexed keywords

ACTUATOR FAULT; ATTITUDE STABILIZATION; CLOSED-LOOP PERFORMANCE; CONTROL DESIGN; CONTROL LAWS; CONTROL SYNTHESIS; CONVENTIONAL APPROACH; EFFECTIVENESS FACTOR; EXTERNAL DISTURBANCES; FAULT DETECTION AND ISOLATION; FAULT TOLERANT CONTROL; FAULT-TOLERANT; INERTIA PARAMETERS; INPUT CONSTRAINT; NUMERICAL SIMULATION; SLIDING MODES; SPACECRAFT ATTITUDE;

ACTUATORS; ATTITUDE CONTROL; COMPUTER SIMULATION; CONTROL THEORY; FAULT DETECTION; FLEXIBLE SPACECRAFT; LYAPUNOV FUNCTIONS; NAVIGATION; QUALITY ASSURANCE; SLIDING MODE CONTROL; SPATIAL VARIABLES CONTROL; STABILIZATION; UNCERTAINTY ANALYSIS;

FAULT TOLERANCE;

EID: 79953024740     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11071-010-9842-z     Document Type: Article

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