Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft

European Journal of Control

Volumn 12, Issue 6, 2006, Pages 654-668

  Hu, Qinglei ^a   Guangfu, Ma ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Attitude control; Flexible spacecraft; Input nonlinearities; Variable structure output feedback control; Vibration suppression;

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AEROSPACE VEHICLES; ATTITUDE CONTROL; CLOSED LOOP SYSTEMS; CONTROL NONLINEARITIES; DYNAMICS; FEEDBACK CONTROL; FLEXIBLE SPACECRAFT; LAUNCH VEHICLES; ROBUST CONTROL; STRUCTURAL DESIGN;

ADAPTIVE VARIABLE STRUCTURE; CONTROL INPUTS; INPUT NONLINEARITIES; MANEUVERING CONTROL; SLIDING MODES; THREE AXES; UNCERTAINTY; VARIABLE STRUCTURE OUTPUT FEEDBACK CONTROL; VIBRATION SUPPRESSION; VIBRATION SUPPRESSION;;

CONTROLLERS;

EID: 46749147541     PISSN: 09473580     EISSN: None     Source Type: Journal    
DOI: 10.3166/ejc.12.654-668     Document Type: Article

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