Sliding mode attitude control with L2-gain performance and vibration reduction of flexible spacecraft with actuator dynamics

Acta Astronautica

Volumn 67, Issue 5-6, 2010, Pages 572-583

  Hu, Qinglei ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Actuator dynamics; Attitude maneuver; Flexible spacecraft; Sliding mode control; Vibration reduction

Indexed keywords

ACTUATOR DYNAMICS; ADAPTIVE VERSIONS; ATTITUDE MANEUVER; CONTROL LAWS; DESIGN APPROACHES; DUAL STAGE; EXTERNAL DISTURBANCES; GAIN PERFORMANCE; INDUCED VIBRATIONS; INPUT VOLTAGES; LOW ORDER MODELS; NUMERICAL SIMULATION; REACTION WHEELS; SENSORS AND ACTUATORS; SLIDING MODES; STRAIN RATE FEEDBACK; SUB-SYSTEMS; UNIFORMLY ULTIMATELY BOUNDED; UPPER BOUND; VIBRATION REDUCTIONS; VIBRATION SUPPRESSION;

ATTITUDE CONTROL; COMPUTER SIMULATION; FLEXIBLE SPACECRAFT; NAVIGATION; PIEZOELECTRIC ACTUATORS; SLIDING MODE CONTROL; SPATIAL VARIABLES CONTROL; STRAIN RATE;

CONTROL THEORY;

EID: 77955328348     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2010.04.018     Document Type: Article

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