Spacecraft vibration suppression using variable structure output feedback control and smart materials

Journal of Vibration and Acoustics

Volumn 128, Issue 2, 2006, Pages 221-230

  Hu, Qinglei ^a   Ma, Guangfu ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Attitude maneuver; Flexible spacecraft; Linear quadratic Gaussian (LQG); Positive position feedback (PPF); Variable structure output feedback control (VSOFC); Vibration suppression

Indexed keywords

COMPUTER SIMULATION; FEEDBACK CONTROL; FLEXIBLE STRUCTURES; INTELLIGENT MATERIALS; PIEZOELECTRIC MATERIALS; VIBRATIONS (MECHANICAL);

ATTITUDE MANEUVER; FLEXIBLE SPACECRAFT; LINEAR-QUADRATIC GAUSSIAN (LQG); POSITIVE POSITION FEEDBACK (PFP); VARIABLE STRUCTURE OUTPUT FEEDBACK CONTROL (VSOFC); VIBRATION SUPPRESSION;

SPACECRAFT;

EID: 33645822334     PISSN: 10489002     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2159039     Document Type: Article

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