Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver

Aerospace Science and Technology

Volumn 9, Issue 4, 2005, Pages 307-317

  Hu, Qinglei ^a   Ma, Guangfu ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Active vibration control; Flexible spacecraft; Nonlinear sliding mode; Positive position feedback; Variable structure control

Indexed keywords

MANEUVERABILITY; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PARTIAL DIFFERENTIAL EQUATIONS; PIEZOELECTRIC DEVICES; SENSORS; SLIDING MODE CONTROL; SPACECRAFT;

ACTIVE VIBRATION CONTROL; FLEXIBLE SPACECRAFT; NONLINEAR SLIDING MODE; POSITIVE POSITION FEEDBACK; VARIABLE STRUCTURE CONTROL;

VIBRATION CONTROL;

EID: 19944391998     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.02.001     Document Type: Article

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