Control of three-axis stabilized flexible spacecraft using variable structure strategies subject to input nonlinearities

JVC/Journal of Vibration and Control

Volumn 12, Issue 6, 2006, Pages 659-681

  Hu, Qinglei ^a   Ma, Guangfu ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

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

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; FEEDBACK CONTROL; NONLINEAR SYSTEMS; STRUCTURAL ANALYSIS;

FLEXIBLE SPACECRAFT; INPUT NONLINEARITIES; VARIABLE STRUCTURE OUTPUT FEEDBACK CONTROL; VIBRATION SUPPRESSION;

SPACECRAFT;

EID: 33744738833     PISSN: 10775463     EISSN: 17412986     Source Type: Journal    
DOI: 10.1177/1077546306065398     Document Type: Article

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