Static output feedback control based on iterative LMI for spacecraft's attitude

Yuhang Xuebao/Journal of Astronautics

Volumn 28, Issue 3, 2007, Pages 539-544

  Tong, Xi Yue ^a   Li, Dong Xu ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

Flexible spacecraft; Input saturation; Linear matrix inequality; Static output

Indexed keywords

FEEDBACK CONTROL; LINEAR MATRIX INEQUALITIES; SATURATION (MATERIALS COMPOSITION); SPECIFICATIONS; STABILIZATION; UNCERTAIN SYSTEMS;

FLEXIBLE SPACECRAFT; INPUT SATURATION; LINEAR MATRIX INEQUALITY; STATIC OUTPUT;

SPACECRAFT;

EID: 34547614317     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

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