Unified design for H2, H∞, and mixed control of spacecraft

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 6, 1999, Pages 884-896

  Wu, Charng Shi ^a   Chen, Bor Sen ^a,c   Jan, Ying Wen ^b  

^a NATIONAL TSING HUA UNIVERSITY   (Taiwan)

^b NATIONAL SPACE ORGANIZATION   (Taiwan)

^c UNIVERSITY OF SOUTHERN CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRA; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; MATHEMATICAL TRANSFORMATIONS; OPTIMAL CONTROL SYSTEMS; PERTURBATION TECHNIQUES; POSITION CONTROL; RICCATI EQUATIONS; SPACECRAFT;

LINEAR QUADRATIC OPTIMAL CONTROL; NASH GAME CONTROL PROBLEM; NONLINEAR MINIMAX THEORY; SPACECRAFT ATTITUDE CONTROL; STATE VARIABLE TRANSFORMATION;

NONLINEAR CONTROL SYSTEMS;

EID: 0033226869     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4466     Document Type: Article

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