Output feedback variable structure adaptive control of a flexible spacecraft

Acta Astronautica

Volumn 44, Issue 1, 1999, Pages 11-22

  Zeng, Y ^a   Araujo, A D ^a   Singh, S N ^a  

^a University of Nevada Las Vegas   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL NONLINEARITIES; CONTROL SYSTEM SYNTHESIS; ELASTICITY; FEEDBACK CONTROL; FLEXIBLE STRUCTURES; MATHEMATICAL MODELS; PROBABILITY; ROBUSTNESS (CONTROL SYSTEMS); UNCERTAIN SYSTEMS;

ELASTIC APPENDAGES; FLEXIBLE SPACECRAFTS; OUTPUT FEEDBACK VARIABLE STRUCTURE ADAPTIVE CONTROL; RIGID BODIES;

SPACECRAFT;

EID: 0032668422     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(98)00187-8     Document Type: Article

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