Nonlinear adaptive spacecraft attitude control using solar radiation pressure

IEEE Transactions on Aerospace and Electronic Systems

Volumn 41, Issue 3, 2005, Pages 770-779

  Singh, Sahjendra N ^a   Yim, Woosoon ^a  

^a University of Nevada Las Vegas   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY VALUE PROBLEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FEEDBACK CONTROL; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; SOLAR RADIATION; SPACE FLIGHT; SPACE PROBES; SPACECRAFT; TRAJECTORIES;

FEEDBACK LINEARIZATION TECHNIQUE; INTERPLANETARY PROBES; NONLINEAR ADAPTIVE SPACECRAFT; REFERENCE TRAJECTORIES; SATELLITE MODEL; SOLAR RADIATION PRESSURE;

ADAPTIVE CONTROL SYSTEMS;

EID: 27844569885     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2005.1541428     Document Type: Article

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