A simple output-based stabilizing controller for attitude regulation of a rigid spacecraft with gas-jet actuators

Proceedings of the American Control Conference

Volumn 3, Issue , 2001, Pages 2345-2350

  Ailon, Amit ^a   Grinberg, Boris ^a   Segev, Reuven ^a   Gil, Michael I ^a  

^a BEN GURION UNIVERSITY OF THE NEGEV   (Israel)

Author keywords

Attitude stabilization; Model uncertainty; Output based controller; Roll pitch yaw angles

Indexed keywords

ACTUATORS; NONLINEAR SYSTEMS; SPACECRAFT; SYSTEM STABILITY; TORQUE CONTROL;

ATTITUDE STABILIZATION; OUTPUT-BASED CONTROLLER; ROLL-PITCH-YAW ANGLES;

CONTROL EQUIPMENT;

EID: 0034842703     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2001.946102     Document Type: Article

References (11)

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