Optimal control for spacecraft to rendezvous with a tumbling satellite in a close range

IEEE International Conference on Intelligent Robots and Systems

Volumn , Issue , 2006, Pages 4109-4114

  Ma, Zhanhua ^a   Ma, Ou ^b   Shashikanth, Banavara N ^b  

^a Princeton University   (United States)

^b Horeshoe Cir Jett Hall   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; OPTIMAL CONTROL SYSTEMS; ORBITS; SATELLITES; SPACE RENDEZVOUS; TORQUE CONTROL;

OPTIMAL TRAJECTORIES; PONTRYAGIN'S MAXIMUM PRINCIPLE; SATELLITE CHASING PROBLEM; TUMBLING SATELLITES;

MOTION PLANNING;

EID: 34250637240     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/IROS.2006.281877     Document Type: Conference Paper

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