Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques

Proceedings of the American Control Conference

Volumn , Issue , 2007, Pages 2459-2464

  Shihong, Ding ^a   Shihua, Li ^a  

^a SOUTHEAST UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; STABILIZATION;

ATTITUDE STABILIZATION; CONTROL LAWS; EXPONENTIAL CONVERGENCE; EXTERNAL DISTURBANCES; FEEDBACK CONTROL LAWS; FINITE TIME; FINITE TIME CONTROL; NUMERICAL SIMULATIONS; RIGID SPACECRAFT; RODRIGUES PARAMETERS; SETTLING TIME; SMALL REGION; SPACECRAFT ATTITUDE; TERMINAL SLIDING MODE (TSM);

SPACECRAFT;

EID: 46449111466     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.2007.4282259     Document Type: Conference Paper

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