Flexible spacecraft attitude maneuver by application of sliding mode control

Acta Astronautica

Volumn 57, Issue 11, 2005, Pages 841-850

  Bang, Hyochoong ^a   Ha, Cheol Keun ^b   Kim, Jin Hyoung ^c  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b University of Ulsan   (South Korea)

^c Chungnam National University   (South Korea)

Author keywords

Boundary torque; Flexible spacecraft; Output feedback; Sliding mode control; Spacecraft attitude control

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; MANEUVERABILITY; MATHEMATICAL MODELS; SLIDING MODE CONTROL; TORQUE CONTROL; VELOCITY CONTROL;

BOUNDARY TORQUE; FLEXIBLE SPACECRAFT; OUTPUT FEEDBACK; SPACECRAFT ATTITUDE CONTROL;

SPACECRAFT;

EID: 27644513319     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2005.04.009     Document Type: Article

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