A comparative design of satellite attitude control system with reaction wheel

Proceedings - First NASA/ESA Conference on Adaptive Hardware and Systems, AHS 2006

Volumn 2006, Issue , 2006, Pages 359-362

  Shengmin, Ge ^a   Hao, Cheng ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; FEEDBACK CONTROL; LOGIC DESIGN;

REACTION WHEELS; SATELLITE ATTITUDE CONTROL SYSTEMS; SPEED FEEDBACK COMPENSATION;

SATELLITE COMMUNICATION SYSTEMS;

EID: 33845575629     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AHS.2006.2     Document Type: Conference Paper

References (3)

1. Y. Hu, H. Zhao and C. Tang, "Flywheel state feedback control system", Control Engineering, no. 3, 1991, pp. 4-14.
2. C. Canudas, H. Olsson, K.J. Äström, and P. Lischinsky, "A new model for control of systems with friction", IEEE Transactions on Automatic Control, vol 40, no. 3, 1995, pp. 419-425.
3. Y. Kim, Y. Park, H. Bang, and M. Tahk, "Covariance analysis of spacecraft attitude control system", in Proc. IEEE Conf. on Control Applications, vol. 1, Istanbul, Turkey, June 2003, pp. 480-485.