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Advanced reaction wheel controller for attitude control of spacecraft
Authors:K Tsuchiya  M Inoue  N Wakasuqi  T Yamaguchi  
Institution:

Mitsubishi Electric Corporation, 80 Nakomo, Minami Shimizu, Amagasaki City, Hyogo, Japan 661

Abstract:A design procedure is presented for an attitude control system consisting of a momentum wheel and a reaction wheel. Control laws are designed for this system using modern control techniques. The observer based method produces a control scheme which achieves a good transient response.
Keywords:
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