In this paper, a receding-horizon control, using systematic projection on a Chebyshev’s polynomial basis, is proposed for the stabilization of a rigid spacecraft operating with only two actuators. The proposed scheme privileges the speed of the algorithm. Simulations on SPOT4 spacecraft with a robustness test are provided.
Receding Horizon Stabilization of a Rigid Spacecraft With Two Actuators
Contributed by the Dynamic Systems, Measurement, and Control Division of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT, AND CONTROL. Manuscript received by the ASME Dynamic Systems and Control Division March 17, 1999; final revision, October 17, 2002. Associate Editor: G. Fahrenthold.
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Marchand , N., and Alamir , M. (September 18, 2003). "Receding Horizon Stabilization of a Rigid Spacecraft With Two Actuators ." ASME. J. Dyn. Sys., Meas., Control. September 2003; 125(3): 489–491. https://doi.org/10.1115/1.1591806
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