Robust control system for Spacecraft Motion Trajectory

Abstract : In aerospace field the economic realization of a spacecraft is one of the main objectives which should be accomplished by conceiving the optimal propulsion system and best control programs. This article focuses on the implementation of uncertain control system theory and development of a robust control system of Spacecraft Motion Trajectory (SMT). The proposed strategy involves the nonlinear mathematical model of SMT expressed in the central field, which is linearized by the Taylor expansion, and model reference Adaptive Control Approach (ACA) with the second Lyapunov method to offer a high rate and unfailing performance in the functioning. The efficiencies of the linearization procedure and the control approach are theoretically investigated through some realistic simulations and tests under Matlab.
Type de document :
Article dans une revue
European Journal of Pure and Applied Mathematics, Mathematical Reviews, 2014, 7 (3), pp.289-303
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https://hal.inria.fr/hal-01017472
Contributeur : Hassen Fourati <>
Soumis le : mercredi 2 juillet 2014 - 15:41:23
Dernière modification le : lundi 5 octobre 2015 - 16:59:19

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  • HAL Id : hal-01017472, version 1

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Zarina Samigulina, Olga Shiryayeva, Galina Samigulina, Hassen Fourati. Robust control system for Spacecraft Motion Trajectory. European Journal of Pure and Applied Mathematics, Mathematical Reviews, 2014, 7 (3), pp.289-303. <hal-01017472>

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