LMI-based design of a structured direct adaptive satellite attitude control with actuator rate feedback - Équipe Méthodes et Algorithmes en Commande
Conference Papers Year : 2015

LMI-based design of a structured direct adaptive satellite attitude control with actuator rate feedback

Abstract

Satellite attitude control of a microsatellite of the CNES Myriade series is considered. Reduction of saturations on the angular rate of reaction wheel actua-tors is addressed by means of control gain adaptation. The proposed adaptive control design has the following features: performances of the adaptive law are the same as those of a predefined linear time-invariant control when the state is close to the equilibrium; adaptation is structured allowing to include engineering considerations in the design; asymptotic stability is guaranteed based on Lyapunov arguments; fine tuning of adaptive gains is made by linear matrix inequality based convex optimization. The novelties compared to previous results are: to include mag-netotorquer information in the adaptive scheme; to provide a simplified design procedure.

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Dates and versions

hal-01388191 , version 1 (28-10-2016)

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Harmonie Leduc, Dimitri Peaucelle, Christelle Pittet-Mechin. LMI-based design of a structured direct adaptive satellite attitude control with actuator rate feedback. 2015 IEEE 54th Annual Conference on Decision and Control (CDC 2015), Dec 2015, Osaka, Japan. ⟨10.1109/CDC.2015.7402732⟩. ⟨hal-01388191⟩
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