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Altitude control of a satellite using a feedback linearization

Abstract : This study is dedicated to the problem of non linear attitude control for a rigid large angle maneuver satellite. The non linear control method is based upon the linearization of the input-output of the system, also called feedback linearization, via state feedback. The output function is chosen amongst the attitude quaternion parameters.
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https://hal-enac.archives-ouvertes.fr/hal-01422733
Contributor : Laurence Porte <>
Submitted on : Monday, December 26, 2016 - 6:55:54 PM
Last modification on : Thursday, March 26, 2020 - 6:41:41 PM

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M Benenia, Hadj Batatia, Felix Mora-Camino, Malek Benslama. Altitude control of a satellite using a feedback linearization. Control and Automation Conference 2013: Uniting Problems and Solutions, Jun 2013, Glasgow, United Kingdom. pp.ISBN: 978-1-84919-710-6, ⟨10.1049/cp.2013.0018⟩. ⟨hal-01422733⟩

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