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Altitude control of a satellite using a feedback linearization

M Benenia 1 Hadj Batatia 2 Felix Mora-Camino 3 Malek Benslama 4
1 University of Constantine
2 IRIT - Institut de recherche en informatique de Toulouse
3 ENAC - Ecole Nationale de l'Aviation Civile
4 LET - Laboratoire électromagnetisme et télécommunications Université de Constantine Algérie
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.
Keywords : sliding mode control spacecraft attitude control feedback linearization quaternion
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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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ENAC | CNRS | TDS-MACS | SMS | UNIV-TLSE2 | UNIV-TLSE3 | UT1-CAPITOLE | IRIT

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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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