Altitude control of a satellite using a feedback linearization

M Benenia 1 Hadj Batatia 2 Felix Antonio Claudio 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
Type de document :
Communication dans un congrès
Control and Automation Conference 2013: Uniting Problems and Solutions, Jun 2013, Glasgow, United Kingdom. IET, pp.ISBN: 978-1-84919-710-6, Control and Automation 2013: Uniting Problems and Solutions, IET Conference on. 〈10.1049/cp.2013.0018〉
Liste complète des métadonnées
https://hal-enac.archives-ouvertes.fr/hal-01422733
Contributeur : Laurence Porte <>
Soumis le : lundi 26 décembre 2016 - 18:55:54
Dernière modification le : mercredi 23 mai 2018 - 17:58:07

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ENAC | UNIV-TLSE3 | TDS-MACS | SMS | UNIV-TLSE2

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M Benenia, Hadj Batatia, Felix Antonio Claudio 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. IET, pp.ISBN: 978-1-84919-710-6, Control and Automation 2013: Uniting Problems and Solutions, IET Conference on. 〈10.1049/cp.2013.0018〉. 〈hal-01422733〉

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