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-TCI - Traitement et Compréhension d’Images
3 ENAC - Ecole Nationale de l'Aviation Civile
4 LET - Laboratoire électromagnetisme et télécommunications Université de Constantine Algérie

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.

Mots clés: sliding mode control; spacecraft attitude control; feedback linearization; quaternion

Domaines: Sciences de l'ingénieur [physics]; Automatique / Robotique

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⟩