Coupled LPV and flatness based approach for ARD guidance

Abstract : This paper presents a flatness and LPV-based methodology for an Apollo-Like Re-entry vehicle (ALRV) guidance. The main contribution is considered to be a proposition which converts the original nonlinear longitudinal ALRV flat model into a fictitious Linear Parameter Varying (LPV) model over which a LPV control law can be designed using a finite set of Linear Matrix Inequalities (LMIs). It is shown that the overall scheme is able to ensure robust stability and robust erformances when off-nominal conditions are present. Finally, simulation results are presented to demonstrate the potential of the proposed approach.
Type de document :
Communication dans un congrès
IFAC. 17th IFAC Symposium on Automatic Control in Aerospace, Jun 2007, TOULOUSE, France. pp.MO-PO-04, 2007, 〈10.3182/20070625-5-FR-2916.00033〉
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https://hal.archives-ouvertes.fr/hal-00180805
Contributeur : Franck Cazaurang <>
Soumis le : dimanche 21 octobre 2007 - 16:26:42
Dernière modification le : jeudi 11 janvier 2018 - 06:21:07

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Madjid Zerar, Franck Cazaurang, Ali Zolghadri. Coupled LPV and flatness based approach for ARD guidance. IFAC. 17th IFAC Symposium on Automatic Control in Aerospace, Jun 2007, TOULOUSE, France. pp.MO-PO-04, 2007, 〈10.3182/20070625-5-FR-2916.00033〉. 〈hal-00180805〉

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