Coupled LPV and Flatness-based Approach for Space Reentry Vehicles Guidance

Abstract : This paper presents an Linear Parameter Varying guidance method for the hypersonic phase of a space re-entry vehicle. The suggested guidance scheme, relying on Flatness approach, is applied to the nonlinear model of the European Atmospheric Re-entry Demonstrator. It is shown that the overall guidance scheme achieves robust stability and performance, even in the presence of entry point kinematics dispersions. The design problem is formulated and solved using a finite set of Linear Matrix Inequalities. Finally, Monte Carlo simulation results are presented to demonstrate the effectiveness of the suggested approach.
Type de document :
Article dans une revue
IEE Proceedings. Control Theory and Applications, 2009, 3 (8), pp.1081-1092. 〈10.1049/iet-cta.2008.0057〉
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https://hal.archives-ouvertes.fr/hal-00367295
Contributeur : Franck Cazaurang <>
Soumis le : mardi 10 mars 2009 - 21:26:07
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 Space Reentry Vehicles Guidance. IEE Proceedings. Control Theory and Applications, 2009, 3 (8), pp.1081-1092. 〈10.1049/iet-cta.2008.0057〉. 〈hal-00367295〉

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