Control of input redundant affine systems : application to runway axis tracking at landing

Fabrice Villaumé 1, 2 P Fabre 2 S.N. Singh 3 Felix Antonio Claudio Mora-Camino 4
1 LAAS - Laboratoire d'analyse et d'architecture des systèmes [Toulouse]
2 Airbus [France]
3 Department of Electrical and Computer Engineering [Las Vegas]
4 LAAS-DISCO - Équipe DIagnostic, Supervision et COnduite
LAAS - Laboratoire d'analyse et d'architecture des systèmes [Toulouse]
Abstract : Among the specific methodologies for the control of nonlinear systems, Nonlinear Dynamic Inversion has gained considerable popularity over the last decade. A complete theory is now available for the design of feedback control laws which associates to a nonlinear system a dynamic linear input-output relationship easily inversible. Nevertheless, the possible saturation of the actuators has not been taken into account. In order to solve this limitation, a supervision strategy is proposed in the case of input redundant affine systems. In this paper, while a generic force and moment nonlinear inverse control laws is displayed, the viability and efficiency of the proposed supervision strategy is highlighted.
keyword : aircraft control automatic control controls laws inverse dynamic control nonlinear control saturation supervision
Type de document :
Communication dans un congrès
ACA 2001, 15th IFAC Symposium on Automatic Control in Aerospace, Sep 2001, Bologna, Italy. pp xxxx, 2001
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https://hal-enac.archives-ouvertes.fr/hal-01022427
Contributeur : Laurence Porte <>
Soumis le : jeudi 10 juillet 2014 - 15:54:43
Dernière modification le : mercredi 28 février 2018 - 10:23:12
Document(s) archivé(s) le : vendredi 10 octobre 2014 - 11:43:21

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  • HAL Id : hal-01022427, version 1

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Fabrice Villaumé, P Fabre, S.N. Singh, Felix Antonio Claudio Mora-Camino. Control of input redundant affine systems : application to runway axis tracking at landing. ACA 2001, 15th IFAC Symposium on Automatic Control in Aerospace, Sep 2001, Bologna, Italy. pp xxxx, 2001. 〈hal-01022427〉

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