A novel approach to the automatic control of scale model airplanes

Abstract : This paper explores a new approach to the control of scale model airplanes as an extension of previous studies addressing the case of vehicles presenting a symmetry of revolution about the thrust axis. The approach is intrinsically nonlinear and, with respect to other contributions on aircraft nonlinear control, no small attack angle assumption is made in order to enlarge the controller's operating domain. Simulation results conducted on a simplified, but not overly simplistic, model of a small airliner illustrate the soundness of the approach.
Type de document :
Communication dans un congrès
53rd IEEE Conference on Decision and Control , Dec 2014, Los Angeles, United States. IEEE, pp.805 - 812, 2014, <10.1109/CDC.2014.7039480>


https://hal.archives-ouvertes.fr/hal-01342063
Contributeur : Tarek Hamel <>
Soumis le : mardi 5 juillet 2016 - 13:11:32
Dernière modification le : mercredi 6 juillet 2016 - 01:04:53

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Minh-Duc Hua, Daniele Pucci, Tarek Hamel, Pascal Morin, Claude Samson. A novel approach to the automatic control of scale model airplanes. 53rd IEEE Conference on Decision and Control , Dec 2014, Los Angeles, United States. IEEE, pp.805 - 812, 2014, <10.1109/CDC.2014.7039480>. <hal-01342063>

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