Partial linearization of the PVTOL aircraft with internal stability

The planar vertical take-off and landing (PVTOL) aircraft is worked out by inspecting the various feedback linearization solutions. Partial linearizations of the state space are performed, which ensure the stability of the associated internal dynamics. The results are obtained through the search of dummy outputs with a 0-dimensional, 1-dimensional or 2-dimensional zero-dynamics that are stable.

Mots clés

nonlinear partial linearization algebraic method internal dynamics PVTOL stabilization MIMO underactuated non-minimum phase zero-dynamics

Domaines

Automatique / Robotique

Fichier principal

cdc_2013_hal.pdf (179.39 Ko)

Origine	Fichiers produits par l'(les) auteur(s)

Vincent Léchappé : Connectez-vous pour contacter le contributeur

https://hal.science/hal-00858102

Soumis le : lundi 25 janvier 2016-11:08:56

Dernière modification le : vendredi 5 janvier 2024-03:22:47

Archivage à long terme le : mardi 26 avril 2016-10:51:14

Dates et versions

hal-00858102 , version 1 (25-01-2016)

Identifiants

HAL Id : hal-00858102 , version 1
DOI : 10.1109/CDC.2013.6760268

Citer

Vincent Léchappé, Yannick Aoustin, L. Marquez Martinez, Claude Moog. Partial linearization of the PVTOL aircraft with internal stability. 52nd Conference on Decision and Control, Dec 2013, Florence, Italy. ⟨10.1109/CDC.2013.6760268⟩. ⟨hal-00858102⟩

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UNIV-NANTES CNRS EC-NANTES IRCCYN IRCCYN-ADTSI UNAM TDS-MACS LS2N NANTES-UNIVERSITE

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