Nonlinear Control of Multi-Rotor Aerial Vehicles Based on the Zero-Moment Direction - LAAS - Laboratoire d'Analyse et d'Architecture des Systèmes Accéder directement au contenu
Communication Dans Un Congrès Année : 2017

Nonlinear Control of Multi-Rotor Aerial Vehicles Based on the Zero-Moment Direction

Résumé

A quaternion-based nonlinear control strategy is here presented to steer and keep a generic multi-rotor platform in a given reference position. Exploiting a state feedback structure, the proposed solution ensures the stabilization of the aerial vehicle so that its linear and angular velocity are zero and its attitude is constant. The main feature of the designed controller is the identification of a zero-moment direction in the feasible force space, i.e., a direction along which the control force intensity can be assigned independently of the control moment. The asymptotic convergence of the error dynamics is confirmed by simulation results on a hexarotor with tilted propellers.
Fichier principal
Vignette du fichier
2017i-MicCenZacFra-preprint.pdf (1.04 Mo) Télécharger le fichier
Origine : Fichiers produits par l'(les) auteur(s)
Loading...

Dates et versions

hal-01513229 , version 1 (24-04-2017)

Identifiants

  • HAL Id : hal-01513229 , version 1

Citer

Giulia Michieletto, Angelo Cenedese, Luca Zaccarian, Antonio Franchi. Nonlinear Control of Multi-Rotor Aerial Vehicles Based on the Zero-Moment Direction. IFAC World Congress 2017, Jul 2017, Toulouse, France. ⟨hal-01513229⟩
248 Consultations
67 Téléchargements

Partager

Gmail Facebook X LinkedIn More