AustralieFrV1, Main, Exploration, bibRecord, 007756

Longitudinal modelling and control of a flapping-wing micro aerial vehicle

Identifieur interne : 007756 ( Main/Exploration ); précédent : 007755; suivant : 007757

Longitudinal modelling and control of a flapping-wing micro aerial vehicle

Auteurs : Thomas Rakotomamonjy [France] ; Mustapha Ouladsine [France] ; Thierry Le Moing [France]

Source :

Control engineering practice [ 0967-0661 ] ; 2010.

RBID : Pascal:10-0442069

Descripteurs français

Pascal (Inist)
- Engin volant autonome, Dynamique solide, Système périodique, Commande non linéaire, Commande boucle fermée, Synthèse commande, Stabilisation, Aérodynamique, Battement alaire, Microaéronef, Robot mobile, Pilotage, Force aérodynamique, Aile, Structure périodique, Ecoulement instationnaire, Modélisation, Modèle dynamique, Modèle animal, Méthode moyenne.
Wicri :
- topic : Aérodynamique.

English descriptors

KwdEn :
- Aerodynamic force, Aerodynamics, Animal model, Averaging method, Closed loop control, Control synthesis, Dynamic model, Microaircraft, Mobile robots, Modelling, Non linear control, Periodic structures, Periodic system, Pilotage, Solid dynamic, Stabilization, Unmanned aerial vehicle, Unsteady flow, Wing, Wing beat.

Abstract

A simulation model, flight-dynamics oriented, of a flapping-wing micro aerial vehicle (MAV) is presented here. The model, based on animal flapping flight, integrates the aerodynamic forces computed along each wing to determine the global motion of the MAV with respect to an inertial reference frame. After some analytic simplifications, and taking into account the periodic nature of the system inputs, an averaged model is derived, and a simple, nonlinear closed-loop control law is designed for the dynamics along the vertical and pitch axis, allowing an efficient stabilization of the naturally unstable model.

Affiliations:

Links toward previous steps (curation, corpus...)

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to stream PascalFrancis, to step Curation: 003C38
to stream PascalFrancis, to step Checkpoint: 002285
to stream Main, to step Merge: 007D53
to stream Main, to step Curation: 007756

Le document en format XML

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<term>Commande non linéaire</term>
<term>Commande boucle fermée</term>
<term>Synthèse commande</term>
<term>Stabilisation</term>
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<term>Pilotage</term>
<term>Force aérodynamique</term>
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<front><div type="abstract" xml:lang="en">A simulation model, flight-dynamics oriented, of a flapping-wing micro aerial vehicle (MAV) is presented here. The model, based on animal flapping flight, integrates the aerodynamic forces computed along each wing to determine the global motion of the MAV with respect to an inertial reference frame. After some analytic simplifications, and taking into account the periodic nature of the system inputs, an averaged model is derived, and a simple, nonlinear closed-loop control law is designed for the dynamics along the vertical and pitch axis, allowing an efficient stabilization of the naturally unstable model.</div>
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Longitudinal modelling and control of a flapping-wing micro aerial vehicle

Longitudinal modelling and control of a flapping-wing micro aerial vehicle

Source :

Descripteurs français

English descriptors

Abstract

Links toward previous steps (curation, corpus...)

Le document en format XML

Pour manipuler ce document sous Unix (Dilib)

Pour mettre un lien sur cette page dans le réseau Wicri