Robust Altitude and Attitude Sliding Mode ...
Type de document :
Communication dans un congrès avec actes
Titre :
Robust Altitude and Attitude Sliding Mode Controllers for Quadrotors
Auteur(s) :
Abci, Boussad [Auteur]
Centre de Recherche en Informatique, Signal et Automatique de Lille - UMR 9189 [CRIStAL]
Zheng, Gang [Auteur]
Non-Asymptotic estimation for online systems [NON-A]
Deformable Robots Simulation Team [DEFROST ]
Efimov, Denis [Auteur]
Non-Asymptotic estimation for online systems [NON-A]
El Badaoui El Najjar, Maan [Auteur]
Centre de Recherche en Informatique, Signal et Automatique de Lille - UMR 9189 [CRIStAL]
Centre de Recherche en Informatique, Signal et Automatique de Lille - UMR 9189 [CRIStAL]
Zheng, Gang [Auteur]
Non-Asymptotic estimation for online systems [NON-A]
Deformable Robots Simulation Team [DEFROST ]
Efimov, Denis [Auteur]
Non-Asymptotic estimation for online systems [NON-A]
El Badaoui El Najjar, Maan [Auteur]
Centre de Recherche en Informatique, Signal et Automatique de Lille - UMR 9189 [CRIStAL]
Titre de la manifestation scientifique :
IFAC World Congress
Ville :
Toulouse
Pays :
France
Date de début de la manifestation scientifique :
2017-07-10
Mot(s)-clé(s) en anglais :
Sliding-mode control
robustness
stability analysis
Lyapunov stability
quadrotors
Newton-Euler equations
robustness
stability analysis
Lyapunov stability
quadrotors
Newton-Euler equations
Discipline(s) HAL :
Informatique [cs]/Automatique
Résumé en anglais : [en]
This paper considers the problem of attitude and altitude control of quadrotors using the sliding mode control theory. The mathematical model of the quadrotor is derived using the Euler-Newton formalism with extended ...
Lire la suite >This paper considers the problem of attitude and altitude control of quadrotors using the sliding mode control theory. The mathematical model of the quadrotor is derived using the Euler-Newton formalism with extended assumptions on disturbing aerodynamical forces (not necessary uniformly bounded). The proposed control demonstrates an enhanced robustness against such disturbances. The comparison between the classical controller and the proposed one is demonstrated analytically, through Lyapunov theory, and in simulations to validate the proposed sliding mode control algorithm.Lire moins >
Lire la suite >This paper considers the problem of attitude and altitude control of quadrotors using the sliding mode control theory. The mathematical model of the quadrotor is derived using the Euler-Newton formalism with extended assumptions on disturbing aerodynamical forces (not necessary uniformly bounded). The proposed control demonstrates an enhanced robustness against such disturbances. The comparison between the classical controller and the proposed one is demonstrated analytically, through Lyapunov theory, and in simulations to validate the proposed sliding mode control algorithm.Lire moins >
Langue :
Anglais
Comité de lecture :
Oui
Audience :
Internationale
Vulgarisation :
Non
Collections :
Source :