DocumentCode
3165424
Title
Sliding Mode Observer and Backstepping Control for a Quadrotor Unmanned Aerial Vehicles
Author
Madani, Tarek ; Benallegue, Abdelaziz
Author_Institution
Lab. d´´Ingenierie des Systemes de Versailles, Velizy
fYear
2007
fDate
9-13 July 2007
Firstpage
5887
Lastpage
5892
Abstract
In this paper, we propose a new approach of the backstepping control running parallel with a sliding mode observer for a quadrotor unmanned aerial vehicle. The sliding mode observer works as an observer of the quadrotor velocities and estimator of the external disturbances such as wind and parameter uncertainties. The controller objective is to achieve good tracking of desired (x,y,z) absolute positions and yaw angle while keeping the stability of the pitch and roll angles, in spite of the presence of bounded external disturbances. For this reason, the observer-controller is proposed to estimate the effect of external perturbations in order to compensate them. The design methodology is based on Lyapunov stability. Simulation results show the good performances and the robustness of the proposed observer-controller.
Keywords
Lyapunov methods; aircraft control; compensation; control system synthesis; mobile robots; observers; position control; remotely operated vehicles; robust control; tracking; uncertain systems; variable structure systems; velocity control; Lyapunov stability; absolute position tracking; backstepping control; design methodology; external disturbances; external perturbation compensation; observer-controller robustness; parameter uncertainties; pitch stability; quadrotor unmanned aerial vehicles; quadrotor velocities; roll angles stability; sliding mode observer; wind; yaw angle tracking; Backstepping; Helicopters; Linear feedback control systems; Noise measurement; Pollution measurement; Rotors; Sliding mode control; Stability; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2007. ACC '07
Conference_Location
New York, NY
ISSN
0743-1619
Print_ISBN
1-4244-0988-8
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2007.4282548
Filename
4282548
Link To Document