DocumentCode :
2418987
Title :
A Two-Rule-based Fuzzy Logic Controller for Contrarotating Coaxial Rotors UAV
Author :
Vidolov, Boris ; De Miras, Jérôme ; Bonnet, Stéphane
Author_Institution :
Univ. de Technol. de Compiegne, Compiegne
fYear :
0
fDate :
0-0 0
Firstpage :
1563
Lastpage :
1569
Abstract :
This paper presents the development and hardware experimentations for the attitude control of a UAV. The AURYON system consists of a particular contrarotating coaxial rotors aircraft, an embedded and a ground control systems, a distributed real-time 3D simulator based on The Mathworks xPC-Target toolbox and Laminar Research X-Plane flight simulator. The controller developed for the attitude and altitude stabilization is based on a two-rule fuzzy controller. A parameter-tuning procedure, using a real-time 3D simulator is proposed. The performances of the UAV mechatronic system are illustrated trough real demonstrator experimentations.
Keywords :
aerospace simulation; aircraft control; attitude control; distributed control; embedded systems; fuzzy control; helicopters; remotely operated vehicles; stability; AURYON system; Mathworks xPC-Target toolbox; altitude stabilization; attitude control; contrarotating coaxial rotors aircraft; embedded system; ground control system; laminar research x-plane flight simulator; real-time 3D simulator; two rule-based fuzzy logic controller; unmanned aerial vehicle; Aerospace control; Aerospace simulation; Aircraft; Coaxial components; Control system synthesis; Distributed control; Fuzzy logic; Hardware; Real time systems; Unmanned aerial vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fuzzy Systems, 2006 IEEE International Conference on
Conference_Location :
Vancouver, BC
Print_ISBN :
0-7803-9488-7
Type :
conf
DOI :
10.1109/FUZZY.2006.1681916
Filename :
1681916
Link To Document :
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