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