An Application of Fuzzy PID Algorithm on Unmanned Helicopter Attitude Control

Author

Hou, Xin ; Li, Ping ; Fang, Zhou ; Han, Bo

Author_Institution

Nat. Lab. of Ind. Control Technol., Zhejiang Univ., Hangzhou

Volume

2

fYear

0

fDate

0-0 0

Firstpage

9129

Lastpage

9133

Abstract

the design of an attitude controller for an unmanned helicopter is addressed. The controller proposed is based on fuzzy PID algorithm, and is used for stable and robust roll, pitch, and yaw control. The fuzzy logic rules are established through a combination of expert knowledge and experiment data which is obtained from a real unmanned helicopter platform. Both the simulation and the experimental results verify the validity of fuzzy PID algorithm which integrates the advantage of fuzzy control and PID control

Keywords

aircraft control; attitude control; fuzzy control; fuzzy logic; helicopters; mobile robots; motion control; remotely operated vehicles; three-term control; PID control; fuzzy PID algorithm; fuzzy control; fuzzy logic rules; pitch control; roll control; unmanned helicopter attitude control; yaw control; Attitude control; Automation; Fuzzy control; Fuzzy logic; Helicopters; Industrial control; Intelligent control; Laboratories; Robust control; Three-term control; attitude control; fuzzy PID; unmanned helicopter;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on

Conference_Location

Dalian

Print_ISBN

1-4244-0332-4

Type

conf

DOI

10.1109/WCICA.2006.1713766

Filename

1713766