DocumentCode
2656532
Title
Hybrid PID velocity control for an unmanned helicopter based on single neuron
Author
Jiande, Wu ; Zhou, Wan ; Xin, Xiong
Author_Institution
Sch. of Inf. Eng. & Autom., Kunming Univ. of Sci. & Technol., Kunming
fYear
2008
fDate
16-18 July 2008
Firstpage
295
Lastpage
299
Abstract
The miniature unmanned helicopter exhibits a complex and nonlinear dynamic behavior, open- loop unstable and a high degree of inter-axis coupling. This paper describes a hybrid PID velocity control method based on single neuron for an unmanned helicopter. This method possesses both the simple structure of PID controller, and adjusting papameters on-line by intelligent technique. The application results of an unmanned helicopter show that the proposed controller can have helicopter achieve stable attitude in hover and improve the stability of the attitude control system. And the fine robustness for imprecise helicopter model is accounted for.
Keywords
aircraft control; attitude control; helicopters; mobile robots; neurocontrollers; remotely operated vehicles; stability; three-term control; velocity control; attitude control system; hybrid PID velocity control; intelligent technique; nonlinear dynamic behavior; single neuron; unmanned helicopter; Attitude control; Control systems; Couplings; Helicopters; Intelligent structures; Neurons; Open loop systems; Stability; Three-term control; Velocity control; Adjusting paramenters on-line; Hybrid PID velocity control; Robustness; Unmanned helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location
Kunming
Print_ISBN
978-7-900719-70-6
Electronic_ISBN
978-7-900719-70-6
Type
conf
DOI
10.1109/CHICC.2008.4604954
Filename
4604954
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