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
Link To Document :
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