DocumentCode
495120
Title
The Design and Development of a Flight Control System for a Small Size Unmanned Helicopter
Author
Gong, Zhengbang ; Feng, Wei ; Gao, Tongyue ; Luo, Jun
Author_Institution
Dept. of Precision Mech. Eng., Shanghai Univ., Shanghai, China
Volume
1
fYear
2009
fDate
21-22 May 2009
Firstpage
103
Lastpage
106
Abstract
Small size unmanned helicopter has found diverse applications for both civil and military missions. In order to develop a flight robot based on a small size unmanned remotely controlled helicopter, a flight control system is presented in this paper. The hardware and software of the system are designed. The design goal is to have the helicopter achieve stable hover. As the kernel of the system, the flight control strategies are described which based on artificial neural network and human operator´s skill. The processed flight data are used to train and validate a multilayer artificial neural network offline, and then the trained artificial neural network is reconstructed in the flight control system for control strategies.
Keywords
aerospace robotics; aircraft control; helicopters; neural nets; remotely operated vehicles; flight control system; flight data; flight robot; human operator skill; multilayer artificial neural network offline; small size unmanned remotely controlled helicopter; Aerospace control; Application software; Artificial neural networks; Control systems; Hardware; Helicopters; Military aircraft; Robots; Size control; Software systems; Artificial Neural Network; flight control system; small size unmanned helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Information and Computing Science, 2009. ICIC '09. Second International Conference on
Conference_Location
Manchester
Print_ISBN
978-0-7695-3634-7
Type
conf
DOI
10.1109/ICIC.2009.33
Filename
5169550
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