DocumentCode
1924397
Title
Development of autonomous flight control system for unmanned helicopter by use of neural networks
Author
Nakanishi, Hiroaki ; Inoue, Koichi
Author_Institution
Graduate Sch. of Eng., Kyoto Univ., Japan
Volume
3
fYear
2003
fDate
20-24 July 2003
Firstpage
2400
Abstract
This paper describes methods to develop autonomous flight control systems for UAVs. The unmanned helicopter "RMAX" produced by Yamaha Motor Co., Ltd. is used in this study. It was difficult to develop flight control systems, because the dynamics of the helicopter is nonlinear. An efficient method to design controllers by training neural networks is proposed in this paper. It is easy to use trained neural network together with online training neural networks or adaptive controllers to compensate undesirable effects which are not modeled or sudden changes of the target and environment, therefore the control system can be highly reliable. Results of flight experiments are shown to demonstrate the effectiveness of our approach.
Keywords
adaptive control; aircraft control; helicopters; learning (artificial intelligence); neurocontrollers; remotely operated vehicles; RMAX; UAV; Yamaha Motor; adaptive controller; autonomous flight control system; neural network; nonlinear dynamics; online training; reliability; unmanned air vehicle; unmanned helicopter; Aerospace control; Aerospace engineering; Chemicals; Control systems; Design methodology; Helicopters; Neural networks; Robust control; Spraying; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Neural Networks, 2003. Proceedings of the International Joint Conference on
ISSN
1098-7576
Print_ISBN
0-7803-7898-9
Type
conf
DOI
10.1109/IJCNN.2003.1223788
Filename
1223788
Link To Document