| ID | 30012 |
| FullText URL | |
| Author |
Inoue, Akira
Deng, Mingcong
Harima, Takanori
Nakano, Seiji
Ueki, Nobuyuki
|
| Abstract | In this paper, we consider the problem of attitude control of a helicopter experimental system. We design a nonlinear controller which combines nonlinear adaptive robust control and nonlinear feedback controls. Simulation and experimental results show the effectiveness of the proposed method. |
| Keywords | adaptive control
aircraft control
control system synthesis
feedback
helicopters
nonlinear control systems
robust control
|
| Note | Digital Object Identifier: 10.1109/ICIT.2005.1600825
Published with permission from the copyright holder. This is the institute's copy, as published in Industrial Technology, 2005. ICIT 2005. IEEE International Conference on, 14-17 Dec. 2005, Pages 1240-1245. Publisher URL:http://dx.doi.org/10.1109/ICIT.2005.1600825 Copyright © 2005 IEEE. All rights reserved. |
| Published Date | 2005-12
|
| Publication Title |
Industrial Technology
|
| Start Page | 1240
|
| End Page | 1245
|
| Content Type |
Journal Article
|
| language |
English
|
| Refereed |
True
|
| DOI | |
| Submission Path | industrial_engineering/68
|
