DocumentCode
1111439
Title
Adaptive Neural Network Control for Helicopters in Vertical Flight
Author
Tee, Keng Peng ; Ge, Shuzhi Sam ; Tay, Francis E H
Author_Institution
Dept. of Electr. & Comput. Eng., Nat. Univ. of Singapore, Singapore
Volume
16
Issue
4
fYear
2008
fDate
7/1/2008 12:00:00 AM
Firstpage
753
Lastpage
762
Abstract
In this brief, robust adaptive neural network (NN) control is presented for helicopters in vertical flight, with dynamics in single-input-single-output (SISO) nonlinear nonaffine form. Based on the use of the implicit function theorem and the mean value theorem, we propose a constructive approach for adaptive NN control design with guaranteed stability. Considering both full-state and output feedback cases, it is shown that the output tracking error converges to a small neighborhood of the origin, while the remaining closed-loop signals remain bounded. The simulation study demonstrates the effectiveness of the proposed control.
Keywords
adaptive control; aircraft control; closed loop systems; control system synthesis; helicopters; neurocontrollers; nonlinear control systems; robust control; state feedback; vehicle dynamics; full-state feedback; guaranteed stability; helicopter control; output feedback; robust adaptive neural network control; single-input-single-output nonlinear nonaffine form; tracking error; vertical flight; Adaptive control; helicopters; neural networks (NNs); output feedback; uncertain systems;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2007.912242
Filename
4476154
Link To Document