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 :
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