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2013 Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control
Wendong Gai, Honglun Wang, Jing Zhang, Yuxia Li
J. Appl. Math. 2013(SI16): 1-12 (2013). DOI: 10.1155/2013/452653

Abstract

An adaptive neural network dynamic inversion with prescribed performance method is proposed for aircraft flight control. The aircraft nonlinear attitude angle model is analyzed. And we propose a new attitude angle controller design method based on prescribed performance which describes the convergence rate and overshoot of the tracking error. Then the model error is compensated by the adaptive neural network. Subsequently, the system stability is analyzed in detail. Finally, the proposed method is applied to the aircraft attitude tracking control system. The nonlinear simulation demonstrates that this method can guarantee the stability and tracking performance in the transient and steady behavior.

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Wendong Gai. Honglun Wang. Jing Zhang. Yuxia Li. "Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control." J. Appl. Math. 2013 (SI16) 1 - 12, 2013. https://doi.org/10.1155/2013/452653

Information

Published: 2013
First available in Project Euclid: 14 March 2014

zbMATH: 06950684
Digital Object Identifier: 10.1155/2013/452653

Rights: Copyright © 2013 Hindawi

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Vol.2013 • No. SI16 • 2013
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