Design for Adaptive Flight/Propulsion Control System Based on Wavelet Neural Networks
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Design for Adaptive Flight/Propulsion Control System Based on Wavelet Neural Networks
Vol. 18, Issue 3, (2003)
作者机构:
南京航空航天大学自动化学院,江苏,南京,210016
作者简介:
基金信息:
DOI:
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Published:2003
稿件说明:
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CHEN Mou, JIANG Chang-sheng, WU Qing-xian, et al. Design for Adaptive Flight/Propulsion Control System Based on Wavelet Neural Networks[J]. 2003, 18(3).
DOI:
CHEN Mou, JIANG Chang-sheng, WU Qing-xian, et al. Design for Adaptive Flight/Propulsion Control System Based on Wavelet Neural Networks[J]. 2003, 18(3).DOI:
Design for Adaptive Flight/Propulsion Control System Based on Wavelet Neural Networks
an adaptive H∞ control method based on wavelet neural network is proposed for the nonlinear uncertain systems. The controller is made up of equivalent controller and H∞ controller. The wavelet neural networks are used to approximate the nonlinear functions and the approximation errors of the neural networks are introduced to the adaptive law in order to improve the quality of the system. H∞ controller is designed for attenuating the external disturbance and approximation errors of the neural networks. The controller can not only guarantee the stability of the overall system
but also attenuate the effect of the external disturbance and approximation errors of the neural networks to a prescribed level. At last
based on forgoing designed control method a flight/propulsion control system has been designed and high angle attack flight simulation has been made. The simulation results suggest that the flight/propulsion control system is valid. They validate the availability of this control method for the uncertain nonlinear system too.