不确定气动条件下高性能飞机智能动态面控制策略

IF 1.6 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Manish Sharma, Somya Dubey, Sachin Puntambekar, Vinit Gupta
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引用次数: 0

摘要

高性能飞行器姿态跟踪中存在动力学的不确定性和执行器的饱和问题,对精确控制策略的制定提出了严峻的挑战。本文提出了一种自适应观测器-控制器策略来解决这些问题。利用小波神经网络(WNN)对六自由度飞行器非线性动力学中的功能不确定性进行估计。小波神经网络采用小波作为激活函数,实现了较好的学习特性。该系统非常接近实时模型,但由于外部随机参数导致的建模不确定性和执行器饱和,使得控制设计非常复杂。本文的新颖之处在于通过改进的深度学习网络、小波神经网络和各自的控制器-观测器策略来估计这些高度随机的非线性不确定性。通过仿真分析来评估本文提出的理论发展的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Intelligent dynamic surface control strategy for high-performance aircraft subject to uncertain aerodynamics
The uncertain dynamics and actuator saturation in attitude tracking of high-performance aircrafts have posed a serious challenge in deriving an accurate control strategy. This paper presents an adaptive observer-controller strategy to deal with these problems. It uses wavelet neural networks (WNN) to estimate the functional uncertainties in the nonlinear dynamics of the aircraft with 6 degree of freedom (6 DoF). WNN uses wavelets as activation function to achieve superior learning characteristics. This system is very close to the real time model as it is subjected to the modelling uncertainties and actuator saturation owing to the external random parameters which makes the control design very complicated. The novelty of this paper lies within the estimation of these highly random nonlinear uncertainties by the modified deep learning network, WNN and the respective controller-observer strategy. Simulation analysis has been performed to evaluate the performance of the theoretical development presented in the paper.
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来源期刊
International Journal of Intelligent Engineering Informatics
International Journal of Intelligent Engineering Informatics COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS-
CiteScore
1.20
自引率
27.00%
发文量
0
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