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An evolutionary optimizing approach to neural network architecture for improving identification and modeling of aircraft nonlinear dynamics

机译:神经网络架构的进化优化方法,用于改善飞机非线性动力学的辨识和建模

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摘要

In this paper, modified genetic algorithm has been used as a simultaneous optimizer of recurrent neural network to improve identification and modeling of aircraft nonlinear dynamics. Weighted connections, network architecture, and learning rules are features that play important roles in the quality of neural networks training and their generalizability in order to model nonlinear systems. Therefore, the main focus of this paper is to apply appropriate evolutionary methods in order to simultaneously optimize the parameters of neural networks for the improvement identification and modeling of aircraft nonlinear dynamics. To validate this study, the results have been compared with the recorded data from a fourth generation highly maneuverable fighter aircraft flight test. Furthermore, having been compared to normal genetic algorithm, the results of the present study have showed significant improvement of the neural networks generalization which leads to better identification and modeling of aircraft nonlinear dynamics.
机译:本文采用改进的遗传算法作为递归神经网络的同步优化器,以改进飞机非线性动力学的辨识和建模。加权连接,​​网络体系结构和学习规则是功能,它们在神经网络训练的质量及其可推广性中发挥重要作用,从而为非线性系统建模。因此,本文的主要重点是应用适当的进化方法,以便同时优化神经网络的参数,以改进飞机非线性动力学的识别和建模。为了验证这项研究,已将结果与第四代高度机动战斗机飞行测试的记录数据进行了比较。此外,与常规遗传算法相比,本研究的结果显示神经网络泛化的显着改进,这导致对飞机非线性动力学的更好识别和建模。

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