Intelligent Flight Control of Combat Aircraft Based on Autoencoder

Bo Li, Peixin Gao, Shiyang Liang, Daqing Chen
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Abstract

The intelligent flight control of the aircraft is the key process in the air combat maneuver process. The traditional flight control method has many steps, long time and low precision, which have great drawbacks in the air combat process. In this paper, based on the background of deep learning, a flight control model based on autoencoder is proposed. Using the characteristics of autoencoder dimension reduction and feature extraction, the low-dimensional attitude parameters of high-dimensional aircraft can be extracted from high-dimensional flight attitude parameters. The eigenvalues are then automatically obtained through the neural network to change the attitude control of the aircraft. In this paper, the basic framework and training methods of the model are designed, and the influence of various parameters of the autoencoder network on the performance of the model is deeply studied. The experimental results show that the proposed model has better prediction accuracy and convergence performance than the traditional BP neural network, and achieves the purpose of intelligently and quickly obtaining flight attitude control to intelligently control aircraft flight.
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基于自编码器的作战飞机智能飞行控制
飞机的智能飞行控制是空战机动过程中的关键环节。传统的飞行控制方法步骤多、时间长、精度低,在空战过程中存在很大的弊端。本文以深度学习为背景,提出了一种基于自编码器的飞行控制模型。利用自编码器降维和特征提取的特点,可以从高维飞行姿态参数中提取高维飞机的低维姿态参数。然后通过神经网络自动获取特征值来改变飞行器的姿态控制。本文设计了模型的基本框架和训练方法,并深入研究了自编码器网络的各种参数对模型性能的影响。实验结果表明,该模型比传统的BP神经网络具有更好的预测精度和收敛性能,达到了智能快速获取飞行姿态控制的目的,实现了对飞机飞行的智能控制。
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