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导弹与制导技术

基于小波神经网络反演的制导控制一体化设计

  • 马晨 ,
  • 赵国荣 ,
  • 冯淞琪
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  • 海军航空工程学院,山东烟台 264001

马晨(1989-),男,陕西西安人,硕士研究生,研究方向:飞行器先进技术。

收稿日期: 2014-02-28

  网络出版日期: 2025-05-26

基金资助

国家自然科学基金(61473306)

Design of Integrated Guidance and Control Based on Wavelet Neural Network Backsteppting Method

  • MA Chen ,
  • ZHAO Guorong ,
  • FENG Songqi
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  • Naval Aeronautical and Astronautical University, Shandong Yantai 264001, China

Received date: 2014-02-28

  Online published: 2025-05-26

摘要

设计了一种适用于制导控制一体化的小波神经网络反演方法(WNNBM)。首先,将目标运动学特性与导弹动力学的系统模型相结合,建立并简化了俯仰通道制导控制一体化模型,综合设计制导律与控制器;其次,利用自适应反演方法对一体化控制器进行总体设计,并针对一体化模型简化程度高,未建模动态难以确定的特点,引入小波神经网络(WNN)逼近系统模型;最后,进行弹道仿真。结果表明,该方法可以有效打击目标,提高系统性能。

本文引用格式

马晨 , 赵国荣 , 冯淞琪 . 基于小波神经网络反演的制导控制一体化设计[J]. 弹箭与制导学报, 2015 , 35(1) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2015.01.001

Abstract

A wavelet neural networks backsteppting method (WNNBM) was designed for integrated guidance and control. First, the integrative control model of missile was built and simplified, the target kinematics characteristics and missile dynamics model of the system were combined, and guidance law and controller were put together. Controller was designed for integrative model by using backstepping method (BSM), in view of high degree of model simplification and uncertainty of unmodeled dynamics, wavelet neural networks (WNN) in backstepping method was used. Finally, trajectory simulations were carried out and simulation results show the method can hit the target effectively and improve maneuverability and efficiency of missile.

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参考文献

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