Trajectory prediction algorithm of ballistic missile driven by data and knowledge

IF 5 Q1 ENGINEERING, MULTIDISCIPLINARY
Hongyan Zang, Changsheng Gao, Yudong Hu, Wuxing Jing
{"title":"Trajectory prediction algorithm of ballistic missile driven by data and knowledge","authors":"Hongyan Zang,&nbsp;Changsheng Gao,&nbsp;Yudong Hu,&nbsp;Wuxing Jing","doi":"10.1016/j.dt.2025.02.001","DOIUrl":null,"url":null,"abstract":"<div><div>Recently, high-precision trajectory prediction of ballistic missiles in the boost phase has become a research hotspot. This paper proposes a trajectory prediction algorithm driven by data and knowledge (DKTP) to solve this problem. Firstly, the complex dynamics characteristics of ballistic missile in the boost phase are analyzed in detail. Secondly, combining the missile dynamics model with the target gravity turning model, a knowledge-driven target three-dimensional turning (T3) model is derived. Then, the BP neural network is used to train the boost phase trajectory database in typical scenarios to obtain a data-driven state parameter mapping (SPM) model. On this basis, an online trajectory prediction framework driven by data and knowledge is established. Based on the SPM model, the three-dimensional turning coefficients of the target are predicted by using the current state of the target, and the state of the target at the next moment is obtained by combining the T3 model. Finally, simulation verification is carried out under various conditions. The simulation results show that the DKTP algorithm combines the advantages of data-driven and knowledge-driven, improves the interpretability of the algorithm, reduces the uncertainty, which can achieve high-precision trajectory prediction of ballistic missile in the boost phase.</div></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"48 ","pages":"Pages 187-203"},"PeriodicalIF":5.0000,"publicationDate":"2025-02-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Defence Technology(防务技术)","FirstCategoryId":"1087","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2214914725000406","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MULTIDISCIPLINARY","Score":null,"Total":0}
引用次数: 0

Abstract

Recently, high-precision trajectory prediction of ballistic missiles in the boost phase has become a research hotspot. This paper proposes a trajectory prediction algorithm driven by data and knowledge (DKTP) to solve this problem. Firstly, the complex dynamics characteristics of ballistic missile in the boost phase are analyzed in detail. Secondly, combining the missile dynamics model with the target gravity turning model, a knowledge-driven target three-dimensional turning (T3) model is derived. Then, the BP neural network is used to train the boost phase trajectory database in typical scenarios to obtain a data-driven state parameter mapping (SPM) model. On this basis, an online trajectory prediction framework driven by data and knowledge is established. Based on the SPM model, the three-dimensional turning coefficients of the target are predicted by using the current state of the target, and the state of the target at the next moment is obtained by combining the T3 model. Finally, simulation verification is carried out under various conditions. The simulation results show that the DKTP algorithm combines the advantages of data-driven and knowledge-driven, improves the interpretability of the algorithm, reduces the uncertainty, which can achieve high-precision trajectory prediction of ballistic missile in the boost phase.
基于数据和知识驱动的弹道导弹弹道预测算法
近年来,弹道导弹助推段弹道的高精度预测已成为一个研究热点。本文提出了一种数据与知识驱动的轨迹预测算法(DKTP)。首先,详细分析了弹道导弹助推段的复杂动力学特性。其次,将导弹动力学模型与目标重力转向模型相结合,建立了知识驱动的目标三维转向模型;然后,利用BP神经网络对典型场景下的助推相轨迹数据库进行训练,得到数据驱动的状态参数映射(SPM)模型。在此基础上,建立了数据和知识驱动的在线轨迹预测框架。在SPM模型的基础上,利用目标的当前状态预测目标的三维转弯系数,结合T3模型得到目标下一时刻的状态。最后,在各种条件下进行仿真验证。仿真结果表明,DKTP算法结合了数据驱动和知识驱动的优点,提高了算法的可解释性,降低了算法的不确定性,能够实现弹道导弹助推段弹道的高精度预测。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Defence Technology(防务技术)
Defence Technology(防务技术) Mechanical Engineering, Control and Systems Engineering, Industrial and Manufacturing Engineering
CiteScore
8.70
自引率
0.00%
发文量
728
审稿时长
25 days
期刊介绍: Defence Technology, a peer reviewed journal, is published monthly and aims to become the best international academic exchange platform for the research related to defence technology. It publishes original research papers having direct bearing on defence, with a balanced coverage on analytical, experimental, numerical simulation and applied investigations. It covers various disciplines of science, technology and engineering.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信