Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review

IF 3.3 3区 工程技术 Q1 ENGINEERING, MULTIDISCIPLINARY Journal of Zhejiang University-SCIENCE A Pub Date : 2023-04-20 DOI:10.1631/jzus.A2200423
Shuangxi Liu, B. Yan, Wei Huang, Xu Zhang, Jie Yan
{"title":"Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review","authors":"Shuangxi Liu, B. Yan, Wei Huang, Xu Zhang, Jie Yan","doi":"10.1631/jzus.A2200423","DOIUrl":null,"url":null,"abstract":"临近空间高超声速飞行器是指在临近空间能够以大于5马赫速度飞行的一类飞行器, 具有飞行速度快、 突防能力强、 作战半径大和响应迅速等特点. 凭借其优异的性能优势, 高超声速飞行器逐渐成为各个国家新的空天博弈焦点, 给现有防御体系带来巨大挑战. 为满足临近空间高超声速飞行器防御需求, 本文系统性地梳理高超声速飞行器的“五大优势”及拦截高超声速飞行器的“四大难点”. 其次, 针对现阶段高超声速飞行器拦截制导律, 对基于单弹制导律和多弹协同制导律进行综述, 并归纳其优缺点. 最后, 从“信息域”、 “空间域”、 “物理域”和“效费比”四个方面对协同拦截高超声速飞行器未来发展方向进行了展望, 为临近空间拦截制导技术研究提供参考. The unique performance advantages of hypersonic vehicles represent a critical challenge for existing defense systems. To facilitate defensive operations against hypersonic vehicles in near space, this paper systematically discusses both the advantages of these vehicles and the difficulties in intercepting them. Focusing on the state-of-the-art terminal guidance laws for intercepting hypersonic vehicles in near space, we examine research progress in the area of single- and multi-interceptor cooperative guidance laws and summarize their advantages and disadvantages. We also highlight future research directions for developing an effective terminal guidance law for multi-interceptor cooperative interception of hypersonic vehicles, based on four aspects: the information domain, space domain, physical domain, and effect-cost ratio. The findings provide a reference for further research into near-space interceptor terminal guidance technologies.","PeriodicalId":17508,"journal":{"name":"Journal of Zhejiang University-SCIENCE A","volume":"58 1","pages":"387-403"},"PeriodicalIF":3.3000,"publicationDate":"2023-04-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Zhejiang University-SCIENCE A","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1631/jzus.A2200423","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MULTIDISCIPLINARY","Score":null,"Total":0}
引用次数: 3

Abstract

临近空间高超声速飞行器是指在临近空间能够以大于5马赫速度飞行的一类飞行器, 具有飞行速度快、 突防能力强、 作战半径大和响应迅速等特点. 凭借其优异的性能优势, 高超声速飞行器逐渐成为各个国家新的空天博弈焦点, 给现有防御体系带来巨大挑战. 为满足临近空间高超声速飞行器防御需求, 本文系统性地梳理高超声速飞行器的“五大优势”及拦截高超声速飞行器的“四大难点”. 其次, 针对现阶段高超声速飞行器拦截制导律, 对基于单弹制导律和多弹协同制导律进行综述, 并归纳其优缺点. 最后, 从“信息域”、 “空间域”、 “物理域”和“效费比”四个方面对协同拦截高超声速飞行器未来发展方向进行了展望, 为临近空间拦截制导技术研究提供参考. The unique performance advantages of hypersonic vehicles represent a critical challenge for existing defense systems. To facilitate defensive operations against hypersonic vehicles in near space, this paper systematically discusses both the advantages of these vehicles and the difficulties in intercepting them. Focusing on the state-of-the-art terminal guidance laws for intercepting hypersonic vehicles in near space, we examine research progress in the area of single- and multi-interceptor cooperative guidance laws and summarize their advantages and disadvantages. We also highlight future research directions for developing an effective terminal guidance law for multi-interceptor cooperative interception of hypersonic vehicles, based on four aspects: the information domain, space domain, physical domain, and effect-cost ratio. The findings provide a reference for further research into near-space interceptor terminal guidance technologies.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
近空间拦截高超声速飞行器末制导规律研究现状与展望
临近空间高超声速飞行器是指在临近空间能够以大于5马赫速度飞行的一类飞行器, 具有飞行速度快、 突防能力强、 作战半径大和响应迅速等特点. 凭借其优异的性能优势, 高超声速飞行器逐渐成为各个国家新的空天博弈焦点, 给现有防御体系带来巨大挑战. 为满足临近空间高超声速飞行器防御需求, 本文系统性地梳理高超声速飞行器的“五大优势”及拦截高超声速飞行器的“四大难点”. 其次, 针对现阶段高超声速飞行器拦截制导律, 对基于单弹制导律和多弹协同制导律进行综述, 并归纳其优缺点. 最后, 从“信息域”、 “空间域”、 “物理域”和“效费比”四个方面对协同拦截高超声速飞行器未来发展方向进行了展望, 为临近空间拦截制导技术研究提供参考. The unique performance advantages of hypersonic vehicles represent a critical challenge for existing defense systems. To facilitate defensive operations against hypersonic vehicles in near space, this paper systematically discusses both the advantages of these vehicles and the difficulties in intercepting them. Focusing on the state-of-the-art terminal guidance laws for intercepting hypersonic vehicles in near space, we examine research progress in the area of single- and multi-interceptor cooperative guidance laws and summarize their advantages and disadvantages. We also highlight future research directions for developing an effective terminal guidance law for multi-interceptor cooperative interception of hypersonic vehicles, based on four aspects: the information domain, space domain, physical domain, and effect-cost ratio. The findings provide a reference for further research into near-space interceptor terminal guidance technologies.
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 去求助
来源期刊
Journal of Zhejiang University-SCIENCE A
Journal of Zhejiang University-SCIENCE A 工程技术-工程:综合
CiteScore
5.60
自引率
12.50%
发文量
2964
审稿时长
2.9 months
期刊介绍: Journal of Zhejiang University SCIENCE A covers research in Applied Physics, Mechanical and Civil Engineering, Environmental Science and Energy, Materials Science and Chemical Engineering, etc.
期刊最新文献
A novel approach for the optimal arrangement of tube bundles in a 1000-MW condenser Influence of overhanging tool length and vibrator material on electromechanical impedance and amplitude prediction in ultrasonic spindle vibrator Dynamics of buoyancy-driven microflow in a narrow annular space Key technologies and development trends of the soft abrasive flow finishing method Solid-liquid flow characteristics and sticking-force analysis of valve-core fitting clearance
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1