指挥控制与仿真2017，Vol.39Issue(4)：16-21,6.DOI:10.3969/j.issn.1673-3819.2017.04.004
助推滑翔高超声速反舰导弹末制导雷达搜索过程分析
Research on Searching Process of Operational Application of Boost-glide Hypersonic Anti-ship Missile
王少平 1董受全 1刘亿 1李晓阳2
作者信息
- 1. 海军大连舰艇学院, 辽宁 大连 116018
- 2. 中国人民解放军92956部队, 辽宁 大连 116041
- 折叠
摘要
Abstract
On the basis of analyzing the ballistic trajectory character of boost-glide hypersonic anti-ship missile, the process of terminal guidance radar searching target is described. The detectable area and acquisiton probability are simulated by the method of Monte-Carlo,which are influenced by autocontrol end-poingt scattering accuracy,missile velocity,target`s diffuxing and so on. The law of terminal guidance radar searching is got,which is providing theoretical support for operational use of boost-glide hypersonic anti-ship missile.关键词
高超声速/反舰导弹/末制导雷达/搜索过程Key words
hypersonic/anti-ship missile/terminal guidance radar/searching process分类
军事科技引用本文复制引用
王少平,董受全,刘亿,李晓阳..助推滑翔高超声速反舰导弹末制导雷达搜索过程分析[J].指挥控制与仿真,2017,39(4):16-21,6.
