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助推滑翔高超声速反舰导弹突防密集阵武器能力分析

王少平 董受全 李晓阳 张华英

指挥控制与仿真2017,Vol.39Issue(5):30-36,7.
指挥控制与仿真2017,Vol.39Issue(5):30-36,7.DOI:10.3969/j.issn.1673-3819.2017.05.007

助推滑翔高超声速反舰导弹突防密集阵武器能力分析

Analysis of the Ability of Boost-glide Hypersonic Anti-ship Missile Breaking the Defense of Phalanx System

王少平 1董受全 1李晓阳 2张华英1

作者信息

  • 1. 海军大连舰艇学院, 辽宁 大连 116018
  • 2. 92956部队, 辽宁 大连 116041
  • 折叠

摘要

Abstract

On the basis of analyzing and comparing the ballistic trajectory difference between boost-glide hypersonic anti-ship missile and traditional anti-ship missile, point-mass equation for missiles and target maneuver models are built, which are founded on the optimum guidance law with a terminal angular constraint of the dive phase, simulation analysis of the bal-listic trajectory of boost-glide hypersonic anti-ship missile is conducted. Then engagement simulation models are built that be-tween boost-glide hypersonic anti-ship missile and phalanx system. The penetration probability of boost-glide hypersonic anti-ship missile is simulated by the method of Monte-Carlo, which is influenced by vehicle and path angle. The ability of boost-glide hypersonic anti-ship missile breaking the defense of phalanx system is got, which is providing theoretical support for op-erational use of boost-glide hypersonic anti-ship missile.

关键词

高超声速/反舰导弹/密集阵系统/突防能力

Key words

hypersonic/anti-ship missile/phalanx system/penetration ability

分类

军事科技

引用本文复制引用

王少平,董受全,李晓阳,张华英..助推滑翔高超声速反舰导弹突防密集阵武器能力分析[J].指挥控制与仿真,2017,39(5):30-36,7.

指挥控制与仿真

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1673-3819

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