指挥控制与仿真2017，Vol.39Issue(2)：55-60,6.DOI:10.3969/j.issn.1673-3819.2017.02.012
助推滑翔高超声速反舰导弹多方向协同突防可行性研究
Feasibility Study of Multi-direction Coordinated Penetration of the Boost-glide Hypersonic Anti-ship Missile
王少平 1董受全 1李晓阳 2葛津华3
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
- 3. 91329部队,山东威海264200
- 折叠
摘要
Abstract
On the basis of analyzing the ballistic trajectory character of boost-glide hypersonic anti-ship missile,some possible penetration strategy is designed.Point-mass equation for missiles is built,and the feasibility of muti-directional penetration of multi-missiles in coordination which launching by single platform is studied,which is based on the optimum guidance law with a terminal angular constraint.Some conclusions are obtained through simulation that the muti-directional penetration of multi-missiles in coordination which launching by single platform is feasible by manually setting virtual targets under the constraints,such as the normal overload,trajectory inclination angle,dynamic pressure.关键词
助推滑翔高超声速反舰导弹/下压段/突防策略/可行性Key words
boost-glide hypersonic anti-ship missile/the dive phase/penetration strategy/feasibility分类
军事科技引用本文复制引用
王少平,董受全,李晓阳,葛津华..助推滑翔高超声速反舰导弹多方向协同突防可行性研究[J].指挥控制与仿真,2017,39(2):55-60,6.
