摘要
以垂直发射型舰空导弹为研究对象,分别建立了无控段、转弯段和制导段弹道数学模型。通过对弹道进行仿真,获取给定脱靶量的命中点集合,并拟合得到杀伤区。该模型基本满足针对不同高度、速度入侵目标相应杀伤区的解算,所得数据可作为舰艇防空作战指挥决策、编队防空队形配置和编队协同防空作战效能评估、防空火力协同的依据。
In this paper,the mathematical models of no control phase,turn phase and guidance phase of vertical launching ship-to-air missile are set up. Through trajectory simulation,the hit point database is built based on the given miss distance,and the kill zone is obtained using fitting method.The model of killing zone can basically meet the calculation needs for targets of different height and speed,the killing zone data can be base of making operation scheme of air defense,formation order configuration,and effectiveness assessment of formation,cooperation of firepower of air defense.
出处
《火力与指挥控制》
CSCD
北大核心
2015年第5期8-11,共4页
Fire Control & Command Control
基金
国家自然科学基金(61305133)
航空科学基金资助项目(2013ZC53037)
关键词
舰空导弹
杀伤区
垂直发射
弹道仿真
ship-to-air missile,killing zone,vertical launch,trajectory simulation
作者简介
陈军（1979-）,男,江西樟树人,副教授.研究方向：火力与指挥控制理论、作战效能分析及复杂系统建模与仿真研究.
