摘要
分析了导弹破片战斗部对空中目标的杀伤概率计算模型及其影响因素,介绍了制导误差规律、引信引爆点散布规律、引信引爆概率、目标坐标杀伤概率的计算模型,给出了积分区间的确定方法.以某拦截弹破片式战斗部杀伤战术弹道导弹为例进行了仿真计算,并对仿真结果进行了分析,结果表明增大战斗部破片的杀伤半径对提高战斗部的杀伤概率有利.
The killing probability of fragmentation warhead of missile to air target and its influence factors were analyzed. The error distributing probability of control and guide, the real detonating area distributing law of fuze, and the detonating probability of fuze, and the conditional killing probability of warhead were introduced. The integral range of probability calculation was determined. Taking a fragmentation warhead of missile killing a tactical missile for example, the simulation was conducted and the results were analyzed. The results indicat that increasing the killing radius of fragments is of benefit to the killing probability.
出处
《弹道学报》
CSCD
北大核心
2006年第1期45-47,共3页
Journal of Ballistics
关键词
破片式战斗部
仿真
杀伤概率
引战配合
fragmentation warhead
simulation
killing probability
coordination of fuze and warhead
作者简介
郑平泰（1973- ）,男,讲师,博士生,研究方向为飞行器设计与仿真、弹药与战斗部技术.
