直升机载远程空地导弹发射后截获概率分析  

After-launching Interception Probability Analysis of Helicopter-borne Long-range Air-to-ground Missile

作　　者：薛晓东[1,2] 刘代军[2] 杨亚丽[2] 

机构地区：[1]上海交通大学,上海200240 [2]中国空空导弹研究院,河南洛阳471009

出　　处：《弹箭与制导学报》2012年第3期227-229,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：直升机载远程空地导弹主要特点就是采用发射后截获技术,因此,发射后截获概率是影响其毁伤概率的重要因素。影响截获概率的误差源很多,文中通过对各种误差源的定量分析,指出了影响截获概率的主要误差源,提供了一种发射后截获概率的近似估算方法,在武器系统初步方案设计时,可用该方法进行发射后截获概率的计算。Adoption of after-launching interception technique is a major feature of helicopter-borne long-range air-to-ground missile. With quantitative analysis, the major error source that affects the interception probability was found. It provides a method of estimating the inter-ception probability approximately. The method can be used for calculating the interception probability during preliminary scheme design phase of the weapon system.

关 键 词：直升机载远程空地导弹 发射后截获 截获概率 误差源 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]