摘要
本文提出了全向攻击型空 -空导弹单发杀伤概率的计算方法 ,建立了以尾追和迎攻为特征的完整的杀伤概率数学模型 ;用灵敏度分析技术研究了遭遇参数、战斗部及引信参数对杀伤概率的影响。本文方法用于红外导弹总体设计方案算例 ,仿真结果与工程设计经验相符 ,证实了该方法有效可行。
An algorithm for kill probability of single air to air missile in omnidirectional attack is presented. Complete mathematical models of kill probability with attack characteristics of tail pursue or head on are established. Using the sensitivity technology, the influence of encounter parameters, warhead and fuze parameters on kill probability is calculated and analyzed. As an example, the synthesis scheme of an infrared air to air missile is designed by using the methods. The simulation results coincide with engineering practice, which shows that the methods are feasible.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
2000年第z1期52-57,共6页
Journal of Astronautics
关键词
空空导弹
杀伤概率
全向攻击
遭遇参数
Air to air missile Kill probability Omnidirectional attack Encounter parameters