导弹拦截点计算及其仿真分析  

Calculation and simulation analysis of missile intercept point

作　　者：田宪科[1] 张科[1] 

机构地区：[1]西北工业大学航天学院,陕西西安710072

出　　处：《飞行力学》2011年第2期93-96,共4页Flight Dynamics

基　　金：航空科学基金资助(20090153003);西北工业大学基础研究基金资助(G9KY1004)

摘　　要：导弹拦截点的计算对研究引信战斗部一体化设计和毁伤效果的分析及评价具有重要意义。以防空导弹和空空导弹广泛使用的破片式战斗部为例,建立了求解拦截点的数学模型,通过控制变量法用Matlab软件分析研究了导弹拦截点的影响因素并得出为获得较理想拦截距离的相关参数要求。从而为导弹引信战斗部一体化设计和毁伤评估奠定了必要基础。It is important of the calculation of missile intercept point for the fuze-warhead integration design besides analysis and evaluation of damage effect.In this paper,we take fragmentation warhead used widely in the anti-aircraft missiles and air-to-air missiles for an example,establish the mathematical model to solve intercept point,research an influence on factors of the missile intercept point and finally come to obtain the relevant parameters required in ideal intercept distance using the Matlab by controlling the variables.Thereby,the necessary foundation for damage assessment and the fuze-warhead integration design are established.

关 键 词：破片式战斗部 拦截点 数学模型 MATLAB 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]