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战术弹道导弹拦截的数学建模与仿真
引用本文:强胜,姚静,易东云. 战术弹道导弹拦截的数学建模与仿真[J]. 系统仿真学报, 2007, 19(7): 1424-1427,1484
作者姓名:强胜  姚静  易东云
作者单位:国防科学技术大学理学院,湖南,长沙,410073
基金项目:全国优秀博士论文资金;解放军总装备部预研项目
摘    要:拦截系统是反导系统的最后一环,也是关键所在。拦截系统反应的灵敏、迅速、有效性是十分重要的。针对拦截战术弹道导弹这一特殊任务,对传统的K-比例导引法进行推广,以适应侧面逆轨拦截,从理论上给出了此导引法对弹道影响的分析证明,并结合STK,对拦截弹道导弹进行了仿真,实验结果说明此方法形式简单、方便,具有实用价值。

关 键 词:战术弹道导弹(TBM)  K-比例导引法  过载  攻击平面  动能拦截器
文章编号:1004-731X(2007)07-1424-04
收稿时间:2006-03-02
修稿时间:2006-03-022007-01-09

Mathematical Modeling and Simulations of Tactical Ballistic Missile Interception
QIANG Sheng,YAO Jing,YI Dong-yun. Mathematical Modeling and Simulations of Tactical Ballistic Missile Interception[J]. Journal of System Simulation, 2007, 19(7): 1424-1427,1484
Authors:QIANG Sheng  YAO Jing  YI Dong-yun
Affiliation:School of Science, National University of Defense Technology, Changsha 410073, China
Abstract:The interception is the last step and one of the most important parts in the anti-TBM system. The sensitivity, rapidity and efficiency of the interception system reaction are crucial for the system performance. Based on the special mission of intercepting the tactical ballistic missiles, the traditional K-proportional navigation method was generalized to intercept TBM on flank. The analysis and proof of its influence on the trajectory were also deduced theoretically. Combined with the software STK, the simulations of the TBM interception show the conciseness and practicability of the method.
Keywords:tactical ballistic missile (TBM)  k-proportional navigation trajectory  overload  attack plane  kinetic kill vehicle (KKV)
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