首页 | 本学科首页   官方微博 | 高级检索  
   检索      

天基反导拦截打击平台作战部署建模分析
引用本文:王还乡,李为民,周晓光,谢鑫,邓思思.天基反导拦截打击平台作战部署建模分析[J].现代防御技术,2011,39(3).
作者姓名:王还乡  李为民  周晓光  谢鑫  邓思思
作者单位:空军工程大学,导弹学院,陕西三原,713800
摘    要:研究了反助推段弹道导弹的天基载EKV拦截打击平台的轨道选择及构造问题.根据建立的弹道估计状态转移矩阵、平台拦截能力以及弹道导弹发射点位置参数等相关信息,确定了天基载EKV反导拦截打击平台的轨道属性参数.该模型可以为研究及建设天基载EKV反导拦截打击平台相关问题提供参考依据.

关 键 词:轨迹  助推段  天基反导

Analysis and Modeling of Interception of TBM Deployment of Space-Based Platforms
WANG Huan-xiang,LI Wei-min,ZHOU Xiao-guang,XIE Xin,DENG Si-si.Analysis and Modeling of Interception of TBM Deployment of Space-Based Platforms[J].Modern Defence Technology,2011,39(3).
Authors:WANG Huan-xiang  LI Wei-min  ZHOU Xiao-guang  XIE Xin  DENG Si-si
Institution:WANG Huan-xiang,LI Wei-min,ZHOU Xiao-guang,XIE Xin,DENG Si-si(AFEU,Missile Institute,Shaanxi Sanyuan 713800,China)
Abstract:The orbit selection and configuration of the space-based exo-atmospheric kill vehicle(EKV) launch platforms are studied.According to the related information like the trajectory parameters of the tactical ballistic missiles(TBM),platform intercepting capability and launch sites to determine the orbit parameters of the EKV platform for a successful interception.The research may provide a theoretical reference for selection and configuration orbit of interception of boost phase of TBM of space-based platforms.
Keywords:trajectory  boost phase  space-based antiballistic missile  
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号