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.%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 .
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