| 低轨星载拦截器对高轨卫星的拦截 |
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| 引用本文： | 陈建祥,任萱.低轨星载拦截器对高轨卫星的拦截[J].航天控制,1993(4). |
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| 作者姓名： | 陈建祥 任萱 |
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| 作者单位： | 国防科技大学自动控制系，国防科技大学自动控制系 |
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| 摘 要： | 本文分析了低轨星载拦截器进行轨道机动拦截高轨卫星的能力。在拦截系统分析中,威胁区、防区和拦截区是三个基本概念。本文给出了其建模及求解方法,并利用数字仿真,给出了对应于不同拦截时间的典胁威胁区、防区和拦截区。
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| 关 键 词： | 卫星轨道 航天截击器 截击弹道 |
Interception of Satellite-board Interceptor on Low Orbits to the Satellites on High Orbits |
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| Cheng JianXiang Ren Xuan National Defence Science and Technology University Automatic Control.Interception of Satellite-board Interceptor on Low Orbits to the Satellites on High Orbits[J].Aerospace Control,1993(4). |
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| Authors: | Cheng JianXiang Ren Xuan National Defence Science and Technology University Automatic Control |
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| Institution: | Cheng JianXiang Ren Xuan National Defence Science and Technology University Automatic Control Department |
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| Abstract: | The paper analyzes the capability of satellite-board interceptor on low orbits to intercept the satellites on high orbits by orbit maneuvering. The paper introduces the model establishment and solving method of the killing range, defence range and interception range, which are three basic concepts in the analysis of interception system. It also gives out the typical graphes of the three ranges corresponding to different intercepting time by using simulation. |
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| Keywords: | Satellite orbit Interceptor spacecraft Intercept trajectory |
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