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航天器对空间目标追踪及绕飞研究
引用本文:刘猛,李全. 航天器对空间目标追踪及绕飞研究[J]. 沈阳理工大学学报, 2011, 0(2): 80-83
作者姓名:刘猛  李全
作者单位:沈阳理工大学信息科学与工程学院;
摘    要:最小冲量追踪是指航天器对空间目标的轨道追踪时,所需要的最小速度冲量。应用拉格朗日极小值原理,以航天器转移轨道六要素为目标函数,通过调整航天器轨道六要素对空间目标设计出最小冲量入轨,对空间目标进行绕飞,从而得出航天器追踪到绕飞编队所需冲量基本关系。通过施加两个最小冲量,使得航天器对空间目标实现绕飞.

关 键 词:轨道追踪  绕飞  最小冲量

Research on Achievement of Tracking and Flying Around Space Targe
LIU Meng,LI Quan. Research on Achievement of Tracking and Flying Around Space Targe[J]. Transactions of Shenyang Ligong University, 2011, 0(2): 80-83
Authors:LIU Meng  LI Quan
Affiliation:LIU Meng,LI Quan(Shenyang Ligong University,Shenyang 110159,China)
Abstract:The minimum impulse of tracking is used by the spacecraft when it tracks the orbit of space target.It follows the principle of the Lagrange and its target function is the orbit of the space target.The spacecraft tracks the orbit of space target by adjusting its six elements,so we can conclude the fundamental relation between tracking and flying around the spacecraft.The spacecraft is made to fly around the target in the space by applying two minimum impulses.
Keywords:tracking the orbit  flying around  minimum impulse  
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