| 空间交会中脉冲变轨燃料消耗研究 |
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| 引用本文： | 向开恒,肖业伦.空间交会中脉冲变轨燃料消耗研究[J].中国空间科学技术,1999,19(3):9-15. |
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| 作者姓名： | 向开恒 肖业伦 |
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| 作者单位： | 北京航空航天大学 |
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| 摘 要： | 导出了空间交会中多脉冲变轨的一般算法。在此基础上，重点研究了双脉冲变轨的燃料消耗情况，提出了双脉冲变轨条件下的“不可达点”及其附近的“高耗能区域”，并给出了相应的物理解释。最后对多脉冲变轨与双脉冲变轨进行了比较。
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| 关 键 词： | 航天交会 变轨控制 燃料消耗量 研究 |
A Study of Propellant Consumption of Impulsive Maneuvers in Space Rendezvous |
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| Xiang Kaiheng,Xiao Yelun.A Study of Propellant Consumption of Impulsive Maneuvers in Space Rendezvous[J].Chinese Space Science and Technology,1999,19(3):9-15. |
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| Authors: | Xiang Kaiheng Xiao Yelun |
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| Abstract: | A general solution for multi impulse maneuvers in space rendezvous is derived.On the basis of the solution,the propellant consumption of two impulse maneuvers is studied,the “unreachable point”and “high consumption area”nearby are presented.A physical explanation of the terms is also given.Finally,a comparison between two impulse and multi impulse maneuvers is introduced. |
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| Keywords: | Space rendezvous Transfer orbital control Fuel consumption Research |
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