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。
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.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1999年第3期9-15,共7页
Chinese Space Science and Technology
关键词
航天器
交会
变轨控制
燃料消耗量
多脉冲变轨
Space rendezvous Transfer orbital control Fuel consumption Research
