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绕月自由返回轨道的设计与分析
引用本文:张磊,于登云,张熇.绕月自由返回轨道的设计与分析[J].航天器工程,2010,19(2):128-135.
作者姓名:张磊  于登云  张熇
作者单位:1. 北京空间飞行器总体设计部,北京,100094
2. 中国航天科技集团公司,北京,100048
基金项目:国家重大科技专项工程 
摘    要:绕月自由返回轨道用于早期载人登月任务及相关试验任务,对保证任务成功起了重要作用。作为可选的轨道飞行方案之一,其对当前及未来的月球探测任务设计仍具有重要的工程意义。文章阐述了给定约束条件下绕月自由返回轨道的设计方法,并基于该方法分析了绕月自由返回轨道的相关特性,为任务设计和分析提供了基础。

关 键 词:月球探测  轨道设计  绕月自由返回

Design and Analysis of Circumlunar Free-Return Orbits
ZHANG Lei,YU Dengyun,ZHANG He.Design and Analysis of Circumlunar Free-Return Orbits[J].Spacecraft Engineering,2010,19(2):128-135.
Authors:ZHANG Lei  YU Dengyun  ZHANG He
Institution:ZHANG Lei YU Dengyun ZHANG He(1 Beijing Institute of Spacecraft System Engineering,Beijing 100094,China)(2 China Aerospace Science and Technology Corporation,Beijing 100048,China)
Abstract:Circumlunar free-return orbits were applied to early manned lunar-landing and other related testing missions,and play an important role in ensuring mission success.As one of the optional orbital flight schemes,the circumlunar free-return orbit still has important engineering significance.In this paper,the design method for circumlunar free-return orbits is described,and the property analysis is given.The research results provide the basis for the mission design and analysis.
Keywords:lunar exploration  orbit design  circumlunar free-return
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