载人登月轨道月面可达区域分析  

Reachable Region Analysis of Orbits for Manned Lunar Landing Mission

作　　者：贺波勇[1] 彭祺擘[2] 沈红新[1] 李海阳[1] 

机构地区：[1]国防科学技术大学航天科学与工程学院,长沙410073 [2]中国航天员科研训练中心,北京100094

出　　处：《载人航天》2014年第4期290-295,共6页Manned Spaceflight

基　　金：国家自然科学基金(11372345);国家重点基础研究发展计划(2013CB733100)资助

摘　　要：全月面到达是21世纪以来载人登月研究的主要目标之一。影响月面可达区域的因素有很多,而阳光入射角约束和转移轨道约束是主要因素。首先分析了不同纬度区域阳光入射角规律,其次建立了一种适于月面可达区域分析的双二体圆锥曲线拼接算法,分析了自由返回轨道和混合轨道月面可达区域,并计算了变轨策略及其速度增量关系,为未来实现载人登月月面着陆区选择提供参考。Lunar global access is one of the main goals of manned lunar landing mission in the 21 st century .The sunshine incidence angle and translunar orbits are the main factors influencing the lu-nar reachable region, although there are many others.First, the sunshine incidence angle of dif-ferent latitude regions was analyzed .Then a double two-body conic model suitable for analyzing the lunar capable region was established.The reachable region of the free-return orbit and hybrid orbit was analyzed and the relationship between the orbital maneuver strategy and speed increase was calculated.The results can serve as a reference for manned lunar landing region selection in the future.

关 键 词：载人登月 月面可达区域 自由返回轨道 混合轨道 

分 类 号：V412[航空宇航科学与技术—航空宇航推进理论与工程]