Abstract As evidenced by the Global Exploration Roadmap, international interest exists in a new era of human exploration of the solar system. Such an effort is commencing with the examination of options for maintaining a facility—at times crewed—in an orbit nearby the Moon. Thus, the key objectives in advancing colonization of interplanetary space include positioning and maintaining an inhabited facility in a long-term and relatively stable orbit in the lunar vicinity. At this time, one orbit of interest for a habitat spacecraft is a Near Rectilinear Halo Orbit (NRHO). Near rectilinear halo orbits near the Moon are members of the L 1 or L 2 halo orbit families and are characterized by favorable stability properties. As such, they are strong candidates for a future habitat facility in cislunar space. This type of trajectory is identified in cislunar space in terms of the Earth-Moon Circular Restricted Three-Body Problem (CR3BP). However, for arrival to and departure from the Earth-Moon region, the impact of the solar gravity generally cannot be ignored. Thus, the orbital characteristics and stability properties are examined within the context of the bicircular restricted four-body problem.

中文翻译：

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双圆四体问题中会合共振近直线晕轨道的动力学

摘要 正如全球探索路线图所证明的那样，人类探索太阳系的新时代存在国际兴趣。这种努力是从检查在月球附近的轨道上维护设施（有时是载人）的选项开始的。因此，推进行星际空间殖民的关键目标包括在月球附近的长期和相对稳定的轨道上定位和维护有人居住的设施。目前，栖息地航天器感兴趣的一个轨道是近直线光晕轨道 (NRHO)。月球附近的近直线晕轨道是 L 1 或 L 2 晕轨道家族的成员，具有良好的稳定性特性。因此，它们是未来地月空间栖息地设施的有力候选者。根据地月圆形受限三体问题 (CR3BP)，在地月空间中确定了这种类型的轨迹。但是，对于到达和离开地月区，太阳引力的影响一般不能忽视。因此，在双圆受限四体问题的背景下检查了轨道特性和稳定性特性。