中文摘要：

这篇文章探讨从土转到光圈轨道的轨道的设计，并且建议预定修正演习的靠近环的策略在在通报的框架的转移期间限制了三个身体问题(CR3BP ) 。在 Floquet multipliers 和光圈轨道的大小之间的关系被建立，以便为太空使命的合适的大小以光圈轨道的稳定性被选择。马厩歧管从茅印射定义与以前的研究不同的 Poincar 被调查，并且单个推动的转移轨道的六种类型从不变的 manifolds 的几何学被达到。基于在文学的大多数被忽略的间接转移的轨道之一，为分离线性随机的系统的有瑕疵的信息的随机的控制理论被使用设计轨道修正演习。统计分散分析被 Monte-Carlo 模拟执行。

英文摘要：

This article addresses the design of the trajectory transferring from Earth to Halo orbit, and proposes a timing closed-loop strategy of correction maneuver during the transfer in the frame of circular restricted three body problem （CR3BP）. The relation between the Floquet multipliers and the magnitudes of Halo orbit is established, so that the suitable magnitude for the aerospace mission is chosen in terms of the stability of Halo orbit. The stable manifold is investigated from the Poincar6 mapping defined which is different from the previous researches, and six types of single-impulse transfer trajectories are attained from the geometry of the invariant manifolds. Based on one of the trajectories of indirect transfer which are ignored in the most of literatures, the stochastic control theory for imperfect information of the discrete linear stochastic system is applied to design the trajectory correction maneuver. The statistical dispersion analysis is performed by Monte-Carlo simulation,