Trajectories and some key parameters of the three stages, the earth escape stage, coast arc stage, and lunar capture stage, are presented as well.

给出了在地球逃逸段、惯性漂移段和月球捕获段的运动轨迹和关键点的参数。

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Flight trajectories control technology from low earth orbit to lunar sphere of influence (LSOI) is present as well.

完成了从近地低轨道到月球影响球附近的轨道飞行控制方法的研究。

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The flight trajectories from low earth parking orbit (LEO) to low lunar parking orbit (LLO) based on a planar three-body model are studied.

进行了基于平面三体模型的登月飞行器轨道控制方法的研究；研究了从近地低轨道到近月低轨道的飞行轨道；

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