一个宇宙飞行员希望确定出他接近月球时的逼近速度。
A space navigator wishes to determine his velocity of approach as he nears the moon.
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;
The flight trajectories from low earth parking orbit (LEO) to low lunar parking orbit (LLO) based on a planar three-body model are studied.
1990年,日本发射了一个小型探测器,完成一次靠近月球的短暂飞行。
In 1990, Japan launched a small probe completing a brief fly-by the moon.
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