The flight trajectories from low earth parkingorbit (LEO) to low lunar parkingorbit (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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A typical orbit of lunar probe includes earth parkingorbit segment, earth-moon transfer orbit segment, lunar satellite orbit segment and moon-landing orbit segment.