The low-energy lunarlandingtrajectory design using the invariant manifolds of restricted three body problem is studied.
研究了基于三体问题的不变流形设计低成本登月轨道的问题。
2
In this paper, obtained the translunar trajectory for direct striking the moon, which satisfied some constraints including translunar flight time, lunarlanding date.
在给定飞行时间、着月时间、着月入射角及停泊轨道等约束条件下,建立飞月轨道数学模型;
3
The problem of rapid Lunar soft-landingtrajectory optimization by using a Legendre pseudospectral method was studied in this paper.