...不变流形 [gap=1010]ar restricted threebody problem;libration point;earthmoon transfer trajectory;invariant manifolds ...
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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。
The low-energy lunar landing trajectory design using the invariant manifolds of restricted three body problem is studied.
然后基于不变流形理论和庞加莱截面方法，设计了不同拉格朗日点间转移轨道。
Then on the basis of invariant manifold theory and Poincaré section, a transfer trajetory between L1 and L2 of the Earth-Moon system was given.
通过找出两端边界层的不变流形，并且给出边值条件解耦的条件，成功构造了边界层函数。
Boundary functions are successfully constructed through finding out invariant manifolds at both end boundary layers and giving out decoupling conditions of boundary value conditions.
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