The low-energy lunar landing trajectory 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。

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Boundary functions are successfully constructed through finding out invariant manifolds at both end boundary layers and giving out decoupling conditions of boundary value conditions.

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。

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Boundary functions are successfully constructed through finding out invariant manifolds at both end boundary layers and giving out decoupling conditions of boundary value conditions.

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。

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