...不变流形 [gap=1010]ar restricted threebody problem;libration point;earthmoon transfer trajectory;invariant manifolds ...
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characteristic invariant manifolds 特征不变流形
invariant manifolds of odes 不变流形
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。
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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