In this paper, a technique for the analysis and the design of low-energy interplanetary transfers, exploiting the invariant manifolds of the restricted three-body problem, is presented. This approach decomposes the full four-body problem describing the dynamics of an interplanetary transfer between two planets, in two three-body problems each one having the Sun and one of the planets as primaries; then the transit orbits associated to the invariant manifolds of the Lyapunov orbits are generated for each Sun-planet system and linked by means of a Lambert’s arc defined in an intermediate heliocentric two-body system.

中文翻译：

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低能行星际转移利用有限三体问题的不变流形

本文提出了一种利用受限三体问题的不变流形来分析和设计低能行星际传递的技术。这种方法分解了完整的四体问题，描述了两个行星之间的行星际传递的动力学，在两个三体问题中，每个问题都以太阳和一个行星为主要行星。然后，为每个太阳行星系统生成与Lyapunov轨道的不变流形相关的过渡轨道，并通过在中间日心中心两体系统中定义的Lambert弧进行链接。