Article ID Journal Published Year Pages File Type
1716593 Acta Astronautica 2009 8 Pages PDF
Abstract

This paper deals with the cislunar transfer problem. A new type of distant retrograde orbit (DRO) is proposed and its stability is investigated. The Lyapunov orbits tangential to the retrograde orbit are applied to design the entry of transfer trajectories, i.e., the invariant manifolds of Lyapunov orbit around L1L1 are applied to achieve the quick transfer to DRO, meanwhile the Lyapunov orbit around L2L2 is used as the entrance to weak stability boundary (WSB) transfer, so that the low energy transfer to DRO is achieved. The numerical simulations is given to validated the feasibility of the two transfer modes.

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Physical Sciences and Engineering Engineering Aerospace Engineering
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