Design and optimization of low-energy transfer orbit to Mars with multi-body environment

Author:

Lu Yi,Li HengNian,Li JiSheng,Che Zheng,Yang YiKang,Yang Yuan,Sun Yang

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference36 articles.

1. Gomez G, Koon W S, Lo M W, et al. Invariant manifolds, the spatial three-body problem and space mission design. In: Astro-dynamics Specialist Meeting, Quebec City: AIAA/AAS, Canada, 2001

2. Xu M, Tan T, Xu S J. Research on the transfers to Halo orbits from the view of invariant manifolds. Sci China Tech Sci, 2012, 55: 671–683

3. Wang S, Shang H B, Wu W R, Interplanetary transfers employing invariant manifolds and gravity assist between periodic orbits. Sci China Tech Sci, 2013; 56: 786–794

4. Gomez G, Koon W S, Lo M W, et al. Connecting orbits and invariant manifolds in the spatial restricted three-body problem. Nonlinearity, 2004; 17: 157–1606

5. Koon W S, Lo M W, Marsden J E, et al. Constructing a low energy transfer between jovian moons. Contem Math, 2002. 292: 129–145

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