Design of low-energy transfer from lunar orbit to asteroid in the Sun-Earth-Moon system

DOI10.1007/s10409-014-0071-4zbMath1342.70066OpenAlexW1982593192MaRDI QIDQ531036

Yong-Cai Geng, Sumit K. Garg

Publication date: 3 August 2016

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-014-0071-4

zbMATH Keywords

Sun-Earth-Moon systemasteroid explorationlunar orbitlow-energy transfer

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

Cites Work

• Unnamed Item
• Study of the transfer from the Earth to a halo orbit around the equilibrium point \(L_ 1\)
• An elegant Lambert algorithm
• Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
• Connecting orbits and invariant manifolds in the spatial restricted three-body problem
• Low energy transfer to the Moon

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