Sun-Earth \(L_1\) and \(L_2\) to Moon transfers exploiting natural dynamics

DOI10.1007/S10569-014-9581-4zbMath1409.70008OpenAlexW1628430719MaRDI QIDQ5962792

Massimiliano Vasile, Willem van der Weg

Publication date: 24 February 2016

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-014-9581-4

zbMATH Keywords

survivabilitycoupled circular restricted three-body problemlibration pointlunar capturelunar impactsolar radiation pressureweak capture

Mathematics Subject Classification ID

Celestial mechanics (70F15) (n)-body problems (70F10)

Cites Work

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• Solar sail orbits at the Earth-Moon libration points
• A note on weak stability boundaries
• Introduction to Hamiltonian dynamical systems and the \(N\)-body problem.
• Dynamics and Mission Design Near Libration Points
• On the Relation Between the Bicircular Model and the Coupled Circular Restricted Three-Body Problem Approximation
• New methods in celestial mechanics and mission design
• Dynamics and Mission Design Near Libration Points
• Low Energy Transit Orbits in the Restricted Three-Body Problems
• Low energy transfer to the Moon

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