Further advances on low-energy lunar impact dynamics

DOI10.1016/j.cnsns.2011.06.037zbMath1252.70028OpenAlexW2057014861MaRDI QIDQ430355

Elisa Maria Alessi, Josep J. Masdemont, Gerard Gomez

Publication date: 21 June 2012

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cnsns.2011.06.037

zbMATH Keywords

invariant manifoldslibration point orbitsbicircular modelcollisional ejectaCR3BPimpact craters

Mathematics Subject Classification ID

Three-body problems (70F07)

Related Items (3)

A picture of solar-sail heteroclinic enhanced connections between Lissajous libration point orbits ⋮ Low-energy lunar transfers using spatial transit orbits ⋮ Transfers from the Earth to \(L_2\) halo orbits in the Earth-Moon bicircular problem

Cites Work

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• The role of the unstable equilibrium points in the transfer of matter in galactic potentials
• A motivating exploration on lunar craters and low-energy dynamics in the Earth-Moon system
• Dynamics and Mission Design Near Libration Points
• Low Energy Transit Orbits in the Restricted Three-Body Problems
• The dynamics around the collinear equilibrium points of the RTBP
• Resonance and capture of Jupiter comets

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