Comparison of low-energy lunar transfer trajectories to invariant manifolds

DOI10.1007/S10569-012-9466-3zbMath1342.70027OpenAlexW2094303880WikidataQ58468403 ScholiaQ58468403MaRDI QIDQ736946

Rodney L. Anderson, Jeffrey S. Parker

Publication date: 5 August 2016

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

Full work available at URL: https://doi.org/10.1007/s10569-012-9466-3

zbMATH Keywords

invariant manifoldsdynamical systems theorylibration point orbitsLyapunov orbitsEarth-Moon landing geometrylunar transfers

Mathematics Subject Classification ID

Dynamical systems in classical and celestial mechanics (37N05) (n)-body problems (70F10)

Related Items (2)

Study of the transfer between libration point orbits and lunar orbits in Earth-Moon system ⋮ Cylindrical isomorphic mapping applied to invariant manifold dynamics for Earth-Moon missions

Cites Work

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• The use of invariant manifolds for transfers between unstable periodic orbits of different energies
• Leaving the moon by means of invariant manifolds of libration point orbits
• Triple collision in the collinear three-body problem
• Study of the transfer from the Earth to a halo orbit around the equilibrium point \(L_ 1\)
• Regularization of vector fields by surgery
• Low Energy Transit Orbits in the Restricted Three-Body Problems
• ON MOULTON'S ORBITS IN THE RESTRICTED PROBLEM OF THREE BODIES

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