Cylindrical isomorphic mapping applied to invariant manifold dynamics for Earth-Moon missions
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Publication:5962788
DOI10.1007/S10569-014-9563-6zbMath1409.70004OpenAlexW2053179279MaRDI QIDQ5962788
Paolo Teofilatto, Mauro Pontani, Marco Giancotti
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/s10569-014-9563-6
invariant manifoldsheteroclinic connectionsend-of-life strategiesimage trajectoriesisomorphic mapplanar circular restricted three body problem
Related Items (2)
Linking low- to high-energy dynamics of invariant manifolds, transit orbits, and singular collision orbits in the planar circular restricted three-body problem ⋮ Long-term capture orbits for low-energy space missions
Cites Work
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- Optimal transfers between unstable periodic orbits using invariant manifolds
- Using space manifold dynamics to deploy a small satellite constellation around the Moon
- The use of invariant manifolds for transfers between unstable periodic orbits of different energies
- Indirect transfer to the Earth-Eoon L1 libration point
- Comparison of low-energy lunar transfer trajectories to invariant manifolds
- Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
- Low Energy Transit Orbits in the Restricted Three-Body Problems
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