High-order resonant orbit manifold expansions for mission design in the planar circular restricted 3-body problem
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Publication:2656792
DOI10.1016/j.cnsns.2021.105691zbMath1477.70012arXiv2109.14800OpenAlexW3119363060MaRDI QIDQ2656792
Rafael de la Llave, Rodney L. Anderson, Bhanu Kumar
Publication date: 16 March 2021
Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)
Full work available at URL: https://arxiv.org/abs/2109.14800
Three-body problems (70F07) Invariant manifolds for ordinary differential equations (34C45) Dynamical systems in classical and celestial mechanics (37N05)
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- Chebyshev–Taylor Parameterization of Stable/Unstable Manifolds for Periodic Orbits: Implementation and Applications
- Stability and Chaos in Celestial Mechanics
- Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
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