Transit and capture in the planar three-body problem leveraging low-thrust invariant manifolds

DOI10.1007/S10569-021-10022-YzbMath1472.70024OpenAlexW3162747751MaRDI QIDQ2049204

David C. Folta, Andrew D. Cox, Kathleen C. Howell

Publication date: 24 August 2021

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

Full work available at URL: https://doi.org/10.1007/s10569-021-10022-y

zbMATH Keywords

multi-body dynamicsdynamical systems theorytrajectory designlow thrust

Mathematics Subject Classification ID

Three-body problems (70F07) Symmetries and conservation laws, reverse symmetries, invariant manifolds and their bifurcations, reduction for problems in Hamiltonian and Lagrangian mechanics (70H33)

Cites Work

• Unnamed Item
• Low-energy, low-thrust transfers to the Moon
• Dynamical structures in a low-thrust, multi-body model with applications to trajectory design
• A Framework for Constructing Transfers Linking Periodic Libration Point Orbits in the Spatial Circular Restricted Three-Body Problem
• Low Energy Transit Orbits in the Restricted Three-Body Problems

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