Using invariant manifolds to capture an asteroid near the \(L_3\) point of the Earth-Moon bicircular model

DOI10.1016/J.CNSNS.2021.105948zbMath1477.70045OpenAlexW3181816940MaRDI QIDQ2045999

Àngel Jorba, Begoña Nicolás

Publication date: 16 August 2021

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.2021.105948

zbMATH Keywords

quasi-periodic orbitsparametrization methodjet transportasteroid capture

Mathematics Subject Classification ID

Orbital mechanics (70M20) Symmetries and conservation laws, reverse symmetries, invariant manifolds and their bifurcations, reduction for problems in Hamiltonian and Lagrangian mechanics (70H33)

Related Items (6)

Numerical Computation of High-Order Expansions of Invariant Manifolds of High-Dimensional Tori ⋮ The vicinity of Earth-Moon \(L_1\) and \(L_2\) in the Hill restricted 4-body problem ⋮ Invariant manifolds near \(L_1\) and \(L_2\) in the quasi-bicircular problem ⋮ Breakdown of homoclinic orbits to \(L_3\) in the RPC3BP. II: An asymptotic formula ⋮ Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture ⋮ Transfers from the Earth to \(L_2\) halo orbits in the Earth-Moon bicircular problem

Uses Software

• Taylor

Cites Work

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