Computation of low energy Earth-to-Moon transfers with moderate flight time

DOI10.1016/j.physd.2004.07.005zbMath1076.70019OpenAlexW2041135309MaRDI QIDQ1888065

Kazuyuki Yagasaki

Publication date: 22 November 2004

Published in: Physica D (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.physd.2004.07.005

zbMATH Keywords

planar circular restricted three-body problemcomputer software AUTO

Mathematics Subject Classification ID

Three-body problems (70F07) Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

Related Items (12)

Optimal round trip lunar missions based on the patched-conic approximation ⋮ A note on weak stability boundaries ⋮ Extension of fast periodic transfer orbits from the Earth-Moon RTBP to the Sun-Earth-Moon quasi-bicircular problem ⋮ Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture ⋮ Intersecting invariant manifolds in spatial restricted three-body problems: design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario ⋮ Optimal two-impulse trajectories with moderate flight time for Earth-Moon missions ⋮ Perturbation solutions to the nonlinear motion of displaced orbits ⋮ Invariant manifolds and control of hyperbolic trajectories on infinite- or finite-time intervals ⋮ Minimum fuel trajectories for round trip lunar missions ⋮ Low-energy transfers to the Moon with long transfer time ⋮ Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time ⋮ High-order solutions around triangular libration points in the elliptic restricted three-body problem and applications to low energy transfers

Uses Software

• AUTO
• Dynamics
• HomCont
• HomMap

Cites Work

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• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
• Solving Ordinary Differential Equations I
• Practical Runge–Kutta Processes
• Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
• Computation of Periodic Solutions of Conservative Systems with Application to the 3-Body Problem
• Targeting in Hamiltonian systems that have mixed regular/chaotic phase spaces
• Chaos
• Low energy transfer to the Moon

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