End-to-end trajectory concept for close exploration of Saturn's inner large moons

DOI10.1016/J.CNSNS.2023.107458arXiv2305.17548OpenAlexW4385163866MaRDI QIDQ6058720

F. Solano, M. Sanjurjo-Rivo, Roberto Flores, B. M. Burhani, Elisa Maria Alessi, Elena Fantino

Publication date: 1 November 2023

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://arxiv.org/abs/2305.17548

zbMATH Keywords

optimal controlcircular restricted three-body problemgravity assistpatched conicslow thrusthyperbolic invariant manifoldsplanar Lyapunov orbitsSaturn moons

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Cites Work

• Intersecting invariant manifolds in spatial restricted three-body problems: design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario
• Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter
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• High-order resonant orbit manifold expansions for mission design in the planar circular restricted 3-body problem
• Numerical continuation of families of heteroclinic connections between periodic orbits in a Hamiltonian system
• Numerical continuation of families of homoclinic connections of periodic orbits in the RTBP
• Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
• Connecting orbits and invariant manifolds in the spatial restricted three-body problem
• Low-thrust Lyapunov to Lyapunov and Halo to Halo missions with L²-minimization
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