Spacecraft trajectories to the \(L_{3}\) point of the Sun-Earth three-body problem

DOI10.1007/S10569-010-9299-XzbMath1223.70100OpenAlexW2061350851WikidataQ56050839 ScholiaQ56050839MaRDI QIDQ642393

Yuan Ren, P. Pergola, Elena Fantino, Marco Tantardini, Gerard Gomez

Publication date: 26 October 2011

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

Full work available at URL: https://doi.org/10.1007/s10569-010-9299-x

zbMATH Keywords

periodic orbitscircular restricted three-body probleminvariant manifoldslibration pointsgravity assistlow-thrustpatched conicstwo-body impulsive maneuvers

Mathematics Subject Classification ID

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

Related Items (6)

High-Order Parameterization of Stable/Unstable Manifolds for Long Periodic Orbits of Maps ⋮ Breakdown of homoclinic orbits to \(L_3\) in the RPC3BP. II: An asymptotic formula ⋮ A picture of solar-sail heteroclinic enhanced connections between Lissajous libration point orbits ⋮ Transport and invariant manifolds near \(L_3\) in the Earth-Moon bicircular model ⋮ Transfers between libration point orbits of Sun-Earth and Earth-Moon systems by using invariant manifolds ⋮ Efficient representation of invariant manifolds of periodic orbits in the CRTBP

Uses Software

• Unnamed Item

Cites Work

• Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
• Invariant manifolds ofL₃and horseshoe motion in the restricted three-body problem
• Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
• Connecting orbits and invariant manifolds in the spatial restricted three-body problem
• SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization
• BURRAU'S PROBLEM OF THREE BODIES

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