Direct and indirect capture of near-Earth asteroids in the Earth-Moon system

DOI10.1007/s10569-017-9764-xzbMath1478.70012OpenAlexW2606839648MaRDI QIDQ1682183

Matteo Ceriotti, Minghu Tan, Colin R. Mcinnes

Publication date: 28 November 2017

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

Full work available at URL: https://doi.org/10.1007/s10569-017-9764-x

zbMATH Keywords

periodic orbitscircular restricted three-body problemstable manifoldsdirect asteroid captureindirect asteroid capture

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

Related Items (2)

Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory ⋮ Using invariant manifolds to capture an asteroid near the \(L_3\) point of the Earth-Moon bicircular model

Cites Work

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• Optimal transfers between unstable periodic orbits using invariant manifolds
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• Numerical determination of Lissajous trajectories in the restricted three-body problem
• Analytic construction of periodic orbits about the collinear points
• Dynamics and Mission Design Near Libration Points
• Low energy transfer to the Moon
• Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun-Earth circular restricted three-body problem

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