The rectilinear three-body problem as a basis for studying highly eccentric systems

DOI10.1007/s10569-017-9796-2zbMath1447.70012arXiv1708.04856OpenAlexW2747651028MaRDI QIDQ1706318

M. Gaitanas, Kleomenis Tsiganis, George Voyatzis

Publication date: 21 March 2018

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

Full work available at URL: https://arxiv.org/abs/1708.04856

zbMATH Keywords

periodic orbitsorbital stabilityplanetary systemselliptic restricted TBPrectilinear model

Mathematics Subject Classification ID

Three-body problems (70F07) Celestial mechanics (70F15)

Related Items (3)

Determination of the doubly symmetric periodic orbits in the restricted three-body problem and Hill's lunar problem ⋮ On quasi-satellite periodic motion in asteroid and planetary dynamics ⋮ Networks and Bifurcations of Eccentric Orbits in Exoplanetary Systems

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