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Ejection-collision orbits in the Restricted three-body problem

Autor
Olle, M.; Rodriguez, O.; Soler, J.
Tipus d'activitat
Article en revista
Revista
Communications in nonlinear science and numerical simulation
Data de publicació
2018-02
Volum
55
Pàgina inicial
298
Pàgina final
315
DOI
https://doi.org/10.1016/j.cnsns.2017.07.013 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/110642 Obrir en finestra nova
URL
http://www.sciencedirect.com/science/article/pii/S1007570417302642?via%3Dihub Obrir en finestra nova
Resum
In this paper we analyse the ejection-collision (EC) orbits of the planar restricted three body problem. Being µ¿¿¿(0, 0.5] the mass parameter, and taking the big (small) primary with mass (µ), an EC orbit will be an orbit that ejects from the big primary, does an excursion and collides with it. As it is well known, for any value of the mass parameter µ¿¿¿(0, 0.5] and sufficiently restricted Hill regions (that is, for big enough values of the Jacobi constant C), there are exactly four E...
Citació
Olle, M., Rodriguez, O., Soler, J. Ejection-collision orbits in the Restricted three-body problem. "Communications in nonlinear science and numerical simulation", Febrer 2018, vol. 55, p. 298-315.
Paraules clau
Regularization, Ejection-collision Orbits, Invariant Manifolds, Bifurcations
Grup de recerca
SD - Sistemes Dinàmics