2011
DOI: 10.1007/s10509-011-0641-x
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Symmetric horseshoe periodic orbits in the general planar three-body problem

Abstract: We present some families of horseshoe periodic orbits in the general planar three-body problem for the case of two equal masses. The considered system is a symmetric version of the one formed by Saturn, Janus and Epimetheus. We use a mass ratio equal to 35 × 10 −5 , corresponding to 10 5 times the Saturn-Janus mass parameter of the restricted case; for this mass ratio the satellites have a significantly bigger influence on the planet than in the classical Saturn, Janus and Epimetheus system. To obtain periodic… Show more

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Cited by 8 publications
(5 citation statements)
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“…Thus, we follow a different way. We use as Γ an initial condition of a periodic horseshoe orbit computed for the threebody problem [9] (any initial condition given in such reference works-it was corroborated that these initial conditions give rise to exchange-a orbits in the five-body problem). In the three-body problem, take the initial condition of that horseshoe orbit and integrate it numerically until the isosceles reversible configuration is reached.…”
Section: Determination Of γ Rmentioning
confidence: 84%
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“…Thus, we follow a different way. We use as Γ an initial condition of a periodic horseshoe orbit computed for the threebody problem [9] (any initial condition given in such reference works-it was corroborated that these initial conditions give rise to exchange-a orbits in the five-body problem). In the three-body problem, take the initial condition of that horseshoe orbit and integrate it numerically until the isosceles reversible configuration is reached.…”
Section: Determination Of γ Rmentioning
confidence: 84%
“…First, obtain an initial condition Γ with the additional requirement of appropriate encounters by the corresponding orbit, that is of exchange-a type (horseshoeshaped in the rotating frame). To obtain Γ we use as a guide an initial condition of some known horseshoe orbit belonging to the three-body problem [9]. Second, determine S restricted to those orbits with appropriate encounters.…”
Section: Numerical Analysismentioning
confidence: 99%
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