Planetary and satellite three body mean motion resonances

•A method for calculating three body resonances between massive bodies is presented.•Dependence with masses, orbital elements and resonance order is showed.•Outwards and inwards migrations coexist inside a three body resonance.•An application to the Galilean satellites is presented. We propose a sem...

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Veröffentlicht in:	Icarus (New York, N.Y. 1962) N.Y. 1962), 2016-08, Vol.274, p.83-98
Hauptverfasser:	Gallardo, Tabaré, Coito, Leonardo, Badano, Luciana
Format:	Artikel
Sprache:	eng
Schlagworte:	Celestial mechanics Dynamics Eccentricity Inclination Jupiter satellites Mathematical models Orbital Orbital resonances (celestial mechanics) Orbits Planetary dynamics Resonances Satellites Strength
Online-Zugang:	Volltext
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