Modeling the evection resonance for trojan satellites: application to the Saturn system
C. A. Giuppone, F. Roig, X. Saad-Olivera

TL;DR
This paper develops an analytical and numerical study of the evection resonance's impact on trojan satellites, focusing on Saturn's moons, revealing how resonance influences their stability and past orbital configurations.
Contribution
It introduces an analytic model for the evection resonance in trojan pairs and compares it with numerical simulations, highlighting differences from single satellite cases.
Findings
The phase space structure for trojan satellites resembles that of single satellites.
Libration centers are shifted depending on the periastron difference and mass ratio.
Rhea's past may have involved crossing the evection resonance, affecting its satellite system.
Abstract
The stability of satellites in the solar system is affected by the so-called evection resonance. The moons of Saturn, in particular, exhibit a complex dynamical architecture in which co-orbital configurations occur, especially close to the planet where this resonance is present. We address the dynamics of the evection resonance, with particular focus on the Saturn system, and compare the known behavior of the resonance for a single moon to that of a pair of moons in co-orbital trojan configuration. We developed an analytic expansion of the averaged Hamiltonian of a trojan pair of bodies, including the perturbation from a distant massive body. {The analysis of the corresponding equilibrium points was restricted to the asymmetric apsidal corotation solution of the co-orbital dynamics.} We also performed numerical N-body simulations to construct dynamical maps of the stability of the…
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