2010
DOI: 10.1051/0004-6361/200913048
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About the dynamics of the evection resonance

Abstract: Context.The evection resonance appears to be the outermost region of stability for prograde satellite orbiting a planet, the critical argument of the resonance indeed being found librating in regions surrounded only by chaotic orbits. The dynamics of the resonance itself is thus of great interest for the stability of satellites, but its analysis by means of an analytical model is not straightforward because of the high perturbations acting on the dynamical region of interest. Aims. It is thus important to show… Show more

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Cited by 24 publications
(32 citation statements)
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“…In addition, the inner orbit precession frequency can be close to, but still longer than the outer orbital period in some cases (such as in the Earth-Moon system), in which case evection terms may become important. In case of comparable inner orbit precession frequency and outer orbital period, the evection resonance can come into play (e.g., Frouard et al 2010;Grishin et al 2017). Another example is the occurrence of mean-motion resonance in 2+2 systems (Breiter & Vokrouhlický 2018).…”
Section: Breakdown Of the Averaging Approximationmentioning
confidence: 99%
“…In addition, the inner orbit precession frequency can be close to, but still longer than the outer orbital period in some cases (such as in the Earth-Moon system), in which case evection terms may become important. In case of comparable inner orbit precession frequency and outer orbital period, the evection resonance can come into play (e.g., Frouard et al 2010;Grishin et al 2017). Another example is the occurrence of mean-motion resonance in 2+2 systems (Breiter & Vokrouhlický 2018).…”
Section: Breakdown Of the Averaging Approximationmentioning
confidence: 99%
“…Special care has been taken in the study of (i) the secular resonance ν =˙ −˙ (Saha & Tremaine 1993;Whipple & Shelus 1993;Beaugé & Nesvorný 2007;Nesvorný et al 2003;Yokoyama et al 2003;Ćuk & Burns 2004;Correa Otto et al 2009), which is one of the most important secular resonances acting on the satellites; (ii) the Lidov-Kozaï resonance for distant satellites (Beaugé et al 2006;Beaugé & Nesvorný 2007;Carruba et al 2002;Ćuk & Burns 2004;Nesvorný et al 2003); and (iii) the evection resonancė − n (Yokoyama et al 2008;Frouard et al 2010;Nesvorný et al 2003). In most of these works, the important need for the development of high-order perturbation methods or numerical ones is clearly stressed.…”
Section: Introductionmentioning
confidence: 99%
“…We note that when m 3 = 0, all the A ki and C k functions are zero and the expansion reduces to the same expansion as reported by Robutel & Pousse (2013), with the addition of the oblateness terms D i . On the other hand, when m 2 = 0, all the B k and C k functions are zero, and the expansion reduces to the classical expansion of the lunar theory, again with the addition of the oblateness terms (Frouard et al 2010).…”
Section: Analytical Model For Trojan Satellitesmentioning
confidence: 99%
“…Therefore, regions with large variations in δe i are more sensitive to perturbations and are very likely chaotic. Frouard et al (2010) used a similar indicator in their study of the evection resonance in Jupiter satellites, defined as (e τa max −e τ b max )/e τa max , where the total integration time, τ , was divided into two consecutive samples τ a and τ b . Nevertheless, we realized that this indicator is quite sensitive to the value of τ and may artificially create some structures that are not related with actual resonances.…”
Section: Numerical Studymentioning
confidence: 99%