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Secular resonances between bodies on close orbits: a case study of the Himalia prograde group of jovian irregular satellites

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Abstract

The gravitational interaction between two objects on similar orbits can effect noticeable changes in the orbital evolution even if the ratio of their masses to that of the central body is vanishingly small. Christou (Icarus 174:215–229, 2005) observed an occasional resonant lock in the differential node \(\varDelta \varOmega \) between two members in the Himalia irregular satellite group of Jupiter in the N-body simulations (corresponding mass ratio \(\sim 10^{-9}\)). Using a semianalytical approach, we have reproduced this phenomenon. We also demonstrate the existence of two additional types of resonance, involving angle differences \(\varDelta \omega \) and \(\varDelta (\varOmega +\varpi )\) between two group members. These resonances cause secular oscillations in eccentricity and/or inclination on timescales \(\sim \)1 Myr. We locate these resonances in (aei) space and analyse their topological structure. In subsequent N-body simulations, we confirm these three resonances and find a fourth one involving \(\varDelta \varpi \). In addition, we study the occurrence rates and the stability of the four resonances from a statistical perspective by integrating 1000 test particles for 100 Myr. We find \(\sim \)10 to 30 librators for each of the resonances. Particularly, the nodal resonance found by Christou is the most stable: 2 particles are observed to stay in libration for the entire integration.

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Notes

  1. Dia was discovered in 2000 and then lost. It was recently recovered by S. S. Sheppard; see http://dtm.carnegiescience.edu/news/long-lost-moon-jupiter-found. For the mass estimates of the members, see http://ssd.jpl.nasa.gov/?sat_phys_par. For orbital elements, see http://ssd.jpl.nasa.gov/?sat_elem. Parameters of other satellites from the latter two links will be used in Sect. 5.

  2. Though the form appears asymmetric in \(e_{\mathrm {r}}\) and \(i_{\mathrm {r}}\), exchanging \(e_{\mathrm {r}}\) and \(i_{\mathrm {r}}\) will not alter the value.

  3. All integrations of the equations of motion derived from Kozai and/or coorbital theory are carried out with a 7th order Runge–Kutta method; the step-size is adjusted with an 8th order error estimate. The single step error tolerance is \(10^{-14}\).

  4. In fact, the node precesses with negative rates. Thus when above the SEPR, the test particle has smaller absolute precession rate.

  5. We generate 500 randomly distributed particles on the SEPR in \(\varpi \) and integrate them for \(2\times 10^6\). Visual check shows no apsidal resonance.

  6. All N-body simulations are implemented with the general Bulirsch-Stoer algorithm in the MERCURY package (Chambers 1999; Hahn and Malhotra 2005) with a tolerance \(10^{-12}\). Over an integration time of \(10^8\) yr, the errors in energy and angular momentum are both of order \(10^{-10}\).

  7. Note that, when they published the paper, four satellites: Himalia, Elara, Leda and Lysithea were confirmed as group members. The recently recovered fifth member, Dia, has the largest semimajor axis and eccentricity. Our simple experiments show that the criterion has to be updated to \( d \lesssim \) 510 m/s to include Dia. In this paper, we stick to the results of Beaugé and Nesvorný (2007).

  8. In the N-body simulations, the initial osculating elements of the real objects are taken from the JPL HORIZONS System http://ssd.jpl.nasa.gov/?horizons.

  9. The particle in Fig. 18 described below is not a typical example: for a librator to be stable for \(5.3\times 10^7\), it has to lie well within the resonance. Most librators only pass through libration.

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Acknowledgments

DL thanks Dr. Matjia Ćuk for correspondences on the evection phenomenon. We are grateful for the helpful comments from two anonymous referees, increasing the quality of the paper. The authors wish to acknowledge the SFI/HEA Irish Centre for High-End Computing (ICHEC) for the provision of computational facilities and support. Astronomical research at the Armagh Observatory is funded by the Northern Ireland Department of Culture, Arts and Leisure (DCAL). Figure 1 is produced using LibreOffice Draw; all the other figures are generated with gnuplot.

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Appendices

Appendix 1: Derivation of the “averaged” Kozai Hamiltonian

We derive the Kozai Hamiltonian (11) from its original form (4) here. First, we substitute e and i in Eq. (4) in terms of the angular momenta G and H. Then we solve for G so \(G=G(F,H,\omega ,const.)\), where const. refers to combinations of k, \(m_\odot \), a and \(a_\odot \). Note that in this expression, F, H and const. are all constant and only \(\omega \) and G are variable. Furthermore, it can be shown with this equation that the variation in eccentricity during a Kozai cycle, \(\varDelta e^2\) is a small quantity (e.g., for Himalia’s nominal orbit, \(\varDelta e^2\lesssim 0.03\)). Therefore, we assume that the angular momentum \(G\propto \sqrt{1-e^2}\) can be expressed as

$$\begin{aligned} G^2=b_0+b_1 \cos 2 \omega + \cdots , \end{aligned}$$
(29)

where the coefficients \(b_1\ll b_0\). We can then express \(b_0\) and \(b_1\) as functions of F, H and const. by comparing the above equation with \(G=G(F,H,\omega ,const.)\). Now, if we further omit the term \(b_1 \cos 2 \omega \) we have

$$\begin{aligned} G^2=b_0=b_0(F,H,const.)\propto {1-\langle e\rangle ^2}. \end{aligned}$$
(30)

Here, \(\langle e\rangle \) is not the e in the original Hamiltonian (4) but the averaged e over a Kozai cycle. Meanwhile, we also have \(H^2\propto (1-\langle e\rangle ^2)\cos ^2\langle i\rangle \) and \(\langle i\rangle \) is the averaged i. Then we solve Eq. (30) for F. So now F is a function of H, \(b_0=G^2\) and const.. After substituting \(\langle e\rangle \) and \(\langle i\rangle \) into it, we arrive at the “averaged” Kozai Hamiltonian (11). The new eccentricity and inclination are constant under the solar forcing; for simplicity, we still use the old notations e and i.

Appendix 2: The non-canonical property of coorbital potential

As stated in Sect. 3.3, the coorbital potential (6) (and hence (17)) is not canonical in the variables used in Eq. (16). To prove this, we presume it is canonical and introduce the following canonical transformations. For the first transformation, we name the variables on the left side as “absolute Cartesian” variables.

$$\begin{aligned} {\bar{G}}_{\mathrm {y},\mathrm {H}}= & {} \sqrt{2 {{\bar{G}}}_{\mathrm {H}}} \sin {\bar{g}_{\mathrm {H}}} ,\quad {\bar{G}}_{\mathrm {x},\mathrm {H}}= \sqrt{2 {{\bar{G}}}_{\mathrm {H}}} \cos {\bar{g}_{\mathrm {H}}} ;\nonumber \\ \bar{H}_{\mathrm {y},\mathrm {H}}= & {} \sqrt{2 {\bar{H}}_{\mathrm {H}}} \sin {\bar{h}_{\mathrm {H}}} ,\quad \bar{H}_{\mathrm {x},\mathrm {H}}= \sqrt{2 {\bar{H}}_{\mathrm {H}}} \cos {\bar{h}_{\mathrm {H}}} ;\nonumber \\ {\bar{G}}_\mathrm {y,P}= & {} \sqrt{2 {{\bar{G}}}_{\mathrm {P}}} \sin {\bar{g}_{\mathrm {P}}} ,\quad {\bar{G}}_\mathrm {x,P}= \sqrt{2 {{\bar{G}}}_{\mathrm {P}}} \cos {\bar{g}_{\mathrm {P}}} ;\nonumber \\ \bar{H}_\mathrm {y,P}= & {} \sqrt{2 {\bar{H}}_{\mathrm {P}}} \sin {\bar{h}_{\mathrm {P}}} ,\quad \bar{H}_\mathrm {x,P}= \sqrt{2 {\bar{H}}_{\mathrm {P}}} \cos {\bar{h}_{\mathrm {P}}} . \end{aligned}$$
(31)

On the right-hand sides of the above expressions, \(({\bar{g}},\,{{\bar{G}}})\) and \(({\bar{h}},\,{\bar{H}})\) are conjugate Poincaré variables with subscripts “H” and “P” referring to Himalia and a particle, respectively. Then another transformation is introduced. The variables on the left are referred to as “relative Cartesian” variables.

$$\begin{aligned} {\bar{G}}_\mathrm {y,t}= & {} {\bar{G}}_\mathrm {y,P}/\sqrt{2}+ {\bar{G}}_{\mathrm {y},\mathrm {H}}/\sqrt{2} ,\quad {\bar{G}}_\mathrm {x,t}= {\bar{G}}_\mathrm {x,P}/\sqrt{2}+{\bar{G}}_{\mathrm {x},\mathrm {H}}/\sqrt{2} ;\nonumber \\ \bar{H}_\mathrm {y,t}= & {} \bar{H}_\mathrm {y,P}/\sqrt{2}+\bar{H}_{\mathrm {y},\mathrm {H}}/\sqrt{2} ,\quad \bar{H}_\mathrm {x,t}=\bar{H}_\mathrm {x,P}/\sqrt{2}+\bar{H}_{\mathrm {x},\mathrm {H}}/\sqrt{2} ;\nonumber \\ {\bar{G}}_\mathrm {y,r}= & {} {\bar{G}}_\mathrm {y,P}/\sqrt{2}-{\bar{G}}_{\mathrm {y}, \mathrm {H}}/\sqrt{2} ,\quad {\bar{G}}_\mathrm {x,r} {\bar{G}}_\mathrm {x,P}/\sqrt{2}-{\bar{G}}_{\mathrm {x}, \mathrm {H}}/\sqrt{2} ;\nonumber \\ \bar{H}_\mathrm {y,r}= & {} \bar{H}_\mathrm {y,P}/\sqrt{2}-\bar{H}_{\mathrm {y}, \mathrm {H}}/\sqrt{2} ,\quad \bar{H}_\mathrm {x,r}= \bar{H}_\mathrm {x,P}/\sqrt{2}-\bar{H}_{\mathrm {x},\mathrm {H}}/\sqrt{2} . \end{aligned}$$
(32)

This relates the variables with subscript “r” to the variables used in the coorbital theory as given by Namouni (1999); see the paragraph containing Eqs. (6)–(9).

Now note that, since we assume the coorbital potential is canonical in the original Poincaré variables, it should preserve the Hamiltonian property in the variables above. However, since the coorbital potential contains only the relative elements, i.e., in the relative Cartesian variables, it only depends on the variables with subscript “r”. Hence, if we consider the Jupiter–Himalia-particle system. The quantities with subscript “t” will be conserved. However, this is not possible. Taking \({\bar{G}}_\mathrm {y,t}={\bar{G}}_\mathrm {y,P}/\sqrt{2}+{\bar{G}}_{\mathrm {y},\mathrm {H}}/\sqrt{2}\) for instance. Since the test particle is massless, it should have no influence on Himalia and thus the second term on the right hand side \({\bar{G}}_{\mathrm {y},\mathrm {H}}/\sqrt{2}\) is constant. From the above reasoning, we know that, \({\bar{G}}_\mathrm {y,t}\) should be conserved. This means that, the first term on the right hand side, \({\bar{G}}_\mathrm {y,P}/\sqrt{2}=\sqrt{{{\bar{G}}}_{\mathrm {P}}} \sin {\bar{g}_{\mathrm {P}}}\) will no change. Similarly, \(\sqrt{{{\bar{G}}}_{\mathrm {P}}} \cos {\bar{g}_{\mathrm {P}}}\), \(\sqrt{{\bar{H}}_{\mathrm {P}}} \sin {\bar{h}_{\mathrm {P}}}\) and \(\sqrt{{\bar{H}}_{\mathrm {P}}} \cos {\bar{h}_{\mathrm {P}}}\) should all be constant. If so, the orbital elements of the particle are not evolving under the perturbation of Himalia. Of course this is not true—the coorbital potential is not a Hamiltonian in the variables used here.

However, the level-curve like structure in the phase diagrams Figs. 8, 10 and 11 of the three types of resonance suggests the existence of a conserved quantity (a Hamiltonian) for these two-dimensional systems. We have tried to construct one of the form of \(F_\mathrm {T}=F_{\mathrm {S}}+A \times R_{\mathrm {S}}\) (see Eqs. (16) and (17)), where A is a constant depending on some non-changing parameters. For instance, for the case of nodal resonance, A could be a function of the masses, the semimajor axes and the eccentricities (but not a function of inclinations). However, the solution for A seems to be nonexistent (at least for the nodal resonance). Thus we argue that, the conserved quantity of the two-dimensional systems might be of more complicated forms.

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Li, D., Christou, A.A. Secular resonances between bodies on close orbits: a case study of the Himalia prograde group of jovian irregular satellites. Celest Mech Dyn Astr 125, 133–160 (2016). https://doi.org/10.1007/s10569-016-9676-1

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