Abstract

A classical approach to the restricted three-body problem is to analyze the dynamics of the massless body in the synodic reference frame. A different approach is represented by the perturbative treatment: in particular the averaged problem of a mean-motion resonance allows to investigate the long-term behavior of the solutions through a suitable approximation that focuses on a particular region of the phase space. In this paper, we intend to bridge a gap between the two approaches in the specific case of mean-motion resonant dynamics, establish the limit of validity of the averaged problem and take advantage of its results in order to compute trajectories in the synodic reference frame. After the description of each approach, we develop a rigorous treatment of the averaging process, estimate the size of the transformation and prove that the averaged problem is a suitable approximation of the restricted three-body problem as long as the solutions are located outside the Hill’s sphere of the secondary. In such a case, a rigorous theorem of stability over finite but large timescales can be proven. We establish that a solution of the averaged problem provides an accurate approximation of the trajectories on the synodic reference frame within a finite time that depend on the minimal distance to the Hill’s sphere of the secondary. The last part of this work is devoted to the co-orbital motion (i.e., the dynamics in 1:1 mean-motion resonance) in the circular-planar case. In this case, an interpretation of the solutions of the averaged problem in the synodic reference frame is detailed and a method that allows to compute co-orbital trajectories is displayed.

Highlights

  • This work focuses on the restricted three-body problem, that is the study of the motion of a massless body affected by the gravitational attraction of two massive bodies

  • The analysis of the dynamics in the synodic reference frame, that is the frame rotating with the mean longitude of the secondary, is the classical approach adopted for the restricted three-body problem

  • We showed that the averaged problem provides another approach in order to study some families of periodic orbits of the restricted three-body problem

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Summary

Introduction

This work focuses on the restricted three-body problem, that is the study of the motion of a massless body affected by the gravitational attraction of two massive bodies. When the massless body is in mean-motion resonance with the secondary, that is, when their orbital periods are commensurable, the transformation leading to the secular Hamiltonian is no more close to the identity and the solutions of the secular problem do not provide a good representation of the real motion In such a case, it is still possible to use averaging techniques: the averaging process is performed over one mean longitude, generally the one of the secondary, and after the introduction of a resonant angle, that is a particular linear combination of the two mean longitudes which characterizes the mean-motion resonance. In the present paper, we intend to generalize the result given by Robutel et al [29] and provide rigorous estimates on the averaging process in order to define a domain of validity of the averaged problem, in the case of a generic mean-motion resonance, and for any value of inclination and eccentricities (massless body as well as secondary). Appendix A gives the proof of the theorems and lemma used in our reasonings

Definition in the heliocentric reference frame
Hamiltonian formalism
The synodic reference frame
Perturbative treatment of a mean-motion resonance: the averaged problem
The resonant variables
The averaged problem
Some conclusions about the averaged problem
Notations
The averaging process
Quantitative treatment of the averaging process
Discussion
The co-orbital motion in the circular-planar case
Reading a phase portrait
A “map” of the co-orbital motion in the circular-planar case
Conclusions
Proof of Lemma 1
Proof of Theorem 1
Proof of Theorem 2
Full Text
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