Author:
Pousse Alexandre,Alessi Elisa Maria
Abstract
AbstractA 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.
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering
Reference37 articles.
1. Arnol’d, V.I.: Small denominators and problems of stability of Motion in classical and celestial mechanics. Russian Math. Surv. 18, 85–191 (1963)
2. Arnol’d, V.I.: Mathematical Methods of Classical Mechanics. Springer-Verlarg, New York (1989)
3. Barrabés, E., Ollé, M.: Invariant manifolds of L3 and horseshoe motion in the restricted three-body problem. Nonlinearity 19, 2065–2089 (2006)
4. Benest, D.: Effects of the mass ratio on the existence of retrograde satellites in the circular plane restricted problem. Astron. Astrophys. 32, 39–46 (1974)
5. Chenciner, A.: Poincaré and the three-body problem. Séminaire Poincaré (Bourbaphy) XVI: Poincaré 1912-2012 pp. 45–133 (2012)
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献