Breakdown of homoclinic orbits to L3 in the RPC3BP (II): an asymptotic formula

The Restricted 3-Body Problem models the motion of a body of negligible mass under the gravitational influence of two massive bodies called the primaries. If one assumes that the primaries perform circular motions and that all three bodies are coplanar, one has the Restricted Planar Circular 3-Body...

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Detalles Bibliográficos
Autores: Baldomá Barraca, Inmaculada|||0000-0002-4838-1186, Giralt Miron, Mar, Guardia, Marcel
Tipo de recurso: artículo
Fecha de publicación:2023
País:España
Institución:Universitat Politècnica de Catalunya (UPC)
Repositorio:UPCommons. Portal del coneixement obert de la UPC
Idioma:inglés
OAI Identifier:oai:upcommons.upc.edu:2117/394711
Acceso en línea:https://hdl.handle.net/2117/394711
https://dx.doi.org/10.1016/j.aim.2023.109218
Access Level:acceso abierto
Palabra clave:Hamiltonian systems
Exponentially small phenomena
Splitting of separatrices
Celestial mechanics
Coorbital motions
L3 Lagrange point
Classificació AMS::37 Dynamical systems and ergodic theory
Classificació AMS::70 Mechanics of particles and systems::70M20 Orbital mechanics
Àrees temàtiques de la UPC::Matemàtiques i estadística
Descripción
Sumario:The Restricted 3-Body Problem models the motion of a body of negligible mass under the gravitational influence of two massive bodies called the primaries. If one assumes that the primaries perform circular motions and that all three bodies are coplanar, one has the Restricted Planar Circular 3-Body Problem (RPC3BP). In rotating coordinates, it can be modeled by a two degrees of freedom Hamiltonian, which has five critical points called the Lagrange points L1, . . . , L5. The Lagrange point L3 is a saddle-center critical point which is collinear with the primaries and beyond the largest of the two. In this paper, we obtain an asymptotic formula for the distance between the stable and unstable manifolds of L3 for small values of the mass ratio 0 < \mu \leqslant 1. In particular we show that L3 cannot have (one round) homoclinic orbits. If the ratio between the masses of the primaries \mu is small, the hyperbolic eigenvalues of L3 are weaker, by a factor of order \sqrt{\mu }, than the elliptic ones. This rapidly rotating dynamics makes the distance between manifolds exponentially small with respect to \sqrt{\mu } . Thus, classical perturbative methods (i.e. the Melnikov-Poincaré method) can not be applied.