Classical trajectories in Coulomb three body systems

ABSTRACT: computer program for calculating orbits and Poincaré sections in the classical Coulomb three body problem with arbitrary masses and charges in three dimensional space is presented.The regularization procedure necessary to obtain a reliable numerical integration of the equations of motion i...

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Autores:
Mahecha Gómez, Jorge Eduardo
Pérez Arango, Fernando
Tipo de recurso:
Article of investigation
Fecha de publicación:
1995
Institución:
Universidad de Antioquia
Repositorio:
Repositorio UdeA
Idioma:
eng
OAI Identifier:
oai:bibliotecadigital.udea.edu.co:10495/30629
Acceso en línea:
https://hdl.handle.net/10495/30629
https://rmf.smf.mx/ojs/index.php/rmf/article/view/2636
Palabra clave:
Órbitas
Orbits
Mecánica celeste
Mechanics, celestial
Problema de los tres cuerpos
Problem of three bodies
Rights
openAccess
License
http://creativecommons.org/licenses/by-nc-nd/2.5/co/