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 is sketched. Different configurations of the helium atom and the positronium negative ion (ps-),obtained with the program, are analyzed.

• 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/