A new method for computing special perturbations in the three-body problem
In Nº 13 of the Information Bulletin for the Southern Hemisphere I have given an outline of this method. Let there be thee mass points S = Sun, J = Jupiter, and A = Asteroid (or Satellite) and let us suppose that the orbital plane of Jupiter is taken as a fixed plane of reference in which a frame of...
Guardado en:
| Autor principal: | |
|---|---|
| Formato: | Articulo Comunicacion |
| Lenguaje: | Español |
| Publicado: |
1970
|
| Materias: | |
| Acceso en línea: | http://sedici.unlp.edu.ar/handle/10915/97953 |
| Aporte de: |
| Sumario: | In Nº 13 of the Information Bulletin for the Southern Hemisphere I have given an outline of this method. Let there be thee mass points S = Sun, J = Jupiter, and A = Asteroid (or Satellite) and let us suppose that the orbital plane of Jupiter is taken as a fixed plane of reference in which a frame of fixed axes has been chosen in such a way that the X axis is oriented towards the perihelion of Jupiter. This system will be called “System I”. |
|---|