dc.creatorAltavista, Carlos Alberto
dc.date1970
dc.date2020-06-10T13:54:52Z
dc.date.accessioned2023-07-14T20:46:07Z
dc.date.available2023-07-14T20:46:07Z
dc.identifierhttp://sedici.unlp.edu.ar/handle/10915/97953
dc.identifierissn:1669-9521
dc.identifier.urihttps://repositorioslatinoamericanos.uchile.cl/handle/2250/7440523
dc.descriptionIn 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”.
dc.descriptionAsociación Argentina de Astronomía
dc.formatapplication/pdf
dc.languageen
dc.rightshttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rightsCreative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
dc.subjectAstronomía
dc.subjectGalaxias
dc.titleA new method for computing special perturbations in the three-body problem
dc.typeArticulo
dc.typeComunicacion


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