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dc.date.accessioned 2022-04-05T19:03:32Z
dc.date.available 2022-04-05T19:03:32Z
dc.date.issued 1996
dc.identifier.uri http://sedici.unlp.edu.ar/handle/10915/133969
dc.description.abstract The stability and capture regions in phase space for retrograde and direct planetary satellites are investigated in the frame of the Circular Restricted Three-Body Problem. We show that a second integral of motion furnishes an accurate description for the stability limit of retrograde satellites. The distribution of heliocentric orbital elements is studied, and possible candidates to be temporary Jovian satellites are investigated. Previous results, limited to orbits satisfying the Mirror Theorem, are extended in order to give a complete set of capture conditions in phase-space. en
dc.format.extent 79-92 es
dc.language es es
dc.subject Restricted Three-Body Problem es
dc.subject Planetary Satellites es
dc.title On the Satellite Capture Problem en
dc.type Articulo es
sedici.identifier.other doi:10.1007/978-94-009-0307-4_7 es
sedici.title.subtitle Capture and stability regions for planetary satellites en
sedici.creator.person Brunini, Adrián es
sedici.subject.materias Ciencias Exactas es
sedici.subject.materias Bioquímica es
sedici.description.fulltext true es
mods.originInfo.place Facultad de Ciencias Astronómicas y Geofísicas es
sedici.subtype Articulo es
sedici.rights.license Creative Commons Attribution 4.0 International (CC BY 4.0)
sedici.rights.uri http://creativecommons.org/licenses/by/4.0/
sedici.description.peerReview peer-review es
sedici.relation.journalTitle Celestial Mechanicsand Dynamical Astronomy es
sedici.relation.journalVolumeAndIssue vol. 64, no. 1 es


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Creative Commons Attribution 4.0 International (CC BY 4.0) Excepto donde se diga explícitamente, este item se publica bajo la siguiente licencia Creative Commons Attribution 4.0 International (CC BY 4.0)