The Gravisphere Method Algorithm Programming

dc.creatorRosaev, A. E.
dc.date2008-01-23
dc.date.accessioned2026-07-07T08:56:02Z
dc.date.available2026-07-07T08:56:02Z
dc.descriptionThe action sphere method program is written. The initial conditions set at pericenter of planetocentric orbits. When action sphere radius is reached, the heliocentric orbit is calculated and data redirected to numeric integration program. The method is useful for capture and collision problem investigation. The very preliminary numeric results were obtained and discussed. A manifold in orbital elements space, leads to temporary capture about 50 year (4 Jupiter revolutions), was found.
dc.description8 pages with 4 figures
dc.identifierhttps://arxiv.org/abs/0801.3508
dc.identifierhttp://arxiv.org/abs/0801.3508
dc.identifier.urihttp://salesiana.dossiersoluciones.com/handle/123456789/146471
dc.subjectAstrophysics
dc.titleThe Gravisphere Method Algorithm Programming
dc.typetext

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