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Orbit's Structure in the Isosceles Rectilinear Restricted Three-Body Problem
Authors:J Martínez Alfaro  R B Orellana
Institution:(1) Department de Matemàtica Aplicada i Astronomia, Universitat de València, Spain;(2) CONICET (Profoeg), Observatorio Astgronómico de La Plata, Argentina
Abstract:The isosceles rectilinear restricted three-body problem can be considered as the Sitnikov's problem with eccentricity one or, as the isosceles problem when the central mass is zero and the primaries move having consecutive elliptic collisions. We compactify the phase space and analyze the flow on their boundary. This allows us to separate the phase space into different regions depending on the kind of orbits. This revised version was published online in July 2006 with corrections to the Cover Date.
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