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Doubly Asymptotic Orbits at the Unstable Equilibrium in the Elliptic Restricted Problem
[chapter]
1983
Astrophysics and Space Science Library
Preserved Fulltext
Outgoing asymptotic orbits at a collinear Equilibrium point of the elliptic restricted three-body problem are constructed analytically and numerically and those which intersect perpendicularly the axis of symmetry are selected by means of a numerical procedure of differential corrections. Due to the symmetry properties of the problem, the latter orbits terminate asymptotically back to the equilibrium point and therefore provide a kind of "asymptotic trapping" at the unstable equilibrium, a
doi:10.1007/978-94-009-7214-8_37
fatcat:fqswoe5szbfwhhbvs23eipzn5m