Article ID Journal Published Year Pages File Type
8056551 Acta Astronautica 2015 11 Pages PDF
Abstract
A computational procedure is presented for approximating elliptic halo orbits about the collinear equilibrium points based on the variation of constants in the sense of the second-order approximation. Simulation results show that the approximate solutions agree well with the results of two-point boundary-value problems. The existence conditions of the elliptic halo orbits are also determined with respect to the mass ratio of the primaries and the eccentricity.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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