Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8056551 | Acta Astronautica | 2015 | 11 Pages |
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.
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Aerospace Engineering
Authors
Yuta Asano, Katsuhiko Yamada, Ichiro Jikuya,