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Second-order matching in the restricted three-body problem (smallμ)
Authors:J. V. Breakwell  L. M. Perko
Affiliation:1. Dept. of Astronautics and Aeronautics, Stanford University, Stanford, Calif., USA
2. Dept. of Mathematics, Northern Arizona University, Flagstaff, Ariz., USA
Abstract:Elliptic orbits around the large primary are matched to hyperbolas, osculating at closest approach, around the small primary of the circular restricted three-body problem. The distance of closest approach to the small primary is assumed to be of the same order as the mass-ratio μ of small to large primary. The dependence of the hyperbola on initial conditions for the elliptic orbit is carried to second order jointly in μ and in the variations of the initial conditions, which are three-dimensional rather than two-dimensional.
Keywords:
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