Abstract
The three-body problem with masses mo, εm1, εm2 is considered in the limiting case ε → 0. By appropriately scaling the coordinates the motion is described by the following two matched approximations: (1) the outer solution consisting of two independent Kepler motions about mo, (2) the inner solution satisfying Hill’s lunar equation. The discussion of Hill’s problem with appropriate boundary conditions at infinity correctly predicts that Saturn’s coorbiting satellites Janus and Epimetheus exchange orbits at the close encounter, whereas the F ring shepherds (1980S26 and 1980S27) do not.
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© 1985 D. Reidel Publishing Company
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Spirig, F., Waldvogel, J. (1985). The Three-Body Problem with Two Small Masses: A Singular-Perturbation Approach to the Problem of Saturn’s Coorbiting Satellites. In: Szebehely, V.G. (eds) Stability of the Solar System and Its Minor Natural and Artificial Bodies. NATO ASI Series, vol 154. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-5398-7_5
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DOI: https://doi.org/10.1007/978-94-009-5398-7_5
Publisher Name: Springer, Dordrecht
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