Abstract
Starting from the differential equations that describe the motion of a body of infinitesimal mass under the Newtonian gravitational field produced by two bodies of comparable mass which orbit in circular orbits about their common center of mass (circular, restricted, three-body problem), we obtained, by a Lie operator, solutions that permit, by recurrent algebraic expressions, to find the components of the position and velocity vectors by means of Lie series. We present a comparison between the numerical direct integrations and the solution by Lie series.
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References
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