Comparison of ELP-2000 with a numerical integration at the JPL

Astronomy and Astrophysics – Astronomy

Scientific paper

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Moon, Orbits, Motion, Comparisons, Models, Perturbations, Data, Tidal Effects, Ephemeris, Celestial Mechanics, Theoretical Studies, Procedure, Astronomy

Scientific paper

The semianalytical solution for the lunar orbit, called ELP-2000, is compared to results of a numerical integration, LE-51, at the Jet Propulsion Laboratory. LE-51 was designed to compare a lunar ephemeris with observations, including laser ranging. The components of ELP-2000 are described, noting the contributions to the Main Problem, perturbations due to the presence of the earth, direct and indirect planetary perturbations, etc. An ephemeris of 1980-2002 has been generated in two-day steps. The models are compared for lunar and solar parameters, reference frames, and trends in lunar angles, with specific attention to the shifting of the nodes and perigee. It is noted that the results are tentative, as ELP-2000 is as yet incomplete and LE-51 is the only model available for comparison.

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