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Some Aspects of Constructing Long Ephemerides of the Sun, Major Planets and the Moon: Ephemeris AE95

Published online by Cambridge University Press:  12 April 2016

G.I. Eroshkin ,
N.I. Glebova ,
M.A. Fursenko  and
A. A. Trubitsina
G.I. Eroshkin
Affiliation:
Institute of Theoretical Astronomy, Russian Acad. of Sciences St. Petersburg, Russia
N.I. Glebova
Affiliation:
Institute of Theoretical Astronomy, Russian Acad. of Sciences St. Petersburg, Russia
M.A. Fursenko
Affiliation:
Institute of Theoretical Astronomy, Russian Acad. of Sciences St. Petersburg, Russia
A. A. Trubitsina
Affiliation:
Institute of Theoretical Astronomy, Russian Acad. of Sciences St. Petersburg, Russia

Extract

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The construction of long-term numerical ephemerides of the Sun, major planets and the Moon is based essentially on the high-precision numerical solution of the problem of the motion of these bodies and polynomial representation of the data. The basis of each ephemeris is a mathematical model describing all the main features of the motions of the Sun, major planets, and Moon. Such mathematical model was first formulated for the ephemerides DE/LE and was widely applied with some variations for several national ephemeris construction. The model of the AE95 ephemeris is based on the DE200/LE200 ephemeris mathematical model. Being an ephemeris of a specific character, the AE95 ephemeris is a basis for a special edition “Supplement to the Astronomical Yearbook for 1996–2000”, issued by the Institute of the Theoretical Astronomy (ITA) (Glebova et al., 1995). This ephemeris covering the years 1960–2010 is not a long ephemeris in itself but the main principles of its construction allow one to elaborate the long-term ephemeris on an IBM PC-compatible computer. A high-precision long-term numerical integration of the motion of major bodies of the Solar System demands a choice of convenient variables and a high-precision method of the numerical integration, taking into consideration the specific features of both the problem to be solved and the computer to be utilized.

Type
Solar System Dynamics
Information
International Astronomical Union Colloquium , Volume 165: Dynamics and Astrometry of Natural and Artificial Celestial Bodies , 1997 , pp. 245 - 250
Copyright
Copyright © Kluwer 1997

References

Belikov, M.V.: 1993, “Methods of numerical integiation with uniform and mean square approximation for solving problems of ephemeris astronomy and satellite geodesy”, Manuscr. Geod. 15, 182–200.Google Scholar
Eroshkin, G.I., Taibatorov, K.A., and Trubitsina, A.A.: 1993, “Constructing the specialized numerical ephemerides of the Moon and the Sun for solving the problems of the Earth’s artificial satellite dynamics”, ITA RAS Preprint No. 31 (in Russian).Google Scholar
Glebova, N.I., Fursenko, M.A. Eroshkin, G.I., and Trubitsina, A.A.: 1995, “Supplement No 29-30 to the Astronomical Yearbook for 1996-2000”, ITA RAS, 347 pp. (in Russian).Google Scholar
Trubitsina, A.A.: 1996, “Experience of numerical integration and approximation with applying Chebyshev polynomials for constructing ephemerides of the solar system natural and artificial bodies”, in: Dynamics, Ephemerides and Astrometry of the Solar System, IAU Symposium 172 (Ferraz-Mello, S., Morando, B., Arlot, J.E., eds), Kluwer, Dordrecht, 347–352.Google Scholar