Astronomy and Astrophysics – Astronomy
Scientific paper
Sep 1985
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985sva....29..584h&link_type=abstract
(Astronomicheskii Zhurnal, vol. 62, Sept.-Oct. 1985, p. 1008-1017) Soviet Astronomy (ISSN 0038-5301), vol. 29, Sept.-Oct. 1985,
Astronomy and Astrophysics
Astronomy
Astrodynamics, Satellite Orbits, Trigonometric Functions, Two Body Problem, Coordinates, Expansion, Kepler Laws
Scientific paper
Analytic expressions for the coordinates of the intermediate motion of two fixed centers are derived in the form of trigonometric series of linear functions of time. These expansions are required for expanding the perturbation function in solving the problem of the motion of a satellite about a planet. For sigma = 0 and epsilon = 0, the coefficients of these expansions are converted into the coefficients of the classical Keplerian motion.
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