An intermediate orbit of a planetary satellite

Details An intermediate orbit of a planetary satellite An intermediate orbit of a planetary satellite

Jun 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989azh....66..622a&link_type=abstract

Astronomicheskii Zhurnal (ISSN 0004-6299), vol. 66, May-June 1989, p. 622-630. In Russian.

Statistics

Computation

4

Computational Astrophysics, Natural Satellites, Orbital Mechanics, Planetary Orbits, Gravitational Effects, Liapunov Functions, Orbit Calculation

Scientific paper

A method for constructing the intermediate orbit of a planetary satellite is presented. It is based on the theory of Liapunov's periodic solutions. The intermediate orbit includes all of the inequalities in the satellite's motion caused by the second zonal harmonic of the planetary attraction potential. It can be used for the formulation of the analytical theory of planetary satellite motion, at least in those cases when the inclinations of their orbits to the equatorial plane are small.

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