One form of the differential equations of motion for an artificial satellite of the moon

Details One form of the differential equations of motion for an artificial satellite of the moon One form of the differential equations of motion for an artificial satellite of the moon

Feb 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975sva....19..129k&link_type=abstract

(Astronomicheskii Zhurnal, vol. 52, no. 1, 1975, p. 207-209.) Soviet Astronomy, vol. 19, July-Aug. 1975, p. 129, 130. Translatio

Astronomy and Astrophysics

Astronomy

Differential Equations, Equations Of Motion, Lunar Satellites, Orbital Elements, Satellite Orbits, Lunar Gravitation, Orbit Calculation, Orbit Perturbation, Zonal Harmonics

Scientific paper

The differential equations describing the elements of the intermediate
orbit of a lunar satellite are derived. Contrary to a Keplerian orbit,
the intermediate orbit takes into account the disturbances from the
second and third zonal harmonics in the expansion of the lunar
attraction potential.

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