Third- and fourth-order perturbations relative to the flattening of a planet in the orbit of a satellite

Details Third- and fourth-order perturbations relative to the flattening of a planet in the orbit of a satellite Third- and fourth-order perturbations relative to the flattening of a planet in the orbit of a satellite

Oct 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979sva....23..604e&link_type=abstract

(Astronomicheskii Zhurnal, vol. 56, Sept.-Oct. 1979, p. 1070-1076.) Soviet Astronomy, vol. 23, Sept.-Oct. 1979, p. 604-607. Tra

Mathematics

Computerized Simulation, Geopotential, Oblate Spheroids, Orbit Perturbation, Planetary Orbits, Satellite Orbits, Computer Programs, Eccentricity, Fixed Points (Mathematics), Fortran

Scientific paper

The intermediate orbit of a satellite is examined in the framework of the generalized problem of two fixed centers. The intermediate orbit takes into account the influence of second and third zonal harmonics in the expansion of planetary gravitational potential. A computer program is developed for calculating the intermediate orbit with any given accuracy relative to planetary oblateness. Accuracy up to fourth order relative to planetary oblateness is obtained.

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