The third order solution of orbital perturbation of artificial earth's satellite

Details The third order solution of orbital perturbation of artificial earth's satellite The third order solution of orbital perturbation of artificial earth's satellite

Jun 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981scisn..24..813l&link_type=abstract

Scientia Sinica, vol. 24, June 1981, p. 813-828.

Statistics

Computation

Artificial Satellites, Astrodynamics, Elliptical Orbits, Perturbation Theory, Satellite Perturbation, Eccentric Orbits, Natural Satellites, Oblate Spheroids, Orbit Calculation, Tesseral Harmonics

Scientific paper

A third order solution of the orbital perturbation of artificial earth satellites is presented, which is closed for eccentricity, making use of the intermediate orbit and the elliptic orbit perturbation theory, in addition to various methods for the computation of fast and slow variables. Vinti's (1961) method is generalized, and the corresponding accurate solution of the intermediate orbit is given. The method may be applied to the motion of natural satellites in the solar system for cases when the primary body is an oblate planet with revolutionary symmetry.

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