Accuracy of formulas for the intermediate orbit of a satellite

Details Accuracy of formulas for the intermediate orbit of a satellite Accuracy of formulas for the intermediate orbit of a satellite

Apr 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990azh....67..400e&link_type=abstract

Astronomicheskii Zhurnal (ISSN 0004-6299), vol. 67, Mar.-Apr. 1990, p. 400-408. In Russian.

Astronomy and Astrophysics

Astronomy

2

Astrodynamics, Orbit Calculation, Satellite Orbits, Accuracy, Equations Of Motion, Numerical Integration, Planetary Orbits

Scientific paper

The accuracy of intermediate-orbit formulas based on the solution of the generalized problem of two fixed centers is analyzed. Results obtained using this approach are compared with numerical-integration results for long periods of time. For an artificial earth satellite over a time period of 150 days, the accuracy of the formulas is not worse than 2.2 cm. For Phobos, the acccuracy is 0.3 cm for a time period of 360 days.

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