A Computational Method of the Combined Perturbations for the Orbit of the Close Orbit Terrestrial Satellite

Details A Computational Method of the Combined Perturbations for the Orbit of the Close Orbit Terrestrial Satellite A Computational Method of the Combined Perturbations for the Orbit of the Close Orbit Terrestrial Satellite

Dec 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983acasn..24..137x&link_type=abstract

Acta Astronomica Sinica, Vol.24:2, P. 136, 1983

Statistics

Computation

Scientific paper

This paper proposes a computational method for the combined perturbations for the orbit of a close-orbit terrestrial satellite, and gives the computational formulae if the perturbations due to the earth's figure and air drag are of the same order of magnitude O(10-3). These formulae are evaluated for a close-orbit terrestrial satellite whose perigeon height z0 and orbital eccentricity e should satisfy the conditions: 160 km ≤ z0 ≤ 250 km and 0 ≤ e ≤ 0.01, respectively.

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