Oblateneess and drag effects on the motion of satellites in the set of Eulerian redundant parameters

Details Oblateneess and drag effects on the motion of satellites in the set of Eulerian redundant parameters Oblateneess and drag effects on the motion of satellites in the set of Eulerian redundant parameters

Aug 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993em%26p...62..161a&link_type=abstract

Earth, Moon, and Planets, Volume 62, Issue 2, pp.161-177

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Scientific paper

In this paper, the perturbed motion of the artificial satellites under the effects of the earth's oblateness and atmospheric drag will be established. These equations will be expressed in terms of the Eulerian redundant parameters. Applications of the method for the perturbed motion are illustrated by numerical examples for some test cases of the orbits.

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