Orbit computations with the Eulerian topological regular elements with oblateness

Details Orbit computations with the Eulerian topological regular elements with oblateness Orbit computations with the Eulerian topological regular elements with oblateness

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992ap%26ss.193..109s&link_type=abstract

Astrophysics and Space Science (ISSN 0004-640X), vol. 193, no. 1, July 1992, p. 109-122.

Astronomy and Astrophysics

Astrophysics

Equations Of Motion, Oblate Spheroids, Orbit Calculation, Satellite Orbits, Two Body Problem, Gravitational Effects, Numerical Integration, Orbital Elements, Topology

Scientific paper

In this paper, the Eulerian set of topological regular elements was utilized to develop an orbit computation package for the initial value problem for any conic motion of artificial satellites in the earth's gravitational field with axial symmetry. Applications for the two types of short- and long-term predictions are considered. The numerical results proved the high efficiency and flexibility of the package.

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