Perturbed motion of a satellite in the atmosphere based on the total density model

Details Perturbed motion of a satellite in the atmosphere based on the total density model Perturbed motion of a satellite in the atmosphere based on the total density model

Oct 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991baicz..42..298m&link_type=abstract

Astronomical Institutes of Czechoslovakia, Bulletin (ISSN 0004-6248), vol. 42, no. 5, Oct. 1991, p. 298-304.

Astronomy and Astrophysics

Astronomy

2

Artificial Satellites, Astrodynamics, Satellite Drag, Satellite Perturbation, Atmospheric Models, Density Distribution, Equations Of Motion, Orbital Elements, Thermosphere

Scientific paper

Analytical expressions have been derived for the variations of the five orbital parameters, caused by aerodynamic drag over a nodal period of the satellite. The total density thermospheric model was used to study artificial satellite dynamics into the terrestrial atmosphere. The variations of the orbital elements are obtained in a very concentrated form. All three components of the perturbing acceleration as well as the rotation of the atmosphere have been taken into account.

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