Drag perturbations in artificial satellite orbital motion based on the Total Density model

Details Drag perturbations in artificial satellite orbital motion based on the Total Density model Drag perturbations in artificial satellite orbital motion based on the Total Density model

Feb 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991an....312..127m&link_type=abstract

Astronomische Nachrichten (ISSN 0004-6337), vol. 312, no. 2, 1991, p. 127-132.

Astronomy and Astrophysics

Astronomy

4

Artificial Satellites, Atmospheric Density, Satellite Drag, Satellite Orbits, Satellite Perturbation, Atmospheric Models, Circular Orbits, Thermosphere

Scientific paper

Analytical expressions for the aerodynamic drag perturbations undergone by five independent orbital elements of an artificial satellite moving in an orbit with small eccentricity, over a nodal period, are established. All three components of the perturbing acceleration are taken into account. The TD model is used to describe the density distribution of the upper atmosphere.

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