Secular variations of satellite motion associated with diurnal distributions of atmospheric density

Details Secular variations of satellite motion associated with diurnal distributions of atmospheric density Secular variations of satellite motion associated with diurnal distributions of atmospheric density

Jul 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17..488n&link_type=abstract

Kosmicheskie Issledovaniia, vol. 17, July-Aug. 1979, p. 488-497. In Russian.

Physics

1

Atmospheric Density, Orbit Perturbation, Satellite Orbits, Differential Equations, Orbital Mechanics, Secular Variations

Scientific paper

Analytical expressions are obtained for the motion of an earth satellite caused by diurnal variations of atmospheric density (the so-called diurnal effect). The intermediate orbit of the satellite is represented in the form of a solution to the generalized problem of two fixed centers. Formulas are derived for orbit-element perturbation which are valid for all values of the intermediate parameter e less than 1.

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