Contraction of satellite orbits using KS uniformly regular canonical elements in an oblate diurnally varying atmosphere

Author:

Xavier James Raj M.,Sharma R.K.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference18 articles.

1. The advance of the perigee of a satellite in a rotating oblate atmosphere with a diurnal variation on density;Boulton;Proc. R. Soc. London A,1983

2. Near-circular orbits within a rotating oblate atmosphere with a diurnal variation in density and variable density scale height;Brookes;Proc. R. Soc. London A,1992

3. The contraction of satellite orbits under the influence of air drag II With oblate atmosphere;Cook;Proc. R. Soc. London A,1961

4. Fominov, A.M., 1976. A new atmospheric model and Earth satellite motion. NASA TTF-17108.

5. Jacchia, L.G., 1977. Thermospheric temperature, density and composition: new models. Smithsonian Astrophysics Observatory Special Report, no. 375.

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