Contraction of high eccentricity satellite orbits using KS elements in an oblate atmosphere-Reference-Cited by-同舟云学术

Contraction of high eccentricity satellite orbits using KS elements in an oblate atmosphere

Published:1999-01 Issue:4 Volume:23 Page:693-698
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Sharma Ram Krishan

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference13 articles.

1. COSPAR International reference atmosphere;CIRA,1972

2. The contraction of satellite orbits under the influence of air drag. Part II. With oblate atmosphere;Cook,1961

3. The contraction of satellite orbits under the influence of air drag. Part III. High eccentricity orbits;King-Hele,1962

4. Kalil, F. Effect of an oblate rotating atmosphere on the eccentricity, semi-major axes and period of a close Earth satellite. The Martin Company, Baltimore 3, Maryland.

5. General perturbation theory;Kampos;NASA CR - 1008,1968

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1. Extension of the King-Hele orbit contraction method for accurate, semi-analytical propagation of non-circular orbits;Advances in Space Research;2019-07

2. Decay of high eccentricity satellite orbits with air drag using uniformly regular KS canonical elements;Acta Astronautica;2011-06

3. Decay of Satellite Orbits Due to the Drag of Rotating Oblate Atmosphere with Scale Height Dependent on Altitude;Arabian Journal for Science and Engineering;2011-02-03

4. Analytical approach using KS elements to high eccentricity orbit predictions including drag;Acta Astronautica;2010-03

5. Fourth-order theories for orbit predictions for low- and high-eccentricity orbits in an oblate atmosphere with scale height dependent on altitude;Acta Astronautica;2009-11