Radial, transverse and normal satellite position perturbations due to the geopotential

Details Radial, transverse and normal satellite position perturbations due to the geopotential Radial, transverse and normal satellite position perturbations due to the geopotential

Sep 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987cemec..40..409r&link_type=abstract

Celestial Mechanics (ISSN 0008-8714), vol. 40, no. 3-4, 1987, p. 409-421.

Computer Science

29

Geopotential, Orbit Perturbation, Position (Location), Satellite Orbits, Bessel Functions, Kepler Laws, Orbital Elements

Scientific paper

Perturbations in the position of a satellite due to the earth's gravitational effects are presented. The perturbations are given in the radial, transverse (or along-track) and normal (or cross-track) components. The solution is obtained by projecting the Kepler element perturbations obtained by Kaula (1966) into each of the three components. The resulting perturbations are presented in a form analogous to the form of Kaula's solution which facilitates implementation and interpretation.

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