Taking precession and nutation into account in the equations of the motion of an artificial earth satellite

Details Taking precession and nutation into account in the equations of the motion of an artificial earth satellite Taking precession and nutation into account in the equations of the motion of an artificial earth satellite

Aug 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kfnt....5...20t&link_type=abstract

Kinematika i Fizika Nebesnykh Tel (ISSN 0233-7665), vol. 5, July-Aug. 1989, p. 20-26. In Russian.

Physics

Earth Orbits, Equations Of Motion, Nutation, Precession, Spacecraft Motion, Differential Equations, Error Correcting Devices

Scientific paper

Accurate differential corrections for precession and nutation to
satellite orbital motion in a quasi-inertial coordinate system are
derived. The derived formulas retain their validity in the case of zero
eccentricity and/or zero inclination.

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