Calculation of satellite orbits for purposes of geodynamical research

Details Calculation of satellite orbits for purposes of geodynamical research Calculation of satellite orbits for purposes of geodynamical research

Feb 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985kfnt....1...55t&link_type=abstract

Kinematika i Fizika Nebesnykh Tel (ISSN 0233-7665), vol. 1, Jan.-Feb. 1985, p. 55-60. In Russian.

Physics

Geodynamics, Numerical Integration, Orbit Calculation, Satellite Orbits, Algorithms, Assembly Language, Cartesian Coordinates, Differential Equations, Equations Of Motion, Error Analysis, Integral Equations, Trajectory Analysis

Scientific paper

It is shown that the calculation of satellite orbits for the determination of geodynamical parameters can be carried out efficiently through the use of current numerical-integration algorithms combined with regularized equations of satellite motion (KS theory). It is demonstrated that Lageos observations can be analyzed using the direct integration of equations in rectangular coordinates by the Adams algorithm of variable order (based on divided differences, for example).

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