Increased accuracy of computations in the main satellite problem through linearization methods

Astronomy and Astrophysics – Astronomy

Scientific paper

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Artificial Satellites, Linearization, Orbital Mechanics, Differential Equations, Orbital Elements, Perturbation Theory

Scientific paper

A set of canonical redundant variables is derived from Cartesian coordinates in a simplified form which allows the reduction of the Kepler problem to four harmonic oscillations with unit frequency. The coordinates are defined to be the direction cosines of the position of the particle along with the inverse of its distance. True anomaly is the new independent variable. The behavior of this transformation is studied when applied to the numerical integrations of the main problem in satellite theory. In particular, computation time and accuracy of orbits in these variables are compared with those in K-S and Cartesian variables. For high eccentricities the proposed variables require the least computation time for comparable accuracy regardless of the integration scheme.

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