Influence of the residual accuracy measure on determination of EAS orbits.

Mathematics – Probability

Scientific paper

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Artificial Satellites: Orbits

Scientific paper

Currently, probabilistic and guaranteeing approaches are used to devise methods for determining orbits and choosing error distribution laws. The leading role is given to probability theory methods rather than to qualitative celestial mechanics methods. As a result, solutions that almost always differ from the true solutions are obtained, and secular error components inevitably arise in the precalculated satellite ephemerides. Moreover, secular components also arise due to theoretical methodical errors associated with the development of a mathematical formalism for the precise determination of orbits. In this paper, some aspects of determining the "bestfit" satellite orbits, free of secular error components in the precalculated satellite ephemerides, are considered.

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