Decrease in the magnitude of the correlation coefficients between orbit elements

Mathematics

Scientific paper

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Celestial Mechanics, Orbital Elements, Satellite Orbits, Cartesian Coordinates, Correlation, Matrices (Mathematics)

Scientific paper

An analytical technique for constructing the matrix of correlation coefficients (MCC) in the classical-elements approach to semidynamic problems in celestial mechanics is described and demonstrated, generalizing the results reported by Kabelac (1984). Elements designed to have a weighting-coefficient matrix as close as possible to the diagonal matrix are introduced, so that the MCC is as close as possible to the unit matrix. The elements are characterized mathematically; line-of-sight adjustment procedures are explained; and numerical results for three types of satellite orbits are presented in tables.

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