GEOMETRIC FACTOR AND ITS INFLUENCE ON NAVIGATION PARAMETERS DETERMINING ERROR IN PSEUDOSATELLITE RADIO SYSTEM

Authors

  • O. V. Shulga
  • O. V. Shefer

Keywords:

geometric factor, pseudosatellite, consumer pseudorange, honeycomb structure, elevation angle, unit cell, line of sight, geodesic distance

Abstract

TIt is proved that the relation between errors definition of primary and secondary navigation parameters depends on the type of matrix consumer gradients (C), that is, the geometry of the mutual position of pseudosatellites (PS) and the consumer C. The analysis showed that in the general expression for the geometrical factor (MS) can be written as the ratio of GDOR = = σq/σD, where σq – mean square error (MSE) of the consumer C state vector definition; σD – MSE to determine pseudorange to PS. It is determined that the practice of consumers interested in the degree of deterioration in the accuracy of positioning separate horizontal and vertical planes relative to the Earth's surface, as well as the degree of time corrections determining accuracy deterioration.

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References

Шебшаевич B.C. Введение в теорию космической навигации / В.С. Шебшаевич. – М: Сов. радио, 1971. – 296 с.

Соловьев Ю.А. Системы спутниковой навигации / Ю.А. Соловьев. – М: Эко-трендз, 2000. – 270 с.

Глобальная спутниковая радионавигационная система ГЛОНАСС / Под ред. В.Н.Харисова, А.И.Перова, В.А.Болдина. – М: ИПРЖР, 1999. – 560 с.

Published

2017-12-30

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