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Estimating The GNSS Broadcast Ephemeris Error - Presentation by Sebastian Ciuban is a document available to read on EtoBox.

The orbit of GNSS SV 12 was computed using: broadcast ephemerides data contained in the RINEX navigation file. Precise post-processed orbits were Used to obtain the orbit of the satellite. The results show that the errors between them are small enough for obtaining the right solution for navigation and positioning problems.

Author
Sebastian Ciuban
Language
EN