Software Module for GNSS Navstar Radio Efemeris Processings

This paper represents the developed with MatLab algorithms for extracting radio ephemeris from the receiver to the global satellite navigation system NAVSTAR and handling in order to realize the possibility of calculating the reference orbits of navigation satellites. The results can be used to extrapolate the location of navigational satellites, determining the exact location in ECEF coordinate system to a point in time or to a period of time.

Language

  • English

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Filing Info

  • Accession Number: 01519171
  • Record Type: Publication
  • Files: TRIS
  • Created Date: Mar 21 2014 12:56PM