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NASA NTRS · 20210001392

Ionospheric specification algorithms for precise GPS-based aircraft navigation

Abstract

We present a technique for converting real-time total electron content (TEC) measurements into gridded vertical delay corrections at the GPS L***sub***1 frequency, which will be broadcast to users every 5 min via geosynchronous satellite. Users will convert these delays to slant corrections for their own particular lines of sight to GPS satellites. To preserve user safety, estimates of the error in the user delay corrections will also be broadcast.

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BibTeXRIS

Wilson, B., Pi, X., Muna, D., Lindqwister, U., Iijima, B., Mannucci, A., Harris, I.. 2000-03-01. Ionospheric specification algorithms for precise GPS-based aircraft navigation. https://ntrs.nasa.gov/citations/20210001392

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