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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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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