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Ionospheric specification algorithms for precise GPS-based aircraft navigationWe 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.
Document ID
20210001392
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Wilson, B.
Pi, X.
Muna, D.
Lindqwister, U.
Iijima, B.
Mannucci, A.
Harris, I.
Date Acquired
March 1, 2000
Publication Date
March 1, 2000
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Global
Positioning
System
aircraft
ionosphere
wave
propagation
algorithms
broadcasting

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