Notes
Slide Show
Outline
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Summary of GPS Errors

  •      Typical Error  [m]           Standard GPS          Differential GPS
  •           (per satellites)


  • Satellite Clocks 1.5             0
  • Orbit Errors 2.5             0
  • Ionosphere 5.0             0.4
  • Troposphere 0.5             0.2
  • Receiver Noise 0.3             0.3
  • Multipath 0.6             0.6


  •   The ionosphere is the largest source of error for Standard GPS and second largest for Differential GPS.


  • http://www.trimble.com/gps/howgps-error2.shtml#3
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Electron\Ion Density Profile
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Regional Composition Changes and Ion Density
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Ionospheric Corrections
  • Need to model the ionosphere to compute corrections
  • Empirical climatological models:  Klobuchar coefficients
  • Physics based numerical models: CTIPe, TIE-GCM
  • Data assimilation schemes: US-TEC, GAIM


  •  Models can provide both specification and forecast


  • The ionosphere is highly variable in space and time
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New Products
  • Gradient Detection



  • OPUS Ionospheric Correction Function
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Background/Rationale
  • NGS was running US-TEC in 3-day latent mode
  • As the space weather agency, SWPC to provide ionospheric correctors
  • Avoid the need to continue to update ionospheric activities at NGS every time SWPC makes an improvement to services
  • SWPC is the natural place for providing the service of characterizing the ionosphere
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Proposal
  • SWPC to provide a web-based customer application for providing ionospheric correctors from a user specified list of options
  • User submits a RINEX file over a particular interval
  • SWPC either uses “best-available” model to evaluate correctors or user specified model (e.g. US-TEC, GAIM, IRI, rtIRI, ….)
  • Return RINEX file to user with correctors inserted
  • Next version of RINEX format has place for corrector



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Ionosphere Correction
 for NGS
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USTEC Product
  • Current NOAA capability for characterizing the total number of free electrons (TEC) in the ionosphere, with parallel input data streams for reliability
  • Since 2004, a product characterizing the ionospheric TEC over the continental US (CONUS) has been running in real-time at NOAA’s Space Environment Center (SEC)
  • The ionospheric data assimilation model uses a Kalman filter and ingests ground-based GPS data to produce 2-D maps of total electron content over the CONUS
  • Product evolved from a collaboration between SEC and NOAA’s National Geodetic Survey (NGS), National Geophysical Data Center (NGDC), and Forecast Systems Laboratory (FSL)
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Slant-Path TEC Maps
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 Validation Summary
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SWPC Ionosphere Goals
  •  Improve USTEC
  •   CONUS: Specification
  •      US-TEC slant path total electron content uncertainty < 2 TECU
  •      US-TEC vertical electron content uncertainty < 1 TECU


  •   CONUS: Forecast
  •       1 hour forecast as good as specification
  •       3 hour forecast: uncertainty < 3 TEC units
  •       6-12 hour forecasts


  •   GPS User Tools
  •        Color coded regional maps of ionosphere disturbance
  •        Support vendors to produce color coded maps for specific applications


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Conclusions



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