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Satellite Based Augmentation Systems Brazilian Ionosphere Group Training at Stanford University October 27-30, 2003. MODULE 2: IONOSPHERE ESTIMATION USING GPS Part A: Measurements. This module covers:. Why?. Topics. IONOSPHERE ESTIMATION USING GPS, Part A.
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Satellite Based Augmentation SystemsBrazilian Ionosphere GroupTraining at Stanford UniversityOctober 27-30, 2003
MODULE 2: IONOSPHERE ESTIMATION USING GPS Part A: Measurements
This module covers: Why? Topics IONOSPHERE ESTIMATION USING GPS, Part A Using GPS signals to measure the ionosphere Understand purpose and operation of SBAS reference stations Understand how ionospheric corrections are formed Forming ionospheric measurements from GPS observables Data quality and editing Calibration of GPS data
Introduction • Currently the largest error sources in GPS positioning is that of ionospheric refraction causing signal propagation delays L What can be done? • If we have a dual-frequency GPS receiver, then the ionospheric effect can be almost totally accounted for J • What if we have a single-frequency receiver? • We can ignore the effect and live with the consequences M • We can minimize it using various processing techniques J • We can model it using empirical ionospheric models such as the GPS single-frequency Broadcast model, IRI2000 model, PIM, etc. J • We can measure it using nearby dual-frequency receiver observations (pseudorange only, carrier-phase only, pseudorange/carrier-phase combined) and apply it as a correction to the single-frequency observations. J • What is the error in positioning accuracy caused by the ionosphere and how can we reduce it?
IRI-95 profile Illustration for GPS and Ionosphere
GPS Observation Equations GPS pseudorange observation equation: GPS carrier phase observation equation: Range, clock, ambiguity, ionosphere, troposhere, satellite bias, receiver bias, multipath, noise
Generating GPS Ionospheric Observables phase-leveled ionospheric observable precise but ambiguous less precise but unambiguous
GPS Ionospheric Measurements Code measurement Phase measurement
Leveling the Phase Using Code Measurements The level is computed by averaging PI-LI using an elevation-dependent weighting. Higher elevation data is weighted more heavily. (The weighting is based on historical Turborogue PI-LI noise/ multipath data giving a historical PI-LI scatter of th(E) where E is elevation.) The level is computed as: where E is the elevation angle. The uncertainty on the level is computed in a rather rough way using a combination of th(E) and observed pseudorange scatter: The TEC sigma in the JPL Processed Data files are the level uncertainty.
Global Ionospheric Mapping: GIM For three shells, our model is For single shell, our model is where is the slant TEC; is the thin shell mapping function for shell 1, etc; is the horizontal basis function (C2, TRIN, etc); are the basis function coefficients solved for in the filter, indexed by horizontal (i) and vertical (1,2,3 for three shells) indices; are the satellite and receiver instrumental biases.
Example for Single Shell Model Results An Example of the Diurnal Variation of TEC for a Geomagnetically Quiet Day Components in TECU, TECU/hour, TECU/km
An Example for Repeatibility of Estimated Satellite Biases: Multi-Shell versus Single-Shell • Multi-shell significantly improves repeatibility in daily bias estimates • We compare bias averages over 7–10 days • Scatter (std. dev.) over a week improved by factor of 2 to 4 • Satellite biases • 7-day scatter improved from 2–6 cm to 8–24 mm • This may indicate reduction of systematic errors in bias estimation 6 cm 0 cm
An Example for Repeatibility in Estimated Receiver Biases:Multi-Shell versus Single-Shell 0.6 m • Receiver biases • 7-day scatter improved from 8–64 cm to 0.5–19 cm • Larger scatter due to stations in low latitude sector • Systematic error? • Examine long time-series of biases • Look for shifts in ionospheric delay level for all biases simultaneously 0 m
Comparison of Single and Multi-Shell Results for ENG1 Postfit Residuals ENG1 = English Turn, LA Improvement at low elevation angles Prediction Residuals
Comparison of Single and Multi-Shell Results for MBWW Postfit Residuals Improvement at low elevation angles MBWW = Medicine Bow, WY Prediction Residuals
What You Have Learned Ionosphere is the largest error source in GPS positioning Empirical models can be used to mitigate effects Dual-frequency GPS data can be used to solve for the ionospheric effect Error sources affecting GPS-based ionospheric estimation: arc length,leveling, biases, multipath, noise, etc. Global Ionospheric Mapping techniques: single vs multi-shell approaches: ionospheric delay and biases estimation Validation of maps, point plots, movies, etc.