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OVERVIEW OF IGS PRODUCTS & ANALYSIS CENTER MODELING

OVERVIEW OF IGS PRODUCTS & ANALYSIS CENTER MODELING. Status of core products focus on Ultra-rapid predicted orbits issues with current products Comparisons of AC analysis strategies evidence for systematic errors, esp. fortnightly harmonics Recommendations. Jim Ray, NOAA/NGS

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OVERVIEW OF IGS PRODUCTS & ANALYSIS CENTER MODELING

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  1. OVERVIEW OF IGS PRODUCTS & ANALYSIS CENTER MODELING • Status of core products • focus on Ultra-rapid predicted orbits • issues with current products • Comparisons of AC analysis strategies • evidence for systematic errors, esp. fortnightly harmonics • Recommendations Jim Ray, NOAA/NGS Jake Griffiths, NOAA/NGS IGS 2008 Workshop, Miami Beach, 2 June 2008

  2. * indicates AC contributions that are weaker than others

  3. Predicted IGU Orbit WRMS IGU Orbits (1st 6 hr of predictions) wrt IGR Orbits • WRMS of IGU orbit predictions have improved to <5 cm RMS • PRN29 (IIA) decommissioned • GOP solutions improved

  4. Scale & Rotations of Predicted IGU Orbits IGU Orbits (24 h of predictions) wrt IGR Orbits (shifted) • Z rotations (UT1 prediction error) reach 1 mas level • equivalent to equatorial shift of 12.9 cm at GPS altitude (shifted)

  5. Issues with Current Products • IGU orbit combination only marginally robust • sometimes AC predictions are better than combo Ultra-Rapid IGS Orbit Comparison for 1478_6_06 (10 May 2008 06h) CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS MEDI | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] [mm] --------+-------------------------------------------------------- cou 73| 11 -1 -4 536 -389 254 -.29 64 34 33 emu 49| 7 0 0 486 38 -60 .03 84 44 21 esu 95| 4 5 -2 -396 687 -72 .13 77 77 29 gfu 65| 1 -2 -2 302 -21 127 -.34 77 78 29 gou 82| -5 -4 -1 260 334 48 -.35 89 78 31 siu 62| 0 17 -33 -221 1068 730 .02 130 131 71 usu 33| 19 9 0 297 -394 -20 .14 123 111 56 igu n/a| 5 0 -5 283 103 45 -.08 74 79 18 • would benefit from more high-quality ACs • accuracy now limited by ERP predictions, mostly • may also apply to IGR orbits (but less severe) • IGU combined clocks are very poor • clock predictions no better than BRDC • not enough clock ACs • even IGR clocks sometimes weak when some ACs miss

  6. effect of 15-deg cutoff

  7. Aliased Tidal Peaks in PM Discontinuities • Spectra of polar motion day-boundary discontinuities show signatures of aliased O1, Q1, & N2 tides + unknown 7.2 d line

  8. VLBI (1-hr) UT1 residuals white over full frequency range Kalman Filter of VLBI UT1 + GPS LOD(Senior, Kouba, Ray – EGU 2008) • GPS LOD residuals • approximately white • with small peak at 13.7 d • possible difference in a priori tidal models wrt VLBI EMR analysis upgrade • Gauss-Markov values for GPS LOD biases • peak-to-peak range = ± 40 μs • RMS = 9 μs • 14.19-d periodic • treated as GPS artifact • amplitude varies between 5 & 11 μs • phase varies linearly w/ time due to changing period

  9. Fortnightly Band – Spurious IGS LOD(Senior, Kouba, Ray – EGU 2008) LODS – (AAM+OAM) spectra 14.12 d signal in IGS & C04 probably due to mix of GPS errors

  10. Day-boundary Orbit Discontinuities • Orbit discontinuities between days show temporally correlated errors & broad fortnightly spectral peak • From Griffiths & Ray (AGU 2007)

  11. Conclusions • Despite huge progress by IGS since 1994, numerous small systematic errors remain in products • see EGU 2008 presentation by J. Ray http://www.ngs.noaa.gov/IGSWorkshop2008/docs/igs-errs_egu08.pdf • Applications to cutting-edge science are currently limited • need to focus on identifying, understanding, & mitigating errors • should avoid rush to premature science conclusions • must renew basic GNSS research efforts, not just in geophysical applications • requires accurate knowledge of AC processing strategies • Improvements will probably require better station installations (to reduce near-field multipath biases) & analysis upgrades • more research into field configuration effects badly needed • need better leadership to popularize lessons learned • need better cooperation & coordination between analysts & network

  12. Recommendations • For more robust products: • recruit new or improved IGU ACs & more IGR clock ACs • investigate improved near-RT & predicted ERPs • should IGS start (UT1 + LOD) service ? (à la Senior et al., EGU08) • Reject GGOS UAW actions for: • SINEX parameter & naming extensions • piecewise, continuous segment parameterization as SINEX standard • Reject rigidly standardized AC procedures & parameterizations • would lead to stagnation & end of progress • would eliminate basis for multi-solution product combinations • but ACs must agree on conventional choices & use of modern models • Instead, set up inter-service SINEX & combinations WG • investigate technique-specific systematic errors • maintain SINEX format

  13. Recommendations (cont’d) • Updated AC summaries are required: • EMR 23 Jan 2002 • GFZ 27 Feb 2003 • JPL 13 Apr 2004 • SIO 31 Oct 2005 • (USNO 12 Sep 2006) • Suggest suspending ACs with no updates by 30 Sep 2008 • if processing summary is older than 2 years • submissions would be rejected from IGS products after Sep 2008 • Rescind AC status if no updates by 31 Dec 2008 • would need to formally rejoin IGS ACs after Dec 2008 • Or ask above ACs for effective alternative proposal

  14. Backup Slides 1

  15. A SURVEY OF SOME SYSTEMATIC ERRORS IN IGS PRODUCTS • Clock jumps at day boundaries & near-field multipath • Position time series show N * 1.04 cpy harmonics • N/S distortions in IGS frames • Earth rotation parameters smoothed & filtered • Spurious tidal lines in EOPs • Orbit discontinuities have fortnightly variations Jim Ray, NOAA/National Geodetic Survey EGU 2008 General Assembly, Paper G4 #A-01694, Vienna, 15 April 2008

  16. Context • GPS errors are propagated formally but true data noise is unknown • highly site-dependent & not white noise • e.g., variances of AC frame solutions differ by > x 100 • dealt with by empirical rescaling of covariance matrix • Evidence for systematic effects in IGS product covariances is well known • e.g., user velocity errors are routinely inflated to account for temporal correlation of position errors • but methods are purely empirical • Objective: Survey systematic errors in some IGS product values • underlying causes mostly unknown or not confirmed

  17. 1) Day-boundary Clock Jumps • clock bias accuracy is based on mean of code data per arc • for 24-hr arc with code σ = 1 m, clock accuracy should be ~120 ps • can study local code biases via clock jumps at day boundaries (H-maser stations only) • observed clock jumps vary hugely among stations: 110 ps to >1500 ps • presumably caused mainly by local code multipath conditions, esp. in near-field of antenna

  18. expect largest & longest-period MP errors when height H of antenna is small [Elósegui et al., 1995] • may have special problems when H is near multiples of λ/4 • reflected RCP GPS signals enter from behind as LCP • choke-ring design esp sensitive to L2 reflections from below [Byun et al. 2002] • most IGS RF antennas mounted over flat surfaces! Near-field Multipath Mechanism

  19. Correlated Clock & Position Effects: ALGO • ALGO day-boundary clock jumps increase in winters • every winter ALGO also has large position anomalies • IGS deletes outliers >5 σ • implies common near-field multipath effect is likely (phase & code)

  20. Probably better to mount antennas away from closereflecting surfaces!worse better

  21. Other Hardware Choices Also Important PIE1 AOA D/M_T antenna ASH701945E_M antenna + new cables • receiver health, firmware, antenna model, & cables also affect day-boundary clock jumps AOA firmware 3.2.32.8 3.2.32.11 Ashtech UZ-12 receiver Rogue SNR-8000 receiver Ashtech UZ-12 receiver

  22. 2) Stacked/Smoothed Spectra of Site Residuals (shifted) • for 167 IGS sites with >200 weekly points in 1996.0 – 2006.0 • large annual + semi-annual variations • plus harmonics in all components at N * (1.040 ± 0.008) cpy • flicker noise spectra down to periods of ~few months (shifted)

  23. Position Harmonics Linked to GPS Year • 1.040 ± 0.008 cpy fundamental does not match any expected alias or geophysical frequency • also not seen in VLBI, SLR, or fluid load spectra • Closely matches GPS “draconitic” year • rotation period of Sun w.r.t. GPS nodes (viewed from Earth) • GPS nodal drift is -14.16° per year (due to Earth’s oblateness) • period = 351.4 day or frequency = 1.039 cpy • Two possible coupling mechanisms suggested: 1) direct orbit modeling errors (e.g., related to eclipse periods & planes) 2) alias of site position biases (e.g., near-field phase multipath) due to beating of 24-hr processing arc against 23.93-hr GPS repeat period • useful distinguishing tests not yet made

  24. 3) N/S Distortions of IGS Frames N E U • Weekly mean biases of IGS frames compared to long-term frame

  25. IGS Frame Distortions • N/S mean component of IGS weekly frames shows largest annual variation • after weekly 7-parameter Helmert alignment • also largest dispersion among ACs in N/S direction • Not likely to be caused by annual inter-hemisphere fluid load cycle • load signal should be largest in heights, not N/S • Could possibly be related to along-track GPS orbit errors • but no mechanism identified • Likelier explanation: possible neglected 2nd order ionospheric effect

  26. 4) High-frequency Smoothing of EOPs • Day-boundary continuity constraint by some ACs smoothes & filters EOP estimates near Nyquist limit

  27. Filter/Smoother by Continuity Constraints • Some ACs estimate EOPs (& others) by continuous linear segments • attenuates power by factor 4 at Nyquist limit • smoothes estimates • filters certain phase components • To avoid contaminating IGS combination, such EOP solutions rejected since January 2008 (wk 1460) • but effects on other parameters probably still present • Past high-frequency studies should be reconsidered • Can use GFZ polar motion to estimate background, non-tidal, sub-daily variance: 13.6 to 20.7 μas2

  28. 5) Aliased Tidal Peaks in EOP Discontinuities • Spectra of polar motion day-boundary discontinuities show signatures of aliased O1, Q1, & N2 tides + unknown 7.2 d line

  29. 6) Day-boundary Orbit Discontinuities • Orbit discontinuities between days show temporally correlated errors & broad fortnightly spectral peak

  30. Conclusions • Despite huge progress by IGS since 1994, numerous small systematic errors remain in products • Applications to cutting-edge science must recognize limitations • need to focus on identifying, understanding, & mitigating errors • must renew basic GNSS research efforts, not just in geophysical applications • should avoid rush to premature science conclusions • Improvements will probably require better station installations (to reduce near-field multipath) & analysis upgrades • more research into field configuration effects badly needed • need better leadership to popularize lessons learned • need better cooperation & coordination between analysts & network

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