1
IG2 5-min Clocks (AC solutions compared to combined) 6. ORBIT DAY-BOUNDARY DISCONTINUITIES 2016 AGU FALL MEETING DECEMBER 12-16, 2016 SAN FRANCISCO, CA Combined orbits and clocks from the IGS 2 nd reprocessing Jake Griffiths Naval Center for Space Technology U.S. Naval Research Laboratory, Washington, DC, USA [email protected] 1. OVERVIEW In early 2015, the Analysis Centers (ACs) of the International GNSS Service (IGS) completed their second reanalysis of the full history of globally distributed GPS and GLONASS data collected since 1994. The suite of reprocessed AC solutions includes daily product files containing station positions, Earth rotation parameters, satellite orbits and clocks. This second reprocessing—or repro2—provided the IGS contribution to ITRF2014; it follows the successful first reprocessing, which provided the IGS input for ITRF2008. For this poster, we will discuss the newly combined repro2 GPS orbits and clocks. We also revisit our previous analysis of orbit day- boundary discontinuities with several significant changes and improvements. (1) Orbit discontinuities for the contributing ACs were studied in addition to those for the IGS repro2 combined orbits. (2) Apart from homogeneous reprocessing with updated analysis models, the main difference compared to the IGS Final operational products is that NOAA/NGS inputs were not submitted for the IGS reprocessing, yet they contribute heavily in the operational orbits in recent years. Also, during spring 2016, the ESA modified their orbit model so that it is no longer consistent with the one used for reprocessing. (3) A much longer span of orbits was available now, up to 11.2 years for some individual satellites, which allows a far better resolution of spectral features. (4) The procedure to compute orbit discontinuities has been further refined to account for extrapolation edge effects, improved geopotential fields, and to allow for spectral analysis of a longer time series of jumps. The satellite position time series used are complete enough that linear interpolation is necessary for only sparse gaps. So the key results are based on standard FFT power spectra (stacked over the available constellation and lightly smoothed). However, we computed Lomb-Scargle periodgrams to provide higher frequency resolution of some spectral peaks and to permit tests of the effect of excluding eclipse periods. From this test, we found that the effect of eclipses is negligible; we do not discuss the matter further in this poster. 2. AC CONTRIBUTIONS O 7 Operational Centers - COD, ESA, GFZ (GF2), GRG, JPL, MIT O 2 TIGA Centers for densifying ITRF2014 with GNSS stations at tide-gauges - GFZ (GT2), ULR LEGEND slash: snx, sp3, erp [brdc clk in sp3] dots: snx, sp3, clk (5m), erp solid: snx, sp3, clk (30s), erp hachure: operational products ACKNOWLEDGEMENTS: Support for this work was provided by the NASA ROSES-2016 program under NRA #: NNH16AC75I. Thanks to Kevin Choi for helping to verify IGS software performance on NRL computers. 7. PPP: IG2 ORBIT+CLOCK PERFORMANCE Jim Ray Retired National Geodetic Survey, Silver Spring, MD, USA 3. ORBIT COMBINATION STATISTICS 5. ORBITAL FRAME Rotations Translations Scale - X - - Y - - Z - Model changes in IGS Finals operations O AC orbit scale drifts - EM2, JP2 similar scale used by GIPSY - ES2 similar to IG1/IGF (Wks 1050-1550) Scale change of ~0.55 ppb is smaller than the expected ~0.72 ppb O Earth albedo modeling by all ACs O Antenna thrust not modeled by ESA O Large annual motion in GR2 Tz offsets O Other ACs show smaller ~annual Tz motions but with various phases - Up to +9/-5 mm offsets Combination approach same as official IGS Finals a priori AC weighting: O UL2 -> comparison only (all; not shown) O MI2 -> comparison only (0730 thru 1250) O GR2 -> comparison only (all) O GT2 -> comparison only (0730 thru 1720) Other products for comparison only: O IG1 = IGS 1 st reprocessing O IGF = IGS Finals operational solution O Large offsets in early years: CF2, ES2, GT2 O Periods of spurious rotations for GF2 O Large offsets for IG1 and IGF until Wk 1702 (switch to daily products & combo s/w bug fix) Combination approach same as official IGS Finals a priori AC weighting: O UL2 -> comparison only (all; not shown) O MI2, GR2, GT2 -> comparison only (all) Other products for comparison only: O IG1 = IGS 1 st reprocessing O IGF = IGS Finals operational solution 4. CLOCK COMBINATION STATISTICS IGF & IG2 most similar O ops AC products used O remaining difference from missing NGS in repro2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 o IG1 o IGF ²IG2 Avg. Scale O IGF/IG1: -0.15 (± 0.21) ppb O IG2: -0.04 (± 0.63) ppb Avg. Rx O IGF/IG1: -15.6 (± 42.6) μas O IG2: 0.5 (± 114.8) μas Avg. Ry O IGF/IG1: -1.1 (± 48.8) μas O IG2: -1.4 (± 94.0) μas Avg. Rz O IGF/IG1: -66.5 (± 73.0) μas O IG2: -35.5 (± 195.1) μas Avg. Tx O IGF/IG1: 0.91 (± 1.36) mm O IG2: 0.25 (± 4.77) mm Avg. Ty O IGF/IG1: 0.23 (± 1.40) mm O IG2: 0.52 (± 4.48) mm Avg. Tz O IGF/IG1: 4.51 (± 2.54) mm O IG2: 0.10 (± 3.37) mm Power spectra for ~11.22 years (2003.90 – 2015.12) of IG2 orbit day-boundary discontinuities Annual, semi-annual, and harmonics of GPS draconitic year (351.6d), up to at least 10 th 9-peak comb near 14d: O sub-daily EOP tide alias (M2,O1,Oo1) errors and Mf/ Mf’ direct tide errors present possibly frequency shifted due to draconitic orbital frame rotation O other spectral peaks in 14d band, in particular, in cross- track, are unexplained (see details in tables to right) Approach Compared to IG1/IGF, the IG2 orbits+clocks deliver long- term global coordinate sets that are noisier and also slightly more biased, perhaps due to AC repro2 satellite clock issues prior to 2004.5. Exploring mitigating steps. For IGS14, the IGS may apply satellite clock corrections consistent with igs08.atx -> igs14.atx APV Z-PCO changes. This may offer potential for PPP users to access IGS14 using IG2 products. Still under evaluation. WRMS agreement between IG2 & IG1/IGF orbits at the 5 mm level for most of repro2 span; early years range from 50 mm to 10 mm WRMS agreement. in terrestrial frame in orbit frame Expected Peak f (cpd) P (d) f (cpd) P (d) pro/retro M2 24-hr alias 0.067727 14.765 0.064882 15.412 P 0.070571 14.170 R O1 24-hr alias 0.070464 14.192 0.067620 14.788 P Mf tide 0.073203 13.661 0.070359 14.213 P 0.076047 13.150 R Mf' tide 0.073349 13.633 0.070505 14.183 P 0.076193 13.125 R Oo1 24-hr alias 0.075940 13.168 0.073096 13.681 P 0.078784 12.693 R Weekly means of the daily AC clock RMS values from the repro2 5-min clock combination. The shift in RMS for IGF at the time of IGS05 -> IGS08 switch also corresponds to frame origin (Tz) and rotation (Rz) offset (see PPP analysis in Panel 7). in orbit frame Observed peak f (cpd) P (d) attributed source (see Table 2) 1 (ACR) 0.061994 16.131 ??? 2 (ACR) 0.064860 15.418 M2 alias P (shown at left) 3 (C) 0.067713 14.768 O1 alias P (shown at left) 4 (ACR) 0.070512 14.181 Mf' tide P (shown at left) + M2 alias R 5 (CR) 0.073364 13.631 ??? Oo1 alias ??? (shown at left) 6 (C) 0.076225 13.119 ??? Mf’ tide R ??? 7 (C) 0.079070 12.647 ??? 8 (C) 0.081898 12.210 ??? 9 (C) 0.084727 11.803 ??? Table 1. Details for 14d band. Robust number of contributing ACs to form combined orbit products. Reduced redundancy amongst clock contributing ACs compared to IGS Finals operational products could cause added noise in 5-min clocks. PPP analysis is performed (Panel 7) to assess whether the added noise is significant. JP2 only usable 30-sec clock AC from GPS Wk 1061 until GPS Wk 1773 when AC operational products were used to extend series to GPS Wk 1831. IGF: IGS05 -> IGS08 IGS operational products a priori reference frame switch (IGS05 -> IGS08) IG2 COMBINED ORBITS AC CONTRIBUTED ORBITS CF2 EM2 ES2 GF2 GR2 GT2 JP2 MI2 Table 2. Alias and direct tidal errors, and their frequency shifts due to rotating orbital frame. ~14d Strikingly different spectral content from other ACs O higher background power in along-track direction O more structure at periods shorter than 14d Effects of multi-day constraints on SRPs? Missing ocean tidal perturbations of geopotential? Relatively little background flicker noise, broader band thermal (white) noise Compared to JP2 (also GIPSY), background power in radial component drops off—different noise modeling in Kalman filter? O Bernese v. 5.2 PPP analysis performed O Daily coordinates estimated for 163 core IGS14 stations using IG1/IGF and IG2 products O Three main steps in the analysis: - fit satellite positions using the SP3 orbit, IG2 official EOPs and extended CODE (6+9) orbit model - preprocess clocks and RINEX observations to detect and eliminate clock jumps and cycle slips - data reduction with iterative post-fit cleaning; outliers are phase residuals exceeding 25 mm and code residuals exceeding 2.5 m O IERS 2010 Conventions generally implemented O GMF/GPT2 with daily tropospheric delay gradients following Chen and Herring (1997) O Daily coordinate sets compared to IG2 combined daily SINEX solutions, which are aligned to IGb08 IG1/IGF products O E: 4.3 (± 0.96) mm O N: 2.3 (± 0.82) mm O U: 6.4 (± 1.43) mm IG2 products O E: 4.5 (± 1.39) mm O N: 2.7 (± 1.43) mm O U: 6.9 (± 2.04) mm Avg. RMS of coordinate residuals after frame comparison IG2 Orbits (AC solutions compared to combined) IG2 improved Tx & Ty origin stability compared to IG1/IGF? IG2 improved rotational stability compared to IG1/IGF? IG2 orbit scale consistent with current operational Finals? IGF: s/w bug fix Spurious rotations and translations prior to 2004.5 due to high numbers of stations/ observations rejected for IG2—rejection criteria too small for IG2 clock biases??

Combined orbits and clocks from the IGS 2 reprocessingacc.igs.org/repro2/griffiths_ig2.pdfresiduals exceeding 2.5 m OIERS 2010 Conventions generally implemented OGMF/GPT2 with daily

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  • IG2 5-min Clocks (AC solutions compared to combined)

    6. ORBIT DAY-BOUNDARY DISCONTINUITIES

    2016 AGU FALL MEETING DECEMBER 12-16, 2016 SAN FRANCISCO, CA

    Combined orbits and clocks from the IGS 2nd reprocessing Jake Griffiths Naval Center for Space Technology U.S. Naval Research Laboratory, Washington, DC, USA [email protected]

    1. OVERVIEW In early 2015, the Analysis Centers (ACs) of the International GNSS Service (IGS) completed their second reanalysis of the full history of globally distributed GPS and GLONASS data collected since 1994. The suite of reprocessed AC solutions includes daily product files containing station positions, Earth rotation parameters, satellite orbits and clocks. This second reprocessing—or repro2—provided the IGS contribution to ITRF2014; it follows the successful first reprocessing, which provided the IGS input for ITRF2008. For this poster, we will discuss the newly combined repro2 GPS orbits and clocks. We also revisit our previous analysis of orbit day-boundary discontinuities with several significant changes and improvements. (1) Orbit discontinuities for the contributing ACs were studied in addition to those for the IGS repro2 combined orbits. (2) Apart from homogeneous reprocessing with updated analysis models, the main difference compared to the IGS Final operational products is that NOAA/NGS inputs were not submitted for the IGS reprocessing, yet they contribute heavily in the operational orbits in recent years. Also, during spring 2016, the ESA modified their orbit model so that it is no longer consistent with the one used for reprocessing. (3) A much longer span of orbits was available now, up to 11.2 years for some individual satellites, which allows a far better resolution of spectral features. (4) The procedure to compute orbit discontinuities has been further refined to account for extrapolation edge effects, improved geopotential fields, and to allow for spectral analysis of a longer time series of jumps. The satellite position time series used are complete enough that linear interpolation is necessary for only sparse gaps. So the key results are based on standard FFT power spectra (stacked over the available constellation and lightly smoothed). However, we computed Lomb-Scargle periodgrams to provide higher frequency resolution of some spectral peaks and to permit tests of the effect of excluding eclipse periods. From this test, we found that the effect of eclipses is negligible; we do not discuss the matter further in this poster.

    2. AC CONTRIBUTIONS

      7 Operational Centers -  COD, ESA, GFZ (GF2), GRG, JPL, MIT

      2 TIGA Centers for densifying ITRF2014 with GNSS stations at tide-gauges -  GFZ (GT2), ULR

    LEGEND slash: snx, sp3, erp [brdc clk in sp3] dots: snx, sp3, clk (5m), erp solid: snx, sp3, clk (30s), erp

    hachure: operational products

    ACKNOWLEDGEMENTS: Support for this work was provided by the NASA ROSES-2016 program under NRA #: NNH16AC75I. Thanks to Kevin Choi for helping to verify IGS software performance on NRL computers.

    7. PPP: IG2 ORBIT+CLOCK PERFORMANCE

    Jim Ray Retired National Geodetic Survey, Silver Spring, MD, USA

    3. ORBIT COMBINATION STATISTICS

    5. ORBITAL FRAME

    Rotations Translations

    Scale

    - X -

    - Y -

    - Z -

    Model changes in IGS Finals operations

      AC orbit scale drifts -  EM2, JP2 similar scale used by GIPSY -  ES2 similar to IG1/IGF (Wks 1050-1550)

    Scale change of ~0.55 ppb is smaller than the expected ~0.72 ppb   Earth albedo modeling by all ACs   Antenna thrust not modeled by ESA

      Large annual motion in GR2 Tz offsets   Other ACs show smaller ~annual Tz motions

    but with various phases -  Up to +9/-5 mm offsets

    Combination approach same as official IGS Finals a priori AC weighting:   UL2 -> comparison only (all; not shown)   MI2 -> comparison only (0730 thru 1250)   GR2 -> comparison only (all)   GT2 -> comparison only (0730 thru 1720)

    Other products for comparison only:   IG1 = IGS 1st reprocessing   IGF = IGS Finals operational solution

      Large offsets in early years: CF2, ES2, GT2   Periods of spurious rotations for GF2   Large offsets for IG1 and IGF until Wk 1702

    (switch to daily products & combo s/w bug fix)

    Combination approach same as official IGS Finals a priori AC weighting:   UL2 -> comparison only (all; not shown)   MI2, GR2, GT2 -> comparison only (all)

    Other products for comparison only:   IG1 = IGS 1st reprocessing   IGF = IGS Finals operational solution

    4. CLOCK COMBINATION STATISTICS

    IGF & IG2 most similar   ops AC products used   remaining difference from

    missing NGS in repro2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    o  IG1 o  IGF ² IG2

    Avg. Scale   IGF/IG1: -0.15 (± 0.21) ppb   IG2: -0.04 (± 0.63) ppb

    Avg. Rx   IGF/IG1: -15.6 (± 42.6) µas   IG2: 0.5 (± 114.8) µas

    Avg. Ry   IGF/IG1: -1.1 (± 48.8) µas   IG2: -1.4 (± 94.0) µas

    Avg. Rz   IGF/IG1: -66.5 (± 73.0) µas   IG2: -35.5 (± 195.1) µas

    Avg. Tx   IGF/IG1: 0.91 (± 1.36) mm   IG2: 0.25 (± 4.77) mm

    Avg. Ty   IGF/IG1: 0.23 (± 1.40) mm   IG2: 0.52 (± 4.48) mm

    Avg. Tz   IGF/IG1: 4.51 (± 2.54) mm   IG2: 0.10 (± 3.37) mm

    Power spectra for ~11.22 years (2003.90 – 2015.12) of IG2 orbit day-boundary discontinuities

    Annual, semi-annual, and harmonics of GPS draconitic year (351.6d), up to at least 10th

    9-peak comb near 14d:   sub-daily EOP tide alias

    (M2,O1,Oo1) errors and Mf/Mf’ direct tide errors present possibly frequency shifted due to draconitic orbital frame rotation

      other spectral peaks in 14d band, in particular, in cross-track, are unexplained (see details in tables to right)

    Approach

    Compared to IG1/IGF, the IG2 orbits+clocks deliver long-term global coordinate sets that are noisier and also slightly more biased, perhaps due to AC repro2 satellite clock issues prior to 2004.5. Exploring mitigating steps. For IGS14, the IGS may apply satellite clock corrections consistent with igs08.atx -> igs14.atx APV Z-PCO changes. This may offer potential for PPP users to access IGS14 using IG2 products. Still under evaluation.

    WRMS agreement between IG2 & IG1/IGF orbits at the 5 mm level for most of repro2 span; early years range from 50 mm to 10 mm WRMS agreement.

    in terrestrial frame in orbit frame Expected Peak f (cpd) P (d) f (cpd) P (d) pro/retro M2 24-hr alias 0.067727 14.765 0.064882 15.412 P

    0.070571 14.170 R

    O1 24-hr alias 0.070464 14.192 0.067620 14.788 P

    Mf tide 0.073203 13.661 0.070359 14.213 P 0.076047 13.150 R

    Mf' tide 0.073349 13.633 0.070505 14.183 P 0.076193 13.125 R

    Oo1 24-hr alias 0.075940 13.168 0.073096 13.681 P 0.078784 12.693 R

    Weekly means of the daily AC clock RMS values from the repro2 5-min clock combination. The shift in RMS for IGF at the time of IGS05 -> IGS08 switch also corresponds to frame origin (Tz) and rotation (Rz) offset (see PPP analysis in Panel 7).

    in orbit frame Observed peak f (cpd) P (d) attributed source (see Table 2) 1 (ACR) 0.061994 16.131 ??? 2 (ACR) 0.064860 15.418 M2 alias P (shown at left) 3 (C) 0.067713 14.768 O1 alias P (shown at left) 4 (ACR) 0.070512 14.181 Mf' tide P (shown at left) + M2 alias R 5 (CR) 0.073364 13.631 ??? Oo1 alias ??? (shown at left) 6 (C) 0.076225 13.119 ??? Mf’ tide R ??? 7 (C) 0.079070 12.647 ??? 8 (C) 0.081898 12.210 ??? 9 (C) 0.084727 11.803 ???

    Table 1. Details for 14d band.

    Robust number of contributing ACs to form combined orbit products. Reduced redundancy amongst clock contributing ACs compared to IGS Finals operational products could cause added noise in 5-min clocks. PPP analysis is performed (Panel 7) to assess whether the added noise is significant. JP2 only usable 30-sec clock AC from GPS Wk 1061 until GPS Wk 1773 when AC operational products were used to extend series to GPS Wk 1831.

    IGF: IGS05 -> IGS08

    IGS operational products a priori reference frame switch (IGS05 -> IGS08)

    IG2 COMBINED ORBITS

    AC CONTRIBUTED ORBITS

    CF2

    EM2

    ES2

    GF2

    GR2

    GT2

    JP2

    MI2

    Table 2. Alias and direct tidal errors, and their frequency shifts due to rotating orbital frame.

    ~14d

    Strikingly different spectral content from other ACs   higher background power in along-track direction   more structure at periods shorter than 14d

    Effects of multi-day constraints on SRPs? Missing ocean tidal perturbations of geopotential?

    Relatively little background flicker noise, broader band thermal (white) noise

    Compared to JP2 (also GIPSY), background power in radial component drops off—different noise modeling in Kalman filter?

      Bernese v. 5.2 PPP analysis performed   Daily coordinates estimated for 163 core IGS14 stations

    using IG1/IGF and IG2 products   Three main steps in the analysis: -  fit satellite positions using the SP3 orbit, IG2 official

    EOPs and extended CODE (6+9) orbit model -  preprocess clocks and RINEX observations to detect

    and eliminate clock jumps and cycle slips -  data reduction with iterative post-fit cleaning; outliers

    are phase residuals exceeding 25 mm and code residuals exceeding 2.5 m

      IERS 2010 Conventions generally implemented   GMF/GPT2 with daily tropospheric delay gradients

    following Chen and Herring (1997)   Daily coordinate sets compared to IG2 combined daily

    SINEX solutions, which are aligned to IGb08

    IG1/IGF products   E: 4.3 (± 0.96) mm   N: 2.3 (± 0.82) mm   U: 6.4 (± 1.43) mm

    IG2 products   E: 4.5 (± 1.39) mm   N: 2.7 (± 1.43) mm   U: 6.9 (± 2.04) mm

    Avg. RMS of coordinate residuals after frame comparison

    IG2 Orbits (AC solutions compared to combined)

    IG2 improved Tx & Ty origin stability compared to IG1/IGF?

    IG2 improved rotational stability compared to IG1/IGF?

    IG2 orbit scale consistent with current operational Finals?

    IGF: s/w bug fix

    Spurious rotations and translations prior to 2004.5 due to high numbers of stations/observations rejected for IG2—rejection criteria too small for IG2 clock biases??

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