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SMOS-BEC – Barcelona (Spain)
LO calibration frequency impact
Part II
C. Gabarró, J. Martínez, V. González,
A. Turiel & BEC team
SMOS Barcelona Expert CentrePg. Marítim de la Barceloneta 37-49, Barcelona SPAINE-mail: [email protected] : www.smos-bec.icm.csic.es
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
LO CAL FREQ ANALYSIS
INDEX
1)BRIEF SUMMARY OF QWG-4 (March-2011) & QWG- 5 (June) RESULTS & CONCLUSIONS :
- ICM STUDY- UPC STUDY
2)NEW ANALYSIS WITH DECIMATED DATA FROM MARCH 2010 (processors v500)
2)ANALYSIS OF NOVEMBER/ DECEMBER 2011 DATA (using 2 weeks of LO=2min)
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
ICM QWG-4 STUDY
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20100325T040821descending
TBH_10min-TBH_2min TBV_10min-TBV_2min
Decimation Study(10min, 6min and 2min)57 orbits from 24th – 25th March 2010
TB_10min-TB_2min
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SSS LO 10min -2min SSS LO 6min -2min
ICM QWG-4 STUDY
SSS LO 10min - 2min
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
6min
-2m
in
10m
in-2
min
Spatial structures appear both cross-track and along-track The structures are still present after averaging
data with decimated calibration. (Tx+Ty)/2 averaging 0 to 40º incidence angles.
UPC LO ANALYSIS
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
UPC LO ANALYSIS
10
min
-2m
in6
min
-2m
inThe LO-phase error induces structure in xi-eta
Average of 126 snapshots of TBn-TB2
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
CONCLUSIONS FROM QWG-4 & 5
•Clear impact on TB (larger in V-pol) and SSS.
•TB differences between LO-10min and LO-2min have a global STD of 0.47 K.
•LO phase drift produces non-random visibilities errors -> TB spatial structures in xi-eta.
•Relatively small phase error (low STD) may have impact on the image due to this systematic behaviour.
•Spatial structures are expected in SSS retrievals due to imperfect LO phase error cancellation.
•Differences in SSS global STD 0.48 psu.7
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
LO Cal Freq Analysis in QWG-7
2) DATA SET: DECIMATION STUDY
•24th-26th March 2010 (81 semi-orbits) with MIRAS at LO=2 min
•Repeated the decimitation with the newest versions of processors:• L1PP5.00 (no land-sea contamination bug)• L2PP5.00
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Different impact across track : Spatial structures, as observed in UPC study.
SSS 10 min- SSS 2min
X-Swath (Km) X-Swath (Km)
SSS 10 min- SSS 2minAveragingAveraging
One half-orbit from Pacific(similar with many)
2) DECIMATION MARCH 2010
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
3 days, 81 semi-orbitsStrong filtering (optimal conditions)World except N. Atlantic & Med.Different OTTs for 2, 6, 10 min.
• Large Reduction of STD in TB• Reduction of tails
2) DECIMATION MARCH 2010
TB 10 min- TB 2min TB 6 min- TB 2min
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Comparing calibration at 10 min vs. 6 min
0.55 0.15
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
SSS 10min – SSS 2min
Latit
udin
al a
vera
ge
Lat=[45S, 30N]Bias = 0.05 psu Std = 0.11 psu
Lat=[45S, 30N]Bias = 0.05 psu Std = 0.11 psu
SSS L3 map 10 min – SSS L3 map 2 min -> 3 days, 0.5o binned
Filtered by:X-Swath < 400 kmPoor_geo & poor_ret
2) DECIMATION MARCH 2010
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
2) DECIMATION MARCH 2010
• Significant reduction of bias & Std SSS by going to 6min, reduction of tails• Accuracy req. SSS maps 0.1 psu. -> low cal. freq implies additional non negligible error!
SSS
10 m
in-
SSS
2min
SSS
6 m
in-
SSS
2min
WORLD LAT=[45S, 30N]
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0.28
0.070.16
0.11
Comparing10 and 6 min.
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
3) DATA FROM NOVEMBER – DECEMBER 2011:
3 periods of 10 days have been selected (from DPGS)
•20th – 29th November : LO=10 min•6th – 15th December : LO=2 min•20th - 29th December : LO=10 min
Maps of 10 days at 4H9 have been constructed.
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SMOS QWG-7 ESRIN, 31 January – 1 February 2012
Mean AVERAGE (SMOSminus ARGO)Periods of 10 days -> one every 3 days
Mean AVERAGE (SMOSminus ARGO)Periods of 10 days -> one every 3 days
high variation over timehigh variation over time
5-19 DecLO =2min
<SSS
-ARG
O>
LO effect between different periods of time is maskedLO effect between different periods of time is masked
01-10 July 2011
31 Dec, 201110 Jan 2012Mixed LO data
2min & 10 min
3) DATA FROM NOV. – DEC. 2011
L1PP500 L2PP500
L2PP550
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SSS Nov 21 to 30 (LO = 10min)- SSS Dec 6 to 15 (LO = 2min)
Latit
udin
al a
vera
ge
3) DATA FROM NOV. – DEC. 2011
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Lat=[45S, 30N]Bias = 0.25 psu -> higher than decimated
Lat=[45S, 30N]Bias = 0.25 psu -> higher than decimated
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(SSS10min – SSS2min)_AB = Δ_impact_LO_AB + Δ_SSSvariability_AB + Δ_other_AB (SSS10min – SSS2min)_AB = Δ_impact_LO_AB + Δ_SSSvariability_AB + Δ_other_AB
20-29 NovLO =10min
6-15 DecLO =2min
20-29 DecLO =10min
Period A Period B Period C
Estimated withARGO measurementsEstimated withARGO measurements
Includes TEC, Sun, galaxy, instrument …Hard to estimate; we have used a
linear interpolation from AC period
Includes TEC, Sun, galaxy, instrument …Hard to estimate; we have used a
linear interpolation from AC period
TO BE ESTIMATEDTO BE ESTIMATED
3) DATA FROM NOV. – DEC. 2011
To compare data from different periods it is necessary to consider all the factors that contribute to the differences in SSS.
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4H9 L3 binned mapaveraged to 1x1 degree
4H9 L3 binned mapaveraged to 1x1 degree
low noise: candidate to detect LO contributionLat: 0N-30S Bias = -0.21Lon: 180W-90W STD = 0.34
low noise: candidate to detect LO contributionLat: 0N-30S Bias = -0.21Lon: 180W-90W STD = 0.34
highly noisyhighly noisy
highly noisyhighly noisy (SSS10min – SSS2min)_AB (SSS10min – SSS2min)_AB
3) DATA FROM NOV. – DEC. 2011
Δ_impact_LO_AB = (SSS10min – SSS2min)_AB - Δ_SSSvariability_AB - Δ_other_AB
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Δ_SSSvariability_ABΔ_SSSvariability_AB
Optimal interpolation1x1 degree
Optimal interpolation1x1 degree
Differences between OI mapsof ARGO measurementsDifferences between OI mapsof ARGO measurements
3) DATA FROM NOV. – DEC. 2011
Δ_impact_LO_AB = (SSS10min – SSS2min)_AB - Δ_SSSvariability_AB - Δ_other_AB
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Δ_other_AB Δ_other_AB
high noise:LO effect will be masked
high noise:LO effect will be maskedlow noise: changes in other factors low enough
to allow assessing LO contributionLatitude: 0N-30S
Longitude: 180W-90W
low noise: changes in other factors low enough to allow assessing LO contribution
Latitude: 0N-30SLongitude: 180W-90W
3) DATA FROM NOV. – DEC. 2011
Δ_impact_LO_AB = (SSS10min – SSS2min)_AB - Δ_SSSvariability_AB - Δ_other_AB
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Δ_impact_LO_AB = -0.03 bias, 0.3 stdin the most favorable case
Δ_impact_LO_ABΔ_impact_LO_AB
3) DATA FROM NOV. – DEC. 2011
Δ_impact_LO_AB = (SSS10min – SSS2min)_AB - Δ_SSSvariability_AB - Δ_other_AB
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LO cal. freq. seems to impact on land contamination
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Δ_impact_LO_AB in optimal situation
Lat=[30S , 0N]Lon=[180W , 90W]
Mean: -0.0320 psuMedian: -0.0318 psuStd dev.: 0.2940 psu
Δ_impact_LO_AB in optimal situation
Lat=[30S , 0N]Lon=[180W , 90W]
Mean: -0.0320 psuMedian: -0.0318 psuStd dev.: 0.2940 psu
3) DATA FROM NOV. – DEC. 2011
Δ_impact_LO_ABΔ_impact_LO_AB
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∆_SSSvariability mean = 0.0183 median = 0.0206 std = 0.1126 ∆_other mean = -0.2579 median = -0.2559 std = 0.1831
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CONCLUSIONS (I)
• In previous QWG it was shown that LO impact is not negligible nor at TB neither at SSS level.• TB spatial structures in xi-eta and across track are observed Study on decimated data (3 days, March 2010) using v500:
- TB 10min – 2min:mean= 0.07 K & std=0.54 K
- SSS L3 0.5o binned maps 10min – 2min: bias = 0.08 psu & Std = 0.28 psu
Study of two different periods (Nov-Dec 2011) - Instrumental factors are much larger than LO contribution
(thus hard to estimate). However, our analysis points to a significant LO impact on SSS maps (under optimal conditions: box in S Pacific)
bias = -0.03 psu & std = 0.29 psu22
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CONCLUSIONS (II)
• Evidence is limited as the data for the study are limited. However, now as before, the issue seems serious enough to be taken into account.
• Incremental studies on incremental samples of data will probably lead to more or less the same conclusions.
• Processing improvements (CW and so on) are unlikely to change this situation.
• Definitively: with 10 min LO calibration we will never meet the mission requirements over ocean
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In summary:
• 10 min kills SMOS salinity requirements
• Processing options will not help
• Time to turn on Guillermo’s proposal