Long-term radiometric validation of the ATSR SST record using the M-AERI

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Long-term radiometric validation of the ATSR SST record using the M-AERI Gary Corlett, David Llewellyn-Jones University of Leicester and Peter Minnett RSMAS, University of Miami

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Long-term radiometric validation of the ATSR SST record using the M-AERI. Gary Corlett, David Llewellyn-Jones University of Leicester and Peter Minnett RSMAS, University of Miami. Thermal and Vis/IR imaging radiometer Similar Thermal channels to AVHRR, MODIS. - PowerPoint PPT Presentation

Transcript of Long-term radiometric validation of the ATSR SST record using the M-AERI

Page 1: Long-term radiometric validation of the ATSR SST record using the M-AERI

Long-term radiometric validationof the ATSR SST record

using the M-AERI

Gary Corlett, David Llewellyn-JonesUniversity of Leicester

and

Peter MinnettRSMAS, University of Miami

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What is an ATSR?• Thermal and Vis/IR imaging

radiometer• Similar Thermal channels to

AVHRR, MODIS. • Dual view (nadir and 55º to

nadir)– Along-track scanning, two views of

same scene at different angles, for better atmospheric correction

• On board calibration – 2 on-board black bodies for IR

calibration– VISCAL unit for visible channel

calibration• 500 km swath • 1 km IFOV at nadir

• Stirling Cycle Coolers, cooling low noise detectors to 80K, for optimum signal-to-noise ratios

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V2.0 ATSR 18 Year SST Climatology

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http://www.rsmas.miami.edu/rccl/maeri.html

M-AERI Instrument• Marine - Atmospheric Emitted

Radiance Interferometer (M-AERI)

• Spectral range: 500 – 3300 cm-1 (3-18 m)

• Resolution: 1.0 cm-1

• Field of View: 1.3 °• Measurement cycle: ~ 11

minutes• Views ahead of the ship’s bow

wave to avoid disturbance

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M-AERI SSTs• SST calculated from 10 spectral points near 7.7 µm• Corrected for reflected sky radiance and atmosphere

between the sea surface and the M-AERI instrument (~1 km atmospheric path length)

• Emissivity value used in SST retrieval was derived from previous M-AERI measurements made at sea

• Calibration using two internal black bodies

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M-AERI Accuracies

• Traceability to NIST through the NIST EOS Transfer Radiometer (TXR) and NIST traceable reference thermometers.

• Residual uncertainties <0.03K

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M-AERI Cruises

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AATSR Overpass

-15 mins +15 mins-120 mins +120 mins

AATSR pixel closest to lat and long of in situ

measurement1 x 1 block

3 x 3 block

Match-up Criteria

All results in following slides are for clear-sky match-ups to thenearest 1-km pixel within 2 hours for ATSR version 2.0 data

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Match-up Locations (AATSR)

Day time match-upsNight time match-ups

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Histograms of differences

N2 N3 D2 D3

N2 D2

Without filter ofM-AERI SD < 0.1 K

N2: Nadir-only, 11 & 12N3: Nadir-only, 3.7, 11 & 12D2: Dual-view, 11 & 12D3: Dual-view, 3.7, 11 & 12

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Wind Speed Dependence

D2/N2 – redD3/N3 – blackLH axis – Median difference plus/minus standard errorRH axis – Number of match-ups (solid line)Asterisk is 90% confidence from Student’s T-test

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Which Statistics?All D3 retrievals versus drifting buoys

• Simple Arithmetical– Mean: -0.09 K– SD: 0.49 K

• 3-sigma– Mean: -0.09 K– SD: 0.35 K

• D-N (GHRSST L2P)– Mean: -0.08 K– SD: 0.37 K

• Robust– Median: -0.08 K– RSD: 0.33 K

• Gaussian fit– Mean: -0.07 K– SD: 0.27 K

Uncertainty usually quoted as Standard Deviation,which is 1 σ (k=1) or 68.27% of the distribution

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AATSR/M-AERI Match-up StatsRetrieval

Nadir-only Dual-view

Number Mean/Median (K) SD/RSD (K) Mean/Median (K) SD/RSD (K)

All data: Non-robust statistics

Day time (2-channel) 269 +0.84 0.90 +0.24 0.61

Night time (3-channel) 734 +0.08 0.32 +0.11 0.40

After 3-sigma filter: Non-robust statistics

Day time (2-channel) 264 +0.80 0.82 +0.20 0.48

Night time (3-channel) 718 +0.07 0.25 +0.10 0.33

After D-N filter: Non-robust statistics

Day time (2-channel) 231 +1.03 0.64 +0.19 0.57

Night time (3-channel) 677 +0.09 0.31 +0.07 0.36

All data: Robust statistics

Day time (2-channel) 269 +0.93 0.54 +0.15 0.40

Night time (3-channel) 734 +0.10 0.23 +0.09 0.31

All data: Gaussian Fit to Histogram

Day time (2-channel) 269 +0.93 0.54 +0.15 0.40

Night time (3-channel) 734 +0.11 0.18 +0.10 0.23

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Compare AATSR/M-AERI and AATSR/drifters

Retrieval

M-AERI Drifters

NumberNadir-only Dual-view

NumberNadir-only Dual-view

Median (K)

RSD (K)Median

(K)RSD(K)

Median (K)

RSD (K)Median

(K)RSD (K)

Day time

269 +0.93 0.54 +0.16 0.45 577 +0.86 0.44 +0.06 0.34

Night time

734 +0.10 0.23 +0.09 0.31 684 -0.07 0.28 +0.01 0.38

Drifter match-ups limited to wind speeds > 6 ms-1

Expect ‘constant’ offset of -0.17 KRobust statistics

Note: Radiometer night time RSD smaller than drifters, but radiometer day time RSD largerthan drifters. Similar results seen for ISAR match-ups. Likely due to higher natural variabilityin day time ocean skin due to small scale changes in wind speed and solar insolation. Impactof such changes will be lower below the ocean skin.

Note: Radiometer night time RSD smaller than drifters, but radiometer day time RSD largerthan drifters. Similar results seen for ISAR match-ups. Likely due to higher natural variabilityin day time ocean skin due to small scale changes in wind speed and solar insolation. Impactof such changes will be lower below the ocean skin.

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Compare AATSR/ISAR and AATSR/M-AERIRetrieval D minus N

Location Data N3 (K) D2 (K) D3 (K) D3 – N3 (K)

Bay of Biscay & English Channel

Drifters - 0.07 (0.01) - 0.02 (0.01) - 0.14 (0.01) - 0.07

ISAR + 0.09 (0.01) - 0.04 (0.02) + 0.01 (0.01) - 0.08

Skin-effectISAR

- 0.16 (0.01) +0.02 (0.01) - 0.15 (0.01) -

Caribbean Sea

Drifters - 0.07 (0.01) + 0.08 (0.01) - 0.03 (0.01) + 0.04

M-AERI + 0.09 (0.01) + 0.11 (0.03) + 0.08 (0.01) - 0.01

Skin-effectM-AERI

- 0.16 (0.01) +0.03 (0.01) - 0.11 (0.01) -

All match-ups limited to wind speeds > 3 ms-1 < 9 ms-1

Median difference and standard errorNote difference in D-N in Caribbean compared to BoB/EC

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Compare AATSR/M-AERI and ATSR-2/M-AERI

Retrieval

AATSR ATSR-2

NumberNadir-only Dual-view

NumberNadir-only Dual-view

Median (K)

RSD (K)

Median (K)

RSD(K)Median

(K)RSD (K)

Median (K)

RSD (K)

Day time

269 +0.93 0.54 +0.16 0.45 204 +0.58 0.39 -0.05 0.33

Night time

734 +0.10 0.23 +0.09 0.31 612 -0.06 0.22 +0.02 0.31

All match-ups from Explorer of the Seas M-AERIFull records shown, not just overlap periodsRobust statistics

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Conclusions (1)• Long-term reference data set for satellite validation

provided by M-AERI on Explorer of the Seas– Radiometers are only reference data that is fully traceable to

national standards (NIST) at all times• Used to validate both ATSR-2 and AATSR

– Small number of three-way match-ups during overlap period (not shown here)

• Results show good agreement for D3 match-ups– AATSR warm relative to ATSR-2– Evidence that observed 12 micron difference is indeed due to

AATSR SRF and not ATSR-2• N3 match-ups have lowest noise

– Evidence of poor cloud screening and alignment uncertainty in dual view retrievals

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Conclusions (2)• Good agreement between M-AERI, AATSR & drifters

– All biases ~ 0.1 K for D3• Good agreement between radiometer/drifter results

between Caribbean Sea and Bay of Biscay/English channel

• M-AERI and ISAR match-ups have lower noise at night compared to drifters but higher noise during the day– Evidence of increased skin variability in day time

• Clearly an issue with outliers– Very small (few %) number of outliers have large impact

on statistics– Robust statistics provide more realistic uncertainties for

users and are recommended

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Looking Forward• AATSR is now expected to operate until the end of 2013 at the latest• The ATSR follow-on instrument (SLSTR) on the ESA Sentinel 3 satellite is not

expected to fly before 2013 and so there may be an enforced break in the ATSR record.– Any break will mean that an overlap between AATSR and Sentinel 3 will not be

possible.

• This raises two fundamental SST data continuity questions:– How can the calibration of the ATSR dataset record be transferred to Sentinel 3 if there is a gap?

– How might the data gap between the two missions be filled using alternative SST data with the minimum loss of quality?

• The former is by far the most critical issue, as climate scientists need to be assured that there are no biases between AATSR and Sentinel 3 and that any observed change in temperature is real.

• Situation not just true for AATSR/SLSTR– Need to protect existing and future satellite SST records

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Reference Data Sources

• Satellite SST validation uses the various types of ref. Data available. Ideally we require combination of these measurements

• Radiometers– Provide SST-skin; only traceable reference source; expensive; very poor

coverage owing to low number of deployments; long-term deployments preferred; funding not guaranteed

• Argo floats– Provide SST-depth; excellent calibration (0.005 K); only surface every 10 days;

funding not guaranteed; provides global uncertainties• Drifting buoys

– Provide SST-depth; depth unknown; not calibrated; main workhorse for global uncertainties

• Moored buoys– Provide SST-depth; reasonable calibration; often in tough regions for

validation (e.g. coasts); good for regional uncertainties• Ship thermometry

– Provide SST-depth; usually poor calibration; can be useful for areas without drifters

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Generic SST validation• Need to move to generic validation

– Validation should not be mission specific– Provides protection for data gaps– Costs can be shared– Offers maximum benefit to all

• Work with GHRSST– To agree best practices and methods for the “community”

• Work with CEOS– To implement QA4EO guidelines– For intercomparisons

• Maintain links to other communities– Argo; DBCP; JCOMM SOT

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Potential Next Steps

• Get ship-borne radiometry on firmer footing– Need long-term funding for several deployments

• Get more secure funding for Argo– Ideally obtain near-surface profiles

• Improve calibration of drifting buoys– Pilot project underway

• Use ships more opportunistically– But need improved measurements (e.g. IMOS)

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Acknowledgementsare due to:

• NASA for funding M-AERI operations

• Personnel at RSMAS for M-AERI support

• DECC for funding AATSR sensor and support teams, including ISAR Programme at the University of Southampton

• ESA for funding the Envisat Mission and for provision of AATSR data

GKC and the PI/Val Team at the University of Leicester are funded by DECC through Space ConneXions contract 2004-03-001/CPEG10