FY-3D/HIRAS On-orbit performance and validation

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Presentation transcript:

FY-3D/HIRAS On-orbit performance and validation Chengli Qi, Chunqiang Wu, Xiuqing Hu, Hanlie Xu, Lu Li, Fang Zhou National Satellite Meteorological Center(NSMC), CMA Mingjian Gu, Chunyuan Shao Shanghai Institude of Technical Physics(SITP), CAS GSICS Annual Meeting, 04-08 Mar 2019

Outline HIRAS on-orbit Performance L1 Products overview and Status Spectral accuracy validation Radiometric Calibration validation Summary

1. HIRAS on-orbit status Mar ,2018 - HIRAS infrared detectors powered on - Telemetry parameters check - Checks of 1st IGM, Raw Spectra, Calibrated spectra - Initial alignment of Interferometer fixed-mirror Apr, 2018 - Temperature changing of detector from 85Deg to 82Deg - Fine alignment of Interferometer fixed-mirror - Temperature cooling down of ICT - Cold space observations - ILS parameters tuning - NL coefficients generation Mar ~ Jun commission test , 17 items - NEdT evaluation - Spectral channel frequencies validation - Radiance validation - Inter-pixel comparison Aug, 2018 - commission finished

HIRAS performance: NEdT LW @ 0.625cm-1 Res MW @ 1.25cm-1 Res SW @ 2.5cm-1 Res Noise performance: derived from DS and ICT measurements NEdTs derived from DS and ICT are consistent. NEdTs in forward and reverse sweep direction are consistent. Meet requirements.

After preliminary assignment:2018-03-11,noise dominated by correlated noise Random noise FOV3 FOV4 After fine assignment:2018-04-30,noise dominated by random noise Total NEdN Correlated NEdN random NEdN Nt2 = Nc2 + Nr2

After preliminary assignment :2018-03-11, more than 90% dominated by correlated noise After fine assignment :2018-04-30,more than 90% dominated by random, proportion of correlated noise reduced. MW

After fine assignment :SW random noise proportion reached 95% After fine assignment :SW random noise proportion reached 95%. Correlated noise proportion reduced and without obvious wavelength dependence . MW2

NEdT monitoring for some channels in 3 bands, Performs stable;

2. L1 Products overview and Status Band Spectral Range (cm-1) Spectral Resolution(cm-1) MPD(cm) Ch No FR DR LW 650~1135 0.625 0.8 777 MW 1210~1750 1.25 0.4 869 433 SW 2155~2550 2.5 0.2 637 159 FY3D_HIRAS_GBAL_L1_20180501_1310_L1AXX_MS.HDF FY3D_HIRAS_GBAL_L1_20180501_1310_016KM_MS.HDF FY3D_HIRAS_GBAL_L1_20180501_1310_OBCXX_MS.HDF FY3D_HIRAS_GBAL_L1_20180501_1310_L1AXX_DR.HDF FY3D_HIRAS_GBAL_L1_20180501_1310_016KM_DR.HDF FY3D_HIRAS_GBAL_L1_20180501_1310_OBCXX_DR.HDF FY-3D/HIRAS L1 data valid from 2018.04.20, data with Quality control flag valid from 2018.08.22

3. Spectral accuracy validation HIRAS OBS compared with LBLRTM simulation in clear ocean condition. Clear pixels filtering: Using MERSI cloud mask production. Clear pixels determined from MERSI cloud mask MERSI-II Cloudmask

Spectral bias vs LBLRTM – first optical assignment Spc bias mean(ppm) FOV1 FOV2 FOV3 FOV4 LW 38.299 32.145 24.97 29.822 MW -15.18 -4.6811 -10.813 -3.4975 Spc bias std(ppm) FOV1 FOV2 FOV3 FOV4 LW 0.996 0.774 0.751 1.085 MW 1.185 2.143 2.592 1.834

Spectral bias vs LBLRTM after fine optical assignment Spc Bias mean(ppm) FOV1 FOV2 FOV3 FOV4 LW -3.06 -0.67 1.05 1.58 MW -3.76 -1.02 -1.17 -2.60 SW -1.38 1.61 2.39 Spc Bias std(ppm) FOV1 FOV2 FOV3 FOV4 LW 1.18 1.11 0.81 1.39 MW 1.35 1.34 1.65 1.68 SW 4.52 5.22 3.09 3.32

Instrument responsivity function (ISRF) used to monitor the signal variation HIRAS suffered signal attenuation due to silica gel gas contamination, in LW band most serious region of 800cm-1 attenuation rate is about 9% per month

In MW and SW bands, attenuation rate is about 2.7% and 3.7% per month

LW band decontamitation MW band Spectral bias monitoring in 9 months, spectral bias is in range of 5ppm for MW and SW in 9 months. There is 5~10 ppm trend in LW, after on-orbit heating it recovered. SW band

4. Radiometric Calibration validation SNO Pairing Method Time Constrains: 10 minutes Air Path Constrains FOR 14-17 for CrIS FOR 14-16 for HIRAS. Distance constrains: 5 km Scene uniformity VIIRS and MERSI: std < 0.2K Method: Wang et al 2016 Data:2018.04.25-2018.05.15 20 days LW bias better than 0.5K,MW less than 0.7K; LW bias std better than 0.3K,MW std 0.2~1K;

Data:2018.04.22-2018.05.26 17 days LW bt bias better than 0.5K,MW bt bias less than 0.7K; LW bias std lett than 0.5K, MW bias std in 0.5~1K, SW window and weak absorption region meet 0.5K ;

4 months of HIRAS-CrIS bias monitoring shows stable error characteristics.

O-B monitoring shows stable error characteristics.

Comparison between HIRAS and MERSI advanced MEdium Resolution Spectral Imager (MERSI II)  FY-3D/MERSI-II Spectral Characteritics Channel Wavelenth (m) Bandwidth (nm) Nadir spatial resolution (m) 20 3.8 180 1000 21 4.05 155 22 7.2 500 23 8.55 300 24 10.8 250 25 12.0

After scene uniformity check MERSI-HIRAS bias changed with scene brightness temperature MERSI Ch 4.05 7.2 10.8 12.0 Scene_bt(K) 284 251 286 285 Mean bias(K) -0.90 0.68 0.74 0.26

HIRAS RTTOV simulation and measurement Mean bias Bias std Mean bias are within 1K in LW and MW bands, FOV3 exhibits inconsistency with Other 3 FOVs due to a little field sheltering.

LW MW SW HIRAS-CrIS bias for each FOV, FOV3 exhibits 0.3~0.5K of inconsistency with other FOVs.

Future Work To improve data quality in SW band To improve the FOV uniformity To decrease scene temperature and scan angle dependent BIAS Move to FY-3E, Early Morning Orbit scan angle dependent BIAS Irregular response

HIRAS Improvement from FY-3D to FY-3E Early Morning orbit Band Spectral Range (cm-1) Spectral Resolution Sensitivity (NET@280K) Num of Channels FY-3D FY-3E LWIR 650~1136 (15.38m~8.8 m) 0.625 0.15(Expectation) 0.4K(Requirement) 650 ~667 cm-1 0.8K 778 667~689 cm-1 0.4K 689~1000 cm-1 0.2K 1000~1136 cm-1 MWIR1 1210~1750 (8.26m~5.71 m) 1.25 0.1(Expectation) 0.7K(Requirement) 1210~1538 cm-1 433 1538~1750 cm-1 0.3K MWIR2 2155~2550 (4.64m~3.92 m) 2.5 0.3(Expectation) 1.2K(Requirement) 2155~2300 cm-1 0.3 159 2300~2550 cm-1 0.5

SUMMARY FY-3D/HIRAS Commission test which contain 17 test items finished and results are promising. Ground processing system is running smoothly and is generating L1 data in real time. The accuracy of HIRAS radiometric and spectral calibration and its stability are assessed using SNO samples and Simulation Data. Overall, radiometric biases (O-S) are small and stable over time, FOV-2-FOV differences are less than ~0.2 K for LW and MW bands. The spectral accuracy is better than 3ppm for LW and 5 ppm for MW/SW band. HIRAS is a great improvement to Chinese satellite infrared atmospheric sounding system