JMA lunar calibration report [MTSAT-2 and GMS-5]

Slides:



Advertisements
Similar presentations
Preliminary Study of Lunar Calibration for Geostationary Imagers Japanese Multi-functional Transport SATellite-2 (MTSAT-2) incorporates the special device.
Advertisements

Japan Meteorological Agency, June 2016 Coordination Group for Meteorological Satellites - CGMS JMA’s Cal/Val activities Presented to CGMS-44 Working Group.
Japan Meteorological Agency, June 2016 Coordination Group for Meteorological Satellites - CGMS Non-Meteorological Application for Himawari-8 Presented.
2015 GSCIS annual meeting, March, 2015, New Delhi, India Application of GIRO to Himawari-8/AHI Hidehiko Murata and Masaya Takahashi Meteorological.
Visible vicarious calibration using RTM
Thomas C. Stone U.S. Geological Survey, Flagstaff, AZ USA GSICS Research Working Group Meeting EUMETSAT 24−28 March 2014 Using the Moon as a Radiometric.
A.K. Mitra, Shailesh Parihar, S.K. Peshin Ministry of Earth Sciences
PLEIADES Lunar Observations Sophie Lachérade, Bertrand Fougnie
Future eumetsat missions: MTG/FCI, MTG/UVNS and EPS-SG/METimage
Description of the giro ON THE DETAILS OF THE IMPLEMENTATION
Proposal for input/output data of GIRO application
PREPARATION OF THE GiRO executable
GIRO Input/Output data convention
Tim Hewison (1) Sébastien Wagner (1), Tom Stone (2), Gary Fowler (1)
Calibrating the METEOSAT SEVIRI solar channels using lunar observations Sébastien Wagner (1) Bartolomeo Viticchie (1), Tom Stone (2), Tim Hewison(1), Gary.
EUMETSAT’s Lunar Calibration Capabilities
Lunar observation data set preparation
Progress toward DCC Demo product
Sébastien Wagner, Tim Hewison In collaboration with D. Doelling (NASA)
SEVIRI Solar Channel Calibration system
Technical Expectations from Organizers & Participants B. Fougnie, S
Fangfang Yu and Xiangqian Wu
Fangfang Yu, Xiangqian Wu and Tom Stone
Meteorological Satellite Center Japan Meteorological Agency
Vicarious calibration by liquid cloud target
Requirements for GSICS Plotting Tool to support VIS/NIR products
DCC inter-calibration of Himawari-8/AHI VNIR bands
JMA’s GSICS and SCOPE-CM activities Presented to CGMS-43 Working Group II session, agenda item 3 (from MTSAT-2) Japan Meteorological Agency.
GOES-16 ABI Lunar Data Preparation to GIRO
JMA Agency Report Arata Okuyama, Masaya Takahashi, Hidehiko Murata, Ryoko Yoshino, Keita Hosaka, Tasuku Tabata Meteorological Satellite Center, Japan Meteorological.
Sébastien Wagner (1) Tom Stone (2), Gary Fowler (1), Tim Hewison (1)
GOES Lunar Calibration
MODIS Lunar Calibration Data Preparation and Results for GIRO Testing
Combining Vicarious Calibrations
Lunar data preparation for FY-2
Japan Meteorological Agency / Meteorological Satellite Center
Lunar INTER-CALIBRAION of AHI with MODIS
Data Preparation for ASTER
JMA Agency Report 2017 Arata Okuyama, Masaya Takahashi and Hidehiko Murata Meteorological Satellite Center, Japan Meteorological Agency.
Update on the GIRO Benchmark
Estimating MTF post-launch using lunar imagery – the case of SEVIRI
MTF Evaluation of Himawari-8/AHI using Lunar Observations
Effort toward Characterization of Selected Lunar Sites for the Radiometric Calibration of Solar Reflective Bands Fangfang Yu1, Xi Shao1, Xiangqian Wu2.
Sensitivity ANALYSIS Sébastien Wagner (EUMETSAT) In collaboration with
AHI IR Tb bias variation diurnal & at low temperature
Implementation of DCC at JMA and comparison with RTM
Himawari-8 Launch and its calibration approaches
Lunar data preparation for PROBA-V
EUMETSAT implementation of the DCC algorithm Sébastien Wagner
GOES Imager Lunar Calibration: Angular Variation of the Scan Mirror Visible Reflectivity Fangfang Yu (ERT, Xiangqian Wu(NOAA/NESDIS), Tom Stone(USGS),
National Satellite Meteorological Centre
Moving toward inter-calibration using the Moon as a transfer
GIRO APPLICATION Current status and NEXT STEPS
Sensitivity ANALYSIS Sébastien Wagner (EUMETSAT) In collaboration with
Lunar Observation Data for GIRO Landsat–8 Operational Land Imager
JMA Agency Report 2018 Masaya Takahashi, Yusuke Yogo and Hidehiko Murata Meteorological Satellite Center, Japan Meteorological Agency.
Inter-calibration of the SEVIRI solar bands against MODIS Aqua, using Deep Convective Clouds as transfer targets Sébastien Wagner, Tim Hewison In collaboration.
KMA Agency Report NMSC/KMA
An introduction of FY2 and its Lunar calibration
Moving toward inter-calibration using the Moon as a transfer
Traceability of the GIRO to the ROLO: Definition of a benchmark
Lunar calibration of COMS visible channel using GIRO
Masaya Takahashi (JMA) Dohyeong Kim (KMA)
Implementation of DCC algorithm for MTSAT-2/Imager
Inter-band calibration using the Moon
Impacts of I01 and M05 of S-NPP/VIIRS on AHI-VIIRS Ray-matching
goes-16/17 abi lunar calibration
S3B OLCI Lunar Observations
JMA Agency Report 2019 Masaya Takahashi, Yusuke Yogo and Kazuki Kodera
Towards a GSICS DCC product...
Presentation transcript:

JMA lunar calibration report [MTSAT-2 and GMS-5] Masaya Takahashi1, Bartolomeo Viticchie2, and Sebastien Wagner2 1Japan Meteorological Agency, 2EUMETSAT Acknowledgement: Tom Stone (USGS) Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Contents Introduction MTSAT-2/Imager lunar calibration GMS-5/VISSR lunar calibration Summary and future plans Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

JMA geostationary (GEO) satellites GMS (Geostationary Meteorological Satellite) Jul 1977 GMS (Himawari) Aug 1981 GMS-2 (Himawari-2) Aug 1984 GMS-3 (Himawari-3) Sep 1989 GMS-4 (Himawari-4) Mar 1995 GMS-5 (Himawari-5) (GOES-9) Back-up operation of GMS-5 w/ GOES-9 by NOAA/NESDIS: 2003/05/22-2005/06/28 Satellite Operation period GMS 1978 – 1981 GMS-2 1981 – 1984 GMS-3 1984 – 1989 GMS-4 1989 – 1995 GMS-5 1995 – 2003 GOES-9 2003 – 2005 MTSAT-1R 2005 – 2010 MTSAT-2 2010 – 2015 Himawari-8 2015 – 2022 Himawari-9 2022 – 2029 ⒸNASDA ⒸNASDA ⒸNASDA ⒸNASDA ⒸNASDA MTSAT (Multi-functional Transport SATellite ) Feb 2005 MTSAT-1R (Himawari-6) Feb 2006 MTSAT-2 (Himawari-7) Himawari Himawari-8 Himawari-9 launched on 7 Oct. 2014! 2014 2016 ⒸSS/L ⒸMELCO Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Lunar observations of JMA GEO satellites SSP Lon H. Reso. of VIS/NIR at SSP # of bands Operation Period used in this study # of Obs. (for ROLO/total) Phage angle Himawari-8 ~140 E 0.5/1/2km VIS:3 NIR:3 IR:10 2015 – 2022 (planned) N/A at present MTSAT-2 145 E 1km VIS:1 IR:4 2010 – 2015 2010 – 2013 62/98 [-138,147] MTSAT-1R 140 E 2005-2014 (Incl. back-up operation) N/A due to its scanning pattern GMS-5 1.25km IR:3 1995 – 2003 48/50 [-94,96] # of lunar observations for MTSAT-2 and GMS-5 will increase Lunar observations for past GMS satellites will be extracted in future Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Spectral Response Functions MTSAT-2/Imager GMS-5/VISSR MSG-3/SEVIRI Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

MTSAT-2/Imager lunar calibration: general 3-axis stabilized GEO satellite Satellite position: from telemetry Located at ~ 145 E Instrument: VIS/IR optical imager Similar to GOES/Imager 1 visible channel (0.68µm) 1 km horizontal resolution at SSP 8 detectors for N-S direction 10-bit (1024 digital counts) Scanning: E-W direction Hourly Full-disk obs. + NH/SH obs. The Moon acquisition NO maneuver, unscheduled 2-5 lunar observations / month Visible channel calibration Constant pre-launch values Post launch cal. (not operationally used) Vicarious calibration using RTM Inter-calibration using deep convective clouds (DCCs) 2010-09-24T02:30Z 2012-02-09T04:15Z 2012-10-24T22:00Z Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

MTSAT-2/Imager lunar calibration: dataset Absolute phase angle [deg] Full moon Low illumination 0 30 60 90 120 150 180 Manual extraction of lunar observations Predict the Moon position using JPL DE405 IR (10.8µm) image is used to find the Moon 62 of total 98 observations for the ROLO model (Jul. 2010-Dec.2013) Lunar observation: L1A equivalent data Converted to L1B equivalent DC/radiance (i.e., detector equalization using pre-launch values) Oversampling: 1.75 in E-W direction ( = IFOV:28µrad / sampling width: 16µrad ) Dark signal correction: N/A Computation of observables Same method used in the GIRO imagette processing Earth disk Positions of the Moon wrt. the centre of the Earth for MTSAT-2/Imager (Jul.2010 – Dec.2013) Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

ΔIrr (Calibration + Instrument drift) Difference between the observed Irradiance and the ROLO Irradiance (in %) Visible calibration coefficients for MTSAT-2/Imager Constant pre-launch values -> ΔIrr shows only instrument drift Time series of ΔIrr for MTSAT-2/Imager Hatch: 95% confidence interval of a linear regression line Δirr [%] Outliers Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Outliers caused by incorrect extraction of lunar observations Case #1 Case #2 Case #1: Careless extraction Incomplete lunar disk image Root cause of significant ΔIrr IR1 (10.8 µm) VIS Case #2: Reasonable extraction at a glance East portion of the Moon: behind the Earth Difficult to find out the Earth edge from VIS image during the night time IR1 (10.8 µm) VIS Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Calibration slope vs. the ROLO (on the relative scale) - A way to monitor the instrument drift and compare with other calibration results FPIX : Oversampling factor ΩPIX : Pixel solid angle [sr-1] Dci : Digital count of the Moon pixel OffDC : Averaged deep space DC NPIX : Number of the Moon pixels [W m-2 µm-1 DC-1] Lunar calibration Good agreements with RTM and DCC, the smallest uncertainty of a regression line Time series of MTSAT-2/Imager calibration slope difference (each method is rescaled at the first calibration result) Hatch: 95% confidence interval of a linear regression line Δslope [%] Annual drift [%/yr] DCC: 3.07 ± 0.16 Moon: 2.71 ± 0.15 RTM: 3.69 ± 0.62 Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

GMS-5/VISSR lunar calibration: general Spin stabilized GEO satellite Satellite position: from telemetry Located at ~ 140 E Instrument: VIS/IR optical imager 1 broad visible channel (similar to SEVIRI HRV) 1.25 km horizontal resolution at SSP 4 detectors for N-S direction 6-bit (64 digital counts) Scanning: E-W direction Hourly Full-disk observation The Moon acquisition NO maneuver, unscheduled 0-3 lunar observations / month Visible channel calibration Constant pre-launch values Post launch cal. (not operationally used) Vicarious calibration using RTM Inter-calibration using deep convective clouds (DCCs) Digital count Radiance GMS-5/VISSR VIS 1996-05-02T00:53:40Z Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Positions of the Moon wrt. the centre of the Earth for GMS-5/VISSR GMS-5/VISSR lunar calibration: dataset Absolute phase angle [deg] 2 18 34 50 66 82 98 Lunar observation: L1A equivalent data Conversion of DC to radiance/reflectivity Based on LUT, no calibration equation Equalized DC does not exist Radiance: derived using calibration coefficients for each detector Oversampling: 1.475 for E-W direction Dark signal correction: N/A 48 of total 50 useful lunar observations for the ROLO model (Jul. 1995-Feb. 2003) Computation of observables Radiance for the Moon masking Full moon Low illumination Pixel number Positions of the Moon wrt. the centre of the Earth for GMS-5/VISSR (Jul. 1995-Feb.2003) Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Digital counts handling in the GMS-5/VISSR lunar calibration Sanity check file Observed Irradiance: consistent, but not identical due to the Moon mask method Radiance for “User”, DC for “Imgt Processing” DC cannot be used because detectors are not equalized at count level Observed DC, DC Offset and Total number of pixels: NO meaning in GMS-5/VISSR GMS-5/VISSR VIS channel detector#2 signal-DC-reflectivity relationships (a) (b) (c) Reflectivity Reflectivity Detector signal [V] Digital count Detector signal [V] Digital count Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany (Figures: Hashimoto et al. 2008)

Phase angle dependence in ΔIrr Difference between the observed Irradiance and the ROLO Irradiance (in %) Clear phase angle dependence in ΔIrr may be caused by: Incorrect computation of IrrOBS Stray light effect, scan mirror angle dependence ROLO model … Time series of ΔIrr for GMS-5/VISSR Δirr [%] Δirr [%] The Moon phase angle [deg] Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Summary and future plans Lunar calibration using the GIRO application MTSAT-2/Imager 62 lunar observations (Jul. 2010 – Dec. 2013) Calibration trend (annual drift) : consistent with other calibration method in terms of the uncertainty GMS-5/VISSR 48 lunar observations (Jul. 1995 – Feb. 2003) Need for the further investigation (phase angle dependence, detector equalization, usage of detector signals instead of digital counts, etc.) Future plans Application of GIRO apps. to Himawari-8/AHI 6 VIS/NIR bands Combination of multiple calibration methods (DCC, desert, …) Will be discussed/developed within the GSCIS framework Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Thank you for your attention Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany

Correction of phase angle dependence w/o correction GIRO (w/ phase angle correction) ΔIrrCORR [%] g : the Moon phase angle [deg] ΔIrrCORR : ΔIrr w/ phase angle correction Drift: -0.58±0.11 [%/year] Δirr [%] Vicarious calibration using RTM and Terra/MODIS Drift: -0.52±0.28 [%/year] The Moon phase angle [deg] Good agreement in annual drift Uncertainty is still large Lunar Calibration Workshop, 1-4 December 2014, Darmstadt, Germany