Infrared Atmospheric Sounding Interferometer IASI on METOP On-Ground Calibration of the FM2 Instrument International TOVS Study Conference 25-31, May 2005 Beijing China D. Blumstein1, B.Tournier2, T.Carlier1, T.Maciaszek1, T.Phulpin1, G.Chalon1, P.Astruc3, D.Miras3, D.Siméoni3 (1) Centre National d'Etudes Spatiales (CNES), Toulouse, France (2) NOVELTIS, Toulouse, France (3) ALCATEL SPACE, Cannes, France ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 1 Outline Key Performance specifications On-ground characterization of IASI FM2 ¾ First IASI instrument in flight (on METOP 2) IASI Program Status ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 2 Key performances specifications Radiometric sensitivity ¾ Apodized and non-apodized spectra Radiometric accuracy ¾ Absolute accuracy ¾ Relative accuracy (at a given time) Between pixels, channels, viewing direction ¾ Stability Spectral & geometry ¾ Spectral calibration ¾ Spectral response function ¾ Point Spread Function ( & interband registration) ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 3 Measured radiometric sensitivity AVM result — IASI FM2 Noise Spectrum (NedT at 280 K) — Session SM0410060647 — CBS 91.7 K IASI FM2 testing in vacuum non apodized (293 K scene) 1,0 Loss of transmission : 1.5 % at 850 cm-1 over a period of 6 days Equivalent to the absorption by a 40 nm thin film of water ice B1 0,8 0,7 NedT at 280 K (K) ¾ Detectors temperature 91.7 K ¾ Measured on blackbody ¾ No evolution of noise (ice cont.) 0,9 0,6 B2 B3 NeDT in K (at 280 K) 0,5 0,4 0,3 0,2 0,1 0,0 64500 82500 100500 118500 136500 154500 172500 190500 208500 226500 Wavenumber (m^-1) Measurement SM0410111609 — Pixel 3 Mission radiometric performance in NeDT — T_CBS=91,7 K — (IASI FM2 OV Test) apodized + pseudo-noise 1.0 0,8 0.9 Noise Spectrum in NedT at 280 K after drift correction - P4 - c10693_avm_SM0410060647 Effect of scene temperature on B3 noise (scene at 240 & 280 K) Noise Spectrum in NedT at 280 K after drift correction - P1 - c10693_avm_SM0410060647 Noise Spectrum in NedT at 280 K after drift correction - P3 - c10693_avm_SM0410060647 NedT at 280 K Noise Spectrum in NedT at 280 K after drift correction - P2 - c10693_avm_SM0410060647 NedT at 280 K measurements 0,7 0.8 0,6 NeDT at 280 K (K) NeDT at 280 K (K) 0.7 0.6 0.5 0.4 0,5 0,4 0,3 0.3 0,2 0.2 0,1 0.1 0.0 645 845 1045 1245 1445 1645 1845 Wavenumber (cm-1) Spécification ITSC-14 – Beijing, 25-31May. 2005 FM2 (Delta-QR) 2045 2245 0,0 1900 1950 2000 2050 2100 2150 2200 2250 2300 2350 Wavenumber (cm-1) 240 K 280 K spec D. Blumstein – CNES DCT/PO/EV 4 2400 Measured radiometric accuracy (1/4) Session SM 06 22h59 — T_HBB about 299 K, no Non-Linearity correction 300,2 IASI FM2 testing in vacuum 300,0 299,6 B1 299,4 299,2 299,0 298,8 Session SM 06 22h59 — T_HBB around 299 K, Non-Linearity correction applied 300,2 Pixel 1 300,0 298,6 298,4 298,2 645 Result valid for other incidences ¾ Post-calibration done by Level 1 proc. to achieve "differential" requirements Pixel 2 Pixel 3 Pixel 4 2045 2245 299,8 845 1045 1245 1445 1645 299,6 Wave numbers (cm-1) NL (B1) corrected Brigthness temperature (K) ¾ Need for NL correction in B1 band ¾ DT < 0.25 K ¾ Target in nadir position Brigthness temperature (K) 299,8 1845 299,4 299,2 299,0 298,8 298,6 Between pixels, scan views or channels Pixel 1 Pixel 2 1645 1845 Pixel 3 Pixel 4 2045 2245 298,4 298,2 645 845 1045 1245 1445 Wave numbers (cm-1) Tscene : 220 – 300 K Pixel 1, Nominal Conf., Cold Case 0 .5 0 .4 H B B c o a t i n g e m i s s iv it y l o s s 0 .2 B B C c o a t i n g e m i s s i v i t y lo s s 0 .1 0 -0 .1 -0 .2 -0 .3 -0 .4 300 K 294 K 280 K 260 K 0 .4 0 .3 B B C c o a t i n g e m is s i v it y l o s s H B B c o a t i n g e m i s s iv i t y lo s s 0 .2 0 .1 0 - 0 .1 - 0 .2 - 0 .3 - 0 .4 300 294 280 260 240 240 K 220 K -0 .5 64500 0 .5 Radiometric Calibration Error in NedT at 280 K (K) Radiometric Calibration Error in NedT at 280 K (K) 0 .3 Tscene : 240 – 300 K Pixel 1, Redundant Conf., Hot Case 114500 164500 W a v e N u m b e r (m ^ -1 ) ITSC-14 – Beijing, 25-31May. 2005 214500 264500 - 0 .5 64500 114500 164500 214500 264500 W a v e N u m b e r (m ^ -1 ) D. Blumstein – CNES DCT/PO/EV 5 Measured radiometric accuracy (2/4) Raw measurements versus model comparison Pixel 1 Nominal Conf. Cold Case 0 .5 0 .4 H B B c o a tin g e m is s iv ity lo s s 0 .2 B B C c o a tin g e m is s iv ity lo s s 0 .1 0 -0 .1 Radiometric Calibration Error Model — Nominal configuration, Cold Case T_env HBB = 280 K, T_env BBC = 275 K, T_env CBB = 230 K -0 .2 -0 .3 -0 .4 300 K 294 K 280 K 260 K 0.5 240 K 220 K -0 .5 64500 0.4 114500 164500 214500 W a v e N u m b e r (m ^ -1 ) 264500 0.3 DT at 280 K (Kelvin) Radiometric Calibration Error in NedT at 280 K (K) 0 .3 0.2 0.1 0.0 645 -0.1 1145 1645 2145 2645 -0.2 -0.3 -0.4 -0.5 Wave Number (cm-1) 220 K ITSC-14 – Beijing, 25-31May. 2005 240 K 260 K 280 K 294 K 300 K D. Blumstein – CNES DCT/PO/EV 6 Measured radiometric accuracy (3/4) Raw measurements versus model comparison Pixel 1 Redundant Conf Hot Case 0 .5 0 .3 B B C c o a tin g e m is s iv ity lo s s H B B c o a t in g e m is s iv it y lo s s 0 .2 0 .1 0 -0 .1 Radiometric Calibration Error Model — Redundant configuration, Hot Case T_env HBB = 295 K, T_env BBC = 285 K, T_env CBB = 230 K -0 .2 -0 .3 -0 .4 300 294 0.5 280 260 0.4 240 -0 .5 64500 114500 0.3 164500 W a v e N u m b e r (m ^ -1 ) 214500 DT at 280 K (Kelvin) Radiometric Calibration Error in NedT at 280 K (K) 0 .4 264500 0.2 0.1 0.0 645 -0.1 1145 1645 2145 2645 -0.2 -0.3 -0.4 -0.5 Wave Number (cm-1) 240 K ITSC-14 – Beijing, 25-31May. 2005 260 K 280 K 294 K 300 K D. Blumstein – CNES DCT/PO/EV 7 Measured radiometric accuracy (4/4) More in-depth verifications performed during the test ¾ Scan angle effect verified ¾ Interpixel & interscan calibration ¾ Sensitivity to thermal drifts Simulation of Entry/Exit of eclipse Mission Objectives on radiometric calibration are expected to be achieved in orbit ¾ Absolute Calibration Error : < 0.5 K ¾ Intercalibration error at a given time : < 0.2 K All geophysical conditions 4 pixels, all viewing directions, all channels ¾ Intercalibration error over time : < 0.3 K Short term (orbital period) Long term ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 8 Measured Spectral Response Function IASI PFM testing in vacuum B1 ISRF (944 cm-1) ¾ 2 laser beams (B1:CO2, B3:HF/DF) 4,0 Field and Aperture illuminated 3,0 Resolution (FWHM) compliant (w. margins) ISRF Model accuracy achieved ISRF Model input are precisely measured • Instrument Point Spread Function • Interferometric axis and shear • Corner Cube trajectory Measured P1 Model P1 0,03 Normalised to Surface ¾ ISRF measured on +/- 16 cm-1 (+) 3,5 2,5 0,02 0,01 0,00 2,0 -15,0 -14,5 -14,0 -13,5 -13,0 -0,01 -0,02 1,5 -0,03 -0,04 1,0 0,5 0,0 -0,5 -1,0 -16,00 -12,00 -8,00 -4,00 0,00 4,00 8,00 12,00 16,00 Wave numbers (cm-1) B3 ISRF (2655 cm-1) 3,0 2,5 Measured P1 0,20 Model P1 0,15 Normalised to Surface 2,0 0,10 0,05 0,010 1,5 0,00 0,005 0,000 -15,0 -14,5 -14,0 -13,5 -0,05 -13,0 -4 -2 0 2 4 -0,005 -0,10 -0,010 1,0 -0,15 -0,015 -0,020 -0,20 -0,025 0,5 0,0 -0,5 -16,00 -12,00 -8,00 -4,00 0,00 4,00 8,00 12,00 16,00 Wave numbers (cm-1) ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 9 Measured Spatial Response Function Point Spread Function (IPSF) measured for the 3 IASI bands Interband registration verified ¾ Integrated absolute difference < 0.03 12 km FOV (at nadir) ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 10 Spectral Performances (1/3) First assessment done on few parameters ¾ Dν/ν with respect to nominal instrument ¾ Spectral resolution (Full Width at Half Maximum) At 944 cm-1 (B1) and 2655 cm-1 (B3) ¾ Shape error index Epsilon2 = variations of the ISRF Absolute difference between average and instantaneous Summed over +/- 16 cm-1 Band 1 Dν/ν FWHM Epsilon2 P1 -1 cm cd0 cd1 Band 3 Dν/ν FWHM Epsilon2 ITSC-14 – Beijing, 25-31May. 2005 0.32 0.014 0.015 P1 -1 cm cd0 cd1 0.43 0.020 0.020 P2 P3 -5 1 10 0.32 0.32 0.014 0.010 0.013 0.009 P2 P3 -5 1 10 0.40 0.43 0.025 0.015 0.023 0.011 P4 0.32 0.011 0.012 Specification -4 2 10 0.35 0.026 P4 -4 2 10 0.42 0.019 0.014 0.48 0.042 D. Blumstein – CNES DCT/PO/EV 11 Spectral Performances (2/3) Spectral stability over 80 sec. Spec = 1.10-6 ¾ Standard deviation of the position of the quadratic barycentre of the ISRF Band 1 cd0 cd1 P1 8.27E-08 7.66E-08 P2 8.30E-08 7.46E-08 P3 7.70E-08 4.79E-08 P4 7.36E-08 8.08E-08 Band 3 cd0 cd1 P1 1.67E-08 1.58E-08 P2 2.29E-08 2.55E-08 P3 2.36E-08 2.09E-08 P4 1.66E-08 1.49E-08 + very good long term stability between measurement sessions ¾ Observed Dν/ν (average of the 4 pixels) < 1.10-6 ¾ Hot Case / Cold Case ¾ 14 days between first and last measurements ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 12 Spectral Performances (3/3) Shape error index 1 Spec b1 < 0.02, Spec b3 < 0.05 ¾ ISRF knowledge errors ¾ Shape_index_1 = Σ( abs( Isrf_Model(n) – Isrf_Average(n) ) * dn ) Ghost has to be removed from the averaged ISRF (computation on 13 cm-1) Band 1 +/- 13 cm +/- 16 cm cd0 cd1 cd0 cd1 P1 0.025 0.029 0.034 0.034 P2 0.023 0.023 0.031 0.028 P3 0.023 0.021 0.026 0.023 P4 0.023 0.022 0.027 0.024 cd0 cd1 cd0 cd1 P1 0.029 0.032 0.043 0.039 P2 0.042 0.046 0.053 0.056 P3 0.026 0.019 0.030 0.021 P4 0.049 0.050 0.056 0.053 Band 3 +/- 13 cm +/- 16 cm ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 13 Summary Excellent performances measured on 2nd IASI model (FM2) ¾ The instrument ran flawlessly for the 3 weeks of test ¾ Design modifications decided after PFM testing (ice contamination) successfully implemented on FM2 & FM3 • PFM model will be refurbished to benefit from these modifications ¾ Big investment put into the on-ground calibration (human & financial) ¾ Excellent stability of the instrument (spectral & radiometric) ¾ Spectral Response Function of the instrument • Accurately measured at 2 wavenumbers (use of 2 laser beams for test) • Model accuracy verified at these 2 wavenumbers ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 14 IASI Project Status : instruments (1/2) FM2 ¾ On-ground calibration completed (TVAC test in October 2004) ¾ Integration & tests on METOP 2 completed ¾ Launch planned April 2006 FM3 ¾ Subsystem Integration & Test completed ¾ Thermal Vacuum Test planned in October 2005 PFM ¾ ¾ ¾ ¾ Instrument TVAC test in June 2003 METOP Payload TVAC test in February 2004 Now dismounted from METOP 2 Detectors refurbishment planned end of year 2005 ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 15 IASI Project Status : system (2/2) OPS software (Level 1 processing) ¾ Delivered by CNES to EUMETSAT : Sept. 2004 ¾ Now integrated & tested in CGS ¾ Delivered to METEO FRANCE for integration in direct readout software TEC (IASI Technical Expertise Center) ¾ Acceptance test completed : Feb. 2005 ¾ NRT terminal installed. First tests completed ¾ TEC ready for system level testing with EPS/CGS Participation of IASI Instrument team to EPS system level tests with METOP 2 (SSVT4a, May 2005) In-flight commissioning preparation ¾ Instrument on-orbit Verification Plan completed ¾ Level 1 Cal/Val Plan completed (see poster B20), implementation on-going ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 16 Aknowledgements The authors would like to express their thanks to the many people involved in the development, integration and test of the IASI instruments either in the industry, in the space agencies or in the universities for their efforts which made IASI a reality. A special thought goes to F.R.Cayla who has been so involved with IASI project since the beginning and is still very close from us in spite of his retirement four years ago. ITSC-14 – Beijing, 25-31May. 2005 D. Blumstein – CNES DCT/PO/EV 17