ANALYSIS OF COMS INFRARED CHANNEL AND VISIBLE CHANNEL CALIBRATION Dohyeong Kim, Ho-Seung Lee, Won-seok Lee, Sunmi Na and Tae-Hyeong Oh National Meteorological Satellite Center, Korea Meteorological Administration, Gwanghyewon-myeon, Jincheon-gun, Chungcheongbuk-do, Republic of Korea Abstract COMS (Communication, Ocean, and Meteorological Satellite), the first Korean geostationary th meteorological satellite, was launched on 27 June, 2010, and has been fully operating its own missions since the end of in-orbit test period in April 2011. The inter-calibration system using COMS for infrared radiation based on the GSICS (Global Spacebased Inter-Calibration System) Coordinate Center (GCC) Algorithm Theoretical Basis Document (ATBD). Reference instrument uses the hyperspectral Infrared Atmospheric Sounding Interferometer (IASI) on the low Earth orbit Metop-A satellite. In Infrared channels calibrations, the results from Apr. 2011 to Mar. 2012 showed that the averages of temperature difference between COMS and IASI are 0.37K for IR1(10.8μm), -0.46K for IR2(12.0μm), 0.27K for IR3(6.7μm) and -0.22K for IR4(3.7μm). KMA had developed vicarious calibration of visible channel using cloud-free ocean, cloud-free desert (Australian Simpson), water cloud top and Deep convective cloud(DCC) targets whose method was developed as part of COMS meteorological data processing system(CMDPS). The results from Sep. 2011 to Aug. 2012 showed that the average of reflectance difference between observed and simulated are -0.8% for ocean target, +0.3% for desert target, -4.4% for water cloud target, -10.7% for deep convective cloud target and the overall average shows about -4.0% for all targets. The slope trend of forced intercept to zero shows about 2% of visible channel degradation from Sep. 2011 to Aug. 2012. As one of visible-calibration methods, NMSC has observed moon twice a month and used this data for monitoring COMS visible channel degradation trend since Feb 2011. The observed moon data has been processed by Moon Processing system in NMSC’s IMPS(Image Processing Subsystem). In this Moon Processing system, the total irradiance of observed moon data is computed and compared with ROLO model value, which is Moon irradiance output model in USGS. The trend from this compared data shows nearly 3% of visible channel degradation from Feb 2011 to Aug 2012. INTRODUCTION COMS (Communication, Ocean, and Meteorological Satellite), the first Korean geostationary meteorological satellite, was launched on 27th June, 2010, and has been fully operating its own missions since the end of in-orbit test period in April 2011. COMS is stationed at an altitude of 36,000 km above the Earth’s equator and at a longitude of 128.2°. Even though COMS had been designed for having unform accuracy before launch, the performance of the meteorological imager have been changed by optical alignment and change of sensitivity, etc, during operation period. Meteorological Imager(MI) which is the meteorological instrument of COMS has 1 visible and 4 infrared channels. In infrared channel, the blackbody and calibration monitoring should be continuously conducted. The goal of the inter-calibration of infrared channel as a part of GSICS (Global Space-based Inter-Calibration System) is to ensure the comparability of satellite measurements provided at different time, by different instruments, and under the responsibility of different satellite operators. The basic premise of inter-calibration is that measurements by two instruments should be the same if they view the same target at the same time, with the same spectral response and viewing geometry, or any and all such differences have been properly accounted for. Consequently, inter-calibration requires a series of processes that collocate, transform, select, and analyze the measurements by two instruments to produce corrections that homogenize all the observations to a common reference (Wu and Yu 2011). KMA has checked the quality of infrared channels from Apr. 2011 to Mar. 2012. We used IASI level1C data for reference data. The light reached to satellite sensor are observed as DC values expressed with integer. For utilizing the observation values, the radiometric calibration, from which way the DC values are changed to radiance, is needed. The idealistic method for precise radiometric calibration is to ensure the indicator for radiometric calibration in satellite instrument. But, in case that the ensurance of black body is limited, the radiometric calibration can be conducted by outer value of satellite. By using the vicarious calibration, which is the way using the other satellite data having well-known properties or the corresponded theoritical radiance value with the observation point and time, the radiometric calibration can be conducted. In this study, we used radiative transfer modeling for ocean, desert, cloud and DCC (deep convective cloud) targets. DATA The meteorological mission and data service of COMS has begun since 1st April 2011. Normally COMS MI measurement has two different observation modes: Full Disk (FD) and Extended Northern Hemisphere (ENH). And COMS MI produces FD imagery every 3 hours and ENH imagery every 15 minutes. The COMS MI has one visible and four infrared channels.(Table 1) Channel Visible Shortwave IR (IR4) Water Vapor (IR3) IR1 IR2 Wavelength Center Range(㎛) 0.55~0.8 Wavelength(㎛) 0.67 3.5~4.0 3.7 4 6.5~7.0 6.7 4 10.3~11.3 10.8 11.5~12.5 12.0 Table 1 : Specification of MI channels. Spatial Resolution(km) 1 4 4 For inter-calibration of COMS infrared, reference instrument uses the hyperspectral Infrared Atmospheric Sounding Interferometer (IASI) on the low Earth orbit Metop-A satellite. IASI has been designed for operational meteorological soundings with a very high level of accuracy being devoted to improved medium range weather forecast. KMA has checked the quality of infrared channels from Apr. 2011 to Mar. 2012. For the vicarious calibration of the visible channel of COMS MI, ocean, desert, cloud targets and DCC (deep convective cloud) are used. NCEP total water vapor, NCEP wind speed and direction, OMI column ozone amount, MODIS aerosol optical thickness, and SeaWiFS monthly climatology are used as inputs for ocean target. NCEP total water vapor, OMI column ozone amount, and MODIS BRDF parameter are used as inputs for desert target. MODIS cloud products are used as inputs for water cloud and DCC target. In this analysis, we used the data during the period from Sep. 2011 to Aug. 2012. In Moon calibration, to compute the annual degradation of the COMS MI visible channel, it is assumed that several Moon views (typically once per month) are available, which fulfill the following geometric and radiometric conditions in order to integrate the full signal produced by the Moon : The Moon view used in this method is a global Moon image. KMA obtains the moon images by using LA(Local Area) observation mode which is Korean peninsula observation mode, one of the three COMS MI observation mode. This data have been obtained twice a month. In this paper, we used the data for Feb 2011 to Aug 2012. Figure 1 : The process of taking a moonmask There is no data in the Moon image from the Earth, the atmosphere, the Sun (no straylight) or any star whatsoever. For this, we take off the moonmask(only moon part of the image) of above image. The Sun must be far enough, i.e. the phase angle as seen from the Imager shall be less than 90 deg. METHOD The inter-calibration system using COMS for infrared radiation based on the GSICS Coordinate Center (GCC) Algorithm Theoretical Basis Document (ATBD). In order to verify infrared channel calibration, COMS and IASI data are selected if meet the collocation matching conditions. We checked three types of condition. First, to check difference of observation time, we verified that the observation time difference is within 5 minutes. Second, to check difference of SZA (Satellite zenith Angle), we selected pixels which less than threshold value using SZA data both COMS and IASI. This threshold value is defined as 0.01 in clear and 0.03 in cloudy weather condition that is correspond to a maximum 1% and 3% difference of SZA. The third is environment uniformity check. To reduce uncertainty between the observation conditions of two satellites due to temporal and spatial mismatches, only measurements over uniform scenes are selected. The collocated COMS and IASI data cannot be compared without considering the sensor’s spectral response difference. Therefore, IASI radiances are converted into a simulated COMS radiance according to the spectral responses of COMS infrared channels using constraint method. The method, called the constraint method, generates a super channel consisting of combination of the hyper channel to imitate a broadband channel. For IR4 band (shortwave IR), considering the solar radiance we used only the nighttime data. In order to calculate the simulated radiance of COMS using IASI data, we produce the super channel having a very similar spectral response to a broadband channel in the hyper channels within the spectral range of the broadband channel. And then we produce the weight of the super channels. So, we could calculate the radiance (𝐼𝑣 ) of super channel using by Eq. (1): (1) where 𝑊𝑖 is weight for IASI and 𝐼𝑖 is radiance of IASI and 𝑖 is channel index number of IASI. The spectral range of IASI data does not cover the spectral range of COMS SWIR channel data. So, radiances of gap channels estimated by using valid hyper channel observations and simulated radiances for 8 profiles (Tahara and Kato 2008). For the vicarious calibration of the visible channel of COMS MI, ocean, desert, cloud targets and DCC (deep convective cloud) are used. For the simulation of ocean and desert target, 6S (Second Simulation of the Satellite Signal in the Solar Spectrum) radiative transfer model is used. NCEP total water vapor, NCEP wind speed and direction, OMI column ozone amount, MODIS aerosol optical thickness, and SeaWiFS monthly climatology are used as inputs for ocean target. NCEP total water vapor, OMI column ozone amount, and MODIS BRDF parameter are used as inputs for desert target. For the simulation of water cloud and DCC, SBDART (Santa Barbara DISORT Atmospheric Radiative Transfer) radiative transfer model is used. MODIS cloud products are used as inputs for water cloud and DCC target. The Ocean targets that are homogeneous and dark should be considered only a clear pixel. In this case, it is affected by aerosol, because the surface reflectance is so small. Therefore, aerosol optical thickness has to be considered as an auxiliary data in radiative transfer modeling. In addition, it has the advantage that radiance can be calculated without BRDF (bidirectional reflectance distribution function) because the surface reflectance of the ocean is nearly homogeneous. In case of the cloud target, atmosphere and surface effects can be minimized in the simulation of TOA radiance due to strong reflection of cloud layer. And properties of cloud as an auxiliary data should be used in radiative transfer modeling. Thus, in case of the target with the ocean or the cloud, it has the disadvantage that has to match the COMS MI data with aerosol or cloud product data from other satellite (Ham and Sohn 2010). On the other hand, in case of the target of the desert, aerosol effect can be minimized in the simulation of radiance due to strong reflectance of desert and aerosol can assume the value of the climate in RTM. Since surface reflectance varies with the positions of the sun and satellite, the BRDF of target surface was required for radiative transfer calculation (Chun et al., 2012). The visible calibration using moon is based on the lunar database provided by the RObotic Lunar Observatory (ROLO) of USGS, that describes an empirical model of the lunar disk reflectance as a function of its phase angle (the angle between the Moon-Sun direction and Moon-Earth direction) and irrespective of the librations and the properties of the Moon surface. In order to monitor the degradation of the Imager visible channel, it is proposed to use a method based on the comparison between the global signal measured by the instrument and the model provided by ROLO. ROLO measurements have very good relative performances, i.e. from one measurement condition to another. The absolute accuracy is however not as good. Thus the best use of ROLO model is its application in a multi-temporal approach. With a long-term set of observations, relative visible response trending of the Imager have residuals about 0.1%. Then to monitor the behaviour of the instrument we define a quantity which depends only of the instrument response. The instrument state at a given time is used as a reference point; the Moon image is then used to monitor the instrument evolution with respect to this reference. P= Where • 𝐼𝑖𝑛𝑠𝑡𝑟𝑢𝑚𝑒𝑛𝑡 𝐼𝑟𝑒𝑓 𝐼𝑖𝑛𝑠𝑡𝑟𝑢𝑚𝑒𝑛𝑡 is the Moon irradiance as measured by the Imager 𝐼𝑟𝑒𝑓 is the Moon irradiance computed from the ROLO model, under the same conditions All Imager responses are linearly trended over the various Moon images with the ratio 𝑃(𝑡) expressed in percentage. 𝑘= RESULTS 𝑃(𝑡0 ) The results of infrared inter-calibration from Apr. 2011 to Mar. 2012 showed the averages of temperature difference between COMS and IASI are 0.4K for IR1(10.8μm), -0.4K for IR2(12.0μm), 0.3K for IR3(6.7μm) and -0.2K for IR4(3.7μm). For each channels, the difference between daytime bias and nighttime bias is less than 0.1K. IR1 is the largest difference only 0.06K. Overall, there is little difference between night and daytime. And COMS MI TB of all channels is correlated with IASI brightness temp within 0.5K in figure 2. For IR1 band, the difference in low TB around 200K is about 1.4K, while the difference in high TB around 290K decrease in 0.2K. Namely, In low range of TB below 250K, the TB of COMS data is higher than IASI. But the difference is smaller and to zero in high TB. On the other hand, for IR2 band, the difference between MI TB and IASI TB tend to negative bias. The difference in low TB around 200K is about 0.3K, while the difference in high TB around 290K decrease in -0.4K. For IR3, tendency of the bias is similar to IR1. For IR4, the difference TB is large in low TB, but the bias is small about -0.2K in figure 3. The difference between COMS and IASI brightness temperature shows positive bias for IR1, IR3 while negative bias for IR2, IR4. And for each channels, the slope of monthly variation is less than 0.01K/month in figure 4. Although there is a slight bias, infrared channels of COMS MI are correlated well with IASI data. Figure 2 : Scatter plots of observed brightness temperature for COMS versus the corresponding brightness temperature for IASI from Apr. 2011 to Mar. 2012. Figure 3 : Scatter plots of the difference between observed brightness temperature for COMS and brightness temperature for IASI from Apr. 2011 to Mar. 2012. Figure 4 : Time series of monthly mean bias to COMS and IASI brightness temperature from Apr. 2011 to Mar. 2012. The results of vicarious calibratoin from Sep. 2011 to Aug. 2012 showed that the average of reflectance difference between observed and simulated are -0.8% for ocean target, +0.3% for desert target, -4.4% for water cloud target, -10.7% for deep convective cloud target and the overall average showed about -4.0% in figure 5. Therefore, the difference in low reflectance around 0.05 between COMS reflectance and simulated reflectance is smaller and to zero. On the other hand, the difference in high reflectance around 1 tends to be larger about 10%. And the slope average of forced intercept to zero from Sep. 2011 to Aug. 2012 shows about 0.9 for all targets. The slope trend of forced intercept to zero shows about 2% of visible channel degradation from Sep. 2011 to Aug. 2012 in figure 6. For obtaining more precise result, we need more data through the long term observation. Figure 5 : Scatter plots of observed reflectance for COMS versus the corresponding simulated reflectance from Sep. 2011 to Aug. 2012 for all targets. Figure 6 : Time series of monthly slope from Sep. 2011 to Aug. 2012 for all targets The image responses graph of moon is shown in figure 7. This graph shows that the instrument irradiance is degraded to about maximum 7% compared with ROLO values. Especially, we can confirm degradation trend from Aug 2011 to Mar 2012 easily. But, in the results from Jun 2012 to Aug 2012, visible channel performance looks like improved. These phenomena are found in two point, about Jun 2011 and Jun 2012. So, we assume that there is some seasonal effect in this period. In advance, we have a plan to research whether this phenomena is truly related with seasonal effect. If this is not related this, we are confirming whether any other problems with our methods and calculations on the way of applying these methods are exist or not. The regression line from image responses is shown in figure 7. From this regression line, there is about 3.0345% visible channel degradation in total period of observing moon (Feb 2011 ~ Aug 2012). Even though some data are contrary to overall trend in Jun 2011 and Jun 2012, visible channel has some degradation patterns in total period. Since the number of moon observation is normally twice a month. Total number of data is only 36. Therefore, for obtaining more precise result and confirming the accuracy of data, more data and long term observation are needed. Figure 7 : Image responses(left) and trend(right) from Feb 2011 to Aug 2012 SUMMARY For confirming the radiometric performance of COMS, National Meteorological Satellite Center(NMSC/KMA) has own infrared-calibration system using Metop-IASI data and visible-calibration system using ocean, desert, water cloud, deep convective clouds and moon data. In Infrared channels calibrations, COMS MI IR channels have low-bias within 0.5K accuracy. IR1 and IR3 of difference between COMS TB and IASI TB showed positive bias while IR2 and IR4 showed negative bias. Bias of COMS visible channel can be obtained by using ocean, desert and cloud targets. In vicarious calibration of the visible channel, COMS visible channel underestimates about 4%. The slope average shows about 0.9 for all targets. And the slope trend shows about 2% of visible channel degradation. COMS MI visible channel degradation for Feb 2011 to Aug 2012 is shown about 3% from the regression line of monthly moon data. But, some data are contrary to overall trend in Jun 2011 and Jun 2012. Although there is a slight bias, infrared and visible channels match up well with reference data. KMA has been doing research on calibration of visible and IR channels through the long term observation. REFERENCES Chun, H. W., B. J. Sohn, D. H. Kim, M. H. Ahn, M. L. Ou, (2012) Solar channel calibration using desert targets in Australia: application to the MTSAT-1R Visible Sensor. Journal of the Meteorological Society of Japan, 90,191-205. COMS.TN.00116.DP.T.ASTR.COMS MI Radiometric Model.p.30-41. Ham, S.-H., and B. J. Sohn, (2010) Assessment of the calibration performance of satellite visible channel using cloud targets: application to meteosat-8/9 and MTSAT-1R. Atoms. Chem. Phys., 10, 11131-11149 Tahara, Y., and K. Kato, (2008) Spectral Adjustment for Intercalibration between Broadband Sensor and High Spectral Resolution Sounder. Japan Meteorological Agency Technical Note. Wu, X., and F. Yu, (2011) GSICS algorithm theoretical basis document (ATBD) for GOES-AIRS/IASI inter-calibration.
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