首页> 外文会议>Conference on sensors, systems, and next-generation satellites >Ground through on-orbit transfer of the International Temperature Scale of 1990 (ITS-90): radiometeric scale using the CERES thermistor bolometers and built-in flight calibration systems
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Ground through on-orbit transfer of the International Temperature Scale of 1990 (ITS-90): radiometeric scale using the CERES thermistor bolometers and built-in flight calibration systems

机译:通过1990年国际温度等级的轨道转移(IT-90):使用CERES热敏电阻钻头和内置飞行校准系统的辐射计

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The Clouds and Earth's Radiant Energy System (CERES thermistor bolometers were calibrated using filtered radiances, characterized on an International Temperature Scale of 1990 (ITS-90) derived absolute radiometric scale. Longwave filtered radiances were characterized using the optical and geometric surface properties of the reference Narrow-Field-of-View Blackbody (NFBB), the NFBB temperature measurements from the ITS-90 calibrated platinum resistance thermometers (PRT) embedded in the blackbodies, and the spectral responses of the CERES bolometers. Shortwave filtered radiances were characterized using the cryogenically-cooled Transfer Active Cavity Radiometer (TACR) which was an ITS-90 transfer standard, and using the spectral responses of the bolometers. In ground vacuum facilities, the ITS-90, temperature-based radiometric scale was transferred to the CERES bolometers. As ITS-90 transfer standards, the bolometers were used to characterize the emitted filtered radiances from in-flight systems: (1) the internal calibration module (ICM) which consisted of anodized aluminum blackbodies and tungsten lamp sources; and (2) mirror attenuator mosaic (MAM) which was an aluminum solar diffuser plate, built into the bolometer instrumentation. From the ground $LB@October 1995$RB through the on-orbit phases $LB@December 1998 -July 1999$RB of the Tropical Rainfall Measuring Mission (TRMM) Spacecraft CERES instrument mission, the stabilities of the bolometer's responses were assessed from periodical observations of the in-flight calibration systems radiances. Each CERES instrument package consisted of broadband shortwave $LB@0.3 micrometer to 5.0 micrometer$RB@, broadband total $LB@0.3 micrometer to greater than 100 micrometer$RB@, and narrowband window $LB@8 micrometer and 12 micrometer$RB@, scanning thermistor bolometer sensor units; and of in-flight calibration systems. Between the ground and initial on-orbit calibrations, the TRMM CERES bolometers and the built-in, flight calibration system sources maintained their filtered radiance measurement ties to ITS-90 at the plus or minus 0.2 Wm$+$MIN@2$/sr$+$MIN@1$/ precision level. On-orbit calibration studies indicate that the radiance measurements were stable at the plus or minus 0.2 Wm$+$MIN@2$/sr$+$MIN@1$/ precision level. The ground and on- orbit calibration results are presented and discussed.
机译:云和地球的辐射能量系统(CERES热敏电阻钻孔仪使用过滤的辐射校准,其特征在于1990年的国际温度等级(其-90)衍生的绝对辐射尺度。使用参考的光学和几何表面特性表征了长波滤波的辐射狭窄的视场黑体(NFBB),来自其-90校准的铂电阻温度计(PRT)的NFBB温度测量,以及CERES钻孔仪的光谱响应。短波滤波的辐射使用低温进行了表征-cooled激活传送腔辐射仪(TACR),它是一个ITS-90传输标准,并且使用辐射热测量计的光谱响应。在接地的真空设备中,ITS-90,基于温度的辐射规模转移至测辐射热计CERES作为其-90转移标准,钻孔器用于表征来自牵伸的发出的滤波的辐射T Systems:(1)由阳极氧化铝黑码和钨灯源组成的内部校准模块(ICM); (2)镜像衰减器马赛克(MAM)是铝制太阳能漫射板,内置于鼓声机仪表中。从地面$ LB @ 10月1995年10月通过On-Orbit阶段$ LB @ 12月1998年12月 - 799 $ RB热带降雨测量使命(TRMM)宇宙飞船CERES仪器使命,评估钻头的响应的稳定性来自期刊飞行中校准系统的观察。每个CERES仪器包装由宽带短波超过5.03微米$ 5.0微米$ RB @,宽带总量超过100微米$ RB @,窄带窗口$ LB @ 8微米和12微米$ RB @ ,扫描热敏电阻电压计传感器单元;和飞行中的校准系统。在地面和初始轨道校准之间,TRMM CERES钻孔器和内置的飞行校准系统源将其过滤的辐射测量与其-90的滤波过辐射测量与0.2 WM $ + $ MIN @ 2 $ / SR保持过滤$ + $ min @ 1 $ /精确级别。在轨道校准研究表明,辐射测量在加号0.2 WM $ + $ MIN @ 2 $ / SR $ + $ MIN @ 1 $ /精度级别。提出和讨论了地面和轨道校准结果。

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