首页> 外文会议>SPIE Conference on Earth Observing Systems >On-orbit solar calibrations using the Clouds and Earth's Radiant Energy System (CERES) in-flight calibration system
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On-orbit solar calibrations using the Clouds and Earth's Radiant Energy System (CERES) in-flight calibration system

机译:使用云和地球辐射能量系统(CERES)在飞行中校准系统的轨道太阳校准

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The Clouds and Earth's Radiant Energy System (CERES) scanning thermistor bolometers measure earth-reflected solar and earth-emitted longwaveradiances, at the top- of-the-atmosphere. The bolometers measure the earthradiances in the broadband shortwave solar (0.3-5.0 microns) and total (0.3->100 microns) spectral bands as well as in the 8->12 microns water vapor window spectral band over geographical footprints as small as 10 kilometers at nadir. December 1999, the second and third set of CERES bolometers was launchedon the Earth Observing Mission Terra Spacecraft. May 2003, the fourth and fifth set of bolometers was launched on the Earth Observing Mission Aqua Spacecraft. Ground vacuum calibrations define the initial count conversion coefficients that are used to convert the bolometer output voltages into filtered earth radiances. The mirror attenuator mosaic (MAM), a solar diffuser plate, was built into the CERES instrument package calibration system in order to define in-orbit shifts or drifts in the sensor responses. The shortwave and shortwave part of total sensors are calibrated using the solar radiances reflected from the MAM's. Each MAM consists of baffle-solar diffuser plate systems, which guide incoming solar radiances into the instrument fields of view of the shortwave and total wave sensor units. The MAM diffuser reflecting type surface consists of an array of spherical aluminum mirror segments, which are separated by a Merck Black A absorbing surface, overcoated with SIOx. Thermistors are located in each MAM plate and the total channel baffle. The CERES MAM is designed to yield calibration precisions approaching .5 percent for the total and shortwave detectors. However, in their first year of operation the Terra and Aqua MAMs showed shifts in their calibrations larger than expected. Shifts of tfis nature have been seen in other Solar viewing instruments in the past. A possible explanation has attributed the changes to pre-orbit or on-orbit contamination combined with solar ultraviolet/atomic oxygen induced chemical changes to the contaminant during solar exposure. In the subsequent year of operation all instruments begin to stabilize within the .5 percent precision range. In this presentation, the MAM solar calibration procedures will be presented along with on-orbit measurements for the nine years the CERES instruments have been on-orbit. A switch to an azimuth rotation raster scan of the Sun rather than an elevation scan will be discussed. The implementation of a thermal correction to the shortwave channel will also be discussed. Comparisons are also made between the Terra CERES instruments and the Aqua instruments during their MAM solar calibrations and total solar irradiance experimental results to determine how precise the CERES solar calibration facilities are at tracking the sun's irradiance.
机译:云和地球的辐射能量系统(CERES)扫描热敏电阻钻头测量在大气层的顶部 - 反射的地球反射的太阳能和地球发射的龙墙等。钻头测量宽带短波太阳能(0.3-5.0微米)和总(0.3-> 100微米)光谱带以及在8-> 12微米水蒸气窗口谱段中的地理占地面积小于10公里的地域在Nadir。 1999年12月,第二组和第三组CERES钻孔徒被启动地球观察Mission Terra Spacofraft。 2003年5月,第四组和第五组钻孔机在地球上观察了Mission Aqua SpaceCraft。地面真空校准定义了用于将鼓阀输出电压转换为过滤的地球辐射的初始计数转换系数。镜衰减器马赛克(MAM),太阳能漫射板,内置于CERES仪器包校准系统中,以便在传感器响应中定义轨道移位或漂移。总传感器的短波和短波部分使用从MAM的太阳面校准。每个MAM都包括挡板 - 太阳漫射板系统,该板系统引导到短波和总波传感器单元的仪器视野中的进入的太阳辐射。 MAM扩散器反射类型表面由一组球形铝镜段组成,该铝膜段由Merck黑色A吸收表面分开,用SiOx过涂。热敏电阻位于每个MAM板和总通道挡板。 CERES MAM旨在产生总和短波检测器的校准精度.5%。但是,在他们的第一年的运作中,Terra和Aqua Mams在校准中显示出大于预期的转变。在过去的其他太阳能观景仪器中看到了TFIS自然的转变。可能的解释归因于在太阳曝光期间与太阳紫外/原子氧诱导的污染物结合的轨道前或轨道污染的变化。在随后的操作年份,所有乐器都开始稳定在.5%的精度范围内。在本演示文献中,MAM太阳能校准程序将随着九年的轨道测量而呈现,CERES仪器已经在轨道上。将讨论转换到太阳的方位角旋转光栅扫描而不是高程扫描。还将讨论对短波通道的热校正的实现。在MAM太阳能校准期间,在Terra Ceres仪器和Aqua仪器之间也进行了比较,并确定了CERES太阳能校准设施在跟踪太阳辐照方面的精确度。

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