SNPP VIIRS solar diffuser on-orbit change factor determination without the screens (Conference Presentation)

N. Lei, Q. Ji, X. Xiong
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Abstract

The Visible Infrared Imaging Radiometer Suite (VIIRS) aboard Suomi National Polar-orbiting Partnership satellite performs radiometric calibrations of its reflective solar bands through an onboard sunlit solar diffuser (SD). On orbit, the bidirectional reflectance distribution function of the SD changes over time. The change factor, known as the H-factor, is determined by an onboard solar diffuser stability monitor (SDSM) using the signal strength ratio determined by observing the Sun through an attenuation screen and the sunlit SD. The sunlight goes through another attenuation screen before striking the SD. The screen relative transmittances can be accurately characterized with on-orbit data, except for the regions where the solar azimuth angles are at or close to the extremes. It is unfortunate that over the initial orbits (< orbit 154) of the SNPP, the solar azimuth angle is at one of the extreme regions. Since there are no SDSM data over the initial orbits, the measured H-factors from late orbits are extrapolated to orbit zero to find a scale factor that yields, at orbit zero, the final H-factor of a value of one. The accuracy of the extrapolation depends on the quality of the transmittances of the screens. Due to inaccuracy of the transmittances over the initial orbits, the scale factor may not be accurate. Here, we use our previously developed technique to determine the H-factor without using the screen transmittances and thus are able to examine the accuracy of the scale factor and obtain the H-factor time change rate at early satellite orbits.
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SNPP VIIRS太阳扩散器在轨变化因子的测定(会议报告)
Suomi国家极轨伙伴关系卫星上的可见光红外成像辐射计套件(VIIRS)通过机载阳光漫射器(SD)对其反射太阳波段进行辐射校准。在轨道上,SD的双向反射率分布函数随时间变化。变化因子,称为h因子,由机载太阳能扩散器稳定性监测器(SDSM)确定,使用通过衰减屏幕和阳光照射的SD观察太阳确定的信号强度比。太阳光在照射到标清之前要经过另一个衰减屏。除了太阳方位角处于极值或接近极值的区域外,屏幕相对透射率可以用在轨数据精确表征。不幸的是,在SNPP的初始轨道(<轨道154)上,太阳方位角处于一个极端区域。由于没有初始轨道上的SDSM数据,从后期轨道测量的h因子被外推到轨道0,以找到一个比例因子,该比例因子在轨道0处产生最终值为1的h因子。外推的准确性取决于屏幕透射率的质量。由于初始轨道上的透射率不准确,比例因子可能不准确。在这里,我们使用我们之前开发的技术来确定h因子,而不使用屏幕透射率,从而能够检查比例因子的准确性,并获得早期卫星轨道上的h因子时间变化率。
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