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In-orbit Earth reflectance validation of TROPOMI on board the Sentinel-5 Precursor satellite

机译:在哨子-5前体卫星船上的轨道地球反射验证robomi

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The goal of the study described in this paper is to determine the accuracy of the radiometric calibration of the TROPOMI instrument in flight, using its Earth radiance and solar irradiance measurements, from which the Earth reflectance is determined. The Earth reflectances are compared to radiative transfer calculations. We restrict ourselves to clear-sky observations as these are less difficult to model than observations containing clouds and/or aerosols. The limiting factor in the radiative transfer calculations is then the knowledge of the surface reflectance. We use OMI and SCIAMACHY surface Lambertian-equivalent reflectivity (LER) information to model the reflectivity of the Earth's surface. This Lambertian, nondirectional description of the surface reflection contribution results in a relatively large source of uncertainty in the calculations. These errors can be reduced significantly by filtering out geometries for which we know that surface LER is a poor approximation of the real surface reflectivity. This filtering is done by comparing the OMI/SCIAMACHY surface LER information to MODIS surface BRDF information.
机译:本文描述的研究的目的是确定飞行中的Tropomi仪器的辐射校准的准确性,利用其地球光线和太阳辐照度测量,从中确定地球反射率。将地球反射与辐射转移计算进行比较。我们将自己限制在明确的天空观测中,因为这些观察比含有云和/或气溶胶的观察结果较小。辐射转移计算中的限制因素是表面反射率的知识。我们使用OMI和Sciamachy Super Lambertian - 等效反射率(LER)信息来模拟地球表面的反射率。该朗伯语,非透视图的表面反射贡献的描述导致计算中的相对大的不确定性源。通过过滤掉地几何形状可以显着减小这些误差,我们知道表面LER是真实表面反射率差的近似。通过将OMI / Sciamachy Surface Ler信息与Modis Surface BRDF信息进行比较来完成此过滤。

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