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S-NPP VIIRS thermal band spectral radiance performance through 18 months of operation on-orbit

机译:S-NPP VIIRS热带光谱辐射性能通过18个月的轨道操作

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The Suomi National Polar-orbiting Partnership (S-NPP) satellite, carrying the first Visible Infrared Imager Radiometer Suite (VIIRS) was successfully launched on October 28, 2011 with first light on November 21, 2011. The passive cryo-radiator cooler doors were opened on January 18, 2012 allowing the cold focal planes (S/MWIR and LWIR) to cool to the nominal operating temperature of 80K. After an early on-orbit functional checkout period, an intensive Cal/Val (ICV) phase has been underway. During the ICV, the VIIRS SDR performance for thermal emissive bands (TEB) has been under evaluation using on-orbit comparisons between VIIRS and the CrIS instrument on S-NPP, as well as VIIRS and the IASI instrument on MetOp-A. CrIS has spectral coverage of VIIRS bands M13, M15, M16, and I5 while IASI covers all VIIRS TEB. These comparisons largely verify that VIIRS TEB SDR are performing within or nearly within pre-launch requirements across the full dynamic range of these VIIRS bands, with the possible exception of warm scenes (<280 K) in band M12 as suggested by VIIRS-IASI comparisons. The comparisons with CrIS also indicate that the VIIRS Half Angle Mirror (HAM) reflectance versus scan (RVS) is well-characterized by virtue that the VIIRS-CrIS differences show little or no dependence on scan angle. The VIIRS-IASI and VIIRS-CrIS findings closely agree for bands M13, M15, and M16 for warm scenes but small offsets exist at cold scenes for M15, M16, and particularly M13. IASI comparisons also show that spectral out-of-band influence on the VIIRS SDR is >0.05 K for all bands across the full dynamic range with the exception of very cold scenes in Band M13 where the OOB influence reaches 0.10 K. TEB performance, outside of small adjustments to the SDR algorithm and supporting look-up tables, has been very stable through 18 months on-orbit. Preliminary analysis from an S-NPP underflight using a NASA ER-2 aircraft with the SHIS instrument (NIST-traceable source) confirms TEB SDR accuracy as compliant for a typical warm earth scene (285-290 K).
机译:2011年10月28日成功推出了载有第一个可见红外成像仪透射仪套件(VIIRS)的苏米国家极性轨道伙伴关系(S-NPP)卫星(VIIRS)。2011年11月21日,第一盏灯成功推出。被动冷冻机冷却器2012年1月18日开业,允许冷焦平面(S / MWIR和LWIR)冷却到标称工作温度为80k。在轨道早期的轨道功能结账期之后,正在进行密集的CAL / VAL(ICV)阶段。在ICV期间,在S-NPP上的VIIR和CRIC仪器之间的轨道比较以及viirs和Metop-a上的IASI仪器,VIIRS SDRS SDR性能(TEB)的性能已经在评估中进行了评估。 Ciss具有Viirs带M13,M15,M16和I5的光谱覆盖,而IASI涵盖所有VIIR TEB。这些比较在很大程度上验证了VIIRS TEB SDR在这些VIIRS频段的完整动态范围内在预发射要求内或几乎在发布前的要求内,如VIIRS-IASI比较所建议的频带M12中的温暖场景(<280 k)的可能性发生。与Cris的比较也表明Viirs半角镜(火腿)反射率与扫描(RVS)是众所周知的,因为Viirs-Cris差异显示很少或没有对扫描角度的依赖性。 VIIRS-IASI和VIIRS-CRICS-CRIC调查结果非常同意温暖场景的频带M13,M15和M16,但在M15,M16,特别是M13的冷场上存在小的偏移。 IASI比较还表明,在整个动态范围内的所有频段,VIIRS SDR上的频谱外频谱影响为0.05 k,除了频段M13中的非常冷的场景,OOB影响达到0.10 K. TEB性能,外面对SDR算法的小调整和支持查找表,通过18个月在轨道上非常稳定。使用NASA ER-2飞机与SHIS仪器(NIST可追溯源)使用NASA ER-2飞机的初步分析证实了TEB SDR精度,符合典型的温暖地球场景(285-290 k)。

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