Earth Observing Systems XXIV 2019
DOI: 10.1117/12.2529776
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The Operational Land Imager-2: prelaunch spectral characterization

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Cited by 10 publications
(6 citation statements)
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“…The Landsat 9 OLI onboard radiometric calibration system is identical to that of Landsat 8 OLI, and the various subsystems include a shutter for dark measurements, two solar diffusers (working and pristine), two stimulation lamp assemblies, and the ability to view the moon through a spacecraft maneuver [2,5]. As with the Landsat 8 OLI, the Landsat 9 OLI underwent a rigorous pre-launch calibration and characterization process [6][7][8][9][10].…”
Section: Bandmentioning
confidence: 99%
“…The Landsat 9 OLI onboard radiometric calibration system is identical to that of Landsat 8 OLI, and the various subsystems include a shutter for dark measurements, two solar diffusers (working and pristine), two stimulation lamp assemblies, and the ability to view the moon through a spacecraft maneuver [2,5]. As with the Landsat 8 OLI, the Landsat 9 OLI underwent a rigorous pre-launch calibration and characterization process [6][7][8][9][10].…”
Section: Bandmentioning
confidence: 99%
“…The total uncertainty is provided in Figure 3. This section will describe the improvement in select elements of the uncertainty budget since the test of the Landsat Operational Land Imager-2 in 2018 [11,12].…”
Section: Uncertaintymentioning
confidence: 99%
“…Radiometric sources used are typically SI‐traceable FEL lamps with a 10 or more cm aperture integrating sphere. It is possible to combine radiometric and spectral responses during characterization using a tunable laser reference (Ahtee et al., 2007), such as spectral irradiance and radiance responsivity calibrations using uniform sources (SIRCUS) (Brown et al., 2006) or Traveling SIRCUS (T‐SIRCUS) or the Goddard Laser for Absolute Measurement of Radiance systems (Angal et al., 2016; Barsi et al., 2019). This combined radiometric and spectral response is called the absolute spectral response (Barnes et al., 2015).…”
Section: Pre‐launch Characterization and Calibrationmentioning
confidence: 99%