2005
DOI: 10.1117/12.623965
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HIRDLS proto-flight model radiometric calibration from pre-launch calibration data

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Cited by 3 publications
(3 citation statements)
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“…By clever design of the facility and use of remote actuators, it was only necessary to open the vacuum chamber once, and the complete calibration, including some preliminary data evaluation, took place in less than 3 months. All the requirements on the radiometric, spectral and spatial calibration were met [ Eden et al , 2003a, 2003b, 2005a, 2005b; Moorhouse et al , 2003; T. D. Eden et al, Radiometric calibration of the HIRDLS flight instrument from pre‐launch calibration data, manuscript in preparation, 2008a].…”
Section: Instrument Overviewmentioning
confidence: 99%
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“…By clever design of the facility and use of remote actuators, it was only necessary to open the vacuum chamber once, and the complete calibration, including some preliminary data evaluation, took place in less than 3 months. All the requirements on the radiometric, spectral and spatial calibration were met [ Eden et al , 2003a, 2003b, 2005a, 2005b; Moorhouse et al , 2003; T. D. Eden et al, Radiometric calibration of the HIRDLS flight instrument from pre‐launch calibration data, manuscript in preparation, 2008a].…”
Section: Instrument Overviewmentioning
confidence: 99%
“…Once a minute the scan mirror was to be turned to view the IFC by way of the IFC mirror; the difference between this and the offset measurement leads to the gain. To convert the measured signals to radiances, it is necessary to apply the calibration equation [ Eden et al , 2005b] where S are the measured signals, with subscripts 0 and IFC indicating views to space and the IFC, whose blackbody radiance is B IFC , and k is the quadratic term determined during calibration.…”
Section: Algorithms For the Recovery Of Radiometric Datamentioning
confidence: 99%
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