Space based calibration transfer spectroradiometer
A Space-based Calibration Transfer Spectroradiometer (SCATS) instrument that establishes a maintainable SI traceable radiometric calibration on-orbit with long-term stability accuracy, such as is required for long term climate monitoring missions, is provided. The SCATS instrument includes sensors that directly measure the highly stable solar irradiance and/or the lunar irradiance, and the Earth radiance through an invariant instrumental optical path. This common path measurement concept eliminates uncertainties associated with the calibration and degradation of intervening solar attenuation elements that represent the current state of the art. The SCATS instrument can be used to calibration of hyperspectral and multi-spectral sensors operating from the ultra-violet to long wave infrared. A suitable selection of detectors and filters enables this wide wavelength application.
1. A method for providing calibration information, comprising:
scanning a field of view of an instrument in orbit around the Earth over at least one of the solar disk and the lunar disk, wherein the instrument includes at least one sensor;
measuring an irradiance signal obtained by scanning the field of view of the instrument over at least one of the solar disk and the lunar disk;
slewing the field of view of the instrument to the Earth;
scanning the field of view of the instrument over a selected area of the Earth;
measuring a radiance signal obtained by scanning the field of view of the instrument over the selected area of the Earth;
obtaining a calibration coefficient by calculating a ratio of an integrated signal obtained by scanning the field of view of the instrument over the selected area of the Earth to an integrated signal obtained by scanning the field of view of the instrument over the at least one of the solar disk and the lunar disk.
2. The method of claim 1 , further comprising:
scanning the field of view of the instrument over the solar disk at a first scan rate;
storing the irradiance signal obtained by scanning the field of view of the instrument over the solar disk;
scanning the field of view of the instrument over the selected area of the Earth at a second scan rate, wherein obtaining a calibration coefficient includes calculating a ratio of the radiance signal obtained by scanning the field of view of the instrument over the selected area of the Earth to the irradiance signal obtained by scanning the field of view of the instrument over the solar disk.
3. The method of claim 1 , further comprising:
scanning the field of view of the instrument over the solar disk at a first scan rate;
storing the irradiance signal obtained by scanning the field of view of the instrument over the solar disk;
scanning the field of view of the instrument over the lunar disk at a second scan rate;
storing the irradiance signal obtained by scanning the field of view of the instrument over the lunar disk;
scanning the field of view of the instrument over the selected area of the Earth at a third scan rate,
wherein obtaining a calibration coefficient includes:
calculating a ratio of the radiance signal obtained by scanning the field of view of the instrument over the selected area of the Earth to the irradiance signal obtained by scanning the field of view of the instrument over the solar disk to obtain a first calibration coefficient, and
calculating a ratio of the radiance signal obtained by scanning the field of view of the instrument over the selected area of the Earth to the irradiance signal obtained by scanning the field of view of the instrument over the lunar disk to obtain a second calibration coefficient.
4. The method of claim 1 , wherein scanning the field of view of the instrument includes rotating a sensor head of the instrument to scan the field of view of the sensor within a scan plane.
5. The method of claim 4 , wherein the sensor head of the instrument includes a plurality of sensors.
6. The method of claim 5 , wherein the plurality of sensors are sensitive to different optical wavelengths.
7. The method of claim 5 , wherein each of the plurality of sensors provides a linear output over an operative dynamic range of the sensor.