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(ATBD) SMAP Level 1 Radar Data Products - NASA

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61<br />

12.2.2 Radiometric Accuracy Validation<br />

Radiometric accuracy validation can be divided into the reduction of short-term<br />

variability coming from the instrument, and vicarious calibration against external<br />

reference targets. Short term variations of transmit power and receiver gain are<br />

expected due primarily to temperature variations. Pre-launch models based on the<br />

loopback data will be constructed and implemented in the calibration preprocessor<br />

to supply the L1B and L1C processors with time varying calibration coefficients.<br />

During the L1 cal/val period, the performance of the loopback calibration modelling<br />

will be validated by plotting the loopback measurements and the output σ 0 results<br />

with and without the loopback correction against time and temperature.<br />

Vicarious calibration will be handled by collecting and averaging data in the<br />

L1B and L1C processors over stable calibration target areas such as the Amazon,<br />

the oceans, and the ice sheets. Assuming that these data are stable, they can be<br />

used to track longer term trends in system performance, and to catch other issues<br />

such as biases between polarization channels, antenna pointing knowledge errors,<br />

RFI, and Faraday rotation effects. Comparisons with Aquarius and PALSAR-2 data<br />

(if available) and other instruments will be useful to separate instrument variations<br />

from possible scene variations.<br />

12.2.3 Geolocation Validation<br />

Final verification of geolocation will be performed post-launch by looking at highcontrast<br />

features with known locations. Coastlines and shorelines should work well<br />

and are widely available. Some natural or man-made point-like targets may also<br />

work. Specific candidate targets should be identified prior to launch. It may be<br />

beneficial to conduct this validation with the high resolution single look image data.<br />

13 Acknowledgments<br />

This work was performed at the Jet Propulsion Laboratory, California Institute of<br />

Technology, under contract with the National Aeronautics and Space Administration.

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