DocumentCode :
838181
Title :
Polarization rotation and the third Stokes parameter: the effects of spacecraft attitude and Faraday rotation
Author :
Meissner, Thomas ; Wentz, Frank J.
Author_Institution :
Remote Sensing Syst., Santa Rosa, CA, USA
Volume :
44
Issue :
3
fYear :
2006
fDate :
3/1/2006 12:00:00 AM
Firstpage :
506
Lastpage :
515
Abstract :
The third Stokes parameter of ocean surface brightness temperatures measured by the WindSat instrument is sensitive to the rotation angle between the polarization vectors at the ocean surface and the instrument. This rotation angle depends on the spacecraft attitude (roll, pitch, yaw) as well as the Faraday rotation of the electromagnetic radiation passing through the Earth´s ionosphere. Analyzing the WindSat antenna temperatures, we find biases in the third Stokes parameter as function of the along-scan position of up to 1.5 K in all feedhorns. This points to a misspecification of the reported spacecraft attitude. A single attitude correction of -0.16° roll and 0.18° pitch for the whole instrument eliminates all the biases. We also study the effect of Faraday rotation at 10.7 GHz on the accuracy of the third Stokes parameter and the sea surface wind direction retrieval and demonstrate how this error can be corrected using values from the International Reference Ionosphere for the total electron content when computing Faraday rotation.
Keywords :
Faraday effect; artificial satellites; atmospheric radiation; oceanographic techniques; oceanography; remote sensing; wind; 10.7 GHz; Earth ionosphere; Faraday rotation; International Reference Ionosphere; WindSat antenna temperatures; WindSat instrument; electromagnetic radiation; ocean surface brightness temperatures; polarization rotation; polarization vectors; rotation angle; sea surface wind direction retrieval; spacecraft attitude; third Stokes parameter; total electron content; Brightness temperature; Instruments; Ionosphere; Ocean temperature; Polarization; Rotation measurement; Sea measurements; Sea surface; Space vehicles; Stokes parameters; Faraday rotation; Stokes vector; WindSat; spacecraft attitude;
fLanguage :
English
Journal_Title :
Geoscience and Remote Sensing, IEEE Transactions on
Publisher :
ieee
ISSN :
0196-2892
Type :
jour
DOI :
10.1109/TGRS.2005.858413
Filename :
1597458
Link To Document :
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