NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Polarization Rotation and the Third Stokes Parameter: The Effects of Spacecraft Attitude and Faraday RotationThe 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 -0.16deg roll and 0.18deg 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.
Document ID
20090001331
Acquisition Source
Headquarters
Document Type
Reprint (Version printed in journal)
Authors
Meissner, Thomas
(Remote Sensing Systems, Inc. Santa Rosa, CA, United States)
Wentz, Frank J.
(Remote Sensing Systems, Inc. Santa Rosa, CA, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2006
Publication Information
Publication: IEEE Transactions on Geoscience and Remote Sensing
Publisher: Institute of Electrical and Electronics Engineers
Volume: 44
Issue: 3
Subject Category
Geosciences (General)
Funding Number(s)
CONTRACT_GRANT: NNH06CC29C
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available