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Polarization rotation and the third Stokes parameter: the effects of spacecraft attitude and Faraday rotation

机译:极化旋转和第三个斯托克斯参数:航天器姿态和法拉第旋转的影响

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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/spl deg/ roll and 0.18/spl deg/ 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.
机译:WindSat仪器测量的海洋表面亮度温度的第三个Stokes参数对海洋表面和仪器的极化矢量之间的旋转角度敏感。该旋转角度取决于航天器的姿态(侧倾,俯仰,偏航)以及穿过地球电离层的电磁辐射的法拉第旋转。分析WindSat天线温度,我们发现在所有馈电喇叭中,第三个Stokes参数中的偏差与沿扫描位置的最大1.5 K有关。这表明所报告的航天器姿态有误。整个仪器的-0.16 / spl deg / roll和0.18 / spl deg / pitch的单个姿态校正消除了所有偏差。我们还研究了10.7 GHz的法拉第旋转对第三个斯托克斯参数和海面风向反演精度的影响,并演示了如何在计算法拉第旋转时使用国际参考电离层中总电子含量的值来校正此误差。 。

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