02.06.2013 Views

SMOS L2 OS ATBD - ARGANS

SMOS L2 OS ATBD - ARGANS

SMOS L2 OS ATBD - ARGANS

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

164<br />

ICM-CSIC<br />

LOCEAN/SA/CETP<br />

IFREMER<br />

Faraday<br />

rotation<br />

<br />

<strong>SM<strong>OS</strong></strong> <strong>L2</strong> <strong>OS</strong><br />

Algorithm Theoretical<br />

Baseline Document<br />

Doc: SO-TN-ARG-GS-0007<br />

Issue: 3 Rev: 9<br />

Date: 25 January 2013<br />

Page: 164<br />

that follows the conventions described in Earth Explorer CFI Software Mission Convention<br />

Document (Deimos), we introduce the mathematical expressions for the angles to be used in<br />

the transport from ground to antenna reference frames.<br />

Arc cossint sin g sing cost cos g<br />

Arc sin sin t cos <br />

g cost sin gsin g <br />

sin<br />

<br />

Arcsin costsin <br />

g sint cos g sing <br />

sin <br />

for –/2 ≤ g ≤ /2 :<br />

for /2 ≤ g ≤ 3/2: has to be replaced by and ψ by ψ<br />

We define the rotation angle a = ψ ω, being ω the Faraday rotation angle. Then,<br />

following ACRI Reqts_<strong>L2</strong>Draft-2.doc<br />

Dual polarization mode:<br />

Direct transformation from surface reference frame to antenna reference frame is

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!