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<!DOCTYPE article PUBLIC "-//NLM//DTD Journal Publishing with OASIS Tables v3.0 20080202//EN" "journalpub-oasis3.dtd">
<article xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:oasis="http://docs.oasis-open.org/ns/oasis-exchange/table" xml:lang="en" dtd-version="3.0"><?xmltex \makeatother\@nolinetrue\makeatletter?>
  <front>
    <journal-meta><journal-id journal-id-type="publisher">AMT</journal-id><journal-title-group>
    <journal-title>Atmospheric Measurement Techniques</journal-title>
    <abbrev-journal-title abbrev-type="publisher">AMT</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Atmos. Meas. Tech.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">1867-8548</issn><publisher>
    <publisher-name>Copernicus Publications</publisher-name>
    <publisher-loc>Göttingen, Germany</publisher-loc>
  </publisher></journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.5194/amt-12-3573-2019</article-id><title-group><article-title>A generalized simulation capability for rotating- <?xmltex \hack{\break}?>beam scatterometers</article-title><alt-title>A generalized simulation capability for rotating-beam scatterometers</alt-title>
      </title-group><?xmltex \runningtitle{A generalized simulation capability for rotating-beam scatterometers}?><?xmltex \runningauthor{Z.~Li et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes">
          <name><surname>Li</surname><given-names>Zhen</given-names></name>
          <email>li@knmi.nl</email>
        </contrib>
        <contrib contrib-type="author" corresp="no">
          <name><surname>Stoffelen</surname><given-names>Ad</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-4018-4073</ext-link></contrib>
        <contrib contrib-type="author" corresp="no">
          <name><surname>Verhoef</surname><given-names>Anton</given-names></name>
          
        </contrib>
        <aff id="aff1"><institution>R&amp;D Satellite Observation, Royal Netherlands Meteorological
Institute, de Bilt, 3731 GA, the Netherlands</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Zhen Li (li@knmi.nl)</corresp></author-notes><pub-date><day>4</day><month>July</month><year>2019</year></pub-date>
      
      <volume>12</volume>
      <issue>7</issue>
      <fpage>3573</fpage><lpage>3594</lpage>
      <history>
        <date date-type="received"><day>12</day><month>July</month><year>2018</year></date>
           <date date-type="rev-request"><day>30</day><month>November</month><year>2018</year></date>
           <date date-type="rev-recd"><day>12</day><month>June</month><year>2019</year></date>
           <date date-type="accepted"><day>13</day><month>June</month><year>2019</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2019 Zhen Li et al.</copyright-statement>
        <copyright-year>2019</copyright-year>
      <license license-type="open-access"><license-p>This work is licensed under the Creative Commons Attribution 4.0 International License. To view a copy of this licence, visit <ext-link ext-link-type="uri" xlink:href="https://creativecommons.org/licenses/by/4.0/">https://creativecommons.org/licenses/by/4.0/</ext-link></license-p></license></permissions><self-uri xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019.html">This article is available from https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019.html</self-uri><self-uri xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019.pdf</self-uri>
      <abstract><title>Abstract</title>
    <p id="d1e97">Rotating-beam wind scatterometers exist in two types: rotating
fan-beam and rotating pencil-beam. In our study, a generic simulation frame
is established and verified to assess the wind retrieval skill of the three
different scatterometers: SCAT on CFOSAT (China France Oceanography SATellite), WindRad (Chinese Wind Radar) on FY-3E, and SeaWinds on
QuikSCAT. Besides the comparison of the so-called first rank solution
retrieval skill of the input wind field, other figures of merit (FoMs) are
applied to statistically characterize the associated wind retrieval
performance from three aspects: wind vector root mean square error,
ambiguity susceptibility, and wind biases. The evaluation shows that,
overall, the wind retrieval quality of the three instruments can be ranked
from high to low as WindRad, SCAT, and SeaWinds, where the wind retrieval
quality strongly depends on the wind vector cell (WVC) location across the
swath. Usually, the higher the number of views, the better the wind
retrieval, but the effect of increasing the number of views reaches
saturation, considering the fact that the wind retrieval quality at the
nadir and sweet swath parts stays relatively similar for SCAT and WindRad.
On the other hand, the wind retrieval performance in the outer swath of
WindRad is improved substantially as compared to SCAT due to the increased
number of views. The results may be generally explained by the different
incidence angle ranges of SCAT and WindRad, mainly affecting azimuth
diversity around nadir and number of views in the outer swath. This
simulation frame can be used for optimizing the Bayesian wind retrieval
algorithm, in particular to avoid biases around nadir but also to
investigate resolution and accuracy through incorporating and analyzing the
spatial response functions of the simulated Level-1B data for each WVC.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d1e109">The wind scatterometer has been proven to be a powerful instrument for
global sea surface wind measurement. The wind retrievals have a wide variety
of applications, including nowcasting and assimilation in numerical
weather prediction models, as well as oceanography, climate research, and
offshore energy applications
(Offiler,
1984; Naderi et al., 1991; Stoffelen and Anderson, 1997; Portabella, 2002;
Bajo et al., 2017). The wind retrieval is achieved by inverting a set of
radar cross-section measurements (<inline-formula><mml:math id="M1" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>) at different
geometries (incidence and/or azimuth look angles) over a wind vector cell
(WVC) through a geophysical model function (GMF) to extract the wind. The
more diversity in the geometry, the better wind retrieval will be achieved
(Portabella, 2002).</p>
      <p id="d1e123">Currently, there are two types of scatterometer in orbit: multiple fixed
fan-beam and rotating pencil-beam instruments. The first wind scatterometer
in space was the SEASAT-A Scatterometer System (SASS) on SEASAT-A launched
in June 1978 by NASA with four fixed fan beams and dual co-polarization (VV
and HH) Ku-band (13.2 <inline-formula><mml:math id="M2" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula>) emitting and receiving antennas, which failed in
October 1978 (Offiler, 1984). The term “views” in this paper
means measurements of the surface <inline-formula><mml:math id="M3" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> at different azimuth angle
and/or incidence angle and/or polarizations, and each surface <inline-formula><mml:math id="M4" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>
measurement is aggregated from the samples with the same polarization and
similar azimuth and incidence angle. The geometric diversity of the views is
able to improve the wind retrieval accuracy. “Views” is different from the
term “looks” in radar, which is defined as the equivalent number of
independent samples in a particular <inline-formula><mml:math id="M5" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> measurement and specifies
the measurement variance (Ulaby and Long, 2013). This
scatterometer had two views only per wind vector cell (WVC), a VV view and
an HH view, which turned<?pagebreak page3574?> out to be insufficient to resolve the wind direction
unambiguously well. The ERS-1 and ERS-2 satellites carried a scatterometer on board
as of 1991 three fixed fan beams and vertical co-polarization (VV) at C-band
frequency (5.4 <inline-formula><mml:math id="M6" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula>), with all beams pointing to the right-hand side of the
satellite. After ERS-1 and ERS-2, the NASA Scatterometer (NSCAT) was launched in
1996 on the Japanese Advanced Earth Observing Satellite (ADEOS-I). It had
six fan beams with VV capability on the fore and after beams and both VV
and horizontal (HH) co-polarization on the mid beams
(Naderi et al., 1991). The European Space
Agency (ESA) developed the Advanced Scatterometer (ASCAT) on the Metop
satellite series, which has six C-band VV fan beams, three of each pointing to the
left and right of the swath, and it started to provide data in 2006
(Gelsthorpe et al., 2000). The ERS-1 and ERS-2, NSCAT, and ASCAT
instruments all use three independent views per WVC, leading to a reduced
wind direction ambiguity as compared to SASS, by sampling the main
second harmonic wind direction dependency of the geophysical model function
(GMF) well
(Stoffelen
and Anderson, 1997; Stoffelen and Portabella, 2006). SeaWinds, the first
rotating pencil-beam scatterometer, was developed by NASA and launched on
QuikSCAT (1999), on the Japanese satellite ADEOS-2 (2003), and flew as
RapidScat on the International Space Station in 2014. It has two Ku-band
rotating pencil beams measuring VV and HH, respectively, at two fixed
incidence angles (Hoffman and Leidner, 2005). All current and
prior rotating pencil-beam scatterometers are similar in design concept to
SeaWinds and differ primarily in the incidence angles used. The OSCAT
scatterometer on OceanSat-2 is a Ku-band rotating pencil-beam instrument
similar to SeaWinds and developed by the Indian Space Research Organization
(ISRO). It was launched in 2009 and failed in 2014 (Singh et
al., 2012). After that, ISRO launched SCATSat-1 in 2016 as an OceanSat-2
replacement mission with the same scatterometer design, and OceanSat-3 will
be launched in 2020. China launched its first Ku-band rotating pencil-beam
scatterometer on board HY-2A in 2011, and it is still currently in operation (Jiang et al., 2012). SeaWinds-class rotating pencil-beam
scatterometers are able to obtain four independent views per WVC in the
inner swath but only two independent views per WVC in the outer swath,
where only vertically polarized views are available. This will impose
similar ambiguity problems as in the SASS design.</p>
      <p id="d1e175">A new type of scatterometer – the Rotating Fan-beam SCATterometer (RFSCAT) – in the Ku band was proposed in 2000 (Lin et al.,
2000b). It combines the features from fixed fan-beam and rotating
pencil-beam scatterometers, which provide large swath coverage and increase
the diversity in the observation geometry. The scatterometer (referred to as
SCAT from now on) on board CFOSAT (China France Oceanography SATellite) and
WindRad (Chinese Wind Radar on FY-3E) belong to this type of scatterometer,
and CFOSAT was launched on 29 October 2018, while WindRad is
planned to be launched in 2019 (Dou et al., 2014). These
represent a rotating fan-beam instrument with Ku band only (SCAT), a
rotating fan-beam instrument with both Ku and C band (WindRad), and a
rotating pencil-beam instrument with Ku band only (SeaWinds).</p>
      <p id="d1e178">The aim of our study is to build a generic simulation system and construct
an evaluation frame, particularly fit for the above rotating-beam
scatterometers, including Ku-band and C-band types. The simulation system includes
the complete simulation of satellite orbital movement, Level-1B (L1B) data
generation, Level-2A (L2A) data generation, and Level-2B (L2B) wind
retrieval. The three different rotating-beam scatterometers are expected to
perform differently, due to their varying observation geometry and
nonlinear wind retrieval characteristics, e.g., wind direction ambiguity.
The wind retrieval results are carefully evaluated and compared. The
advantages and disadvantages are analyzed such that they can be used as
a design reference.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Simulation method</title>
<sec id="Ch1.S2.SS1">
  <label>2.1</label><title>CFOSAT, WindRad, and SeaWinds characteristics</title>
      <p id="d1e196">The RFSCAT characteristics have been studied and assessed by Lin et al. (2000a, 2002).
The slowly rotating fan beam sweeps over the swath and the different views
overlap in each WVC, which leads to multiple views in a given WVC (Fig. 1). Contrary to the fixed fan-beam and rotating pencil-beam instruments, the
number of views in a WVC depends on its location and varies across the swath
as a function of the rotating speed. The scanning geometry results in a
smaller number of views and less azimuth diversity in the outer and the
nadir parts of the swath, which lead to a degraded wind retrieval
performance. In contrast, the other region of the swath (named the sweet
swath) has a better wind retrieval performance than the outer and nadir
swath.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><?xmltex \currentcnt{1}?><label>Figure 1</label><caption><p id="d1e201">Rotating fan-beam scatterometer. <bold>(a)</bold> SCAT
(Lin et al., 2000a). <bold>(b)</bold> WindRad
(Dou et al., 2014).</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f01.png"/>

        </fig>

      <p id="d1e216">SCAT and WindRad are both rotating fan-beam designs, but they have somewhat
different characteristics. They both follow the RFSCAT principles, but SCAT
has two fan beams operating in the Ku band with VV and HH respectively, whereas
WindRad has four fan beams. Two of these beams are operating in the Ku band at
VV and HH respectively, while the other two are operating at VV and HH in the C band. All the antennas transmit and receive pulses in turns (see the
illustrations in Fig. 1). The main parameters for
simulating SCAT and WindRad are listed in Tables 1
and 2.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1"><?xmltex \currentcnt{1}?><label>Table 1</label><caption><p id="d1e223">Main parameters of CFOSAT SCAT.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="2">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="justify" colwidth="56.905512pt"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Parameters</oasis:entry>
         <oasis:entry colname="col2">Value</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Orbit height</oasis:entry>
         <oasis:entry colname="col2">514 <inline-formula><mml:math id="M7" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Swath</oasis:entry>
         <oasis:entry colname="col2">1000 <inline-formula><mml:math id="M8" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Footprint</oasis:entry>
         <oasis:entry colname="col2">280 <inline-formula><mml:math id="M9" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Satellite speed</oasis:entry>
         <oasis:entry colname="col2">7.1 <inline-formula><mml:math id="M10" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna rotating speed</oasis:entry>
         <oasis:entry colname="col2">3.5 rpm</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Polarization</oasis:entry>
         <oasis:entry colname="col2">VV and HH alternating</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Incidence angle range</oasis:entry>
         <oasis:entry colname="col2">25–48<inline-formula><mml:math id="M11" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna pointing angle</oasis:entry>
         <oasis:entry colname="col2">40<inline-formula><mml:math id="M12" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak transmit power</oasis:entry>
         <oasis:entry colname="col2">120 <inline-formula><mml:math id="M13" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">W</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">WVC resolution</oasis:entry>
         <oasis:entry colname="col2">25 <inline-formula><mml:math id="M14" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Center frequency</oasis:entry>
         <oasis:entry colname="col2">13.256 <inline-formula><mml:math id="M15" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula> (Ku band)</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of transmit pulse</oasis:entry>
         <oasis:entry colname="col2">1.3 <inline-formula><mml:math id="M16" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of receiving pulse</oasis:entry>
         <oasis:entry colname="col2">2.7 <inline-formula><mml:math id="M17" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Pulse repetition frequency (PRF)</oasis:entry>
         <oasis:entry colname="col2">75 <inline-formula><mml:math id="M18" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">Hz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Two-way <inline-formula><mml:math id="M19" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M20" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula> beam width (azimuth)</oasis:entry>
         <oasis:entry colname="col2">1.28<inline-formula><mml:math id="M21" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak antenna gain</oasis:entry>
         <oasis:entry colname="col2">30 <inline-formula><mml:math id="M22" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Transmit bandwidth</oasis:entry>
         <oasis:entry colname="col2">0.5 <inline-formula><mml:math id="M23" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MHz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

<?xmltex \floatpos{p}?><table-wrap id="Ch1.T2"><?xmltex \currentcnt{2}?><label>Table 2</label><caption><p id="d1e544">Main parameters of FY-3E WindRad.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="justify" colwidth="85.358268pt"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:colspec colnum="3" colname="col3" align="left"/>
     <oasis:thead>
       <oasis:row>
         <oasis:entry colname="col1">Parameters</oasis:entry>
         <oasis:entry rowsep="1" namest="col2" nameend="col3" align="center">Value </oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">Ku band</oasis:entry>
         <oasis:entry colname="col3">C band</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Orbit height</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">836 <inline-formula><mml:math id="M24" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Swath</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">1400 <inline-formula><mml:math id="M25" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Footprint</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">200 <inline-formula><mml:math id="M26" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Satellite speed</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">7.4 <inline-formula><mml:math id="M27" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna rotating speed</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">3.0 rpm </oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Polarization</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">VV and HH alternating </oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Incidence angle range</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">34.7–44.5<inline-formula><mml:math id="M28" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna pointing angle</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">34.8<inline-formula><mml:math id="M29" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">WVC resolution</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">25 <inline-formula><mml:math id="M30" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak transmit power</oasis:entry>
         <oasis:entry colname="col2">120 <inline-formula><mml:math id="M31" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">W</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">100 <inline-formula><mml:math id="M32" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">W</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Center frequency</oasis:entry>
         <oasis:entry colname="col2">13.256 <inline-formula><mml:math id="M33" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">5.4 <inline-formula><mml:math id="M34" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of transmit <?xmltex \hack{\newline}?>pulse</oasis:entry>
         <oasis:entry colname="col2">1.8 <inline-formula><mml:math id="M35" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">1.7 <inline-formula><mml:math id="M36" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of receiving <?xmltex \hack{\newline}?>pulse</oasis:entry>
         <oasis:entry colname="col2">1.25 <inline-formula><mml:math id="M37" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">1 <inline-formula><mml:math id="M38" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Pulse repetition <?xmltex \hack{\newline}?>frequency (PRF)</oasis:entry>
         <oasis:entry colname="col2">208 <inline-formula><mml:math id="M39" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">Hz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">104 <inline-formula><mml:math id="M40" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">Hz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Two-way <inline-formula><mml:math id="M41" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M42" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula> <?xmltex \hack{\newline}?>azimuth beam width</oasis:entry>
         <oasis:entry colname="col2">1.3<inline-formula><mml:math id="M43" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">0.52<inline-formula><mml:math id="M44" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak antenna gain</oasis:entry>
         <oasis:entry colname="col2">37 <inline-formula><mml:math id="M45" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">32 <inline-formula><mml:math id="M46" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Transmit bandwidth</oasis:entry>
         <oasis:entry namest="col2" nameend="col3" align="center">0.6 <inline-formula><mml:math id="M47" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MHz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p id="d1e953">Rotating pencil-beam scatterometers have been flying on board several satellites
as described in the Introduction. SeaWinds is taken as representative for
the rotating pencil-beam design in our study. It has one dish antenna of
about 1 <inline-formula><mml:math id="M48" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> diameter with a VV and HH beam conically scanning at a speed of 18 rpm, which is much faster than the rotating fan beam
(Fig. 2). The VV beam has a higher incidence
angle than the HH beam, resulting in a wider VV swath. There are four
integrated views produced at all WVCs, for those<?pagebreak page3575?> located in the inner swath
by segregating both VV and HH and fore and aft views. The four views in the
outer swath that are used in the retrieval are all VV views, also divided
into fore and aft views but each split in two azimuth groups. The
main parameters of the SeaWinds instrument are listed in
Table 3.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><?xmltex \currentcnt{2}?><label>Figure 2</label><caption><p id="d1e966">Rotating pencil-beam scatterometer.</p></caption>
          <?xmltex \igopts{width=199.169291pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f02.png"/>

        </fig>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T3"><?xmltex \currentcnt{3}?><label>Table 3</label><caption><p id="d1e979">Main parameters of QuikSCAT SeaWinds.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="2">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="justify" colwidth="56.905512pt"/>
     <oasis:thead>
       <oasis:row>
         <oasis:entry colname="col1">Parameters</oasis:entry>
         <oasis:entry colname="col2">Value (inner and</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">outer beam)</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Orbit height</oasis:entry>
         <oasis:entry colname="col2">800 <inline-formula><mml:math id="M49" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Swath</oasis:entry>
         <oasis:entry colname="col2">1800 <inline-formula><mml:math id="M50" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Footprint</oasis:entry>
         <oasis:entry colname="col2">36 <inline-formula><mml:math id="M51" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Satellite speed</oasis:entry>
         <oasis:entry colname="col2">7.0 <inline-formula><mml:math id="M52" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna rotating speed</oasis:entry>
         <oasis:entry colname="col2">18 rpm</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Polarization</oasis:entry>
         <oasis:entry colname="col2">VV and HH</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Incidence angle range</oasis:entry>
         <oasis:entry colname="col2">51.8 and 46.7<inline-formula><mml:math id="M53" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Antenna pointing angle</oasis:entry>
         <oasis:entry colname="col2">44.9 and 38.9<inline-formula><mml:math id="M54" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak transmit power</oasis:entry>
         <oasis:entry colname="col2">120 <inline-formula><mml:math id="M55" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">W</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">WVC resolution</oasis:entry>
         <oasis:entry colname="col2">25/12.5 <inline-formula><mml:math id="M56" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Center frequency</oasis:entry>
         <oasis:entry colname="col2">13.256 <inline-formula><mml:math id="M57" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">GHz</mml:mi></mml:mrow></mml:math></inline-formula> (Ku band)</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of transmit pulse</oasis:entry>
         <oasis:entry colname="col2">1.5 <inline-formula><mml:math id="M58" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Duration of receiving pulse</oasis:entry>
         <oasis:entry colname="col2">2.1 <inline-formula><mml:math id="M59" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ms</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Pulse Repetition Frequency (PRF)</oasis:entry>
         <oasis:entry colname="col2">96 <inline-formula><mml:math id="M60" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">Hz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Two-way <inline-formula><mml:math id="M61" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M62" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula> beam width (azimuth)</oasis:entry>
         <oasis:entry colname="col2">1.8<inline-formula><mml:math id="M63" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Peak antenna gain</oasis:entry>
         <oasis:entry colname="col2">38 <inline-formula><mml:math id="M64" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">dB</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Transmit bandwidth</oasis:entry>
         <oasis:entry colname="col2">0.375 <inline-formula><mml:math id="M65" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MHz</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <?pagebreak page3576?><p id="d1e1305">NESZ (noise equivalent sigma-zero) is a range of values depending on the
specific slice position within the antenna footprint on the ground.
Figures 3, 4, and
5 give the NESZ distribution as a function of
the slice number for SCAT, WindRad, and SeaWinds.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><?xmltex \currentcnt{3}?><label>Figure 3</label><caption><p id="d1e1310">SCAT NESZ distribution as a function of slice number. <bold>(a)</bold> Ku-band
HH polarization. <bold>(b)</bold> Ku-band VV polarization.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f03.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><label>Figure 4</label><caption><p id="d1e1327">WindRad NESZ distribution as a function of slice number. <bold>(a)</bold> Ku-band HH polarization. <bold>(b)</bold> Ku-band VV polarization.
<bold>(c)</bold> C-band HH polarization. <bold>(d)</bold> C-band VV polarization.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f04.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><?xmltex \currentcnt{5}?><label>Figure 5</label><caption><p id="d1e1351">SeaWinds NESZ distribution as a function of slice number. <bold>(a)</bold> Ku-band HH polarization. <bold>(b)</bold> Ku-band VV polarization.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f05.png"/>

        </fig>

</sec>
<sec id="Ch1.S2.SS2">
  <label>2.2</label><title>Simulation procedure</title>
      <p id="d1e1374">The simulation is designed to be generic and able to adapt to all of the
current rotating-beam wind scatterometers, i.e., both pencil-beam and fan-beam types. It consists of four components: (1) generate satellite state vectors
by the orbit propagator SGP4 (Simplified perturbation models)
(Hoots and Roehrich, 1980); (2) simulate L1B data; (3) assign the L1B data onto the proper WVCs; (4) aggregate L1B data in one WVC
into views (L2A data). The work flowcharts are shown in
Figs. 6 and 7. We
use ECMWF model wind as the input wind field to initialize the L1B simulation,
which provides a spatially smooth ocean wind truth. In order to simplify the
simulation procedure, the pulse is cut into equal-size slices. To represent
the sampling of local wind variability (turbulence), geophysical noise is
added by disturbing the input wind components <inline-formula><mml:math id="M66" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M67" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> assigned on each slice
by injecting Gaussian distributed noise. Together with the instrument
configurations and satellite state vectors, the observation geometries on
slice level are calculated. The instrument noise Kpc (Long et
al., 2004) is estimated by
<inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:msup><mml:mtext>Kpc</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mi>A</mml:mi><mml:mo>+</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mi>B</mml:mi><mml:mtext>SNR</mml:mtext></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mi>C</mml:mi><mml:mrow><mml:msup><mml:mtext>SNR</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></inline-formula>. However, the coefficients <inline-formula><mml:math id="M69" display="inline"><mml:mi>A</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M70" display="inline"><mml:mi>B</mml:mi></mml:math></inline-formula>, and <inline-formula><mml:math id="M71" display="inline"><mml:mi>C</mml:mi></mml:math></inline-formula> need onboard processing details,
which are not the same nor available for all scatterometers. In order to
make the simulator generic, <inline-formula><mml:math id="M72" display="inline"><mml:mi>A</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M73" display="inline"><mml:mi>B</mml:mi></mml:math></inline-formula>, and <inline-formula><mml:math id="M74" display="inline"><mml:mi>C</mml:mi></mml:math></inline-formula> for each slice are calculated by
<inline-formula><mml:math id="M75" display="inline"><mml:mrow><mml:mi>A</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mi mathvariant="normal">s</mml:mi></mml:msub><mml:mo>×</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></inline-formula>,
<inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:mi>B</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">2</mml:mn><mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mi mathvariant="normal">s</mml:mi></mml:msub><mml:mo>×</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">r</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></inline-formula>, and <inline-formula><mml:math id="M77" display="inline"><mml:mrow><mml:mi>C</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mi mathvariant="normal">s</mml:mi></mml:msub><mml:mo>×</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">r</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></inline-formula>, where <inline-formula><mml:math id="M78" display="inline"><mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mi mathvariant="normal">s</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is
the bandwidth for each individual slice, <inline-formula><mml:math id="M79" display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the transmit duration
time, and <inline-formula><mml:math id="M80" display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">r</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the receiving time. The distribution of <inline-formula><mml:math id="M81" display="inline"><mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mi mathvariant="normal">s</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> on each
slice in one pulse is assigned according to the antenna gain pattern of the
pulse.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6" specific-use="star"><?xmltex \currentcnt{6}?><label>Figure 6</label><caption><p id="d1e1597">The workflow for generating L1B simulation data.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f06.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><label>Figure 7</label><caption><p id="d1e1608">The workflow to assign L1B data to the proper WVCs and aggregate
into views.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f07.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><?xmltex \currentcnt{8}?><label>Figure 8</label><caption><p id="d1e1620"><bold>(a)</bold> One simulated satellite orbit for CFOSAT starting from
12 November 2011, with the circular motion of the slice located at the end of each
pulse. <bold>(b)</bold> The zoomed-in location of all slices on the earth.</p></caption>
          <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f08.png"/>

        </fig>

      <p id="d1e1634">An example of the simulated satellite orbit together with the location of
the slices is given in Fig. 8. <inline-formula><mml:math id="M82" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> is derived using the NSCAT-4 GMF for the Ku band and the
CMOD5n GMF for the C band and the corresponding beam geometries. Subsequently,
the L1B data are obtained after adding the instrument noise on the “true”
<inline-formula><mml:math id="M83" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>. The instrument noise is added by multiplying a
Gaussian random number in this way: <inline-formula><mml:math id="M84" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">noise</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>×</mml:mo><mml:mfenced open="(" close=")"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:mtext>Kpc</mml:mtext><mml:mo>×</mml:mo><mml:mtext>Gaussian_random_nr</mml:mtext></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>. The L1B data are assigned to
the proper WVCs (Dunbar et al., 2001) and then aggregated into
views. A view is a group of slices with similar azimuth angle and the same
polarization in one WVC; the properties (i.e., incidence angle, azimuth
angle, latitude, longitude, etc.) on the corresponding slices are also
aggregated to represent the view (Li et al., 2017). We note
that the simulation does currently not include rain effect.</p>
</sec>
<sec id="Ch1.S2.SS3">
  <label>2.3</label><title>Wind field retrieval principle</title>
      <?pagebreak page3577?><p id="d1e1701">Maximum likelihood estimation (MLE) is the most classic algorithm for
wind retrieval. It has been applied in many wind retrieval studies
(Chi and Li, 1988; JPL,
2001; Pierson, 1989; Portabella and Stoffelen, 2002). We adopted it and
applied it in our wind retrievals. The MLE can be expressed as
(JPL, 2001)
            <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M85" display="block"><mml:mrow><mml:mtext>MLE</mml:mtext><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mi>N</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:msup><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">s</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow><mml:mrow><mml:mtext>Kp</mml:mtext><mml:mfenced open="(" close=")"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">x</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:mfenced></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M86" display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> is the number of views, and <inline-formula><mml:math id="M87" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">x</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is
either <inline-formula><mml:math id="M88" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> (measured <inline-formula><mml:math id="M89" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>) or <inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">s</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> (trial simulated
<inline-formula><mml:math id="M91" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>. <inline-formula><mml:math id="M92" display="inline"><mml:mrow><mml:mtext>Kp</mml:mtext><mml:mfenced open="(" close=")"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">x</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is the expected Gaussian observation noise with the form of
<inline-formula><mml:math id="M93" display="inline"><mml:mrow><mml:mtext>Kp</mml:mtext><mml:mo>×</mml:mo><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">x</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>. The wind inversion
procedure takes L2A data and searches for the <inline-formula><mml:math id="M94" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">s</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> with minimum MLE by varying trial wind speeds and
directions. The <inline-formula><mml:math id="M95" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">s</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> with the minimum MLE is
known as the first rank solution. However, the first solution is often not
the best solution because the wind retrieval results usually consist of a
set of ambiguous solutions due to the combination of measurement geometry,
the harmonic modulation of the GMF (nonlinear GMF), and noise, etc. After the
wind retrieval step, one of the ambiguous solutions is selected by the
two-dimensional variational ambiguity removal (2DVAR)
(Vogelzang, 2013) after minimizing a total cost function that
combines both observational and NWP background contributions. The retrieved
wind field can be compared with the input wind field to assess the wind
retrieval quality.</p>
</sec>
<sec id="Ch1.S2.SS4">
  <label>2.4</label><title>Simulation assessment</title>
<sec id="Ch1.S2.SS4.SSS1">
  <label>2.4.1</label><title>Simulation model validation</title>
      <p id="d1e1945">The performance of the scatterometer simulator on actual wind field is a
good means to establish the validity of the simulation model. SeaWinds is
chosen to compare real data with simulated data because it is the only
scatterometer for which real data are available among the three
scatterometers here. In total 14 orbits (one day) of data are included in
the validation. The maximum collocation distance between real and simulated
data points is set to 10 <inline-formula><mml:math id="M96" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>, and the number of collocated data is 75 867;
Fig. 9 shows the collocated wind retrieval result.
The simulated wind speed and wind direction give a good correlation with
the real SeaWinds data, which means the simulation model has a good
performance as compared to the real scatterometer, and it is suitable for
the comparison among the different types of scatterometers.</p><?xmltex \hack{\newpage}?><?xmltex \floatpos{t}?><fig id="Ch1.F9" specific-use="star"><?xmltex \currentcnt{9}?><label>Figure 9</label><caption><p id="d1e1958">The collocation between SeaWinds (ScatA) and simulated SeaWinds
(ScatB) in wind speed (<bold>a</bold>: red points are the average value as a
function of wind speed of ScatA; blue points are the average value as a
function of wind speed of ScatB), wind direction <bold>(b)</bold>, <inline-formula><mml:math id="M97" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> component <bold>(c)</bold>, <inline-formula><mml:math id="M98" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> component <bold>(d)</bold>.</p></caption>
            <?xmltex \igopts{width=398.338583pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f09.png"/>

          </fig>

</sec>
<sec id="Ch1.S2.SS4.SSS2">
  <label>2.4.2</label><title>SCAT, WindRad, and SeaWinds view number comparison</title>
      <p id="d1e2002">The most important differences between SCAT, WindRad, and SeaWinds are the
shape of the antenna and the number of antennas, directly leading to a
different distribution of the number of views across the swath. SeaWinds, as
a rotating pencil-beam instrument, has four views in each WVC across the swath,
where the fore and aft views in the outer swath are each split in two views.
The number of slices in each view varies across the swath though. For
rotating fan-beam instruments, the view number varies across the swath, with
the feature of fewer views in the outer and nadir swath and more views in
the parts of the swath in between (Fig. 10). It
can be observed that both SCAT and WindRad contain more views than SeaWinds
for all WVCs, with a saddle shape in the view count. Moreover, the number of
views of WindRad is about twice the number of views of SCAT.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F10"><?xmltex \currentcnt{10}?><label>Figure 10</label><caption><p id="d1e2007">Averaged number of views at the WVCs across the swath.</p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f10.png"/>

          </fig>

</sec>
<sec id="Ch1.S2.SS4.SSS3">
  <label>2.4.3</label><title>Instrument noise</title>
      <p id="d1e2024">The instrument noise (Kpc) of the simulator for SCAT, WindRad, and SeaWinds
is estimated at various wind speeds (4, 9, and 16 <inline-formula><mml:math id="M99" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>) on slice
level and WVC level. The Kpc for each view is aggregated by weighting the
Kpc of the slices in this view, and the Kpc on WVC level is derived by
averaging the Kpc for all the views in the corresponding WVC.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F11" specific-use="star"><?xmltex \currentcnt{11}?><label>Figure 11</label><caption><p id="d1e2046">SCAT instrument noise in ratio (1 is 100 %) at 4, 9, and
16 <inline-formula><mml:math id="M100" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> on <bold>(a)</bold> slice level and <bold>(b)</bold> WVC mean Kp.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f11.png"/>

          </fig>

      <p id="d1e2078">Figure 11a shows the slice Kpc of SCAT as a
function of incidence angle. The slices with low wind speed and high
incidence angle contain high Kpc, and Kpc for VV polarization overall is
lower than for HH, except for the slices with incidence angle lower than
30.25<inline-formula><mml:math id="M101" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> (indicated by the dashed line in
Fig. 11a). The Kpc in a WVC for SCAT
(Fig. 11b) is much lower than the Kpc on slice
level, as expected due to the aggregation of the slices in a WVC. The outer
swath contains<?pagebreak page3578?> relatively high instrument noise as compared to sweet and
nadir swath. Low wind speed leads to a higher Kpc. On the WVC level, the
instrument noise is lower than 20 % except for low wind speed.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F12" specific-use="star"><?xmltex \currentcnt{12}?><label>Figure 12</label><caption><p id="d1e2093">WindRad instrument noise in ratio (1 is 100 %) at 4, 9,
and 16 <inline-formula><mml:math id="M102" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> on <bold>(a)</bold> slice level of the Ku band, <bold>(b)</bold> slice level of the C band (slices
with <inline-formula><mml:math id="M103" display="inline"><mml:mrow><mml:mtext>SNR</mml:mtext><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0.05</mml:mn></mml:mrow></mml:math></inline-formula> are excluded), and <bold>(c)</bold> WVC mean Kp.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f12.png"/>

          </fig>

      <p id="d1e2140">WindRad has two frequencies at the Ku and C band. As illustrated in
Fig. 12a and b, the VV Kpc is lower than the
HH Kpc for the Ku and C band, and the C-band Kpc is much lower than the Ku-band
Kpc. On the WVC level (Fig. 12c), it shows a
similar pattern to SCAT, and generally the instrument noise is lower than
10 % if the outer swath and low wind speeds are excluded.</p>
      <p id="d1e2143">The SeaWinds Kpc on slice level (Fig. 13a, b)
is more constant at a wind speed of 9 and 16 <inline-formula><mml:math id="M104" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, while it is increasing
along with the incidence angle at a low wind speed of 4 <inline-formula><mml:math id="M105" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. On WVC level, the Kpc
is lower than 20 % except for wind speeds below 4 <inline-formula><mml:math id="M106" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. We note that a
random error of 20 % at 4 <inline-formula><mml:math id="M107" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> is still acceptable in terms of absolute
random wind error after wind retrieval.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F13" specific-use="star"><?xmltex \currentcnt{13}?><label>Figure 13</label><caption><p id="d1e2216">SeaWinds instrument noise in ratio (1 is 100 %) at 4, 9,
and 16 <inline-formula><mml:math id="M108" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> on <bold>(a)</bold> slice level of Ku-band HH polarization, <bold>(b)</bold> slice level of Ku-band
VV polarization (slices with <inline-formula><mml:math id="M109" display="inline"><mml:mrow><mml:mtext>SNR</mml:mtext><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0.05</mml:mn></mml:mrow></mml:math></inline-formula> are excluded), and <bold>(c)</bold> WVC mean Kp.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f13.png"/>

          </fig>

      <p id="d1e2263">In general, low wind speeds cause high instrument noise, as expected, and
the instrument noise on WVC level is less than 20 % for SCAT, less than
10 % for WindRad, and less than 20 % for SeaWinds, when the outer swath
and low wind speeds are excluded. All three scatterometers have a pattern of
higher Kpc at the outer swath as compared to the other parts of the swath.</p>
</sec>
<sec id="Ch1.S2.SS4.SSS4">
  <label>2.4.4</label><title>First rank wind retrieval and 2DVAR performances</title>
      <p id="d1e2274">As already known, the first rank wind solution is not always the best
solution. However, the more often the first rank<?pagebreak page3579?> solution is chosen to be
the best solution, the lower the ambiguity in the inverted instrument wind
solutions. The quality of the first rank solution thus reflects the ambiguity
in the wind measurement system. So, it is chosen for the comparison of the
wind retrieval performance on SCAT, WindRad, and SeaWinds. The difference
between first rank solution and 2DVAR performance provides insight into the
effects of the wind direction ambiguities on the final selected wind field,
which may depend on measurement geometry. 2DVAR with MSS (Multiple Solution
Scheme) (Vogelzang, 2013) has been applied in our simulation. A
weighted analysis field is constructed by combining the scatterometer
observations and a model prediction, and then the one lying closest to the
analysis field is selected as the output solution. The problem is solved by
minimizing a total cost function that combines both observation and NWP
information: <inline-formula><mml:math id="M110" display="inline"><mml:mrow><mml:mi>J</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>J</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>J</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mfenced open="[" close="]"><mml:mrow><mml:mi mathvariant="normal">ln</mml:mi><mml:mi>P</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="bold-italic">k</mml:mi></mml:msub><mml:mi mathvariant="normal">|</mml:mi><mml:mi mathvariant="bold-italic">x</mml:mi></mml:mrow></mml:mfenced><mml:mo>+</mml:mo><mml:mi>ln⁡</mml:mi><mml:mi>P</mml:mi><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="bold-italic">b</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>, where <inline-formula><mml:math id="M111" display="inline"><mml:mi mathvariant="bold-italic">x</mml:mi></mml:math></inline-formula> is the true state of the surface wind field,
<inline-formula><mml:math id="M112" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="bold-italic">k</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the possible ambiguous wind solutions, <inline-formula><mml:math id="M113" display="inline"><mml:mrow><mml:mi>P</mml:mi><mml:mfenced close=")" open="("><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="bold-italic">k</mml:mi></mml:msub><mml:mi mathvariant="normal">|</mml:mi><mml:mi mathvariant="bold-italic">x</mml:mi></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is the conditional probability of
the <inline-formula><mml:math id="M114" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="bold-italic">k</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> observed given <inline-formula><mml:math id="M115" display="inline"><mml:mi mathvariant="bold-italic">x</mml:mi></mml:math></inline-formula>, and <inline-formula><mml:math id="M116" display="inline"><mml:mrow><mml:mi>P</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="bold-italic">b</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is the conditional probability of
surface wind field <inline-formula><mml:math id="M117" display="inline"><mml:mi mathvariant="bold-italic">x</mml:mi></mml:math></inline-formula> given <inline-formula><mml:math id="M118" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="bold-italic">b</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. Details of the method can
be found in
de Vries et al. (2005), Vogelzang et al. (2009), Vogelzang (2013).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F14" specific-use="star"><?xmltex \currentcnt{14}?><label>Figure 14</label><caption><p id="d1e2434">SCAT-retrieved wind field. <bold>(a)</bold> First rank solution. <bold>(b)</bold> 2DVAR
result. The orange flags are artificial quality control points and may be ignored.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f14.png"/>

          </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F15" specific-use="star"><?xmltex \currentcnt{15}?><label>Figure 15</label><caption><p id="d1e2451">WindRad-retrieved wind field. <bold>(a)</bold> First rank solution. <bold>(b)</bold> 2DVAR result. The orange flags are artificial QC points and may be ignored.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f15.png"/>

          </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F16" specific-use="star"><?xmltex \currentcnt{16}?><label>Figure 16</label><caption><p id="d1e2469">SeaWinds-retrieved wind field. <bold>(a)</bold> First rank solution. <bold>(b)</bold> 2DVAR result. The orange flags are artificial QC points and may be ignored.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f16.png"/>

          </fig>

      <?pagebreak page3580?><p id="d1e2484">Comparisons of first rank solution and 2DVAR performances of SCAT, WindRad,
and SeaWinds are shown in Figs. 14,
15, and 16. For
SCAT, the first rank solution wind field (Fig. 14a) shows poor retrieval quality in the nadir and outer swath, while 2DVAR
(Fig. 14b) effectively improves the retrieval
results here; a similar improvement occurs for SeaWinds
(Fig. 16). The nadir swath of WindRad shows worse
wind retrieval quality than the other parts of the swath
(Fig. 15a), and 2DVAR is able to correct the
false solutions appearing in the first rank solution. Note that the rotation
sampling pattern of WindRad is visible as regular disturbances along the
swath. This implies that for the same WVC number, different sets of views
are collected, depending on the phase of the antenna rotation; hence the
wind retrieval performance may vary, e.g., the expected MLE. One aspect
needs to be noted: the 2DVAR with MSS works properly in our simulation, but
the input wind field of the simulation is ECMWF model data, which is consistent with the 2DVAR background field. Even though a
Gaussian-distributed geophysical noise has been added in the input wind
field, it still might lead to a selection of wind solutions that tends to be
close to the model wind field, and hence it may somewhat overestimate the
performance.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Simulation result and wind retrieval performance comparison</title>
      <p id="d1e2497">The simulation has been performed on SCAT, WindRad, and SeaWinds with ECMWF
model wind data (17 December 2011) as the input wind field. The swath widths for
the three instruments are different; in order to make the following figures
more comparable, the nadir WVCs of the three instruments are aligned.</p>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Wind retrieval performance evaluation</title>
<sec id="Ch1.S3.SS1.SSS1">
  <label>3.1.1</label><title>Assessments with the input wind field</title>
      <p id="d1e2514">Four orbits of data on 17 December 2011 have been generated to be used for the
wind retrieval simulation. The contoured histograms in
Figs. 17, 18, and
19 provide statistics of the wind speed,
wind direction with respect to a wind blowing from the north, and wind
components <inline-formula><mml:math id="M119" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> (eastward) and <inline-formula><mml:math id="M120" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> (northward) versus the variable “true” input
wind field for<?pagebreak page3581?> SCAT, WindRad, and SeaWinds. We note that opposing wind
solutions will have opposite <inline-formula><mml:math id="M121" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M122" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> signs and similar amplitude, and
therefore such common ambiguity appears as a cross pattern in the <inline-formula><mml:math id="M123" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M124" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula>
histograms. This ambiguity is directly related to the main double harmonic
dependency of the GMF (Wang et al., 2019).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F17" specific-use="star"><?xmltex \currentcnt{17}?><label>Figure 17</label><caption><p id="d1e2562">Contoured histograms of SCAT-retrieved first rank wind solution
versus input wind field for four orbits. <bold>(a)</bold> All WVCs within the swath; <bold>(b)</bold> excluding the WVCs in the outer swath, for which WVC numbers from 8 to 42 are included;
<bold>(c)</bold> excluding the WVCs in the outer swath and nadir swath, for which WVC numbers from 8
to 17 and 26 to 42 are included. From <bold>(a)</bold> to <bold>(c)</bold>, upper left: wind speed;
upper right: wind direction; lower left: <inline-formula><mml:math id="M125" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> component; lower right: <inline-formula><mml:math id="M126" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> component. The contour lines are logarithmic.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f17.png"/>

          </fig>

      <?pagebreak page3584?><p id="d1e2601">For SCAT (Fig. 17a), the first rank solution of
all WVCs across the swath is included. It shows rather poor statistics when
compared with the input wind field. However, by simply excluding the WVCs
located in the outer swath, the first rank solution quality improves
substantially (Fig. 17b). The spread in the
wind speeds is reduced, and some derived false wind directions, which are
shown as parallel and perpendicular lobes to the true value in the plots,
are removed. When the nadir-swath WVCs are also excluded
(Fig. 17c), then the wind speed collocation
statistics stay almost unchanged as compared to
Fig. 17b, while most of the false wind directions
perpendicular to the true value are removed. This means that the outer swath
contains the most ambiguous wind vector results, while the nadir swath
ambiguities cause mainly wind direction errors.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F18" specific-use="star"><?xmltex \currentcnt{18}?><label>Figure 18</label><caption><p id="d1e2607">Contoured histograms of WindRad retrieved first rank wind
solution versus input wind field for four orbits. <bold>(a)</bold> All WVCs within the
swath; <bold>(b)</bold> excluding the WVCs in the outer swath, for which WVC numbers from 20 to 60
are included; <bold>(c)</bold> excluding the WVCs in the nadir swath, for which WVC numbers from 35
to 45 are included; <bold>(d)</bold> excluding the WVCs in the outer swath and nadir
swath, for which WVC numbers from 20 to 35 and 45 to 60 are included. The four panels
in <bold>(a)–(d)</bold>, upper left: wind speed; upper right: wind direction; lower left: <inline-formula><mml:math id="M127" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> component; lower right: <inline-formula><mml:math id="M128" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> component. The contour lines are logarithmic.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f18.png"/>

          </fig>

      <p id="d1e2646">Figure 18a shows the first rank wind retrieval for
WindRad with all WVCs, and it shows much better statistics as compared to
SCAT (Fig. 17a), due to the availability of
twice the number of views in each WVC. Excluding outer WVCs
(Fig. 18b) has less effect on the wind
retrieval quality for WindRad than for SCAT. The retrieved wind speed shows
slightly better statistics, but wind direction statistics stay almost
unchanged, which means that the outer WVCs do not have a much larger wind
direction ambiguity. On the other hand, when we only exclude nadir WVCs
(Fig. 18c), the wind direction retrieval is
improved. The average wind speed bias is 0.42 <inline-formula><mml:math id="M129" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, and the standard deviation
of wind direction is 32.21<inline-formula><mml:math id="M130" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> (Fig. 18c), while they are 0.51 <inline-formula><mml:math id="M131" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and
41.30<inline-formula><mml:math id="M132" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> for Fig. 18b,
respectively. The last experiment shown for WindRad is with the exclusion of
both outer and nadir WVCs (Fig. 18d), with an
averaged wind speed bias of 0.44 <inline-formula><mml:math id="M133" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and a standard deviation of wind
direction of 35.61<inline-formula><mml:math id="M134" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. The largest performance improvement
of<?pagebreak page3585?> WindRad occurs when excluding nadir WVCs. The outer swath mainly
influences the wind speed retrieval skill, while the nadir swath provides
wind direction ambiguity.</p>
      <p id="d1e2728">SeaWinds's outer swath contains only two views (fore-VV and aft-VV), and in
order to process outer swath winds, each of these two views is split into
two views based on their azimuth angle (four views in total in the end).
Even though there are four views at the outer swath, the limited azimuth
diversity leads to more ambiguous wind retrieval results
(Fig. 19). The wind retrieval quality of SeaWinds
is the poorest one among these three instruments.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F19" specific-use="star"><?xmltex \currentcnt{19}?><label>Figure 19</label><caption><p id="d1e2733">Contoured histograms of SeaWinds retrieved first rank wind
solution versus input wind field for four orbits. <bold>(a)</bold> All WVCs within the
swath; <bold>(b)</bold> excluding the WVCs in the outer swath, for which WVC numbers from 10 to 65
are included. From <bold>(a)</bold> to <bold>(b)</bold>, upper left: wind speed; upper right: wind
direction; lower left: <inline-formula><mml:math id="M135" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> component; lower right: <inline-formula><mml:math id="M136" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> component. The contour
lines are logarithmic.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f19.png"/>

          </fig>

      <p id="d1e2769">The averaged wind retrieval statistics against the input wind field are
dominated by the lack of ambiguity removal and nonlinearity. In practice
these issues are successfully dealt with in the ambiguity removal step,
using prior background information. In the next section we determine figures of merit (FoMs) to compare scatterometer performances with and without such
prior information.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS2">
  <label>3.1.2</label><title>Figures of merit</title>
      <p id="d1e2780">The first rank solutions contain ambiguities and because the input wind field
is the ECMWF model wind, but without spatially correlated error, it leads to
a nearly perfect 2DVAR result, which is unrealistic. In order to further
evaluate the wind retrieval performance, the ambiguity of the solutions may
be statistically evaluated in the context of generally available background
(NWP) information. Figures of merit (FoMs) are a set of parameters to
evaluate the wind retrieval quality of different scatterometer concepts,
taking into account imprecise, ambiguous, and biased wind solutions. Three
FoMs, which are the normalized wind vector rms (root mean square) (VRMS) error, ambiguity
susceptibility (AMBI), and systematic error (BIAS), are introduced here based
on Rivas et al. (2009). A brief description is given first.</p>
      <p id="d1e2783">The VRMS FoM is defined to quantify the ability of the scatterometer wind
retrieval to handle ambiguous solutions with a priori NWP model information,
such as in 2DVAR, but without actually simulating realistic spatially
correlated errors. The input wind field to our simulation is considered as
true winds (denoted with <inline-formula><mml:math id="M137" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>). VRMS quantifies the total simulated
wind retrieval error with respect to <inline-formula><mml:math id="M138" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. It is, however,
calculated by down-weighting ambiguous wind vector solutions that are very
distant from <inline-formula><mml:math id="M139" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, since in practice it is easiest for 2DVAR and
other applications to discard such solutions. The down-weighting involves
the common prior knowledge in these applications, which is the general NWP
background wind component uncertainty, denoted <inline-formula><mml:math id="M140" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and assumed
equal for <inline-formula><mml:math id="M141" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M142" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula>. The ambiguous retrieved wind vector distribution,
expressed in the wind probability <inline-formula><mml:math id="M143" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>, is multiplied by a Gaussian probability distribution
<inline-formula><mml:math id="M144" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> centered at the input
wind field and with a variance <inline-formula><mml:math id="M145" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M146" display="inline"><mml:mrow class="unit"><mml:msup><mml:mi mathvariant="normal">m</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> in both wind components. The VRMS FoM is subsequently obtained by
normalizing this expression by the prior NWP VRMS error:
              <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M147" display="block"><mml:mrow><mml:msub><mml:mtext>FoM</mml:mtext><mml:mi mathvariant="normal">VRMS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mtext>rms</mml:mtext><mml:mi mathvariant="normal">obs</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mtext>rms</mml:mtext><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where
              <disp-formula id="Ch1.Ex1"><mml:math id="M148" display="block"><mml:mrow><mml:msub><mml:mtext>rms</mml:mtext><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mfenced close=")" open="("><mml:msqrt><mml:mrow><mml:mo movablelimits="false">∫</mml:mo><mml:msup><mml:mfenced open="|" close="|"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>×</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:msup><mml:mi>d</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi>v</mml:mi></mml:mrow></mml:msqrt></mml:mfenced></mml:mrow></mml:math></disp-formula>
            and
              <disp-formula id="Ch1.Ex2"><mml:math id="M149" display="block"><mml:mrow><mml:msub><mml:mtext>rms</mml:mtext><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mfenced open="(" close=")"><mml:msqrt><mml:mrow><mml:mo movablelimits="false">∫</mml:mo><mml:msup><mml:mfenced close="|" open="|"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:msup><mml:mi>d</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi>v</mml:mi></mml:mrow></mml:msqrt></mml:mfenced><mml:mo>=</mml:mo><mml:msqrt><mml:mn mathvariant="normal">2</mml:mn></mml:msqrt><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            VRMS quantifies the wind solution's relative rms about the true wind with
respect to the general prior background uncertainty. If its value is 1, then
the wind retrieval failed to<?pagebreak page3587?> provide new and useful information in the wind
field, i.e., corresponding to <inline-formula><mml:math id="M150" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>=</mml:mo><mml:mtext>constant</mml:mtext></mml:mrow></mml:math></inline-formula>.</p>
      <p id="d1e3122">On the other hand, AMBI is defined to quantify the ability of the
scatterometer and its processing to handle ambiguous solutions without a
priori NWP model information. It is a ratio of the wind solution output
falling outside the general prior wind field constraint, relative to the
output falling inside the prior wind field constraint. The lower the ratio,
the better the AMBI FoM, where <inline-formula><mml:math id="M151" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mrow><mml:mi mathvariant="normal">NWP</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">max</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is the maximum
probability of <inline-formula><mml:math id="M152" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>.
              <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M153" display="block"><mml:mrow><mml:msub><mml:mtext>FoM</mml:mtext><mml:mi mathvariant="normal">AMBI</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∫</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>×</mml:mo><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mrow><mml:mi mathvariant="normal">NWP</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">max</mml:mi></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:mfenced><mml:msup><mml:mi>d</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∫</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>×</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:msup><mml:mi>d</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi>v</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula>
            BIAS quantifies the systematic vector wind bias, again in the context of the
background prior, which is the shift of the average location of the output
wind solution away from the location of the prior wind caused by skewness in
the output wind solutions (Eq. 4).
              <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M154" display="block"><mml:mrow><mml:msub><mml:mtext>FoM</mml:mtext><mml:mi mathvariant="normal">BIAS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo movablelimits="false">∫</mml:mo><mml:mfenced close=")" open="("><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>⋅</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">obs</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mo>×</mml:mo><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">NWP</mml:mi></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">v</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:msup><mml:mi>d</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi>v</mml:mi></mml:mrow></mml:math></disp-formula>
            The wind retrieval is a nonlinear problem, and the output wind error depends
on the true wind vector (wind speed and direction distribution). In order to
minimize this dependence, the calculated FoMs are averaged over a
climatology of wind inputs with uniformly distributed directions and wind
speeds (3 to 16 <inline-formula><mml:math id="M155" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>) following a Weibull distribution with a maximum
around 8 <inline-formula><mml:math id="M156" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> (Liu et al., 2008). The input wind speeds are
from 3 to 16 <inline-formula><mml:math id="M157" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> with steps of 1 <inline-formula><mml:math id="M158" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, and the input wind directions are from
0 to 360<inline-formula><mml:math id="M159" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> with steps of 10<inline-formula><mml:math id="M160" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. Each wind speed and wind
direction combination contains the equivalent number of WVCs from the same
orbit.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F20" specific-use="star"><?xmltex \currentcnt{20}?><label>Figure 20</label><caption><p id="d1e3440">FoM results of SCAT, WindRad, and SeaWinds. <bold>(a)</bold> VRMS comparison.
<bold>(b)</bold> AMBI comparison. <bold>(c)</bold> BIAS comparison.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f20.png"/>

          </fig>

      <p id="d1e3458">Figure 20 gives the three FoM comparisons of SCAT,
WindRad, and SeaWinds as a function of the WVC positions in the swath.
Overall, the wind retrieval performance of the rotating fan-beam instruments
is better than the pencil-beam instrument, while the outer and nadir swaths
of the three instrument types yield a poorer performance than the sweet
swaths. The outer swath of SeaWinds only has two independent views, which
result in very ambiguous winds and the worst simulated wind retrieval
quality. The wind retrieval quality across the swath strongly depends on the
location of the WVC; it degrades substantially in the outer and nadir swaths
as expected. The outer swath has worse quality than the nadir swath for both
SCAT and SeaWinds, whereas these two regions show comparable wind
retrieval quality for WindRad. Although the number of views in the sweet
swath for WindRad is twice the number for SCAT
(Fig. 10), the wind retrieval quality is not
improved as expected, but it shows very similar quality to SCAT. The elevated
values for AMBI and BIAS indicate that, despite the high number of views,
the wind retrieval tends to be not well determined and slightly nonlinear.
At the same time, the quality in the outer swath of WindRad shows very
pronounced improvement with respect to SCAT, due to the increased number of
available views.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F21" specific-use="star"><?xmltex \currentcnt{21}?><label>Figure 21</label><caption><p id="d1e3463">FoM VRMS map as a function of across-track location and wind
direction (wind speed is 9 <inline-formula><mml:math id="M161" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>). <bold>(a)</bold> SCAT. <bold>(b)</bold> SeaWinds. <bold>(c)</bold> WindRad.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f21.png"/>

          </fig>

      <p id="d1e3498">Figure 21 illustrates the VRMS as a function of
wind direction and WVC location at 9 <inline-formula><mml:math id="M162" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> wind speed. The wind retrieval
performance across the swath for all wind directions gives the same pattern
as described above with some modulations at different wind direction. There
is one different feature occurring for WindRad. The VRMS at nadir swath
shows higher values than in the outer swath, which is opposite to SCAT and
SeaWinds. AMBI and BIAS (not shown here) have similar patterns to VRMS.</p>
</sec>
<?pagebreak page3588?><sec id="Ch1.S3.SS1.SSS3">
  <label>3.1.3</label><title>Wind direction bias</title>
      <p id="d1e3526">Wind direction bias between the wind retrieval result (2DVAR result) and the
ECMWF model wind has been evaluated as a function of WVC and relative wind
direction, using 15 orbits. The relative wind direction means the retrieved
wind direction relative to the satellite motion direction. In this
evaluation, we are able to see the wind direction bias with respect to the
true direction at all the WVCs (Fig. 22). No
matter whether the biases are negative or positive, both signs indicate that the
wind directions have a tendency to be closer to the satellite motion
direction, and if the wind direction bias is averaged over all the relative
wind directions, a small value of the bias remains.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F22" specific-use="star"><?xmltex \currentcnt{22}?><label>Figure 22</label><caption><p id="d1e3531">Wind direction bias between wind retrieval result and true wind as
a function of WVC number and the relative wind direction. (The <inline-formula><mml:math id="M163" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula> axis is the
retrieved wind direction relative to the satellite motion direction. The color
scale is consistent for easy comparison; all the values outside [<inline-formula><mml:math id="M164" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">20</mml:mn></mml:mrow></mml:math></inline-formula>, 20]
are marked as dark blue and dark red.) <bold>(a)</bold> SCAT. <bold>(b)</bold> SeaWinds. <bold>(c)</bold> WindRad.</p></caption>
            <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f22.png"/>

          </fig>

      <p id="d1e3566">SeaWinds gives stronger bias both on the outer swath and nadir swath
(Fig. 22b), while the nadir swath of SCAT
gives weaker bias compared to the outer swath due to the increased number
of views (Fig. 22a). For WindRad, when the
retrieved wind direction is close to satellite motion direction (relative
wind direction is 0), it shows rather strong negative and positive bias, but
the nonbiased area for WindRad is larger than it is in SCAT and SeaWinds.
This phenomenon can also be observed with real data from SCATSAT
(Wang et al., 2019). This retrieved wind direction preference
might be caused by the retrieval method.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Discussion</title>
      <p id="d1e3579">Our results confirm that the wind retrieval quality of Ku-band rotating-beam
scatterometers (rotating fan-beam and rotating pencil-beam) varies according
to the location of the WVCs across the swath, and the outer and nadir swaths
show generally lower wind retrieval skill than the sweet swath. The wind
retrieval comparisons suggest that WindRad gives the best wind retrieval
quality of the three scatterometer types, although its increased number of
views does not always result in further wind retrieval quality improvement,
particularly not in the sweet swath.</p>
      <p id="d1e3582">For the rotating fan-beam and rotating pencil-beam instruments, FoMs give quite a clear
wind retrieval quality comparison. In general, both rotating systems have
the same performance pattern across the track as mentioned above,
while the rotating fan-beam system has a better performance for<?pagebreak page3589?> all the FoMs compared
to the pencil-beam system through all WVCs, and the nadir swath tends to spread larger
for the pencil-beam type. The obvious reason is that the pencil-beam type classified the views
as fore and aft with HH and VV polarization, which are a maximum of four views
in the sweet swath, while for the fan-beam type it is possible to ensure that the
number of views and the diversity of the geometry are high due to its fan
shape.</p>
      <p id="d1e3585">Prior work on SCAT and WindRad mainly focused on the instrument
configuration choices and tests with various settings of pulse frequency,
polarization, rotating speed, and transmitted peak power, etc.
(Lin et al.,
2000a, 2002; Lin and Dong, 2011). The main wind retrieval performance
characteristics of these two-rotating fan-beam scatterometers, as obtained
in these papers, are in line with our study with respect to sweet swath,
nadir swath, and outer swath performance. SCAT has been compared with SeaWinds
(Lin and Dong, 2011) in an end-to-end simulation, and
now we add a cross comparison among SCAT, WindRad, and SeaWinds in the same
simulation framework as before.</p>
      <p id="d1e3588">WindRad shows distinguished and new wind retrieval features in our study
with respect to SCAT and SeaWinds. The outer swaths of SCAT and SeaWinds
clearly provide the worst wind retrieval skill as compared to nadir, but for
WindRad this does not occur. WindRad gives very similar wind retrieval
quality in the nadir and outer swaths according to its FoM
(Fig. 20). However, the spread of the WindRad FoM
values are largest in the inner swath (Fig. 21),
and excluding the inner swath leads to a better wind retrieval as compared
to excluding the outer swath. This is opposite to SCAT and SeaWinds, for which
performance increases most when excluding the outer swath.</p>
      <p id="d1e3592">Increasing the number of views and azimuth diversity leads to an improved
wind retrieval. While this is generally true, comparing SCAT and WindRad,
the increased number of WindRad views on their own provides a strong
improvement in the outer swath, but it appears not to be effective in the sweet
and nadir swath. The azimuths in the nadir swath are always either looking
forward of the satellite track or looking backward. The additional views in
this case will still have similar azimuths, and these are not effective<?pagebreak page3590?> in
improving the azimuth diversity. In the sweet swath, there are up to 18 views
in the WVCs, leading to a more diverse observation geometry.</p>
      <p id="d1e3595">One question is raised here: the relationship between the number of views
and their diversity. It seems that the views with similar azimuth angle and
the same polarization do not really add diversity into the system, which
means they will not improve the wind retrieval result. Such views in the
rotating pencil-beam scatterometer are averaged into one view without
affecting the wind retrieval. Will we get the same effect for rotating
fan-beam scatterometers? In order to investigate this, an experiment was
done for SCAT in which the views with azimuth angle difference within 5<inline-formula><mml:math id="M165" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> are averaged together into one super view, and the other parts of
the wind retrieval are kept the same. This averaging procedure influences the
nadir swath strongest since there are only forward and backward azimuth
angles (Fig. 23), and the number of views has been
reduced according to the similarity of the azimuth angle. The same wind
retrieval procedure is performed afterwards, and the results are shown in
Fig. 24. The wind retrieval result with all WVCs
(Fig. 24a) looks quite similar to the wind
retrieval result without azimuth averaging (Fig. 17a). However, the wind retrieval results get worse when excluding outer
WVCs (Figs. 24b and
17b) and excluding both outer and nadir
WVCs (Figs. 24c and
17c). This leads to a conclusion that the
averaging of the number of views with similar azimuth angle into a single
view is not able to improve the wind retrieval for a rotating fan-beam system, and
even if the azimuth diversity of the views is similar, it still adds
geometry diversity into the wind retrieval procedure, which leads to a better
retrieval result.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F23" specific-use="star"><?xmltex \currentcnt{23}?><label>Figure 23</label><caption><p id="d1e3609">SCAT azimuth angle distribution of the WVC located at the nadir
swath. (The values of <inline-formula><mml:math id="M166" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula> axis and <inline-formula><mml:math id="M167" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula> axis are for the angle display; they do
not have actual meanings. The <inline-formula><mml:math id="M168" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula> axis is the cross-track direction, and the <inline-formula><mml:math id="M169" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula> axis is the
satellite moving direction.) <bold>(a)</bold> Azimuth angles of the views with HH
polarization. <bold>(b)</bold> Azimuth angles of the views with VV polarization. <bold>(c)</bold> Azimuth angles of the views with HH polarization (views with similar azimuth
angles are aggregated into one view). <bold>(d)</bold> Azimuth angles of the views with
VV polarization (views with similar azimuth angles are aggregated into one
view).</p></caption>
        <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f23.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F24" specific-use="star"><?xmltex \currentcnt{24}?><label>Figure 24</label><caption><p id="d1e3661">Contoured histograms of SCAT retrieved first rank wind solution
(the views with similar azimuth angles are aggregated into one view) versus input
wind field for four orbits. <bold>(a)</bold> All WVCs within the swath; <bold>(b)</bold> excluding the
WVCs in the outer swath, for which WVC numbers from 8 to 42 are included; <bold>(c)</bold> excluding
the WVCs in the outer swath and nadir swath, for which WVC numbers from 8 to 17 and 26
to 42 are included. From <bold>(a)</bold> to <bold>(c)</bold>, upper left: wind speed; upper right:
wind direction; lower left: <inline-formula><mml:math id="M170" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> component; lower right: <inline-formula><mml:math id="M171" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> component. The
contour lines are logarithmic.</p></caption>
        <?xmltex \igopts{width=483.69685pt}?><graphic xlink:href="https://amt.copernicus.org/articles/12/3573/2019/amt-12-3573-2019-f24.png"/>

      </fig>

      <p id="d1e3700">The incidence angle range of SCAT, with almost 25<inline-formula><mml:math id="M172" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> between lowest and
highest incidence angle, is much broader than that of WindRad, which is
approximately 10<inline-formula><mml:math id="M173" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. Moreover, the minimum SCAT incidence angle at 25<inline-formula><mml:math id="M174" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> is about 10<inline-formula><mml:math id="M175" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> lower than that from WindRad. This implies that,
while moving away from nadir, the azimuth diversity of SCAT increases much
faster than that of WindRad, hence the steep<?pagebreak page3591?> performance increase for SCAT
when moving away from nadir. On the other hand, the many channels on WindRad
and its fan beam add a lot of additional views and azimuth diversity near
the outer swath, as compared to SCAT and SeaWinds, hence the outstanding
outer swath performance of WindRad. We found that the number of slices
located in the outer swath is the least, and the geometrically unbalanced
<inline-formula><mml:math id="M176" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> distribution within the views of a WVC is one of
the reasons for the low retrieval quality. The instrument noise also
contributes, and it is lower for WindRad than it is for SCAT on average.</p>
      <p id="d1e3751">All in all, the wind retrieval is substantially better in the outer swath
for WindRad. We also note that SCAT is essentially providing reference wind
information for the CFOSAT small-incidence wave instrument SWIM and as such
is well designed for this task.</p>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <label>5</label><title>Conclusions</title>
      <p id="d1e3763">In summary, we have presented and assessed a generic simulation framework,
which has been adapted to all existing rotating-beam scatterometer types.
The representative set of SCAT, WindRad, and SeaWinds is chosen to evaluate
the wind retrieval performance of the rotating scatterometers using the Ku band.
The wind retrieval quality strongly<?pagebreak page3592?> depends on the location of the WVCs
across the swath, and the sweet swath shows the most favorable geometries
for wind retrieval. Among the more unfavorable outer and nadir swath
regions, SCAT and SeaWinds both perform best in the nadir swath, while for
WindRad the outer swath wind retrieval is substantially better than for the
other two instruments. On the other hand, WindRad's nadir swath region with
lower wind retrieval quality is larger than its outer swath region with
degraded quality, while SCAT and SeaWinds have a relatively large outer
swath region with degraded quality. The outer swath of SCAT shows both wind
speed and wind direction retrieval problems, while for WindRad only the wind
speed retrieval is affected. Although rotating fan-beam scatterometers,
particularly SCAT, much improve nadir performance with respect to SeaWinds.
the nadir swath still shows significant wind direction ambiguity for both
SCAT and WindRad.</p>
      <p id="d1e3766">The increased number of views in the nadir and sweet swath for WindRad does
not lead to an improved wind retrieval, but the wind quality shows a
saturation effect and is similar to SCAT. The retrieved wind direction has a
tendency to be biased towards the satellite motion direction for all three
instruments, which is related to the retrieval procedure. Rain effects are
not taken into consideration, so the rain disturbance in the Ku band and the
advantage of the C band on WindRad cannot be shown here. Future studies may
focus on this aspect.</p>
      <p id="d1e3769">To facilitate good-quality collocations with the CFOSAT SWIM instrument, the
SCAT design is clearly focused on an optimal performance close to nadir and
employs small incidence angles, combined with a large incidence angle range.
This facilitates the availability of additional views near nadir with
enhanced azimuth and incidence angle diversity. On the other hand, WindRad's
most useful complement is clearly its dual-frequency capability, providing
many views in the outer swath, for which excellent performance is obtained
according to our simulations.</p>
      <?pagebreak page3593?><p id="d1e3772">This simulation allows us to further investigate the true resolution of the
instruments before their launch and also the non-overlap of the views in a
WVC, which contributes to the geophysical noise. The WVC size is not the
true spatial resolution, and nor is it the true representation of the
contributing views, which depend on the spatial response function of each
sample, how these are aggregated into a view, and which views contribute to
the WVC (Vogelzang et al., 2017; Vogelzang and Stoffelen,
2017). For rotating-beam scatterometers the sampling and hence wind
retrieval characteristics vary potentially both by across-track and
along-track WVC, which may be further investigated. Such developments may
much help users interested in coastal winds.</p>
      <p id="d1e3776">Our simulation does not consider the rain effect. Ku-band ocean radar
returns are affected by rain, and moderate and heavy rain will certainly
degrade the wind retrieval. At KNMI, we use the wind retrieval MLE for rain
screening of Ku-band systems, much aided by MSS 2DVAR. This successful
methodology developed for SeaWinds will also be attempted for CFOSAT. On the
other hand, C-band backscatter is much less sensitive to rain and is included
in WindRad. This advantage of WindRad should be further investigated, e.g.,
by using collocated measurements of Ku-band and C-band scatterometers.</p>
      <p id="d1e3779">The broader user community is looking forward to an increased temporal
sampling of the ocean surface with scatterometer winds, including both
WindRad and SCAT. These will be useful contributions to the global ocean
surface vector winds' virtual constellation.</p>
</sec>

      
      </body>
    <back><notes notes-type="dataavailability"><title>Data availability</title>

      <p id="d1e3786">All the data results and specific algorithms created in this study are available from the authors upon request. If you are interested in having access to them, please send an email to li@knmi.nl. The ECMWF data are available at <uri>https://www.ecmwf.int/en/forecasts/datasets</uri> (last access: 3 July 2019).  (registration needed). SeaWinds data are available at <uri>https://navigator.eumetsat.int/product/EO:EUM:DAT:QUIKSCAT:REPSW25</uri> (last access: 3 July 2019) (OSI SAF, 2015, <ext-link xlink:href="https://doi.org/10.15770/EUM_SAF_OSI_0002" ext-link-type="DOI">10.15770/EUM_SAF_OSI_0002</ext-link>).</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e3801">ZL designed the model, collected the data, performed the analysis, and took lead in writing the manuscript. AS contributed to the idea of designing the model and the idea of how to perform the analysis and reviewed the manuscript. AV helped to improve the simulation, contributed his idea of the pencil-beam simulation, and reviewed the manuscript.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d1e3807">The authors declare that they have no conflict of interest.</p>
  </notes><ack><title>Acknowledgements</title><p id="d1e3813">We are grateful to the anonymous reviewers for their constructive and useful comments. We thank Wenming Lin and National Ocean Satellite Application Center China for providing CFOSAT SCAT simulation parameters.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e3818">This work was supported by the project of “the development and provision of scatterometer wind processing software and wind products for the China France Oceanography SATellite (CFOSAT)” between CNES (Centre National d'etudes Spatiales) and KNMI (Royal Netherlands Meteorological Institute), supported by the EUMETSAT Ocean and Sea Ice Satellite Application Facility (OSI SAF).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e3824">This paper was edited by Andreas Richter and reviewed by two anonymous referees.</p>
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    <!--<article-title-html>A generalized simulation capability for rotating- beam scatterometers</article-title-html>
<abstract-html><p>Rotating-beam wind scatterometers exist in two types: rotating
fan-beam and rotating pencil-beam. In our study, a generic simulation frame
is established and verified to assess the wind retrieval skill of the three
different scatterometers: SCAT on CFOSAT (China France Oceanography SATellite), WindRad (Chinese Wind Radar) on FY-3E, and SeaWinds on
QuikSCAT. Besides the comparison of the so-called first rank solution
retrieval skill of the input wind field, other figures of merit (FoMs) are
applied to statistically characterize the associated wind retrieval
performance from three aspects: wind vector root mean square error,
ambiguity susceptibility, and wind biases. The evaluation shows that,
overall, the wind retrieval quality of the three instruments can be ranked
from high to low as WindRad, SCAT, and SeaWinds, where the wind retrieval
quality strongly depends on the wind vector cell (WVC) location across the
swath. Usually, the higher the number of views, the better the wind
retrieval, but the effect of increasing the number of views reaches
saturation, considering the fact that the wind retrieval quality at the
nadir and sweet swath parts stays relatively similar for SCAT and WindRad.
On the other hand, the wind retrieval performance in the outer swath of
WindRad is improved substantially as compared to SCAT due to the increased
number of views. The results may be generally explained by the different
incidence angle ranges of SCAT and WindRad, mainly affecting azimuth
diversity around nadir and number of views in the outer swath. This
simulation frame can be used for optimizing the Bayesian wind retrieval
algorithm, in particular to avoid biases around nadir but also to
investigate resolution and accuracy through incorporating and analyzing the
spatial response functions of the simulated Level-1B data for each WVC.</p></abstract-html>
<ref-html id="bib1.bib1"><label>1</label><mixed-citation>
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<ref-html id="bib1.bib2"><label>2</label><mixed-citation>
Chi, C. Y. and Li, F. K.: A comparative study of several wind estimation
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