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  <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-15-3925-2022</article-id><title-group><article-title>A statistically optimal analysis of systematic differences <?xmltex \hack{\break}?>between Aeolus horizontal line-of-sight winds and <?xmltex \hack{\break}?>NOAA's Global Forecast System</article-title><alt-title>Aeolus HLOS winds and NOAA's Global Forecast System</alt-title>
      </title-group><?xmltex \runningtitle{Aeolus HLOS winds and NOAA's Global Forecast System}?><?xmltex \runningauthor{H. Liu et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Liu</surname><given-names>Hui</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Garrett</surname><given-names>Kevin</given-names></name>
          <email>kevin.garrett@noaa.gov</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff3">
          <name><surname>Ide</surname><given-names>Kayo</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Hoffman</surname><given-names>Ross N.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Lukens</surname><given-names>Katherine E.</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>NOAA/NESDIS/Center for Satellite Applications and Research (STAR), College Park, MD 20740, USA</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Cooperative Institute for Satellite Earth System Studies (CISESS),
University of Maryland, <?xmltex \hack{\break}?>College Park, MD 20740, USA</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>Department of Atmospheric and Oceanic Science, University of Maryland, College Park, MD 20740, USA</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Kevin Garrett (kevin.garrett@noaa.gov)</corresp></author-notes><pub-date><day>5</day><month>July</month><year>2022</year></pub-date>
      
      <volume>15</volume>
      <issue>13</issue>
      <fpage>3925</fpage><lpage>3940</lpage>
      <history>
        <date date-type="received"><day>14</day><month>January</month><year>2022</year></date>
           <date date-type="rev-request"><day>18</day><month>January</month><year>2022</year></date>
           <date date-type="rev-recd"><day>21</day><month>May</month><year>2022</year></date>
           <date date-type="accepted"><day>9</day><month>June</month><year>2022</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2022 Hui Liu et al.</copyright-statement>
        <copyright-year>2022</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/15/3925/2022/amt-15-3925-2022.html">This article is available from https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022.html</self-uri><self-uri xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022.pdf</self-uri>
      <abstract><title>Abstract</title>

      <p id="d1e137">The European Space Agency Aeolus mission launched a first-of-its-kind spaceborne Doppler wind lidar in August 2018. To optimize the assimilation of the Aeolus Level-2B (B10) horizontal line-of-sight (HLOS) winds, significant systematic differences between the observations and numerical weather prediction (NWP) background winds should be removed. Total least squares (TLS) regression is used to estimate speed-dependent systematic differences between the Aeolus HLOS winds and the National Oceanic and Atmospheric Administration (NOAA) Finite-Volume Cubed-Sphere Global Forecast System (FV3GFS) 6 h forecast winds. Unlike ordinary least squares regression, TLS regression optimally accounts for random errors in both predictors and predictands. Large, well-defined, speed-dependent systematic differences are found in the lower stratosphere and troposphere in the tropics and Southern Hemisphere. Correction of these systematic differences improves the forecast impact of Aeolus data assimilated into the NOAA global NWP system.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d1e149">The spaceborne Doppler wind lidar onboard the European Space Agency (ESA)
Aeolus mission measures both Mie (i.e., clouds and aerosols) and Rayleigh
(i.e., molecular) backscatter to derive wind profiles along the sensor's
horizontal line of sight (HLOS) throughout the troposphere and lower
stratosphere (Straume-Lindner, 2018; Straume et al., 2020). The Aeolus HLOS
Level-2B (L2B) winds have demonstrated positive impacts on global weather
forecasts (Rennie et al., 2021; Cress, 2020; Garrett et al., 2020, 2022).</p>
      <p id="d1e152">To optimize the positive impact of Aeolus HLOS winds on weather forecasts,
large systematic differences between Aeolus winds and numerical weather
prediction (NWP) model background winds should be corrected (Daley, 1991).
Therefore, it is important to identify potential systematic differences
between Aeolus winds and their NWP model background counterparts (Liu et
al., 2020, 2021). The systematic differences may come from both the NWP
model background and the Aeolus winds. First, current operational global NWP
background winds still have larger errors or uncertainty in regions where
conventional wind observations are sparse or absent. For example, the 6 h
forecast zonal winds from the ECMWF model (<uri>https://www.ecmwf.int/en/forecasts</uri>, last access: 19 December 2019) and the NOAA Finite-Volume Cubed-Sphere
Global Forecast System (FV3GFS) model (Kleist et al., 2021) show large
systematic differences in the upper troposphere and lower stratosphere of
the tropics, the Southern Hemisphere (SH), and poleward of 70<inline-formula><mml:math id="M1" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N,
with maxima of the order of 2.0, <inline-formula><mml:math id="M2" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn></mml:mrow></mml:math></inline-formula>, and 0.5 m s<inline-formula><mml:math id="M3" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, respectively (Fig. 1). Such systematic differences in regions where conventional data are sparse may be due in part to differences in the assimilation of satellite radiances at the NWP centers. Second, although corrections to several substantial sources of systematic differences in the Aeolus HLOS winds (baseline B10) have been implemented, including corrections to the dark current signal anomalies of single pixels (so-called hot pixels) on the accumulation charge-coupled devices (ACCDs), to the linear drift in the illumination of the Mie and Rayleigh spectrometers, and to the telescope M1 mirror temperature variations (Reitebuch et al., 2020; Weiler et al., 2021), uncorrected systematic differences due to potential calibration issues might remain in Aeolus HLOS winds and may contribute to potential systematic differences between Aeolus and the NWP background HLOS winds. The residual systematic differences may lead to suboptimal assimilation of Aeolus HLOS winds in NWP systems.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1"><?xmltex \currentcnt{1}?><?xmltex \def\figurename{Figure}?><label>Figure 1</label><caption><p id="d1e191">Zonal and time mean difference of ECMWF minus FV3GFS backgrounds
(defined as 6 h forecasts) for analysis times 00:00, 06:00, 12:00, and 18:00 UTC) for zonal wind (m s<inline-formula><mml:math id="M4" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>). Note that the sample in Figs. 1–15 is for 1–7 September 2019.</p></caption>
        <?xmltex \igopts{width=199.169291pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f01.png"/>

      </fig>

      <?xmltex \floatpos{h!}?><fig id="Ch1.F2" specific-use="star"><?xmltex \currentcnt{2}?><?xmltex \def\figurename{Figure}?><label>Figure 2</label><caption><p id="d1e215">Vertical and daily variations in global horizontal biases (m s<inline-formula><mml:math id="M5" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) for Mie winds <bold>(a, b)</bold> and Rayleigh winds <bold>(c, d)</bold> in ascending <bold>(a, c)</bold> and descending <bold>(b, d)</bold> orbits.</p></caption>
        <?xmltex \igopts{width=389.802756pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f02.png"/>

      </fig>

      <p id="d1e248">For clarity in the remainder of this article, certain words and phrases are
assigned specific definitions. Thus, throughout this article, the phrase
“Aeolus winds” specifically means the observations of Aeolus Level-2B (B10) HLOS winds. Similarly, the phrase “FV3GFS winds” specifically means the numerical weather prediction (NWP) background HLOS winds evaluated from the FV3GFS 6 h forecasts at the observation location and time. (In discussions of winds that are not HLOS winds, terms like <inline-formula><mml:math id="M6" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula> wind, <inline-formula><mml:math id="M7" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> wind, or wind vector are used.) Further, the phrase “Mie winds” specifically means Aeolus winds derived from Mie backscatter observations, and the phrase “Rayleigh winds” specifically means Aeolus winds derived from Rayleigh backscatter observations. Also, throughout this article, the word “innovations” without further qualification specifically refers to the differences between these Aeolus and FV3GFS winds, and the word “bias” (and the phrases “Mie bias” and “Rayleigh bias”) without further qualification specifically refers to the mean of these innovations, where the sample mean is over some specified space–time volume for either the Mie or Rayleigh winds.</p>
      <p id="d1e265">Speed-dependent biases identified and estimated using ordinary least squares
(OLS) are subject to contamination from random errors in Aeolus and/or
FV3GFS winds (Frost and Thompson, 2000), since OLS assumes no errors in the
predictor or independent variable, which in this case would be either the
Aeolus or FV3GFS winds or a combination of the two. In contrast, total least squares (TLS) regression accounts for errors in both dependent and independent variables and generates a statistically optimal analysis of the
biases (Deming, 1943; Ripley and Thompson, 1987; Markovsky and Van Huffel,
2007). For the case of Aeolus and FV3GFS winds, the use of linear TLS
regression (Ripley and Thompson, 1987) finds an optimal estimate of the true
(assumed linear) relationship between Aeolus and FV3GFS winds.</p>
      <p id="d1e268">In this study, the TLS regression approach is used to estimate biases that
depend linearly on wind speed. The suboptimality of OLS bias estimates is
demonstrated by comparison to the TLS bias estimates, which are treated as the “truth” in this study. A bias correction based on the TLS bias analysis is proposed to optimize Aeolus wind assimilation by the FV3GFS model and thus
improve the impact of Aeolus winds on FV3GFS forecasts. Section 2 describes
the Aeolus and FV3GFS winds, the TLS bias analysis method, and the estimation of the ratio of error variances of Aeolus to FV3GFS winds, for which the ratio is used in the TLS regression. Section 3 describes the variations in the TLS bias estimates with height, latitude, and wind speed. Section 4 demonstrates the substantial differences between the TLS and OLS bias estimates. Section 5 proposes a TLS bias correction for Aeolus data assimilation. The forecast impact of the TLS bias correction is presented in
Sect. 6. Section 7 presents a summary of the findings and conclusions.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Data and methodology</title>
<sec id="Ch1.S2.SS1">
  <label>2.1</label><title>Aeolus L2B and FV3GFS background wind data</title>
      <p id="d1e286">The Aeolus L2B cloudy-sky Mie winds and clear-sky Rayleigh winds are
examined for the period 1–7 September 2019. This 1-week period provides a
sufficient sample to estimate the biases. The Aeolus winds were obtained
from the Aeolus dataset (baseline B10) reprocessed by ESA (Rennie et al., 2021, Weiler et al., 2021). The reprocessing includes the M1 bias correction, which removes most of the globally and vertically averaged biases of both Mie and Rayleigh winds (Weiler et al., 2021). The Aeolus winds are reported at a standard set of vertical layers (de Kloe, 2020). This study examines Mie and Rayleigh winds within height ranges of 0–22 km that include nearly all Aeolus winds. The height is defined relative to the EGM96 geoid for the L2B winds (Tan et al., 2008).</p>
      <p id="d1e289"><?xmltex \hack{\newpage}?>The Aeolus and FV3GFS winds are obtained from a data assimilation experiment
(hereafter the BASE experiment), where the Aeolus winds are monitored, and the Aeolus wind observation operator <inline-formula><mml:math id="M8" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is applied to the
FV3GFS background <inline-formula><mml:math id="M9" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>x</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> to obtain the value of FV3GFS wind (<inline-formula><mml:math id="M10" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msup><mml:mi>x</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>)) corresponding to each Aeolus wind <inline-formula><mml:math id="M11" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>. This experiment employs the FV3GFS data assimilation system, called Global Statistical Interpolation (GSI; Kleist et al., 2009), configured for the 4DEnVar algorithm, with 64 vertical levels and horizontal resolutions of C384 (<inline-formula><mml:math id="M12" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">25</mml:mn></mml:mrow></mml:math></inline-formula> km) for the deterministic analysis and forecast and C192 (<inline-formula><mml:math id="M13" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">50</mml:mn></mml:mrow></mml:math></inline-formula> km) for the 80 ensemble members (Wang and Lei, 2014).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3"><?xmltex \currentcnt{3}?><?xmltex \def\figurename{Figure}?><label>Figure 3</label><caption><p id="d1e390">Latitudinal and height distributions of Mie biases <bold>(a, c)</bold> and Rayleigh biases <bold>(b, d)</bold> (color scale; m s<inline-formula><mml:math id="M14" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) in ascending <bold>(a, b)</bold> and descending <bold>(c, d)</bold> orbits.</p></caption>
          <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f03.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><?xmltex \def\figurename{Figure}?><label>Figure 4</label><caption><p id="d1e426">Density plots of global collocated <bold>(a)</bold> Mie and FV3GFS winds in the layer at <inline-formula><mml:math id="M15" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">3.5</mml:mn></mml:mrow></mml:math></inline-formula> km altitude and <bold>(b)</bold> Rayleigh and FV3GFS winds in the layer at <inline-formula><mml:math id="M16" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">15</mml:mn></mml:mrow></mml:math></inline-formula> km altitude in descending orbits. The TLS analysis lines (blue), the OLS regression lines of FV3GFS winds on Aeolus winds (red), and the OLS regression lines of Aeolus winds on FV3GFS winds (transformed and plotted as a function of Aeolus winds in brown) are shown, with the corresponding regression coefficients displayed above each panel.</p></caption>
          <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f04.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><?xmltex \currentcnt{5}?><?xmltex \def\figurename{Figure}?><label>Figure 5</label><caption><p id="d1e463">Density plots of global <bold>(a)</bold> Mie–FV3GFS winds in the layer at <inline-formula><mml:math id="M17" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">3.5</mml:mn></mml:mrow></mml:math></inline-formula> km altitude and <bold>(b)</bold> Rayleigh–FV3GFS winds in the
layer at <inline-formula><mml:math id="M18" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">15</mml:mn></mml:mrow></mml:math></inline-formula> km altitude in descending orbits. The average innovation (brown dots), the OLS regression lines of the innovations on Aeolus winds (brown), and TLS analysis lines (blue) are shown.</p></caption>
          <?xmltex \igopts{width=375.576378pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f05.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6"><?xmltex \currentcnt{6}?><?xmltex \def\figurename{Figure}?><label>Figure 6</label><caption><p id="d1e500">Vertical variation in the square root of the ratio of random error
variance in Mie (solid black) and Rayleigh (dashed blue) winds versus FV3GFS
winds. Results are based on global innovations from the BASE experiment
using the Hollingsworth–Lonnberg method. The symbols are plotted at the average height of the observations in each layer.</p></caption>
          <?xmltex \igopts{width=119.501575pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f06.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><?xmltex \def\figurename{Figure}?><label>Figure 7</label><caption><p id="d1e511">Vertical variations in TLS bias coefficients for Mie <bold>(a–c)</bold>, and Rayleigh <bold>(d–f)</bold> winds. Each point plotted represents a separate TLS analysis for all observations in each layer for all latitudes and for either ascending (black solid) or descending (blue dashed) orbits. The symbols are plotted at the average height of the observations in each layer.</p></caption>
          <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f07.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F8" specific-use="star"><?xmltex \currentcnt{8}?><?xmltex \def\figurename{Figure}?><label>Figure 8</label><caption><p id="d1e529">Vertical distributions of average TLS estimated biases (color
scale; m s<inline-formula><mml:math id="M19" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) for Mie <bold>(a, c)</bold> and Rayleigh <bold>(b, d)</bold> winds as a function of observed Aeolus winds (m s<inline-formula><mml:math id="M20" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) in ascending <bold>(a, b)</bold> and descending <bold>(c, d)</bold> orbits for all latitudes. The TLS estimated biases are obtained from the TLS fits displayed in Fig. 7.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f08.png"/>

        </fig>

      <p id="d1e575">Similar Aeolus data quality control procedures, as recommended by ESA and
ECMWF (Rennie et al., 2021), were implemented to reject the following
observations: the HLOS L2B confidence flag “invalid”, Rayleigh winds at layers below 850 hPa, L2B uncertainties greater than 12 m s<inline-formula><mml:math id="M21" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, accumulation lengths less than 60 km, and atmospheric pressure within 20 hPa of topographic surface pressure, and Mie winds with L2B uncertainties greater than 5 m s<inline-formula><mml:math id="M22" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> and accumulation lengths less than 5 km. Further, a standard outlier check rejects any Aeolus wind for which <inline-formula><mml:math id="M23" display="inline"><mml:mrow><mml:mo>|</mml:mo><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>|</mml:mo></mml:mrow></mml:math></inline-formula> is greater than 4 times the estimated errors for Aeolus winds prescribed by the data assimilation system.</p>
      <p id="d1e628">When examining Aeolus wind statistics, we stratify the Aeolus data by
orbital phase, either ascending when the spacecraft is moving northward or
descending when the spacecraft is moving southward. The vertical and daily
variations in Mie and Rayleigh biases for global horizontal samples are
consistent throughout the period (Fig. 2). For ascending orbits, the Mie
biases are positive above 6 km and negative below 6 km and are as large as
<inline-formula><mml:math id="M24" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1.8</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M25" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M26" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, respectively. The Mie biases are smaller and
positive at most levels in descending orbits. In descending orbits, the
Rayleigh biases are as positive as <inline-formula><mml:math id="M27" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1.2</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M28" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> above 10 km and as negative as <inline-formula><mml:math id="M29" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1.2</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M30" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> below 8 km. The positive biases in ascending orbits are smaller. The results indicate that the biases vary substantially with height and orbit phase for both Mie and Rayleigh winds. The Mie and Rayleigh biases also vary considerably with latitude (Fig. 3). Mie biases are as positive as <inline-formula><mml:math id="M31" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1.5</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M32" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in the upper troposphere, and Rayleigh biases are as positive as <inline-formula><mml:math id="M33" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2.0</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M34" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in the tropical upper troposphere. Both Mie and Rayleigh biases are as negative as <inline-formula><mml:math id="M35" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M36" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in the lowest layers.</p>
      <p id="d1e775">The statistical relationship between Aeolus and FV3GFS winds is illustrated
by the density plots in Fig. 4. There is a strong correlation of 0.93 between Mie and FV3GFS winds and of 0.96 between Rayleigh and FV3GFS winds. The average and OLS regression of the innovations as a function of Aeolus wind suggest considerable speed-dependent biases with both linear and nonlinear components (Fig. 5). In this study, we focus on the estimation and correction of the linear part of the biases using the TLS linear regression.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <label>2.2</label><title>TLS linear regression</title>
      <p id="d1e786">In this section, we review the TLS linear regression method (Ripley and
Thompson, 1987) in the context of estimating potential speed-dependent
biases. The TLS estimate for each collocated pair of Aeolus and FV3GFS winds
(<inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M38" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is defined by the following:
            <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M39" display="block"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mi mathvariant="normal">and</mml:mi><mml:mspace linebreak="nobreak" width="0.25em"/><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mo>(</mml:mo><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>,</mml:mo><mml:mi>N</mml:mi><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M40" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M41" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are the TLS estimates of the true Aeolus and FV3GFS winds, <inline-formula><mml:math id="M42" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are random errors, and <inline-formula><mml:math id="M44" display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> is the number of Aeolus/FV3GFS wind collocations in the sample. The sample might be defined by a vertical layer or a latitude band. In OLS regression, since it is assumed that there are no errors in the predictor, the predictor can be used directly to estimate the predictand. The situation is a little more complicated in TLS regression, where (<inline-formula><mml:math id="M45" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, the most probable true state, is the point on the regression line that is closest in a statistical sense to the point <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M48" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>.</p>
      <p id="d1e1032">Here it is assumed that <inline-formula><mml:math id="M49" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M50" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are independent and that the random error variance ratio <inline-formula><mml:math id="M51" display="inline"><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:mo>=</mml:mo><mml:mfenced open="(" close=")"><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:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mi>E</mml:mi><mml:mfenced close="]" open="["><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:mfenced><mml:mo>/</mml:mo><mml:mi>E</mml:mi><mml:mfenced open="[" close="]"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is known. The error variance ratio <inline-formula><mml:math id="M52" display="inline"><mml:mi mathvariant="italic">δ</mml:mi></mml:math></inline-formula> is a crucial parameter in determining the TLS bias analysis and is estimated as described in the next section. Furthermore, the true relationship between the Aeolus and FV3GFS winds is assumed to be described by a linear function (as seen in
Fig. 5) as follows:
            <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M53" display="block"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mo>(</mml:mo><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>,</mml:mo><mml:mi>N</mml:mi><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is an offset or constant coefficient, and <inline-formula><mml:math id="M55" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is a
speed-dependent coefficient.
<?xmltex \hack{\newpage}?></p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9" specific-use="star"><?xmltex \currentcnt{9}?><?xmltex \def\figurename{Figure}?><label>Figure 9</label><caption><p id="d1e1220">TLS estimated biases (m s<inline-formula><mml:math id="M56" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) before (brown lines) and after (blue lines) TLS bias correction for Mie <bold>(a)</bold> and Rayleigh <bold>(b)</bold> winds as a function of the observed Aeolus winds (m s<inline-formula><mml:math id="M57" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>), vertically averaged for all latitudes of Aeolus winds. The solid and dashed lines are for ascending and descending orbits, respectively. The black lines report the number of Aeolus winds in each 2 m s<inline-formula><mml:math id="M58" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> bin.</p></caption>
          <?xmltex \igopts{width=384.112205pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f09.png"/>

        </fig>

      <p id="d1e1272">The TLS regression finds an optimal estimate of the <inline-formula><mml:math id="M59" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>,
<inline-formula><mml:math id="M60" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, and <inline-formula><mml:math id="M61" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> by minimizing the cost function <inline-formula><mml:math id="M62" display="inline"><mml:mi>J</mml:mi></mml:math></inline-formula>, as follows:
            <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M63" display="block"><mml:mtable rowspacing="0.2ex" class="split" displaystyle="true" columnalign="right left"><mml:mtr><mml:mtd><mml:mrow><mml:mi>J</mml:mi></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:mo>=</mml:mo><mml:msubsup><mml:mo>∑</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:msubsup><mml:mfenced close=")" open="("><mml:mrow><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</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:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>/</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfenced></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:msubsup><mml:mo>∑</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:msubsup><mml:mfenced open="(" close=""><mml:mrow><mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfenced></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mfenced open="" close=")"><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfenced><mml:mo>.</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
          To determine the <inline-formula><mml:math id="M64" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, the derivative of <inline-formula><mml:math id="M65" display="inline"><mml:mi>J</mml:mi></mml:math></inline-formula> with respect to <inline-formula><mml:math id="M66" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is set to zero, resulting in the following:
            <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M67" display="block"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mfenced close=")" open="("><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mfenced open="(" close=")"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:mfenced><mml:mo>+</mml:mo><mml:mi mathvariant="italic">δ</mml:mi><mml:msubsup><mml:mi>y</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:mfenced><mml:mo>/</mml:mo><mml:mfenced close=")" open="("><mml:mrow><mml:msubsup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>+</mml:mo><mml:mi mathvariant="italic">δ</mml:mi></mml:mrow></mml:mfenced><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mo>(</mml:mo><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>,</mml:mo><mml:mi>N</mml:mi><mml:mo>)</mml:mo><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Equation (4) thereby reduces the problem to a minimization in terms of <inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M69" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. A similar equation holds even if the error variances vary with <inline-formula><mml:math id="M70" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>, but then there is no closed form solution for <inline-formula><mml:math id="M71" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M72" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> as there is in the current case, which is known as the Deming problem (Ripley and Thompson, 1987). When the coefficients <inline-formula><mml:math id="M73" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M74" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> are obtained, the TLS estimate for the new or within-sample observation is given by Eq. (4). Finally, the estimate of the bias for the <inline-formula><mml:math id="M75" display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula>th observation, either for a new or within-sample observation, is given by the following:
            <disp-formula id="Ch1.E5" content-type="numbered"><label>5</label><mml:math id="M76" display="block"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>d</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>k</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>k</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>k</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>k</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Given the form of Eq. (5), we will refer to <inline-formula><mml:math id="M77" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and (<inline-formula><mml:math id="M78" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> as the offset and speed-dependent bias coefficients, respectively, hereafter.</p>
</sec>
<sec id="Ch1.S2.SS3">
  <label>2.3</label><title>Estimation of the random error variance ratio</title>
      <p id="d1e1812">In this study, errors of Aeolus winds are estimated by the Hollingsworth–Lonnberg method (Hollingsworth and Lonnberg, 1986; Garrett et
al., 2022), which include Aeolus instrument errors and forward modeling error and representativeness errors of the FV3GFS background at the specific 25 km horizontal resolution. The random error variance ratio <inline-formula><mml:math id="M79" display="inline"><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:mo>=</mml:mo><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:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> in the TLS bias analysis is estimated from the innovations from the BASE experiment for 1–7 September 2019. It is assumed that there are no correlations between the random errors of the Aeolus and FV3GFS winds and no horizontal correlations between the random errors of Aeolus winds separated by more than 90 km. These assumptions are justified a posteriori by the reasonable error estimate of FV3GFS background winds (Garrett et al., 2022).</p>
      <p id="d1e1844">Global error estimates are calculated for all Mie and Rayleigh winds in each
layer as follows. First, the spatial covariance of the innovations is
calculated. Since these are innovations from the BASE experiment where
Aeolus data are not assimilated, it is reasonable to assume that the Aeolus
and FV3GFS wind errors are uncorrelated. Then the spatial covariance of the
innovations, <inline-formula><mml:math id="M80" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">o</mml:mi><mml:mo>-</mml:mo><mml:mi mathvariant="normal">b</mml:mi></mml:mrow></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, at zero separation distance,
is equal to the following:
            <disp-formula id="Ch1.E6" content-type="numbered"><label>6</label><mml:math id="M81" display="block"><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">o</mml:mi><mml:mo>-</mml:mo><mml:mi mathvariant="normal">b</mml:mi></mml:mrow></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mo>)</mml:mo><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="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> and <inline-formula><mml:math id="M83" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> are the
random error standard deviations of Aeolus and FV3GFS winds, respectively.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F10" specific-use="star"><?xmltex \currentcnt{10}?><?xmltex \def\figurename{Figure}?><label>Figure 10</label><caption><p id="d1e1949">Latitudinal variation in TLS bias coefficients for Mie <bold>(a–c)</bold> and Rayleigh <bold>(d–f)</bold> winds. Each point plotted represents a separate TLS analysis for all observations in all vertical layers in a 10<inline-formula><mml:math id="M84" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> latitude band for either ascending (black solid) or
descending (blue dashed) orbits. The latitude bands are centered every 10<inline-formula><mml:math id="M85" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> from 90<inline-formula><mml:math id="M86" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S to 90<inline-formula><mml:math id="M87" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N. The symbols are plotted at the center in each latitude band. The vertical layers are 0–16 km for Mie winds and 3–22 km for Rayleigh winds.</p></caption>
          <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f10.png"/>

        </fig>

      <p id="d1e2002">By assumption, at separation distances greater than 90 km, the innovation
covariances are estimates of the FV3GFS wind error covariance alone and can
be extrapolated back to zero separation to obtain an estimate of the error
variance of the FV3GFS winds, <inline-formula><mml:math id="M88" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, and then,
using Eq. (6), the error variance of the Aeolus winds, <inline-formula><mml:math id="M89" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, may be determined. Note that this can only be done
using innovation covariances at separation distances large enough to have
negligible covariances between the Aeolus winds. Since the calculated
innovation covariances are globally averaged over all HLOS winds, it is not
surprising that the corresponding biases are small. The small residual
biases in the innovations may introduce small (<inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">0.1</mml:mn></mml:mrow></mml:math></inline-formula>) spurious spatial correlations. This spurious correlation, taken as the value calculated for the last bin (at 990 km), is removed from the correlation curves at all separation distances. The estimated random error variance ratio <inline-formula><mml:math id="M91" display="inline"><mml:mi mathvariant="italic">δ</mml:mi></mml:math></inline-formula> is assigned to the layer center height, defined as the global average heights of the Mie and Rayleigh wind in each vertical range bin. Figure 6 shows that the vertical profiles of the square root of <inline-formula><mml:math id="M92" display="inline"><mml:mi mathvariant="italic">δ</mml:mi></mml:math></inline-formula> vary in the range of 1.2–1.6 for Mie winds versus FV3GFS winds and 2–3 for Rayleigh winds versus FV3GFS winds, respectively.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F11" specific-use="star"><?xmltex \currentcnt{11}?><?xmltex \def\figurename{Figure}?><label>Figure 11</label><caption><p id="d1e2067">Latitudinal distributions of average TLS estimated biases (color
scale; m s<inline-formula><mml:math id="M93" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) for Mie <bold>(a, c)</bold> and Rayleigh <bold>(b, d)</bold> winds as a function of Aeolus wind in ascending <bold>(a, b)</bold> and descending <bold>(c, d)</bold> orbits, obtained from the TLS fits displayed in Fig. 10.</p></caption>
          <?xmltex \igopts{width=389.802756pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f11.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F12" specific-use="star"><?xmltex \currentcnt{12}?><?xmltex \def\figurename{Figure}?><label>Figure 12</label><caption><p id="d1e2102">Vertical distributions of average bias estimates (color scale; m s<inline-formula><mml:math id="M94" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) for Mie <bold>(a, c, e)</bold> and Rayleigh <bold>(b, d, f)</bold> winds as a function of Aeolus winds using one of three methods for descending orbits for all latitudes. The methods are OLS using FV3GFS winds as a <?xmltex \hack{\mbox\bgroup}?>predictor <bold>(a, b)</bold>,<?xmltex \hack{\egroup}?> TLS (<bold>c, d</bold>; same as the bottom panels of Fig. 8), and OLS using the average of Aeolus and FV3GFS as a predictor <bold>(e, f)</bold>.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f12.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F13" specific-use="star"><?xmltex \currentcnt{13}?><?xmltex \def\figurename{Figure}?><label>Figure 13</label><caption><p id="d1e2145">Vertical distributions of average TLS estimated biases (color
scale; m s<inline-formula><mml:math id="M95" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) for Mie <bold>(a, c)</bold> and Rayleigh <bold>(b, d)</bold> winds as a function of Aeolus winds (m s<inline-formula><mml:math id="M96" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) in the latitudinal bands centered at the Equator <bold>(a, b)</bold> and at 80 S <bold>(c, d)</bold> for the descending orbits.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f13.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F14" specific-use="star"><?xmltex \currentcnt{14}?><?xmltex \def\figurename{Figure}?><label>Figure 14</label><caption><p id="d1e2194">As in Fig. 8 but for the mean innovation after the TLS bias
correction is applied. For each 6 h cycle during 1–7 September 2019, the TLS bias correction is calculated from the 28 preceding 6 h cycles.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f14.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F15"><?xmltex \currentcnt{15}?><?xmltex \def\figurename{Figure}?><label>Figure 15</label><caption><p id="d1e2205">As in Fig. 3 but after the TLS bias correction is applied.</p></caption>
          <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f15.png"/>

        </fig>

      <p id="d1e2214">In the future, we plan to explore the benefit of the scene-dependent L2B
estimated errors on the TLS bias estimates and Aeolus wind assimilation.</p><?xmltex \hack{\newpage}?>
</sec>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>The TLS bias estimates</title>
      <p id="d1e2227">In this section, variations in the TLS bias estimates with orbital phase and
height are examined to motivate the use of a TLS bias correction scheme
proposed in Sect. 5.</p>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Variation in TLS bias estimates with height</title>
      <p id="d1e2237">The variation in the TLS solution with height and orbital phase is described
here. The TLS samples include winds at all latitudes in each layer. The
vertical distribution of the TLS constant and speed-dependent bias analysis
coefficients in Eq. (5) is shown in Fig. 7. The speed-dependent bias
coefficient (<inline-formula><mml:math id="M97" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> varies substantially with height and orbital phase.
For Mie winds, this coefficient is quite large at most heights, ranging from
3 % to 6 %, with maxima at 3 and 12–16 km. For Rayleigh winds, this
coefficient is smaller and ranges from 1 % to 3 % in ascending orbits
and 1 %–5 % in descending orbits, with maxima around 3.5 and 16 km.</p>
      <p id="d1e2257">The offset bias coefficient <inline-formula><mml:math id="M98" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> for both Mie and Rayleigh winds also shows large variations with height and orbit, with its value as large as <inline-formula><mml:math id="M99" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M100" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. In general, the offset bias coefficient
is positive in upper layers and negative in layers close to the Earth's
surface, consistent with the patterns seen in the global horizontal average
of the innovations in Fig. 2. The vertical distribution of the average TLS
bias estimate as a function of Aeolus wind is shown in Fig. 8. The biases
vary substantially with height. Since the TLS biases are in part dependent
on speed, at most heights the biases increase substantially as the magnitude
of Aeolus wind speed increases. The biases at the extreme Aeolus wind speeds
are as large as <inline-formula><mml:math id="M101" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2.5</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M102" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M103" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> for Mie winds and <inline-formula><mml:math id="M104" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1.5</mml:mn></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math id="M105" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M106" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> for Rayleigh winds. There are clear speed-dependent biases in the vertical average of these biases as well (Fig. 9). The results suggest that the innovations have both vertically varying and vertically averaged speed-dependent biases.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F16" specific-use="star"><?xmltex \currentcnt{16}?><?xmltex \def\figurename{Figure}?><label>Figure 16</label><caption><p id="d1e2360">The summary assessment metric (SAM) overall forecast scores for
AEOM and AEOT versus BASE experiments in the North American (NA) region for day 1–7 forecasts validated at 00:00 UTC 22–28 November 2019. The scores are shown for <bold>(a)</bold> forecast parameters of temperature (Temp), geopotential height (HGT), vector wind (Wind), relative humidity (RH), <bold>(b)</bold> lead times, and <bold>(c)</bold> the overall performance of AEOM and AEOT. The forecasts are verified to their self-analyses. Values above 0.0 demonstrate an increase in the mean of the normalized distribution and improvement of the forecast versus the BASE, while the shaded region represents the 95 % significance level. The gray areas indicate the 95 % confidence level under the null hypothesis that there is no difference between experiments for this metric. In addition, the estimated uncertainty at the 95 % level is indicated by small error bars at the ends of the color bars. In total, two normalizations are used, i.e., the ECDF (colors) and rescaled min/max normalization (black outline). Details can be found in Hoffman et al. (2018). A value of 0.02, for example, indicates the average normalized statistic over all statistics is better (greater) by 0.02 than BASE. Under the null hypothesis that there are no differences, all SAMs would be one-half, so a 0.02 improvement can be considered a 4 % improvement (<inline-formula><mml:math id="M107" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.02</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn></mml:mrow></mml:math></inline-formula>) in normalized scores.</p></caption>
          <?xmltex \igopts{width=284.527559pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f16.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F17" specific-use="star"><?xmltex \currentcnt{17}?><?xmltex \def\figurename{Figure}?><label>Figure 17</label><caption><p id="d1e2393">The 200–1000 hPa vertically integrated water vapor transport
(IVT; kg m s<inline-formula><mml:math id="M108" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>; contour) and wind vectors (m s<inline-formula><mml:math id="M109" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>; arrows) in the day 7 forecasts, validated at 00:00 UTC on 27 <bold>(a, c, e</bold>) and on 28 <bold>(b, d, f)</bold> November 2019 for <bold>(a, b)</bold> BASE, <bold>(c, d)</bold> AEOM, <bold>(e, f)</bold> AEOT, <?xmltex \hack{\mbox\bgroup}?>and <bold>(g, h)</bold> ECMWF<?xmltex \hack{\egroup}?> analyses.</p></caption>
          <?xmltex \igopts{width=412.564961pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f17.png"/>

        </fig>

</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Variation in biases with latitude</title>
      <p id="d1e2457">The variation in the TLS solution with latitude and orbital phase is
described here. For this purpose, the samples include all heights in each
10<inline-formula><mml:math id="M110" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> latitude band, and the vertical average of the error ratio
<inline-formula><mml:math id="M111" display="inline"><mml:mi mathvariant="italic">δ</mml:mi></mml:math></inline-formula> is used. In general, the bias coefficients obtained are
large and vary considerably with latitude and orbital phase, with maxima
found in the tropics (Fig. 10). For example, the speed-dependent bias
coefficient (<inline-formula><mml:math id="M112" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> for Mie winds in the tropics can be quite large,
ranging up to a maximum of 11 %. This coefficient is smaller for Rayleigh
winds, ranging from <inline-formula><mml:math id="M113" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> % to 5 %, with maxima found in the tropics. The offset bias coefficient <inline-formula><mml:math id="M114" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> for Mie winds also varies considerably
with latitude and orbit, ranging from <inline-formula><mml:math id="M115" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula> to <inline-formula><mml:math id="M116" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1.6</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M117" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. The offset bias coefficient <inline-formula><mml:math id="M118" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is smaller for Rayleigh winds.</p>
      <p id="d1e2558"><?xmltex \hack{\newpage}?>The latitudinal distribution of the average TLS bias as a function of Aeolus
wind speed is shown in Fig. 11. For both Mie and Rayleigh winds, the average
TLS biases increase considerably at most latitudes as the magnitude of
Aeolus wind speed increases, particularly in the tropics and SH, with
extreme values of about <inline-formula><mml:math id="M119" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1.5</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M120" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>.</p>
</sec>
<sec id="Ch1.S3.SS3">
  <label>3.3</label><title>Discussion</title>
      <p id="d1e2592">The results indicate that the speed-dependent bias coefficient (<inline-formula><mml:math id="M121" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>
is quite large, reaching <inline-formula><mml:math id="M122" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">10</mml:mn></mml:mrow></mml:math></inline-formula> % and 5 % for Mie and
Rayleigh winds, respectively, particularly in the lower stratosphere and
lower troposphere of the tropics. This suggests that there exist large
speed-dependent biases in the FV3GFS and/or Aeolus winds. Given that there
exist large uncertainties in the FV3GFS (and ECMWF) background winds in the
tropics (see Fig. 1), it is likely that the FV3GFS background may be a
significant source of the biases, and this will require further investigation. In any case, these large speed-dependent biases should be
corrected to optimize Aeolus wind assimilation and the impact of Aeolus
winds on NWP forecasts. The large variations in the TLS bias estimates with
latitude and height guide the design of the proposed TLS bias correction in
Sect. 5.</p>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Comparison to OLS regressions</title>
      <p id="d1e2631">Parallel OLS regressions using three different predictors of the biases are
compared with the TLS bias estimate results presented in Sect. 3. The OLS
predictors are the FV3GFS winds, the Aeolus winds, and their average. The
first two of these OLS regressions are equivalent to OLS regressing Aeolus
winds on FV3GFS winds and OLS regressing FV3GFS winds on Aeolus winds. The
regression lines of these two cases are added to Fig. 4. The TLS speed-dependent coefficient (<inline-formula><mml:math id="M123" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> (in Eq. 5) is 6 % and 4 % for
Mie and Rayleigh winds, respectively. However, the OLS regression of Aeolus
winds on FV3GFS winds produces considerably smaller bias estimates, with
<inline-formula><mml:math id="M124" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> estimated as 1 % and 2 % for Mie and Rayleigh winds, respectively. On the other hand, the OLS regression of the FV3GFS winds on Aeolus winds exhibits much larger bias estimates relative to the TLS bias analysis, with <inline-formula><mml:math id="M125" display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> estimated as 18 % and 15 % for Mie and Rayleigh winds, respectively.</p>
      <p id="d1e2689">The vertical distributions of the average biases as a function of Aeolus
winds are shown in Fig. 12 for the descending orbits for the following three methods: (1) OLS regression using FV3GFS winds as a predictor (top row), (2) TLS regression (middle row, which repeats the bottom two panels of Fig. 8), and (3) OLS regression using the average of FV3GFS and Aeolus as a predictor (bottom row). The average bias estimates in the top panels are about 0.5 m s<inline-formula><mml:math id="M126" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> smaller in magnitude in most layers compared to the middle panels. The average biases in the bottom panels are about 0.5–1.0 m s<inline-formula><mml:math id="M127" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in magnitude larger than the middle panels in most layers, particularly for Rayleigh winds. The bias estimates of OLS regression using Aeolus winds only as a predictor (not shown) are even larger than what is shown in the bottom panels. The large differences in the bias estimates using the TLS and OLS regression are due to the fact that both Aeolus and FV3GFS winds have large errors. If the predictor (either Aeolus or FV3GFS winds) has very small errors, then the OLS regressions would be close to perfect, and the OLS and TLS regressions would give very similar results. In such situation, the random error ratio would be either infinity small (<inline-formula><mml:math id="M128" display="inline"><mml:mrow><mml:mo>≪</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>) or infinity large (<inline-formula><mml:math id="M129" display="inline"><mml:mrow><mml:mo>≫</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>). However, the Aeolus and FV3GFS winds have considerable errors, and the actual random error ratio is about 2–3 for the Rayleigh winds versus FV3GFS winds and about 1.2–1.5 for the Mie winds versus FV3GFS winds (Fig. 6). This leads to the large differences in the OLS and TLS bias estimates. Specifically, the OLS bias estimates using Aeolus winds as a predictor have larger differences from the TLS estimates than the OLS estimates using FV3GFS winds as a predictor.</p>
</sec>
<sec id="Ch1.S5">
  <label>5</label><title>A TLS bias correction</title>
      <p id="d1e2745">In this section, a TLS bias correction is proposed to optimize Aeolus wind
data assimilation. Because the findings in Sect. 3 show substantial variation in the bias coefficients with latitude, vertical layer, and orbital phase, the TLS bias coefficients are calculated from the winds in 19 discrete bins of latitude (centered every 10<inline-formula><mml:math id="M130" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> between 90<inline-formula><mml:math id="M131" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S to 90<inline-formula><mml:math id="M132" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N) for each vertical range/layer and for ascending and descending orbits separately. The error ratio <inline-formula><mml:math id="M133" display="inline"><mml:mi mathvariant="italic">δ</mml:mi></mml:math></inline-formula> shown in Fig. 6 is used in all latitude bands for each layer. For each assimilation cycle, the bias coefficients are computed by TLS regression for the innovations in the week before the cycle (i.e., for the previous 28 cycles). The period of 1 week provides a large enough sample for the regression. As shown by Ripley and Thompson (1987), the TLS solution only involves solving a quadratic equation with coefficients given by sample sums. Therefore, an efficient approach is to calculate and save these sums for every cycle and accumulate them over the 28 cycles. For each of the innovations in the assimilation cycle, values of the TLS regression coefficients <inline-formula><mml:math id="M134" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M135" display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> are linearly interpolated to the latitude of the Aeolus observation. Subsequently, the TLS estimated bias, calculated using Eq. (5), is subtracted from the innovation. Note that the bias correction is determined by the TLS analysis solution for <inline-formula><mml:math id="M136" display="inline"><mml:mrow><mml:msubsup><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>k</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> that, in turn, is determined from the observation and background wind, <inline-formula><mml:math id="M137" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>k</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M138" display="inline"><mml:mrow><mml:msubsup><mml:mi>y</mml:mi><mml:mi>k</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, following Eq. (4).</p>
      <p id="d1e2847"><?xmltex \hack{\newpage}?>The proposed scheme is applied to the Aeolus and FV3GFS winds of the BASE
experiment. As expected, the corresponding TLS bias estimates show
considerable speed-dependent biases. For example, in the bins centered at
the Equator and 80<inline-formula><mml:math id="M139" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S, where the speed-dependent biases are
expected to be largest based on Fig. 9, the TLS bias estimates vary
considerably with speed and are in some cases larger in magnitude than 1.5 m s<inline-formula><mml:math id="M140" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> at higher Aeolus wind magnitudes (Fig. 13).</p>
      <p id="d1e2872">The vertical distribution of the global average of the remaining biases
(i.e., after TLS bias correction) as a function of Aeolus wind is shown in
Fig. 14, which is in the same format and for the same sample of observations
as Fig. 8. A comparison of these two figures reveals that most of the biases
are removed by the proposed TLS bias correction. The latitudinal variations
in the biases are also corrected (Fig. 15). In addition, the biases in the
vertical average are also mostly removed, as shown in Fig. 9.</p>
</sec>
<sec id="Ch1.S6">
  <label>6</label><title>Impact of the TLS bias correction on forecast skill</title>
      <p id="d1e2883">Several observing system experiments (OSEs) using the NOAA global data
assimilation system are performed using the Aeolus winds with and without
the TLS bias correction. For the period of 2 August–16 September 2019,
Garrett et al. (2022) demonstrate the positive impact of Aeolus winds on the NOAA global forecast. The largest impact is seen in the tropical upper
troposphere and lower stratosphere where the day 1–3 wind vector forecast root mean square error (RMSE) is reduced by up to 4 %. Specifically, the assimilation of Aeolus impacts the steering currents ambient to tropical cyclones, resulting in up to a 20 % reduction in track forecast error in the eastern Pacific and Atlantic basins. The application of TLS bias correction increases the positive impact of Aeolus data assimilation on the forecasts.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F18"><?xmltex \currentcnt{18}?><?xmltex \def\figurename{Figure}?><label>Figure 18</label><caption><p id="d1e2888">The 24 h accumulated precipitation (mm) for 156 to 180 h,
averaged for the forecasts validated from 12:00 UTC 26 to 28 November 2019
for <bold>(a)</bold> BASE, <bold>(b)</bold> AEOM, <bold>(c)</bold> AEOT, and <bold>(d)</bold> the National Centers for Environmental Prediction (NCEP) precipitation rain gauge data analysis.</p></caption>
        <?xmltex \igopts{width=213.395669pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f18.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F19" specific-use="star"><?xmltex \currentcnt{19}?><?xmltex \def\figurename{Figure}?><label>Figure 19</label><caption><p id="d1e2911">The forecast skill scores for 24 h accumulated precipitation for
156 to 180 h forecasts validated from 12:00 UTC on 26–28 November 2019. The equitable threat <bold>(a)</bold> and bias score <bold>(b)</bold> are measures of the forecast skill for location and amount of precipitation, respectively. The differences relative to the BASE and the statistical significances are shown in panels <bold>(c)</bold> and <bold>(d)</bold>, respectively. The equitable threat and bias scores closer to 1.0 indicate improved precipitation forecast skill.</p></caption>
        <?xmltex \igopts{width=406.874409pt}?><graphic xlink:href="https://amt.copernicus.org/articles/15/3925/2022/amt-15-3925-2022-f19.png"/>

      </fig>

      <p id="d1e2933">OSE results for a 2019 record-breaking winter storm case over the USA are
reported here. On 26 November 2019, one major storm approached the West
Coast of the USA from the eastern Pacific and produced a record-breaking low
pressure of 973 hPa and wind gust of 171 km h<inline-formula><mml:math id="M141" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> near the Oregon/California border. Over the next few days, the low merged with the subtropical jet as it tracked eastward across the USA. The combination of cold air, moisture, and high winds produced snow blizzard conditions across the USA.</p>
      <p id="d1e2948">As in Garrett et al. (2022), the OSEs include the baseline experiment (BASE)
without the assimilation of Aeolus winds, the experiment AEOM that is identical to BASE except that Aeolus winds are assimilated, and the experiment AEOT hat is identical to AEOM, except that it also includes the TLS bias correction. A difference summary assessment metric (SAM; Hoffman et al., 2018) is computed for day 1–7 forecasts in the North American (NA) region of the experiments validated at 00:00 UTC on 22–28 November 2019. The SAM illustrates the overall forecast skill by normalizing the AC and RMSE values for each parameter (temperature, geopotential height, wind, and relative humidity) and each lead time. Figure 16 shows that the TLS bias correction improves the impact of Aeolus winds on the forecasts of wind, temperature, and geopotential height for day 3–7 and especially for day 5–7 lead times. The overall improvement of Aeolus winds for AEOM and AEOT is about 4 % and 10 %, respectively (above the 95 % significance level, Fig. 16c), illustrating the usefulness of the TLS bias correction.</p>
      <p id="d1e2951">The vertically integrated water vapor transport (IVT) is a useful metric in
forecasting precipitation associated with winter storms (e.g., Lavers et al.,
2017). The IVTs of the day 7 forecast for the experiments validated for 00:00 UTC on 27 and 28 November are shown in Fig. 17. Aeolus winds have a strong impact on the locations and intensities of the IVT maxima near the USA West Coast and in the Midwest. In general, the IVTs are closer to the ECMWF
analyses in AEOT than in AEOM. As a result, Aeolus winds show strong impact
on the locations and corresponding amounts of precipitation, as seen in Fig. 18 and quantified by the equitable threat and BIAS skill scores
(<uri>https://www.wpc.ncep.noaa.gov/rgnscr/verify.html</uri>, last access: 15 January 2022, Wang, 2014),
respectively (Fig. 19). Specifically, the precipitation amounts near the
West Coast and the Midwest are much less in AEOT than in BASE and AEOM. The
precipitation in the Midwest also shifts eastward in AEOT, compared to BASE
and AEOM (Fig. 18). The precipitation forecast skills (verified against NCEP
precipitation rain gauge data analyses) over the contiguous United States
(CONUS) region, that is, the equitable threat (location) and BIAS (amount)
scores are shown in Fig. 19. The precipitation amount is overpredicted (BIAS
score <inline-formula><mml:math id="M142" display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">1.0</mml:mn></mml:mrow></mml:math></inline-formula>) in both BASE and AEOM but is closer to the analysis
(BIAS score closer to 1.0) in AEOT. The equitable threat is larger (with
marginal significance level; Fig. 19c) in AEOT than in BASE and AEOM,
indicating that the location of precipitation in the forecast is improved in
AEOT. These results suggest the potential benefit of the TLS bias correction to precipitation forecasts.</p>
</sec>
<sec id="Ch1.S7" sec-type="conclusions">
  <label>7</label><title>Summary and conclusions</title>
      <p id="d1e2975">In this study, a TLS linear regression is used to optimally estimate
speed-dependent linear biases in the Aeolus innovations. The Aeolus and
FV3GFS winds for 1–7 September 2019 are analyzed. Clear speed-dependent
linear biases for both Mie and Rayleigh winds are found, particularly in the
lower troposphere and stratosphere of the tropics and Southern Hemisphere.
The largest biases are about 10 % and 5 % of FV3GFS wind speed and are as large as <inline-formula><mml:math id="M143" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">2.5</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M144" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1.5</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M145" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> at high Aeolus wind magnitudes for Mie and Rayleigh winds, respectively.</p>
      <p id="d1e3010">It is found that the TLS linear bias estimates are considerably larger than
the OLS regression of Aeolus innovations on FV3GFS winds. However, they are
much smaller than the OLS regression on both Aeolus winds only and on the
average of Aeolus and FV3GFS winds. This is more evident for the Rayleigh
winds.</p>
      <p id="d1e3013">The proposed TLS bias correction removes much of the biases in the
innovations before Aeolus wind assimilation. In a companion paper, Garrett
et al. (2022) demonstrate that the application of this TLS bias correction
considerably enhances the positive impact of Aeolus winds on NOAA FV3GFS
global and tropical cyclone forecasts for the period of 2 August to 15
September 2019. In this study, it is also demonstrated that the application
of the TLS bias correction improves the impact of Aeolus winds on the
forecast of a record-breaking 2019 winter storm, including the associated
precipitation over the USA. It is expected that the application of the TLS
bias correction can improve and enhance Aeolus data impacts on the analysis
and forecast skill of other NWP systems. It should be noted that the
proposed TLS approach presented here might be applied to other types of
observations that have errors typically characterized as a percentage of the
observed value, including quantities related to the concentrations or mass
fractions of chemical species or hydrometeors or quantities like radio
occultation refractivity and bending angle.</p>
</sec>

      
      </body>
    <back><notes notes-type="codeavailability"><title>Code availability</title>

      <p id="d1e3020">The Aeolus data assimilation code with NOAA GSI data assimilation system is publicly available from <uri>https://essic.umd.edu/joom2/index.php/faculty-and-staff?layout=user&amp;user_id=1020&amp;dir=JSROOT%2Fhliu6/CODE</uri> (Liu et al., 2022).</p>
  </notes><notes notes-type="dataavailability"><title>Data availability</title>

      <p id="d1e3029">The Aeolus L2B Earth Explorer data used in this study are publicly available and can be accessed via the ESA Aeolus Online Dissemination System (<uri>https://aeolus-ds.eo.esa.int/oads/access/</uri>; European Space Agency, 2020). The data related to the Aeolus assimilation experiment outputs are not publicly available due to the huge volume of data. We will try to provide access to the data upon request.</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e3038">KG and KI proposed the project as co-investigators thereby acquiring funding for the project. KG and KI  provided the expertise and project management that guided this work. KG and HL designed and interpreted the Aeolus assimilation experiments. HL and RNH developed the TLS bias correction. HL wrote the initial manuscript, RNH and KEL helped him to revise and edit the manuscript, and all the authors reviewed the manuscript.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d1e3044">The contact author has declared that none of the authors has any competing interests.</p>
  </notes><notes notes-type="disclaimer"><title>Disclaimer</title>

      <p id="d1e3050">The scientific results and conclusions, as well as any views or opinions expressed herein, are those of the author(s) and do not necessarily reflect those of NOAA or the U.S. Department of Commerce.
<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>
Publisher’s note: Copernicus Publications remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.</p>
  </notes><notes notes-type="sistatement"><title>Special issue statement</title>

      <p id="d1e3060">This article is part of the special issue “Aeolus data and their application (AMT/ACP/WCD inter-journal SI)”. It is not associated with a conference.</p>
  </notes><ack><title>Acknowledgements</title><p id="d1e3066">The authors thank the two anonymous reviewers, for their careful and helpful
reviews. This work has been supported by the NOAA/NESDIS Office of Projects,
Planning, and Acquisition (OPPA) Technology Maturation Program (TMP),
managed by Patricia Weir and Nai-Yu Wang. The authors would
like to acknowledge Michael Rennie and Lars Isaksen (ECMWF), for their
comments and suggestions on the assimilation of Aeolus observations, and
William McCarty with NASA/GMAO, for providing earlier versions of the GSI
with Aeolus ingest and observation operator capability. The Aeolus L2B BUFR
data were provided by ECMWF.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e3071">This research has been supported by the National Oceanic and Atmospheric Administration, National Environmental Satellite, Data, and Information Service (grant nos. NA14NES4320003 and NA19NES4320002).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e3077">This paper was edited by Ad Stoffelen and reviewed by two anonymous referees.</p>
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