<?xml version="1.0" encoding="UTF-8"?>
<!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" article-type="research-article"><?xmltex \bartext{Development and technical paper}?>
  <front>
    <journal-meta><journal-id journal-id-type="publisher">GMD</journal-id><journal-title-group>
    <journal-title>Geoscientific Model Development</journal-title>
    <abbrev-journal-title abbrev-type="publisher">GMD</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Geosci. Model Dev.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">1991-9603</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/gmd-16-1823-2023</article-id><title-group><article-title>Estimation of CH<inline-formula><mml:math id="M1" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emission based on an advanced 4D-LETKF assimilation system</article-title><alt-title>Estimation of CH<inline-formula><mml:math id="M2" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emission based on an advanced 4D-LETKF assimilation system</alt-title>
      </title-group><?xmltex \runningtitle{Estimation of CH${}_{{4}}$ emission based on an advanced 4D-LETKF assimilation system}?><?xmltex \runningauthor{J. S. H. Bisht et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Bisht</surname><given-names>Jagat S. H.</given-names></name>
          <email>jagatbisht@jamstec.go.jp</email><email>jshbisht@gmail.com</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Patra</surname><given-names>Prabir K.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-5700-9389</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Takigawa</surname><given-names>Masayuki</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-5666-6026</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Sekiya</surname><given-names>Takashi</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-2319-7753</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Kanaya</surname><given-names>Yugo</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Saitoh</surname><given-names>Naoko</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff3">
          <name><surname>Miyazaki</surname><given-names>Kazuyuki</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-1466-4655</ext-link></contrib>
        <aff id="aff1"><label>1</label><institution>Research Institute for Global Change, JAMSTEC, Yokohama, 235-0019,
Japan</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Center for Environmental Remote Sensing, Chiba University, Chiba,
263-8522, Japan</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>Jet Propulsion Laboratory, California Institute for Technology, Pasadena, CA, USA</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Jagat S. H. Bisht (jagatbisht@jamstec.go.jp, jshbisht@gmail.com)</corresp></author-notes><pub-date><day>31</day><month>March</month><year>2023</year></pub-date>
      
      <volume>16</volume>
      <issue>6</issue>
      <fpage>1823</fpage><lpage>1838</lpage>
      <history>
        <date date-type="received"><day>30</day><month>July</month><year>2022</year></date>
           <date date-type="rev-request"><day>15</day><month>August</month><year>2022</year></date>
           <date date-type="rev-recd"><day>23</day><month>February</month><year>2023</year></date>
           <date date-type="accepted"><day>7</day><month>March</month><year>2023</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2023 </copyright-statement>
        <copyright-year>2023</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://gmd.copernicus.org/articles/.html">This article is available from https://gmd.copernicus.org/articles/.html</self-uri><self-uri xlink:href="https://gmd.copernicus.org/articles/.pdf">The full text article is available as a PDF file from https://gmd.copernicus.org/articles/.pdf</self-uri>
      <abstract><title>Abstract</title>

      <p id="d1e168">Methane (CH<inline-formula><mml:math id="M3" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>) is the second major greenhouse gas after carbon dioxide
(CO<inline-formula><mml:math id="M4" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:math></inline-formula>) which has substantially increased during recent decades in the
atmosphere, raising serious sustainability and climate change issues. Here,
we develop a data assimilation system for in situ and column-averaged
concentrations using a local ensemble transform Kalman filter (LETKF) to
estimate surface emissions of CH<inline-formula><mml:math id="M5" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>. The data assimilation performance is
tested and optimized based on idealized settings using observation system
simulation experiments (OSSEs), where a known surface emission distribution
(the truth) is retrieved from synthetic observations. We tested three
covariance inflation methods to avoid covariance underestimation in the
emission estimates, namely fixed multiplicative (FM), relaxation-to-prior
spread (RTPS), and adaptive multiplicative. First, we assimilate the
synthetic observations at every grid point at the surface level. In such a
case of dense observational data, the normalized root mean square error
(RMSE) in the analyses over global land regions is smaller by 10 %–15 % in
the case of RTPS covariance inflation method compared to FM. We have shown that
integrated estimated flux seasonal cycles over 15 regions using RTPS
inflation are in reasonable agreement between true and estimated flux, with
0.04 global normalized annual mean bias. We then assimilated the column-averaged CH<inline-formula><mml:math id="M6" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration by sampling the model simulations at Greenhouse Gases Observing
Satellite (GOSAT) observation locations and time for another OSSE. Similar to the
case of dense observational data, the RTPS covariance inflation method performs
better than FM for GOSAT synthetic observation in terms of normalized RMSE
(2 %–3 %) and integrated flux estimation comparison with the true flux. The
annual mean averaged normalized RMSE (normalized mean bias) in LETKF
CH<inline-formula><mml:math id="M7" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation in the case of RTPS and FM covariance inflation is
found to be 0.59 (0.18) and 0.61 (0.23), respectively. The <inline-formula><mml:math id="M8" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test
performed for GOSAT synthetic observations assimilation suggests high
underestimation of background error covariance in both RTPS and FM
covariance inflation methods; however, the underestimation is much higher
(<inline-formula><mml:math id="M9" display="inline"><mml:mrow><mml:mi mathvariant="italic">&gt;</mml:mi><mml:mn mathvariant="normal">100</mml:mn></mml:mrow></mml:math></inline-formula> % always) for FM compared to RTPS covariance inflation
method.</p>
  </abstract>
    
<funding-group>
<award-group id="gs1">
<funding-source>Environmental Restoration and Conservation Agency</funding-source>
<award-id>n/a</award-id>
</award-group>
</funding-group>
</article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d1e247">Methane (CH<inline-formula><mml:math id="M10" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>) is the second major greenhouse gas, after carbon dioxide
(CO<inline-formula><mml:math id="M11" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:math></inline-formula>), that has anthropogenic sources. According to the contemporary
record of the global CH<inline-formula><mml:math id="M12" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> budget, the total of all CH<inline-formula><mml:math id="M13" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> sources
ranged 538–593 Tg yr<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> during 2008–2017
(Saunois
et al., 2020). The primary natural sources are from wetlands
(<inline-formula><mml:math id="M15" display="inline"><mml:mo lspace="0mm">∼</mml:mo></mml:math></inline-formula> 40 %). The main anthropogenic CH<inline-formula><mml:math id="M16" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emissions are from
microbial emissions associated with ruminants (livestock and waste), rice
cultivation, fugitive emissions (oil and gas production and use), and
incomplete combustion of biofuels and fossil fuels. The major fraction of
atmospheric CH<inline-formula><mml:math id="M17" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> sinks (range: 474–532 Tg yr<inline-formula><mml:math id="M18" 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>) occurs in the
troposphere by oxidation via reaction with hydroxyl (OH) radicals
(Patra,
et al., 2011; Saunois et al., 2020); other loss processes include oxidation
by soil and reactions with O<inline-formula><mml:math id="M19" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">1</mml:mn></mml:msup></mml:math></inline-formula>D and Cl. The lifetime of CH<inline-formula><mml:math id="M20" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> in the
atmosphere is estimated to be 9.1 <inline-formula><mml:math id="M21" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.9 years
(Szopa
et al., 2021).</p>
      <?pagebreak page1824?><p id="d1e362"><?xmltex \hack{\newpage}?>Regional CH<inline-formula><mml:math id="M22" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emissions can be estimated from CH<inline-formula><mml:math id="M23" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration
fields and chemistry transport models using Bayesian synthesis approaches
based on inverse modeling techniques (e.g., Enting, 2002).
In such approaches, emissions are optimized on a coarse resolution (e.g., for
a limited number of predefined regions) mostly using surface-based
observations. CH<inline-formula><mml:math id="M24" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations are provided by the NOAA cooperative
air sampling network sites
(Lan et al., 2022)
and other networks by the World Data Centre for Greenhouse Gases (WDCGG)
website, hosted by the Japan Meteorological Agency. In recent years,
satellite measurements have been made by the Greenhouse Gases Observing
Satellite (GOSAT) or the TROPOspheric Monitoring Instrument (TROPOMI)
(Lorente et al., 2021),
covering the globe with fine spatiotemporal scales. GOSAT has provided an
extensive global observations of column CH<inline-formula><mml:math id="M25" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations since 2009
(Yoshida
et al., 2013). Some of the inverse modeling studies utilize the satellite
observations for CH<inline-formula><mml:math id="M26" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation
(Zhang et al., 2021; Maasakkers et al.,
2016), but this requires enormous computational resources as a result of dealing with
more flux regions and more observations.</p>
      <p id="d1e411">Grid-based CH<inline-formula><mml:math id="M27" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux optimization is also performed using adjoint
technique (4-D Var data assimilation) and an ensemble Kalman filter (EnKF) but
was limited to small sets of observations
(Houweling et
al., 1999; Meirink et al., 2008; Bruhwiler et al., 2014).
Bruhwiler et al. (2014) followed the EnKF method
of Peters et al. (2005) to estimate the
CH<inline-formula><mml:math id="M28" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> surface fluxes that utilizes an offline atmospheric chemistry tracer model (ACTM) framework. Techniques
such as 4-D Var and EnKF are important to estimate CH<inline-formula><mml:math id="M29" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> fluxes since
they can assimilate a large number of observations and manage high-resolution
fluxes. In the EnKF system, a flow-dependent forecast error covariance
structure is provided by ensemble model forecasts, while it does not need an
adjoint model, which makes it a simple but powerful tool for flux estimation.
One of the limitations of the EnKF method is the dependence of the resolution of
state vector on ensemble size, which can give spurious results if the number
of ensemble members is much smaller than the rank of the error covariance
matrix (Houtekamer and Zhang, 2016).</p>
      <p id="d1e441">A local ensemble transform Kalman filter (LETKF) is a type of square-root EnKF that performs analysis locally in space
without perturbing the observations
(Ott et al., 2002,
2004; Hunt et al., 2007). LETKFs are computationally efficient since the
observations are assimilated simultaneously and not serially; it is simple to
account for observation error correlation. Miyazaki et al. (2011) and Kang et al. (2012) demonstrated the
implementation of LETKF data assimilation system by coupling an ACTM for
carbon-cycle research using atmospheric CO<inline-formula><mml:math id="M30" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:math></inline-formula> observations. It is also
extensively applied for the emission estimation of short-lived species using
satellite data
(Skachko
et al., 2016; Miyazaki et al., 2019; Sekiya et al., 2021). In this work, we
will estimate the CH<inline-formula><mml:math id="M31" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> fluxes using a LETKF data assimilation system.
Assimilation windows ranging from 6 h (Kang et al., 2012)
to several months (Bruhwiler et al., 2014) have been
used, depending on the desired time resolution of the estimated emissions,
which is often limited by the observational data density. The time frame
over which the system behaves linearly and in what time frame the
observations respond to the control variables, such as atmospheric
transport, as well as observation abundance, must also be taken into
consideration. Within an assimilation window, where and when the fluxes
would be constrained by specific observations is to be ascertained by the
correlation between ensemble prior fluxes and the ensemble CH<inline-formula><mml:math id="M32" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
concentration simulation from a forward model (Liu et al.,
2016).</p>
      <p id="d1e472">The main objective of this work is to develop an advanced 4-D data assimilation
system based on a LETKF that simultaneously estimates atmospheric
distributions and surface fluxes of CH<inline-formula><mml:math id="M33" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>. Observation system
simulation experiments (OSSEs) are conducted to assess
the performance of the LETKF since it is important to test the system against
the known emissions or the truth. The OSSE LETKF setup of top-down CH<inline-formula><mml:math id="M34" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation using an online ACTM is an essential step before implementation in real in situ and satellite observation.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Formulation of the LETKF system</title>
      <p id="d1e501">We briefly describe the LETKF in the application of CH<inline-formula><mml:math id="M35" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux
estimation, while detailed derivation of equations and code implementation
are given elsewhere (Hunt et
al., 2007; Miyazaki et al., 2011; Miyoshi et al., 2010). The notation used
here for LETKF formulation is adopted from Kotsuki et al. (2017). In the LETKF, the background ensemble (columns of matrix
<inline-formula><mml:math id="M36" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">x</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>) in a local region evolved from a set of perturbed
initial conditions. The background ensemble mean, <inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>,
and its perturbation, <inline-formula><mml:math id="M38" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>, are estimated from the
ensemble forecast as
          <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M39" display="block"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mi>m</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>m</mml:mi></mml:munderover><mml:msubsup><mml:mi mathvariant="bold">x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>;</mml:mo><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msubsup><mml:mi mathvariant="bold">X</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msubsup><mml:mi mathvariant="bold">x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M40" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula> indicates the ensemble size. The background error covariance
matrix <inline-formula><mml:math id="M41" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> in the <inline-formula><mml:math id="M42" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula>-dimensional ensemble is defined
as
          <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M43" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mi>m</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:mfrac></mml:mstyle><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mfenced open="[" close="]"><mml:mrow><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
        The analysis ensemble mean <inline-formula><mml:math id="M44" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> is derived using
background ensemble mean <inline-formula><mml:math id="M45" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> and ensemble perturbations
<inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> as
          <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M47" display="block"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:msup><mml:mi>Y</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:msup><mml:mi>R</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:msup><mml:mi>y</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>-</mml:mo><mml:mi>H</mml:mi><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mo>=</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mi>w</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M48" display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M49" display="inline"><mml:mi>Y</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M50" display="inline"><mml:mi>R</mml:mi></mml:math></inline-formula>, and <inline-formula><mml:math id="M51" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> denote the linear observation
operator, ensemble perturbation matrix in the observation space (<inline-formula><mml:math id="M52" display="inline"><mml:mrow><mml:mi>Y</mml:mi><mml:mo>≡</mml:mo><mml:mi>H</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:math></inline-formula>), observation error covariance matrix, and analysis error covariance
matrix in the ensemble space, respectively.<?pagebreak page1825?> The superscripts “o”, “b”, and
“a” denote the observations, background (prior), and analysis (posterior),
respectively. <inline-formula><mml:math id="M53" display="inline"><mml:mrow><mml:msup><mml:mi>w</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> defines the analysis increment (or
analysis weight) in observation space and is derived using the information
about observational increment
<inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:msup><mml:mi>y</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>-</mml:mo><mml:mi>H</mml:mi><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>. The analysis error
covariance matrix (<inline-formula><mml:math id="M55" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>) in the <inline-formula><mml:math id="M56" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula>-dimensional ensemble
space is spanned by ensemble perturbation (Hunt et al., 2007) and defined
as
          <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M57" display="block"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:mo mathvariant="italic">{</mml:mo><mml:mfenced open="(" close=")"><mml:mrow><mml:mi>m</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:mfenced><mml:mi>I</mml:mi><mml:mo>+</mml:mo><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:mi>H</mml:mi><mml:msup><mml:mi>X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:msup><mml:mi>R</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup><mml:mi>H</mml:mi><mml:msup><mml:mi>X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mo mathvariant="italic">}</mml:mo><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
        Finally, the analysis ensemble perturbations <inline-formula><mml:math id="M58" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> at
the central grid point are derived such as
          <disp-formula id="Ch1.E5" content-type="numbered"><label>5</label><mml:math id="M59" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mo mathvariant="italic">{</mml:mo><mml:mo>(</mml:mo><mml:mi>m</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:msup><mml:mo mathvariant="italic">}</mml:mo><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M60" display="inline"><mml:mrow><mml:mo mathvariant="italic">{</mml:mo><mml:mo>(</mml:mo><mml:mi>m</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo><mml:msup><mml:mover accent="true"><mml:mi>P</mml:mi><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">a</mml:mi></mml:msup><mml:msup><mml:mo mathvariant="italic">}</mml:mo><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> is a multiple of the symmetric
square root of the local analysis error covariance matrix in ensemble space
and could be computed by a singular vector decomposition method. The LETKF
solves the analysis update (Eqs. 3 and 5) at every model grid point
independently by assimilating local observations within the localization
cutoff radius.</p>
      <p id="d1e1109">We have applied a gross error check as a quality control to exclude
observations that are far from the first guess; the appropriate degrees of
the gross error check are also examined. Figure 1 shows the schematic
diagram of our LETKF setup with two ensemble members for three consecutive
assimilation cycles with an 8 d assimilation window. The analysis is
obtained at the midpoint time of the assimilation window (Fig. 1). The
analyzed (updated) surface flux is used for the next data assimilation cycle
starting from the midpoint time of the previous data assimilation window.
The state vector augmentation approach is used to estimate the atmospheric
CH<inline-formula><mml:math id="M61" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> surface flux (Kang et al., 2012; Miyazaki
et al., 2011).</p>
      <p id="d1e1121">Assimilation window size and ensemble members are chosen based on
computational efficiency and estimation accuracy. A larger assimilation
window means fluxes are constrained by more observations; however, it
requires handling of large matrix optimization which is difficult in cases
of dense observation and introduces sampling errors related to transport
errors. In this study, a few sensitivity experiments were performed to demonstrate
the choice of assimilation window length and ensemble size when GOSAT
synthetic observations are assimilated in Sect. 4.2.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><?xmltex \currentcnt{1}?><?xmltex \def\figurename{Figure}?><label>Figure 1</label><caption><p id="d1e1127">Schematic represents the temporal evolution of the LETKF cycle. In the
first assimilation window (Cycle 1), the dotted lines show the ensemble
forecast of CH<inline-formula><mml:math id="M62" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations (with two ensemble members), the solid
line shows the linear combination of the forecasts, and the filled circles show
the observations of CH<inline-formula><mml:math id="M63" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration. The data assimilation finds the
linear combination of the ensemble forecast by estimating the weight
(<inline-formula><mml:math id="M64" display="inline"><mml:mrow><mml:msup><mml:mi>w</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>) that best fits the observations throughout the assimilation
window. The analysis weight is applied to obtain optimal surface fluxes (<inline-formula><mml:math id="M65" display="inline"><mml:mi>F</mml:mi></mml:math></inline-formula>)
and the concentration of CH<inline-formula><mml:math id="M66" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> at the intermediate time of the data
assimilation window. The updated analyzed concentration ensembles are used
as initial conditions after relaxation (<inline-formula><mml:math id="M67" display="inline"><mml:mrow><mml:msup><mml:mi>X</mml:mi><mml:mrow><mml:mi mathvariant="normal">a</mml:mi><mml:mo>,</mml:mo><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">RLX</mml:mi></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>) (Eq. 8) for the next
ensemble forecast. The spread of the ensemble members represents the
forecast error. The schematic is adapted from Kalnay
and Yang (2010) and Miyazaki et al. (2011).</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f01.png"/>

      </fig>

<sec id="Ch1.S2.SS1">
  <label>2.1</label><title>Covariance inflation</title>
      <p id="d1e1206">The LETKF data assimilation needs variance inflation to mitigate the underdispersed ensemble. We tested three methods: fixed multiplicative (FM),
relaxation-to-prior spread (RTPS), and adaptive multiplicative covariance
inflation.</p>
      <p id="d1e1209">The fixed multiplicative (FM) inflation method (Anderson
and Anderson, 1999) inflates the prior ensemble by inflating the background
error covariance matrix <inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> defined in Eq. (2) as
            <disp-formula id="Ch1.E6" content-type="numbered"><label>6</label><mml:math id="M69" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">inf</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mi mathvariant="italic">γ</mml:mi><mml:msubsup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">tmp</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M70" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">tmp</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> represents the temporary
background error covariance matrix, which is inflated by a factor <inline-formula><mml:math id="M71" display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula>.</p>
      <p id="d1e1269">The other inflation methods used to prevent the reduction of ensemble spread
are relaxation-to-prior perturbation (RTPP) (Zhang et
al., 2004) and relaxation-to-prior spread (RTPS)
(Whitaker and Hamill, 2012). The RTPP method relaxes the
reduction of the ensemble spread after updating the ensemble perturbations,
which blends the background and analysis ensemble perturbations as
            <disp-formula id="Ch1.E7" content-type="numbered"><label>7</label><mml:math id="M72" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">inf</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPP</mml:mi></mml:msub><mml:msup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPP</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:msubsup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">tmp</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M73" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPP</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> denotes the relaxation parameter of
the RTPP.</p>
      <p id="d1e1333">The RTPS inflation method relaxes the reduction of the ensemble spread by
relaxing the analysis spread to prior spread as
            <disp-formula id="Ch1.E8" content-type="numbered"><label>8</label><mml:math id="M74" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">RLX</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:mfenced close=")" open="("><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:msubsup><mml:mi mathvariant="bold">X</mml:mi><mml:mi mathvariant="normal">tmp</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M75" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> denote the ensemble spread
and relaxation parameter of the RTPS, respectively. The range of the
<inline-formula><mml:math id="M77" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> parameter is bounded by [0, 1]. This study focuses
mainly on the FM and RTPS covariance inflation methods.</p>
      <p id="d1e1428">In addition, Miyoshi (2011) applied adaptive
inflation by determining the multiplicative inflation factors at every grid
point at every analysis step using the observation-space statistics derived
by Daley (1992) and Desroziers et al. (2005).
            <disp-formula id="Ch1.E9" content-type="numbered"><label>9</label><mml:math id="M78" display="block"><mml:mrow><mml:mo>&lt;</mml:mo><mml:mi>d</mml:mi><mml:msup><mml:mi>d</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>&gt;</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mo>=</mml:mo><mml:mi>H</mml:mi><mml:msubsup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">inf</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msubsup><mml:msup><mml:mi>H</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:mi mathvariant="bold">R</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where the operator “<inline-formula><mml:math id="M79" display="inline"><mml:mrow><mml:mi mathvariant="italic">&lt;</mml:mi><mml:mo>⋅</mml:mo><mml:mi mathvariant="italic">&gt;</mml:mi></mml:mrow></mml:math></inline-formula>” denotes the
statistical expectation and
<inline-formula><mml:math id="M80" display="inline"><mml:mrow><mml:mi>d</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mi>y</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>-</mml:mo><mml:mi>H</mml:mi><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>
(observation minus first guess), and <inline-formula><mml:math id="M81" display="inline"><mml:mi mathvariant="bold">R</mml:mi></mml:math></inline-formula> is the error observation covariance
matrix.</p>
      <p id="d1e1518">The impact of using the adaptive multiplication inflation method is
discussed in the GOSAT synthetic observation assimilation experiments in
Sect. 4.2.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <label>2.2</label><title>MIROC4-ACTM</title>
      <p id="d1e1529">Model for Interdisciplinary Research on Climate, version 4.0 (MIROC4)-based
ACTM (hereafter referred to as MIROC4-ACTM)
(Patra et al., 2018; Bisht et al.,
2021) is used here for CH<inline-formula><mml:math id="M82" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration simulations. The model
simulations have been performed at a horizontal grid resolution of
approximately 2.8 <inline-formula><mml:math id="M83" display="inline"><mml:mo>×</mml:mo></mml:math></inline-formula> 2.8<inline-formula><mml:math id="M84" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> latitude–longitude (T42 spectral
truncations) and at hybrid vertical coordinates of 67 levels (Earth's surface to
0.0128 hPa; Watanabe et al., 2008).
Bisht et al. (2021) performed multi-tracer analysis and
demonstrated the importance of very well resolved stratosphere in the
MIROC4-ACTM that illustrates better extratropical stratospheric
variabilities and simulated tropospheric dynamical fields. The
meteorological fields in MIROC4-ACTM are nudged to the JMA reanalysis
(JRA-55) data (Kobayashi et al., 2015).</p>
</sec>
</sec>
<?pagebreak page1826?><sec id="Ch1.S3">
  <label>3</label><title>Experimental setup</title>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Construction of known surface emissions (truth)</title>
      <p id="d1e1573">Present OSSEs intend to develop basic tuning strategies before the actual
data to be assimilated, which is useful to accelerate the operational use of
real observations. The OSSE has been discussed here by exploiting the known
“truth”. The synthetic observations to be assimilated in the OSSE are
generated from nature runs which use bottom-up surface emission (true) data
to simulate global 3-D CH<inline-formula><mml:math id="M85" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations. The true surface CH<inline-formula><mml:math id="M86" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
emissions are prepared on the monthly scale using anthropogenic and natural
sectors, minus the surface sinks due to bacterial consumption in the soil
(Chandra et al., 2021). The anthropogenic emissions
were obtained from the Emission Database for Global Atmospheric Research,
version 4.3.2 inventory (EDGARv4.3.2) (Janssens-Maenhout
et al., 2019), which includes the emissions from the major sectors, such as fugitive sources, enteric fermentation and manure management, and solid waste and
wastewater handling. The biomass burning emissions are taken from the Global
Fire Database (GFEDv4s)
(van
der Werf et al., 2017) and Goddard Institute for Space Studies emissions
(Fung et al., 1991). The wetland and rice emissions
are taken from the process-based model of the terrestrial biogeochemical
cycle, Vegetation Integrated Simulator of Trace gases (VISIT)
(Ito, 2019), which is based on Cao et al. (1996). Other natural emissions, such as those from the ocean, termites, and mud volcanoes are
taken from the TransCom-CH<inline-formula><mml:math id="M87" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> inter-comparison experiment
(Patra
et al., 2011). The total emissions are taken as the truth for the OSSEs, and
the concentration simulated by MIROC4-ACTM will be referred to as synthetic
observations.</p>
</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Prior flux preparation and LETKF setting</title>
      <p id="d1e1611">Based on our understanding of CH<inline-formula><mml:math id="M88" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> inverse modeling, the uncertainty in
regional flux estimation is found to be 30 % or lower
(Chandra et al., 2021). Therefore, we attempted to
reproduce the true flux by starting with a prior flux that is lower than the true flux by
30 % (prior flux has the same seasonal cycles as true flux).
The MIROC4-ACTM is initialized with a spin-up of 3 years (2007–2009)
with prior flux distribution. The initial CH<inline-formula><mml:math id="M89" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> distribution on 1 January 2007 was taken from an earlier simulation of 27 years. An initial
perturbation with standard deviation of approximately 6 %–8 % spread is
applied to the a priori flux as the initial ensemble spread, whereas no
ensemble perturbation was applied to the initial CH<inline-formula><mml:math id="M90" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration. The
sensitivity of the initial ensemble spread to CH<inline-formula><mml:math id="M91" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation is
discussed in Sect. 4.2. The uncertainty to perturb prior fluxes is
generated based on random positive values with normal distribution. The
monthly scale prior emission is linearly interpolated at 6-hourly intervals
to be used in the MIROC4-ACTM simulation for data assimilation. This study
performs two LETKF data assimilation experiments. In these experiments, we
provided initial perturbation on a regional basis over land (53 different land
regions; Chandra et al., 2021), and at every grid over
ocean,<?pagebreak page1827?> no spatial error correlation between grid points is considered among
ensemble members. However, in Sect. 4.2.5, we also discussed the
sensitivity of CH<inline-formula><mml:math id="M92" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> data assimilation by providing the initial ensemble
spread at every grid by considering the horizontal spatial error correlation
between grid points among ensemble members, with a global mean correlation
of 20 %.</p>
</sec>
<sec id="Ch1.S3.SS3">
  <label>3.3</label><title>Experiment 1: synthetic dense observation formulation</title>
      <p id="d1e1667">The OSSE setting with very accurate and dense observation surface data is an
attempt to demonstrate that the data assimilation system works reasonably in the
estimation of the true surface flux. Errors in the estimated flux could
arise due to the insufficient ensemble size and also the implemented
inflation methods to overcome the undersampling, along with a simplified
forecast process of the emissions. In real data assimilation, there are
additional sources of potential errors, such as atmospheric transport and
inappropriate prior or observation uncertainties. In our OSSEs, CH<inline-formula><mml:math id="M93" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
fluxes as mentioned in Sect. 3.2 are used as “true” fluxes in generating
synthetic observations (CH<inline-formula><mml:math id="M94" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations). In Experiment 1, the
simulated surface layer CH<inline-formula><mml:math id="M95" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations at each grid for the entire
globe were used as synthetic observations. We added a constant
measurement uncertainty of 5 ppb, which is typically achieved by the
present-day measurement systems (e.g.,
Lan et al., 2022).</p>
      <p id="d1e1697">In this study, the CH<inline-formula><mml:math id="M96" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observations are assimilated by applying the
observation error covariance localization (Kotsuki et al.,
2020) to reduce the spurious spatial correlation due to a smaller ensemble
size than the degrees of freedom of the system (<inline-formula><mml:math id="M97" display="inline"><mml:mrow><mml:mi mathvariant="bold">R</mml:mi><mml:mo>←</mml:mo><mml:mi mathvariant="bold">R</mml:mi><mml:mo>×</mml:mo><mml:mi>exp⁡</mml:mi><mml:mo>(</mml:mo><mml:mo>-</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:mo mathvariant="italic">{</mml:mo><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub></mml:mrow></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo mathvariant="italic">}</mml:mo><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>), where <inline-formula><mml:math id="M98" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math id="M99" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> denote the horizontal distance (km) and vertical
difference (log[Pa]) between the analysis model grid point and observation
location. The tunable parameters <inline-formula><mml:math id="M100" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math id="M101" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are the horizontal localization scale (km)
and vertical localization scale (log[Pa]), respectively. Using the spatial
localization technique, we have estimated the CH<inline-formula><mml:math id="M102" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux for each grid by
choosing the CH<inline-formula><mml:math id="M103" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observations that influence the grid point using
an optimal cutoff radius (<inline-formula><mml:math id="M104" display="inline"><mml:mrow><mml:mo>≃</mml:mo><mml:mn mathvariant="normal">3.65</mml:mn><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:mo>,</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="normal">v</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>; Miyoshi et al., 2007) with a horizontal covariance
localization (<inline-formula><mml:math id="M105" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) of 2200 km and a vertical
covariance localization (<inline-formula><mml:math id="M106" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) of 0.3 in the
natural logarithmic pressure (log[Pa]) coordinate. The localization is
performed to improve the signal-to-noise ratio of ensemble-based covariance.
Numerous sensitivity experiments have been performed by varying the
horizontal and vertical localization length in order to obtain the optimized
CH<inline-formula><mml:math id="M107" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux that best compares with the truth. The LETKF assimilates the
observations within the specified radius to solve the analysis state at each
grid point independently (Liu et al., 2016; Kotsuki
et al., 2020). The state vector of the analysis includes the atmospheric
CH<inline-formula><mml:math id="M108" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration, which is the prognostic variable of forecast model,
and the state vector is further augmented by the surface CH<inline-formula><mml:math id="M109" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux, which is
not a model prognostic variable. This augmentation enables the LETKF to
directly estimate the parameter through the background error covariance with
observed variables (Baek et al., 2006). The state vector
augmentation is implemented similar to that used by Miyazaki
et al. (2011). This approach analyzes CH<inline-formula><mml:math id="M110" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux during the analysis
step. The purpose of the simultaneous CH<inline-formula><mml:math id="M111" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emission and concentration
optimization is to reduce the uncertainty of the initial CH<inline-formula><mml:math id="M112" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
concentrations on the CH<inline-formula><mml:math id="M113" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> evolution during the assimilation window and
to maximize the observations potential (Tian et al.,
2014).</p>
      <p id="d1e1949">The atmospheric CH<inline-formula><mml:math id="M114" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration is changed during both the analysis
and forecast steps. A challenge of this scheme is that the analysis
increment is added to the model state at each analysis step, without
considering the global total CH<inline-formula><mml:math id="M115" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> mass conservation in the model but
consistent with the observed local CH<inline-formula><mml:math id="M116" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> abundance.</p>
      <p id="d1e1979">In this case, the surface flux at every model grid point is analyzed with an 8 d
assimilation window during the year 2010 with 100 ensemble members. The
ensemble size and assimilation window are chosen based on the CH<inline-formula><mml:math id="M117" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux
estimation accuracy calculated by performing a sensitivity experiment for
the ensemble size (60, 80, and 100) and assimilation window (3 and 8 d),
respectively (not shown).</p>
</sec>
<sec id="Ch1.S3.SS4">
  <label>3.4</label><title>Experiment 2: synthetic satellite observation formulation</title>
      <p id="d1e1999">One way to address the real-world CH<inline-formula><mml:math id="M118" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation problem is to
first make the OSSE dataset like real observations. In this OSSE,
we have assimilated synthetic column-averaged CH<inline-formula><mml:math id="M119" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations with a
coverage mimicking GOSAT satellite observations. We prepared a model-simulated column-averaged CH<inline-formula><mml:math id="M120" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration (XCH<inline-formula><mml:math id="M121" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>) dataset that
is spatiotemporally sampled with GOSAT observations as follows:
            <disp-formula id="Ch1.E10" content-type="numbered"><label>10</label><mml:math id="M122" display="block"><mml:mrow><?xmltex \hack{\hbox\bgroup\fontsize{8.5}{8.5}\selectfont$\displaystyle}?><mml:mrow class="chem"><mml:msub><mml:mi mathvariant="normal">XCH</mml:mi><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">XCH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mtext>a priori</mml:mtext><mml:mo>)</mml:mo></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:munder><mml:mo movablelimits="false">∑</mml:mo><mml:mi>j</mml:mi></mml:munder><mml:msub><mml:mi>h</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:msub><mml:mi>a</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">CH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mi mathvariant="normal">ACTM</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">CH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mtext>a priori</mml:mtext><mml:mo>)</mml:mo></mml:mrow></mml:msub><mml:msub><mml:mo>)</mml:mo><mml:mi>j</mml:mi></mml:msub><mml:mo>,</mml:mo><?xmltex \hack{$\egroup}?></mml:mrow></mml:math></disp-formula>
          where XCH<inline-formula><mml:math id="M123" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> is the column-averaged model-simulated CH<inline-formula><mml:math id="M124" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
concentration. <inline-formula><mml:math id="M125" display="inline"><mml:mrow><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">XCH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mtext>a priori</mml:mtext><mml:mo>)</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is a priori
column-averaged concentration. <inline-formula><mml:math id="M126" display="inline"><mml:mrow><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">CH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mi mathvariant="normal">ACTM</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math id="M127" display="inline"><mml:mrow><mml:msub><mml:mrow class="chem"><mml:mi mathvariant="normal">CH</mml:mi></mml:mrow><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>(</mml:mo><mml:mtext>a priori</mml:mtext><mml:mo>)</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are the CH<inline-formula><mml:math id="M128" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> profile from ACTM
and a priori, respectively. <inline-formula><mml:math id="M129" display="inline"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the pressure weighting function (<inline-formula><mml:math id="M130" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula> is
the vertical layer index), and <inline-formula><mml:math id="M131" display="inline"><mml:mrow><mml:msub><mml:mi>a</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> represents the averaging kernel matrix
for the column retrieval, which is the sensitivity of the retrieved total
column at the various (“<inline-formula><mml:math id="M132" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula>”) atmospheric levels. In the next step, we added
the same retrieval (XCH<inline-formula><mml:math id="M133" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>) error as GOSAT to the XCH<inline-formula><mml:math id="M134" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> (ACTM-simulated) to make the OSSE more realistic and then attempt to estimate the
true fluxes.</p>
      <p id="d1e2262">In this case, the CH<inline-formula><mml:math id="M135" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux has been estimated for each grid by choosing
the CH<inline-formula><mml:math id="M136" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observation with a cutoff radius (<inline-formula><mml:math id="M137" display="inline"><mml:mrow><mml:mo>≃</mml:mo><mml:mn mathvariant="normal">3.65</mml:mn><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">v</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>), with a horizontal covariance localization (<inline-formula><mml:math id="M138" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) of 5000 km and a vertical covariance localization
(<inline-formula><mml:math id="M139" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">v</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) of 0.35 in the natural logarithmic
pressure (log[Pa]) coordinate. The optimal horizontal and vertical
covariance localization values<?pagebreak page1828?> are chosen based on a trial-and-error method
(those with the best fits to estimate the CH<inline-formula><mml:math id="M140" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux when compared with truth). A long
cutoff radius has been chosen due to sparse observational coverage of GOSAT.
Covariance localization is necessary to remove long-range erroneous
correlations and for mitigating sampling errors in the ensemble-based error
covariance with a limited ensemble size
(Miyoshi et al., 2007; Greybush et
al., 2011; Kotsuki et al., 2020). The surface flux is analyzed at every
model grid point with an 8 d assimilation window and 100 ensemble members; they are chosen based on the sensitivity experiments discussed in Sect. 4.2.</p>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Results and discussion</title>
<sec id="Ch1.S4.SS1">
  <label>4.1</label><title>Experiment with dense OSSEs</title>
      <p id="d1e2352">The time series of normalized root mean square error (RMSE; <inline-formula><mml:math id="M141" display="inline"><mml:mrow><mml:msqrt><mml:mrow><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:mo>(</mml:mo><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msubsup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>/</mml:mo><mml:mi>n</mml:mi></mml:mrow></mml:msqrt><mml:mo>/</mml:mo><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">t</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>, where <inline-formula><mml:math id="M142" display="inline"><mml:mrow><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M143" display="inline"><mml:mrow><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are
the analysis and true state at <inline-formula><mml:math id="M144" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>th model grid point, <inline-formula><mml:math id="M145" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula> is the total number of
grid points, and <inline-formula><mml:math id="M146" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>x</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mi mathvariant="normal">t</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> represents the mean of true flux) in the
analyses over the global landmass region is shown in Fig. 2. The normalized
global RMSE is calculated using FM and RTPS inflation methods (Fig. 2) after
assimilating synthetic observation at every grid (Sect. 3.4). Noteworthy
is that the experiment with the FM inflation method shows 10 %–15 % larger error
in estimating the atmospheric surface CH<inline-formula><mml:math id="M147" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux compared to the RTPS
inflation method. One of the reasons of the better RMSE using the RTPS inflation
method is the higher number of degrees of freedom provided by relaxation
(<inline-formula><mml:math id="M148" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) in the ensemble spread (Eq. 8) that could
nudge the ensemble of CH<inline-formula><mml:math id="M149" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations towards observations. The
initial flux analysis spread using RTPS and FM is shown in the Supplement (Fig. S1) and shows larger initial analysis flux spread over
Brazil, tropical America, and Asia in RTPS inflation compared to the FM
inflation method. We performed numerous sensitivity tests with the RTPS inflation
method and found that uniform relaxation is not substantial for some of the
regions. Figure 2 shows the RMSE for FM, fixed RTPS (<inline-formula><mml:math id="M150" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.4</mml:mn></mml:mrow></mml:math></inline-formula>; applied globally, the optimized value is obtained
by manual fine-tuning), and conditional RTPS (<inline-formula><mml:math id="M151" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.3</mml:mn></mml:mrow></mml:math></inline-formula>–0.7 applied different <inline-formula><mml:math id="M152" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> values regionally by manual fine-tuning). In the case of conditional
RTPS, the optimal values of <inline-formula><mml:math id="M153" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, i.e., 0.6,
0.3, and 0.7 for the regions south of 20<inline-formula><mml:math id="M154" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S, 20<inline-formula><mml:math id="M155" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S–20<inline-formula><mml:math id="M156" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, and
north of 20<inline-formula><mml:math id="M157" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, respectively, were obtained from data assimilation
sensitivity calculations with varying <inline-formula><mml:math id="M158" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> values for
the three regions separately to best match the true states. We find that the
conditional RTPS method improves the accuracy by <inline-formula><mml:math id="M159" display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 5 %
compared to fixed RTPS and 10 %–15 % compared to FM. In the following, we
discuss the results obtained using the conditional RTPS and FM inflation
methods.</p>
      <p id="d1e2604">We have also shown the RMSE (not normalized) of the surface flux in the Supplement (Fig. S2). The flux RMSE has been estimated globally for both the
inflation methods and also for the region south of 20<inline-formula><mml:math id="M160" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N (by considering only
those land grids which fall in the region south of 20<inline-formula><mml:math id="M161" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N; Fig. S2) for
comparative purposes. It was noticed that (Fig. S2 in the Supplement), above north of 20<inline-formula><mml:math id="M162" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, the flux estimation error is higher,
specifically during spring–summer when CH<inline-formula><mml:math id="M163" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> emissions peak over most of
the northern hemispheric regions (Fig. 3). The high uncertainty during
spring–summer (Fig. S2) in the flux estimation over these regions could
appear due to the attenuation of surface observations as a result of active
vertical mixing. The RMSE during autumn (Fig. S2) is comparable in the case of
the global region and the region south of 20<inline-formula><mml:math id="M164" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, which indicates that the RMSE is arising from southern
hemispheric regions, likely over Brazil, as it peaks during autumn (Fig. 3).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><?xmltex \currentcnt{2}?><?xmltex \def\figurename{Figure}?><label>Figure 2</label><caption><p id="d1e2654">Time series of normalized RMSE of surface CH<inline-formula><mml:math id="M165" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux analysis,
for 1 year of data assimilation using FM, fixed RTPS, and conditional RTPS
inflation methods over the global landmass region.</p></caption>
          <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f02.png"/>

        </fig>

      <p id="d1e2673">Figure 3 shows a regional total flux seasonal cycle comparison of the
estimated fluxes for 15 terrestrial regions with the cycles of the prior and true
fluxes. The estimated flux retrieved using RTPS inflation method over
different regions agrees well with that of the true flux. We intend to show the
capability of LETKF-estimated fluxes over these regions using surface
observations to mimic the true fluxes in our understanding of the terrestrial
biosphere CH<inline-formula><mml:math id="M166" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> cycle. These results are consistent with Fig. 2, with
an annual global normalized mean bias (<inline-formula><mml:math id="M167" display="inline"><mml:mrow><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:mo>(</mml:mo><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msubsup><mml:mo>)</mml:mo><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 open="(" close=")"><mml:mrow><mml:msubsup><mml:mi>x</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">t</mml:mi></mml:msubsup></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>) of <inline-formula><mml:math id="M168" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">0.04</mml:mn></mml:mrow></mml:math></inline-formula>. It can also be noticed from Fig. 3 that estimated
fluxes converge to true fluxes over most of the regions after about 2–3 months.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><?xmltex \currentcnt{3}?><?xmltex \def\figurename{Figure}?><label>Figure 3</label><caption><p id="d1e2758">The 1-year CH<inline-formula><mml:math id="M169" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> total flux seasonal cycles of the true flux (black),
prior flux (blue), and flux estimated from the LETKF (orange) conditional RTPS
inflation method in 15 regions after assimilating dense synthetic surface
CH<inline-formula><mml:math id="M170" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observations.</p></caption>
          <?xmltex \igopts{width=497.923228pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f03.png"/>

        </fig>

      <p id="d1e2785">To see the degree of similarity in the flux distribution between the
estimated and true fluxes, we show monthly mean spatial flux distribution
for June and November in Figs. 4 and 5, respectively, along with the bias
in the prior and estimated flux. As shown in Figs. 4 and 5, the general
spatial patterns of the true flux are estimated well. These results suggest
that our LETKF system is capable of reproducing continental spatial flux
patterns by using such idealized dense surface observational data.
However, some clear differences in flux estimation could be noticed from the FM
and RTPS inflation method (Figs. 4 and 5); e.g., over the Eurasian and
American continent, analysis with RTPS shows clear improvement<?pagebreak page1829?> compared to
the FM covariance inflation method. We calculated the global mean normalized
bias with the RTPS and FM covariance inflation method, which is found to be <inline-formula><mml:math id="M171" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">0.04</mml:mn></mml:mrow></mml:math></inline-formula>
and <inline-formula><mml:math id="M172" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">0.11</mml:mn></mml:mrow></mml:math></inline-formula>, respectively, over land regions, and this showed that RTPS significantly
improved the flux estimation compared to the FM covariance inflation method.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><?xmltex \def\figurename{Figure}?><label>Figure 4</label><caption><p id="d1e2810">Spatial distribution of surface CH<inline-formula><mml:math id="M173" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> fluxes (true; top left
panel, FM analysis; middle left panel, RTPS analysis; bottom left panel) and
the associated bias in prior (prior-true; top right panel) and estimated
(FM-true; middle right panel, RTPS-true; bottom right panel) fluxes during
June 2010.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f04.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F5" specific-use="star"><?xmltex \currentcnt{5}?><?xmltex \def\figurename{Figure}?><label>Figure 5</label><caption><p id="d1e2831">Same as Fig. 4 but for November 2010.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f05.png"/>

        </fig>

</sec>
<sec id="Ch1.S4.SS2">
  <label>4.2</label><title>Experiment by mimicking the real satellite observational dataset</title>
      <p id="d1e2848">In this section we discuss the LETKF flux estimation by assimilation of
GOSAT synthetic CH<inline-formula><mml:math id="M174" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration observations. Figure 6 shows the
model-simulated mean XCH<inline-formula><mml:math id="M175" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentration sampled spatiotemporally with
GOSAT observations during January and July for the year 2010 (sampling
method discussed in Sect. 3.4). In this case we have shown different LETKF
sensitivity experiments, such as LETKF sensitivity to (1) FM, RTPS, and adaptive
multiplicative inflation; (2) the assimilation window; (3) the ensemble size; (4)
the <inline-formula><mml:math id="M176" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test; and (5) the prior ensemble spread. In the LETKF sensitivity
experiments from 1–4, the initial ensemble spread employed a similar method to
Experiment 1, and conditional RTPS inflation method is used. A conditional RTPS
method is also used in Sect. 4.2.6 for CH<inline-formula><mml:math id="M177" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation.</p>
<sec id="Ch1.S4.SS2.SSS1">
  <label>4.2.1</label><title>LETKF sensitivity to FM, RTPS, and adaptive multiplicative inflation</title>
      <p id="d1e2896">This study mainly emphasizes FM and RTPS inflation methods used in
CH<inline-formula><mml:math id="M178" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF data assimilation. The annual average normalized RMSE
(absolute bias) with RTPS and FM covariance inflation is found to be 0.59
(0.18) and 0.64 (0.22), respectively. The RTPS inflation method performs
better than the FM inflation method overall. In addition to RTPS inflation,
a sensitivity test is also performed using an adaptive multiplicative inflation
method.</p>
      <?pagebreak page1830?><p id="d1e2908">In the adaptive inflation, we need to provide an initial multiplicative
inflation factor at the beginning of data assimilation cycle (Cycle 1 in
Fig. 1). Following the method of Miyoshi (2011), the multiplication inflation factor information calculated in the previous cycle (i.e., Cycle 1 in Fig. 1) is used for the next data assimilation
cycle at every grid point (Cycle 2 in Fig. 1). We perform two sensitivity
experiments. In the first (second) case, we provided 50 % (40 %) initial
inflation in the beginning of Cycle 1 (Fig. 1). The normalized RMSE in the
both the adaptive inflation sensitivity experiments is comparable (0.65,
Supplement Fig. S3a) till July, but from the beginning of
August, the RMSE increases exponentially in the first experiment. However, in
terms of the <inline-formula><mml:math id="M179" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> distribution, CH<inline-formula><mml:math id="M180" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation with the first
sensitivity adaptive multiplicative inflation experiment (50 % initial
inflation case) is better than with the second sensitivity experiment (Supplement Fig. S3b; <inline-formula><mml:math id="M181" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test described in Sect. 4.2.4). To
identify the regions of high estimated CH<inline-formula><mml:math id="M182" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux error, we have shown
the background error spread in CH<inline-formula><mml:math id="M183" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation over 15 regions
(Supplement Fig. S3c) and found that the spread over west and southeast Asia rises exponentially post-July, which indicates the rise of estimated
CH<inline-formula><mml:math id="M184" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux error over these regions in the first sensitivity adaptive
multiplicative inflation experiment. Our analysis suggests that CH<inline-formula><mml:math id="M185" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
flux estimation depends on the initial inflation factor provided in the
beginning of the data assimilation cycle (Cycle 1, Fig. 1) in the adaptive
multiplication method. Also, we need to be very careful to monitor the
background error spread evolution with time to estimate the CH<inline-formula><mml:math id="M186" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux
with adaptive inflation; the <inline-formula><mml:math id="M187" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> distribution analysis is not sufficient.</p>
      <p id="d1e2999">In the case of RTPP inflation, we found the parameter <inline-formula><mml:math id="M188" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPP</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is very difficult to fine-tune due to its very high
sensitivity to estimating the CH<inline-formula><mml:math id="M189" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux. We fail to obtain an optimized
<inline-formula><mml:math id="M190" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPP</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> value to estimate the CH<inline-formula><mml:math id="M191" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux.
Whitaker and Hamill (2012) also demonstrated the better
accuracy of the LETKF meteorological data assimilation with RTPS compared to
the RTPP covariance inflation method. They found the RTPP method produces very large
errors if the inflation parameter exceeds the optimal value.</p>
</sec>
<sec id="Ch1.S4.SS2.SSS2">
  <label>4.2.2</label><title>Assimilation window</title>
      <p id="d1e3050">The LETKF data assimilation window length determines the time span of the
observations assimilated in each assimilation cycle. We have shown the
sensitivity of two assimilation window size configurations, 3 and 8 d, in the Supplement Fig. S4. Our sensitivity experiments with
window size configurations show that the 8 d long assimilation window
estimates the CH<inline-formula><mml:math id="M192" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux with better accuracy (<inline-formula><mml:math id="M193" display="inline"><mml:mo lspace="0mm">∼</mml:mo></mml:math></inline-formula> 10 %)
compared to the 3 d assimilation window because more observational
information is incorporated into the system with the 8 d long assimilation
window. This study uses an 8 d assimilation window for CH<inline-formula><mml:math id="M194" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF data
assimilation.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F6" specific-use="star"><?xmltex \currentcnt{6}?><?xmltex \def\figurename{Figure}?><label>Figure 6</label><caption><p id="d1e3080">Monthly mean ACTM-simulated XCH<inline-formula><mml:math id="M195" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> (ppb) sampled with GOSAT
observations to be assimilated (valid during the year 2010). The actual
retrieval errors are added in the synthetic GOSAT observations. Data are
shown for 2 representative months, depicting the Southern and Northern
Hemisphere differences in data coverage.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f06.png"/>

          </fig>

</sec>
<sec id="Ch1.S4.SS2.SSS3">
  <label>4.2.3</label><title>Ensemble size</title>
      <?pagebreak page1832?><p id="d1e3106">Figure 7a shows the RMSE using different ensemble members. The RMSE
stabilizes gradually as the ensemble size increases from 60 to 80 to 100
ensemble members. The ensemble size dependency of flux estimation suggests
the further scope of the improvement in flux estimation by increasing the
ensemble members. In this study we stick to 100 ensemble members due to high
computational cost while solving large covariance matrices. The larger error
in flux estimation in the case of column-averaged synthetic GOSAT CH<inline-formula><mml:math id="M196" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
observations assimilation compared to dense observations (Fig. 2) is likely
due to the weaker constraint on surface fluxes provided by satellite
observations and sparse observations.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><?xmltex \def\figurename{Figure}?><label>Figure 7</label><caption><p id="d1e3120"><bold>(a)</bold> Flux estimation RMSE using different ensemble sizes with RTPS
covariance inflation. <bold>(b)</bold> <inline-formula><mml:math id="M197" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> distribution using FM and RTPS
covariance inflation methods, with an ensemble size of 100.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f07.png"/>

          </fig>

</sec>
<sec id="Ch1.S4.SS2.SSS4">
  <label>4.2.4</label><?xmltex \opttitle{$\chi^{{2}}$ test}?><title><inline-formula><mml:math id="M198" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test</title>
      <p id="d1e3165">We have carried out a <inline-formula><mml:math id="M199" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test for the evaluation of background error
covariance matrix (Miyazaki et al.,
2012). For the <inline-formula><mml:math id="M200" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> test, the innovation statistics are diagnosed
from the observation minus forecast <inline-formula><mml:math id="M201" display="inline"><mml:mrow><mml:mfenced close=")" open="("><mml:mrow><mml:msup><mml:mi>y</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>-</mml:mo><mml:mi>H</mml:mi><mml:msup><mml:mi mathvariant="bold">x</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula>, the
estimated error covariance in the observation space
(<inline-formula><mml:math id="M202" display="inline"><mml:mrow><mml:mi>H</mml:mi><mml:msup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mi>H</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:mi mathvariant="bold">R</mml:mi></mml:mrow></mml:math></inline-formula>), and
the number of observations <inline-formula><mml:math id="M203" display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> as
              <disp-formula id="Ch1.E11" content-type="numbered"><label>11</label><mml:math id="M204" display="block"><mml:mrow><mml:mi>Y</mml:mi><mml:mo>=</mml:mo><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:msqrt><mml:mi>k</mml:mi></mml:msqrt></mml:mfrac></mml:mstyle><mml:msup><mml:mfenced close=")" open="("><mml:mrow><mml:mi>H</mml:mi><mml:msup><mml:mi mathvariant="bold">P</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup><mml:msup><mml:mi>H</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>+</mml:mo><mml:mi mathvariant="bold">R</mml:mi></mml:mrow></mml:mfenced><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msup><mml:mi>y</mml:mi><mml:mi mathvariant="normal">o</mml:mi></mml:msup><mml:mo>-</mml:mo><mml:mi>H</mml:mi><mml:msup><mml:mi mathvariant="bold">x</mml:mi><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:mrow></mml:mfenced><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            Using this statistic, the <inline-formula><mml:math id="M205" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> is defined as follows:
              <disp-formula id="Ch1.E12" content-type="numbered"><label>12</label><mml:math id="M206" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:msup><mml:mi mathvariant="normal">traceYY</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            The performance of the background error covariance matrix is determined based on
the high and lower value of <inline-formula><mml:math id="M207" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>. The <inline-formula><mml:math id="M208" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> value should converge to
1; a value higher (lower) than 1 indicates underestimation (overestimation)
of the background error covariance matrices. Our results suggest that the background error covariance matrix is highly underestimated in both RTPS and
FM covariance inflation methods (Fig. 7b). However, the <inline-formula><mml:math id="M209" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> values'
convergence towards 1 is better in the case of RTPS compared to the FM
covariance inflation method, which indicates the improved representation of
background errors and then more appropriate data assimilation corrections in
the case of the RTPS inflation method. The <inline-formula><mml:math id="M210" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> distribution starts
saturating after the month of March. Post-March analysis shows the
background error covariance matrix underestimation is much higher
(<inline-formula><mml:math id="M211" display="inline"><mml:mrow><mml:mi mathvariant="italic">&gt;</mml:mi><mml:mn mathvariant="normal">100</mml:mn></mml:mrow></mml:math></inline-formula> %) in the case of FM compared to the RTPS covariance inflation
method.</p>
</sec>
<sec id="Ch1.S4.SS2.SSS5">
  <label>4.2.5</label><?xmltex \opttitle{CH${}_{{4}}$ LETKF sensitivity to the initial ensemble spread}?><title>CH<inline-formula><mml:math id="M212" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF sensitivity to the initial ensemble spread</title>
      <p id="d1e3410">A test case for CH<inline-formula><mml:math id="M213" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF data assimilation has been performed, where
the initial spread is provided by considering the initial perturbation on
each model grid with spatial error correlation between grid points among
ensemble members, with a global mean correlation of 20 %. In this case, we
found that the analysis fluxes are extremely sensitive to the initial
ensemble spread if prior fluxes are perturbed with more than 5 % prior
uncertainty. Therefore, we used initial ensemble perturbation with only
2 % prior uncertainty. Reducing the initial ensemble spread reduces the
CH<inline-formula><mml:math id="M214" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation sensitivity (<inline-formula><mml:math id="M215" display="inline"><mml:mrow><mml:mi mathvariant="italic">&gt;</mml:mi><mml:mn mathvariant="normal">60</mml:mn></mml:mrow></mml:math></inline-formula> %). However, it also
poses a challenge to mitigate the underdispersed background error
covariance matrix. We performed LETKF data assimilations in this case with
the RTPS covariance inflation method (<inline-formula><mml:math id="M216" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">RTPS</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.9</mml:mn></mml:mrow></mml:math></inline-formula>
optimized value is used here uniformly) with an 8 d long assimilation window
and 100 ensemble members and calculated the normalized RMSE between the analysis
and true fluxes (Supplement Fig. S5). It is noteworthy that the
estimated error between the analysis and true fluxes (Fig. S5) with this setting
(grid-wise initial ensemble spread) is still larger (25 %) than the case
when the region-wise initial ensemble spread is used (Fig. 7a; 100 ensemble
size). It suggests that initial ensemble spreads among ensemble members
need to be meticulously chosen so that they best represent CH<inline-formula><mml:math id="M217" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> variability
among ensembles to estimate the CH<inline-formula><mml:math id="M218" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux.</p>
      <p id="d1e3475">Note that the OSSEs used in this study did not consider the effects of
model errors other than CH<inline-formula><mml:math id="M219" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> fluxes, such as model transport errors. In
real situations, model errors can have a substantial impact on flux
estimates
(Locatelli et al.,
2013), which needs to be taken into account in background covariances.
Therefore, the optimal data assimilation setting can differ between the
OSSEs presented in this study and real observation cases. Further efforts,
e.g., by conducting a more comprehensive OSSE that accounts for various
model errors and by performing various sensitivity calculations in real
cases, would provide an improved understanding of the optimal inflation
settings to improve CH<inline-formula><mml:math id="M220" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimates in following study.</p>
</sec>
<sec id="Ch1.S4.SS2.SSS6">
  <label>4.2.6</label><?xmltex \opttitle{Estimated CH${}_{{4}}$ flux analysis}?><title>Estimated CH<inline-formula><mml:math id="M221" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux analysis</title>
      <p id="d1e3514">Figure 8 shows the regional flux seasonal cycle comparison for the
estimated fluxes over 15 terrestrial regions with the cycles of the prior and
true fluxes. We have also shown assimilation results in the case of the FM inflation
method in the Supplement (Fig. S6), which shows the flux estimation
disagreement over more regions compared to the RTPS inflation method, e.g., for
tropical and North America, the whole African continent, and Australia–New Zealand.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><?xmltex \currentcnt{8}?><?xmltex \def\figurename{Figure}?><label>Figure 8</label><caption><p id="d1e3519">Same as Fig. 3 but after assimilating synthetic GOSAT
observations.</p></caption>
            <?xmltex \igopts{width=497.923228pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f08.png"/>

          </fig>

      <p id="d1e3528">We have shown the GOSAT observations in Figs. 6 and S7. We found very marginal flux estimation improvement over Central
Africa after May (Fig. 8), which could be associated with the lower GOSAT
coverage over this region (Fig. 6). On the other hand, over northern Africa,
no improvement in flux estimation is found. In the case of dense OSSEs too (Fig. 3), we did not find satisfactory flux estimation over northern Africa, which
is most probably related to the insufficient initial spread among ensemble
members over this region (we used the same initial ensemble spread in both
OSSE cases). Over Europe, GOSAT observations are remarkably fewer,
specifically for the first few months (January–April; Supplement
Fig. S7). Therefore, the flux update over Europe would be influenced by the
observations from neighboring regions falling under the chosen cutoff radius
that are mainly in northern Africa, where the flux estimation itself not
satisfactory. It could also be noticed that the retrieval error added in
this OSSE case is high over Europe (September–October;<?pagebreak page1833?> Supplement Fig. S7) and its adjacent sea (Mediterranean Sea; June–August),
which could also affect the surface CH<inline-formula><mml:math id="M222" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation.</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="d1e3543">Monthly mean true (true; top left panel) and estimated (FM
analysis; middle left panel, RTPS analysis; bottom left panel) CH<inline-formula><mml:math id="M223" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux
after assimilating column-averaged synthetic CH<inline-formula><mml:math id="M224" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations (Fig. 6) during June using FM and RTPS inflation methods. The associated bias with
prior and estimated fluxes is also shown (prior-true; top right panel;
FM-true; middle right panel, RTPS-true; bottom right panel).</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f09.png"/>

          </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F10" specific-use="star"><?xmltex \currentcnt{10}?><?xmltex \def\figurename{Figure}?><label>Figure 10</label><caption><p id="d1e3572">Same as Fig. 9 but for November.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/16/1823/2023/gmd-16-1823-2023-f10.png"/>

          </fig>

      <p id="d1e3581">Figures 9 and 10 show spatial patterns of the true and estimated fluxes by
assimilating the column-averaged CH<inline-formula><mml:math id="M225" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations during June and
November (Fig. 6). It may be noticed that the RTPS covariance inflation method
is more able to estimate the true flux pattern compared to the FM covariance
inflation method. The spatial pattern shown using the RTPS inflation method
emphasizes the positive and negative bias in the estimated flux (Figs. 9 and
10) but generally agrees with the flux seasonal cycle plots shown in Fig. 8.</p>
      <?pagebreak page1834?><p id="d1e3593">Our LETKF CH<inline-formula><mml:math id="M226" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> data assimilation experiment by assimilating GOSAT
synthetic observation with the implementation of the advanced RTPS
covariance inflation method better estimates the time-evolving surface
CH<inline-formula><mml:math id="M227" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> fluxes compared to the FM covariance inflation method. The difficulty
to estimate the surface CH<inline-formula><mml:math id="M228" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux over a few regions may be overcome by
applying additional methodologies, such as the assimilation of surface
observations simultaneously and the use of information about the CH<inline-formula><mml:math id="M229" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
flux climatology. A correction factor derived based on empirical
formulation that could use CH<inline-formula><mml:math id="M230" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux climatology information is needed
to apply to maintain the CH<inline-formula><mml:math id="M231" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> mass conservation. This could be
implemented by checking the simulated CH<inline-formula><mml:math id="M232" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> burden gain between years
in comparison with the observed CH<inline-formula><mml:math id="M233" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> growth rates.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <label>5</label><title>Summary</title>
      <p id="d1e3680">In this study, we have introduced a 4D-LETKF data assimilation system that
utilizes MIROC4-ACTM as a forward model for CH<inline-formula><mml:math id="M234" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation. This
study has extensively tested both FM and RTPS inflation methods for the
LETKF CH<inline-formula><mml:math id="M235" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation. We have conducted two experiments to
demonstrate the ability of LETKF system to estimate the CH<inline-formula><mml:math id="M236" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> surface
flux globally. In Experiment 1, we have assimilated the synthetic dense
surface CH<inline-formula><mml:math id="M237" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observations, while in Experiment 2, synthetic GOSAT
CH<inline-formula><mml:math id="M238" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> observations are assimilated. Based on the results of the
sensitivity tests using FM and RTPS inflation methods in Experiment 1, we
have found that RTPS inflation produces significantly less normalized RMSE
(10 %–15 %) compared to the FM inflation method. In Experiment 2, we discussed
LETKF parameters, such as different inflation techniques, ensemble size,
assimilation window, initial ensemble spread sensitivity, and <inline-formula><mml:math id="M239" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>
test. The ensemble size (this study uses maximum 100 ensemble members)
sensitivity test suggests that more ensemble members could help to
accurately represent the covariance matrix with a higher number of degrees of freedom. The
assimilation window sensitivity test shows that an 8 d assimilation
window reduces the normalized flux RMSE by about 10 % compared to a 3 d
assimilation window in the case of GOSAT synthetic observations assimilation.</p>
      <?pagebreak page1835?><p id="d1e3740">Our approach of assimilation with RTPS inflation could provide a higher number of degrees
of freedom to fit the ensemble of CH<inline-formula><mml:math id="M240" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> concentrations to the observed
ones, resulting in the improved analyzed fluxes. The RTPS inflation method is
capable of obtaining reasonable flux estimates with a normalized annual mean
bias of 0.04 and 0.61 in the case of dense surface synthetic observations and
GOSAT synthetic observations, respectively. We demonstrated in our
sensitivity OSSE with synthetic GOSAT observations that, over
American and African continents and also over Australia–New Zealand, the
LETKF data assimilation with the FM inflation method does not show much
improvement in the true flux estimation, but the RTPS inflation method
reasonably estimates the true flux over most of these regions. One of the
reasons for better flux estimates with the RTPS inflation method is the drastic prevention of analysis spread. In the CH<inline-formula><mml:math id="M241" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF flux
estimation, the surface CH<inline-formula><mml:math id="M242" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux is not a prognostic state vector in the
ACTM, which results in the continuous decay of spread in analysis steps.
The RTPS inflation method could mitigate such an underdispersed spread problem.
This study finds that spatially homogeneous relaxation is not sufficient. It
needs to be fine-tuned and applied conditionally.</p>
      <p id="d1e3770">The sensitivity of LETKF CH<inline-formula><mml:math id="M243" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> flux estimation to the initial ensemble spread
needs to be carefully dealt with when applied to real data assimilation
system. A future OSSE with an additive covariance inflation technique could be
interesting while applied with the RTPS inflation method for CH<inline-formula><mml:math id="M244" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> LETKF data
assimilation since in additive covariance inflation, initial estimated flux
error cannot propagate. The state vector augmentation technique used here
updates the flux after each data assimilation cycle, but it does not conserve
the total atmospheric CH<inline-formula><mml:math id="M245" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> amount, which is one of the limitations of
this work. A correction factor needs to be implemented to conserve the total
atmospheric CH<inline-formula><mml:math id="M246" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> amount after completion of a few data assimilation
cycles. We have not accounted for the transport error due to meteorological
fields in this work
(Patra
et al., 2011); in the case of real observation data assimilation, a week-long
window may introduce transport errors in CH<inline-formula><mml:math id="M247" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> analysis because of
the nonlinear growth of ensemble perturbations.</p>
</sec>

      
      </body>
    <back><notes notes-type="codedataavailability"><title>Code and data availability</title>

      <p id="d1e3822">The LETKF source codes can be accessed from <ext-link xlink:href="https://doi.org/10.5281/zenodo.7127658" ext-link-type="DOI">10.5281/zenodo.7127658</ext-link> (Bisht et al., 2022a). All the scripts for running the
LETKF data assimilation software and the input and output result data files are
available at <ext-link xlink:href="https://doi.org/10.5281/zenodo.7098323" ext-link-type="DOI">10.5281/zenodo.7098323</ext-link> (Bisht et al., 2022b). The CH<inline-formula><mml:math id="M248" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>
ACTM simulation module coupled with MIROC4-AGCM can be accessed from
<ext-link xlink:href="https://doi.org/10.5281/zenodo.7118365" ext-link-type="DOI">10.5281/zenodo.7118365</ext-link> (Bisht et al., 2022c). The source code of
MIROC4-AGCM is archived at <ext-link xlink:href="https://doi.org/10.5281/zenodo.7274240" ext-link-type="DOI">10.5281/zenodo.7274240</ext-link> (Patra et al., 2022) with restriction because of the
copyright policy of the MIROC developer community. This work did not contribute to the MIROC4 source code development.</p>
  </notes><app-group>
        <supplementary-material position="anchor"><p id="d1e3846">The supplement related to this article is available online at: <inline-supplementary-material xlink:href="https://doi.org/10.5194/gmd-16-1823-2023-supplement" xlink:title="pdf">https://doi.org/10.5194/gmd-16-1823-2023-supplement</inline-supplementary-material>.</p></supplementary-material>
        </app-group><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e3855">The LETKF data assimilation experiments were designed by JSHB. PKP, MT, and
TS helped to set up the LETKF code on MIROC4-ACTM for CH<inline-formula><mml:math id="M249" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula> data assimilation.
The manuscript was prepared by JSHB, and analysis interpretation input and
feedback were provided by PKP, TS, and KM. All coauthors, KM, TS, PKP, NS, MT, and
YK, contributed to the writing and revision of the paper.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <?pagebreak page1836?><p id="d1e3870">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="d1e3876">Publisher’s note: Copernicus Publications remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.</p>
  </notes><ack><title>Acknowledgements</title><p id="d1e3882">We acknowledge Ryu Saito for the initial setup of the LETKF code on MIROC4-ACTM for CH<inline-formula><mml:math id="M250" display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">4</mml:mn></mml:msub></mml:math></inline-formula>. We also thank Takemasa Miyoshi for his LETKF scheme, which served as the basis for the development of our data assimilation system.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e3896">This research has been supported by the Environment Research and Technology Development Fund (grant no. JPMEERF20182002) of the Environmental Restoration and Conservation
Agency of Japan and the GOSAT-GW project fund.</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e3902">This paper was edited by Shu-Chih Yang and reviewed by two anonymous referees.</p>
  </notes><ref-list>
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