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  <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-19-10077-2026</article-id><title-group><article-title>Optimization of the fast layer transmittance algorithm in RTTOV v13.1 for strong water vapor absorption channels of the FY-3F HIRAS-II instrument using LBLRTM v12.11</article-title><alt-title>Optimization of the fast layer transmittance algorithm in RTTOV v13.1</alt-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Zhang</surname><given-names>Panxiang</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="yes" rid="aff3">
          <name><surname>Zhang</surname><given-names>Peng</given-names></name>
          <email>zhangp@cma.gov.cn</email>
        <ext-link>https://orcid.org/0000-0002-7115-1389</ext-link></contrib>
        <contrib contrib-type="author" corresp="yes" rid="aff4">
          <name><surname>Ma</surname><given-names>Gang</given-names></name>
          <email>magang@cma.gov.cn</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Li</surname><given-names>Rui</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff5">
          <name><surname>Lee</surname><given-names>Lu</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-3665-1556</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff5">
          <name><surname>Bai</surname><given-names>Wenguang</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff5">
          <name><surname>Qi</surname><given-names>Chengli</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>University of Science and Technology of China, Hefei, 230052, China</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Beijing Huayun Shinetek Technology Co., Ltd., Beijing, 100081, China</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>Meteorological Observation Centre of CMA, Beijing, 100081, China</institution>
        </aff>
        <aff id="aff4"><label>4</label><institution>China Meteorological Administration Earth System Numerical Prediction Centre, Beijing, 100081, China</institution>
        </aff>
        <aff id="aff5"><label>5</label><institution>National Satellite Meteorological Centre, Beijing, 100081, China</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Peng Zhang (zhangp@cma.gov.cn) and Gang Ma (magang@cma.gov.cn)</corresp></author-notes><pub-date><day>22</day><month>October</month><year>2026</year></pub-date>
      
      <volume>19</volume>
      <issue>20</issue>
      <fpage>10077</fpage><lpage>10101</lpage>
      <history>
        <date date-type="received"><day>17</day><month>October</month><year>2025</year></date>
           <date date-type="rev-request"><day>7</day><month>April</month><year>2026</year></date>
           <date date-type="rev-recd"><day>10</day><month>August</month><year>2026</year></date>
           <date date-type="accepted"><day>19</day><month>August</month><year>2026</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2026 Panxiang Zhang et al.</copyright-statement>
        <copyright-year>2026</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/19/10077/2026/gmd-19-10077-2026.html">This article is available from https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026.html</self-uri><self-uri xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026.pdf">The full text article is available as a PDF file from https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026.pdf</self-uri>
      <abstract><title>Abstract</title>

      <p id="d2e165">Fast and accurate calculation of atmospheric transmittance is essential for infrared atmospheric remote sensing and satellite data assimilation. However, fast radiative transfer models show significant errors in strong water vapor absorption channels (e.g., near 6.7 <inline-formula><mml:math id="M1" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>). An important reason is the numerical instability encountered during the regression of transmittance coefficients when dealing with lower and middle atmosphere. To address this, this study proposes an optimized scheme to calculate atmospheric transmittance vertical profiles for the RTTOV (Radiative Transfer for TOVS) fast transmittance algorithm. The method introduces a physically motivated transmittance threshold to sub-select training samples and employs a cumulative transmittance-based weighting factor within a weighted least squares regression to recalibrate the transmittance coefficients. It aims to optimize the calculation scheme for transmittance coefficients of the Hyperspectral Infrared Atmospheric Sounder-II (HIRAS-II) instrument onboard the Fengyun-3F satellite (FY-3F). The method is assessed by calculations on the training profile datasets provided within the RTTOV model framework. By comparing transmittance and brightness temperature calculations at 6.7 <inline-formula><mml:math id="M2" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> from this method with those from a line-by-line model and observations from HIRAS-II, the results show that the accuracy of the forward model for the 6.7 <inline-formula><mml:math id="M3" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption channel is significantly enhanced by applying a threshold-based noise reduction method. This improvement enhances the stability and reliability of the transmittance calculations for this strong absorption band. Further accuracy enhancements are obtained by incorporating weighting corrections into the calculations of transmittance coefficients. The root mean square error (RMSE) and bias of the observation minus background (OMB) time series for FY-3F HIRAS-II demonstrate that the transmittance coefficient calculation scheme with weighting factor correction improves the forward model accuracy, which is more consistent with RTTOV simulation results. The mean OMB bias at the 6.7 <inline-formula><mml:math id="M4" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption-peak channel is closer to zero than that of RTTOV, whereas the OMB biases at the channels on either side of the absorption peak remain consistent with those of RTTOV.</p>
  </abstract>
    
<funding-group>
<award-group id="gs1">
<funding-source>National Natural Science Foundation of China</funding-source>
<award-id>U2442214</award-id>
<award-id>42475170</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="d2e217">The Hyperspectral Infrared Atmospheric Sounder (HIRAS; Li et al., 2022; Zhou et al., 2025) is a key instrument onboard the FengYun-3 (FY-3) polar-orbiting meteorological satellite series, specifically FY-3D (Zhang et al., 2018), and the second- generation HIRAS-II instrument on FY-3E (Zhang et al., 2024) and FY-3F (Zeng et al., 2025). The first-generation HIRAS-I instrument onboard FY-3D covers three spectral bands: long-wave infrared (LW) from 648.75 to 1136.25 cm<sup>−1</sup> (15.41 to 8.8 <inline-formula><mml:math id="M6" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>), medium-wave infrared (MW) from 1208.75 to 1751.25 cm<sup>−1</sup> (8.27 to 5.71 <inline-formula><mml:math id="M8" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>), and short-wave infrared (SW) from 2153.75 to 2551.25 cm<sup>−1</sup> (4.64 to 3.92 <inline-formula><mml:math id="M10" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>), with a nadir spatial resolution of 16 km (Wu et al., 2020). In contrast, the second-generation HIRAS-II instrument on FY-3E and FY-3F offers expanded spectral coverage: the LW band extends to 1169.375 cm<sup>−1</sup>, the MW band spans 1167.5 to 1921.25 cm<sup>−1</sup> (8.57 to 5.2 <inline-formula><mml:math id="M13" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>), and the SW band starts from 1919.375 cm<sup>−1</sup>, while maintaining 0.625 cm<sup>−1</sup> spectral resolution and improving nadir resolution to 14 km (Zeng et al., 2025). This instrument is primarily used to retrieve high-precision vertical profiles of atmospheric temperature, humidity, ozone, and atmospheric composition variables, from the Earth's surface to the lower stratosphere (Alvarado et al., 2013; Menzel et al., 2018; Zhou et al., 2025). Retrieval of such profiles from hyperspectral infrared remote sensing data typically adopts the one-dimensional variational (1D-VAR) technique, and the performance of this retrieval algorithm is highly dependent on the simulation accuracy of the radiative transfer forward model (Zhu et al., 2020; Li et al., 2022). High-resolution infrared atmospheric sounding data have been assimilated into global Numerical Weather Prediction Models (NWP) by organizations such as the European Centre for Medium-Range Weather Forecasts (ECMWF), making it one of the most influential satellite observations for improving numerical forecast quality (Eyre et al., 2020, 2022). Fast radiative transfer models establish functional relationships between atmospheric state variables in numerical weather prediction models and satellite channel radiances (Bai et al., 2017, 2020). Therefore, both aspects must be scrutinized to ensure the accuracy of the fast radiative transfer model in the assimilation of satellite observations (Eyre et al., 1993; Matricardi et al., 2004).</p>
      <p id="d2e345">Although line-by-line radiative transfer models, such as the Line-by-line Radiative Transfer Model (LBLRTM; Clough et al., 2005) by Atmospheric and Environmental Research and the Reference Forward Model (RFM; Dhudia, 2017), exhibit high computational accuracy, their high computational cost makes them difficult to apply in operational numerical weather forecasting and retrievals (McMillin and Fleming, 1976; Matricardi and Saunders, 1999; Saunders et al., 1999). Fast radiative transfer models convert layer-by-layer atmospheric transmittance coefficients into linear polynomial approximations. This approach improves computational efficiency, enabling forward models to be applied in assimilation and inversion operations (McMillin et al., 1995; Li et al., 2017; Schmit et al., 2019). By assuming that atmospheric state variables and the radiative spectral characteristics of spaceborne sensor channels exhibit linear uncorrelated, the accurate expression for layer-by-layer monochromatic atmospheric transmittance can be simplified to a channel-independent multivariate linear expression. The least-squares solution to the system of equations constructed from this multivariate linear expression yields the fast forward model coefficients for the transmittance of each channel. These coefficients are multiplied by the predictors derived from atmospheric sample profiles in turn and then summed, which produces the layer transmittance for each channel (Hannon et al., 1996; Kleespies et al., 2004; Chevallier et al., 2006). When atmospheric sample profiles are representative, the fast radiative transfer model can be applied universally (Matricardi, 2003).</p>
      <p id="d2e348">The fast radiative transfer model was first proposed by McMillin and Fleming (1976), based on a Taylor series expansion. It uses statistical regression methods to calculate satellite channel transmittance within fixed gas absorption layers, evolving into the first fast radiative transfer model for satellite forward simulations: Optical Path Transmittance Model (OPTRAN). Subsequently, this model was applied to the Community Radiative Transfer Model (CRTM). Since variations in ozone content significantly affect simulations for channels near 9.6 <inline-formula><mml:math id="M16" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> and 118 GHz, O<sub>3</sub> is separated from fixed gases and treated as a variable gas for independent calculation (Eyre and Woolf, 1988). This approach later evolved into the RTTOV radiative transfer model. At the European Centre for Medium-Range Weather Forecasts, water vapor and ozone are treated as variable gases in fast transmittance calculations for infrared and microwave sounders. Although the simulation errors in the stratosphere, surface, water vapor, and ozone absorption channels exceed instrument noise, this method remains applicable to numerical weather prediction data assimilation systems (Saunders et al., 1999; Matricardi et al., 2004). Using line-by-line models to calculate transmittance as the true value, a fast transmittance calculation model for infrared hyperspectral vertical detectors was developed. This model was used to perform pre-launch simulation studies of the IASI instrument. Results indicate that the simulated brightness temperature difference between the IASI fast radiative transfer model and the line-by-line model is smaller than the instrument noise (Matricardi and Saunders, 1999; Matricardi, 2007, 2009). Subsequently, a high-resolution transmittance database was generated using 83 atmospheric sample profiles (2016) and LBLRTM v12.11, thereby enhancing the accuracy of the forward model for satellite infrared detectors (Matricardi, 2008a, 2009). Di et al. (2018) proposed a weighted least squares method, incorporating local sample profiles alongside the 83 atmospheric sample profiles, to construct a fast transmittance model for FY-4A GIIRS. Compared to line-by-line radiative transfer model simulations of brightness temperatures, the root mean square error was less than 0.4 K. Bormann et al. (2009) and Hocking et al. (2021) successively introduced new parameterization schemes in RTTOV to calculate trace gas channel transmittances, further improving the simulation accuracy of trace gas absorption channels. With the advancement of fast radiative transfer models, the main models currently used are RTTOV (Radiative Transfer for TOVS), developed by the European Centre for Medium-Range Weather Forecasts (Hocking et al., 2021), CRTM (Community Radiative Transfer Model), developed by the Joint Center for Satellite Data Assimilation (Johnson et al., 2023), and ARMS (Advanced Radiative Transfer Modeling System), developed by the China Meteorological Administration (Weng et al., 2020).</p>
      <p id="d2e370">As a key factor influencing weather and climate, water vapor is essential for cloud formation and precipitation. However, existing fast radiative transfer models have been shown to exhibit significant biases in simulating radiances within strong water vapor absorption bands (Saunders et al., 1999; Matricardi et al., 2004; Saunders et al., 2018). These errors directly propagate into retrieved atmospheric profiles, degrading the accuracy of downstream applications such as numerical weather prediction. Saunders et al. (2018) noted that for satellite detection channels affected by water vapor, the error is greater than that of window channels, indicating that the simulation accuracy of fast radiative transfer models still needs improvement. Improving the simulation accuracy of water vapor absorption channels in radiative transfer models is crucial for the effective use of satellite infrared data in numerical forecasting and climate analysis.</p>
      <p id="d2e374">To further reduce simulation errors in Hyperspectral Infrared Atmospheric Sounder (HIRAS; Li et al., 2022; Zhou et al., 2025)  and advance its application in numerical weather prediction, this study addresses the significant simulation brightness temperature errors in the water vapor absorption channels of infrared hyperspectral vertical sounders (Saunders et al., 2018). We optimized the channel transmittance coefficient calculation model for the FY-3F HIRAS-II (Zhou et al., 2025) instrument by applying a thresholding method to exclude poor-quality samples and introducing different weights as constraints. These modifications significantly improved the forward model accuracy in the 1300–1600 cm<sup>−1</sup> water vapor absorption band. The optimization was developed and evaluated using LBLRTM v12.11 on the standard RTTOV atmospheric profile datasets. Applied to the strong water vapor channels of the FY-3F HIRAS-II instrument, the optimized scheme significantly reduces errors in simulated transmittance compared to the baseline RTTOV v13.1 algorithm. Validation against HIRAS-II observations shows a notable improvement.</p>
      <p id="d2e389">From an application perspective, the optimized model not only significantly enhances the reliability of fast radiative transfer models but also provides strong technical support for improving the quality of HIRAS-II satellite data assimilation, and the accuracy of middle and lower atmospheric water vapor retrieval, which is of great significance for deepening the understanding of the water cycle process, monitoring climate change, and improving the level of atmospheric environmental governance. It should be noted that this study focuses on the 6.7 <inline-formula><mml:math id="M19" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> channel of HIRAS-II, but the optimization scheme can be extended to the fast transmittance calculation for strong absorption channels of other trace gases (e.g., carbon dioxide and ozone) in satellite remote sensing.  Section 2 details the experimental methodology for establishing the profile lookup table and weighting function, as well as the data employed. Section 3 outlines the experimental design. Section 4 evaluates the optimized coefficients against LBLRTM, and Sect. 5 assesses the model using HIRAS-II observations. Section 6 provides a synthesis and discussion.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Theory and Methods</title>
<sec id="Ch1.S2.SS1">
  <label>2.1</label><title>Fast Radiative Transfer Model</title>
      <p id="d2e417">RTTOV was first developed as a fast radiative transfer model at the European Centre for Medium-Range Weather Forecasts (ECMWF) in the early 1990s (Eyre, 1991; Eyre et al., 1993). The original fast radiative transfer model (RTTOV v3) was described by Eyre (1991). After the mid-1990s, development was continued by the Numerical Weather Prediction Satellite Application  (<uri>https://nwp-saf.eumetsat.int/site/software/rttov/</uri>, last access: 15 October 2026) Facility (NWP SAF,  Rayer, 1995), supported by the European Organisation for the Exploitation of Meteorological Satellites (EUMETSAT). Subsequently, starting with RTTOV v6 in March 2000, the NWP SAF made the technical documents for this fast radiative transfer model publicly available via its official website (Saunders et al., 2018). The current version, RTTOV v14 (Hocking et al., 2025), supports fast radiative transfer calculations for over 120 satellite sensors covering the visible, near-infrared, infrared, microwave, and ultraviolet.</p>
      <p id="d2e423">In the RTTOV model, infrared spectral gas absorption is primarily caused by water vapor, ozone, and uniformly mixed gases with a nearly constant spatial and temporal distribution. The total channel transmittance is calculated as the product of the transmittances of these three components (as shown in Eq. 1). Equation (1) accounts for the absorption overlap among these gases, thereby reducing the adverse effect on the forward model's accuracy.

            <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M20" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">total</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">mix</mml:mi></mml:msubsup><mml:mo>⋅</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">mix</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="normal">wv</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">mix</mml:mi></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>⋅</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">mix</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="normal">wv</mml:mi><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="normal">o</mml:mi><mml:mn mathvariant="normal">3</mml:mn></mml:msub></mml:mrow></mml:msubsup></mml:mrow><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">mix</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="normal">wv</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula></p>
      <p id="d2e539">The relationship between channel transmittance and optical thickness is defined by Eq. (2). The optical depth for a given atmospheric layer is calculated using the iterative Eq. (3):

                <disp-formula specific-use="gather" content-type="numbered"><mml:math id="M21" display="block"><mml:mtable displaystyle="true"><mml:mlabeledtr id="Ch1.E2"><mml:mtd><mml:mtext>2</mml:mtext></mml:mtd><mml:mtd><mml:mrow><mml:mstyle displaystyle="true" class="stylechange"/><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mi>ln⁡</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:mtd></mml:mlabeledtr><mml:mlabeledtr id="Ch1.E3"><mml:mtd><mml:mtext>3</mml:mtext></mml:mtd><mml:mtd><mml:mrow><mml:mstyle displaystyle="true" class="stylechange"/><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mi>ln⁡</mml:mi><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>n</mml:mi></mml:munderover><mml:msub><mml:mi>a</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>,</mml:mo><mml:mi>k</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula>

          where <inline-formula><mml:math id="M22" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is the predictor, which is a function of zenith angle, temperature, humidity, and pressure. <inline-formula><mml:math id="M23" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> denotes the optical thickness from atmospheric level <inline-formula><mml:math id="M24" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula> to the top of the atmosphere for channel <inline-formula><mml:math id="M25" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>, and<inline-formula><mml:math id="M26" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> represents the transmittance from level  <inline-formula><mml:math id="M27" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula> to the top of the atmosphere. <inline-formula><mml:math id="M28" display="inline"><mml:mrow><mml:msub><mml:mi>a</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>,</mml:mo><mml:mi>k</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is the transmittance coefficient, where <inline-formula><mml:math id="M29" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula> denotes the channel index, <inline-formula><mml:math id="M30" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula> denotes the pressure level index, and <inline-formula><mml:math id="M31" display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> denotes the predictor index. For selected atmospheric sample profiles, we use LBLRTM to compute an accurate channel-by-channel transmittance dataset. When the left-hand side of Eq. (3) and the transmittance predictors are  known, Eq. (3) forms an overdetermined homogeneous linear system of equations: <inline-formula><mml:math id="M32" display="inline"><mml:mrow><mml:msub><mml:mi>a</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>,</mml:mo><mml:mi>k</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is the least-squares solution to this system.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <label>2.2</label><title>A Threshold Approach</title>
      <p id="d2e830">The training dataset comprises 83 atmospheric profiles. While these profiles cover a wide range of extreme meteorological conditions (Chevallier et al., 2006), not every individual profile is utilized in the layer-by-layer training of the fast transmittance coefficients. Based on the instrument characteristics of the Hyperspectral Infrared Atmospheric Sounder, the spectral response function is constructed using the Hamming window function (Harris, 1987). Because the values of the two wings of the spectral response function (SRF) of interferometric instruments oscillate around zero, the shape of this function can lead to physically unrealistic negative transmittance values in strong absorption bands after convolution with the monochromatic spectrum (transmittance is close to zero). Additionally, for strong water vapor absorption channels, under conditions of abundant water vapor content, the total transmittance from a given level to the top of the atmosphere (TOA) becomes an extremely small quantity in the middle and lower atmosphere. Thus, division by small quantities (<inline-formula><mml:math id="M33" display="inline"><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:math></inline-formula>)  arises when calculating the optical depth of this layer. This leads to abnormal values in the total transmittance, causing numerical instability in the least-squares solution for the system of Eq. (3). Threshold screening for transmittance achieves numerically stable and accurate atmospheric profile sampling and enhances the stability of the least-squares regression solution. However, the choice of thresholds significantly affects both the training profiles and the optimality of the least-squares solution. The threshold method sets distinct thresholds for different channels to select atmospheric profiles for the regression. When the level-to-space transmittance falls below this threshold, samples below that height (i.e., at higher pressure/lower altitude) are considered too strongly affected by computational errors and are therefore excluded. Since the magnitude of transmittance is relatively small below that height (i.e., at higher pressure/lower altitude), the transmittance from this layer to the surface layer is considered to make a negligible contribution to the total atmospheric transmittance.</p>
</sec>
<sec id="Ch1.S2.SS3">
  <label>2.3</label><title>The Weighted Least-Squares Method</title>
      <p id="d2e874">Ordinary least squares (OLS) obtains the optimal solution to the objective function when the sum of squared deviations between actual and predicted values is minimized. The error function being minimized, for this optimal solution, is:

            <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M34" display="block"><mml:mrow><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mi>p</mml:mi></mml:mrow></mml:munderover><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi>m</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>m</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mspace width="1em" linebreak="nobreak"/><mml:mfenced open="(" close=")"><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:mo>,</mml:mo><mml:mi mathvariant="normal">…</mml:mi><mml:mo>,</mml:mo><mml:mi>p</mml:mi></mml:mrow></mml:mfenced></mml:mrow></mml:math></disp-formula>

          where  <inline-formula><mml:math id="M35" display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mi>m</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> denotes the optical thickness of a single atmospheric layer for the <inline-formula><mml:math id="M36" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula>th sample, and <inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>m</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> denotes the fitted values of the <inline-formula><mml:math id="M38" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula>th sample, m denotes the index of the training profiles involved in the statistical analysis from 1 to <inline-formula><mml:math id="M39" display="inline"><mml:mrow><mml:mn mathvariant="normal">83</mml:mn><mml:mo>×</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula>, and <inline-formula><mml:math id="M40" display="inline"><mml:mi>p</mml:mi></mml:math></inline-formula> denotes the total number of samples in the training dataset. <inline-formula><mml:math id="M41" display="inline"><mml:mi>S</mml:mi></mml:math></inline-formula> denotes the sum of squared deviations between actual and predicted values. When <inline-formula><mml:math id="M42" display="inline"><mml:mi>S</mml:mi></mml:math></inline-formula> is minimized, the optimal solution for <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>m</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is obtained.</p>
      <p id="d2e1038">The ordinary least squares method assumes homoscedasticity, giving equal weight to all data involved in the calculation. However, in practice, some data are more important than others. To retain a sufficient number of samples involved in the calculation while reducing the contribution of non-critical data, a method of assigning different weights to the data is adopted.</p>
      <p id="d2e1041">Weighted least squares enables models to better fit datasets with heteroscedastic properties by assigning different weights to different data points. In this case, Eq. (4) becomes:

            <disp-formula id="Ch1.E5" content-type="numbered"><label>5</label><mml:math id="M44" display="block"><mml:mrow><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mi>p</mml:mi></mml:mrow></mml:munderover><mml:msub><mml:mi>W</mml:mi><mml:mi>m</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi>m</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>m</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mspace linebreak="nobreak" width="1em"/><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:mn mathvariant="normal">2</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:mo>,</mml:mo><mml:mi mathvariant="normal">…</mml:mi><mml:mo>,</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula>

          where <inline-formula><mml:math id="M45" display="inline"><mml:mrow><mml:msub><mml:mi>W</mml:mi><mml:mi>m</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> represents the weight factor.</p>
      <p id="d2e1139">The weight factor <inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:msub><mml:mi>W</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>⋅</mml:mo><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mrow></mml:math></inline-formula> is selected, and the approach screens out non-physical negative transmittance from satellite radiances.  From the top of the atmosphere to the surface, as the integrated transmittance from a given layer to space decreases, the layer lies closer to the surface. For these near-surface layers, their contribution to the total atmospheric absorption decreases. This is because the overlying atmosphere has already absorbed a significant portion of the incoming radiation, leaving less energy to be absorbed by the lower layers. Consequently, for layers with small transmittance (i.e., near-surface layers with weak signal), their regression weight should be reduced accordingly. Based on this physical understanding, we select a function of transmittance as the basic form of the weight coefficient. After analyzing the characteristics of transmittance variation and comparing the effects of different weight functions (such as <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M48" display="inline"><mml:msqrt><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>⋅</mml:mo><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:math></inline-formula>, <inline-formula><mml:math id="M49" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M50" display="inline"><mml:msqrt><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:math></inline-formula>, etc.) on the regression results, we ultimately adopt the integrated transmittance from the layer out  to space, <inline-formula><mml:math id="M51" display="inline"><mml:msqrt><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>⋅</mml:mo><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:math></inline-formula> as the weight factor in the weighted least squares method.</p>
      <p id="d2e1245">In the second weighting scheme, the weighting factors are applied to both the independent variables (predictors) and the dependent variable prior to the statistical regression, and the regression coefficients are subsequently derived using the weighted data. This entails weighting the left-hand side term <inline-formula><mml:math id="M52" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and the right-hand side term <inline-formula><mml:math id="M53" display="inline"><mml:mrow><mml:msub><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, before solving the system of equations, as shown in Eqs. (6) and (7):

                <disp-formula specific-use="gather" content-type="numbered"><mml:math id="M54" display="block"><mml:mtable displaystyle="true"><mml:mlabeledtr id="Ch1.E6"><mml:mtd><mml:mtext>6</mml:mtext></mml:mtd><mml:mtd><mml:mrow><mml:mstyle class="stylechange" displaystyle="true"/><mml:msubsup><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mo>′</mml:mo></mml:msubsup><mml:mo>=</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:msub><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mtd></mml:mlabeledtr><mml:mlabeledtr id="Ch1.E7"><mml:mtd><mml:mtext>7</mml:mtext></mml:mtd><mml:mtd><mml:mrow><mml:mstyle class="stylechange" displaystyle="true"/><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula></p>
      <p id="d2e1398">The weight factor expression is <inline-formula><mml:math id="M55" display="inline"><mml:mrow><mml:msub><mml:mi>W</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>⋅</mml:mo><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mrow></mml:math></inline-formula>. Equation (3) is transformed into Eq. (8):

            <disp-formula id="Ch1.E8" content-type="numbered"><label>8</label><mml:math id="M56" display="block"><mml:mrow><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfenced><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:msup><mml:mfenced open="(" close=")"><mml:mrow><mml:mo>-</mml:mo><mml:mi>ln⁡</mml:mi><mml:mfenced close=")" open="("><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfenced></mml:mrow></mml:mfenced><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>K</mml:mi></mml:munderover><mml:msub><mml:mi>a</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>,</mml:mo><mml:mi>k</mml:mi></mml:mrow></mml:msub><mml:msubsup><mml:mi>X</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow><mml:mo>′</mml:mo></mml:msubsup></mml:mrow></mml:math></disp-formula></p>
      <p id="d2e1521">Equation (4) becomes:

            <disp-formula id="Ch1.E9" content-type="numbered"><label>9</label><mml:math id="M57" display="block"><mml:mrow><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>p</mml:mi></mml:munderover><mml:msubsup><mml:mi>W</mml:mi><mml:mi>m</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi>m</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mover accent="true"><mml:mi>y</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>m</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mspace linebreak="nobreak" width="1em"/><mml:mspace linebreak="nobreak" width="0.25em"/><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:mn mathvariant="normal">2</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:mo>,</mml:mo><mml:mi mathvariant="normal">…</mml:mi><mml:mi mathvariant="normal">…</mml:mi><mml:mo>,</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
</sec>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Experimental Design</title>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Experimental Scheme</title>
      <p id="d2e1622">This study optimizes the transmittance coefficient for the HIRAS-II 6.7 <inline-formula><mml:math id="M58" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> water vapor absorption channel (Matricardi and Saunders, 1999; Matricardi, 2007) using two methods: atmospheric profile selection and a weighted least-squares algorithm. We evaluate the forward model by comparing its output with both line-by-line radiative transfer model (LBLRTM) simulations and actual HIRAS-II observations. LBLRTM v12.11 by Atmospheric and Environmental Research, Inc. (AER) is used to compute monochromatic transmittances from 650 to 2600 cm<sup>−1</sup> (3.8 to 15.4 <inline-formula><mml:math id="M60" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>) at a 0.001 cm<sup>−1</sup> spectral resolution for 83 profile training datasets. The calculations cover 101 pressure levels (from 1100 to 0.005 hPa) and six zenith angles, accounting for refractive effects. They include absorption by a uniform mixture of 26 gases (CO<sub>2</sub>, N<sub>2</sub>O, CO, CH<sub>4</sub>, O<sub>2</sub>, NO, SO<sub>2</sub>, NO<sub>2</sub>, NH<sub>3</sub>, HNO<sub>3</sub>, OH, HF, HCl, HBr, HI, ClO, OCS, H<sub>2</sub>CO, HOCl, N<sub>2</sub>, HCN, CH<sub>3</sub>Cl, H<sub>2</sub>O<sub>2</sub>, C<sub>2</sub>H<sub>2</sub>, C<sub>2</sub>H<sub>6</sub>, PH<sub>3</sub>), water vapor (line and continuum), and ozone. These high-resolution transmittances are then convolved with the HIRAS-II spectral response function using Eq. (12) to produce the “true” transmittance values.</p>
      <p id="d2e1834">We calculated fast transmittance coefficients for the HIRAS mid-wave channels within the RTTOV framework using the RTTOV v7 predictors (Saunders et al., 2018). To evaluate the impact of the threshold method and weighted least squares on forward model accuracy, we selected channels representing different atmospheric layers. These include the 6.7 <inline-formula><mml:math id="M80" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak (channel 1372, central wavenumber 1506.875 cm<sup>−1</sup>), mid-level (channel 1239, central wavenumber 1423.75 cm<sup>−1</sup>; channel 1596, central wavenumber 1646.875 cm<sup>−1</sup>) and lower-level (channel 1169, central wavenumber 1380 cm<sup>−1</sup>; channel 1729, central wavenumber 1730 cm<sup>−1</sup>), chosen from the left and right ends of the peak region. These channels were selected to analyze the effects of the threshold method and weighted least squares on forward model accuracy, respectively.</p>
      <p id="d2e1908">We analyze the impact of the threshold and weighted least-squares methods on forward model accuracy according to the experimental design in Table 1. Based on the 1976 U.S. standard atmospheric profile, we employ the RTTOV radiative transfer model to analyze mid-wave spectrum simulations of brightness temperature and calculate the height of the weighting function for selected channels (as shown in Fig. 1). The weighting function is calculated using Eq. (10):

            <disp-formula id="Ch1.E10" content-type="numbered"><label>10</label><mml:math id="M86" display="block"><mml:mrow><mml:mi>W</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi mathvariant="italic">τ</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>ln⁡</mml:mi><mml:mi>P</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula>

          where <inline-formula><mml:math id="M87" display="inline"><mml:mi>W</mml:mi></mml:math></inline-formula> denotes the weighting function, <inline-formula><mml:math id="M88" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula> represents the channel transmittance, and <inline-formula><mml:math id="M89" display="inline"><mml:mi>P</mml:mi></mml:math></inline-formula> indicates atmospheric pressure. This derivative with respect to log-pressure is computed using forward-difference discretization. As shown in Fig. 1, the weighting function peak indicates the atmospheric altitude sensed by the channel.</p>

      <fig id="F1" specific-use="star"><label>Figure 1</label><caption><p id="d2e1959">Distribution of Simulated Brightness Temperature and Weighting Functions for HIRAS-II Channels.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f01.png"/>

        </fig>

      <p id="d2e1968">To comprehensively evaluate the influence of different parameterization strategies on the computational accuracy of fast transmittance and brightness temperature, we have designed four experimental schemes, incorporating the aforementioned typical channels identified through Jacobian weighting-function analysis. Specifically, LSM0 serves as the baseline scheme without any data processing. LSM1 selects a reasonable threshold of <inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:msup><mml:mn mathvariant="normal">10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and applies ordinary least squares (OLS) regression after thresholding. LSM2 adopts the threshold-based method, incorporating weighted least squares (WLS) for the regression. LSM3 applies weighting factors to both the independent variables and the dependent variable, prior to performing the statistical regression. These four schemes are systematically compared to quantitatively assess the impact of the respective parameterization approaches on the simulation accuracy of fast transmittance and brightness temperature.</p>

<table-wrap id="T1"><label>Table 1</label><caption><p id="d2e1988">Summary of methodological specifics for the alternate transmittance algorithms.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="2">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="justify" colwidth="6cm"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Algorithm</oasis:entry>
         <oasis:entry colname="col2">Summary of method</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">LSM0</oasis:entry>
         <oasis:entry colname="col2">The model utilizes an unconstrained ordinary least squares regression on all data points to determine the channel transmittance coefficients.</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">LSM1</oasis:entry>
         <oasis:entry colname="col2">Ordinary least squares is employed to determine the channel transmittance coefficients. A thresholding method is used to select the atmospheric profiles.</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">LSM2</oasis:entry>
         <oasis:entry colname="col2">Channel transmittance coefficients are derived using weighted least squares, with atmospheric profiles selected through a thresholding method.</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">LSM3</oasis:entry>
         <oasis:entry colname="col2">Atmospheric profiles are selected through a thresholding method. Subsequently, weighting factors are applied to the chosen samples, and the channel transmittance coefficients are then derived through ordinary least squares regression.</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Experimental Data</title>
      <p id="d2e2059">This study uses 83 profile training datasets from Matricardi (2008b), which are widely adopted for training fast transmittance coefficients in radiative transfer models, including RTTOV, CRTM, and ARMS. These profiles provide global coverage of temperature, water vapor, and ozone across 101 pressure levels (1100 to 0.005 hPa). They represent a range of atmospheric conditions, including seasonal extremes. Temperature ranges from a minimum of 159.62 K to a maximum of 318.26 K. The spatial distribution of the profiles is shown in Fig. 2a, while the vertical distribution characteristics of temperature and humidity profiles are depicted in Fig. 2b and c, respectively.</p>

      <fig id="F2" specific-use="star"><label>Figure 2</label><caption><p id="d2e2064"><bold>(a)</bold> Geographic locations of the 80 profiles used for coefficient training, which cover diverse surface types, latitudes, and meteorological conditions. <bold>(b)</bold> and <bold>(c)</bold> show the vertical distributions of 83 temperature and humidity profiles.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f02.png"/>

        </fig>

      <p id="d2e2081">The Hyperspectral Infrared Atmospheric Sounder-II (HIRAS-II) has a spectral coverage of 650–2550 cm<sup>−1</sup> (3.8 to 15.4 <inline-formula><mml:math id="M92" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>) using continuous spectral scanning with a spectral resolution of 0.625 cm<sup>−1</sup>. Three bands cover the 15 <inline-formula><mml:math id="M94" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> CO<sub>2</sub> band (LW: 648.75–1169.375 cm<sup>−1</sup>), the 6.7 <inline-formula><mml:math id="M97" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> H<sub>2</sub>O band (MW: 1167.5–1921.25 cm<sup>−1</sup>), and the 4.3 <inline-formula><mml:math id="M100" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> CO<sub>2</sub> band (SW: 1919.375–2551.25 cm<sup>−1</sup>), totaling 3053 channels (<uri>http://www.nsmc.org.cn/nsmc/cn/instrument/HIRAS-2.html</uri>, last access: 15 October 2026). Satellite observation data were obtained from the Fengyun Satellite Remote Sensing Data Service Network (<uri>http://data.nsmc.org.cn/DataPortal/cn/home/index.html</uri>, last access: 15 October 2026). FY-3F HIRAS-II L1 observation data from August 2024 and February 2025 were selected to represent summer and winter, respectively.</p>
</sec>
<sec id="Ch1.S3.SS3">
  <label>3.3</label><title>Data Preprocessing</title>
<sec id="Ch1.S3.SS3.SSS1">
  <label>3.3.1</label><title>Apodization of HIRAS-II data</title>
      <p id="d2e2234">HIRAS-II is a Michelson interferometer that measures interference patterns of incoming radiation. This pattern, recorded in the time domain, is converted into frequency-domain spectra via Fourier transform. Because of the finite maximum optical path difference in the interferometer, the interferogram is truncated at both ends, causing a “sinc” function effect. Therefore, the instrument spectral response function has a “sinc” function shape.</p>
      <p id="d2e2237">In the fast radiative transfer model, channel transmittance is calculated by convolving the high-resolution monochromatic transmittance with the instrumental spectral response function of HIRAS. During the transformation of transmittance from monochromatic light (0.001 cm<sup>−1</sup>) to the instrument spectral resolution (0.625 cm<sup>−1</sup>), direct convolution with the sinc function derived from Fourier theory produces unphysical negative values in the results. To mitigate this issue, particularly the spectral leakage caused by sinc function sidelobes, we apply a Hamming window function (Harris, 1987) tailored to the instrument's specific characteristics. Hence, the instrumental line shape results from applying a cosine Fourier transform to the truncated interferogram. This study uses Eq. (11) to represent the instrumental spectral response function.

              <disp-formula id="Ch1.E11" content-type="numbered"><label>11</label><mml:math id="M105" display="block"><mml:mrow><mml:msub><mml:mi>f</mml:mi><mml:mi mathvariant="normal">Hm</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi>a</mml:mi><mml:mo>(</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">27</mml:mn><mml:mn mathvariant="normal">25</mml:mn></mml:mfrac></mml:mstyle><mml:mo>-</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mn mathvariant="normal">16</mml:mn><mml:mn mathvariant="normal">25</mml:mn></mml:mfrac></mml:mstyle><mml:msup><mml:mi>a</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>)</mml:mo><mml:mi mathvariant="normal">sinc</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">π</mml:mi><mml:mi>a</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:msup><mml:mi>a</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula>

            where <inline-formula><mml:math id="M106" display="inline"><mml:mi mathvariant="italic">ν</mml:mi></mml:math></inline-formula> is the wavenumber, and <inline-formula><mml:math id="M107" display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula> is the maximum optical path difference associated with the interferometric instrument detection.</p>
      <p id="d2e2362">The LBLRTM calculates the monochromatic atmospheric level-to-space transmittance for different gases at a spectral resolution of 0.001 cm<sup>−1</sup>. These high-resolution spectra are then convolved with the spectral response function defined in Eq. (12) to produce the channel-integrated transmittances for the HIRAS-II instrument:

              <disp-formula id="Ch1.E12" content-type="numbered"><label>12</label><mml:math id="M109" display="block"><mml:mrow><mml:mi>R</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>*</mml:mo></mml:msup><mml:mo>,</mml:mo><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:mfenced><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∫</mml:mo><mml:mrow><mml:mo>-</mml:mo><mml:mi mathvariant="normal">∞</mml:mi></mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">∞</mml:mi></mml:mrow></mml:munderover><mml:mi>R</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:mfenced><mml:mo>⋅</mml:mo><mml:mi>f</mml:mi><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>*</mml:mo></mml:msup><mml:mo>-</mml:mo><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi mathvariant="italic">ν</mml:mi></mml:mrow></mml:math></disp-formula>

            where <inline-formula><mml:math id="M110" display="inline"><mml:mi>f</mml:mi></mml:math></inline-formula> is the HIRAS-II spectral response function,<inline-formula><mml:math id="M111" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>*</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> is the channel center wavenumber, <inline-formula><mml:math id="M112" display="inline"><mml:mrow><mml:mi>R</mml:mi><mml:mfenced open="(" close=")"><mml:mrow><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is the level-to-space transmittance or radiance calculated by LBLRTM at 0.001 cm<sup>−1</sup> spectral resolution, and <inline-formula><mml:math id="M114" display="inline"><mml:mrow><mml:mi>R</mml:mi><mml:mfenced close=")" open="("><mml:mrow><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>*</mml:mo></mml:msup><mml:mo>,</mml:mo><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:mfenced></mml:mrow></mml:math></inline-formula> is the transmittance or radiance of the instrument channel. The response function is identical for all channels, with the spectral response shown in Fig. 3.</p>

      <fig id="F3"><label>Figure 3</label><caption><p id="d2e2512">HIRAS Instrument Spectral Response Function (ISRF).</p></caption>
            <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f03.png"/>

          </fig>

      <fig id="F4" specific-use="star"><label>Figure 4</label><caption><p id="d2e2523">Impact of far-wing truncation on simulation accuracy.</p></caption>
            <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f04.png"/>

          </fig>

      <p id="d2e2532">Among the 83 profile training datasets used for transmittance coefficients regression, three specific profiles (81, 82, and 83) represent the minimum, maximum, and mean values of atmospheric variables at each level, respectively. Figure 4 compares the simulated brightness temperature differences among the three profiles under the far-wing truncation ranges relative to the centre wavenumbers of <inline-formula><mml:math id="M115" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>32  and <inline-formula><mml:math id="M116" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>64 cm<sup>−1</sup>, respectively. The results show that, regardless of the far-wing truncation range, the vast majority of channel brightness temperature differences are below 0.03 K, which is smaller than the instrument noise. Therefore, the <inline-formula><mml:math id="M118" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>32 cm<sup>−1</sup> convolution range was selected for HIRAS data processing, as it provides comparable accuracy with lower computational cost.</p>
</sec>
<sec id="Ch1.S3.SS3.SSS2">
  <label>3.3.2</label><title>Selection of HIRAS Clear-Sky Pixels</title>
      <p id="d2e2588">According to Wang et al. (2016), using collocated high-resolution imager cloud products (VIIRS) provides superior clear-sky detection for the CrIS sounder. Building on this finding, our study applies the same principle to develop a clear-sky detection scheme for HIRAS. For each HIRAS field of view (FOV), the algorithm identifies the collocated MERSI pixel, leveraging MERSI's superior spatial resolution. A sampling region centered on this MERSI pixel is then defined, with its spatial extent scaled to match the HIRAS FOV coverage based on their resolution ratio. Cloud mask data are extracted from a 43 <inline-formula><mml:math id="M120" display="inline"><mml:mo>×</mml:mo></mml:math></inline-formula> 43 pixel area within this region. The geometric overlap between the HIRAS FOV and the scaled MERSI sampling area is precisely calculated using the HIRAS field-of-view (FOV) parameters. A HIRAS FOV is classified as clear-sky only if all underlying MERSI cloud mask pixels within the overlapping zone are classified as  clear.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Validation of the Optimized Fast Transmittance Scheme Against LBLRTM Calculations</title>
<sec id="Ch1.S4.SS1">
  <label>4.1</label><title>Impact of the Threshold Method (LSM1) on Simulation Accuracy</title>
      <p id="d2e2615">Based on 83 atmospheric profiles, profiles were selected using both unconstrained and threshold methods to calculate transmittance coefficients. The results were validated against LBLRTM benchmarks. At the left wing of the 6.7 <inline-formula><mml:math id="M121" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption band, features due to SO<sub>2</sub>, N<sub>2</sub>, and CH<sub>4</sub> are present. These gases are all contained within a uniform mixture, which increases the complexity of transmittance calculations. The change in transmittance caused by the threshold method is shown in Fig. 5. Channel No. 1169 (central wavenumber 1380 cm<sup>−1</sup>) lies on the far wing of the 6.7 <inline-formula><mml:math id="M126" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line, representing water vapor absorption in the lower atmosphere, as shown in Fig. 5a. Profile 82 represents the maximum values of all level variables among the set of 83 profile samples. For this profile type, applying the threshold has a negligible effect on fast transmittance calculations. The impact of threshold magnitude is essentially the same as that seen for dry profiles, as shown by Profile 81. As the water vapor content decreases, the impact of the threshold on transmittance calculation accuracy increases, but it is mainly limited to altitudes below 600 hPa, which corresponds roughly to the channel detection height (peak height of the weighting function). Furthermore, the lower the water vapor content, the clearer the improvement in transmittance calculation accuracy. Profile 81 has the lowest variable values among sample profiles, and here the threshold's effect is strongest. Compared with the transmittance deviation calculated without constraints, the fast transmittance calculated using a threshold constraint closely matches that from LBLRTM. In Fig. 5b, channel 1239 (central wavenumber 1423.75 cm<sup>−1</sup>) represents water vapor absorption in the mid-level atmosphere. For profiles with above-average water vapor content (water-rich profiles), forward model accuracy matches that in Fig. 5a. For water-poor profiles below the average, the threshold effect becomes stronger. As water vapor content decreases along the profile, the altitude where threshold-induced transmittance deviation increases gradually rises. For profile 81, the highest altitude where the threshold method improves transmittance deviation does not exceed the channel detection height. In Fig. 5c, channel 1372 (central wavenumber 1506.875 cm<sup>−1</sup>) lies within the 6.7 <inline-formula><mml:math id="M129" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line used to detect upper-level water vapor. The effect of the threshold on forward modeling accuracy is similar to Fig. 5a and b, but its influence is more pronounced.</p>

      <fig id="F5" specific-use="star"><label>Figure 5</label><caption><p id="d2e2714">Comparison of fast transmittance calculated by different schemes for LSM0 (pentagrams) and LSM1 (circles) versus LBLRTM (triangles) transmittance across three channels (1380 cm<sup>−1</sup> <bold>(a)</bold>, 1423.75 cm<sup>−1</sup> <bold>(b)</bold>, 1506.875 cm<sup>−1</sup> <bold>(c)</bold>).</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f05.png"/>

        </fig>

      <p id="d2e2769">Figure 6 presents a comparative analysis of transmittance versus atmospheric pressure for the channel at the right end of the 6.7 <inline-formula><mml:math id="M133" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line. Within this spectral range, only the weak absorption lines of NO<sub>2</sub> and CH<sub>4</sub> lie in the near-wing region of the 6.7 <inline-formula><mml:math id="M136" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line. The transmittances calculated using the threshold method and LBLRTM show nearly identical distributions across atmospheric pressure, consistent with Fig. 5. This suggests that trace gases in either the far-wing or near-wing regions do not affect the accuracy improvement achieved by the threshold method.</p>

      <fig id="F6" specific-use="star"><label>Figure 6</label><caption><p id="d2e2813">Comparison of fast transmittance calculated by different methods (LSM0 indicated by pentagrams, LSM1 by circles) versus LBLRTM (triangles) for the 1646.875  and 1730 cm<sup>−1</sup> channels, showing transmittance variation with pressure.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f06.png"/>

        </fig>

      <p id="d2e2834">For 83 atmospheric profiles, level-to-space atmospheric transmittance was calculated at six satellite zenith angles, producing a total of 498 atmospheric samples. At each isobaric surface, this resulted in a system of 498 linear equations. Analysis indicates that when the cumulative transmittance from a level to the top of the atmosphere is less than 10<sup>−4</sup>, the cumulative transmittance from the level below to the top of the atmosphere may become negative. In consideration of both instrument characteristics and transmittance variation patterns, this study adopts a semi-empirical threshold of 10<sup>−4</sup> as the screening criterion to filter out physically meaningless transmittance. Please see Appendix A (Figs. A1 to A3) for further comparison errors between the LSM series models (LSM1, LSM1.1, LSM1.2) with varying thresholds and the LBLRTM (true value) under typical layer, full atmospheric column, and strong absorption channel conditions, respectively. The 10<sup>−5</sup> threshold suffers severe numerical instability caused by division by small values and yields poor fitting accuracy, whereas switching to 10<sup>−4</sup> substantially reduces calculation bias. Further analysis reveals that an excessively large threshold prematurely discards low-level atmospheric samples and introduces notable errors in transmittance calculation for the middle and lower layers of dry atmospheric profiles; by contrast, the 10<sup>−4</sup> threshold exerts negligible adverse effects on weakly absorbing channels with slowly decaying transmittance. Based on the above physical mechanism analysis and quantitative error evaluation, the present threshold was finalized to balance numerical stability and the integrity of atmospheric profile samples.</p>
      <p id="d2e2897">Figure 7 shows that for each profile, there is an identified position indicating the pressure level above which the profile participates in the training of the corresponding channel, and below which the profile does not participate in the training of the corresponding channel: blue for channel 1169, brown for channel 1239, green for channel 1372, yellow for channel 1596, and red for channel 1729. On the vertical axis, 0 indicates the top of the atmosphere, and 100 indicates the surface. As pressure increases, the number of samples used decreases gradually. Applying the threshold method to filter samples reveals a strong correlation between the number of profiles used in calculations and the absorption characteristics of the channels in these levels. The stronger the absorption, the fewer profiles are included in the training for the middle and lower tropospheric layers. All upper-atmosphere profiles can be retained; however, in the lower atmosphere, retainable samples may drop to fewer than ten. The number of retained samples is higher for channels in absorption line wing regions than for those in peak regions. Moreover, retained sample altitudes are lower for wing-region channels (up to 800 hPa) than peak-region channels (up to 600 hPa). This occurs because, as a channel approaches an absorption line peak region, more samples below its detection altitude have near-zero transmittance and are thus filtered out by thresholding. This can be explained as follows: as the channel moves toward the absorption line peak region, the number of samples with near-zero transmittance below the channel detection altitude gradually increases, which results in more samples being affected by threshold filtering. Additionally, the number of retained samples varies between the left and right ends of the peak region.</p>

      <fig id="F7" specific-use="star"><label>Figure 7</label><caption><p id="d2e2902">Profile positions of different channels and atmospheric layers participating in statistics under a threshold condition of 10<sup>−4</sup>.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f07.png"/>

        </fig>

      <fig id="F8" specific-use="star"><label>Figure 8</label><caption><p id="d2e2925">Variation of the difference between fast transmittance calculated by LSM0 and LSM1 schemes and transmittance calculated by LBLRTM, along with the difference in brightness temperature, across channels.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f08.png"/>

        </fig>

      <p id="d2e2935">In Fig. 8, the surface emissivity for all channels is uniformly set to 0.98 to eliminate its influence on forward modeling results across different schemes. The deviations between the 6.7 <inline-formula><mml:math id="M144" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line spectrum transmittances at the top of the atmosphere calculated by LSM0 and LSM1 for all channels and the LBLRTM results are shown in Fig. 8a and b. In the figure, gray indicates the transmittance deviation of all profiles calculated by LSM0 and LSM1 relative to LBLRTM. The LSM0 forward simulation exhibits positive deviations in the absorption line peak and near-wing regions, while negative deviations occur in the distant wing regions. The deviation distribution of LSM1 is more uniform, though negative deviations increase in the peak region. The standard deviation of LSM1 is significantly reduced from approximately 0.1 K for LSM0 to less than 0.05 K, with a uniform distribution across spectral channels. Unlike LSM0, the standard deviation in the absorption line wings does not exceed that in the peak regions. The deviation distribution shows similar characteristics to the standard deviation. Figure 8c and d show the deviation distributions of brightness temperature in the mid-wave channels for LSM0 and LSM1 forward modeling, respectively. As shown in Fig. 8, for both LSM0 and LSM1 calculations of brightness temperature, the maximum deviation from LBLRTM simulated brightness temperature exceeds 0.5 K across all 83 profiles. Regarding average deviation, LSM1 shows an average value around <inline-formula><mml:math id="M145" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.1 K, which is significantly smaller than the <inline-formula><mml:math id="M146" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.2 K deviation of LSM0. At the left end of the 1350 cm<sup>−1</sup> range, the deviations between the two methods are comparable. In terms of standard deviation and root mean square error distributions, LSM1 also significantly outperforms LSM0. These results collectively demonstrate that the threshold method effectively improves forward model accuracy.</p>
</sec>
<sec id="Ch1.S4.SS2">
  <label>4.2</label><title>Impact of the Threshold and Weight Coefficient Method 1 (LSM2) on Simulation Accuracy</title>
      <p id="d2e2982">In the LSM2 experiments, a weight constraint was additionally applied to the threshold-constrained training profiles, as shown by the right-hand side term in Eq. (6). In Fig. 9, the difference between LSM1 and LSM2 is negligible in the far-wing region to the left of the 6.7 <inline-formula><mml:math id="M148" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line, and their correction effects on transmittance are identical to those shown in Fig. 5a. For the extremely dry atmospheric conditions represented by profile 81, LSM2 shows greater discrepancies from LBL transmittance at lower atmospheric levels and near the channel detection altitude. At 1506.875 cm<sup>−1</sup>, LSM2 exhibits negative deviations relative to LBL results across all altitudes from 300  to 600 hPa, clearly contrasting with thepositive deviations produced by LSM1. Moreover, below 700 hPa, LSM1 maintains a constant transmittance of 0.38, differing significantly from LBL transmittance, which monotonically approaches zero. In this region, LSM2 results better match the actual atmospheric transmittance distribution, indicating that LSM2 significantly improves the forward modeling accuracy of transmittance in the lower atmosphere for the 6.7 <inline-formula><mml:math id="M150" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line peak region channel under extremely dry conditions.</p>
      <p id="d2e3017">Figure 10 shows the transmittance distribution for the right-end channel of the 6.7 <inline-formula><mml:math id="M151" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line. For extremely dry atmospheres, the deviation between LSM2 and LBL remains smaller than that of LSM1 below 250 hPa. Between 300  and 600 hPa, the deviation between LSM2 transmittance and LBL gradually decreases. Below 600 hPa, it essentially overlaps with the LBL transmittance profile, with the largest discrepancy occurring in the low-vapor-content atmosphere of profile 81. The maximum deviation between LSM0/LSM1 and LBL transmittance calculations occurs below 900 hPa, increasing at lower altitudes. However, the difference between LSM2 and LBL remains largely constant with height and is smaller than that of LSM1.</p>

      <fig id="F9" specific-use="star"><label>Figure 9</label><caption><p id="d2e3032">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), and LBLRTM (triangles) across three channels (1380, 1423.75, 1506.875 cm<sup>−1</sup>) versus pressure.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f09.png"/>

        </fig>

      <fig id="F10" specific-use="star"><label>Figure 10</label><caption><p id="d2e3056">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), and LBLRTM (triangles)  across three channels (1646.875, 1730 cm<sup>−1</sup>) versus pressure.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f10.png"/>

        </fig>

      <fig id="F11" specific-use="star"><label>Figure 11</label><caption><p id="d2e3079">Differences in fast transmittance (LSM0/LSM2 vs. LBLRTM) and brightness temperature across all channels.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f11.png"/>

        </fig>

      <p id="d2e3088">The configuration in Fig. 11 is essentially identical to that of Fig. 8, showing the distribution of channel transmittance and simulated brightness temperature deviations for LSM0, LSM2, and LBL across channels at the top of the atmosphere. The transmittance deviation between LSM0 and LBL exceeds 0.2 in most channels, while the brightness temperature bias and standard deviation remain within 1 K. After applying thresholding combined with weighting coefficient correction, the maximum channel transmittance deviation falls below 0.1, as shown in Fig. 11b. The mean and standard deviation of transmittance in mid-wave spectral channels are less than 0.02. As shown in Fig. 11d, the mean and standard deviation of brightness temperature differences are both below 0.2 K. In Fig. 11b, the transmittance deviation distribution of LSM2 at the left end of 1380 cm<sup>−1</sup> is identical to that of LSM1, indicating that weight correction does not significantly improve forward modeling accuracy for overlapping absorption spectra of trace gases and water vapor. In other mid-wave spectral channels, LSM2 shows a marked improvement in forward modeling accuracy compared to LSM0. Furthermore, compared to the forward modeling accuracy of LSM1 in Fig. 8b and d, LSM2 exhibits a more uniform deviation distribution across the mid-wave spectrum, eliminating the large deviations observed in some spectral channels of LSM1.</p>
</sec>
<sec id="Ch1.S4.SS3">
  <label>4.3</label><title>Impact of the Threshold and Weight Coefficient Method 2 (LSM3) on Simulation Accuracy</title>
      <p id="d2e3111">Figure 12 shows the effect of LSM3 on the transmittance profile of the left-end channel of the 6.7 <inline-formula><mml:math id="M155" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak compared with LSM2, LSM1, and LSM0, under the same settings as in Fig. 5. As shown in Fig. 12, the improvement in transmittance by LSM3 remains concentrated in the low-to-mid troposphere with low water vapor content, and the altitude of influence closely correlates with the channel detection altitude. The improvements of LSM3 compared to LSM0 and LSM1 are significant. The transmittance profile calculated by LSM3 almost coincides with that of LSM2. Figure 13 compares transmittance for the right-end channel of the 6.7 <inline-formula><mml:math id="M156" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak, using the same settings as in Fig. 6.</p>

      <fig id="F12" specific-use="star"><label>Figure 12</label><caption><p id="d2e3136">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), LSM3 (diamonds) and LBLRTM (triangles) across three channels (1380, 1423.75, 1506.875 cm<sup>−1</sup>) versus pressure.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f12.png"/>

        </fig>

      <fig id="F13" specific-use="star"><label>Figure 13</label><caption><p id="d2e3159">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), LSM3 (diamonds) and LBLRTM (triangles) across two channels (1646.875, 1730 cm<sup>−1</sup>) versus pressure.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f13.png"/>

        </fig>

      <fig id="F14" specific-use="star"><label>Figure 14</label><caption><p id="d2e3183">Differences in fast transmittance (LSM0/LSM3 vs. LBLRTM) and brightness temperature across all channels.</p></caption>
          <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f14.png"/>

        </fig>

      <p id="d2e3192">Figure 14 shows the statistical deviation of total channel transmittance and brightness temperature for the LSM0 and LSM3 schemes, using the same settings as in Fig. 8. As shown, compared to the transmittance deviation in LSM2 from Fig. 11, the deviation in LSM3 is further reduced. In the brightness temperature deviation statistics in Fig. 8d, the mean RMSE for the mid-wave spectrum (1300–1900 cm<sup>−1</sup>) of LSM1, LSM2, and LSM3 progressively decreases from 0.1  to 0.05  and 0.045 K, respectively, while the mean maximum value decreases from 0.45 to 0.22  and 0.15 K. This indicates that combining the threshold method with weighting coefficients for least-squares solutions can further reduce forward modeling deviations in HIRAS-II mid-wave channels, with the LSM3 scheme producing the smallest error distribution.</p>
</sec>
</sec>
<sec id="Ch1.S5">
  <label>5</label><title>Evaluation of the Optimized Scheme Using FY-3F HIRAS-II Satellite Observations</title>
      <p id="d2e3217">The validation against HIRAS observations has near-global coverage, extending from 60° S to 60° N. We use ERA-5 global profiles of temperature and humidity as the input to RTTOV v13.1. The RTTOV baseline experiment employs the coefficient file rtcoef_fy3_5_hiras2.H5, with predictors from version 7. For surface emissivity, the IREMIS scheme is applied over sea, and the CAMEL climatology atlas scheme over land. The cloud detection scheme from Sect. 3.3.2 is used. The comparison experiment is identical to the baseline in all respects except for the transmittance parameterization schemes. The optimized transmittance coefficients are then used to simulate clear-sky brightness temperatures for the FY-3F HIRAS-II channels at 1380, 1506.875, and 1646.875 cm<sup>−1</sup>. The model simulations are evaluated against clear-sky satellite observations.</p>
      <p id="d2e3232">Figure 15 shows selected channels from HIRAS-II in the far-wing region and at the absorption peak of the 6.7 <inline-formula><mml:math id="M161" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line. Using FY-3F HIRAS-II ascending orbit clear-sky observation data from 1 August  2024, and 1 February  2025, the distribution characteristics of observational simulation deviations for LSM3, RTTOV, and HIRAS-II during summer and winter are analyzed. Among these, the 1380  and 1730 cm<sup>−1</sup> channels are lower-level detection channels located at the far wing of the 6.7 <inline-formula><mml:math id="M163" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption line. The 1423.75  and 1646.875 cm<sup>−1</sup> channels are mid-level detection channels, while 1506.875 cm<sup>−1</sup> is an upper-level detection channel positioned near the absorption line peak. In Fig. 15a, the left column shows the deviation distributions for 1 August (summer), while the right column shows those for 1 February (winter). The first row depicts deviations between observations and RTTOV simulated brightness temperatures; the second row shows deviations between observations and LSM3 results; and the third row illustrates deviations between RTTOV simulated brightness temperatures and LSM3 outputs. The figures show that, for both ocean and land surfaces and in both winter and summer, the deviation distribution trends for LSM3 simulated brightness temperatures are essentially identical to those of RTTOV. The root-mean-square error (RMSE) for both simulated brightness temperatures is about 1 K, with the summer RMSE larger than the winter RMSE. The third row shows that the deviation between LSM3 and RTTOV is near zero, indicating that the LSM3 simulated deviation closely matches that of RTTOV. Figure 15c presents the deviation distribution for the 1646.875 cm<sup>−1</sup> channel, using the same settings as (a). The deviation characteristics of LSM3 versus observations and RTTOV versus observations are similar, and both show larger mean and RMSE than the 1380 cm<sup>−1</sup> channel. Figure 15b shows the 1506.875 cm<sup>−1</sup> channel with the same settings as Fig. 15a. The deviation distributions for LSM3 versus observations and RTTOV versus observations resemble those in Fig. 15a and c. However, when comparing LSM3 with RTTOV simulated brightness temperatures, RTTOV has a larger mean and RMSE than LSM3 in both winter and summer by about 0.1 K. The deviation distributions for the 1423.75  and 1730 cm<sup>−1</sup> channels, located at the right side of the 6.7 <inline-formula><mml:math id="M170" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak, are the same as those for the 1380  and 1646.875 cm<sup>−1</sup> channels. Therefore, analysis is omitted here.</p>

      <fig id="F15" specific-use="star"><label>Figure 15</label><caption><p id="d2e3364">Global distribution of brightness temperature differences between FY-3F HIRAS-II simulated clear-sky data and mid-to-low latitude observations, based on ERA-5 reanalysis data, for the 1380 cm<sup>−1</sup> <bold>(a)</bold>, 1506.875 cm<sup>−1</sup> <bold>(b)</bold>, and 1646.875 cm<sup>−1</sup> <bold>(c)</bold> channels.</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f15.jpg"/>

      </fig>

      <fig id="F16" specific-use="star"><label>Figure 16</label><caption><p id="d2e3422">Long-term bias and RMSE of OMB over time for the LSM0, LSM3, and RTTOV models. (1380 cm<sup>−1</sup> <bold>(a)</bold>, 1506.875 cm<sup>−1</sup> <bold>(b)</bold>, 1646.875 cm<sup>−1</sup> <bold>(c)</bold>).</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f16.png"/>

      </fig>

      <p id="d2e3477">Representative summer observation month is obtained from FY-3F HIRAS-II data in August 2024, while winter month came from observations in February 2025. The daily distribution of deviations between observed and simulated brightness temperatures from the LSM0, LSM3, and RTTOV models is shown in Fig. 16. The channel at 1380 cm<sup>−1</sup> used for long-term time series analysis of observation minus background (OMB) in Fig. 16a is the same as in Fig. 15a. The left column shows summer deviation distributions, while the right column shows winter distributions. The first row shows the long-term mean OMB over time, and the second row shows OMB RMSE variations over time. As shown in Fig. 16, simulation errors for all three forward modeling methods are smaller in winter than in summer. The mean and root mean square errors of the OMB for both LSM3 and RTTOV are essentially the same. For both LSM3 and RTTOV, the <inline-formula><mml:math id="M179" display="inline"><mml:mrow><mml:mo>=</mml:mo><mml:mn mathvariant="normal">33</mml:mn><mml:mo>=</mml:mo><mml:mn mathvariant="normal">33</mml:mn></mml:mrow></mml:math></inline-formula> forward-modeling mean error and RMSE are smaller than those of LSM0. Figure 16b shows results for the strong water vapor absorption line at 1506.875 cm<sup>−1</sup> with settings identical to Fig. 16a. The figure shows that RMSE time evolution curves for LSM3 and RTTOV OMB nearly overlap, but the mean OMB for LSM3 is slightly lower by about 0.1 K, suggesting that LSM3 has a smaller forward-modeling bias than RTTOV near the 6.7 <inline-formula><mml:math id="M181" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak channel. Figure 16c presents data for the 1646.875 cm<sup>−1</sup> channel. RMSE over time for LSM3 and RTTOV OMB remains nearly identical, while both mean OMB and RMSE for LSM0 are significantly larger than those of LSM3 and RTTOV. Deviation distributions at 1423.75 and 1730 cm<sup>−1</sup> in the wing region of the 6.7 <inline-formula><mml:math id="M184" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption peak are consistent with those observed at 1646.875 and 1380 cm<sup>−1</sup>, so they are omitted here.</p>

<table-wrap id="T2" specific-use="star"><label>Table 2</label><caption><p id="d2e3578">Statistical comparison of brightness temperature bias (Mean) and standard deviation (SD) between the RTTOV and LSM3 models at 1506.875 cm<sup>−1</sup> under clear-sky and low-to-mid latitude conditions.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="13">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:colspec colnum="4" colname="col4" align="right" colsep="1"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right"/>
     <oasis:colspec colnum="7" colname="col7" align="right" colsep="1"/>
     <oasis:colspec colnum="8" colname="col8" align="right"/>
     <oasis:colspec colnum="9" colname="col9" align="right"/>
     <oasis:colspec colnum="10" colname="col10" align="right" colsep="1"/>
     <oasis:colspec colnum="11" colname="col11" align="right"/>
     <oasis:colspec colnum="12" colname="col12" align="right"/>
     <oasis:colspec colnum="13" colname="col13" align="right"/>
     <oasis:thead>
       <oasis:row>

         <oasis:entry rowsep="1" colname="col1" morerows="2">clear-sky</oasis:entry>

         <oasis:entry rowsep="1" namest="col2" nameend="col7" align="center" colsep="1">RTTOV </oasis:entry>

         <oasis:entry rowsep="1" namest="col8" nameend="col13" align="center">LSM3 </oasis:entry>

       </oasis:row>
       <oasis:row rowsep="1">

         <oasis:entry namest="col2" nameend="col4" align="center" colsep="1">20240801 </oasis:entry>

         <oasis:entry namest="col5" nameend="col7" align="center" colsep="1">20250201 </oasis:entry>

         <oasis:entry namest="col8" nameend="col10" align="center" colsep="1">20240801 </oasis:entry>

         <oasis:entry namest="col11" nameend="col13" align="center">20250201 </oasis:entry>

       </oasis:row>
       <oasis:row rowsep="1">

         <oasis:entry colname="col2">Mean</oasis:entry>

         <oasis:entry colname="col3">SD</oasis:entry>

         <oasis:entry colname="col4">Count</oasis:entry>

         <oasis:entry colname="col5">Mean</oasis:entry>

         <oasis:entry colname="col6">SD</oasis:entry>

         <oasis:entry colname="col7">Count</oasis:entry>

         <oasis:entry colname="col8">Mean</oasis:entry>

         <oasis:entry colname="col9">SD</oasis:entry>

         <oasis:entry colname="col10">Count</oasis:entry>

         <oasis:entry colname="col11">Mean</oasis:entry>

         <oasis:entry colname="col12">SD</oasis:entry>

         <oasis:entry colname="col13">Count</oasis:entry>

       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>

         <oasis:entry colname="col1">Sea</oasis:entry>

         <oasis:entry colname="col2">0.40</oasis:entry>

         <oasis:entry colname="col3">0.90</oasis:entry>

         <oasis:entry colname="col4">59 252</oasis:entry>

         <oasis:entry colname="col5">0.31</oasis:entry>

         <oasis:entry colname="col6">0.84</oasis:entry>

         <oasis:entry colname="col7">37 766</oasis:entry>

         <oasis:entry colname="col8">0.30</oasis:entry>

         <oasis:entry colname="col9">0.90</oasis:entry>

         <oasis:entry colname="col10">59 252</oasis:entry>

         <oasis:entry colname="col11">0.21</oasis:entry>

         <oasis:entry colname="col12">0.85</oasis:entry>

         <oasis:entry colname="col13">37 766</oasis:entry>

       </oasis:row>
       <oasis:row>

         <oasis:entry colname="col1">Land</oasis:entry>

         <oasis:entry colname="col2">0.40</oasis:entry>

         <oasis:entry colname="col3">1.03</oasis:entry>

         <oasis:entry colname="col4">58 795</oasis:entry>

         <oasis:entry colname="col5">0.30</oasis:entry>

         <oasis:entry colname="col6">0.87</oasis:entry>

         <oasis:entry colname="col7">82 102</oasis:entry>

         <oasis:entry colname="col8">0.31</oasis:entry>

         <oasis:entry colname="col9">1.03</oasis:entry>

         <oasis:entry colname="col10">58 795</oasis:entry>

         <oasis:entry colname="col11">0.22</oasis:entry>

         <oasis:entry colname="col12">0.86</oasis:entry>

         <oasis:entry colname="col13">82 102</oasis:entry>

       </oasis:row>
       <oasis:row>

         <oasis:entry colname="col1">Sea <inline-formula><mml:math id="M187" display="inline"><mml:mo>+</mml:mo></mml:math></inline-formula> Land</oasis:entry>

         <oasis:entry colname="col2">0.40</oasis:entry>

         <oasis:entry colname="col3">0.97</oasis:entry>

         <oasis:entry colname="col4">118 047</oasis:entry>

         <oasis:entry colname="col5">0.30</oasis:entry>

         <oasis:entry colname="col6">0.86</oasis:entry>

         <oasis:entry colname="col7">119 868</oasis:entry>

         <oasis:entry colname="col8">0.31</oasis:entry>

         <oasis:entry colname="col9">0.96</oasis:entry>

         <oasis:entry colname="col10">118 047</oasis:entry>

         <oasis:entry colname="col11">0.22</oasis:entry>

         <oasis:entry colname="col12">0.85</oasis:entry>

         <oasis:entry colname="col13">119 868</oasis:entry>

       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p id="d2e3839">Table 2 presents a quantitative comparison of brightness temperature bias (Mean) and standard deviation (SD) between the RTTOV model and the optimized LSM3 model under clear-sky, low-to-mid latitude conditions at the 1506.875 cm<sup>−1</sup> channel. The comparison is conducted across two observation periods (August 2024 and February 2025) and is stratified by surface type (Sea, Land, and Sea <inline-formula><mml:math id="M189" display="inline"><mml:mo>+</mml:mo></mml:math></inline-formula> Land) based on strict clear-sky screening criteria.</p>
      <p id="d2e3861">By integrating the global distribution patterns presented in Fig. 15 with the quantitative statistical results in Table 2, we conduct a systematic uncertainty source analysis for the OMB bias at the 1506.875 cm<sup>−1</sup> channel: <list list-type="order"><list-item>
      <p id="d2e3878">The radiometric calibration accuracy of the FY-3F HIRAS-II in the mid-wave infrared (1300–1900 cm<sup>−1</sup>) is less than 0.2 K. The statistical results in Table 2 indicate that the overall mean bias of the RTTOV model for both observation periods falls within 0.3–0.4 K. However, with the optimized LSM3 model, the mean bias is effectively reduced to 0.21–0.31 K, approaching the upper limit of the calibration uncertainty. This demonstrates that LSM3 effectively mitigates the systematic bias.</p></list-item><list-item>
      <p id="d2e3894">A significant spatiotemporal difference is evident from Table 2. The bias in August 2024 (summer) is markedly higher than that in February 2025 (winter). For instance, under the combined sea and land condition, the RTTOV bias decreases from 0.40 K (August) to 0.30 K (February). Since the 1506.875 cm<sup>−1</sup> channel is situated within a strong water vapor absorption band, its brightness temperature is highly sensitive to water vapor content. During summer at low-to-mid latitudes, high water vapor content and active thermal convection can amplify the errors in ERA-5 reanalysis temperature and humidity profiles, which are directly reflected as seasonal variations in the OMB bias.</p></list-item><list-item>
      <p id="d2e3910">The comparison of surface types in Table 2 is highly indicative: across nearly all statistical samples, the standard deviation (SD) over land is significantly higher than that over ocean (e.g., for LSM3 in August 2024, the SD is 1.03 over land compared to 0.90 over ocean). This disparity indicates that land surface emissivity (based on the CAMEL climatological dataset) struggles to capture rapid surface changes, such as soil moisture fluctuations, vegetation variations, and snowmelt, whereas sea surface emissivity (based on the IREMIS empirical relationship) remains relatively stable. An emissivity error of 0.01 can introduce brightness temperature deviations of 0.5 K in infrared window channels. However, for absorption channels, the influence of surface emissivity variations is generally much smaller.</p></list-item><list-item>
      <p id="d2e3914">The spatial distribution maps in Fig. 15 exhibit localized scattered bias features. Although a strict MERSI clear-sky detection algorithm (purely clear pixels) was applied in the data pre-processing, thin cirrus clouds or sub-pixel clouds over oceans may still evade detection. Such residual clouds attenuate the upwelling infrared radiation from the surface, resulting in simulated brightness temperatures that are warmer than observations (i.e. a negative OMB bias). This residual cloud contamination can contribute to localized errors on the order of 1 K. Even with the application of this strict clear-sky screening criterion, partial cloud contamination cannot be entirely filtered out. In certain regions, the errors remain affected by residual cloud contamination.</p></list-item></list></p>
      <p id="d2e3918">Based on the clear-sky selection sensitivity tests and quantitative analysis, we confirm that the simulation accuracy improvements are robust and insensitive to the strictness of clear-sky selection. Although relaxing the clear-sky threshold to allow up to 5 % cloudy MERSI pixels leads to slightly larger simulation biases for both schemes, the relative improvement of LSM3 over RTTOV remains unchanged, primarily because the fast transmittance model is tailored for clear-sky, low-to-mid latitude conditions, where stricter cloud-screening consistently yields smaller discrepancies. Synthesizing the above uncertainty analysis, the LSM3 model achieves an improvement of approximately 0.1 K in mean bias compared to the RTTOV model in Table 2, while maintaining a comparable standard deviation (SD), indicating that the LSM3 optimization effectively enhances systematic accuracy without introducing additional numerical noise. Although the OMB statistics remain subject to inherent limitations from ERA5 profile errors, surface emissivity uncertainties, and instrument calibration, the LSM3 model demonstrates robust improvement at the 1506.875 cm<sup>−1</sup> channel. This confirms that its parameterization scheme holds significant application advantages under clear-sky, low-to-mid latitude conditions.</p>
</sec>
<sec id="Ch1.S6">
  <label>6</label><title>Synthesis and Discussion of Forward Model Improvements</title>
      <p id="d2e3941">In the transmittance calculation for infrared atmospheric remote sensing, the presence of negative values in the spectral response function can trigger a series of cascading numerical problems, making their proper handling essential. The spectral response function of hyperspectral infrared sounders (such as HIRAS-II) contains negative values due to the limitations of instrument design and spectral calibration processes. During the convolution process that converts theoretical monochromatic transmittance into instrument-measured transmittance, these negative response values can lead to non-physical negative transmittance, particularly in strong absorption channels.</p>
      <p id="d2e3944">For example, 1506.875 cm<sup>−1</sup> is a strong absorption channel for water vapor. Under conditions of abundant water vapor content, transmittance in this band becomes extremely small in the middle and lower atmosphere. The presence of negative values not only violates the basic physical Beer–Lambert law, which requires transmittance to range between 0 and 1, but also severely distorts the true absorption characteristics of water vapor. Moreover, the handling of small transmittance values in strong absorption channels adds another difficulty. The extremely small transmittance magnitudes (close to 0) in these channels are inherently prone to numerical instability.  When combined with the negative value issues, this instability is significantly amplified, resulting in larger deviations in transmittance calculations. The coexistence of unphysical negative values and the difficulty of handling extremely small quantities significantly increases the challenge of achieving accurate radiative transfer simulations.</p>
      <p id="d2e3959">When a threshold of 10<sup>−4</sup> is applied, the accuracy of fast transmittance coefficient calculations improves significantly for certain layers. However, beyond approximately 70 layers, the layer-by-layer error accumulates, leading to increasing deviations in level-to-space transmittance. Although the threshold partially alleviates the negative value problem, it introduces new challenges. The threshold value represents a cutoff pressure level for water vapor absorption channels. A larger threshold corresponds to a lower pressure at the cutoff level. If no training samples exist below this cutoff, the model implicitly sets the transmittance of all lower layers to 1, causing the level-to-space transmittance to remain constant below that point. As a result, for strong absorption channels, the accuracy for dry profiles in the middle and lower troposphere is significantly degraded. In contrast, for weak absorption channels, the transmittance decreases more slowly, and the cumulative transmittance near the surface remains relatively large, making the impact of the threshold much smaller.</p>
      <p id="d2e3974">Therefore, LSM1 adopts a semi-empirical threshold of 10<sup>−4</sup> for filtering the statistical regression samples. However, because the lower atmospheric layers contribute relatively little to the total absorption, it is unnecessary to rely solely on rigid threshold-based exclusion. Instead, lowering the threshold and introducing a weighting scheme can reduce the influence of the lowest layers without depending exclusively on the threshold, as implemented in LSM2 and LSM3.</p>
      <p id="d2e3990">This study optimizes the transmittance coefficient solution for the 6.7 <inline-formula><mml:math id="M197" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> absorption channel of HIRAS-II using two approaches: (1) threshold-based sub-selection of training samples, and (2) weighting in the least-squares solution. Comparisons with line-by-line (LBL) calculations and HIRAS-II observations lead to the following conclusions:</p>
      <p id="d2e4003">First, introducing threshold-based sample selection significantly improves the accuracy of LSM1 in the upper and middle atmosphere for the 6.7 <inline-formula><mml:math id="M198" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> channel, covering both the absorption peak and wing regions. This improvement is robust across both water-poor and water-rich atmospheric conditions. The threshold effectively removes abnormal profiles that tend to produce unphysical negative values, ensuring that the training dataset better matches the actual atmospheric characteristics observed by HIRAS-II. Quantitative comparisons with LBL show that the RMSE of LSM1 is reduced relative to the unfiltered model (LSM0), confirming the effectiveness of the sample selection strategy.</p>
      <p id="d2e4016">Second, incorporating weighting corrections into the least-squares solutions produces a further stepwise improvement beyond LSM1. Compared with the unweighted models (LSM0 and LSM1), the weighted models (LSM2 and LSM3) achieve higher simulation accuracy in both transmittance and brightness temperature calculations. LSM3 outperforms LSM2. The proposed weighting scheme is physically meaningful: in strong absorption regions where transmittance is very small, it increases the weight of samples with larger transmittance, suppressing numerical fluctuations; in weaker absorption regions (line wings), it maintains balanced weights to preserve adaptability. As a result, LSM3 shows reduced bias and RMSE in brightness temperature at the absorption peak, demonstrating that weighting effectively compensates for the limitations of unweighted least squares methods in handling small transmittance values.</p>
      <p id="d2e4019">Third, validation against actual HIRAS-II observations confirms the practical application value of LSM3. In the wing region of the 6.7 <inline-formula><mml:math id="M199" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> channel, LSM3's deviations (both brightness temperature and transmittance) closely match those of RTTOV, with brightness temperature differences below 0.1 K and transmittance differences near zero. More importantly, in the absorption peak region, LSM3 significantly outperforms RTTOV, demonstrating its ability to simultaneously address negative-value interference and small-value instability. Long-term validation further shows that LSM3 maintains stable performance across different times and locations.</p>
      <p id="d2e4032">In summary, introducing thresholds and weighting strategies substantially improves the accuracy of transmittance coefficient calculations for the 6.7 <inline-formula><mml:math id="M200" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> HIRAS-II channel. The proposed scheme clarifies the mechanisms by which sample selection and weighting influence accuracy and provides a reference for addressing negative-value and small-value issues in other instruments and spectral bands. From an application perspective, the optimized model (LSM3) facilitates enhanced data assimilation for the FY-3 HIRAS series. Beyond HIRAS-II aboard FY-3F, this optimization method is also directly applicable to fast transmittance calculations for other trace gas absorption bands (e.g., CO<sub>2</sub>, O<sub>3</sub>) and to other platforms such as FY-3D and FY-3E, providing robust support for future atmospheric constituent retrieval applications.</p>
      <p id="d2e4063">Artificial intelligence (AI) approaches are increasingly being explored in fast radiative-transfer and gas-absorption calculations. The physical threshold screening and adaptive weighted regression strategies established in this study can be seamlessly combined with machine learning algorithms. On the one hand, the optimized sample screening scheme can supply high-quality, low-noise training datasets for AI-driven radiative transfer models, effectively preventing numerical instabilities induced by samples with ultra-low transmittance. On the other hand, the weighting optimization mechanism can be embedded into the loss function of AI models to improve the fitting accuracy for strong water vapor absorption channels. We regard this as a promising direction for our subsequent research.</p>
</sec>

      
      </body>
    <back><app-group>

<app id="App1.Ch1.S1">
  <label>Appendix A</label><title/>
      <p id="d2e4076">Figures A1 through A3 in Appendix A present the error comparisons between the LSM series models (LSM1, LSM1.1, LSM1.2) with varying thresholds and the line-by-line model (true value) under typical layer, full atmospheric column, and strong absorption channel conditions, respectively. In the figures, the subplots are arranged as follows: the left panel corresponds to the LSM1 model with a threshold of 10<sup>−4</sup>, the middle panel corresponds to the LSM1.1 model with a threshold of 5<inline-formula><mml:math id="M204" display="inline"><mml:mo>×</mml:mo></mml:math></inline-formula>10<sup>−5</sup>, and the right panel corresponds to the LSM1.2 model with a threshold of 10<sup>−5</sup>. Specifically, Figure A1 compares the spectral transmittance at the typical layer (atmospheric layer 56); Fig. A2 illustrates the vertical profiles of level-to-space transmittance across the full atmospheric column; and Fig. A3 provides statistical errors for transmittance and brightness temperature difference (K) over the strong absorption channel range of 1300–1900 cm<sup>−1</sup>.</p>

      <fig id="FA1"><label>Figure A1</label><caption><p id="d2e4136">Comparison of transmittance calculations for channel 1372, wavenumber 1506.875 cm<sup>−1</sup>, and atmospheric layer 56. The <inline-formula><mml:math id="M209" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis represents the profile sample index (0–500), and the <inline-formula><mml:math id="M210" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula>-axis represents the transmittance. The three subplots compare the baseline models RTTOV (red line) and LBL (black line) with the proposed variants of the LSM series (blue line): LSM1 with a threshold of <inline-formula><mml:math id="M211" display="inline"><mml:mrow><mml:msup><mml:mn mathvariant="normal">10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> (left), LSM1.1 with a threshold of <inline-formula><mml:math id="M212" display="inline"><mml:mrow><mml:mn mathvariant="normal">5</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn mathvariant="normal">10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> (middle), and LSM1.2 with a threshold of <inline-formula><mml:math id="M213" display="inline"><mml:mrow><mml:msup><mml:mn mathvariant="normal">10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> (right).</p></caption>
        
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f17.png"/>

      </fig>

      <fig id="FA2"><label>Figure A2</label><caption><p id="d2e4222">Comparison of the vertical profile of level-to-space transmittance for channel 1372 and wavenumber 1506.875 cm<sup>−1</sup>. The lower <inline-formula><mml:math id="M215" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis represents the atmospheric level index (Numlevel, with 0 indicating the top of the atmosphere and 100 indicating the surface), while the upper <inline-formula><mml:math id="M216" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis displays the corresponding pressure (hPa). The vermilion, black, and blue curve groups represent three distinct atmospheric optical paths (labeled 81, 82, and 83, respectively), illustrating the attenuation of transmittance as pressure increases (descending through the atmosphere). </p></caption>
        
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f18.png"/>

      </fig>

<fig id="FA3" specific-use="star"><label>Figure A3</label><caption><p id="d2e4263">Statistical error comparisons between the LSM series models (LSM1, LSM1.1, LSM1.2) and the LBL line-by-line benchmark model within the 1300–1900 cm<sup>−1</sup> wavenumber range. The <inline-formula><mml:math id="M218" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis represents the wavenumber (cm<sup>−1</sup>) for all subplots. The left column displays the statistical errors of transmittance calculations, where the red line denotes Bias, the blue line denotes Standard Deviation (SD). The gray scattered background shows the range. The right column presents the statistical characteristics of the differences in brightness temperature, including MAX (red), MEAN (black), SD (blue), and RMSE (yellow).</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f19.png"/>

      </fig>

      <fig id="FA4" specific-use="star"><label>Figure A4</label><caption><p id="d2e4305">Comparison of fast transmittance calculated by different schemes for LSM0 (pentagrams) and LSM1 (circles) versus LBLRTM (triangles) transmittance across three channels (1380 cm<sup>−1</sup> <bold>(a)</bold>, 1423.75 cm<sup>−1</sup> <bold>(b)</bold>, 1506.875 cm<sup>−1</sup> <bold>(c)</bold>).</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f20.png"/>

      </fig>

<fig id="FA5" specific-use="star"><label>Figure A5</label><caption><p id="d2e4363">Comparison of fast transmittance calculated by different methods (LSM0 indicated by pentagrams, LSM1 by circles) versus LBLRTM (triangles) for the 1646.875  and 1730 cm<sup>−1</sup> channels, showing transmittance variation with pressure.</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f21.png"/>

      </fig>

      <fig id="FA6" specific-use="star"><label>Figure A6</label><caption><p id="d2e4386">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), and LBLRTM (triangles) across three channels (1380, 1423.75, 1506.875 cm<sup>−1</sup>) versus pressure.</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f22.png"/>

      </fig>

<fig id="FA7" specific-use="star"><label>Figure A7</label><caption><p id="d2e4411">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), and LBLRTM (triangles)  across three channels (1646.875, 1730 cm<sup>−1</sup>) versus pressure.</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f23.png"/>

      </fig>

      <fig id="FA8" specific-use="star"><label>Figure A8</label><caption><p id="d2e4434">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), LSM3 (diamonds) and LBLRTM (triangles) across three channels (1380, 1423.75, 1506.875 cm<sup>−1</sup>) versus pressure.</p></caption>
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f24.png"/>

      </fig>

<fig id="FA9"><label>Figure A9</label><caption><p id="d2e4458">Comparison of fast transmittance calculated by LSM0 (pentagrams), LSM1 (circles), LSM2 (crosses), LSM3 (diamonds) and LBLRTM (triangles) across two channels (1646.875, 1730 cm<sup>−1</sup>) versus pressure.</p></caption>
        
        <graphic xlink:href="https://gmd.copernicus.org/articles/19/10077/2026/gmd-19-10077-2026-f25.png"/>

      </fig>

</app>
  </app-group><notes notes-type="codedataavailability"><title>Code and data availability</title>

      <p id="d2e4485">The source code for the rapid transmittance algorithm, along with the processed atmospheric profile datasets used for testing and validation in this study, is publicly available on Zenodo (<ext-link xlink:href="https://doi.org/10.5281/zenodo.18263685" ext-link-type="DOI">10.5281/zenodo.18263685</ext-link>, Zhang, 2025).</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d2e4494">PXZ conducted the methodological research, performed the experiments, developed the model code and implemented the simulations, and drafted the initial manuscript. PZ conceived and defined the overall research goals, designed the experiments, and revised and polished the manuscript. GM co-designed the experiments, supervised and guided the experimental implementation, verified the rationality of the simulation results, and revised and polished the manuscript. RL reviewed the manuscript and provided critical comments and experimental suggestions. LL assisted PXZ in understanding the instrument principles and designing the spectral response functions. WB assisted PXZ in verifying the rationality of the line-by-line integration simulation results. CQ assisted PXZ in learning the construction of the HIRAS clear-sky detection methods.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d2e4500">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="d2e4508">Publisher's note: Copernicus Publications remains neutral with regard to jurisdictional claims made in the text, published maps, institutional affiliations, or any other geographical representation in this paper. The authors bear the ultimate responsibility for providing appropriate place names. Views expressed in the text are those of the authors and do not necessarily reflect the views of the publisher.</p>
  </notes><ack><title>Acknowledgements</title><p id="d2e4515">We acknowledge Atmospheric and Environmental Research, Inc. (AER) for providing LBLRTM v12.11 (license: <uri>https://github.com/AER-RC/LBLRTM/blob/master/LICENSE.md</uri>, last access: 15 October 2026), which served as the reference for transmittance validation in this study. We also extend our thanks to the NWP SAF and the RTTOV development team for making the RTTOV model available (<uri>https://www.nwpsaf.eu/site/software/rttov/</uri>, last access: 15 October 2026), which was instrumental in validating the fast transmittance algorithm presented here.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d2e4526">This work was supported by the National Natural Science Foundation of China (grant nos. U2442214 and 42475170).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d2e4532">This paper was edited by Graham Mann and reviewed by two anonymous referees.</p>
  </notes><ref-list>
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