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  <front>
    <journal-meta><journal-id journal-id-type="publisher">AMT</journal-id><journal-title-group>
    <journal-title>Atmospheric Measurement Techniques</journal-title>
    <abbrev-journal-title abbrev-type="publisher">AMT</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Atmos. Meas. Tech.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">1867-8548</issn><publisher>
    <publisher-name>Copernicus Publications</publisher-name>
    <publisher-loc>Göttingen, Germany</publisher-loc>
  </publisher></journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.5194/amt-14-4157-2021</article-id><title-group><article-title>Improved method of estimating temperatures<?xmltex \hack{\break}?> at meteor peak heights</article-title><alt-title>Temperature at meteor peak heights</alt-title>
      </title-group><?xmltex \runningtitle{Temperature at meteor peak heights}?><?xmltex \runningauthor{E. Sarkar et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1 aff2">
          <name><surname>Sarkar</surname><given-names>Emranul</given-names></name>
          <email>emranul.sarkar@oulu.fi</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Kozlovsky</surname><given-names>Alexander</given-names></name>
          
        <ext-link>https://orcid.org/0000-0003-1468-7600</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Ulich</surname><given-names>Thomas</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-8217-022X</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Virtanen</surname><given-names>Ilkka</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-7111-8888</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff3">
          <name><surname>Lester</surname><given-names>Mark</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff4">
          <name><surname>Kaifler</surname><given-names>Bernd</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-5891-242X</ext-link></contrib>
        <aff id="aff1"><label>1</label><institution>Sodankylä Geophysical Observatory, Sodankylä, Finland</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Space Physics and Astronomy Research Unit, University of Oulu, Oulu, Finland</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>Department of Physics and Astronomy, University of Leicester, Leicester, UK</institution>
        </aff>
        <aff id="aff4"><label>4</label><institution>Deutsches Zentrum für Luft- und Raumfahrt, Institut für Physik der Atmosphäre, Oberpfaffenhofen, Germany</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Emranul Sarkar (emranul.sarkar@oulu.fi)</corresp></author-notes><pub-date><day>7</day><month>June</month><year>2021</year></pub-date>
      
      <volume>14</volume>
      <issue>6</issue>
      <fpage>4157</fpage><lpage>4169</lpage>
      <history>
        <date date-type="received"><day>19</day><month>August</month><year>2020</year></date>
           <date date-type="rev-request"><day>5</day><month>November</month><year>2020</year></date>
           <date date-type="rev-recd"><day>22</day><month>March</month><year>2021</year></date>
           <date date-type="accepted"><day>12</day><month>April</month><year>2021</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2021 Emranul Sarkar et al.</copyright-statement>
        <copyright-year>2021</copyright-year>
      <license license-type="open-access"><license-p>This work is licensed under the Creative Commons Attribution 4.0 International License. To view a copy of this licence, visit <ext-link ext-link-type="uri" xlink:href="https://creativecommons.org/licenses/by/4.0/">https://creativecommons.org/licenses/by/4.0/</ext-link></license-p></license></permissions><self-uri xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021.html">This article is available from https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021.html</self-uri><self-uri xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021.pdf</self-uri>
      <abstract><title>Abstract</title>
    <p id="d1e149">For 2 decades, meteor radars have been routinely used to monitor atmospheric temperature around 90 km altitude. A common method, based on a temperature gradient model, is to use the height dependence of meteor decay time to obtain a height-averaged temperature in the peak meteor region. Traditionally this is done by  fitting a linear regression model in the scattered plot of <inline-formula><mml:math id="M1" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height, where <inline-formula><mml:math id="M2" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula> is the half-amplitude decay time of the received signal. However, this method was found to be consistently biasing the slope estimate. The consequence of such a bias is that it produces a  systematic offset in the estimated temperature, thus requiring calibration with other co-located measurements. The main reason for such a biasing effect is thought to be due to the failure of the classical regression model to take into account the measurement error in <inline-formula><mml:math id="M3" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula> and the observed height. This is further complicated by the presence of various geophysical effects in the data, as well as observational limitation in the measuring instruments. To incorporate various error terms in the statistical model, an appropriate regression analysis for these data is the errors-in-variables model. An initial estimate of the slope parameter is obtained by assuming symmetric error variances in normalised height and <inline-formula><mml:math id="M4" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>. This solution is found to be a good prior estimate for the core of this bivariate distribution. Further improvement is achieved by defining density contours of this bivariate distribution and restricting the data selection process within higher contour levels. With this solution, meteor radar temperatures can be obtained independently without needing any external calibration procedure. When compared with co-located lidar measurements, the systematic offset in the estimated temperature is shown to have reduced to 5 % or better on average.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction and background</title>
      <p id="d1e217">As meteoroids enter the Earth's atmosphere, they produce ionised trails which can be detected as back-scattered radio signals by interferometric radars. After the trail has been formed, the ionisation begins to dissipate by various processes, such as ambipolar diffusion, eddy diffusion, or electron loss due to recombination and attachment depending on the height of ablation.  The rate at which the echo power decreases is also determined by the combined effect of electron line density of the trail, ambient pressure and temperature.</p>
      <?pagebreak page4158?><p id="d1e220">If the electron line density of the trail is less than <inline-formula><mml:math id="M5" display="inline"><mml:mrow><mml:mn mathvariant="normal">2.4</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn mathvariant="normal">10</mml:mn><mml:mn mathvariant="normal">14</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> electrons <inline-formula><mml:math id="M6" display="inline"><mml:mrow class="unit"><mml:msup><mml:mi mathvariant="normal">m</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, the trail is called “underdense”, meaning each electron in the trail scatters independently  <xref ref-type="bibr" rid="bib1.bibx1" id="paren.1"><named-content content-type="pre">e.g.</named-content><named-content content-type="post">p. 356</named-content></xref>. The decay of underdense trails is thought to be mainly due to ambipolar diffusion at a height range of 85–95 km, where the majority of the meteors ablate <xref ref-type="bibr" rid="bib1.bibx18" id="paren.2"/>. In  the weak scattering limit the backscattered amplitude of the radio signal from an underdense trail decays with time (<inline-formula><mml:math id="M7" display="inline"><mml:mi>t</mml:mi></mml:math></inline-formula>) as
          <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M8" display="block"><mml:mrow><mml:mi>A</mml:mi><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi>A</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">16</mml:mn><mml:msup><mml:mi mathvariant="italic">π</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub><mml:mi>t</mml:mi><mml:mo>/</mml:mo><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">r</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M9" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">r</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the radar wavelength, and <inline-formula><mml:math id="M10" display="inline"><mml:mrow><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the ambipolar diffusion coefficient <xref ref-type="bibr" rid="bib1.bibx20" id="paren.3"/>. This coefficient depends on the ambient pressure (<inline-formula><mml:math id="M11" display="inline"><mml:mi>P</mml:mi></mml:math></inline-formula>) and temperature (<inline-formula><mml:math id="M12" display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula>) of the neutral gas <xref ref-type="bibr" rid="bib1.bibx3" id="paren.4"/> and can be estimated from the half-amplitude decay time (<inline-formula><mml:math id="M13" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula>) as
          <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M14" display="block"><mml:mrow><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>K</mml:mi><mml:mi mathvariant="normal">amb</mml:mi></mml:msub><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msup><mml:mi>T</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow><mml:mi>P</mml:mi></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">r</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mi>ln⁡</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:mrow><mml:mrow><mml:mn mathvariant="normal">16</mml:mn><mml:msup><mml:mi mathvariant="italic">π</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mi mathvariant="italic">τ</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
        <inline-formula><mml:math id="M15" display="inline"><mml:mrow><mml:msub><mml:mi>K</mml:mi><mml:mi mathvariant="normal">amb</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) is a constant related to the ionic constituent of the plasma in the trail <xref ref-type="bibr" rid="bib1.bibx11" id="paren.5"/>. The pressure at a given height (<inline-formula><mml:math id="M16" display="inline"><mml:mi>h</mml:mi></mml:math></inline-formula>) is
          <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M17" display="block"><mml:mrow><mml:mi>P</mml:mi><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi>P</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:msubsup><mml:mo>∫</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup><mml:mstyle scriptlevel="+1"><mml:mfrac><mml:mrow><mml:mi>m</mml:mi><mml:mi>g</mml:mi></mml:mrow><mml:mrow><mml:mi>k</mml:mi><mml:mi>T</mml:mi><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mi mathvariant="normal">d</mml:mi><mml:mi>z</mml:mi></mml:mrow></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M18" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula> is the mass of a typical atmospheric molecule, <inline-formula><mml:math id="M19" display="inline"><mml:mi>g</mml:mi></mml:math></inline-formula> is the acceleration of gravity, <inline-formula><mml:math id="M20" display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> is the Boltzmann constant and <inline-formula><mml:math id="M21" display="inline"><mml:mi>z</mml:mi></mml:math></inline-formula> is an axis along the vertical.  Substituting the equation for pressure in Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) and differentiating Eq. (<xref ref-type="disp-formula" rid="Ch1.E4"/>) provides the height profile of the decay time:
          <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M22" display="block"><mml:mrow><?xmltex \hack{\hbox\bgroup\fontsize{9.5}{9.5}\selectfont$\displaystyle}?><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mi>T</mml:mi><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mi>e</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi>m</mml:mi><mml:mi>g</mml:mi></mml:mrow><mml:mi>k</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo movablelimits="false">∫</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mi mathvariant="normal">h</mml:mi></mml:munderover><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mi>T</mml:mi><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mi mathvariant="normal">d</mml:mi><mml:mi>z</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="normal">Ψ</mml:mi><mml:mo>,</mml:mo><?xmltex \hack{$\egroup}?></mml:mrow></mml:math></disp-formula>

          <disp-formula id="Ch1.E5" content-type="numbered"><label>5</label><mml:math id="M23" display="block"><mml:mrow><?xmltex \hack{\hbox\bgroup\fontsize{9.5}{9.5}\selectfont$\displaystyle}?><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi mathvariant="normal">d</mml:mi><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mi>e</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>T</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mi>T</mml:mi><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mi>e</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi>m</mml:mi><mml:mi>g</mml:mi></mml:mrow><mml:mi>k</mml:mi></mml:mfrac></mml:mstyle><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mi>T</mml:mi><mml:mo>(</mml:mo><mml:mi>h</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo><?xmltex \hack{$\egroup}?></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M24" display="inline"><mml:mi mathvariant="normal">Ψ</mml:mi></mml:math></inline-formula> is a constant. Equation (<xref ref-type="disp-formula" rid="Ch1.E5"/>) states that the height profile of decay time is a function of both temperature and temperature gradient under the assumption of ambipolar diffusion for underdense meteor trails. In practice, most trail echoes are received at a small altitude range referred to as the region of peak meteor occurrence <xref ref-type="bibr" rid="bib1.bibx8" id="paren.6"/>. Hence a height-averaged temperature gradient near the peak height can be used to estimate the mean temperature (<inline-formula><mml:math id="M25" display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>) at the peak height by fitting a linear function <xref ref-type="bibr" rid="bib1.bibx8" id="paren.7"/>.  A linear approximation of Eq. (<xref ref-type="disp-formula" rid="Ch1.E5"/>) is
          <disp-formula id="Ch1.E6" content-type="numbered"><label>6</label><mml:math id="M26" display="block"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mo mathsize="1.5em">(</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mo>&lt;</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>T</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>&gt;</mml:mo><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi>m</mml:mi><mml:mi>g</mml:mi></mml:mrow><mml:mi>k</mml:mi></mml:mfrac></mml:mstyle><mml:mo mathsize="1.5em">)</mml:mo><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mi>e</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M27" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> is the slope of the scattered plot of <inline-formula><mml:math id="M28" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height, and <inline-formula><mml:math id="M29" display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is the average temperature of the atmosphere at the height of peak meteor occurrence. A typical scattered plot of height and <inline-formula><mml:math id="M30" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> shows significant variation in the measured data along both abscissa and ordinate (Fig. <xref ref-type="fig" rid="Ch1.F1"/>). Traditionally, the slope (<inline-formula><mml:math id="M31" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>) is estimated using the ordinary least-squares (OLS) method with <inline-formula><mml:math id="M32" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>  as the independent variable. The justification of using <inline-formula><mml:math id="M33" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> as an independent variable is that the measurement errors in  <inline-formula><mml:math id="M34" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula> are smaller than those in heights <xref ref-type="bibr" rid="bib1.bibx11" id="paren.8"/>. While the pulse length and angular resolution, etc. of the radar introduces intrinsic measurement errors in heights, much of the variation in decay time is due to various geophysical effects that persist at all altitudes. At higher altitude, the collision frequency with neutrals is reduced, and the diffusion is inhibited in a direction orthogonal to the geomagnetic field <xref ref-type="bibr" rid="bib1.bibx19 bib1.bibx34" id="paren.9"/>. This anisotropic diffusion causes an increase in the duration of meteor radar echoes as compared to ambipolar diffusion, whereas at lower altitude, decay time tends to decrease due to additional effect of electron loss by recombination and attachment <xref ref-type="bibr" rid="bib1.bibx42" id="paren.10"/>. In addition, other geophysical factors, such as meteor fragmentation, turbulence within trail, chemical composition of the meteors or the temperature variation due to passage of tides and gravity waves, can  contribute to the measurements of  decay time and heights at all altitudes <xref ref-type="bibr" rid="bib1.bibx9" id="paren.11"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><?xmltex \currentcnt{1}?><?xmltex \def\figurename{Figure}?><label>Figure 1</label><caption><p id="d1e971"><bold>(a)</bold> Typical scatter plot of  <inline-formula><mml:math id="M35" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height. The lines correspond to best-fit models using different regression methods described in the text. The green and blue line corresponds to the ordinary least-squares method (OLS), with <inline-formula><mml:math id="M36" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height as independent variables respectively.  The red  line corresponds to the geometric mean (GM) of <inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M38" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>. <bold>(b)</bold> The bivariate distribution of the data. The measured height and <inline-formula><mml:math id="M39" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> are converted to dimension-free coordinates using Eq. (<xref ref-type="disp-formula" rid="Ch1.E18"/>). The relative density contours are obtained by counting the number of detections in a circle of unit area relative to the detection density at the height of peak meteor occurrences at the centre.</p></caption>
        <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f01.png"/>

      </fig>

      <p id="d1e1078">Temperature estimation from meteor radar (MR) data requires obtaining the best-fit regression line in the scattered plot of <inline-formula><mml:math id="M40" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height. However, the pioneer work done by <xref ref-type="bibr" rid="bib1.bibx8" id="text.12"/> to implement this method using ordinary least-squares fitting showed a clear systematic offset between the MR temperature and co-located lidar measurements, indicating that the estimated slope was not determined correctly. To correct for this offset, a common practice is to calibrate the meteor radar temperatures using temperatures from lidar, OH spectrometer, satellite or rocket climatology. <xref ref-type="bibr" rid="bib1.bibx13" id="text.13"/> provided a statistical comparison technique (SCT) to calibrate the biased slope estimate as
          <disp-formula id="Ch1.E7" content-type="numbered"><label>7</label><mml:math id="M41" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mo mathsize="1.5em">(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo mathsize="1.5em">)</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">SCT</mml:mi></mml:msub></mml:mrow></mml:math></disp-formula>
        or
          <disp-formula id="Ch1.E8" content-type="numbered"><label>8</label><mml:math id="M42" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">SCT</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo mathsize="1.5em">(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo mathsize="1.5em">)</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M44" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are the error variances of the (log of) diffusion coefficient (or decay time) and height respectively, <inline-formula><mml:math id="M45" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are data variances of <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and of height respectively and <inline-formula><mml:math id="M48" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M49" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are slope coefficients when diffusion coefficient or height is treated as an independent variable respectively in the OLS regression analysis. The calibrated slope, <inline-formula><mml:math id="M50" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">SCT</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, is traditionally obtained by arbitrarily choosing <inline-formula><mml:math id="M51" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math id="M52" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> that gives the best temperature estimates of MR as compared to optical or satellite data  <xref ref-type="bibr" rid="bib1.bibx16 bib1.bibx15 bib1.bibx23" id="paren.14"><named-content content-type="pre">e.g.</named-content></xref>.  A severe shortcoming of such  a calibration procedure is that the calibration factors (<inline-formula><mml:math id="M53" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) in the parentheses of Eq. (<xref ref-type="disp-formula" rid="Ch1.E7"/>) or Eq. (<xref ref-type="disp-formula" rid="Ch1.E8"/>) are dependent on the data selection criteria (e.g. limiting heights, decay time or zenith angle to a certain range). Moreover, the outcome of any such calibration routine will depend on the location of the MR and the choice of the calibration instrument. From a pure statistical context, the arbitrary choice of calibration  parameters makes the estimated temperature also an arbitrary quantity, thereby making it impossible to draw any reasonable statistical inferences.</p>
      <?pagebreak page4159?><p id="d1e1354">In practice, the ordinary least-squares method will not be valid for MR data since neither the height nor the decay time can be predetermined as an independent variable, and both variables are subject to intrinsic measurement errors and various geophysical effects. The reasons for such a bias, and thus the need for calibration, are discussed on theoretical and experimental grounds in Sect. <xref ref-type="sec" rid="Ch1.S3.SS1"/>. In addition, a statistical procedure to estimate <inline-formula><mml:math id="M55" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M56" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> using SCT calibration is formulated and presented in Sect. <xref ref-type="sec" rid="Ch1.S3.SS1"/>. An alternative method that includes measurement errors in the regression model is introduced in Sect. <xref ref-type="sec" rid="Ch1.S3.SS2"/>. This analysis does not require an absolute knowledge of  <inline-formula><mml:math id="M57" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math id="M58" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, but only the relative value is needed. As an alternative to SCT calibration, in Sect. <xref ref-type="sec" rid="Ch1.S4"/>, an independent slope estimation is obtained using the errors-in-variables model. A comparison study of the estimated MR temperatures with co-located lidar temperatures is discussed to validate the method.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><title>Instrumentation and data</title>
      <p id="d1e1418">The All-Sky Interferometric Meteor Radar (SKiYMET) at Sodankylä Geophysical Observatory (SGO; 67<inline-formula><mml:math id="M59" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>22<inline-formula><mml:math id="M60" display="inline"><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:math></inline-formula> N, 26<inline-formula><mml:math id="M61" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>38<inline-formula><mml:math id="M62" display="inline"><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:math></inline-formula> E; Finland) has been routinely monitoring daily meteor-height averaged temperatures and wind velocity since December 2008 <xref ref-type="bibr" rid="bib1.bibx26" id="paren.15"/>. The radar operates at a transmission power of 15 <inline-formula><mml:math id="M63" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">kW</mml:mi></mml:mrow></mml:math></inline-formula> and frequency of 36.9 <inline-formula><mml:math id="M64" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MHz</mml:mi></mml:mrow></mml:math></inline-formula>, with a transmitting antenna which has a broad radiation pattern designed to illuminate a large expanse of the sky. The meteor trails are detected within a circle of 300 <inline-formula><mml:math id="M65" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> diameter around SGO. The phase differences in the five-antennae receiving array allow for the determination of the azimuth, elevation, range, and line-of-sight Doppler velocity of the meteor trails. The 2144 <inline-formula><mml:math id="M66" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">Hz</mml:mi></mml:mrow></mml:math></inline-formula> pulse repetition frequency of MR transmission introduces a range ambiguity of 70 <inline-formula><mml:math id="M67" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>, and the built-in analysis software therefore assumes meteor trails are within the height of 70 to 110 <inline-formula><mml:math id="M68" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> for unambiguous detections. Uncertainty in the height is <inline-formula><mml:math id="M69" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M70" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> (or better for large zenith angle), which is determined by the 2 <inline-formula><mml:math id="M71" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> range resolution. In addition, the half-time (<inline-formula><mml:math id="M72" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula>) of the received signal is calculated from the width of the autocorrelation function. A detailed description of the algorithm of the SKiYMET signal processing software is outlined in <xref ref-type="bibr" rid="bib1.bibx12" id="text.16"/>.</p>
      <?pagebreak page4160?><p id="d1e1546">SGO is located at the corrected geomagnetic latitude of 64.1<inline-formula><mml:math id="M73" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, which is statistically a region of the auroral oval. Hence the radar frequently detects non-meteor targets during substorms associated with ionospheric plasma waves generated due to Farley–Buneman instability <xref ref-type="bibr" rid="bib1.bibx22" id="paren.17"/>. The Doppler velocity of such echoes can be more than a few hundreds of metres per second, which are mostly detected at low elevation <xref ref-type="bibr" rid="bib1.bibx29" id="paren.18"/>. For the Sodankylä radar,  <xref ref-type="bibr" rid="bib1.bibx25" id="text.19"/> identified  ground echoes modulated by the ionosphere during pulsating auroras. These targets have near-zero Doppler velocities and are also observed at low elevation. Furthermore, the SKiYMET system detects both underdense and overdense echoes as valid meteors. However, more than 95 % of detections are underdense <xref ref-type="bibr" rid="bib1.bibx13" id="paren.20"/>. The percentage of overdense trails may be larger during some meteor trails such as Geminids or Quadrantids, and this leads to underestimation of temperatures <xref ref-type="bibr" rid="bib1.bibx26" id="paren.21"/>. This artefact in temperature was  found to be reduced for Sodankylä radar for a zenith angle of less than 50<inline-formula><mml:math id="M74" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. The initial data selection criteria is kept to a bare minimum, such that all heights and decay times are included, as long as they are unambiguous detections above a 40<inline-formula><mml:math id="M75" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> elevation angle with Doppler radial velocity in the range <inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">100</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M77" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. Subsequently, to improve the temperature estimation, we used a contour selection process; i.e. the data outside a certain contour in the normalised height–<inline-formula><mml:math id="M78" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> distribution were rejected (Fig. <xref ref-type="fig" rid="Ch1.F1"/>b).</p>
      <p id="d1e1638">For temperature estimation we considered daily data for a 6-month period from October 2015 to March 2016 since simultaneous lidar measurements were available during this time. The Compact Rayleigh Autonomous Lidar (CORAL) provided vertical profiles of the atmospheric temperature at 27–98 <inline-formula><mml:math id="M79" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> over Sodankylä as part of the GW-LCYCLE-II (Gravity Wave Life Cycle Experiment) campaign in winter 2015/2016 <xref ref-type="bibr" rid="bib1.bibx32" id="paren.22"/>. The median number of daily meteor detections in this data set is 1652, with a minimum of 410 meteor detections on 4 October 2015 and a maximum of 3456 detections during the Geminids meteor shower on 14 December 2015.</p>
      <p id="d1e1652">The Mass Spectrometer–Incoherent Scatter or MSIS90 <xref ref-type="bibr" rid="bib1.bibx7" id="paren.23"/> model temperatures are used to generate a temperature gradient model near the peak heights. Model temperatures are computed for each date at  intervals of 6 h between 85 and 95 <inline-formula><mml:math id="M80" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>. A third-degree polynomial fit is carried out to obtain the height profiles at 06:00, 12:00, 18:00 and 24:00 UT. For each time interval, the gradient at the respective meteor peak height, as well as at 1 <inline-formula><mml:math id="M81" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> above and below the peak height, is estimated. These 12 values are then used to obtain the mean and standard deviation of the temperature gradient for each day near the peak height, which varies in the range <inline-formula><mml:math id="M82" display="inline"><mml:mrow><mml:mn mathvariant="normal">89</mml:mn><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M83" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>. The daily meteor detections, the peak heights and the corresponding temperature gradient model values are shown in Fig. <xref ref-type="fig" rid="Ch1.F2"/>. The standard deviation of the  MSIS model values corresponds to roughly of the order of 0.7 <inline-formula><mml:math id="M84" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">km</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2" specific-use="star"><?xmltex \currentcnt{2}?><?xmltex \def\figurename{Figure}?><label>Figure 2</label><caption><p id="d1e1717"><bold>(a)</bold> Temperature gradient model derived from MSIS90. <bold>(b)</bold> Peak meteor heights for the data used in this work and <bold>(c)</bold> the daily meteor detection for zenith angle less than 50<inline-formula><mml:math id="M85" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> and velocity  in the range <inline-formula><mml:math id="M86" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">100</mml:mn></mml:mrow></mml:math></inline-formula> m s<inline-formula><mml:math id="M87" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f02.png"/>

      </fig>

      <p id="d1e1765">Our reasons for choosing the MSIS temperature gradient are twofold. Firstly, MSIS data are easily accessible from the online version,  which guarantees reproducibility of this work independent of location. Secondly, even if the temperature gradient term in Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>) is ignored, the resulting offset in the estimated temperature is on average 10 % <xref ref-type="bibr" rid="bib1.bibx8" id="paren.24"/> or less. Hence an approximate estimate is sufficient for the main objective of this paper. However, the actual temperature gradient in the atmosphere may be slightly different from these model values,  which can contribute to the biasing effect in the estimated temperatures. Any such possibility and its effect on the estimated temperatures is addressed in the subsequent section.</p>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Method: regression analysis</title>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Estimation of error variances in decay time and height</title>
      <?pagebreak page4161?><p id="d1e1788">In the following text we use the notation and formulation in <xref ref-type="bibr" rid="bib1.bibx6" id="text.25"/>. The observables, <inline-formula><mml:math id="M88" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height, are represented as <inline-formula><mml:math id="M89" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>  and <inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> respectively and the corresponding unobserved true values as <inline-formula><mml:math id="M91" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M92" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> respectively, where the index <inline-formula><mml:math id="M93" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula> represents the <inline-formula><mml:math id="M94" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>th meteor detection. For consistency we also assume that <inline-formula><mml:math id="M95" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is presented in abscissa, and height is in the ordinate in the respective scattered plot (as shown in Fig. <xref ref-type="fig" rid="Ch1.F1"/>). Suppose we are assuming a linear relation in variables <inline-formula><mml:math id="M96" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M97" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> as
            <disp-formula id="Ch1.E9" content-type="numbered"><label>9</label><mml:math id="M98" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mi>i</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:mi mathvariant="normal">…</mml:mi><mml:mo>,</mml:mo><mml:mi>N</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Due to measurement errors and various geophysical processes, the true values <inline-formula><mml:math id="M99" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M100" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> will be subject to random errors, and hence the observable <inline-formula><mml:math id="M101" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>  and <inline-formula><mml:math id="M102" display="inline"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> will have scatter around the linear model in Eq. (<xref ref-type="disp-formula" rid="Ch1.E9"/>):
            <disp-formula id="Ch1.E10" content-type="numbered"><label>10</label><mml:math id="M103" display="block"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></disp-formula>
          and
            <disp-formula id="Ch1.E11" content-type="numbered"><label>11</label><mml:math id="M104" display="block"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M105" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M106" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are errors in the measured <inline-formula><mml:math id="M107" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height respectively and are assumed to be mutually uncorrelated, have zero mean and be independent of the suffix <inline-formula><mml:math id="M108" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>. This implies that the measurement error variances, <inline-formula><mml:math id="M109" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>  and <inline-formula><mml:math id="M110" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, are constant with respect to the suffix <inline-formula><mml:math id="M111" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>. Classical regression analysis or ordinary least-squares (OLS) treats <inline-formula><mml:math id="M112" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> as an independent variable without intrinsic errors (or, <inline-formula><mml:math id="M113" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) and then minimises the sum of squared residuals along the ordinate. The slope from the OLS method can be represented in terms of the covariance (Cov) and variance (Var)  as <xref ref-type="bibr" rid="bib1.bibx37 bib1.bibx21" id="paren.26"><named-content content-type="pre">e.g.</named-content></xref>
            <disp-formula id="Ch1.E12" content-type="numbered"><label>12</label><mml:math id="M114" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mtext>Cov</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mo>≡</mml:mo><mml:mi>r</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M115" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is the OLS slope estimated by considering <inline-formula><mml:math id="M116" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> as an independent variable, and <inline-formula><mml:math id="M117" display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> is the Pearson product-moment correlation coefficient between <inline-formula><mml:math id="M118" display="inline"><mml:mi>d</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M119" display="inline"><mml:mi>h</mml:mi></mml:math></inline-formula>. Likewise, by reversing the arguments above, it is trivial to show that the reciprocal value of the OLS slope estimate with height as an independent variable is <xref ref-type="bibr" rid="bib1.bibx37" id="paren.27"><named-content content-type="pre">e.g.</named-content></xref>
            <disp-formula id="Ch1.E13" content-type="numbered"><label>13</label><mml:math id="M120" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Cov</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mo>≡</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mi>r</mml:mi></mml:mfrac></mml:mstyle><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          To see the effect of errors in the independent variable on the OLS slope estimate, e.g. for <inline-formula><mml:math id="M121" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, Eqs. (<xref ref-type="disp-formula" rid="Ch1.E10"/>) and (<xref ref-type="disp-formula" rid="Ch1.E11"/>) are used in  Eq. (<xref ref-type="disp-formula" rid="Ch1.E12"/>):
            <disp-formula id="Ch1.E14" content-type="numbered"><label>14</label><mml:math id="M122" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mtext>Cov</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Since <inline-formula><mml:math id="M123" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M124" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M125" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are mutually independent, Eq. (<xref ref-type="disp-formula" rid="Ch1.E14"/>) simplifies to
            <disp-formula id="Ch1.E15" content-type="numbered"><label>15</label><mml:math id="M126" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mtext>Cov</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:mstyle displaystyle="false"><mml:mfrac style="text"><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:mfrac></mml:mstyle><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mi mathvariant="italic">ζ</mml:mi><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mi mathvariant="italic">β</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M127" display="inline"><mml:mi mathvariant="italic">ζ</mml:mi></mml:math></inline-formula> is known as the <italic>attenuation</italic> or <italic>regression dilution</italic> bias. Since variances are always positive by definition, Eq. (<xref ref-type="disp-formula" rid="Ch1.E15"/>) shows that in the presence of measurement error in the so-called independent variable (in abscissa), the OLS slope estimate (<inline-formula><mml:math id="M128" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>) will always be smaller than the unbiased slope <inline-formula><mml:math id="M129" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>. Likewise, <inline-formula><mml:math id="M130" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is greater than <inline-formula><mml:math id="M131" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> if there is error in the measured height (specific example presented in Fig. <xref ref-type="fig" rid="Ch1.F1"/>a). By substituting <inline-formula><mml:math id="M132" display="inline"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, Eq. (<xref ref-type="disp-formula" rid="Ch1.E15"/>) can be rearranged as
            <disp-formula id="Ch1.E16" content-type="numbered"><label>16</label><mml:math id="M133" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mo mathsize="2.5em">(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">δ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo mathsize="2.5em">)</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mi mathvariant="italic">β</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Equation (<xref ref-type="disp-formula" rid="Ch1.E16"/>) is a well known identity in statistical literature <xref ref-type="bibr" rid="bib1.bibx2 bib1.bibx5" id="paren.28"><named-content content-type="pre">e.g.</named-content></xref>, that was re-derived by <xref ref-type="bibr" rid="bib1.bibx13" id="text.29"/> in Eq. (<xref ref-type="disp-formula" rid="Ch1.E7"/>) in the context of SCT correction. Equation (<xref ref-type="disp-formula" rid="Ch1.E16"/>) reveals that an absolute knowledge of error variances, <inline-formula><mml:math id="M134" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> ( or <inline-formula><mml:math id="M135" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>), is required to obtain the bias-corrected slope (<inline-formula><mml:math id="M136" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>) if we choose OLS fitting for the slope estimate. A common practice is to calibrate the biased slope  with optical or satellite data by arbitrarily choosing a value of <inline-formula><mml:math id="M137" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math id="M138" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>  <xref ref-type="bibr" rid="bib1.bibx16 bib1.bibx15 bib1.bibx23" id="paren.30"><named-content content-type="pre">e.g.</named-content></xref>. In the remaining part of this section, we demonstrate how to obtain an average value of the error variances in these data following a revised calibration procedure.</p>
      <p id="d1e2868">For each 24 h of the data set, we performed two OLS fittings to estimate <inline-formula><mml:math id="M139" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M140" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> by using Eqs. (<xref ref-type="disp-formula" rid="Ch1.E12"/>) and (<xref ref-type="disp-formula" rid="Ch1.E13"/>). The corresponding biased temperatures, <inline-formula><mml:math id="M141" display="inline"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M142" display="inline"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> respectively, are estimated using Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>). Experimental values of the parameters <inline-formula><mml:math id="M143" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M144" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> can be obtained by comparing these estimated biased temperatures with the co-located lidar temperatures (<inline-formula><mml:math id="M145" display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) as the reference values. Using Eqs. (<xref ref-type="disp-formula" rid="Ch1.E7"/>) and (<xref ref-type="disp-formula" rid="Ch1.E8"/>), and noting that the slope is proportional to the estimated temperatures from Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>), we obtain
            <disp-formula id="Ch1.E17" content-type="numbered"><label>17</label><mml:math id="M146" display="block"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub><mml:mo>≈</mml:mo><mml:mo mathsize="1.5em">(</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo mathsize="1.5em">)</mml:mo><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mtext>and</mml:mtext><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mspace linebreak="nobreak" width="0.25em"/><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub><mml:mo>≈</mml:mo><mml:mo mathsize="1.5em">(</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo mathsize="1.5em">)</mml:mo><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M147" display="inline"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M148" display="inline"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> are MR temperatures estimated using OLS fitting with <inline-formula><mml:math id="M149" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height as an independent variable respectively. Furthermore, if the measurements are normalised with the mean and standard deviation (SD)  as
            <disp-formula id="Ch1.E18" content-type="numbered"><label>18</label><mml:math id="M150" display="block"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:mtext>mean</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mtext>and</mml:mtext><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mspace linebreak="nobreak" width="0.25em"/><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:mtext>mean</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          then <inline-formula><mml:math id="M151" display="inline"><mml:mrow><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mtext>Var</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>, and the OLS estimate of the ratio of the measurement error variance is (from Eqs. <xref ref-type="disp-formula" rid="Ch1.E17"/> and <xref ref-type="disp-formula" rid="Ch1.E18"/>)
            <disp-formula id="Ch1.E19" content-type="numbered"><label>19</label><mml:math id="M152" display="block"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>≈</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup><mml:mo>-</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">d</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:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msubsup><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where the error variances, <inline-formula><mml:math id="M153" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M154" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, are in the dimension-free system defined by Eq. (<xref ref-type="disp-formula" rid="Ch1.E18"/>). In essence, <inline-formula><mml:math id="M155" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is a measure of all sources of errors in the normalised heights and  decay times that cause the real data to deviate from the idealised physical model of Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>), thereby producing a typical scatter as seen in Fig. <xref ref-type="fig" rid="Ch1.F1"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><?xmltex \currentcnt{3}?><?xmltex \def\figurename{Figure}?><label>Figure 3</label><caption><p id="d1e3402"><bold>(a)</bold> Temperature estimated in OLS method using <inline-formula><mml:math id="M156" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> (green) and height (blue) as an independent variable. Also shown are (red) the temperatures obtained using the geometric mean (GM) fitting and the lidar temperatures (in black). <bold>(b)</bold> The offset between the lidar (<inline-formula><mml:math id="M157" display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">lidar</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) temperatures and the estimated MR temperatures (<inline-formula><mml:math id="M158" display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mi mathvariant="normal">MR</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) using OLS fitting and GM fitting (without contour selection).</p></caption>
          <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f03.png"/>

        </fig>

      <?pagebreak page4162?><p id="d1e3460"><inline-formula><mml:math id="M159" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M160" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M161" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> were estimated by Eqs. (<xref ref-type="disp-formula" rid="Ch1.E17"/>) and (<xref ref-type="disp-formula" rid="Ch1.E19"/>) using 24 h of MR data and co-located lidar temperatures at 88, 89 and 90 <inline-formula><mml:math id="M162" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> for the dates for which lidar data were available. The biasing effect on the OLS estimate of MR temperatures with <inline-formula><mml:math id="M163" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height as an independent variable respectively are presented in Fig. <xref ref-type="fig" rid="Ch1.F3"/> (green and blue lines and histogram). As expected from Eq. (<xref ref-type="disp-formula" rid="Ch1.E7"/>) or Eq. (<xref ref-type="disp-formula" rid="Ch1.E8"/>), a mean offset of <inline-formula><mml:math id="M164" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">75</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M165" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">335</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M166" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> occurs depending on whether  <inline-formula><mml:math id="M167" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> or height respectively is considered as an independent variable. In practice, the magnitude of these biases is related to the total errors in heights and <inline-formula><mml:math id="M168" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> from Eq. (<xref ref-type="disp-formula" rid="Ch1.E17"/>), which was not taken into account by the OLS regression model in Eqs. (<xref ref-type="disp-formula" rid="Ch1.E12"/>) and (<xref ref-type="disp-formula" rid="Ch1.E13"/>). Furthermore, the relative density contour lines for each data point is obtained by counting the number of detections in a circle of unit area in the normalised height–<inline-formula><mml:math id="M169" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> plane relative to the number of detections in unit area at the peak meteor region (Fig. <xref ref-type="fig" rid="Ch1.F1"/>b). In addition, all the error estimates from the SCT method are obtained at contour levels 0, 0.2 and 0.4, and the results are presented in Table <xref ref-type="table" rid="Ch1.T1"/>. Several key features of these data are reflected in Table <xref ref-type="table" rid="Ch1.T1"/>. Despite the data transformation via Eq. (<xref ref-type="disp-formula" rid="Ch1.E18"/>), the average error variances for the height data are more than those for the <inline-formula><mml:math id="M170" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> data in these coordinates. This asymmetry in the error variances implies that the bivariate distribution is slightly skewed away from a perfectly normal distribution along the <inline-formula><mml:math id="M171" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula> direction. However, this effect of asymmetric error variances is less pronounced near the core of this distribution. This implies that the parameter <inline-formula><mml:math id="M172" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is closer to 1 near the core of this distribution and further away from 1 near the tail of the distribution. The data near the outer contour area are subject to larger parameter estimation error due to observational limitation.  For example, the zenith-angle-dependent error in height can easily skew the distribution in this direction. On the other hand, natural geophysical variability in these data contributes significantly at all altitudes. As seen in Table <xref ref-type="table" rid="Ch1.T1"/>, the average error in height for contour levels 0, 0.2 and 0.4 are 5.0, 3.0 and 2.2 km respectively. This error is significantly  higher than what is expected from purely parameter estimation error (for zenith angle less than 50<inline-formula><mml:math id="M173" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, the error in height is 1 km or less), indicating that geophysical variability dominates the total error variance in these data at all altitudes. The average error variances estimated at the contour level 0.2 (Table <xref ref-type="table" rid="Ch1.T1"/>) correlate very well with the values reported in <xref ref-type="bibr" rid="bib1.bibx9" id="text.31"/> and <xref ref-type="bibr" rid="bib1.bibx16" id="text.32"/>.  <xref ref-type="bibr" rid="bib1.bibx9" id="text.33"/> estimated <inline-formula><mml:math id="M174" display="inline"><mml:mo>△</mml:mo></mml:math></inline-formula>(height) <inline-formula><mml:math id="M175" display="inline"><mml:mrow><mml:mo>=</mml:mo><mml:mn mathvariant="normal">3.25</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M176" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> using a numerical model for a pulse length equivalent to 2 <inline-formula><mml:math id="M177" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> and a meteor at an altitude of 90 <inline-formula><mml:math id="M178" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> and zenith angle 50<inline-formula><mml:math id="M179" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. Likewise, their estimation of <inline-formula><mml:math id="M180" display="inline"><mml:mrow><mml:mo>△</mml:mo><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.14</mml:mn></mml:mrow></mml:math></inline-formula> was based on simulation studies for meteors below 95 km and confirmed that “decay times' variability” arise due to 27 % variability in <inline-formula><mml:math id="M181" display="inline"><mml:mrow><mml:msub><mml:mi>K</mml:mi><mml:mi mathvariant="normal">amb</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and 8 %  variability in temperatures over the meteor region.  The argument for choosing 95 <inline-formula><mml:math id="M182" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> as the maximum height is that above this altitude, meteor decay rates are substantially affected by processes other than ambipolar diffusion. <xref ref-type="bibr" rid="bib1.bibx16" id="text.34"><named-content content-type="post">p. 5</named-content></xref> applied similar data rejection criteria and found out that <inline-formula><mml:math id="M183" display="inline"><mml:mrow><mml:mo>△</mml:mo><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.14</mml:mn></mml:mrow></mml:math></inline-formula> is required to calibrate the slope if <inline-formula><mml:math id="M184" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is used as an independent variable in the OLS regression model. Likewise, <xref ref-type="bibr" rid="bib1.bibx40" id="text.35"/> performed the comparison between the parameter estimation error and the geophysical variability for estimating the mean wind field in the middle atmosphere and found that the geophysical variability dominated at all heights.</p>
      <?pagebreak page4163?><p id="d1e3863">It is worth noting that instead of directly using the individual observation between biased MR temperatures and lidar measurements from Eq. (<xref ref-type="disp-formula" rid="Ch1.E17"/>), we have used the statistical mean of differences for calibration. This is because lidar data are not available for all days during the 6 months of data used in this work. Moreover, both MR and lidar data have their own intrinsic errors and technical differences in the observation time and volume of sky. MR temperatures are daily averages over 24 <inline-formula><mml:math id="M185" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">h</mml:mi></mml:mrow></mml:math></inline-formula> of observation, whereas lidar data are just the nightly mean profile. The lidar probes a small volume limited to the diameter of the lidar beam, while the radar illuminates a large part of the sky. For a <italic>single</italic> observation, the lidar may see the phase structure of large-scale gravity waves, while the MR averages over the gravity wave structure due to different spatial resolutions. As a result, the radar averages over gravity waves with horizontal wavelengths smaller than few hundred kilometres. On the other hand, the lidar may resolve these gravity waves if the runtime is shorter than the period of these waves. As gravity wave amplitudes can be up to 10–15 <inline-formula><mml:math id="M186" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> at these altitudes <xref ref-type="bibr" rid="bib1.bibx32" id="paren.36"/>, we cannot expect perfect agreement between radar and lidar temperature due to geophysical variation which shows up differently in the two data sets as a result of the different observational volumes.</p>
      <p id="d1e3890">While such calibration routine may prevent large offsets in the estimated temperatures, the day-to-day variation in these error variances  due to natural geophysical processes will persistently introduce artefacts in the estimated temperatures. Moreover, due to the continually changing atmospheric dynamic, these calibration parameters need to be updated at time intervals. This in turn requires availability of optical or satellite data throughout the year for the given location. In all generality, it is desirable to avoid any kind of calibration process and instead formulate an independent estimate of temperatures using MR data alone. As an alternative to the OLS method, errors-in-variables (EIV) regression analysis provides a way to incorporate the error variances in both height and <inline-formula><mml:math id="M187" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> data, thereby reducing the biasing effect in the estimated slope parameter.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1"><?xmltex \currentcnt{1}?><label>Table 1</label><caption><p id="d1e3917">The average value of the (square root of) error variances in height and <inline-formula><mml:math id="M188" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>; <inline-formula><mml:math id="M189" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M190" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are given along with the average value of <inline-formula><mml:math id="M191" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> from SCT calibration (<inline-formula><mml:math id="M192" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>) at contour levels 0, 0.2 and 0.4 for winter 2015–2016.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="4">
     <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"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Contour:</oasis:entry>
         <oasis:entry colname="col2">0</oasis:entry>
         <oasis:entry colname="col3">0.2</oasis:entry>
         <oasis:entry colname="col4">0.4</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M193" display="inline"><mml:mrow><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">ε</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:mo>/</mml:mo></mml:mrow></mml:math></inline-formula>km</oasis:entry>
         <oasis:entry colname="col2">5.0</oasis:entry>
         <oasis:entry colname="col3">3.0</oasis:entry>
         <oasis:entry colname="col4">2.2</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M194" display="inline"><mml:mrow><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:mo>/</mml:mo></mml:mrow></mml:math></inline-formula>s<inline-formula><mml:math id="M195" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">0.18</oasis:entry>
         <oasis:entry colname="col3">0.14</oasis:entry>
         <oasis:entry colname="col4">0.11</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M196" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>&gt;</mml:mo></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">0.62</oasis:entry>
         <oasis:entry colname="col3">0.44</oasis:entry>
         <oasis:entry colname="col4">0.38</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M197" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>&gt;</mml:mo></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">0.37</oasis:entry>
         <oasis:entry colname="col3">0.31</oasis:entry>
         <oasis:entry colname="col4">0.30</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M198" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:msubsup><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="normal">eff</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi></mml:msubsup><mml:mo>&gt;</mml:mo></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">1.68</oasis:entry>
         <oasis:entry colname="col3">1.43</oasis:entry>
         <oasis:entry colname="col4">1.25</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

<?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Errors-in-variables (EIV) model: GM solution</title>
      <p id="d1e4203">For fitting a straight line model, such as
            <disp-formula id="Ch1.E20" content-type="numbered"><label>20</label><mml:math id="M199" display="block"><mml:mrow><mml:mi>y</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi>a</mml:mi><mml:mo>+</mml:mo><mml:mi>b</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:math></disp-formula>
          to a set of <inline-formula><mml:math id="M200" display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> data points (<inline-formula><mml:math id="M201" display="inline"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M202" display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) measured with errors, the corresponding <inline-formula><mml:math id="M203" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> merit function is <xref ref-type="bibr" rid="bib1.bibx31" id="paren.37"><named-content content-type="post">p. 660</named-content></xref>
            <disp-formula id="Ch1.E21" content-type="numbered"><label>21</label><mml:math id="M204" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:mi>a</mml:mi><mml:mo>-</mml:mo><mml:mi>b</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi>y</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>+</mml:mo><mml:msup><mml:mi>b</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M205" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi>y</mml:mi><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M206" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are the standard deviation of the <inline-formula><mml:math id="M207" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>th data point, and the weighted sum in the denominator of Eq. (<xref ref-type="disp-formula" rid="Ch1.E21"/>) can be interpreted as the weighted error of the  <inline-formula><mml:math id="M208" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>th data point. The regression coefficients, <inline-formula><mml:math id="M209" display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M210" display="inline"><mml:mi>b</mml:mi></mml:math></inline-formula>, can be found by minimising the merit function with respect to these coefficients following any suitable numerical root-finding routine. However, under the assumption of symmetric error variances,  it is possible to derive an analytic solution for the regression coefficients. This solution, when the data are appropriately normalised, leads to a slope estimate which is both scale-invariant and symmetric with respect to the data.</p>
      <?pagebreak page4164?><p id="d1e4418">Application of Eq. (<xref ref-type="disp-formula" rid="Ch1.E21"/>) to physics data requires that all measured variables are dimensionally consistent so that <inline-formula><mml:math id="M211" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> is dimension-free. Moreover, the analysis in this section requires that the measurements are presented  in an appropriate dimension-free system. This facilitates the direct comparison between different parameters, such as the measured variables or the associated error variances. By applying the coordinate transformation introduced in Eqs. (<xref ref-type="disp-formula" rid="Ch1.E18"/>) to (<xref ref-type="disp-formula" rid="Ch1.E9"/>), we therefore intend to solve the simplified bivariate linear system of equations,
            <disp-formula id="Ch1.E22" content-type="numbered"><label>22</label><mml:math id="M212" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>=</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mspace linebreak="nobreak" width="0.33em"/><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mo>≡</mml:mo><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mspace width="0.33em" linebreak="nobreak"/><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M213" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">η</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M214" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ξ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M215" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are dimension-free. For the specific choice of normalisation by Eq. (<xref ref-type="disp-formula" rid="Ch1.E18"/>), the intercept (<inline-formula><mml:math id="M216" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) is always zero in the transformed coordinate system. The merit function in Eq. (<xref ref-type="disp-formula" rid="Ch1.E21"/>) can be further simplified by invoking a homoscedastic standard weighting model  <xref ref-type="bibr" rid="bib1.bibx30" id="paren.38"/>. This error model assumes that the error variances are independent of data point, thereby simplifying the merit function as <xref ref-type="bibr" rid="bib1.bibx30 bib1.bibx28" id="paren.39"/>
            <disp-formula id="Ch1.E23" content-type="numbered"><label>23</label><mml:math id="M217" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi mathvariant="italic">α</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo><mml:mo>≡</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>(</mml:mo><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M218" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M219" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are <italic>constant</italic> error variances of the measured <inline-formula><mml:math id="M220" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and heights respectively in the normalised (or, dimension-free) coordinate system, and <inline-formula><mml:math id="M221" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> is the ratio
            <disp-formula id="Ch1.E24" content-type="numbered"><label>24</label><mml:math id="M222" display="block"><mml:mrow><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          The <inline-formula><mml:math id="M223" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> minimisation of Eq. (<xref ref-type="disp-formula" rid="Ch1.E23"/>) with respect to <inline-formula><mml:math id="M224" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> leads to the analytic expression <xref ref-type="bibr" rid="bib1.bibx2 bib1.bibx37 bib1.bibx28" id="paren.40"/> for the EIV slope parameter in terms of the variances (<inline-formula><mml:math id="M225" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math id="M226" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) and covariances (<inline-formula><mml:math id="M227" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) of the measured variables,
            <disp-formula id="Ch1.E25" content-type="numbered"><label>25</label><mml:math id="M228" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:mi mathvariant="italic">λ</mml:mi><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msqrt><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:mi mathvariant="italic">λ</mml:mi><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mi mathvariant="italic">λ</mml:mi><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:msup><mml:mi mathvariant="normal">h</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:mo>′</mml:mo></mml:msup></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msqrt></mml:mrow><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula>
          or
            <disp-formula id="Ch1.E26" content-type="numbered"><label>26</label><mml:math id="M229" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mo>≡</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>+</mml:mo><mml:msqrt><mml:mrow><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>-</mml:mo><mml:mi mathvariant="italic">λ</mml:mi><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mi mathvariant="italic">λ</mml:mi><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:msup><mml:mi mathvariant="normal">h</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:mo>′</mml:mo></mml:msup></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msqrt></mml:mrow><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          since <inline-formula><mml:math id="M230" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> from Eq. (<xref ref-type="disp-formula" rid="Ch1.E18"/>). And the covariance (<inline-formula><mml:math id="M231" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) is computed using the standard definition,
            <disp-formula id="Ch1.E27" content-type="numbered"><label>27</label><mml:math id="M232" display="block"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="normal">h</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mi mathvariant="normal">d</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mi>N</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>)</mml:mo><mml:mo>,</mml:mo><mml:mspace linebreak="nobreak" width="0.33em"/><mml:mtext>for</mml:mtext><mml:mspace width="0.25em" linebreak="nobreak"/><mml:mtext>large</mml:mtext><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mi>N</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Equation (<xref ref-type="disp-formula" rid="Ch1.E26"/>) can be solved if a prior knowledge of <inline-formula><mml:math id="M233" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> is available, which in turn requires a precise estimate of all sources of errors in the measured data. In the more practical case for unknown <inline-formula><mml:math id="M234" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula>, we need to initiate a good starting estimate. Using the calibration procedure described by Eqs. (<xref ref-type="disp-formula" rid="Ch1.E17"/>) and (<xref ref-type="disp-formula" rid="Ch1.E18"/>), the mean values of  <inline-formula><mml:math id="M235" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M236" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are found to be <inline-formula><mml:math id="M237" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.62</mml:mn><mml:mo>±</mml:mo><mml:mn mathvariant="normal">0.04</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M238" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.37</mml:mn><mml:mo>±</mml:mo><mml:mn mathvariant="normal">0.06</mml:mn></mml:mrow></mml:math></inline-formula> respectively (without any contour selection: Table <xref ref-type="table" rid="Ch1.T1"/>). Since the EIV estimate of the slope requires only the ratio between <inline-formula><mml:math id="M239" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M240" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, a good choice of this starting value is <inline-formula><mml:math id="M241" display="inline"><mml:mrow><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>. Furthermore, for <inline-formula><mml:math id="M242" display="inline"><mml:mrow><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>, there is a simple geometric interpretation of the merit function in Eq. (<xref ref-type="disp-formula" rid="Ch1.E23"/>). This  solution corresponds to minimising the Euclidean or orthogonal distance between the fitted line and the measured data. The residual function to be minimised with respect to the regression coefficients is
            <disp-formula id="Ch1.E28" content-type="numbered"><label>28</label><mml:math id="M243" display="block"><mml:mrow><mml:msup><mml:mi mathvariant="italic">χ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>≡</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:mo>-</mml:mo><mml:msub><mml:mi>d</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle></mml:mrow></mml:math></disp-formula>
          since <inline-formula><mml:math id="M244" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">W</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> when <inline-formula><mml:math id="M245" display="inline"><mml:mrow><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> from Eq. (<xref ref-type="disp-formula" rid="Ch1.E26"/>). Following Eq. (<xref ref-type="disp-formula" rid="Ch1.E22"/>), we therefore have our <italic>first estimate</italic> of <inline-formula><mml:math id="M246" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> in the scattered plot of <inline-formula><mml:math id="M247" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and heights,
            <disp-formula id="Ch1.E29" content-type="numbered"><label>29</label><mml:math id="M248" display="block"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          Equation (<xref ref-type="disp-formula" rid="Ch1.E29"/>) is commonly referred to as a reduced major axis (RMA)  solution in statistics literature <xref ref-type="bibr" rid="bib1.bibx37" id="paren.41"/>. In practice, this is just the geometric mean (GM) of the two OLS estimates, <inline-formula><mml:math id="M249" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M250" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>, as can be seen by combining Eqs. (<xref ref-type="disp-formula" rid="Ch1.E12"/>) and (<xref ref-type="disp-formula" rid="Ch1.E13"/>):
            <disp-formula id="Ch1.E30" content-type="numbered"><label>30</label><mml:math id="M251" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">GM</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup><mml:mspace width="0.33em" linebreak="nobreak"/><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msubsup></mml:mrow></mml:msqrt><mml:mo>≡</mml:mo><mml:mspace width="0.33em" linebreak="nobreak"/><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">h</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msub></mml:mrow></mml:msqrt></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          The GM solution in Eq. (<xref ref-type="disp-formula" rid="Ch1.E30"/>) has the unique feature that this is the only case of EIV estimate which is both scale-invariant and symmetric in the variables <xref ref-type="bibr" rid="bib1.bibx33 bib1.bibx37" id="paren.42"><named-content content-type="pre">e.g.</named-content></xref>.  While these properties do not necessarily imply that the GM solution is the correct solution (discussed below), this first estimate reflects the nature of the biasing effect in the estimated slope in relation to the data selection process. A specific example of GM fitting is presented in Fig. <xref ref-type="fig" rid="Ch1.F1"/>a. The standard error in the OLS and GM slope estimate reported in Fig. <xref ref-type="fig" rid="Ch1.F1"/>a is from <xref ref-type="bibr" rid="bib1.bibx41" id="text.43"/>. Due to the relatively low detections with Sodankylä radar (Fig. <xref ref-type="fig" rid="Ch1.F2"/>c), the 2<inline-formula><mml:math id="M252" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> error in the estimated temperature using the GM solution is found to be significantly higher (13 <inline-formula><mml:math id="M253" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> on average at contour level 0). This 13 <inline-formula><mml:math id="M254" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> of noise level in the temperature can be reduced by a factor of <inline-formula><mml:math id="M255" display="inline"><mml:msqrt><mml:mn mathvariant="normal">3</mml:mn></mml:msqrt></mml:math></inline-formula> or <inline-formula><mml:math id="M256" display="inline"><mml:msqrt><mml:mn mathvariant="normal">5</mml:mn></mml:msqrt></mml:math></inline-formula> if a 3 or 5 d running mean of temperature is estimated with this radar. However, to test the robustness of the proposed method, this paper has estimated the daily averaged temperatures.</p>
      <p id="d1e5711">The systematic offset between MR temperature and co-located lidar temperature as a result of using Eq. (<xref ref-type="disp-formula" rid="Ch1.E30"/>) is reflected in Fig. <xref ref-type="fig" rid="Ch1.F3"/>a (red curve) and b (red histogram). Each of these temperatures are then compared with lidar temperatures at 88, 89 and 90 <inline-formula><mml:math id="M257" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> for the dates when lidar data are available. The intrinsic noise in the lidar temperature is about 5–10 <inline-formula><mml:math id="M258" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx32" id="paren.44"/>, which implies no temperature gradient is observed between  88 and 91 <inline-formula><mml:math id="M259" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> in these data.  Figure <xref ref-type="fig" rid="Ch1.F3"/>b (red histogram) reveals that the MR temperatures are overestimated by a mean value of <inline-formula><mml:math id="M260" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">58</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M261" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> for the case of the GM solution.</p>
      <p id="d1e5766">When compared to the temperature gradient model derived from optical, satellite and rocket climatology <xref ref-type="bibr" rid="bib1.bibx16" id="paren.45"><named-content content-type="pre">e.g.</named-content></xref>, it can be easily argued that our MSIS-derived gradient model (Fig. <xref ref-type="fig" rid="Ch1.F2"/>a) is more negative than expected. If these values are shifted by a constant positive offset of <inline-formula><mml:math id="M262" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M263" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">km</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, the absolute value of the estimated temperatures will increase by 10 <inline-formula><mml:math id="M264" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx36" id="paren.46"/>. This will further increase the offset between lidar and MR temperature, thereby shifting the histogram (in red) in Fig. <xref ref-type="fig" rid="Ch1.F3"/>b further to the right.</p>
      <?pagebreak page4165?><p id="d1e5818">On the other hand, lidar temperatures are usually obtained during the night-time, which can lead to a systematic offset due to day–night differences or tidal variations. As discussed by <xref ref-type="bibr" rid="bib1.bibx14" id="text.47"/>, the day–night temperature difference at these altitudes is of the order of 3–4 <inline-formula><mml:math id="M265" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>. This is significantly less than the standard errors in these temperatures, which is on average 6 <inline-formula><mml:math id="M266" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> at contour level 0. Hence we expect the day–night difference in Sodankylä MR temperatures to be  insignificant during the winter period. Moreover, any attempt to estimate MR temperatures using only night-time data has the adverse effect of reducing the accuracy in the estimated temperatures due to data loss. While no specific studies of tidal variation have been made for this location, the data from other sites <xref ref-type="bibr" rid="bib1.bibx10 bib1.bibx39" id="paren.48"><named-content content-type="pre">e.g.</named-content></xref> show that the temperature variation due to tidal activity is typically less than 10 <inline-formula><mml:math id="M267" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>. We can therefore rule out the possibility of an offset in the MSIS gradient model or tidal effects as the primary cause for the <inline-formula><mml:math id="M268" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">58</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M269" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>  offset seen in Fig. <xref ref-type="fig" rid="Ch1.F3"/>b (red histogram).</p>
      <p id="d1e5874"><xref ref-type="bibr" rid="bib1.bibx33" id="text.49"/> emphasised that the biasing in  GM solution is conditional upon the value of the correlation coefficient (<inline-formula><mml:math id="M270" display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula>) between the variables, while <xref ref-type="bibr" rid="bib1.bibx24" id="text.50"/> demonstrated that this solution will be an overestimate in the case of low <inline-formula><mml:math id="M271" display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> values. For the data set used in this work, we found that the correlation between <inline-formula><mml:math id="M272" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height is typically <inline-formula><mml:math id="M273" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.50</mml:mn><mml:mo>±</mml:mo><mml:mn mathvariant="normal">0.05</mml:mn></mml:mrow></mml:math></inline-formula>, thereby indicating the presence of significant natural variation in the measurements. Furthermore,  <xref ref-type="bibr" rid="bib1.bibx17" id="text.51"/> used error modelling to conclude that <inline-formula><mml:math id="M274" display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> must be more than 0.6 for the GM solution to be acceptable. In fact, we have observed that if we restrict our data selection process by excluding all data beyond the density contour 0.2 (Fig. <xref ref-type="fig" rid="Ch1.F1"/>b), this increases the <inline-formula><mml:math id="M275" display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> to be typically around <inline-formula><mml:math id="M276" display="inline"><mml:mrow><mml:mn mathvariant="normal">0.66</mml:mn><mml:mo>±</mml:mo><mml:mn mathvariant="normal">0.06</mml:mn></mml:mrow></mml:math></inline-formula>, with the consequence of reduced biasing in the GM solution. Such a contour selection process essentially removes the erroneous data at higher and lower altitudes from the tail of the distribution, whereby the assumption of equal error variances (i.e. <inline-formula><mml:math id="M277" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub><mml:mo>≈</mml:mo><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) is achieved in the normalised coordinates (Table <xref ref-type="table" rid="Ch1.T1"/>). In other words, the validity of GM solution is conditional upon how close the parameter <inline-formula><mml:math id="M278" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> is to 1 for a given data selection process.</p>
</sec>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Results and discussion</title>
      <p id="d1e6008">The convergence of <inline-formula><mml:math id="M279" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> towards 1 near the core of this bivariate distribution is evident from Table <xref ref-type="table" rid="Ch1.T1"/>. This is demonstrated in Fig. <xref ref-type="fig" rid="Ch1.F4"/>a, where we have estimated the GM slope at various contour levels between 0 and 0.7. In addition, Fig. <xref ref-type="fig" rid="Ch1.F4"/>b reflects the asymptotic behaviour of GM solution at higher contour levels in normalised coordinates. For these data, beyond the contour level 0.4, any change in slope at higher contour level is within the 2<inline-formula><mml:math id="M280" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> error limit. This error in the slope corresponds to an average 2<inline-formula><mml:math id="M281" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> error of 11 <inline-formula><mml:math id="M282" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> in the estimated temperatures at contour level 0.4. In addition, the estimated temperatures can be biased due to small variation of <inline-formula><mml:math id="M283" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> from 1 on a day-by-day basis. For example, If the true value of <inline-formula><mml:math id="M284" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> is 1.25, the GM slope will be  overestimated by 4 % (from Eq. <xref ref-type="disp-formula" rid="Ch1.E26"/> for the date 14 November 2015). For a typical winter temperature of 200 <inline-formula><mml:math id="M285" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> at 90 <inline-formula><mml:math id="M286" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>, a 4 % offset translates to overestimation of temperatures by 8 <inline-formula><mml:math id="M287" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>. In principle, this bias can be further reduced by selecting a higher contour level than 0.4, with the consequence of increased noise level in the estimated temperatures. For these data, the contour level 0.4 is found to provide an optimum condition such that a  maximum of 25 % uncertainty in the parameter <inline-formula><mml:math id="M288" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> leads to 4 % bias in temperature, which, in turn, is comparable to the standard error in the temperature from regression analysis.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><?xmltex \def\figurename{Figure}?><label>Figure 4</label><caption><p id="d1e6097">GM solution at different contour levels in <bold>(a)</bold> original coordinate and in <bold>(b)</bold> normalised coordinate for the date 14 November 2015. The vertical dashed lines in <bold>(a)</bold> correspond to the average value of <inline-formula><mml:math id="M289" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> obtained from SCT calibration at contour level 0.2 and 0.4 respectively for winter 2015–2016. The error bar in <bold>(a)</bold> corresponds to 2<inline-formula><mml:math id="M290" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> error .</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f04.png"/>

      </fig>

      <p id="d1e6133">We have applied the GM slope estimate at contour level 0.4 to the MR data from the period October 2015 to March 2016. This is presented in Fig. <xref ref-type="fig" rid="Ch1.F5"/>, along with the data from co-located lidar observations. The differences between MR temperatures  and lidar are shown in Fig. <xref ref-type="fig" rid="Ch1.F6"/>a for altitudes near peak meteor counts. The mean difference between lidar and MR temperatures is <inline-formula><mml:math id="M291" display="inline"><mml:mrow><mml:mo>+</mml:mo><mml:mn mathvariant="normal">12</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M292" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>, which is expected due to the variation in the true value of <inline-formula><mml:math id="M293" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> from 1. The root-mean-square (rms) difference is about 21 <inline-formula><mml:math id="M294" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>. This difference is partly due the  intrinsic errors of 5–10 <inline-formula><mml:math id="M295" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula> in lidar temperature and partly due to the statistical noise in the estimated MR temperatures.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><?xmltex \currentcnt{5}?><?xmltex \def\figurename{Figure}?><label>Figure 5</label><caption><p id="d1e6185">Comparison of the bias-corrected MR temperatures with lidar data for the winter 2015–2016. The solid line corresponds to the temperature estimated using the GM solution at contour level 0.4. The dashed line corresponds to the SCT-calibrated temperatures using the co-located lidar measurements. The OLS estimates are obtained with <inline-formula><mml:math id="M296" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> as an independent variable. The errors in lidar temperatures are 5–10 <inline-formula><mml:math id="M297" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>, and the 2<inline-formula><mml:math id="M298" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> error (grey shade) of the temperature from EIV analysis is on average 11 K. The differences between lidar and MR temperatures are presented in Fig. <xref ref-type="fig" rid="Ch1.F6"/>.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f05.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6" specific-use="star"><?xmltex \currentcnt{6}?><?xmltex \def\figurename{Figure}?><label>Figure 6</label><caption><p id="d1e6234">Difference between MR temperatures and lidar data for <bold>(a)</bold> the GM solution at contour level 0.4 and <bold>(b)</bold> SCT calibration applied to OLS estimate of <inline-formula><mml:math id="M299" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>. MR temperatures are shown in Fig. <xref ref-type="fig" rid="Ch1.F5"/>.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f06.png"/>

      </fig>

      <p id="d1e6264">For direct comparison with the results above, we have also estimated the MR temperatures using the revised SCT calibration procedure described in Sect. <xref ref-type="sec" rid="Ch1.S3.SS1"/>. For this we have estimated the OLS slope (<inline-formula><mml:math id="M300" display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">β</mml:mi><mml:mi mathvariant="normal">OLS</mml:mi><mml:mi mathvariant="normal">d</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula>) and used <inline-formula><mml:math id="M301" display="inline"><mml:mrow><mml:msqrt><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mi mathvariant="italic">δ</mml:mi></mml:msub></mml:mrow></mml:msqrt><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.11</mml:mn></mml:mrow></mml:math></inline-formula> (Table <xref ref-type="table" rid="Ch1.T1"/>) to obtain the calibrated temperatures from Eqs. (<xref ref-type="disp-formula" rid="Ch1.E16"/>) and (<xref ref-type="disp-formula" rid="Ch1.E6"/>).  These calibrated temperatures are presented in Fig. <xref ref-type="fig" rid="Ch1.F5"/>. The histogram in Fig. <xref ref-type="fig" rid="Ch1.F6"/>b shows the  differences between lidar data and the SCT-calibrated MR temperatures.  The  mean difference between the MR and  lidar temperatures is again about <inline-formula><mml:math id="M302" display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M303" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>, thereby showing that the biasing effect has been properly corrected by this calibration procedure. The rms difference is 15 <inline-formula><mml:math id="M304" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">K</mml:mi></mml:mrow></mml:math></inline-formula>. Although the temperature estimated from the GM solution is slightly biased as compared to that estimated using SCT calibration, the presence of artefacts in the latter is clearly visible in Fig. <xref ref-type="fig" rid="Ch1.F5"/>. As evident from Fig. <xref ref-type="fig" rid="Ch1.F7"/>, the GM solution based on contour selection improves the temperature estimation significantly as compared to the traditional use of the OLS regression analysis.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><?xmltex \def\figurename{Figure}?><label>Figure 7</label><caption><p id="d1e6343"><bold>(a)</bold> Improved temperature estimation using the GM solution (red) as compared to OLS estimates (blue and green) at contour level 0.4. <bold>(b)</bold> Reduced mean offset between MR and lidar temperature for GM slope estimate (red) as compared to OLS estimate (green and blue).</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/4157/2021/amt-14-4157-2021-f07.png"/>

      </fig>

      <p id="d1e6357">The EIV analysis does not distinguish between the measurement error and natural geophysical variability <xref ref-type="bibr" rid="bib1.bibx38" id="paren.52"><named-content content-type="pre">e.g.</named-content><named-content content-type="post">p. 13</named-content></xref>. In other words, the error variances, <inline-formula><mml:math id="M305" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">δ</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>  and  <inline-formula><mml:math id="M306" display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>,  consist of both measurement errors and  the natural geophysical variation. The effective value of <inline-formula><mml:math id="M307" display="inline"><mml:mi mathvariant="italic">λ</mml:mi></mml:math></inline-formula> in a normalised coordinate may vary on a day-by-day basis and may be radar-dependent. For example, meteor trails can get modified by wind effects, ion composition, meteor fragmentation and strong ionospheric currents, as well as temperature and pressure fluctuations, on various spatial and temporal scales <xref ref-type="bibr" rid="bib1.bibx9 bib1.bibx43" id="paren.53"/>. Despite the contour selection process, asymmetric effects of geophysical variation may have increased the effective variance of <inline-formula><mml:math id="M308" display="inline"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:msup><mml:mi/><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, leading to overestimates in the GM solution <xref ref-type="bibr" rid="bib1.bibx6" id="paren.54"/>. Due to the high-latitude location of Sodankylä radar, the geomagnetic effect above 95 <inline-formula><mml:math id="M309" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> can contribute to the systematic bias. Below 85 <inline-formula><mml:math id="M310" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>, the decay of meteor radar echoes may deviate slightly from diffusion-only  evolution <xref ref-type="bibr" rid="bib1.bibx27" id="paren.55"/>, thereby requiring a better physical model that does not assume the linearity of Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>). Assessing the contribution of geophysical variability at various altitudes would require carefully designed replicates of observations as well as long-term comparison of MR temperatures with other co-located instruments. In other words, the case for <inline-formula><mml:math id="M311" display="inline"><mml:mrow><mml:mi mathvariant="italic">λ</mml:mi><mml:mo>≠</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> needs to be handled with careful modelling of errors by taking into account the dominant effect of geophysical variability in these data. This remains a subject of future research.</p>
</sec>
<?pagebreak page4166?><sec id="Ch1.S5" sec-type="conclusions">
  <label>5</label><title>Summary</title>
      <p id="d1e6471">The biasing effect in MR temperature has been a pressing issue for the last 2 decades. Attempts have been made in the past to correct the slope in the scattered plot of  <inline-formula><mml:math id="M312" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height, usually either by direct calibration with optical or satellite data or by an arbitrary choice of data rejection criteria to exclude parts of measurements. This paper has addressed the underlying reasons for such a biasing effect, which is mainly due to the presence of various error terms. We have reviewed the conventional calibration procedure (1) and then provided an alternative method (2) for estimating MR temperature that does not require any calibration. We have applied both of these methods to the MR data from winter 2015–2016 and assessed the quality of the estimated MR temperature using co-located lidar measurements. The key points from each of these two aspects of the paper are given below.
<list list-type="order"><list-item>
      <?pagebreak page4167?><p id="d1e6497">This paper has reviewed the statistical comparison technique (SCT), originally proposed by <xref ref-type="bibr" rid="bib1.bibx13" id="text.56"/>, within the context of MR temperature calibration. We have extended the theoretical basis of the SCT method to obtain an estimate of  error variances of <inline-formula><mml:math id="M313" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height using co-located lidar measurements. No significant offset was seen in the calibrated MR temperature, even without applying any outlier rejection criteria. But artefacts  introduced due to the difference in measurement techniques between MR and lidar were clearly visible in the estimated temperatures.</p></list-item><list-item>
      <p id="d1e6525">As an alternative method, we have applied the errors-in-variables (EIV) regression analysis to estimate the slope in the scattered plot of <inline-formula><mml:math id="M314" display="inline"><mml:mrow><mml:msub><mml:mi>log⁡</mml:mi><mml:mn mathvariant="normal">10</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and height. The model error in EIV analysis takes into account the total errors variances in both abscissa and ordinate. It is observed that the geophysical variability dominates at all altitudes as compared to  measurement errors and is the key factor in addressing the biasing effect. Moreover, any asymmetry in the error variance is minimal near the meteor peak region. This allows for an independent estimate of weighted-averaged atmospheric temperatures at 90 <inline-formula><mml:math id="M315" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> using a suitable contour selection procedure. The<?pagebreak page4168?> temperatures estimated using this method show very good  agreement with co-located lidar measurement and with reduced systematic offset as compared to the traditional least-squares analysis.</p></list-item></list></p>
</sec>

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

      <p id="d1e6561">Data used in the paper are available at <uri>https://www.sgo.fi/pub/AMT_2020_ESarkar/</uri> (last
access: 13 April 2021, <xref ref-type="bibr" rid="bib1.bibx35" id="altparen.57"/>, emranul.sarkar@oulu.fi). The MSIS model data were obtained from <uri>https://ccmc.gsfc.nasa.gov/modelweb/atmos/nrlmsise00.html</uri> (last access: 17 May 2021, <xref ref-type="bibr" rid="bib1.bibx7" id="altparen.58"/>, <ext-link xlink:href="https://doi.org/10.1029/90JA02125" ext-link-type="DOI">10.1029/90JA02125</ext-link>). The lidar data are available at <uri>https://halo-db.pa.op.dlr.de/mission/109</uri> (last access: 17 May 2021, <xref ref-type="bibr" rid="bib1.bibx4" id="altparen.59"/>).</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e6589">ES developed the method, carried out all data analysis and wrote the manuscript. The idea was suggested by AK, who also supervised this work. TU prepared the script for reading the raw data files from the radar and supervises the doctoral thesis of ES. IV co-supervises the doctoral thesis of ES and made suggestions. BK provided the lidar data. ML supported the MR operation at the Sodankylä. All the authors contributed to proofreading the manuscript.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d1e6595">The author declares that there is no conflict of interest.</p>
  </notes><ack><title>Acknowledgements</title><p id="d1e6601">Emranul Sarkar thanks the University of Oulu's Kvantum Institute for their support. We thank the anonymous referees for providing helpful suggestions to improve this paper.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e6606">Ilkka Virtanen has been supported by the Academy of Finland (project no. 301542). Bernd Kaifler has been supported by
the German Research Foundation (DFG), research unit Multiscale Dynamics of Gravity Waves (MS-GWaves; grant no. RA 1400/6-1). Mark Lester has been supported by the Science and Technologies
Facilities Council (STFC; grant no. ST/S000429/1).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e6612">This paper was edited by Jorge Luis Chau and reviewed by two anonymous referees.</p>
  </notes><ref-list>
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<abstract-html><p>For 2 decades, meteor radars have been routinely used to monitor atmospheric temperature around 90&thinsp;km altitude. A common method, based on a temperature gradient model, is to use the height dependence of meteor decay time to obtain a height-averaged temperature in the peak meteor region. Traditionally this is done by  fitting a linear regression model in the scattered plot of <i>log</i><sub>10</sub>(1∕<i>τ</i>) and height, where <i>τ</i> is the half-amplitude decay time of the received signal. However, this method was found to be consistently biasing the slope estimate. The consequence of such a bias is that it produces a  systematic offset in the estimated temperature, thus requiring calibration with other co-located measurements. The main reason for such a biasing effect is thought to be due to the failure of the classical regression model to take into account the measurement error in <i>τ</i> and the observed height. This is further complicated by the presence of various geophysical effects in the data, as well as observational limitation in the measuring instruments. To incorporate various error terms in the statistical model, an appropriate regression analysis for these data is the errors-in-variables model. An initial estimate of the slope parameter is obtained by assuming symmetric error variances in normalised height and <i>log</i><sub>10</sub>(1∕<i>τ</i>). This solution is found to be a good prior estimate for the core of this bivariate distribution. Further improvement is achieved by defining density contours of this bivariate distribution and restricting the data selection process within higher contour levels. With this solution, meteor radar temperatures can be obtained independently without needing any external calibration procedure. When compared with co-located lidar measurements, the systematic offset in the estimated temperature is shown to have reduced to 5&thinsp;% or better on average.</p></abstract-html>
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