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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 GmbH</publisher-name>
<publisher-loc>Göttingen, Germany</publisher-loc>
</publisher>
</journal-meta>

    <article-meta>
      <article-id pub-id-type="doi">10.5194/amt-8-1981-2015</article-id><title-group><article-title>Tomographic retrieval of water vapour and temperature around
polar mesospheric clouds using Odin-SMR</article-title>
      </title-group><?xmltex \runningtitle{Retrieval of water vapour around PMCs from Odin-SMR}?><?xmltex \runningauthor{O.~M.~Christensen et~al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Christensen</surname><given-names>O. M.</given-names></name>
          <email>ole.m.christensen@chalmers.se</email>
        <ext-link>https://orcid.org/0000-0002-2454-549X</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Eriksson</surname><given-names>P.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-8475-0479</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff3">
          <name><surname>Urban</surname><given-names>J.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-7026-793X</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Murtagh</surname><given-names>D.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0003-1539-3559</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Hultgren</surname><given-names>K.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Gumbel</surname><given-names>J.</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>Department of Earth and Space Sciences, Chalmers University of Technology, Gothenburg, Sweden</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Department of Meteorology, Stockholm University, Stockholm, Sweden</institution>
        </aff>
        <aff id="aff3"><label>†</label><institution>deceased, 14 August 2014</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">O. M. Christensen (ole.m.christensen@chalmers.se)</corresp></author-notes><pub-date><day>6</day><month>May</month><year>2015</year></pub-date>
      
      <volume>8</volume>
      <issue>5</issue>
      <fpage>1981</fpage><lpage>1999</lpage>
      <history>
        <date date-type="received"><day>8</day><month>October</month><year>2014</year></date>
           <date date-type="rev-request"><day>28</day><month>November</month><year>2014</year></date>
           <date date-type="rev-recd"><day>8</day><month>April</month><year>2015</year></date>
           <date date-type="accepted"><day>10</day><month>April</month><year>2015</year></date>
      </history>
      <permissions>
<license license-type="open-access">
<license-p>This work is licensed under a Creative Commons Attribution 3.0 Unported License. To view a copy of this license, visit <ext-link ext-link-type="uri" xlink:href="http://creativecommons.org/licenses/by/3.0/">http://creativecommons.org/licenses/by/3.0/</ext-link></license-p>
</license>
</permissions><self-uri xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015.html">This article is available from https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015.html</self-uri>
<self-uri xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015.pdf</self-uri>


      <abstract>
    <p>A special observation mode of the Odin satellite provides the first
simultaneous measurements of water vapour, temperature and polar
mesospheric cloud (PMC) brightness over a large geographical area
while still resolving both horizontal and vertical structures in the
clouds and background atmosphere. The observation mode was
activated during June, July and August of 2010 and 2011, and
for latitudes between 50 and 82<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N.</p>
    <p>This paper focuses on the water vapour and temperature measurements
carried out with Odin's sub-millimetre radiometer (SMR). The
tomographic retrieval approach used provides water vapour and
temperature between 75 and 90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> with a vertical resolution of
about 2.5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> and a horizontal resolution of about
200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. The precision of the measurements is estimated to
0.2 ppmv for water vapour and 2 K for temperature. Due to limited
information about the pressure at the measured altitudes, the
results have large uncertainties (<inline-formula><mml:math display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 3 ppmv) in the retrieved water
vapour.  These errors, however, influence mainly the mean atmosphere
retrieved for each orbit, and variations around this mean are still
reliably captured by the measurements.</p>
    <p>SMR measurements are performed using two different mixer chains,
denoted as frequency mode 19 and 13. Systematic differences between
the two frontends have been noted. A first comparison with the Solar
Occultation For Ice Experiment instrument (SOFIE) on-board the
Aeronomy of Ice in the Mesosphere (AIM) satellite and the Fourier
Transform Spectrometer of the Atmospheric Chemistry Experiment
(ACE-FTS) on-board SCISAT indicates that the measurements using the
frequency mode 19 have a significant low bias in both temperature
(<inline-formula><mml:math display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 15 K) and water vapour (<inline-formula><mml:math display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 0.5 ppmv), while the measurements
using frequency mode 13 agree with the other instruments considering
estimated errors.</p>
    <p>PMC brightness data is provided by OSIRIS, Odin's other
sensor. Combined SMR and OSIRIS data for some example orbits is
considered. For these orbits, effects of PMCs on the water vapour
distribution are clearly seen. Areas depleted of water vapour are
found above layers with PMC, while regions of enhanced water vapour
due to ice particle sedimentation are primarily placed between and
under the clouds.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>Noctilucent, or Polar mesospheric clouds (PMCs) are ice-clouds that
form in the summer mesopause region at high latitudes. During the last
30 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">years</mml:mi></mml:math></inline-formula> there has been much research focused on understanding
the formation and development of these clouds. In particular, the
question has been raised as to how these clouds are responding to the
anthropogenic release of greenhouse gases <xref ref-type="bibr" rid="bib1.bibx44" id="paren.1"/>,
and whether or not these clouds could be used as an indicator of large-scale climate change affecting the mesopause region
<xref ref-type="bibr" rid="bib1.bibx47 bib1.bibx45" id="paren.2"/>.</p>
      <p>To accurately understand possible changes and predict the future of
PMCs, we need to understand the micro-physical properties of the
clouds and the conditions under which they form
<xref ref-type="bibr" rid="bib1.bibx30 bib1.bibx25" id="paren.3"/>. The formation of PMCs
is governed by the amount of supersaturation of the local atmosphere,
thus good measurements of temperature and water vapour in the
mesopause region are needed to accurately assess models and to
identify the processes involved in the creation and sublimation of
PMCs <xref ref-type="bibr" rid="bib1.bibx37" id="paren.4"/>.</p>
      <p>Water vapour and temperature in the vicinity of PMCs have been
measured in several studies using ground-, satellite- as well as
rocket-based instruments <xref ref-type="bibr" rid="bib1.bibx20 bib1.bibx38 bib1.bibx40" id="paren.5"><named-content content-type="pre">e.g.</named-content></xref>. However, for accurate
comparisons to models, both water vapour and temperature should
ideally be measured simultaneously. Such measurements are less common,
and have to date mainly been provided by solar occulting instruments
such as HALOE <xref ref-type="bibr" rid="bib1.bibx26" id="paren.6"/>, ACE-FTS
<xref ref-type="bibr" rid="bib1.bibx48" id="paren.7"/> and AIM-SOFIE
<xref ref-type="bibr" rid="bib1.bibx18" id="paren.8"/>. These measurements have been used in
several studies <xref ref-type="bibr" rid="bib1.bibx34 bib1.bibx48" id="paren.9"><named-content content-type="pre">e.g.</named-content></xref> to
investigate the relationship between the background atmosphere and
PMCs.</p>
      <p>Unfortunately, solar occulting instruments have a limitation when it
comes to the horizontal sampling of the atmosphere. Since only one
profile is generated in each hemisphere per orbit, latitudinal
variations of the atmosphere can only be investigated on a seasonal
basis using these instruments. Emission limb sounders can, unlike
solar occulting instruments, provide global maps of water vapour and
temperature across the entire PMC region within a day. And, unlike
infrared emission sounders <xref ref-type="bibr" rid="bib1.bibx24 bib1.bibx14" id="paren.10"/>,
instruments operating in the microwave region
do not have to account for non-LTE emissions. Accordingly, the
microwave limb sounder (MLS) on board Aura has been used to study the
latitudinal variations in cloud formation
<xref ref-type="bibr" rid="bib1.bibx35" id="paren.11"/>. However, due to the limited vertical
resolution of MLS at the altitudes of concern, and the fact that
a second satellite instrument (AIM-CIPS) had to be used for the PMC
data, only horizontal variations could be studied.</p>
      <p>For a complete picture of the relevant processes involved in the PMC
formation, high resolution and good coverage in both the vertical and
horizontal directions of the background atmosphere and the PMC
distribution is required. In this paper we present a set of
measurements by the sub-millimetre radiometer (SMR) on board the Odin
satellite, which for the first time provides high-resolution water
vapour and temperature measurements around PMCs with a large
geographical coverage. Simultaneous measurements are performed of PMC
brightness by the Optical Spectrograph and InfraRed Imager System
(OSIRIS) on Odin, and as such the combined observations provide
a unique data set useful for the study of PMC formation.</p>
      <p>SMR measures a water vapour transition at 556.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>. In the
normal operational mode it scans the atmosphere between 10 and
110 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, and retrieves both water vapour and temperature. These
measurements have been used in earlier studies to investigate the
water vapour distribution in the mesosphere and above
<xref ref-type="bibr" rid="bib1.bibx23" id="paren.12"/>. However, since the instrument scans the
entire middle atmosphere, the horizontal distance between
measurements at the same tangent altitude can be over 1000 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx22" id="paren.13"/>.  The resulting horizontal sampling
is thus of similar magnitude.</p>
      <p>To increase the horizontal sampling rate, a set of measurements was
made in a special “tomographic” mode during June, July and
August 2010 and 2011. In this mode only altitudes between 75 and
90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> are scanned, which reduces the distance between scans to
200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, thus allowing for a much higher horizontal
resolution. As an additional advantage, the increased density of
measurements opens the possibility of tomographically retrieving the
atmospheric fields using a 2-D retrieval
algorithm.</p>
      <p>Tomographic retrieval from limb-sounding satellite instruments
was first suggested by <xref ref-type="bibr" rid="bib1.bibx6" id="text.14"/>, which used a
non-linear least squares retrieval to implement a “geo-fit“
method that takes into account horizontal inhomogeneities
along the line of sight. Since then, tomographic methods have been applied on
several different limb sounding instruments <xref ref-type="bibr" rid="bib1.bibx9 bib1.bibx42 bib1.bibx7 bib1.bibx29" id="paren.15"><named-content content-type="pre">e.g.</named-content></xref>.
<xref ref-type="bibr" rid="bib1.bibx21" id="text.16"/> used a non-linear optimal estimation method
to retrieve data from the Microwave Limb Sounder on board the Aura spacecraft.
In this paper we apply a similar method to the tomographic
Odin-SMR measurements. This allows a further improvement in resolution
and information content of the tomographic mode retrievals
compared to using the standard Odin-SMR 1-D processing.</p>
      <p>The co-aligned measurements of PMC brightness performed by OSIRIS are
described in <xref ref-type="bibr" rid="bib1.bibx19" id="text.17"/>. A tomographic approach is used to
retrieve both vertical and horizontal structures of the PMCs with
a horizontal resolution down to 330 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> and a vertical
resolution of 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. Combined, the two instruments on board
Odin can thus provide measurements of water vapour, temperature and
PMC brightness with a hitherto unprecedented spatial resolution and
coverage. SMR also performed similar measurements of the Southern
Hemisphere during 2011, but these lack co-located OSIRIS measurements,
and have a slightly different measurement geometry, and as such will
not be considered in this study.</p>

<table-wrap id="Ch1.T1" specific-use="star"><caption><p>Overview of Odin orbits, dates and frequency modes (FM) where tomographic modes are performed.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="8">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:colspec colnum="3" colname="col3" align="left"/>
     <oasis:colspec colnum="4" colname="col4" align="left"/>
     <oasis:colspec colnum="5" colname="col5" align="left"/>
     <oasis:colspec colnum="6" colname="col6" align="left"/>
     <oasis:colspec colnum="7" colname="col7" align="left"/>
     <oasis:colspec colnum="8" colname="col8" align="left"/>
     <oasis:thead>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1">Year</oasis:entry>  
         <oasis:entry colname="col2">Dates</oasis:entry>  
         <oasis:entry colname="col3">Orbit numbers</oasis:entry>  
         <oasis:entry colname="col4">FM</oasis:entry>  
         <oasis:entry colname="col5">Year</oasis:entry>  
         <oasis:entry colname="col6">Dates</oasis:entry>  
         <oasis:entry colname="col7">Orbit numbers</oasis:entry>  
         <oasis:entry colname="col8">FM</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">2010</oasis:entry>  
         <oasis:entry colname="col2">16–17 June</oasis:entry>  
         <oasis:entry colname="col3">50790–50804</oasis:entry>  
         <oasis:entry colname="col4">19</oasis:entry>  
         <oasis:entry colname="col5">2011</oasis:entry>  
         <oasis:entry colname="col6">15–16 June</oasis:entry>  
         <oasis:entry colname="col7">56233–56246</oasis:entry>  
         <oasis:entry colname="col8">19</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">2010</oasis:entry>  
         <oasis:entry colname="col2">14–15 July</oasis:entry>  
         <oasis:entry colname="col3">51209–51223</oasis:entry>  
         <oasis:entry colname="col4">19</oasis:entry>  
         <oasis:entry colname="col5">2011</oasis:entry>  
         <oasis:entry colname="col6">16–17 June</oasis:entry>  
         <oasis:entry colname="col7">56247–56261</oasis:entry>  
         <oasis:entry colname="col8">13</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">2010</oasis:entry>  
         <oasis:entry colname="col2">15–16 July</oasis:entry>  
         <oasis:entry colname="col3">51224–51238</oasis:entry>  
         <oasis:entry colname="col4">13</oasis:entry>  
         <oasis:entry colname="col5">2011</oasis:entry>  
         <oasis:entry colname="col6">17–18 July</oasis:entry>  
         <oasis:entry colname="col7">56711–56725</oasis:entry>  
         <oasis:entry colname="col8">19</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">2010</oasis:entry>  
         <oasis:entry colname="col2">12–13 August</oasis:entry>  
         <oasis:entry colname="col3">51642–51655</oasis:entry>  
         <oasis:entry colname="col4">13</oasis:entry>  
         <oasis:entry colname="col5">2011</oasis:entry>  
         <oasis:entry colname="col6">18–19 July</oasis:entry>  
         <oasis:entry colname="col7">56726–56740</oasis:entry>  
         <oasis:entry colname="col8">13</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">2010</oasis:entry>  
         <oasis:entry colname="col2">13–14 August</oasis:entry>  
         <oasis:entry colname="col3">51656–51671</oasis:entry>  
         <oasis:entry colname="col4">19</oasis:entry>  
         <oasis:entry colname="col5">2011</oasis:entry>  
         <oasis:entry colname="col6">18–19 August</oasis:entry>  
         <oasis:entry colname="col7">57190–57205</oasis:entry>  
         <oasis:entry colname="col8">19</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p>The goal of this paper is to give a detailed description of the
tomographic SMR retrievals, and assess their capabilities and
limitations in the retrieval of the background atmosphere around
PMCs. We will first describe the instrument and the measurement
procedure (Sect. 2), before moving on to the retrieval methodology
(Sect. 3). The first results from the measurements are shown in
Sect. 4, and the accuracy and reliability of the measurements will be
discussed in Sect. 5. Finally, we compare the results to other
satellite instruments and show some early results combining SMR and
OSIRIS data before summarising our findings in Sect. 6.</p>
</sec>
<sec id="Ch1.S2">
  <title>Instrument</title>
<sec id="Ch1.S2.SS1">
  <title>Odin tomographic mode</title>
      <p>The Odin satellite was launched in 2001 with a dual mission: at first
the observation time was split between astronomy and aeronomy, but
since 2007 has purely been dedicated to atmospheric measurements. It flies
in a approximately 600 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> sun-synchronous orbit with an
inclination of 98<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> and the ascending node at 18:00 LT. The
satellite carries two instruments: the SMR
and the OSIRIS. The
instruments are co-aligned and scan the atmosphere in a limb-scanning
configuration, and during standard operation scan tangent altitudes
between roughly 8 and 120 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx27" id="paren.18"/>.</p>
      <p>The Odin satellite and its instruments have many different modes of
operation. In this study we use measurements taken in a special
“tomographic” mode. These measurements were performed during 3 consecutive days in each of June, July and August 2010 and 2011
(see Table <xref ref-type="table" rid="Ch1.T1"/>). In this mode the two
instruments only scan the atmosphere at altitudes between
75 and 90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> to specifically target the summer mesopause region. The
tomographic mode is activated as the satellite crosses the equator,
and measurements are made across the Northern
Hemisphere. Figure <xref ref-type="fig" rid="Ch1.F1"/> shows the coverage of the SMR
tomographic mode during 1 day. As can be seen from the figure, large
parts of the Northern Hemisphere are sampled by Odin over the course of
a day.</p>
      <p>Since the tangent altitudes of the tomographic mode are limited to
75–90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, the distance between each scan through the
atmosphere is reduced from 1000 to 200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, compared to
previous Odin measurements of water vapour in the mesopause
<xref ref-type="bibr" rid="bib1.bibx22" id="paren.19"/>. The shorter distance between scans means that
the line-of-sight through the atmosphere for each scan will
overlap. Figure <xref ref-type="fig" rid="Ch1.F1"/>b shows the line-of-sight from a set of
SMR measurements as a function of altitude and angle along orbit,
where 0<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> is the ascending node and 180<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> the descending
node. The overlap between the scans can clearly be seen. The
line-of-sight overlap means that in order to optimally retrieve
information from these measurements, a tomographic retrieval approach
should be used, hence the name “tomographic” mode.<?xmltex \hack{\newpage}?></p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1"><caption><p><bold>(a)</bold> Coverage of SMR tomographic measurements on 16 July 2010.
The red points are the tangent positions for each
spectrum. The spectra are processed in batches of 150
spectra, the tangent positions for the spectra in one such batch
are shown by the black points. <bold>(b)</bold> The line-of-sight
through the atmosphere for the measurements marked by the black
points in <bold>(a)</bold>.</p></caption>
          <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f01.pdf"/>

        </fig>

</sec>
<sec id="Ch1.S2.SS2">
  <title>SMR</title>
      <p>This paper focuses on the tomographic mode measurements made by
SMR. It measures radiation in five bands at around 118 and between
480–581 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>, and can operate in several different frequency
modes depending on the species of interest <xref ref-type="bibr" rid="bib1.bibx16" id="paren.20"/>. The
tomographic mode uses either the A1 or B2 front-end, operating in the
ranges 541–558 and 547–564 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>, respectively, to measure the
<inline-formula><mml:math display="inline"><mml:mrow class="chem"><mml:msub><mml:mi mathvariant="normal">H</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi mathvariant="normal">O</mml:mi></mml:mrow></mml:math></inline-formula> spectral line at 556.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>. This is achieved by
setting the LO frequency to 553.05 and 553.302 for A1 and B2
frontends, respectively. The resulting frequency modes are labelled
mode 19 and mode 13. A tunable Martin–Pupplet interferometer is used
for single sideband (SSB) filtering. Pre-flight measurements show
a nominal sideband suppression of better than 19 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">dB</mml:mi></mml:math></inline-formula> across the
image band, with a maximum suppression of 35 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">dB</mml:mi></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx10" id="paren.21"/>. However, post-launch analysis of spectra
indicates that the true suppression rather is 11–15 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">dB</mml:mi></mml:math></inline-formula> for
the frequency modes used in this study.</p>
      <p>The spectra are recorded using one of the two autocorrelator
spectrometers among the SMR backends. Each autocorrelator has four
sub-bands of 200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula>, and provides a total bandwidth of
800 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula>. For mesospheric studies of the 557 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula> line
only a part of full bandwidth is needed, and just the 200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula>
sub-band covering the line is used in the retrieval process. The
effective channel resolution of the spectrometer is 2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula>, and
the channel separation 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula>. Furthermore, post-launch
analysis of the instrument has revealed that the autocorrelators have
problem measuring spectra with large dynamic ranges, i.e. large
differences in brightness temperature across the bandwidth of the
instrument. This results in a low bias in the recorded brightness
temperature, which becomes especially apparent in high-altitude
measurements <xref ref-type="bibr" rid="bib1.bibx22" id="paren.22"/>. To compensate for this, the
measured spectra in this study are scaled by 1.03 before they are
inverted.</p>
      <p>The amount of noise in each channel is determined by the noise
temperature of the system, the effective channel resolution, and the
integration time. For the frequency bands used in this study, SMR has
a noise temperature of roughly 3000–3500 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>. For the
tomographic mode measurements, an integration time of 1.8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">s</mml:mi></mml:math></inline-formula> is
used. Due to the time used switching between calibration measurements
and atmospheric measurements, SMR is only measuring the atmosphere
about  half of the total time. Taking this into account, the
resulting thermal noise (1<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula>) is of the order of 2.6 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>
for the measured spectra.</p>
      <p>To relate the measured radiation to a physical brightness temperature
a calibration must be performed. The SMR measurements are calibrated
by switching between the cold sky (space) and the atmosphere, with
a hot-load calibration performed at the end of each scan. In this
study the newest version (V8) of the calibrated Odin spectra is
used. This version was prepared during the autumn of 2013, and beside
improving the treatment of known instrumental artefacts, it corrected
an error related to the transition between orbits, which previously
had made the tomographic observations unusable.</p>
      <p>The vertical resolution of the measurements depends on the size and
shape of the antenna pattern. For SMR the antenna is a 1.1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>
Georgian telescope which provides a half-power beam width better than
0.035<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx16" id="paren.23"/>. This results in a vertical
resolution at the tangent point of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>1.6</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. However, due
to the telescope continuously scanning vertically during the
integration time of 1.8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">s</mml:mi></mml:math></inline-formula> the angular resolution is reduced to
0.04<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>1.8</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) in the tomographic mode.</p>
</sec>
<sec id="Ch1.S2.SS3">
  <title>OSIRIS</title>
      <p>In addition to presenting the results from the SMR tomographic mode
retrievals, this paper also includes some comparisons with the PMC
brightness retrieved from the optical spectrograph of OSIRIS. The
spectrograph is a modified Erbert–Fastie grating spectrometer with
a CCD backend, and can measure light scattered from the atmosphere
between 280 and 800 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">nm</mml:mi></mml:math></inline-formula> with a spectral resolution of around
1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">nm</mml:mi></mml:math></inline-formula>. The entrance slit of OSIRIS is aligned parallel to the
horizon, and subtends a region 30 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> wide and 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>
high at the tangent point.<?xmltex \hack{\newpage}?></p>
      <p>To retrieve PMC properties from the scattered light, the measured
radiation in the wavelength region of 302.8 to 305.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">nm</mml:mi></mml:math></inline-formula> is
compared to a purely Rayleigh scattering background field calculated
using the MSIS climatology. The differences between the measured and
simulated spectra are then used as inputs to a tomographic retrieval
scheme based on a modified version of the Multiplicative Algebraic
Reconstruction Technique <xref ref-type="bibr" rid="bib1.bibx9" id="paren.24"><named-content content-type="pre">MART,</named-content></xref>. The
retrievals return the scattering coefficient of the clouds with
a 330 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> horizontal resolution and 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> vertical
resolution, and an accuracy of
<inline-formula><mml:math display="inline"><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn>11</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><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:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">str</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>. For a detailed description
of the observations and retrieval process the reader is referred to
<xref ref-type="bibr" rid="bib1.bibx19" id="text.25"/>.</p>
</sec>
</sec>
<sec id="Ch1.S3">
  <title>Retrieval methodology</title>
      <p>To extract atmospheric data from the SMR measurements the optimal
estimation method (OEM) is applied. ARTS (Atmospheric Radiative
Transfer Simulator) is used as the forward model, and the retrieval
procedure is implemented using a software package accompanying ARTS.
As previously mentioned, the overlapping lines-of-sight for the
measurements allows for a tomographic retrieval approach. This means
that a 2-D map of the atmospheric fields is
retrieved, rather than single vertical profiles. The following section
describes the forward model and retrieval procedure used in this
study.</p>
<sec id="Ch1.S3.SS1">
  <title>Forward model</title>
<sec id="Ch1.S3.SS1.SSS1">
  <title>General about ARTS</title>
      <p>ARTS is a general purpose radiative transfer program, with a focus on
supporting passive microwave sounding techniques
<xref ref-type="bibr" rid="bib1.bibx5" id="paren.26"/>. It is publicly available software. The
second version of ARTS <xref ref-type="bibr" rid="bib1.bibx13" id="paren.27"/> allows simulations for
1-D, 2-D or 3-D atmospheres, where the 2-D option is applied in this
study. ARTS uses pressure as the main vertical coordinate. For 2-D,
the observations are assumed to be performed along the orbit plane,
and the horizontal coordinate can be seen as the angle along the orbit
(AAO). For a hypothetical satellite having an orbit inclination of
90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, the AAO could be set to match the geocentric latitude
between <inline-formula><mml:math display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mo>+</mml:mo></mml:math></inline-formula>90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, but ARTS allows the AAO to
extend outside this range and the AAO zero point is a user choice.</p>
      <p>The main difference between 1-D, 2-D and 3-D calculations is the ray
tracing – the actual (clear-sky) radiative transfer is solved
identically in all three cases.  That is, after the atmospheric
quantities along the propagation path are determined, the radiative
transfer along the path can be handled independently of the
atmospheric dimensionality. The treatment of weighting functions
(columns of the Jacobian matrix) can be handled in basically the same
way, and ARTS provides these functions for the same set of atmospheric
quantities for 1-D, 2-D and 3-D. Atmospheric weighting functions are
calculated using analytical expressions (ARTS also provides a pure
numerical option), but these consider only local effects. For example,
for temperature the hydrostatic equilibrium around each separate
height is taken into account, but not how the hydrostatic adjustment
propagates to other altitudes. Furthermore, refraction is ignored in
this study, as the effects are negligible for measurements limited to
the mesosphere.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS2">
  <title>Grids</title>
      <p>The forward model atmosphere has a vertical grid stretching from
13.33 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">hPa</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>30</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) to 42 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">Pa</mml:mi></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>150</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>). The grid has an altitude spacing of 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>
between 2.94 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">hPa</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>40</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) and 0.18 mPa (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>140</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), while above and below a spacing of
250 and 500 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> is used, respectively. This dense
vertical spacing is needed to accurately simulate the radiation from the
saturated water vapour line around the mesopause, where strong vertical gradients
are found.</p>
      <p>The horizontal AAO grid used in the forward model starts when the satellite
crosses the equator (<inline-formula><mml:math display="inline"><mml:mrow><mml:mtext>AAO</mml:mtext><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula><inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>) and covers the Northern Hemisphere
from AAO 30 to 150<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. However, since the matrices used in
the tomographic retrieval approach (see Sect. <xref ref-type="sec" rid="Ch1.S3.SS2"/>) generally are non-sparse,
an entire orbit cannot be processed simultaneously on a desktop computer (32 GB RAM) unless
some data reduction technique such as binning channels together or eigenvector expansion
of the Jacobian matrix <xref ref-type="bibr" rid="bib1.bibx11" id="paren.28"/>
is applied. To keep the processing scheme simple, we
have chosen not to apply any such techniques, but following <xref ref-type="bibr" rid="bib1.bibx21" id="text.29"/>
we instead split the measurements into “batches” of 12 scans (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>150</mml:mn></mml:mrow></mml:math></inline-formula> spectra)
covering <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>40</mml:mn></mml:mrow></mml:math></inline-formula><inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO (see Fig. <xref ref-type="fig" rid="Ch1.F1"/>).
This results in that the forward model horizontal grid for each batch
covers <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mspace width="0.125em" linebreak="nobreak"/></mml:mrow></mml:math></inline-formula>30 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>4500</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) around the
centre of the batch, with a spacing of 0.25<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>
(<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>30</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>). Outside this area, 16 additional
grid points cover the AAOs up to <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 50<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO with a lower spacing
to ensure that no errors arise from edge effects.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS3">
  <title>Frequency grid and line parameters</title>
      <p>ARTS is a line-by-line radiative transfer simulator, and for
simulation of the 556.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula> water vapour transition we use
a monochromatic frequency grid ranging from 556.5 to
557.5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>. The spacing is 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula> around the line
centre (556.925–556.945 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula>) decreasing further away from
the line centre reaching 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">MHz</mml:mi></mml:math></inline-formula> at the far end of the
grid. In addition to the frequencies in the signal band, some
frequencies are added in the image band to accurately take into
account influence of the sideband filtering. For the simulations in
this study involving just a handful of transitions, absorption is best
calculated for each point along the propagation paths (“on the fly”
in ARTS terminology), as the option of using a pre-calculated look-up
table is slower.<?xmltex \hack{\newpage}?></p>
      <p>The line parameters for the water vapour line are taken from the JPL and
HITRAN2012 databases. JPL <xref ref-type="bibr" rid="bib1.bibx28" id="paren.30"/> is used for the line
position (556.9359877 GHz) and the line strength
(229.8489 Hz m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>). HITRAN2012 <xref ref-type="bibr" rid="bib1.bibx36" id="paren.31"/> is used
for the pressure broadening coefficient <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">γ</mml:mi><mml:mi mathvariant="normal">p</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. The coefficient is
calculated as <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">γ</mml:mi><mml:mi mathvariant="normal">p</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi>p</mml:mi><mml:msub><mml:mi mathvariant="italic">γ</mml:mi><mml:mtext>air</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>T</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mi>n</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>, where
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">γ</mml:mi><mml:mtext>air</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn>31 362.45</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Hz</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">Pa</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> is the pressure
broadening parameter, <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> the atmospheric temperature, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mn>296</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>
the reference temperature for the broadening parameters, and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>n</mml:mi><mml:mo>=</mml:mo><mml:mn>0.75</mml:mn></mml:mrow></mml:math></inline-formula> the
exponent of the temperature dependency.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS4">
  <title>Instrument parameters</title>
      <p>ARTS includes extensive support for incorporating instruments
characteristics.  Using the methodology introduced by
<xref ref-type="bibr" rid="bib1.bibx10 bib1.bibx12" id="text.32"/>, monochromatic pencil beam
spectra are combined, taking into account the response of antenna,
mixer sidebands and spectrometer, to simulate final sensor brightness
temperatures. For this study, the modelled antenna pattern is based on
the measurements of the SMR antenna system, the single sideband filter
is modelled as a flat function with a sideband suppression of
14 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">dB</mml:mi></mml:math></inline-formula>, and the spectrometer backend channel response is based
on a theoretical model of the spectrometer.</p>
</sec>
</sec>
<sec id="Ch1.S3.SS2">
  <title>Retrieval</title>
<sec id="Ch1.S3.SS2.SSS1">
  <title>General OEM</title>
      <p>In the optimal estimation method the retrieved state vector,
<inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover></mml:math></inline-formula>, is the one minimising the a posteriori error, based
on the known, or assumed, properties of the variations of the
atmosphere and errors in the observation <xref ref-type="bibr" rid="bib1.bibx32" id="paren.33"/>. Due to
the non-linearity of the retrievals in this study an iterative
Levenberg–Marquardt method is applied. The state vector of iteration
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>i</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> from the OEM method is then given by

                  <disp-formula specific-use="align" content-type="numbered"><mml:math display="block"><mml:mtable displaystyle="true"><mml:mtr><mml:mtd><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mrow><mml:mi>i</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msup><mml:mfenced open="[" close="]"><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>)</mml:mo><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msubsup><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msubsup><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:msub><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mfenced><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mtd></mml:mtr><mml:mlabeledtr id="Ch1.E1"><mml:mtd/><mml:mtd/><mml:mtd><mml:mrow><mml:mfenced open="[" close="]"><mml:msubsup><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msubsup><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mo>(</mml:mo><mml:mi mathvariant="bold-italic">y</mml:mi><mml:mo>-</mml:mo><mml:mi>f</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mfenced><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula>

              where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are the covariance
matrices for the a priori state vector, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, and the thermal
noise in the measurement given by <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">y</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the Jacobian
matrix calculated using the forward model of iteration <inline-formula><mml:math display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>f</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>,
and <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> is the Levenberg–Marquardt parameter. It is adjusted after each
iteration based on whether the cost function to be minimised is decreased or increased by the iteration.
For the first iteration <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>=</mml:mo><mml:mn>500</mml:mn></mml:mrow></mml:math></inline-formula>.
For each successful iteration <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> is divided by 10,
and for each failed iteration it is doubled. Convergence
is reached when the change in the retrieved state vectors between
iterations, normalised by the retrieved covariance, is less than
0.0001 times the length of the state vector, <inline-formula><mml:math display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula>, i.e.
              <disp-formula id="Ch1.E2" content-type="numbered"><mml:math display="block"><mml:mrow><?xmltex \hack{\hbox\bgroup\fontsize{9.5}{9.5}\selectfont$\displaystyle}?><mml:mo>(</mml:mo><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mrow><mml:mi>i</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mfenced close="]" open="["><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msubsup><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msubsup><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:msub><mml:mi mathvariant="bold">K</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mfenced><mml:mo>(</mml:mo><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mrow><mml:mi>i</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo><mml:mo>&lt;</mml:mo><mml:mn>0.0001</mml:mn><mml:mo>⋅</mml:mo><mml:mi>n</mml:mi><mml:mo>.</mml:mo><?xmltex \hack{$\egroup}?></mml:mrow></mml:math></disp-formula>
            In most cases this is achieved after 7–10 iterations, and the final
normalised costs are between 0.9–1.1 for 95 % of the retrieved batches. The convergence criterion was tested
by running the retrievals with a higher convergence
threshold (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>n</mml:mi><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>), and ensuring that the differences between the results
with a high and low threshold were sufficiently small
(less than 0.05 ppmv for H<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:math></inline-formula>O and 0.2 K for temperature).</p>
      <p>Of all the retrieved batches, about 30 % have a final iteration where
the ML-parameter increases to 1 after several iterations with a parameter of 0 (and another
2 % where it increases above one).
A final <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> greater than one might imply that the retrievals converged before finding
the local minimum of the cost function. To ensure that the
solution found in these cases do not differ significantly from the
true minimum, the decrease in total cost for the iterations prior (i.e. where <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>)
is analysed, and if changes in normalised cost between these iterations are sufficiently
small (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>0.01</mml:mn></mml:mrow></mml:math></inline-formula>), we regard the solution as valid.</p>
</sec>
<sec id="Ch1.S3.SS2.SSS2">
  <title>The state vector</title>
      <p>The state vector contains all the variables to be retrieved, and in this
study the state vector consists of the logarithm of atmospheric water vapour
relative to the a priori (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">H</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi mathvariant="bold-italic">O</mml:mi></mml:mrow></mml:math></inline-formula>), atmospheric temperatures in
Kelvin (<inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">T</mml:mi></mml:math></inline-formula>) and some instrument variables. These variables are
a baseline fit, a frequency shift and a fit of the pointing error. The
instrumental baseline arises due to standing waves in the receiver, and to
fit this, a first-order polynomial is fitted to each spectrum (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">P</mml:mi><mml:mn mathvariant="bold">0</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">P</mml:mi><mml:mn mathvariant="bold">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>). The exact positioning of the LO frequency has some uncertainty.
This is fitted with a single-frequency fit (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>F</mml:mi></mml:mrow></mml:math></inline-formula>) across each batch.
Finally, there is an uncertainty in the pointing of the antenna, and a single
pointing offset (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula>) is retrieved across the batch.</p>
      <p>The total state vector is given by combining all the sub-vectors:

                  <disp-formula id="Ch1.E3" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>=</mml:mo><mml:mo>[</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">H</mml:mi><mml:mn mathvariant="bold">2</mml:mn></mml:msub><mml:mi mathvariant="bold-italic">O</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="bold-italic">T</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>F</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>,</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">P</mml:mi><mml:mn mathvariant="bold">0</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">P</mml:mi><mml:mn mathvariant="bold">1</mml:mn></mml:msub><mml:msup><mml:mo>]</mml:mo><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>

            For the atmospheric fields (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">H</mml:mi><mml:mn mathvariant="bold">2</mml:mn></mml:msub><mml:mi mathvariant="bold-italic">O</mml:mi></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">T</mml:mi></mml:math></inline-formula>) the elements are sorted
first by altitude then by latitude and the retrieval grid covers altitudes
between 316 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>40</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) and 0.75 mPa (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>130</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) with an altitude spacing of 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> above
17 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>60</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) and a spacing of 2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> below.
The horizontal retrieval grid covers 50<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO centred around the batch
with a spacing of 0.5<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. For both the forward model and retrieval grid
the values are treated to vary linearly between the grid points <xref ref-type="bibr" rid="bib1.bibx5" id="paren.34"/>,
thus effectively, a bilinear interpolation is applied to convert between the two grids.</p>
</sec>
<sec id="Ch1.S3.SS2.SSS3">
  <title>A priori values</title>
      <p>For each state vector variable an a priori value must be given. For the
atmospheric variables, these are given as 2-D fields
across the retrieval grid. For water vapour, an a priori profile
constant with latitude and time was chosen. Using such a fixed a priori
profile makes it easier to ensure that the structures seen in the
retrieved water vapour field actually come from the measurements,
rather than the a priori field. The a priori profile is based on
a climatology of water vapour from the MLS instrument on board the
Aura satellite. Taking the mean of the MLS water vapour concentrations
from June, July and August for latitudes above 60<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, the
profile shown in Fig. <xref ref-type="fig" rid="Ch1.F2"/> is obtained.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><caption><p>The <inline-formula><mml:math display="inline"><mml:mrow class="chem"><mml:msub><mml:mi mathvariant="normal">H</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi mathvariant="normal">O</mml:mi></mml:mrow></mml:math></inline-formula> a priori profile created from the mean of a MLS climatology.</p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f02.pdf"/>

          </fig>

      <p>For temperature the MSISE-90 model <xref ref-type="bibr" rid="bib1.bibx17" id="paren.35"/> is used as
the a priori value. The model gives the mean temperature for each month
as a function of latitude and pressure, covering pressures from
1013 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">hPa</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) to <inline-formula><mml:math display="inline"><mml:mrow><mml:mn>5.7</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> Pa
(<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>130</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>). Furthermore, the MSISE-90 climatology is
used for the pressure–altitude relationship for the
retrievals. However, since temperature, pressure and altitude are
closely interlinked through hydrostatic equilibrium (HSE), the
pressure–altitude relationship must be adjusted during the retrieval
to ensure a consistent relationship between the three variables. This
is done by using the <?xmltex \hack{\mbox\bgroup}?>MSISE-90<?xmltex \hack{\egroup}?> model to find the geometrical altitude
corresponding to a pressure level of 2.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula>, and the
correcting the pressure–altitude relationship for the other pressure
levels by assuming HSE in the retrieved atmosphere.</p>
      <p>For the instrumental variables, the a priori assumption is that the
measurements are correct, i.e. a value of 0 is used for the frequency
shift, pointing error and the baseline fits.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><caption><p><bold>(a)</bold> Vertical and <bold>(b)</bold> horizontal
elements of the covariance matrix for <inline-formula><mml:math display="inline"><mml:mrow class="chem"><mml:msub><mml:mi mathvariant="normal">H</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi mathvariant="normal">O</mml:mi></mml:mrow></mml:math></inline-formula> at AAO 0.09 Pa
and 105 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>.
<bold>(c)</bold> Elements of the total
covariance matrix for water vapour. The black square indicates
a single covariance block, i.e. covariance between altitudes at the
same AAO.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f03.pdf"/>

          </fig>

</sec>
<sec id="Ch1.S3.SS2.SSS4">
  <title>A priori covariance</title>
      <p>The optimal estimation method requires, in addition to a priori values,
a covariance matrix to be created for the state vector variables. The
total covariance matrix is set to a block diagonal matrix with the
covariance matrix for each variable in each block:

                  <disp-formula id="Ch1.E4" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mfenced close=")" open="("><mml:mtable class="matrix" columnalign="center center center center center center" framespacing="0em"><mml:mtr><mml:mtd><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow class="chem"><mml:msub><mml:mi mathvariant="normal">H</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi mathvariant="normal">O</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mtext>Temp</mml:mtext></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:msup><mml:mfenced close=")" open="("><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>F</mml:mi></mml:mrow></mml:msubsup></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:msup><mml:mfenced close=")" open="("><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:msubsup></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mn mathvariant="normal">0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:mfenced><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>For the atmospheric fields the a priori covariance matrices are
matrices with non-zero elements far from the diagonal due to
correlation in the errors in the a priori atmosphere and natural
variation across the 2-D grid. The standard deviation for the
atmospheric fields are set to 30 % for water vapour, and 7 K
for temperature.</p>
      <p>The spatial correlations are set using correlation functions in both
the vertical and horizontal directions. The correlation is modelled as
a function, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ρ</mml:mi></mml:math></inline-formula>, decreasing exponentially with altitude/AAO. The
correlation lengths, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">c</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, defined by <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">ρ</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">c</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:msup><mml:mi>exp⁡</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>, are specified to 5<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> in the
horizontal direction and 8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> in the vertical direction for both water
vapour and temperature. These covariances represent the large-scale uncertainties
of our a priori fields. However, some degree of ad hoc adjustments were made
the to reduce possible vertical and horizontal oscillations in the retrieved data.
The covariance for water vapour in the horizontal
and vertical directions is shown in Fig. <xref ref-type="fig" rid="Ch1.F3"/>a and b.</p>
      <p>The total correlation in both dimensions is calculated as
              <disp-formula id="Ch1.E5" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mi mathvariant="normal">tot</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mi>exp⁡</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:msqrt><mml:mrow><mml:mo>(</mml:mo><mml:mstyle scriptlevel="+1"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">x</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:mstyle scriptlevel="+1"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>y</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">y</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:msqrt></mml:mrow></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>y</mml:mi></mml:mrow></mml:math></inline-formula> is the distance between two points in the horizontal
and vertical direction and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">x</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi mathvariant="normal">y</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> the corresponding
correlation length.
A part of the complete covariance matrix for water vapour is shown in Fig. <xref ref-type="fig" rid="Ch1.F3"/>a.
It can be seen that the matrix has a block structure, where each block
<inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:math></inline-formula>, indicated by the black square in the
figure, is the covariance matrix covering all altitudes at one AAO,
and the off-diagonal blocks are the vertical covariance matrix
multiplied by the correlation between the different AAOs.</p>
      <p>For the instrumental variables the covariance matrices are pure
diagonal matrices (or scalars). For the baseline polynomial fits the
uncertainty is set to 4 and 2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> for the zeroth and first order
respectively. For the frequency fit the covariance matrix is simply
a scalar with an assumed uncertainty of 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula>, whereas for the
pointing error the uncertainty is set to 0.001<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. The strict
constraint on the pointing offset is needed to prevent the
non-linear retrievals from converging to unrealistic results.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><caption><p>Water vapour <bold>(a)</bold> and temperature <bold>(b)</bold> from
the tomographic retrievals where a 50 % enhancement of water vapour is
simulated in the areas marked by the black squares. The results are
presented in terms of deviation from the a priori (% and K). The dashed
lines show the lines-of-sight of SMR.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f04.pdf"/>

          </fig>

</sec>
</sec>
</sec>
<sec id="Ch1.S4">
  <title>Results</title>
<sec id="Ch1.S4.SS1">
  <title>A simulated case</title>
      <p>In order to illustrate the viability of the tomographic methodology,
a simulated retrieval was performed. In this way the sensitivity of
the retrievals to changes in water vapour and temperature can be
investigated. The mean temperature and water vapour retrieved from the
tomographic measurements was used as the atmospheric a priori in the
simulation. Since the purpose of this study is to look at small-scale
variations of water vapour and temperature around PMCs, a water vapour
enhancement of 50 % was simulated in three small regions
of the atmosphere. One such region was centred at 79 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO and 82 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> in altitude.
This region was given a size of <inline-formula><mml:math display="inline"><mml:mrow><mml:mn>200</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">km</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>,
which roughly corresponds to the estimated resolution of the tomographic measurements
(see Sect. <xref ref-type="sec" rid="Ch1.S5.SS1.SSS1"/>). A smaller region (<inline-formula><mml:math display="inline"><mml:mrow><mml:mn>100</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">km</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula>)
was positioned at <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 74 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO, to test the limits of the method.
Finally, a region with a small horizontal (100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), but large vertical
(15 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>) extent was simulated at <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 67 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO to investigate
the effect of horizontal inhomogeneities. Using this atmosphere,
a set of simulated measurements was generated. This
test atmosphere might not be realistic, but should be a useful tool for
qualitatively evaluating the performance of the methodology. The
retrieval was performed as described in
Sect. <xref ref-type="sec" rid="Ch1.S3"/>. No noise was added to the
simulated data, but the simulated retrievals were done
using a noise covariance matrix describing a thermal noise with
a <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> of 2.6 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F4"/>a shows the retrieved water vapour,
relative to the a priori atmosphere, from the simulated retrieval. The
areas with enhanced water vapour are
shown by the black contours, and the retrieved water vapour is
shown by the colour of each pixel. Looking at the area around
79 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> it is clear from the results that the
retrievals can reproduce the water vapour enhancement, though some
smoothing is seen. This smoothing
is expected, as the enhanced area is of the same size as the 67%
centred quantile resolution derived in Sect. <xref ref-type="sec" rid="Ch1.S5.SS1.SSS1"/>.</p>
      <p>The values retrieved for the enhanced area at <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 67 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> show
that inhomogeneities with an even smaller horizontal extent can be
retrieved at the correct position. The vertical edges of the
inhomogeneity are accurately reproduced by the retrievals. However,
a large effect of the limited spatial resolution
can be seen as the retrieved enhancement is around 15–25 %
rather than the true value of 50 %. This is also the case
for the smallest area at 74 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO where an enhancement
of less than 10 % is retrieved. Thus, this small area of
<inline-formula><mml:math display="inline"><mml:mrow><mml:mn>100</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">km</mml:mi><mml:mo>×</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> indicates the
smallest regions of change we can expect our measurements to be sensitive
to, although it should noted that retrieved values from such small areas
in most cases will be overshadowed by the random variations
from noise in the data.</p>
      <p>In addition to water vapour, the tomographic retrieval returns the
temperature field of the atmosphere. Due to the nature of the
measurement method, the Jacobian matrix is not completely
block diagonal with respect to the two atmospheric variables.
This means that the two retrieved quantities will not be
independent of each other. As a result an increase in water vapour
will influence the retrieved temperature field. Figure <xref ref-type="fig" rid="Ch1.F4"/>b
shows the change in retrieved temperature
due to the simulated water vapour enhancements, and
variations of <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> are seen in the retrieved data around
the water vapour enhancements.</p>
      <p>To test the temperature retrievals, another simulation was set up. In
this simulation (not shown) the water vapour distribution was set
equal to the measured mean, and the temperature was perturbed by
reducing it by 10 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> in the same manner as with the test
simulation for water vapour. For the temperature the perturbed
areas were reproduced in the correct position, but the
retrieved values were up to 5 K warmer than the true
value. The reason for this is that the temperature resolution,
in particular the 95% quantile resolution, is worse than resolution
of the retrieved water vapour, thus a larger smoothing effect is seen.
For further discussion on this see Sect. <xref ref-type="sec" rid="Ch1.S5.SS1.SSS1"/>. The influence that
changes in temperature had on the retrieved water vapour field were
up to 8 % in the retrieved water vapour within
the perturbed areas, and no change outside of them.</p>
      <p>These simulated tests are not a complete validation of the retrievals,
but meant to illustrate some of the capabilities and limitations
of the method. The final test of the abilities of the measurements
to estimate the true atmosphere will be done by comparing the
retrieved data to other instruments. A further discussion of this
along with possible sources of uncertainties and errors in
the retrievals can be found in Sect. <xref ref-type="sec" rid="Ch1.S5"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><caption><p>Water vapour <bold>(a)</bold> and temperature <bold>(b)</bold> from
1-D retrievals where a 50 % enhancement of water vapour is
simulated in the areas marked by the black squares. The results are
presented in terms of deviation from the a priori (% and K). The dashed
lines show the lines-of-sight of SMR.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f05.pdf"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6" specific-use="star"><caption><p><bold>(a)</bold> Sample spectra of the 557 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">GHz</mml:mi></mml:math></inline-formula> line
from orbit 51226 at different heights (solid lines), with fitted
spectra (dashed lines). <bold>(b)</bold> Residuals of all spectra in
orbit 51226 (blue), mean of the residuals in that orbit (black)
and the average (<inline-formula><mml:math display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mi mathvariant="italic">σ</mml:mi></mml:mrow></mml:math></inline-formula>) thermal noise of the measurements
(white).</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f06.pdf"/>

        </fig>

<sec id="Ch1.S4.SS1.SSS1">
  <title>Comparison to 1-D retrievals</title>
      <p>The simulated case also provides an opportunity to compare the tomographic
retrieval method to a standard 1-D retrieval. In 1-D retrievals
each scan through the atmosphere is retrieved independently.
To ensure that the definitions and
constraints of the 1-D retrievals are consistent with the tomographic
approach the inversions were done using the same setup as described in
Sect. <xref ref-type="sec" rid="Ch1.S3"/>, but with the state vector only describing
a single AAO centred at the mean tangent point of the scan (i.e. assuming
horizontal homogeneity).</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F5"/> shows the retrieved water vapour and
temperature using the 1-D retrieval method from the
same test case as in Fig. <xref ref-type="fig" rid="Ch1.F4"/>. The
1-D method recreates the water vapour enhancements with reasonable
accuracy, except for the smallest region, which is not detected.
The position of the two regions at 67 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>  and 79 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>
is shifted away from the satellite. This shift occurs due
to the sampling of the atmosphere, so depending
on the position of the measurements in relation to the
enhanced area, the shift might be both towards or away from the satellite.
Furthermore, the lower edge of the area at 67 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> is not
successfully recreated in the 1-D retrievals.</p>
      <p>For the retrieved temperature field, the differences between the tomographic and
1-D methods are larger. Large areas of increased temperatures can be seen
at the latitudes of the water vapour enhancements. These temperature errors
arise since some measurements have a line-of-sight going through the
perturbed area, but not at the tangent point. For these measurements
the 1-D method will misplace perturbation by several kilometres in altitude
and AAO. Since the purpose of the tomographic measurements is to study the atmosphere
around polar mesospheric clouds, an area where large horizontal variations in water vapour
can be expected, the demonstrated temperature and water vapour artefacts
seen in the 1-D approach would significantly degrade the data,
and thus a tomographic retrieval approach is preferred for these measurements.</p>
</sec>
</sec>
<sec id="Ch1.S4.SS2">
  <title>Result from a real case</title>
      <p>To exemplify the results of the tomographic measurements, two orbits
(51221 and 51226) recorded on 15 July 2010 are selected as example
orbits. Orbit 51221 is selected as collocations between Odin-SMR and
both ACE-FTS and AIM-SOFIE can be found along this orbit. Orbit 51226
is used since it is an orbit recorded soon after, where
SMR is using the other frontend.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F6"/> shows some example spectra from orbit 51226
at different tangent altitudes. The saturation of the line at the
lower altitudes is seen, as the brightness temperature of the line
centre is lower than the line wings, reflecting the negative
temperature gradient of the mesosphere. The spectra fitted by the
retrievals are shown as dashed lines showing how they reproduce the
general shape and amplitude of the measured spectra. To get a better
view of the fit, the residuals from all spectra in orbit 51226 are
shown in Fig. <xref ref-type="fig" rid="Ch1.F6"/>b. Ideally the residuals should be
white noise with a standard deviation equal to that of the thermal noise of the
receiver. For most of the spectrometer channels this is true; however,
for the channels closest to the line centre some non-white noise can
be seen in single measurements.</p>

      <fig id="Ch1.F7"><caption><p>Example results from orbit 51221 and orbit 51226 on
15 July 2010. The lower <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis shows the AAO and the top axis
shows the true latitude of the measurements. The black lines
indicate the positions of collocated ACE-FTS and AIM-SOFIE
measurements. The black dots are the tangent position for each measurement.</p></caption>
          <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f07.pdf"/>

        </fig>

<sec id="Ch1.S4.SS2.SSS1">
  <title>Water vapour and temperature</title>
      <p>Figure <xref ref-type="fig" rid="Ch1.F7"/> shows the retrieved water vapour for the two
selected orbits. The retrieved fields cover latitudes (top <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis)
from <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>50</mml:mn></mml:mrow></mml:math></inline-formula> up to 82 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N and then down to <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>50</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N on the other side of the pole. The approximate
altitudes for the pressure levels are given on the right <inline-formula><mml:math display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula>-axis. These
are found by taking the mean altitude of each pressure
level across the orbit. The vertical distribution of
water vapour shows high concentration (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> ppmv) up to <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>85</mml:mn></mml:mrow></mml:math></inline-formula> km
where it quickly drops down to values between 0 and
2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula>. This is consistent with the current understanding of
the dynamics of the summer mesosphere where water vapour is brought up
from the lower altitudes by the mesospheric overturning circulation
and removed by photodissociation as it reaches the mesopause.</p>
      <p>The latitudinal distribution of water vapour shows generally higher
concentrations towards the pole than at lower latitudes, and both
orbits have large areas with water vapour concentrations above
10 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula> between 70 and
80 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N. Figure <xref ref-type="fig" rid="Ch1.F7"/>b in particular shows high
amounts of water vapour in two areas at 80 and 100 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO,
while in Fig. <xref ref-type="fig" rid="Ch1.F7"/>a the concentration is highest at
80 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO. These areas arise as a result of atmospheric
dynamics combined with the redistribution of water vapour due to the
presence of PMCs.</p>

      <fig id="Ch1.F8"><caption><p>Temperature retrieved from orbit 51226 on 15 July 2010. The
lower <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis shows the AAO and the top axis shows the true
latitude of the measurements. The black lines indicate the
positions of collocated ACE-FTS and AIM-SOFIE measurements.
The black dots are the tangent position for each measurement.</p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f08.pdf"/>

          </fig>

      <p>Below 80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> there are significant differences between the two
orbits. Figure <xref ref-type="fig" rid="Ch1.F7"/>b shows less water vapour
overall, and large amount of water between 70 and 100 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO is
not present compared to Fig. <xref ref-type="fig" rid="Ch1.F7"/>a. Comparing
several other orbits shows that this is probably due to instrumental
differences between the two frontends rather than a physical change in
the real atmosphere. The consequences and implication of this will be
elaborated further in Sect. <xref ref-type="sec" rid="Ch1.S5.SS3"/>, where the results
are compared to other satellite instruments.</p>
      <p>The black dots in Figs. <xref ref-type="fig" rid="Ch1.F7"/> and <xref ref-type="fig" rid="Ch1.F8"/> show
the positions of the tangent points for each measurements. At these
points the contribution from the measurements should be the largest.
A retrieval grid point between these dots may suffer from a high a priori contribution,
depending on the exact position relative to the lines-of-sight of the measurements.
This can lead to oscillatory structures in the data if there is a systematic
difference between the true atmosphere and the a priori value. Looking
at the results from the two test orbits, tendencies of such patterns are
seen at the lower edge of the covered area (75–80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), but in general
the results should not be influenced by the sampling of the atmosphere.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9" specific-use="star"><caption><p>The 2-D averaging kernel of water vapour (left) and temperature (right) for
the retrieval grid point marked by the black dot. The dashed lines show the line-of-sight of
the measurements through the atmosphere.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f09.pdf"/>

          </fig>

      <p>Figure <xref ref-type="fig" rid="Ch1.F8"/> shows the temperature field retrieved
from orbit 51226. The retrieved temperature has a mesopause altitude
around 90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> with the lowest mesopause temperatures (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>115</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>) closest to the poles.  This is once again due to the
mesospheric overturning circulation, with the faster ascending air
over the pole causing a stronger cooling than at lower latitudes.<?xmltex \hack{\newpage}?></p>
</sec>
</sec>
</sec>
<sec id="Ch1.S5">
  <title>Discussion</title>
<sec id="Ch1.S5.SS1">
  <title>2-D averaging kernels</title>
      <p>Spatial resolution of retrieved data is usually described by the rows of the
averaging kernel matrix (AKM), <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold">A</mml:mi></mml:math></inline-formula>. Each element in this matrix,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">A</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, gives the change in the retrieved state vector element
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mi mathvariant="bold-italic">i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> from a change in the true state vector element <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.
We calculate the AKM by assuming that the final step in the Levenberg–Marquardt
iteration has a Levenberg–Marquardt parameter of 0, i.e.
            <disp-formula id="Ch1.E6" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="bold">A</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mfenced open="[" close="]"><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msup><mml:mi mathvariant="bold">K</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mi mathvariant="bold">K</mml:mi><mml:mo>)</mml:mo></mml:mfenced><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup><mml:msup><mml:mi mathvariant="bold">K</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msup><mml:msubsup><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup><mml:mi mathvariant="bold">K</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>Note that for these batches where the final ML-parameter differs from zero,
<inline-formula><mml:math display="inline"><mml:mi mathvariant="bold">A</mml:mi></mml:math></inline-formula> is still calculated with an ML-parameter of 0 (i.e using
Eq. <xref ref-type="disp-formula" rid="Ch1.E6"/>). The reason for this is that the final solution
(and hence the AVK) is independent of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> (for further discussion
see e.g. <xref ref-type="bibr" rid="bib1.bibx8" id="altparen.36"/> and the discussion thereof,
and <xref ref-type="bibr" rid="bib1.bibx31" id="altparen.37"/>).</p>
      <p>For non-linear retrievals <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold">A</mml:mi></mml:math></inline-formula> will depend on the atmospheric
state, and will vary between measurements. Thus, in order to give the
most representative picture of the capabilities and limitation of the
retrievals, we have chosen to show the averaging kernels calculated
using the mean retrieved state from all the measurements in this paper.</p>
      <p>The plots in Fig. <xref ref-type="fig" rid="Ch1.F9"/> show a single row
of the AKM, separated into the columns covering water vapour and temperature
respectively. This row can be referred to as the 2-D averaging
kernel (AVK), for the retrieval point considered (positioned at 94.5 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO
and 82 km altitude).</p>
      <p>The 2-D averaging kernel for water vapour is relatively
symmetric around the retrieval point. However, since this point
is not placed directly in a line of sight, all contributions
to the retrieved value will come from measurements of the
adjacent grid points, thus the peak of the AVK will not be in
the centre. We have chosen this point to illustrate  a “worst case” scenario
for the analysis of the averaging kernels. For retrieval grid points where several
lines of sight intersect, the 2-D averaging kernels have
their peak at the grid point.</p>
      <p>Just as for water vapour, the temperature averaging kernel has peaks located at the measurement
points surrounding the retrieval point, rather than at the retrieval point.
Additionally the temperature AVK displays an asymmetry, weighting the
information along the line of sight more than information from adjacent scans.
If the centroid (first moment) position is calculated
it is still placed at the retrieval point.</p>
<sec id="Ch1.S5.SS1.SSS1">
  <title>Spatial resolution</title>
      <p>Although the averaging kernel matrix gives the most complete picture of
where the retrieved information at each retrieval point comes from,
it is still useful to define a resolution for the retrievals. To do this we first
define the horizontal and vertical averaging kernel
for a retrieval point as the sum of the 2-D
averaging kernel for that point over all columns corresponding to a certain pressure
(for the vertical averaging kernel) or AAO (for the horizontal averaging kernel).
Thus the vertical averaging kernel for a retrieval point gives the total contribution
from different altitudes to the retrieved value at the retrieval
point. Similarly the horizontal averaging kernel gives the total contribution
of each AAO to the retrieved value at the retrieval point.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F10" specific-use="star"><caption><p>The estimated vertical <bold>(a)</bold> and horizontal <bold>(b)</bold> resolution
for water vapour (blue) and temperature (red). The solid lines and dash-dotted
lines show the resolution calculated using the 67 and 95 % quantiles, respectively.
The dashed lines in <bold>(a)</bold> indicate the  measurement response multiplied by 10.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f10.pdf"/>

          </fig>

      <p>From this definition an estimation of the horizontal and vertical resolution can be made.
Since the 2-D averaging kernels have multiple peaks, we use a definition of
resolution based on the area under the horizontal and vertical AVKs.
Following <xref ref-type="bibr" rid="bib1.bibx46" id="text.38"/> we use the centred quantile distance
as a measure of resolution. However, due to possible negative sidelobes seen in the
vertical and horizontal AVKs, we perform the quantile integral outwards from the
centroid (first moment) position of corresponding averaging kernel, and not from the
beginning of the horizontal/vertical grid. We thus define the two quantile resolutions (67 and 95 %)
as the shortest distance between two points <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> at the ordinate of the horizontal
or vertical averaging kernel determined such that the area under the curve
between <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> corresponds to 67 or 95 % of the
total area under the horizontal or vertical averaging kernel.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F10"/>a and b show
the estimated 67 and 95 % vertical and horizontal resolution for
temperature and water vapour for each altitude at 84 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO.
For water vapour the vertical resolution (67 %) is between 1 and 2 km for the
region of interest in this study (75–90 km). For temperature the vertical resolution (67 %) deteriorates
for higher altitudes being <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 3 km at 80 km increasing to around 5 km at 90 km. The horizontal
resolution for water vapour and temperature is 1.8–2 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 200 km) between
75 and 87 km. The 95 % resolutions are roughly a factor 2 worse. This leads to particularly poor
resolutions at around 90 km, indicating that a large degree of smoothing should be expected
in this area.</p>
</sec>
<sec id="Ch1.S5.SS1.SSS2">
  <title>Measurement response</title>
      <p>The measurement response (MR) of the retrievals gives an indication of
how sensitive the retrievals are to large-scale changes in the true
atmosphere, and is calculated by summing the AVKs along each row over
all columns corresponding to the retrieved variable
<xref ref-type="bibr" rid="bib1.bibx1" id="paren.39"/>. The measurement response for
water vapour and temperature are shown by the dashed lines in Fig. <xref ref-type="fig" rid="Ch1.F10"/>. For both temperature and water vapour
a response larger than 0.9 can be seen for the entire
area of interest (75–90 km).</p>
</sec>
</sec>
<sec id="Ch1.S5.SS2">
  <title>Errors</title>
      <p>There are several possible sources of errors in the retrievals. Random
errors come from thermal noise in the measurements (retrieval noise),
from the limited resolution of the measurements (smoothing error), and
pointing error in the satellite. Additionally, the results have
systematic errors related to uncertainties in modelling of the
instrument, modelling of the atmosphere, and uncertainties in the
spectral line parameters. Just as with the averaging kernels, the
effect of uncertainties and errors will depend on the true atmospheric
profile. Thus, to give an indication of the average error expected in
the retrievals, the error analysis is based around a case linearised
around the mean retrieved state of the measurements.</p>
      <p>The smoothing error and retrieval noise can be calculated using the
covariance matrices, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold">S</mml:mi><mml:mi mathvariant="italic">ϵ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>
respectively, as described in <xref ref-type="bibr" rid="bib1.bibx32" id="text.40"/>. The retrieval noise
for the measurements presented in this study is <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 0.2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula>
for water vapour and 2–3 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> for temperature. It should be noted
that the errors arising from thermal noise in the data
will be correlated in both the vertical and horizontal direction. From
investigation of the retrieval noise covariance matrix, the correlation length
of the retrieval noise is 2–3 km in altitude and 2–3 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> in
angle along orbit for both temperature and water vapour from 75 to
90 km. An accurate estimation of the smoothing error requires that the atmospheric covariance
matrix is known with certainty, which is not the case for these
retrievals. As such we will not use the smoothing errors
for the error analysis, but rather consider the retrieved result as
the smoothed version of the true atmosphere, with a resolution given
by the averaging kernels.</p>
      <p>For the systematic errors, their influence is estimated by performing
a simulated retrieval on the mean retrieved state with the forward
model perturbed to the <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mi mathvariant="italic">σ</mml:mi></mml:mrow></mml:math></inline-formula> estimate of the investigated
parameter. The parameters investigated are the line strength <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>I</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>,
which is perturbed <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 2 %, based on the JPL uncertainty, and the
pressure broadening parameter <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula>, which is perturbed 5 %,
based on differences between the measurements reported in
<xref ref-type="bibr" rid="bib1.bibx39" id="text.41"/>. Errors in the altitude of the HSE reference
pressure level (2.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula>), <italic>Pressure</italic>, are estimated by moving
the pressure level <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, based on differences between
MSISE-90 and CIRA86 <xref ref-type="bibr" rid="bib1.bibx15" id="paren.42"/> at
70 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. Additionally uncertainties related to the properties of
the SMR instrument are simulated. The instrumental parameters
investigated are an offset in the pointing of <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.02<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx22" id="paren.43"/>, and uncertainties in the sideband suppression
of <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 2 % (11–15 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">dB</mml:mi></mml:math></inline-formula>).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F11" specific-use="star"><caption><p>Estimated uncertainties for water vapour <bold>(a)</bold> and
temperature <bold>(b)</bold> from the tomographic retrievals. The
dashed black line shows the estimated retrieval noise. The
solid lines show the errors due to forward model parameters. Finally,
the dashed red line shows the uncertainty arising from errors in the
background pressure, if number densities are used as the retrieved
quantity. For a complete description of the parameters see the text.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f11.pdf"/>

        </fig>

      <p>It should be noted that the presence of PMCs will not affect the
retrieval of water vapour and temperature from SMR. The radiance
emitted from ice particles is of the order of 0.1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>, and will
be very uniform across the bandwidth of the spectrometer. As such, it
will be completely overshadowed by any baseline in spectrometer, and
thus corrected for in the polynomial baseline fit performed on each
spectrum.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F11"/> shows the random and systematic errors
estimated around the mean atmospheric state. The plotted value,
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>E</mml:mi></mml:mrow></mml:math></inline-formula>, is the mean absolute value of the difference between the
perturbed, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mo>±</mml:mo><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, and unperturbed, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>,
retrievals given by

                <disp-formula id="Ch1.E7" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mo>|</mml:mo><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo><mml:mo>|</mml:mo><mml:mo>+</mml:mo><mml:mo>|</mml:mo><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mo>-</mml:mo><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>(</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>)</mml:mo><mml:mo>|</mml:mo></mml:mrow><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>The two largest sources of uncertainties in the retrievals are the
pressure–altitude relationship (red line) and errors in pointing of
the satellite (cyan line). The reason for this is that the weighting
function for a change in water vapour is similar to the weighting
function from the changing of the pointing angle of the satellite, or
from a change in ambient pressure at different altitudes. Since the
water vapour line is dominated by Doppler (compared to pressure-)
broadening at the observed altitudes, and the number density of
molecules decrease exponentially with altitude, any pointing error (or
errors in altitude of the HSE reference point) will give rise to
a large-scale change in the retrieved water vapour mixing ratio, and
vice versa. The errors arising from assuming the wrong altitude of the
2.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula> pressure level can be adjusted for by ensuring that
comparisons to other instruments or models are done with respect to
a common pressure vs. altitude profile, in effect comparing number
density- rather than mixing ratio profiles. If this is done, the
estimated systematic error from this uncertainty is lowered to
<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula>2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula> (red-dashed curve in
Fig. <xref ref-type="fig" rid="Ch1.F11"/>).</p>
      <p>The uncertainties from the two aforementioned errors
(<italic>Pointing</italic> and <italic>Pressure</italic>) are however highly
correlated across each orbit and will mainly affect the mean water
vapour field retrieved in each orbit, and not the variations around
this field. For these variations the other systematic errors will
dominate, and  these are of the order of 0.5 ppmv. Thus
the measurements can reliably retrieve small-scale variations,
despite the poor accuracy of the mean field. It should also be noted
that the systematic errors introduced from the pointing and pressure
uncertainties do not necessarily lead to a bias as both errors may
vary across the measurement period.</p>
</sec>
<sec id="Ch1.S5.SS3">
  <title>Comparison with other measurements</title>
      <p>As a final test of the ability of the observations to retrieve water
vapour and temperature, the results are compared to measurements from
other satellite instruments. The solar occulting instruments
Atmospheric Chemistry Experiment-Fourier Transform Spectrometer
(ACE-FTS) on board the SCISAT satellite <xref ref-type="bibr" rid="bib1.bibx2" id="paren.44"/>
and Solar Occultation for Ice Experiment (SOFIE) on board the AIM
satellite <xref ref-type="bibr" rid="bib1.bibx37" id="paren.45"/> provide water vapour and
temperature measurements with high vertical resolution in the area
covered by the tomographic retrievals during the time period of the
tomographic measurements.</p>
      <p>ACE-FTS is a Fourier transform spectrometer which measures solar
radiation between 750–4400 <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="normal">cm</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and retrieves water vapour
and temperature profiles <xref ref-type="bibr" rid="bib1.bibx3" id="paren.46"/> between 5–90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>
with an altitude resolution of 3–4 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> and a precision of
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>300</mml:mn></mml:mrow></mml:math></inline-formula> ppbv for water vapour <xref ref-type="bibr" rid="bib1.bibx4" id="paren.47"><named-content content-type="pre">statistical fitting error and
“form-factor” error </named-content></xref> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula> K for
temperature <xref ref-type="bibr" rid="bib1.bibx41" id="paren.48"><named-content content-type="pre">comparison to LIDAR</named-content></xref>. In this study
we use version 3.0 of the water vapour data
<xref ref-type="bibr" rid="bib1.bibx4" id="paren.49"/>, which provides data during July 2010 in
the time period covered by tomographic retrievals.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F12" specific-use="star"><caption><p><bold>(a)</bold> Water vapour profiles from orbit 51226 at
68<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, 81<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E (dashed lines) and 68<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N,
63<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> W (solid lines) from SMR (blue), with collocated
ACE-FTS (red) and SOFIE (green) measurements. <bold>(b)</bold> The
corresponding temperature profiles.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f12.pdf"/>

        </fig>

      <p>SOFIE uses differential absorption spectroscopy at 11 different
wavelengths between 0.292 to 5.316 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> to determine the
temperature and the atmospheric composition. It retrieves water vapour
and temperature between 20 and 95 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> with a vertical resolution
of 1–2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>.  The precision for water vapour is estimated to be
better than 0.2 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula> across the mesopause
<xref ref-type="bibr" rid="bib1.bibx33" id="paren.50"/>, and for temperature the precision is
estimated to 0.1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> at 80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> increasing up to
0.5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> at 95 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx43" id="paren.51"/>. In this
study we use version 1.2 of the data which covers the entire time
period of the tomographic Odin measurements.</p>
      <p>The measurements are collocated by finding the retrieved SMR profile
at the latitude of ACE-FTS/SOFIE measurements and comparing it to the
closest (spatially) ACE-FTS/SOFIE during the same day. Due to the
different orbits of the satellites there is some distance between the
collocated measurements, but 90 % of the collocations are within
350 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. This means that some differences between the profiles
due to natural variability should be expected. Another reason for
discrepancies between the measurements is that, while SOFIE and
ACE-FTS perform measurements at <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 23:00 and
<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 01:00 LT due to their solar
occultation technique, SMR measurements are performed around
17:00 LT. Furthermore, the occultation measurements are made
perpendicular to the orbit, i.e. east–west, while SMR measures along
the orbit, i.e. north–south. The differences due to sampling different
air, however, should largely average out (except possible diurnal
variations) when comparing data over the entire PMC season.</p>
      <p>The result from SMR orbit 51226 (15 July 2010) is compared to
AIM-SOFIE and ACE-FTS in Fig. <xref ref-type="fig" rid="Ch1.F12"/>. The position of
the collocations are showed by the vertical black lines in
Fig. <xref ref-type="fig" rid="Ch1.F7"/>. The solid and dashed lines in
Fig. <xref ref-type="fig" rid="Ch1.F12"/> are the collocations at <inline-formula><mml:math display="inline"><mml:mrow><mml:mtext>AAO</mml:mtext><mml:mo>=</mml:mo><mml:msup><mml:mn>70</mml:mn><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mtext>AAO</mml:mtext><mml:mo>=</mml:mo><mml:msup><mml:mn>110</mml:mn><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> respectively. The data
from the three instruments are interpolated onto a common altitude
grid for intercomparison to minimise the effect of the retrieved
pressure differences between the instruments.
For water vapour the agreement between the instruments is good, but SMR seems to
show too low values below 80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. The retrieved temperature of the
three instruments have larger differences above 85 km. For the profile measured at
63<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> W (dashed lines) SMR and ACE-FTS places the mesopause at the
same altitude (90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), while the profile from SOFIE shows
the mesopause at 86 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. SMR does however measure
a significantly lower mesopause temperature (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:mn>130</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>) than
the two other instruments. At 81<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E (solid lines), SMR
places the mesopause at a higher altitude than both ACE-FTS and SOFIE.
These differences
might be, as previously mentioned, due to different sampling
time/location. In conclusion, the comparison of the single measurement
points show that the tomographic measurements successfully can
retrieve water vapour and temperature structures in the area of
interest.</p>
      <p>To look at the systematic errors in the tomographic retrievals, the
mean of all measurements collocated with SOFIE is analysed. A total of
198 collocations are investigated, and
Fig. 13a and b show the result of this comparison
with respect to each of the two frequency modes of SMR. The
measurements using mode 19 show a low bias compared to SOFIE in both
water vapour (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn>0.5</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">ppmv</mml:mi></mml:math></inline-formula>) and temperature (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn>15</mml:mn></mml:mrow></mml:math></inline-formula> K).
The estimated accuracy of SOFIE is <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> %<inline-formula><mml:math display="inline"><mml:mo>/</mml:mo></mml:math></inline-formula>0.8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> at 80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> and
15 %<inline-formula><mml:math display="inline"><mml:mo>/</mml:mo></mml:math></inline-formula>9.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> at 95 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> for water vapour
<xref ref-type="bibr" rid="bib1.bibx33" id="paren.52"/> and temperature
<xref ref-type="bibr" rid="bib1.bibx43" id="paren.53"/> respectively. Taking this into account
the agreement between SMR and SOFIE is good for mode 13, but not for
mode 19. Above 85 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> a large difference in mean temperature
can be seen (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn>30</mml:mn></mml:mrow></mml:math></inline-formula> K). This is partially explained by a known high bias in
SOFIE <xref ref-type="bibr" rid="bib1.bibx43" id="paren.54"/>. However, comparing SMR and ACE-FTS for
July 2010 (not shown), a similar, albeit smaller (5 K), cold bias is
seen above 85 km, and SMR places the mesopause about 2 km higher than ACE-FTS.
Thus, we cannot rule out the possibility of a cold bias of <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 5 K above 85 km
even in the frequency mode 13 measurements, though these differences are within
combined accuracy of the two instruments.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F13" specific-use="star"><caption><p>Mean water vapour <bold>(a)</bold> and temperature <bold>(b)</bold>
profiles from SMR (blue) and collocated SOFIE measurements
(green). The measurements where SMR is operating in
frequency mode 19/13 are given by
the dashed and solid lines respectively. Mean water vapour <bold>(c)</bold>
and temperature <bold>(d)</bold> profiles from SMR
(solid) and collocated SOFIE measurements (dashed) for June
(blue), July (green) and August (red). For <bold>(c)</bold> and <bold>(d)</bold>
only measurements using frequency mode 13 are considered.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f13.pdf"/>

        </fig>

      <p>The comparison of the mean profiles can be extended by looking at the
mean profile from each month for SOFIE and
SMR. Figure 11c shows the mean water
vapour profiles from both instruments for June, July and August
averaged over 2010 and 2011. Only the collocations from the frequency
mode 13 measurements are used. In June, SOFIE (blue-dashed line) shows
a higher water vapour concentration below 82 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> than SMR (blue
line), while in August (red lines) the reverse is true. The reason for
the larger seasonal variation in water vapour in SMR is unknown, but
it could be linked to systematic errors in the pressure a priori used
for the retrievals. The mean temperature
(Fig. 13d) is very similar for both SMR
and SOFIE for June and July, while for August SOFIE retrieves a much
higher mesopause temperature (155 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>) compared to SMR
(140 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>).</p>
      <p>It should be noted that the measured water vapour mixing ratios are
first converted to number density, before they are rescaled using
a common pressure and temperature profile during the comparisons. This
means that in principle number density profiles are compared rather
than mixing ratios. Doing this mitigates errors arising from the lack
of pressure information in the SMR measurements.</p>
      <p>In conclusion, the overall  agreement between the SMR tomographic
measurements and the two solar occulting instruments are within the
accuracy estimations from Sect. <xref ref-type="sec" rid="Ch1.S5.SS2"/> for the measurements
made with frequency mode 13. For the measurements made with mode 19
however there is a clear systematic low bias in both water vapour and
temperature. The measurements from SMR also show a larger seasonal
variance of water vapour, with lower concentrations than SOFIE in June
and higher concentrations in August.</p>
</sec>
<sec id="Ch1.S5.SS4">
  <title>Comparison to OSIRIS</title>
      <p>As previously mentioned, one of the reason for doing the tomographic
SMR measurements is that measurements by OSIRIS are able to retrieve
PMC coverage at the same time. Figure <xref ref-type="fig" rid="Ch1.F14"/> shows
some example results combining measurements from both
instruments. The left panels show the water vapour distribution around
PMCs from two different orbits recorded on 15 July 2010. The white
contours show the volume scattering coefficient from the PMCs measured
by OSIRIS. The most striking feature is the strong depletion of water
vapour above the clouds. This is seen particularly well above each of
the three cloudy areas at 80, 90 and 100<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO in Fig. 14c. At
82 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, there are areas with higher water vapour concentrations
between the clouds, indicating possible cloud deposition. In Fig. 14a
the water vapour is concentrated in a single area at 80<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>
AAO. The reason for this feature cannot be explained by looking at the
cloud distribution alone, but probably arises as a combination of air
movement as well as cloud formation and particle sedimentation.</p>
      <p>The atmospheric temperatures are shown in the rightmost panels in
Fig. <xref ref-type="fig" rid="Ch1.F14"/>. In general, the existence of clouds
seem to correlate with the cold areas at 82 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. In particular
the warmer area seen at 90–100<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> AAO in
Fig. 14d has a noticeable lack of clouds
compared to the areas around it. This fits well with the water
vapour analysis, indicating that this as a possible area of PMC
sublimation. In some areas, however, the clouds penetrate into areas of
higher temperature (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn>150</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula>); explaining these
intrusions requires further analysis taking into account both cloud
microphysics and the dynamics of the atmosphere.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F14" specific-use="star"><caption><p>Water vapour (left column) and temperature (right column)
fields from two orbits 15 July 2010. The white contours show the
volume scattering coefficient from OSIRIS, where each contour
corresponds to <inline-formula><mml:math display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">9</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><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:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">str</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
150 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">K</mml:mi></mml:math></inline-formula> temperature contour is given by the black line in
the temperature panels. The lower <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>-axis shows the AAO and the
top axis shows the true latitude of the measurements.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/8/1981/2015/amt-8-1981-2015-f14.pdf"/>

        </fig>

</sec>
</sec>
<sec id="Ch1.S6" sec-type="conclusions">
  <title>Conclusions</title>
      <p>Water vapour and temperature have been measured around PMC by several
ground- and satellite-based instruments in the past, but until now,
simultaneous measurements of water vapour, temperature and PMC with
a large geographical coverage and relatively good vertical and
horizontal resolution have not existed. During the arctic summers of
2010 and 2011 the Odin satellite made a set of measurements with
both Odin-SMR and Odin-OSIRIS to obtain such data.</p>
      <p>In this paper we present the measurements of water vapour and
temperature carried out by the SMR instrument. A tomographic retrieval
approach based on the optimal estimation method is applied, and is
described in detail. An error analysis was performed to investigate
possible sources of errors in the retrieved data, and the data were
compared to two other satellite instruments for quality assurance.</p>
      <p>The largest source of errors in the data comes from the uncertainty in
the satellite pointing and the altitude of the 2.9 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Pa</mml:mi></mml:math></inline-formula> pressure
level, which is used as the reference level to adjust the atmosphere
to remain in HSE. These large uncertainties indicate that the
tomographic retrievals have limited capability to retrieve the mean
water vapour mixing ratio for each orbit. However, the retrieved
variations of water vapour around this mean are significantly less
affected by these errors, and can be retrieved by the measurements with
reasonable accuracy.</p>
      <p>Inspecting the retrievals corresponding to the different frequency modes
of SMR revealed discrepancies between measurements done using frequency mode 19 and 13.
By comparing the results to collocated AIM-SOFIE measurements, we
conclude that the best results are achieved with the frequency mode 13
measurements, which had the lowest systematic differences compared to
AIM-SOFIE of the two modes. A larger seasonal variation in water
vapour was found in SMR compared to AIM-SOFIE. The reason for
these systematic differences is not clear, but it is probably a combination of
errors in the modelling of the SMR instrument, and errors in
the assumptions about the forward model atmosphere. The differences
between the measurements are within our estimated
systematic uncertainty for the tomographic measurements.<?xmltex \hack{\newpage}?></p>
      <p>Despite these uncertainties, the SMR tomographic measurements provide
a unique and useful complement to existing data sets. As an example of
the capabilities of the measurements, we compared the retrieved
atmosphere to PMC extinction coefficients measured by OSIRIS for two
of the recorded orbits. The results from the two instruments showed
both depletion and enhancement of water vapour around the clouds as
well as larger-scale horizontal variation in both water vapour and
temperature. To explain the complete water vapour and temperature
fields of the background atmosphere requires a more thorough analysis,
taking into account both cloud microphysics as well as atmospheric
dynamics. Future plans include using the data set to evaluate
atmospheric and cloud models, and thus improve our understanding of
PMCs and their effect on and response to the background atmosphere
under which they form.</p>
</sec>

      
      </body>
    <back><ack><title>Acknowledgements</title><p>We would like to thank Kaley Walker and the ACE-FTS/SCISAT team as
well as Mark Hervig and the SOFIE/AIM team for providing satellite
data of water vapour and temperature for comparison. The Atmospheric
Chemistry Experiment (ACE), also known as SCISAT, is
a Canadian-led mission mainly supported by the Canadian Space Agency
and the Natural Sciences and Engineering Research Council of Canada.</p><p>AIM/SOFIE is funded by NASA's Small Explorers Program.  The SOFIE
v1.2 data used in this work are available online at
<uri>sofie.gats-inc.com</uri>.</p><p>Odin is a Swedish-led satellite project funded jointly by the
Swedish National Space Board (SNSB), the Canadian Space Agency
(CSA), the National Technology Agency of Finland (Tekes), the Centre
National d'études Spatiales (CNES) in France and the European
Space Agency (ESA).</p><p>Finally we would like to thank the Associate Editor Thomas von Clarmann
and the two anonymous referees for their comments and suggestions which
certainly helped improving the quality of both the paper and
the results presented herein.<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>
Edited by: T. von Clarmann</p></ack><ref-list>
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