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<article xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:oasis="http://docs.oasis-open.org/ns/oasis-exchange/table" dtd-version="3.0"><?xmltex \makeatother\@nolinetrue\makeatletter?>
  <front>
    <journal-meta>
<journal-id journal-id-type="publisher">TC</journal-id>
<journal-title-group>
<journal-title>The Cryosphere</journal-title>
<abbrev-journal-title abbrev-type="publisher">TC</abbrev-journal-title>
<abbrev-journal-title abbrev-type="nlm-ta">The Cryosphere</abbrev-journal-title>
</journal-title-group>
<issn pub-type="epub">1994-0424</issn>
<publisher><publisher-name>Copernicus Publications</publisher-name>
<publisher-loc>Göttingen, Germany</publisher-loc>
</publisher>
</journal-meta>

    <article-meta>
      <article-id pub-id-type="doi">10.5194/tc-11-1111-2017</article-id><title-group><article-title>Validation of satellite altimetry by kinematic GNSS <?xmltex \hack{\newline}?> in central East Antarctica</article-title>
      </title-group><?xmltex \runningtitle{Validation of satellite altimetry by kinematic GNSS in central East Antarctica}?><?xmltex \runningauthor{L.~Schr\"{o}der et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Schröder</surname><given-names>Ludwig</given-names></name>
          <email>ludwig.schroeder@tu-dresden.de</email>
        <ext-link>https://orcid.org/0000-0002-6862-0930</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Richter</surname><given-names>Andreas</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Fedorov</surname><given-names>Denis V.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0003-3282-3178</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Eberlein</surname><given-names>Lutz</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Brovkov</surname><given-names>Evgeny V.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff3">
          <name><surname>Popov</surname><given-names>Sergey V.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Knöfel</surname><given-names>Christoph</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Horwath</surname><given-names>Martin</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-5797-244X</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Dietrich</surname><given-names>Reinhard</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Matveev</surname><given-names>Alexey Y.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Scheinert</surname><given-names>Mirko</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff4">
          <name><surname>Lukin</surname><given-names>Valery V.</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>Technische Universität Dresden, Institut für Planetare Geodäsie, Dresden, Germany</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>OAO Aerogeodeziya, St. Petersburg, Russia</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>Polar Marine Geosurvey Expedition (PMGE), St. Petersburg, Russia</institution>
        </aff>
        <aff id="aff4"><label>4</label><institution>Arctic and Antarctic Research Institute (AARI), St. Petersburg, Russia</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Ludwig Schröder (ludwig.schroeder@tu-dresden.de)</corresp></author-notes><pub-date><day>5</day><month>May</month><year>2017</year></pub-date>
      
      <volume>11</volume>
      <issue>3</issue>
      <fpage>1111</fpage><lpage>1130</lpage>
      <history>
        <date date-type="received"><day>7</day><month>December</month><year>2016</year></date>
           <date date-type="rev-request"><day>3</day><month>January</month><year>2017</year></date>
           <date date-type="rev-recd"><day>6</day><month>April</month><year>2017</year></date>
           <date date-type="accepted"><day>7</day><month>April</month><year>2017</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://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017.html">This article is available from https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017.html</self-uri>
<self-uri xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017.pdf">The full text article is available as a PDF file from https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017.pdf</self-uri>


      <abstract>
    <p>Ice-surface elevation profiles of more than 30 000 km in total length are
derived from kinematic GNSS (GPS and the Russian GLONASS) observations on
sledge convoy vehicles along traverses between Vostok Station and the East
Antarctic coast. These profiles have accuracies between 4 and 9 cm. They are
used to validate elevation data sets from both radar and laser satellite
altimetry as well as four digital elevation models. A crossover analysis with
three different processing versions of Envisat radar altimetry elevation
profiles yields a clear preference for the relocation method over the direct
method of slope correction and for threshold retrackers over functional fit
algorithms. The validation of CryoSat-2 low-resolution mode and SARIn mode
data sets documents the progress made from baseline B to C elevation
products. ICESat laser altimetry data are demonstrated to be accurate to a
few decimetres over a wide range of surface slopes. A crossover adjustment in
the region of subglacial Lake Vostok combining ICESat elevation data with our
GNSS profiles yields a new set of ICESat laser campaign biases and provides
new, independent evidence for the stability of the ice-surface elevation
above the lake. The evaluation of the digital elevation models reveals the
benefits of combining laser and radar altimetry.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

      <?xmltex \hack{\newpage}?>
<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>Surface elevation data are crucial for a broad range of applications in polar
sciences. Only satellite altimetry is able to provide this information with a
high and nearly uniform accuracy and precision for almost the entire
Antarctic ice sheet. This high accuracy also allows us to infer temporal changes
in ice surface elevation, which is of prime scientific interest in the
context of ongoing climate change <xref ref-type="bibr" rid="bib1.bibx55 bib1.bibx23" id="paren.1"/>. However,
systematic effects (as varying surface properties or measurement biases) can
deteriorate the derived elevation trend <inline-formula><mml:math id="M1" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> and – if not corrected
thoroughly – they might lead to misinterpretation of the observations
<xref ref-type="bibr" rid="bib1.bibx1 bib1.bibx30" id="paren.2"/>.</p>
      <p>One crucial step in the processing of surface elevations from satellite radar
altimetry (SRA) over ice sheets is the slope correction <xref ref-type="bibr" rid="bib1.bibx5" id="paren.3"/>.
Due to the size of the beam-limited footprint of about 20 km in diameter the
first reflection can originate from a location up to several kilometres away
from the nadir point in a sloping surface. Different approaches exist to
correct for this effect <xref ref-type="bibr" rid="bib1.bibx2 bib1.bibx49" id="paren.4"><named-content content-type="pre">e.g.</named-content></xref> but, as the
corrections can exceed 100 m <xref ref-type="bibr" rid="bib1.bibx6" id="paren.5"/>, remaining model errors
may introduce height errors of up to several metres. This is the major factor
limiting the application of SRA in the steep and rugged coastal areas
<xref ref-type="bibr" rid="bib1.bibx18" id="paren.6"/>. <?xmltex \hack{\newpage}?></p>
      <p>Another issue when deriving ice-surface elevations from SRA data is the
penetration of the microwave signal into the upper firn layers. This results
in a mixed return signal consisting of surface reflection and volume
reflection <xref ref-type="bibr" rid="bib1.bibx47" id="paren.7"/>. Here, the selection of an appropriate
retracking algorithm is essential. One approach to minimize the influence of
the volume echo on the observed surface elevations is to retrack at the very
beginning of the waveform <xref ref-type="bibr" rid="bib1.bibx11" id="paren.8"/>. Another method is to apply
appropriate corrections using parameters of the radar waveform shape
<xref ref-type="bibr" rid="bib1.bibx62 bib1.bibx18 bib1.bibx67" id="paren.9"/>.</p>
      <p>For the Ice Cloud and land Elevation Satellite (ICESat) mission the effects
of topographic correction and signal penetration do not arise or are
negligible as the on-board altimeter uses laser signals. Hence, significantly
higher accuracies can be achieved. Nonetheless, those measurements are also
not free of systematic errors. Pointing errors and orbital variations
<xref ref-type="bibr" rid="bib1.bibx32" id="paren.10"/> or saturation effects <xref ref-type="bibr" rid="bib1.bibx51" id="paren.11"/> may cause
laser campaign biases which induce spurious trends of up to 2 cm yr<inline-formula><mml:math id="M2" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx27 bib1.bibx25" id="paren.12"/> and introduce errors of more than
100 Gt yr<inline-formula><mml:math id="M3" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in mass balance estimates <xref ref-type="bibr" rid="bib1.bibx27" id="paren.13"/>.</p>
      <p>In order to quantify the impact of these errors and to evaluate methods for
their correction, independent elevation data of high precision and accuracy
is crucial. Here, we make use of ice-surface elevation profiles in central
East Antarctica comprising more than 30 000 km in total length. These
profiles are observed with kinematic GNSS (Global Navigation Satellite
System, which means the Global Positioning System (GPS) and the Russian
Global Navigation Satellite System (GLONASS) in this case) carried out over
more than one decade on sledge convoy vehicles along continental traverses.</p>
</sec>
<sec id="Ch1.S2">
  <title>Surface elevations from kinematic GNSS profiles</title>
<sec id="Ch1.S2.SS1">
  <title>Kinematic GNSS observations</title>
      <p>The Russian research station Vostok is located in the central part of East
Antarctica (106.8<inline-formula><mml:math id="M4" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E, 78.5<inline-formula><mml:math id="M5" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S). It is the main base for a
wide range of scientific fieldwork related to the subglacial Lake Vostok.
Between 2001 and 2015 several kinematic GNSS profiles have been measured in
the area of the lake as well as on the scientific traverses from Vostok
Station to the East Antarctic coast.</p>
      <p>Geodetic dual-frequency GNSS receivers with external antennas were used for
kinematic profiling as well as on the reference stations. Two different types
of profiles can be distinguished with respect to the vehicles onto which the
GNSS antennas were mounted. The first type are observations performed on
lightweight snowmobiles. With the help of such profiles <xref ref-type="bibr" rid="bib1.bibx44" id="text.14"/>
have shown that the surface elevation around Vostok Station has been stable
over the last decade, confirming the results of permanent GNSS observations
<xref ref-type="bibr" rid="bib1.bibx42 bib1.bibx44" id="paren.15"/>. Such profiles acquired on snowmobiles
provide accuracies of only a few centimetres <xref ref-type="bibr" rid="bib1.bibx28 bib1.bibx57" id="paren.16"><named-content content-type="pre">see
also</named-content></xref> and
are thus well suited for precise studies on local elevation and elevation
changes. However, due to logistic reasons they usually cover only a very
limited area and are therefore not considered here.</p>
      <p>The second type of observations are carried out on heavy convoy vehicles.
Those are tractors on tracks, designed to pull sledges with containers for
accommodation and fuel tanks (Fig. <xref ref-type="fig" rid="Ch1.F1"/>). Hence, they
are ideal platforms for such measurements over very long distances. This is a
precondition for the validation of satellite altimetry on a larger scale, as
it helps to minimize the influence of regional peculiarities, especially due
to specific topographic conditions <xref ref-type="bibr" rid="bib1.bibx29" id="paren.17"/>. The disadvantage of
such heavy platforms, compared to snowmobiles, is that they sink into the
soft upper snow layers up to several decimetres. The amount of the vehicle's
subsidence, and thus of the height of the antenna above the snow surface,
varies locally. Therefore, this antenna height has to be measured as often as
possible along the traverse.</p>
      <p>In the austral summer 2001/2002, our first surface elevation profile was
acquired during a seismic convoy of the Russian Antarctic Expedition (RAE)
along a 150 km transect in the southern part of Lake Vostok. During this
traverse over 6 days a GNSS antenna was installed on the roof of a trailer,
pulled by a traverse vehicle.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><caption><p><bold>(a)</bold> Overview of the kinematic GNSS profiles (colour coded
by their chronological sequence) and the GNSS reference stations used in the
differential processing. <bold>(b)</bold> Detailed map of the profiles in the
area of subglacial Lake Vostok (outline in grey, hydrostatic equilibrium area
in black). <bold>(c)</bold> Convoy vehicle of type STT-2 Kharkovchanka-2 (profile
K10B) with antenna mounted on the container above the cabin (red circle).
<bold>(d)</bold> Convoy vehicles Kässbohrer PistenBully (profiles K14A and
K14B) with antenna mounted on top of the cabins. </p></caption>
          <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f01.pdf"/>

        </fig>

      <p>Starting from 2006, significantly longer profiles have been measured. In that
time Mirny Station (93.0<inline-formula><mml:math id="M6" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E, 66.6<inline-formula><mml:math id="M7" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S) was the coastal
logistical hub for the supply of Vostok Station by overland traverses.
Several scientific observations were performed during these convoys
<xref ref-type="bibr" rid="bib1.bibx34 bib1.bibx43 bib1.bibx39 bib1.bibx15" id="paren.18"/>. In the austral
summer 2006/2007 kinematic GNSS profiles between Vostok and Mirny were
observed on two convoy vehicles. For the first time these profiles cover the
entire distance of about 1600 km, from the remarkably flat ice surface above
Lake Vostok down to the rugged terrain at the coast. In the following season
these profiles were repeated on two vehicles.</p>
      <p>In 2009, Progress Station (76.4<inline-formula><mml:math id="M8" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E, 69.4<inline-formula><mml:math id="M9" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S) became the main logistic hub for
Vostok Station. Further, an initial reconnaissance traverse from Progress to
Vostok and back was performed in 2007/2008 that already included geodetic
GNSS-equipment. Since austral summer 2009/2010, several profiles between
these two stations were measured each season. A number of different routes
were used according to the needs of the participating scientific groups, snow
conditions or logistical constraints. Figure <xref ref-type="fig" rid="Ch1.F1"/>
gives an overview of the locations and timing of the routes as well as two
examples of the types of vehicles used. Table <xref ref-type="table" rid="Ch1.T1"/> contains
detailed information about each individual profile.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <title>GNSS data processing</title>
      <p>We used the Bernese GNSS Software 5.2 <xref ref-type="bibr" rid="bib1.bibx10" id="paren.19"/> for the differential
post-processing of the kinematic observation data. In such remote locations,
other studies <xref ref-type="bibr" rid="bib1.bibx57 bib1.bibx29" id="paren.20"/> used the precise point
positioning (PPP) technique, which does not require reference stations.
However, PPP depends on precise high-rate satellite clock information, which
is not available for our early campaigns. <xref ref-type="bibr" rid="bib1.bibx22" id="text.21"/> showed that both
techniques are able to reach very high accuracies (<inline-formula><mml:math id="M10" display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 3 cm) for very
long distances to reference stations. The processing provides a 3-D
coordinate of the GNSS antenna for each observational epoch in the
terrestrial reference frame IGS08. Using those coordinates, a profile of
ellipsoidal elevations referenced to WGS-84 is derived. For many of the
profiles multi-system GNSS receivers were used; i.e. observations from the
Russian GLONASS are logged in addition to GPS. The increased amount of
observations improves the reliability of the solution significantly. As
kinematic reference sites in this differential positioning we utilized static
observations from campaign sites, for example in Mirny or Progress, from an
own permanent receiver in Vostok installed in early 2008 <xref ref-type="bibr" rid="bib1.bibx44" id="paren.22"><named-content content-type="pre">for details
see</named-content></xref> and additionally from the sites Casey and Davis of the
IGS-network (see Fig. <xref ref-type="fig" rid="Ch1.F1"/>). To cope with the scarce 30 s
sampling interval of the IGS-sites, those static observations had to
be interpolated to the rate of the kinematic receivers (mainly 5 or 15 s,
sf. Table <xref ref-type="table" rid="Ch1.T1"/>). For that purpose we used WaSoft, a
software tool developed by <xref ref-type="bibr" rid="bib1.bibx60" id="text.23"/>. We adopt the processing
strategy of <xref ref-type="bibr" rid="bib1.bibx21" id="text.24"/>, which corrects or parameterizes the
tropospheric and ionospheric delay, the antenna phase centre offsets and
variations, solid earth tides and loading displacements. Special attention is
paid to the resolution of the GNSS carrier phase ambiguities of the
differenced observations. When the vehicle is halfway between Vostok and the
coast, no baseline to a static reference station is shorter than 800 km.
Then, only very robust ambiguity resolution strategies are able to produce
satisfactory results. Therefore, in this case we used the Melbourne–Wübbena
and the quasi-ionosphere-free linear combination only <xref ref-type="bibr" rid="bib1.bibx10" id="paren.25"/>. As
this is the most critical step in processing, a thorough outlier screening of
the fixed ambiguity solutions is essential. For this reason, we always used
more than one, but typically four to five, baselines to different reference
sites. Undetected cycle slips lead to very large deviations of the affected
baseline. Thus, by processing each baseline independently and comparing the
results to the combined solution, the baseline causing large deviations can
be identified and the undetected cycle slip has to be introduced manually.</p>
</sec>
<sec id="Ch1.S2.SS3">
  <title>Derivation of surface elevation profiles</title>
      <p>The antenna trajectory resulting from the GNSS positioning has to be
corrected for the height of the antenna above the local snow surface in order
to derive surface elevation profiles. This vertical offset is not constant as
the amount to which the vehicle sinks into the snow depends on the regionally
varying surface snow properties, but also on the vehicle type (e.g. track
width). For example, <xref ref-type="bibr" rid="bib1.bibx29" id="text.26"/> had to employ additional laser
measurements on another vehicle in order to retrieve the amount of vehicle
subsidence because the antenna height was not measured repeatedly along their
profiles. During our traverses we measured this antenna height offset AH
several times for each observation day and for each profile. However, the
representativity of a single offset measurement may still be limited due to
small-scale surface structures (sastrugi) at the locations of the
measurements. Thus, to obtain a specific offset for each single epoch <inline-formula><mml:math id="M11" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>, we
use a regional average
            <disp-formula id="Ch1.E1" content-type="numbered"><mml:math id="M12" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="normal">AH</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mo>∑</mml:mo><mml:mi>j</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msubsup><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><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="normal">AH</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mo>∑</mml:mo><mml:mi>j</mml:mi></mml:msub><mml:msubsup><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math id="M13" display="inline"><mml:mrow><mml:msubsup><mml:mi>d</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:math></inline-formula> is the inverse distance between the position at epoch <inline-formula><mml:math id="M14" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula>
and the position of the antenna height measurement AH<inline-formula><mml:math id="M15" display="inline"><mml:msub><mml:mi/><mml:mi>j</mml:mi></mml:msub></mml:math></inline-formula>. The offset of
profile K08C was measured only once. Here we model the subsidence from
similar profiles with comparable vehicles.</p>
      <p>Furthermore, a permanent tilt of the moving vehicles had to be considered.
While driving in soft snow, especially when pulling heavy sledges, the nose
of the vehicle gets lifted up while the rear buries deeper. This dynamic
effect is not determined directly as our offset measurements are taken during
stops when the vehicle stands upright. However, an instantaneous jump in
antenna elevation from GNSS positioning is observed whenever the vehicle
stops. Depending on the antenna's position on the vehicle, it can reach
20 cm. These jumps are used to correct the measurement AH for the vehicle
dynamics. For this purpose we interpolate the <italic>elevations in movement</italic> (i.e.
velocity <inline-formula><mml:math id="M16" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 1 km h<inline-formula><mml:math id="M17" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) to the position of the antenna height
measurement by fitting a quadratic function within a distance of 100 m
around this point and comparing it to the average <italic>elevation in rest</italic>.</p>
      <p>To reduce the noise and the influence of sastrugi, we applied a low-pass
filter to the original antenna trajectory. Depending on the sampling interval
(Table <xref ref-type="table" rid="Ch1.T1"/>) and the velocity of the vehicles (about
7 km h<inline-formula><mml:math id="M18" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>), the usual point distance is in the range of 10 to 30 m. We
applied a Gaussian filter with a Gaussian sigma of 60 m and a total length
of 180 m. In addition, the trajectory positions are thinned out to an
equidistant interval of 30 m. This substantially reduces the data amount
(e.g. when data were logged during overnight stops of the convoy) without loss
of information.</p>
      <p>A comparison between kinematic GNSS profiles and satellite altimetry products
requires consistency in the reference system used <xref ref-type="bibr" rid="bib1.bibx28" id="paren.27"/>. ICESat
<xref ref-type="bibr" rid="bib1.bibx53" id="paren.28"/> and CryoSat-2 <xref ref-type="bibr" rid="bib1.bibx52" id="paren.29"/> refer to ITRF08. This
is identical to IGS08 within sub-millimetre level <xref ref-type="bibr" rid="bib1.bibx41" id="paren.30"/>.
Envisat GDR-C orbits refer to ITRF05 <xref ref-type="bibr" rid="bib1.bibx9" id="paren.31"/> but as this affects
the differences in the order of some millimetres only
<xref ref-type="bibr" rid="bib1.bibx41" id="paren.32"/>, it is considered negligible here, too. However, the
treatment of the permanent tide in the reference systems underlying both
techniques has a significant influence here. According to
<?xmltex \hack{\mbox\bgroup}?><xref ref-type="bibr" rid="bib1.bibx35" id="text.33"/><?xmltex \hack{\egroup}?> the International Terrestrial Reference Frame
(ITRF) and consequently IGS08, is a conventional tide-free frame. Hence, all
tidal effects including the permanent effect have been removed from the
coordinates of the reference stations. Our elevation profiles are henceforth
also conventional tide free. Altimetric elevations, in contrast, refer to the
mean tide system. The GNSS elevations are converted to this mean tide system
using Eq. (7.14a) of <xref ref-type="bibr" rid="bib1.bibx38" id="text.34"/>, which is a function of latitude and
amounts to about <inline-formula><mml:math id="M19" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>10 cm at 70<inline-formula><mml:math id="M20" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S.</p>
</sec>
<sec id="Ch1.S2.SS4">
  <title>Accuracy and precision</title>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1" specific-use="star"><caption><p>Overview of the kinematic GNSS profiles. Estimates of precision
consist of the mean elevation error from GNSS processing (from differences
between combined and single baseline solutions)
<inline-formula><mml:math id="M21" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">BL</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> and the obtained mean formal precision of snow surface elevation <inline-formula><mml:math id="M22" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">S</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>.
The empirical mean crossover difference between independent profiles of one season <inline-formula><mml:math id="M23" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> gives an estimate for the accuracy.
Averages and (in case of more than one) the standard deviation of the crossover differences with Operation ICEBridge ATM at 26 November 2013 is given in the last column.
Duration dates are given as yyyy-mm-dd.
</p></caption><oasis:table frame="topbot"><?xmltex \begin{scaleboxenv}{.95}[.95]?><oasis:tgroup cols="10">
     <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="center"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right"/>
     <oasis:colspec colnum="7" colname="col7" align="right"/>
     <oasis:colspec colnum="8" colname="col8" align="right"/>
     <oasis:colspec colnum="9" colname="col9" align="right"/>
     <oasis:colspec colnum="10" colname="col10" align="right"/>
     <oasis:thead>
       <oasis:row>  
         <oasis:entry colname="col1">Profile</oasis:entry>  
         <oasis:entry colname="col2">Vehicle</oasis:entry>  
         <oasis:entry colname="col3">Area of</oasis:entry>  
         <oasis:entry colname="col4">Duration</oasis:entry>  
         <oasis:entry colname="col5">Length</oasis:entry>  
         <oasis:entry colname="col6">Samp.</oasis:entry>  
         <oasis:entry colname="col7"><inline-formula><mml:math id="M26" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">BL</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col8"><inline-formula><mml:math id="M27" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">S</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col9"><inline-formula><mml:math id="M28" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col10"><inline-formula><mml:math id="M29" display="inline"><mml:mover accent="true"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>h</mml:mi><mml:mi mathvariant="normal">ATM</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1"/>  
         <oasis:entry colname="col2"/>  
         <oasis:entry colname="col3">operation<inline-formula><mml:math id="M30" display="inline"><mml:msup><mml:mi/><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5">[km]</oasis:entry>  
         <oasis:entry colname="col6">[s]<inline-formula><mml:math id="M31" display="inline"><mml:msup><mml:mi/><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col7">[cm]</oasis:entry>  
         <oasis:entry colname="col8">[cm]</oasis:entry>  
         <oasis:entry colname="col9">[cm]</oasis:entry>  
         <oasis:entry colname="col10">[cm]</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">K01A</oasis:entry>  
         <oasis:entry colname="col2">trailer (tracks)</oasis:entry>  
         <oasis:entry colname="col3">V</oasis:entry>  
         <oasis:entry colname="col4">2001-12-07–2001-12-12</oasis:entry>  
         <oasis:entry colname="col5">150</oasis:entry>  
         <oasis:entry colname="col6">30 (G)</oasis:entry>  
         <oasis:entry colname="col7">5.0</oasis:entry>  
         <oasis:entry colname="col8">5.0</oasis:entry>  
         <oasis:entry colname="col9">–</oasis:entry>  
         <oasis:entry colname="col10">10.3</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K07A</oasis:entry>  
         <oasis:entry colname="col2">Ishimbai</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M32" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> M</oasis:entry>  
         <oasis:entry colname="col4">2007-01-07–2007-03-05</oasis:entry>  
         <oasis:entry colname="col5">2280</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">3.8</oasis:entry>  
         <oasis:entry colname="col8">4.0</oasis:entry>  
         <oasis:entry colname="col9">8.0</oasis:entry>  
         <oasis:entry colname="col10">3.8 <inline-formula><mml:math id="M33" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 10.9</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K07B</oasis:entry>  
         <oasis:entry colname="col2">Ishimbai</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M34" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> M</oasis:entry>  
         <oasis:entry colname="col4">2007-01-09–2007-01-23</oasis:entry>  
         <oasis:entry colname="col5">580</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">2.9</oasis:entry>  
         <oasis:entry colname="col8">4.7</oasis:entry>  
         <oasis:entry colname="col9">6.4</oasis:entry>  
         <oasis:entry colname="col10">15.1 <inline-formula><mml:math id="M35" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 8.5</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K07C</oasis:entry>  
         <oasis:entry colname="col2">STT-1</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M36" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> M</oasis:entry>  
         <oasis:entry colname="col4">2007-02-04–2007-03-05</oasis:entry>  
         <oasis:entry colname="col5">1270</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">3.2</oasis:entry>  
         <oasis:entry colname="col8">3.8</oasis:entry>  
         <oasis:entry colname="col9">8.6</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K08A</oasis:entry>  
         <oasis:entry colname="col2">Ishimbai</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M37" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> M</oasis:entry>  
         <oasis:entry colname="col4">2008-01-11–2008-02-18</oasis:entry>  
         <oasis:entry colname="col5">1720</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">2.3</oasis:entry>  
         <oasis:entry colname="col8">2.5</oasis:entry>  
         <oasis:entry colname="col9">8.4</oasis:entry>  
         <oasis:entry colname="col10"><inline-formula><mml:math id="M38" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>7.2</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K08B</oasis:entry>  
         <oasis:entry colname="col2">ATT</oasis:entry>  
         <oasis:entry colname="col3">M</oasis:entry>  
         <oasis:entry colname="col4">2008-02-19–2008-03-13</oasis:entry>  
         <oasis:entry colname="col5">400</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">1.9</oasis:entry>  
         <oasis:entry colname="col8">2.8</oasis:entry>  
         <oasis:entry colname="col9">6.5</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K08C</oasis:entry>  
         <oasis:entry colname="col2">trailer (sledge)</oasis:entry>  
         <oasis:entry colname="col3">P <inline-formula><mml:math id="M39" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> V <inline-formula><mml:math id="M40" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2008-01-06 - 2008-02-07</oasis:entry>  
         <oasis:entry colname="col5">2890</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">1.5</oasis:entry>  
         <oasis:entry colname="col8">10.2</oasis:entry>  
         <oasis:entry colname="col9">–</oasis:entry>  
         <oasis:entry colname="col10">26.6 <inline-formula><mml:math id="M41" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 1.1</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K08D</oasis:entry>  
         <oasis:entry colname="col2">STT-2</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M42" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> M</oasis:entry>  
         <oasis:entry colname="col4">2008-02-08–2008-03-14</oasis:entry>  
         <oasis:entry colname="col5">1960</oasis:entry>  
         <oasis:entry colname="col6">5 (G)</oasis:entry>  
         <oasis:entry colname="col7">2.2</oasis:entry>  
         <oasis:entry colname="col8">2.5</oasis:entry>  
         <oasis:entry colname="col9">6.7</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K10A</oasis:entry>  
         <oasis:entry colname="col2">ATT</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M43" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2010-01-24–2010-03-18</oasis:entry>  
         <oasis:entry colname="col5">1690</oasis:entry>  
         <oasis:entry colname="col6">15 (G)</oasis:entry>  
         <oasis:entry colname="col7">1.6</oasis:entry>  
         <oasis:entry colname="col8">2.0</oasis:entry>  
         <oasis:entry colname="col9">6.1</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K10B</oasis:entry>  
         <oasis:entry colname="col2">STT-2</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M44" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2010-01-31-2010-03-15</oasis:entry>  
         <oasis:entry colname="col5">1460</oasis:entry>  
         <oasis:entry colname="col6">15 (G)</oasis:entry>  
         <oasis:entry colname="col7">2.2</oasis:entry>  
         <oasis:entry colname="col8">2.4</oasis:entry>  
         <oasis:entry colname="col9">6.1</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K11A</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">P <inline-formula><mml:math id="M45" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> V <inline-formula><mml:math id="M46" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2011-01-07–2011-02-08</oasis:entry>  
         <oasis:entry colname="col5">1690</oasis:entry>  
         <oasis:entry colname="col6">15 (G)</oasis:entry>  
         <oasis:entry colname="col7">1.7</oasis:entry>  
         <oasis:entry colname="col8">2.1</oasis:entry>  
         <oasis:entry colname="col9">4.3</oasis:entry>  
         <oasis:entry colname="col10">3.9 <inline-formula><mml:math id="M47" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 10.8</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K11B</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">P</oasis:entry>  
         <oasis:entry colname="col4">2011-02-13–2011-02-14</oasis:entry>  
         <oasis:entry colname="col5">80</oasis:entry>  
         <oasis:entry colname="col6">15 (C)</oasis:entry>  
         <oasis:entry colname="col7">1.5</oasis:entry>  
         <oasis:entry colname="col8">2.9</oasis:entry>  
         <oasis:entry colname="col9">4.3</oasis:entry>  
         <oasis:entry colname="col10">–</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K12A</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M48" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2012-01-25–2012-02-11</oasis:entry>  
         <oasis:entry colname="col5">1560</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.8</oasis:entry>  
         <oasis:entry colname="col8">3.0</oasis:entry>  
         <oasis:entry colname="col9">8.4</oasis:entry>  
         <oasis:entry colname="col10"><inline-formula><mml:math id="M49" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>5.8 <inline-formula><mml:math id="M50" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 11.0</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K12B</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M51" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2012-01-25–2012-02-11</oasis:entry>  
         <oasis:entry colname="col5">1560</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.2</oasis:entry>  
         <oasis:entry colname="col8">2.5</oasis:entry>  
         <oasis:entry colname="col9">8.4</oasis:entry>  
         <oasis:entry colname="col10">3.1 <inline-formula><mml:math id="M52" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 3.8</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K13A</oasis:entry>  
         <oasis:entry colname="col2">trailer (sledge)</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M53" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2013-01-20–2013-02-12</oasis:entry>  
         <oasis:entry colname="col5">2140</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.4</oasis:entry>  
         <oasis:entry colname="col8">2.6</oasis:entry>  
         <oasis:entry colname="col9">6.2</oasis:entry>  
         <oasis:entry colname="col10"><inline-formula><mml:math id="M54" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>4.0</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K13B</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M55" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2013-01-20–2013-02-15</oasis:entry>  
         <oasis:entry colname="col5">2220</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.2</oasis:entry>  
         <oasis:entry colname="col8">2.3</oasis:entry>  
         <oasis:entry colname="col9">6.2</oasis:entry>  
         <oasis:entry colname="col10"><inline-formula><mml:math id="M56" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.4</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K14A</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M57" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2014-01-22–2014-02-11</oasis:entry>  
         <oasis:entry colname="col5">1480</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.6</oasis:entry>  
         <oasis:entry colname="col8">3.0</oasis:entry>  
         <oasis:entry colname="col9">7.1</oasis:entry>  
         <oasis:entry colname="col10">7.1 <inline-formula><mml:math id="M58" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 10.4</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K14B</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M59" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2014-01-22–2014-02-11</oasis:entry>  
         <oasis:entry colname="col5">1550</oasis:entry>  
         <oasis:entry colname="col6">5 (C)</oasis:entry>  
         <oasis:entry colname="col7">3.2</oasis:entry>  
         <oasis:entry colname="col8">3.5</oasis:entry>  
         <oasis:entry colname="col9">7.1</oasis:entry>  
         <oasis:entry colname="col10">8.6 <inline-formula><mml:math id="M60" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 5.9</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K15A</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M61" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2015-01-21–2015-02-03</oasis:entry>  
         <oasis:entry colname="col5">1560</oasis:entry>  
         <oasis:entry colname="col6">15 (C)</oasis:entry>  
         <oasis:entry colname="col7">1.5</oasis:entry>  
         <oasis:entry colname="col8">2.1</oasis:entry>  
         <oasis:entry colname="col9">8.1</oasis:entry>  
         <oasis:entry colname="col10">3.3 <inline-formula><mml:math id="M62" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 4.9</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">K15B</oasis:entry>  
         <oasis:entry colname="col2">Kässbohrer</oasis:entry>  
         <oasis:entry colname="col3">V <inline-formula><mml:math id="M63" display="inline"><mml:mo>→</mml:mo></mml:math></inline-formula> P</oasis:entry>  
         <oasis:entry colname="col4">2015-01-21–2015-02-03</oasis:entry>  
         <oasis:entry colname="col5">1580</oasis:entry>  
         <oasis:entry colname="col6">15 (C)</oasis:entry>  
         <oasis:entry colname="col7">2.1</oasis:entry>  
         <oasis:entry colname="col8">2.8</oasis:entry>  
         <oasis:entry colname="col9">8.1</oasis:entry>  
         <oasis:entry colname="col10">6.6 <inline-formula><mml:math id="M64" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 11.0</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup><?xmltex \end{scaleboxenv}?></oasis:table><?xmltex \begin{scaleboxenv}{.95}[.95]?><table-wrap-foot><p><inline-formula><mml:math id="M24" display="inline"><mml:msup><mml:mi/><mml:mi mathvariant="normal">a</mml:mi></mml:msup></mml:math></inline-formula> V is Vostok, M is Mirny, P is Progress
<inline-formula><mml:math id="M25" display="inline"><mml:msup><mml:mi/><mml:mi mathvariant="normal">b</mml:mi></mml:msup></mml:math></inline-formula> G is GPS only, C is a combination of GPS and GLONASS</p></table-wrap-foot><?xmltex \end{scaleboxenv}?></table-wrap>

      <p>Precision estimates for the epochwise coordinates consist of estimates of the
quality of the antenna positioning and an additional uncertainty due to the
reduction to the snow surface. In a first step we assess the quality of the
GNSS processing. The formal coordinate errors reported by the processing
software are too optimistic as they do not account for non-white-noise
components. A more realistic measure is found by comparing multiple baseline
solutions. As mentioned in Sect. <xref ref-type="sec" rid="Ch1.S2.SS2"/>, the ambiguity
resolution is a critical step in the GNSS data processing. Unrecognized cycle
slips can distort profile sections over several kilometres and are thus not
removed by the low-pass filter. However, such instances are identified within
independent solutions using different reference sites. The average baseline
coordinate differences <inline-formula><mml:math id="M65" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">BL</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are used to derive
realistic estimates for the precision of the kinematic positioning. Mean
baseline differences in the vertical component are shown for each profile in
column <inline-formula><mml:math id="M66" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">BL</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> of Table <xref ref-type="table" rid="Ch1.T1"/>
and are in general of the order of a few centimetres.</p>
      <p>An additional source of uncertainty is imposed by the reduction of the GNSS
antenna elevation to the snow surface. This reduction varies regionally due
to varying snow surface characteristics. Thus, besides the error of the
offset measurements themselves, the offset corrections, obtained by
Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>), contain an additional interpolation error. We
assess both types of errors using semivariograms. Here, we fit a linear
function to the squared differences between the measurements of the antenna
height offsets, with respect to the distances between those measurements. We
obtain a constant part of 6 cm, which relates to the uncertainty of the
antenna height measurement itself. It is potentially affected by local
surface features (sastrugi) and residuals in the dynamic tilt correction. The
distance-related additional uncertainty is 0.25 cm km<inline-formula><mml:math id="M67" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> and accounts
for the specific distance between the location of the respective offset
measurement and the location to be interpolated. Using these values, the
precision of the antenna height reduction through inverse distance
interpolation (<inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">AH</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) is derived. Hence, the total
precision measure for a single surface elevation observation is obtained by
            <disp-formula id="Ch1.E2" content-type="numbered"><mml:math id="M69" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">S</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:msup><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">BL</mml:mi></mml:msub><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">AH</mml:mi></mml:msub><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:msqrt><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
          To account for possible errors in the subsidence modelling for profile K08C,
we add additional 10 cm to the uncertainty there.</p>
      <p>A rigorous empirical test for the absolute accuracy estimate is performed by
the calculation of height differences at crossover locations of two different
profiles of the same season. The elapsed time between the two passes over
this location is typically between a few minutes and some days, thus the
surface elevation is assumed unchanged. We consider those profiles to be highly
independent measurements as the antenna/snow-surface offset is determined
independently, the satellite constellations are usually completely different
and the equipment used is different. During the processing the
tropospheric correction has also been estimated individually for each profile. We
assume the GNSS technique itself to be practically unbiased as it is used to
define the IGS08 reference system as well. As the differences <inline-formula><mml:math id="M70" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:math></inline-formula> are
calculated from two passes, the accuracy RMS<inline-formula><mml:math id="M71" display="inline"><mml:msub><mml:mi/><mml:mi>X</mml:mi></mml:msub></mml:math></inline-formula> of a single profile at the
crossover location is given by
            <disp-formula id="Ch1.E3" content-type="numbered"><mml:math id="M72" display="block"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi><mml:mo>/</mml:mo><mml:msqrt><mml:mn mathvariant="normal">2</mml:mn></mml:msqrt><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>For our profiles we obtain <inline-formula><mml:math id="M73" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> in the range of
4–9 cm (see Table <xref ref-type="table" rid="Ch1.T1"/>). This is slightly higher than the
<inline-formula><mml:math id="M74" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi mathvariant="normal">S</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> because it also includes the effect of
vehicle dynamics. Nevertheless, it is a conservative estimate as in these
crossovers the elevations of the second profile are affected by the
disturbances of the snow surface originating from the first vehicle pass.</p>
      <p>As an additional independent validation, we compare our kinematic GNSS
profiles to airborne elevation measurements from Operation ICEBridge
<xref ref-type="bibr" rid="bib1.bibx58" id="paren.35"/>. The region under investigation is very sparsely
covered by flights, but on 26 November 2013 an Airborne Topographic Mapper
(ATM) lidar profile crossed Lake Vostok twice. <xref ref-type="bibr" rid="bib1.bibx8" id="text.36"/> compared
ATM measurements to ground-based GPS profiles in Greenland and found biases
between <inline-formula><mml:math id="M75" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>11 and 7 cm with precisions of less than 9 cm. After applying
the correction for the mean tidal system, we calculated crossover differences
<inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>h</mml:mi><mml:mi mathvariant="normal">ATM</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> between the nadir measurements and our profiles (see
Table <xref ref-type="table" rid="Ch1.T1"/>, last column). The amount of crossover points of
this validation is very low (maximum 9 with K07A), but still valuable to
check <inline-formula><mml:math id="M77" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> as an estimate for the overall absolute accuracy. The
average offset from the 39 crossovers with all profiles is 4.9 cm and the
standard deviation of the differences is 10 cm. Hence, we find that our
accuracy estimates are realistic. There are several other airborne profiles
with a laser altimeter crossing the convoy route to Mirny, but with an
average of 14 cm and a standard deviation of 36 cm, the crossover
differences with these laser altimeter profiles are not adequate for such a
comparison.</p>
</sec>
<sec id="Ch1.S2.SS5">
  <title>Elevation changes</title>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2" specific-use="star"><caption><p><bold>(a)</bold> Elevation change rate <inline-formula><mml:math id="M78" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> from crossovers between
different seasons (20 km block mean values). <bold>(b)</bold> Maximum
observation time span of crossover differences within each block.
<bold>(c)</bold> <inline-formula><mml:math id="M79" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> in the Lake Vostok region. Crossovers on the convoy
track or with <inline-formula><mml:math id="M80" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>t</mml:mi><mml:mo>&lt;</mml:mo></mml:mrow></mml:math></inline-formula> 5 yr are considered uncertain and thus plotted
half sized. <bold>(d)</bold> Distribution of the valid crossovers (<inline-formula><mml:math id="M81" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>t</mml:mi><mml:mi mathvariant="italic">&gt;=</mml:mi><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> yr, no anthropogenic surface disturbances) in the Lake Vostok region
(100–108.5<inline-formula><mml:math id="M82" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E, 76–79<inline-formula><mml:math id="M83" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S).</p></caption>
          <?xmltex \igopts{width=398.338583pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f02.pdf"/>

        </fig>

      <p>The observation times of our kinematic GNSS profiles do not exactly coincide
with the periods of the satellite missions validated here. Therefore, when comparing
the GNSS-derived elevations with altimetry products, it is crucial to know to
what extent elevation changes occurred between their respective observation
epochs. While crossover differences within one expedition are used for
accuracy estimates, the elevation differences in crossovers between profiles
of different years allow us to assess temporal rates of surface elevation
changes (<inline-formula><mml:math id="M84" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula>). Figure <xref ref-type="fig" rid="Ch1.F2"/>a shows that the obtained
surface elevation rates are very small over the whole area. In
Fig. <xref ref-type="fig" rid="Ch1.F2"/>a they are averaged at 20 km blocks to reduce random
noise. However, the rates shown may still be affected by systematic errors
effective over longer distances. One potential error source, in addition to
those mentioned in Sect. <xref ref-type="sec" rid="Ch1.S2.SS4"/>, is the impact of human
activities on the snow surface. The immediate vicinity of the stations is
obviously heavily affected but this is not the only region which had to be
handled with care. For 5 decades the convoy between Mirny and Vostok used the
same route. Especially above 3000 m, the heavy convoy vehicles and cargo
sledges had followed exactly the same track in order to cope with the soft
snow. This resulted in enhanced snow compaction along the track and the
accumulation of a continuous ridge of several decimetres in height which is
even visible on satellite imagery. The elevations and elevation changes along
this part of the traverse are not representative of this area and are thus
excluded from all subsequent studies. The profiles acquired on the modern
Kässbohrer tractors are not prone to this effect since their wider tracks
and relatively small weight relieves these vehicles of the need to reuse a
pre-existing track.</p>
      <p>The largest rates, but also the largest variations, are found on the traverse
to Mirny. In the lower-elevation parts this is not an effect of anthropogenic
disturbance. As the snow is much harder there, the tractors do not repeat the
exact tracks of their predecessors. Nevertheless, the rates obtained in this
area rely solely on 1 year time spans between the measurements of those
profiles and must therefore be treated with care. In the areas where the time
span is longer, very small rates are obtained. Averaging all 18 000
<inline-formula><mml:math id="M85" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> by introducing weights according to the time span results in a mean
elevation change over the entire area of 4 cm yr<inline-formula><mml:math id="M86" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> and a standard
deviation (<inline-formula><mml:math id="M87" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula>) of a single crossover rate of <inline-formula><mml:math id="M88" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>11 cm yr<inline-formula><mml:math id="M89" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>.</p>
      <p>A detailed look into the results in the Lake Vostok region is given in
Fig. <xref ref-type="fig" rid="Ch1.F2"/>c and d. In order to avoid the limitations arising
from short observation time spans, we used only crossovers spanning 5
years or more. The average <inline-formula><mml:math id="M90" display="inline"><mml:mover accent="true"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mo mathvariant="normal">¯</mml:mo></mml:mover></mml:math></inline-formula> of the 492 crossover differences
in this area is <inline-formula><mml:math id="M91" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.1 cm yr<inline-formula><mml:math id="M92" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> with a standard deviation of a single
rate of <inline-formula><mml:math id="M93" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>2.4 cm yr<inline-formula><mml:math id="M94" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. The <inline-formula><mml:math id="M95" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> values are not uncorrelated,
especially due to possible systematic biases (e.g. antenna height reduction)
which affect multiple crossovers of a profile. Therefore, for the accuracy of
the mean <inline-formula><mml:math id="M96" display="inline"><mml:mover accent="true"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mo mathvariant="normal">¯</mml:mo></mml:mover></mml:math></inline-formula> we only consider the number of combinations of
independent profiles (27) in the estimation, resulting in a standard error of
<inline-formula><mml:math id="M97" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>0.5 cm yr<inline-formula><mml:math id="M98" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This comprises both real variations in surface
elevation change rate and observational uncertainties. These results agree
very well with the elevation changes observed by measurements on snowmobiles
around Vostok Station <xref ref-type="bibr" rid="bib1.bibx44" id="paren.37"><named-content content-type="post">0.1 <inline-formula><mml:math id="M99" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.5 cm yr<inline-formula><mml:math id="M100" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula></named-content></xref>.
The latter profiles have a higher accuracy but yield a smaller amount of
crossovers which may be affected by higher spatial correlation.</p>
      <p>We conclude that the elevation change rates are very small in the region
under investigation, but their spatial pattern is not determined with
homogeneous reliability due to the short observation time span in some areas.
For the following validations we consider the elevation change to be
negligible. On the one hand we have chosen only missions which overlap in
time with our profiles and thus the elevation changes due to the time
differences are fairly small. On the other hand, at coastal regions where the
rates might be larger, the errors of SRA are significantly larger too (metres
for CryoSat-2 in SARIn mode, tens of metres for Envisat; see
Sect. <xref ref-type="sec" rid="Ch1.S3.SS3"/>). As this is not the case for ICESat,
elevation changes will be discussed further in
Sect. <xref ref-type="sec" rid="Ch1.S3.SS3.SSS3"/>.</p>
</sec>
</sec>
<sec id="Ch1.S3">
  <title>Validation of satellite altimetry</title>
<sec id="Ch1.S3.SS1">
  <title>Data</title>
<sec id="Ch1.S3.SS1.SSS1">
  <title>Envisat</title>
      <p>We validate different altimeter missions to reveal characteristic effects of
their respective techniques and approaches to derive optimum results.
Conventional altimeter systems usually use signals in Ku-band and have a beam
limited footprint of 10 to 20 km. Over ice sheets their signals penetrate
into the upper firn layers. As an example for a conventional pulse-limited
radar we validate the Envisat mission, operated by the European Space Agency
(ESA). We use the Ku-band measurements of its altimeter system RA-2 acquired
during the entire operation period (May 2002 to April 2012). In the Level 2
product (SGDR V2.1) the slope-induced error is corrected for using the
relocation method <xref ref-type="bibr" rid="bib1.bibx2" id="paren.38"/>. This algorithm is designed to locate
the measurement to the position where the first return signal comes from. The
ESA data set contains results from two types of radar waveform retrackers
applicable over ice sheets, ICE1 <xref ref-type="bibr" rid="bib1.bibx61" id="paren.39"><named-content content-type="pre">based on the offset centre of gravity
(OCOG) retracker by</named-content><named-content content-type="post"> with a threshold of 30 %</named-content></xref> and ICE2
<xref ref-type="bibr" rid="bib1.bibx31" id="paren.40"><named-content content-type="pre">a functional fit developed by</named-content></xref>. We use both retrackers
and compare their performance.</p>
      <p>The Goddard Space Flight Center (GSFC) developed an in-house processing chain
for radar altimetry with slightly different approaches for deriving surface
elevations. Here, the direct method of slope correction was applied, which
corrects the measurement at the nadir position. This reprocessed Level 2
data set is called the Ice Data Record (IDR) and also contains different
retrackers. We use the GSFC V4 <inline-formula><mml:math id="M101" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>-retracker as <xref ref-type="bibr" rid="bib1.bibx6" id="text.41"/>
summarize that this algorithm provides more accurate absolute elevations than
threshold-based methods.</p>
      <p>To remove potentially corrupted observations from the data, we used the
measurement confidence flags (which are identical in the ESA SGDR
and GSFCs IDR data sets) to find recorded distances out of range and to
identify problems in the onboard processing and data handling, the ultra
stable oscillator, the automatic gain control (AGC) or in the waveform
samples. In addition to these instrumental errors we removed shots where the
GSFC retracking algorithm failed as indicated by the retracking
problem flag. In the SGDR data we furthermore used the fault
identifier and the flag indicating that the ICE1 retracking in Ku-band was
not successful.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS2">
  <title>CryoSat-2</title>
      <p>Compared to the conventional SRA, ESA's CryoSat-2 has an improved resolution
and accuracy due to its innovative design. In the smooth interior of the ice
sheets the altimeter operates in the low-resolution mode (LRM) which is a
conventional pulse-limited observation mode as in the missions before. Above
steeper terrain, the altimeter is switched to SARIn mode. In this mode, the
synthetic aperture radar (SAR) processing considerably improves the along
track resolution utilizing the Doppler/delay shift. Hence, the beam-limited
footprint is subdivided in flight direction into stripes of roughly 250 m in
length. The interferometric processing of the reception times at the two
antennas allows the determination of the across-track angle to the point of
closest approach <xref ref-type="bibr" rid="bib1.bibx63" id="paren.42"/>.</p>
      <p>We compare two different processing versions, Baseline B and C, of ESA's L2I
data set. The “I” in the product identifier stands for the in-depth data
set. It provides more parameters and flags and, over land, offers an
additional feature relevant for our study. In the basic L2 product the SARIn
ambiguity flag indicates an elevation difference between altimetry and a DEM
exceeding 50 m. In this case the interferometric angle is considered
erroneous and the measurement position is set to nadir. In the L2I product,
however, this is not applied. This product allows us, therefore, to also
validate the data at the margins where the a priori DEM itself is prone to
large uncertainties (see Sect. <xref ref-type="sec" rid="Ch1.S4"/>). As an alternative
approach, to identify outliers in the interferometric angle, we used the
coherence flag and additionally excluded all measurements with a across-track
angle exceeding 1<inline-formula><mml:math id="M102" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> (corresponding to the very edge of the antenna
beam). Furthermore, we exclude all data where the respective retracker
height error flag indicates problems in the determination of the retracking
point. For Baseline B, the waveform is processed using the CFI retracker
<xref ref-type="bibr" rid="bib1.bibx63" id="paren.43"/>. In Baseline C two additional retrackers have been
applied to the LRM data: a threshold-based OCOG-retracker and another
functional fit retracker called UCL, which is based on the Brown-model
<xref ref-type="bibr" rid="bib1.bibx7" id="paren.44"/>.</p>
</sec>
<sec id="Ch1.S3.SS1.SSS3">
  <title>ICESat</title>
      <p>In contrast to radar altimeters, the ICESat laser altimeter mission has a
ground footprint of only 65 m and does not penetrate into the snowpack.
Hence, surface elevation accuracies at the decimetre level can be achieved
<xref ref-type="bibr" rid="bib1.bibx20 bib1.bibx56" id="paren.45"/> which are almost comparable to our kinematic
GNSS profiles. We use GLA12 elevation data (Zwally et al., 2014) from Release
34 (R34). We apply the saturation correction <xref ref-type="bibr" rid="bib1.bibx20" id="paren.46"/> to the
elevations and exclude all data where flags indicate off-nadir operation,
orbit manoeuvres or any other factors degrading the orbit accuracy. We also
remove data where the attitude flag indicates any problem with star trackers,
gyro or the laser reference sensor. In order to exclude data affected by
forward scattering in clouds or drifting snow <xref ref-type="bibr" rid="bib1.bibx57" id="paren.47"><named-content content-type="pre">e.g.</named-content></xref>,
we reject all returns with a gain value exceeding 200, with a reflectivity
below 10 %, with a misfit between the received waveform and the Gaussian
model exceeding 0.03 V or where more than one waveform is detected
<xref ref-type="bibr" rid="bib1.bibx3" id="paren.48"/>.</p>
</sec>
</sec>
<sec id="Ch1.S3.SS2">
  <title>Methods</title>
<sec id="Ch1.S3.SS2.SSS1">
  <title>Crossover comparison</title>
      <p>We validate the surface elevation data derived from satellite altimetry by
applying the crossover method, outlined in Sect. <xref ref-type="sec" rid="Ch1.S2.SS4"/>, to
the intersections of the along-track altimetric profiles with our kinematic
GNSS profiles. Therefore we interpolate the elevation of both profiles
linearly if the distance between the two adjacent data points is less than
500 m. The along-track data point spacing amounts to 172 m for ICESat
<xref ref-type="bibr" rid="bib1.bibx54" id="paren.49"/>, 300 m for CryoSat-2 <xref ref-type="bibr" rid="bib1.bibx63" id="paren.50"/> and 400 m for
Envisat <xref ref-type="bibr" rid="bib1.bibx16" id="paren.51"/>. In fact, the altimetry measurements represent
average elevations over the respective footprint area. As we did not measure
2D-grids but straight lines, this cannot be taken into account here. The
smoothing of the profiles with a filter length of 180 m, however, resembles
the ICESat footprint at least in profile direction.</p>
      <p>The largest error source for radar altimetry over a distinctive topography
results from the slope correction. <xref ref-type="bibr" rid="bib1.bibx6" id="text.52"/> found that crossover
differences between ICESat and Envisat are less than 3 m for slopes below
0.1<inline-formula><mml:math id="M103" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, but up to 50 m and more for slopes above 0.7<inline-formula><mml:math id="M104" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. Hence,
the validation of SRA needs to consider different surface slopes.
<xref ref-type="bibr" rid="bib1.bibx6" id="text.53"/> and <xref ref-type="bibr" rid="bib1.bibx26" id="text.54"/> binned their elevation differences
with ICESat with respect to the slope. The obtained quasi-continuous
functions clearly depict the growing differences with increasing surface
slope. The amount and spatial coverage of our crossovers does not allow a
comparison in such a high sampling of slope. Instead, we investigate regions
of different characteristic slope in separate histograms. This allows us not
only to calculate a mean and standard deviation for each zone but also to
identify deviations from a Gaussian distribution. Those histograms display
the full range of results including potential outliers. In order to reduce
their impact, an iterative 5<inline-formula><mml:math id="M105" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> filter is applied in the calculation of
the mean and standard deviation.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3"><caption><p>Crossover differences between Envisat (ESA, relocated, ICE1
retracker) and the kinematic GNSS profiles. The black contour lines mark the
borders between the different zones of slope (0.15 and 0.5<inline-formula><mml:math id="M106" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>) and the
hydrostatic equilibrium area of Lake Vostok (outline in grey from
<xref ref-type="bibr" rid="bib1.bibx40" id="altparen.55"/>).</p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f03.pdf"/>

          </fig>

      <p>We subdivide the region under investigation into four zones according to
their mean surface slopes: <inline-formula><mml:math id="M107" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 0.5, 0.5–0.15, <inline-formula><mml:math id="M108" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 0.15<inline-formula><mml:math id="M109" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> and, as a
subset of the latter characterized by extremely little surface roughness, the
hydrostatic equilibrium area of subglacial Lake Vostok. The crossover
differences between Envisat data and the GNSS profiles
(Fig. <xref ref-type="fig" rid="Ch1.F3"/>) clearly demonstrate the relationship
between surface slope and SRA errors and motivates our subdivision. The first
zone comprises the coastal areas. Outliers and large errors in the SRA
elevations are frequent there due to the rugged topography. On the other
hand, it is the zone where the largest elevation changes would be expected.
Hence, this zone introduces the largest uncertainties in ice-mass balance
estimates based on SRA <xref ref-type="bibr" rid="bib1.bibx64" id="paren.56"/>. The subsequent zone of
intermediate slopes is still close to the coast and of low elevations. It may
therefore also be subject to significant elevation changes. At the same time,
SRA provides a higher accuracy there compared to the first zone. The third
zone comprises the flat interior of the ice sheet. Here, elevation changes
are generally small but, because of its vast areal extent, nevertheless
important for mass balance studies. The ice above Lake Vostok, constituting
the fourth zone, floats in hydrostatic equilibrium <xref ref-type="bibr" rid="bib1.bibx17" id="paren.57"/>.
Surface gradients are very small and homogeneous in this area. Thus, the
influence of the slope-induced error vanishes, offering a unique opportunity
to study other effects such as the surface penetration of the radar signal.</p>
</sec>
<sec id="Ch1.S3.SS2.SSS2">
  <title>ICESat campaign biases</title>
      <p>Due to its smaller footprint size, the ICESat surface elevations are less
sensitive to surface slope compared to SRA. However, the Geoscience Laser
Altimeter System (GLAS) altimeter was operated in several laser operation
campaigns due to laser degradation. Between the campaigns systematic biases
exist <xref ref-type="bibr" rid="bib1.bibx20 bib1.bibx24" id="paren.58"/>. If not accounted for carefully, any
systematic biases between campaigns can corrupt the inference of temporal
surface elevation changes <inline-formula><mml:math id="M110" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula>. To determine those biases, different
surface types have been used, including the salt flat Salar de Uyuni
<xref ref-type="bibr" rid="bib1.bibx20" id="paren.59"/>, the global oceans <xref ref-type="bibr" rid="bib1.bibx51 bib1.bibx24" id="paren.60"><named-content content-type="pre">Urban
in</named-content></xref>, the ice surface above Lake Vostok
<xref ref-type="bibr" rid="bib1.bibx17" id="paren.61"/>, the Antarctic low-precipitation zone
<xref ref-type="bibr" rid="bib1.bibx27 bib1.bibx25" id="paren.62"/> or leads and polynyas in sea ice areas
<xref ref-type="bibr" rid="bib1.bibx67" id="paren.63"/>. The estimated biases differ significantly between
different data releases and, within the same release, depending on the
surface type used for calibration.</p>
      <p>Within the region around subglacial Lake Vostok
(Fig. <xref ref-type="fig" rid="Ch1.F1"/>b, 100–108.5<inline-formula><mml:math id="M111" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E,
76–79<inline-formula><mml:math id="M112" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S) <xref ref-type="bibr" rid="bib1.bibx17" id="text.64"/> applied a least squares adjustment of
crossover differences between elevation profiles of ascending and descending
ICESat (<inline-formula><mml:math id="M113" display="inline"><mml:mi>I</mml:mi></mml:math></inline-formula>) orbits, acquired during laser campaigns <inline-formula><mml:math id="M114" display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M115" display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula> (<inline-formula><mml:math id="M116" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi>I</mml:mi><mml:mo>-</mml:mo><mml:mi>I</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:math></inline-formula>). To cope with the lack of an absolute reference, these authors
introduced a zero-sum condition. As a consequence, the laser campaign biases
were determined as relative biases, relating to their overall average. This
method relies essentially on the assumption of a stable surface throughout
the ICESat observation period. This assumption is justified by the
observational results of <xref ref-type="bibr" rid="bib1.bibx42" id="text.65"/>.</p>
      <p>Using the same region of ice-surface around Lake Vostok we derive a new set
of laser campaign biases <inline-formula><mml:math id="M117" display="inline"><mml:mi>b</mml:mi></mml:math></inline-formula> for release 34. In addition to the ICESat
crossovers (<inline-formula><mml:math id="M118" display="inline"><mml:mi>I</mml:mi></mml:math></inline-formula>) used by <xref ref-type="bibr" rid="bib1.bibx17" id="text.66"/> we also include crossover
differences between ICESat and our kinematic GNSS profiles (<inline-formula><mml:math id="M119" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>q</mml:mi></mml:mrow><mml:mrow><mml:mi>I</mml:mi><mml:mo>-</mml:mo><mml:mi>K</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:math></inline-formula>) and crossover differences between different GNSS profiles
(<inline-formula><mml:math id="M120" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>p</mml:mi><mml:mi>q</mml:mi></mml:mrow><mml:mrow><mml:mi>K</mml:mi><mml:mo>-</mml:mo><mml:mi>K</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:math></inline-formula>). Including the unbiased GNSS profiles allows us to
solve for the surface elevation change rate <inline-formula><mml:math id="M121" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> between the respective
observation epochs <inline-formula><mml:math id="M122" display="inline"><mml:mi>t</mml:mi></mml:math></inline-formula> as an additional parameter and thus to overcome the
assumption of a stable surface. We are hence able to separate real elevation
trends <inline-formula><mml:math id="M123" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> from the apparent trend <inline-formula><mml:math id="M124" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>h</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> implied by the
laser campaign biases. Furthermore, the incorporation of the unbiased GNSS
elevations allows us to avoid the zero-sum condition and thus to determine
absolute laser campaign biases. Combining all crossover differences results
in three different types of observation equations:
              <disp-formula id="Ch1.E4" content-type="numbered"><mml:math id="M125" display="block"><mml:mrow><mml:mtable class="array" columnalign="left center left center left"><mml:mtr><mml:mtd><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi>I</mml:mi><mml:mo>-</mml:mo><mml:mi>I</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mo>=</mml:mo></mml:mtd><mml:mtd><mml:mrow><mml:msub><mml:mi>b</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>b</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mtd><mml:mtd><mml:mo>+</mml:mo></mml:mtd><mml:mtd><mml:mrow><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mi mathvariant="italic">ϵ</mml:mi></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>q</mml:mi></mml:mrow><mml:mrow><mml:mi>I</mml:mi><mml:mo>-</mml:mo><mml:mi>K</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mo>=</mml:mo></mml:mtd><mml:mtd><mml:mrow><mml:msub><mml:mi>b</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mtd><mml:mtd><mml:mo>+</mml:mo></mml:mtd><mml:mtd><mml:mrow><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>q</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mi mathvariant="italic">ϵ</mml:mi></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msubsup><mml:mi>h</mml:mi><mml:mrow><mml:mi>p</mml:mi><mml:mi>q</mml:mi></mml:mrow><mml:mrow><mml:mi>K</mml:mi><mml:mo>-</mml:mo><mml:mi>K</mml:mi></mml:mrow></mml:msubsup></mml:mrow></mml:mtd><mml:mtd><mml:mo>=</mml:mo></mml:mtd><mml:mtd/><mml:mtd><mml:mo>+</mml:mo></mml:mtd><mml:mtd><mml:mrow><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>p</mml:mi><mml:mi>q</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mi mathvariant="italic">ϵ</mml:mi></mml:mrow></mml:mtd></mml:mtr></mml:mtable><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            To account for the individual uncertainty of each GNSS profile, we introduce
the epoch-wise surface elevation uncertainty RMS<inline-formula><mml:math id="M126" display="inline"><mml:msub><mml:mi/><mml:mi>S</mml:mi></mml:msub></mml:math></inline-formula> as weights for the
elevations. As shown in Sect. <xref ref-type="sec" rid="Ch1.S2.SS4"/> the empirical
intra-expedition crossover differences RMS<inline-formula><mml:math id="M127" display="inline"><mml:msub><mml:mi/><mml:mi>X</mml:mi></mml:msub></mml:math></inline-formula> are about 5 cm larger. For
this reason we add 5 cm to each RMS<inline-formula><mml:math id="M128" display="inline"><mml:msub><mml:mi/><mml:mi mathvariant="normal">S</mml:mi></mml:msub></mml:math></inline-formula>. For the ICESat elevations,
we use campaign-specific average <inline-formula><mml:math id="M129" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>
(Table <xref ref-type="table" rid="Ch1.T3"/>) obtained from
intra-campaign crossovers
in the Lake Vostok region.</p>
</sec>
</sec>
<sec id="Ch1.S3.SS3">
  <title>Results</title>
<sec id="Ch1.S3.SS3.SSS1">
  <title>Envisat</title>
      <p>The validation of the Envisat data (Fig. <xref ref-type="fig" rid="Ch1.F4"/>) shows that
in the flat interior all processing versions provide precise elevations.
Nevertheless, the crossovers over Lake Vostok reveal significant differences
between the three retracker versions. The standard deviations of the two
functional fit retrackers yield similar results (51 cm for the
<inline-formula><mml:math id="M130" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>-retracker, 44 cm for ICE2). In contrast, the precision or the
ICE1-retracked data is better by a factor of two (22 cm). This confirms the
findings of <xref ref-type="bibr" rid="bib1.bibx11" id="normal.67"/>, which argued for the superior precision of
threshold retrackers. With respect to the kinematic GNSS profiles, the mean
bias of all processing versions is negative. This can be explained by the
penetration of the radar signal into the upper firn layers. However,
significant differences between the retrackers are evident here. Compared to
the ICE1-retracker, the mean reference surface of the ICE2 functional fit is
90 cm lower. Thus the influence of variations in firn pack properties is
much stronger for this retracker. Between different data sets, a comparison of
the biases of different retrackers should be treated with care. Here,
elevation differences might also be caused by other factors as a different
instrumental calibration value or alternative models for range correction.</p>
      <p>Compared to Lake Vostok, where the slope effect is negligible, significant
differences can already be observed in the zone of least slopes
(<inline-formula><mml:math id="M131" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 0.15<inline-formula><mml:math id="M132" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>). Even the smooth topography there introduces additional
uncertainties of about 30 cm for the relocated ESA data and 1.5 m for the
GSFC data corrected by the direct method. Furthermore, the mean biases are
shifted in the positive direction. The histograms reveal that this is a
consequence of a deviation from the Gaussian distribution of the crossovers.
The increased amount of positive differences means that the GNSS elevation is
lower than the altimeter value. This is a consequence of the inability of the
radar signal to observe depressions which are significantly smaller than the
beam-limited footprint diameter <xref ref-type="bibr" rid="bib1.bibx6" id="paren.68"/>. For all versions, this
effect increases progressively as the slope and hence the magnitudes of
the depressions also get larger. In the intermediate surface slope zone the
standard deviations of the ESA data sets grow to 3 m and in the coastal zone
they grow up to 10 m. Here, the differences between the two ESA retrackers become
negligible. For the GSFC product these errors are significantly larger.
Hence, our results support a clear preference for the relocation method.
Nevertheless, in zones of larger slopes the error of the slope correction
becomes the dominating uncertainty contribution.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><caption><p>Histograms, means and standard deviations of crossover differences
between different Envisat data sets and kinematic GNSS profiles for four zones
of characteristic surface slope. The range of the histograms is adjusted
according to the values found in each zone, the colour scale is the same for
all histograms. The displayed crossover differences contain uncertainties in
the kinematic GNSS profiles (4–9 cm) and possible elevation changes between
the observation epochs of both techniques in addition to the uncertainty in
the Envisat data.</p></caption>
            <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f04.pdf"/>

          </fig>

      <p>To avoid loss of tracking, Envisat switched the tracking bandwidth from high
resolution to two lower-resolution modes when approaching steeper terrain. We
analysed the performance of modes separately.
Table <xref ref-type="table" rid="Ch1.T2"/> shows the results of each mode in the
different zones. The number of crossovers indicates that the majority of
data, even close to the coasts, was acquired in high-resolution mode. In the
central zone the accuracy of the lower-resolution data is, as expected,
worse. In the coastal zone, however, the other modes yield better results (if
their small number of crossovers is considered as representative). The
variations of the mean biases demonstrate, in turn, that these mode switches
induce offsets in the data. We agree therefore with <xref ref-type="bibr" rid="bib1.bibx6" id="text.69"/> not
to use the sparse data of the lower-resolution modes for precise elevation
change studies.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T2" specific-use="star"><caption><p>Statistics of crossover differences between different Envisat
resolution modes with kinematic GNSS profiles similar to Fig.
<xref ref-type="fig" rid="Ch1.F4"/>. Outliers (<inline-formula><mml:math id="M133" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 5<inline-formula><mml:math id="M134" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) are excluded
iteratively. Each set of statistics contains <inline-formula><mml:math id="M135" display="inline"><mml:mrow><mml:mover accent="true"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>±</mml:mo><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and the number of valid crossovers (sums can differ from
the total number due to outlier rejection). Italic values are considered to
be not statistically significant. </p></caption><oasis:table frame="topbot"><oasis:tgroup cols="9">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right" colsep="1"/>
     <oasis:colspec colnum="4" colname="col4" align="right"/>
     <oasis:colspec colnum="5" colname="col5" align="right" colsep="1"/>
     <oasis:colspec colnum="6" colname="col6" align="right"/>
     <oasis:colspec colnum="7" colname="col7" align="right" colsep="1"/>
     <oasis:colspec colnum="8" colname="col8" align="right"/>
     <oasis:colspec colnum="9" colname="col9" align="right"/>
     <oasis:thead>
       <oasis:row>  
         <oasis:entry colname="col1">Data set</oasis:entry>  
         <oasis:entry namest="col2" nameend="col3" align="center" colsep="1">Vostok </oasis:entry>  
         <oasis:entry namest="col4" nameend="col5" align="center" colsep="1"><inline-formula><mml:math id="M136" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 0.15<inline-formula><mml:math id="M137" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>  </oasis:entry>  
         <oasis:entry namest="col6" nameend="col7" align="center" colsep="1">0.15–0.5<inline-formula><mml:math id="M138" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>  
         <oasis:entry namest="col8" nameend="col9" align="center"><inline-formula><mml:math id="M139" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 0.5<inline-formula><mml:math id="M140" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1"/>  
         <oasis:entry colname="col2">[m]</oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math id="M141" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col4">[m]</oasis:entry>  
         <oasis:entry colname="col5"><inline-formula><mml:math id="M142" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col6">[m]</oasis:entry>  
         <oasis:entry colname="col7"><inline-formula><mml:math id="M143" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col8">[m]</oasis:entry>  
         <oasis:entry colname="col9"><inline-formula><mml:math id="M144" display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">Total (ESA, ICE1)</oasis:entry>  
         <oasis:entry colname="col2"><inline-formula><mml:math id="M145" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.25 <inline-formula><mml:math id="M146" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.22</oasis:entry>  
         <oasis:entry colname="col3">10 081</oasis:entry>  
         <oasis:entry colname="col4"><inline-formula><mml:math id="M147" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.89 <inline-formula><mml:math id="M148" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.54</oasis:entry>  
         <oasis:entry colname="col5">120 888</oasis:entry>  
         <oasis:entry colname="col6">0.89 <inline-formula><mml:math id="M149" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 3.09</oasis:entry>  
         <oasis:entry colname="col7">32 524</oasis:entry>  
         <oasis:entry colname="col8">9.62 <inline-formula><mml:math id="M150" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 10.61</oasis:entry>  
         <oasis:entry colname="col9">3736</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">High res. (320 MHz)</oasis:entry>  
         <oasis:entry colname="col2"><inline-formula><mml:math id="M151" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.25 <inline-formula><mml:math id="M152" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.22</oasis:entry>  
         <oasis:entry colname="col3">10 078</oasis:entry>  
         <oasis:entry colname="col4"><inline-formula><mml:math id="M153" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.89 <inline-formula><mml:math id="M154" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.54</oasis:entry>  
         <oasis:entry colname="col5">120 717</oasis:entry>  
         <oasis:entry colname="col6">0.89 <inline-formula><mml:math id="M155" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 3.09</oasis:entry>  
         <oasis:entry colname="col7">32 470</oasis:entry>  
         <oasis:entry colname="col8">9.89 <inline-formula><mml:math id="M156" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 10.62</oasis:entry>  
         <oasis:entry colname="col9">3634</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Medium res. (80 MHz)</oasis:entry>  
         <oasis:entry colname="col2"><italic>–0.86</italic> <inline-formula><mml:math id="M157" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> <italic>0.22</italic></oasis:entry>  
         <oasis:entry colname="col3">3</oasis:entry>  
         <oasis:entry colname="col4"><inline-formula><mml:math id="M158" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.62 <inline-formula><mml:math id="M159" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 1.01</oasis:entry>  
         <oasis:entry colname="col5">136</oasis:entry>  
         <oasis:entry colname="col6">1.29 <inline-formula><mml:math id="M160" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 3.33</oasis:entry>  
         <oasis:entry colname="col7">48</oasis:entry>  
         <oasis:entry colname="col8"><inline-formula><mml:math id="M161" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.15 <inline-formula><mml:math id="M162" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 1.67</oasis:entry>  
         <oasis:entry colname="col9">96</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Low res. (20 MHz)</oasis:entry>  
         <oasis:entry colname="col2"><italic>2.20</italic> <inline-formula><mml:math id="M163" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> <italic>0.12</italic></oasis:entry>  
         <oasis:entry colname="col3">2</oasis:entry>  
         <oasis:entry colname="col4">0.01 <inline-formula><mml:math id="M164" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 1.26</oasis:entry>  
         <oasis:entry colname="col5">39</oasis:entry>  
         <oasis:entry colname="col6"><italic>–0.10</italic> <inline-formula><mml:math id="M165" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> <italic>1.60</italic></oasis:entry>  
         <oasis:entry colname="col7">6</oasis:entry>  
         <oasis:entry colname="col8"><italic>2.94</italic> <inline-formula><mml:math id="M166" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> <italic>5.72</italic></oasis:entry>  
         <oasis:entry colname="col9">6</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

</sec>
<sec id="Ch1.S3.SS3.SSS2">
  <title>CryoSat-2</title>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><caption><p>Histograms, means and standard deviations of crossover differences
between different CryoSat-2 data sets and kinematic GNSS profiles for four
zones of characteristic surface slope. The histogram ranges are the same as
in Fig. <xref ref-type="fig" rid="Ch1.F4"/> (Envisat) for comparability. The displayed
crossover differences contain uncertainties in the kinematic GNSS profiles
(4–9 cm) and possible elevation changes between the observation epochs of
both techniques in addition to the uncertainty in the CryoSat-2 data.</p></caption>
            <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f05.pdf"/>

          </fig>

      <p>The results of the validation of CryoSat-2 elevations are shown in
Fig. <xref ref-type="fig" rid="Ch1.F5"/>. A comparison with those from Envisat
(Fig. <xref ref-type="fig" rid="Ch1.F4"/>) clearly shows the advantage of the SARIn mode
in zones of larger slopes. Furthermore, a comparison of the recent Baseline C
version with the previous Baseline B documents the improvements made by
solving several issues.</p>
      <p>A primary issue solved from Baseline B to C was a range bias of 67 cm in
SARIn and 20 cm in LRM data <xref ref-type="bibr" rid="bib1.bibx50" id="paren.70"/>. In the SARIn data this
bias reduction is clearly visible in all zones. Besides that, no major
changes are evident and the standard deviations remain the same.
Comparing the Baseline B LRM with the respective CFI-retracked version of
Baseline C, we find a significant improvement in standard deviation. The
refinements in the retracking procedure itself, described by
<xref ref-type="bibr" rid="bib1.bibx4" id="text.71"/>, are probably responsible for those improvements. This
holds true especially in the zones of stronger slopes where the retracking is
more challenging. In the absence of slope-related effects on Lake Vostok, the
correction of the range bias is also evident in the LRM data.</p>
      <p>The main improvement in the performance of the Baseline C LRM data has been
introduced by adding two additional retrackers (UCL and OCOG). The OCOG
retracker shows standard deviations of about 20 cm over Lake Vostok, which
is similar to the corresponding ICE1 retracker for Envisat. In contrast, the
functional fit models show standard deviations of <inline-formula><mml:math id="M167" display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 50 cm which is
similar to the results of the ICE2 retracker of Envisat. For the entire low-slope zone (<inline-formula><mml:math id="M168" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 0.15<inline-formula><mml:math id="M169" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>) we obtain similar results when comparing
CryoSat-2 LRM to Envisat. In the intermediate zone (0.15–0.5<inline-formula><mml:math id="M170" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> ) the
two missions cannot be compared directly as the statistics for CryoSat-2 only
relate to the subzone where the LRM is applied, which covers only the gently
sloping areas. It should be noted that, even though SARIn mode is usually
applied in coastal regions only, there are still some SARIn data available
over Lake Vostok. On 28 July 2010 and the first week of June 2013 CryoSat-2
observed whole profiles across Antarctica in SARIn mode and also passed our
region under investigation (including Lake Vostok) several times. These
profiles allow us to directly compare the different modes and, in the case of
Lake Vostok, the performance of their retrackers. The first column of
Fig. <xref ref-type="fig" rid="Ch1.F5"/> shows that the accuracy of SARIn is quite
similar to the CFI retracker in LRM.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6"><caption><p><bold>(a–d)</bold> Monthly averages of crossover differences between different versions of CryoSat-2 data and kinematic GNSS profiles
(black) and the corresponding backscatter <inline-formula><mml:math id="M171" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> (red) within the hydrostatic equilibrium area of Lake Vostok. <bold>(a)</bold> Baseline B data set, <bold>(b–d)</bold> Baseline C using
the three different retrackers applied. The box at the bottom of each plot gives the overall elevation trend. </p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f06.pdf"/>

          </fig>

      <p>Different observational techniques have substantiated the stability of the
surface elevation above Lake Vostok over timescales of typical satellite
altimeter mission life times <xref ref-type="bibr" rid="bib1.bibx42 bib1.bibx44" id="paren.72"/>. This
stability, together with the low precipitation and the continuous monitoring
of relevant parameters at Vostok Station, makes Lake Vostok an ideal area to
examine apparent elevation variations in the altimetric time series. Spurious
variations can be related to changes in surface backscatter and thus the
backscattered power <inline-formula><mml:math id="M172" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> of the altimetric signal
<xref ref-type="bibr" rid="bib1.bibx62" id="paren.73"/>. Commonly, the relationship is determined as a
regression coefficient and its influence is removed from the elevation time
series <xref ref-type="bibr" rid="bib1.bibx62 bib1.bibx12 bib1.bibx67" id="paren.74"/>. Figure
<xref ref-type="fig" rid="Ch1.F6"/> displays monthly averages of the crossover
differences between the kinematic GNSS profiles and different CryoSat-2 LRM
data sets. The Baseline B product (panel a) yields a high correlation as well
as trends of the opposite sign in the elevations and the backscatter values. A
trend derived from this elevation data set suggests a surface increase of
9.8 cm yr<inline-formula><mml:math id="M173" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> which clearly contradicts all results from other studies.
For the three retrackers of the Baseline C product
(Fig. <xref ref-type="fig" rid="Ch1.F6"/>b–d) none of the backscatter curves
show a significant trend any more. Nevertheless, the retracking methods
based on functional fits (CFI in b, UCL in c) still exhibit a high
correlation between <inline-formula><mml:math id="M174" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>h</mml:mi></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M175" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. Here, the retracking point
is defined by the fit of the functional model to the whole waveform. Hence,
it is more affected by volume scattering. In contrast the OCOG retracker uses
a 25 % threshold of the OCOG amplitude and thus locates the retracking
point much closer to the first radar return. The results in
Fig. <xref ref-type="fig" rid="Ch1.F6"/> indicate that threshold retrackers (panel
d) produce the most precise elevations, especially in terms of repeatability.
This confirms similar findings by <xref ref-type="bibr" rid="bib1.bibx11" id="text.75"/>. The seasonal variation
of the signal almost vanishes. However, there is still a very small remaining
amplitude, which correlates quite well with <inline-formula><mml:math id="M176" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. This indicates that
there might still be some remaining effects of the snowpack properties
superimposed on the elevation time series. Once the large variations
disappeared, some jumps of a few decimetres are revealed. Apparent elevation
jumps in two winters (2011/2012 and 2013/2014) correspond to abrupt
backscatter increase at the same time. <xref ref-type="bibr" rid="bib1.bibx30" id="text.76"/> detected a
similar jump in Envisat data and referred it to changes in snowpack
properties due to strong wind. However, the meteorological records from
Vostok Station (wind, precipitation, temperature; not shown here) do not show
any significant peak at the times of the jumps. Inconsistencies in the
applied correction models of the ionosphere, troposphere and tides can be
ruled out as the origin of these jumps. None of the time series of these features
show variations exceeding a few centimetres. Future studies including
additional data sets will hopefully show whether these jumps are related to
remaining processing issues or physical processes.</p>
</sec>
<sec id="Ch1.S3.SS3.SSS3">
  <title>ICESat</title>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T3"><caption><p>Intra-campaign precision <inline-formula><mml:math id="M177" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> from crossovers
within each ICESat laser campaign and obtained campaign biases <inline-formula><mml:math id="M178" display="inline"><mml:mi>b</mml:mi></mml:math></inline-formula> for
release 34, derived from a combined crossover adjustment of ICESat elevations
and kinematic GNSS profiles in the region of subglacial Lake Vostok (to be
subtracted from the elevations for correction). The true surface elevation
change <inline-formula><mml:math id="M179" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula>, estimated simultaneously in
Eq. (<xref ref-type="disp-formula" rid="Ch1.E4"/>), is 0.0 <inline-formula><mml:math id="M180" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.2 cm. </p></caption><oasis:table frame="topbot"><oasis:tgroup cols="6">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="center"/>
     <oasis:colspec colnum="3" colname="col3" align="center"/>
     <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:thead>
       <oasis:row>  
         <oasis:entry colname="col1">Laser</oasis:entry>  
         <oasis:entry colname="col2"><inline-formula><mml:math id="M181" display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="normal">RMS</mml:mi><mml:mi>X</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math id="M182" display="inline"><mml:mi>b</mml:mi></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1">campaign</oasis:entry>  
         <oasis:entry colname="col2">[cm]</oasis:entry>  
         <oasis:entry colname="col3">[cm]</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">L1A</oasis:entry>  
         <oasis:entry colname="col2">9.9</oasis:entry>  
         <oasis:entry colname="col3">0.5 <inline-formula><mml:math id="M183" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 1.0</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2A</oasis:entry>  
         <oasis:entry colname="col2">7.0</oasis:entry>  
         <oasis:entry colname="col3">7.3 <inline-formula><mml:math id="M184" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.9</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2B</oasis:entry>  
         <oasis:entry colname="col2">6.7</oasis:entry>  
         <oasis:entry colname="col3">3.6 <inline-formula><mml:math id="M185" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.9</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2C</oasis:entry>  
         <oasis:entry colname="col2">5.4</oasis:entry>  
         <oasis:entry colname="col3">8.9 <inline-formula><mml:math id="M186" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.8</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3A</oasis:entry>  
         <oasis:entry colname="col2">6.2</oasis:entry>  
         <oasis:entry colname="col3">0.6 <inline-formula><mml:math id="M187" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.9</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3B</oasis:entry>  
         <oasis:entry colname="col2">7.1</oasis:entry>  
         <oasis:entry colname="col3">2.0 <inline-formula><mml:math id="M188" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.8</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3C</oasis:entry>  
         <oasis:entry colname="col2">4.8</oasis:entry>  
         <oasis:entry colname="col3">1.6 <inline-formula><mml:math id="M189" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.7</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3D</oasis:entry>  
         <oasis:entry colname="col2">4.9</oasis:entry>  
         <oasis:entry colname="col3">5.6 <inline-formula><mml:math id="M190" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.7</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3E</oasis:entry>  
         <oasis:entry colname="col2">5.5</oasis:entry>  
         <oasis:entry colname="col3">3.9 <inline-formula><mml:math id="M191" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.7</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3F</oasis:entry>  
         <oasis:entry colname="col2">8.4</oasis:entry>  
         <oasis:entry colname="col3">2.7 <inline-formula><mml:math id="M192" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3G</oasis:entry>  
         <oasis:entry colname="col2">5.4</oasis:entry>  
         <oasis:entry colname="col3">6.1 <inline-formula><mml:math id="M193" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3H</oasis:entry>  
         <oasis:entry colname="col2">5.7</oasis:entry>  
         <oasis:entry colname="col3">3.7 <inline-formula><mml:math id="M194" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3I</oasis:entry>  
         <oasis:entry colname="col2">7.1</oasis:entry>  
         <oasis:entry colname="col3">3.7 <inline-formula><mml:math id="M195" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3J</oasis:entry>  
         <oasis:entry colname="col2">7.0</oasis:entry>  
         <oasis:entry colname="col3">6.2 <inline-formula><mml:math id="M196" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L3K</oasis:entry>  
         <oasis:entry colname="col2">5.5</oasis:entry>  
         <oasis:entry colname="col3">7.4 <inline-formula><mml:math id="M197" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2D</oasis:entry>  
         <oasis:entry colname="col2">6.8</oasis:entry>  
         <oasis:entry colname="col3">9.6 <inline-formula><mml:math id="M198" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2E</oasis:entry>  
         <oasis:entry colname="col2">8.1</oasis:entry>  
         <oasis:entry colname="col3">12.4 <inline-formula><mml:math id="M199" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">L2F</oasis:entry>  
         <oasis:entry colname="col2">7.0</oasis:entry>  
         <oasis:entry colname="col3">9.8 <inline-formula><mml:math id="M200" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.6</oasis:entry>  
         <oasis:entry colname="col4"/>  
         <oasis:entry colname="col5"/>  
         <oasis:entry colname="col6"/>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T4"><caption><p>Apparent trends <inline-formula><mml:math id="M201" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> inferred from different sets of
ICESat laser campaign biases weighted according to their standard deviation
(if given). Results for Hofton (2013) differ from the originally given values
as these authors applied unit weights. The trends in the second column have been calculated using only the laser campaigns <xref ref-type="bibr" rid="bib1.bibx67" id="text.77"/> employed for their study. </p></caption><oasis:table frame="topbot"><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="center"/>
     <oasis:colspec colnum="3" colname="col3" align="center"/>
     <oasis:thead>
       <oasis:row>  
         <oasis:entry colname="col1">Set</oasis:entry>  
         <oasis:entry colname="col2"><inline-formula><mml:math id="M202" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math id="M203" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mrow><mml:mi mathvariant="normal">b</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="normal">L</mml:mi><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="normal">A</mml:mi><mml:mo>-</mml:mo><mml:mi mathvariant="normal">L</mml:mi><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="normal">D</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1"/>  
         <oasis:entry colname="col2">[cm yr<inline-formula><mml:math id="M204" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>]</oasis:entry>  
         <oasis:entry colname="col3">[cm yr<inline-formula><mml:math id="M205" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>]</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">This study</oasis:entry>  
         <oasis:entry colname="col2">1.17 <inline-formula><mml:math id="M206" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.34</oasis:entry>  
         <oasis:entry colname="col3">0.68 <inline-formula><mml:math id="M207" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.41</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Richter (2014)</oasis:entry>  
         <oasis:entry colname="col2">0.66 <inline-formula><mml:math id="M208" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.45</oasis:entry>  
         <oasis:entry colname="col3">0.33 <inline-formula><mml:math id="M209" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.56</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Hofton (2013) 86S</oasis:entry>  
         <oasis:entry colname="col2">1.33 <inline-formula><mml:math id="M210" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.36</oasis:entry>  
         <oasis:entry colname="col3">1.11 <inline-formula><mml:math id="M211" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.46</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Hofton (2013) EAIS</oasis:entry>  
         <oasis:entry colname="col2">1.72 <inline-formula><mml:math id="M212" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.47</oasis:entry>  
         <oasis:entry colname="col3">1.38 <inline-formula><mml:math id="M213" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.53</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Urban (2016)</oasis:entry>  
         <oasis:entry colname="col2">0.01 <inline-formula><mml:math id="M214" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.39</oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math id="M215" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.44 <inline-formula><mml:math id="M216" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.32</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">Zwally (2015)</oasis:entry>  
         <oasis:entry colname="col2">–</oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math id="M217" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.43 <inline-formula><mml:math id="M218" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.44</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><caption><p><bold>(a)</bold> ICESat laser campaign biases (release 34) determined in
the present study in the Lake Vostok region (100–108.5<inline-formula><mml:math id="M219" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E,
76–79<inline-formula><mml:math id="M220" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S) from inter-campaign crossovers and from crossovers with kinematic GNSS profiles (in
dark blue) compared to other recently published sets of biases and their
trends. Error bars represent the standard deviation (if given) for the
respective data set. All bias sets have been reduced by their mean value,
given in the legend. <bold>(b)</bold> Histograms, means and standard deviations
of crossover differences between ICESat and the kinematic GNSS profiles for
four zones of characteristic surface slope. The range of the histograms is
kept fixed to <inline-formula><mml:math id="M221" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula>1 m. The displayed crossover differences contain
uncertainties in the kinematic GNSS profiles (4–9 cm) and possible
elevation changes between the observation epochs of both techniques in
addition to the uncertainty in the ICESat data. <bold>(c)</bold> Monthly averages
of crossover differences between ICESat campaign L3C and the kinematic GNSS
profiles in the region used for the bias determination.</p></caption>
            <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f07.png"/>

          </fig>

      <p>Prior to the validation of ICESat elevation data, we first determine the
ICESat laser campaign biases as described in Sect.
<xref ref-type="sec" rid="Ch1.S3.SS2.SSS2"/>. The resulting biases are given in Table
<xref ref-type="table" rid="Ch1.T3"/>. The simultaneously derived surface elevation
change rate <inline-formula><mml:math id="M222" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> from Eq. (<xref ref-type="disp-formula" rid="Ch1.E4"/>) amounts to
0.0 <inline-formula><mml:math id="M223" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.2 cm yr<inline-formula><mml:math id="M224" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This is new, independent evidence for the
stability of the surface elevation above Lake Vostok. It confirms our results
in Sect. <xref ref-type="sec" rid="Ch1.S2.SS5"/> and those of previous studies
<xref ref-type="bibr" rid="bib1.bibx42 bib1.bibx44" id="paren.78"/>. It also justifies the assumption of a
stable surface made by <xref ref-type="bibr" rid="bib1.bibx17" id="text.79"/> as a precondition for the campaign
bias determination. It is, therefore, not surprising that our biases are very
similar to the updated set of <xref ref-type="bibr" rid="bib1.bibx17" id="text.80"/> for R33 including the
Gaussian-Centroid (G-C) correction, presented by <xref ref-type="bibr" rid="bib1.bibx44" id="text.81"/>. The
major difference is an offset of about 5 cm. This arises from the fact that
in this study, we perform an absolute calibration.</p>
      <p>The chronological sequence of the laser campaign biases implies a trend
<inline-formula><mml:math id="M225" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> which distorts any determination of surface elevation
rates if the biases are not applied. This trend over the entire ICESat
operational period amounts to 1.17 <inline-formula><mml:math id="M226" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.34 cm yr<inline-formula><mml:math id="M227" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>.
Table <xref ref-type="table" rid="Ch1.T4"/> and Fig. <xref ref-type="fig" rid="Ch1.F7"/>a compare
the results of our new set of laser campaign biases with those of recent
publications. For consistency, we limit this comparison to publications using
either R33 data including G-C correction or R34. <xref ref-type="bibr" rid="bib1.bibx27" id="text.82"/> used an
internal crossover adjustment over the low-precipitation zone of the East
Antarctic ice sheet (EAIS) as well as absolute calibration using an ICEBridge
lidar profile along the maximum latitudinal extent of the ICESat mission
(86<inline-formula><mml:math id="M228" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> S). To account for any possible elevation changes, the authors
apply corrections for glacial isostatic adjustment (GIA) and firn
densification. It is interesting to note that, in principle, both sets of their
biases are very similar to our results but their artificial trends
<inline-formula><mml:math id="M229" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> are 0.2–0.6 cm yr<inline-formula><mml:math id="M230" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> larger than ours
(Fig. <xref ref-type="fig" rid="Ch1.F7"/>a, column <inline-formula><mml:math id="M231" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> in
Table <xref ref-type="table" rid="Ch1.T4"/>). This might be due to some unmodelled
effects in the firn densification model and/or GIA correction of
<xref ref-type="bibr" rid="bib1.bibx27" id="text.83"/>. Nevertheless, both of their sets of laser campaign
biases (obtained in different regions of Antarctica and with different
methods) agree with our results within their stated accuracies.</p>
      <p>In contrast, the trends obtained by Urban <xref ref-type="bibr" rid="bib1.bibx51" id="paren.84"><named-content content-type="pre">in</named-content></xref> and
<xref ref-type="bibr" rid="bib1.bibx67" id="text.85"/> from calibrations over the ocean differ significantly
from the results of calibrations over Antarctica. <xref ref-type="bibr" rid="bib1.bibx67" id="text.86"/>
calculated offsets from open water and thin ice in leads and polynyas in
polar sea ice and used them to determine elevation changes over Antarctica.
They obtain an elevation change rate <inline-formula><mml:math id="M232" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> for Lake Vostok of
2.02 cm yr<inline-formula><mml:math id="M233" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This contradicts the results of this study, but also
those of two independent data sets in <xref ref-type="bibr" rid="bib1.bibx44" id="text.87"/>, i.e. static GNSS
observations and kinematic GNSS profiles using snow mobiles
<xref ref-type="bibr" rid="bib1.bibx46" id="paren.88"><named-content content-type="pre">compare</named-content></xref>. It is interesting to note, however, that the
trends implied by our laser campaign biases and those of <xref ref-type="bibr" rid="bib1.bibx67" id="text.89"/>
differ by 2.11 cm yr<inline-formula><mml:math id="M234" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This explains the discrepancies of the
elevation change rates obtained by <xref ref-type="bibr" rid="bib1.bibx67" id="text.90"/> over Lake Vostok as a
result of the applied set of laser campaign biases. The choice of these
biases influences the derivation of elevation change rates from ICESat over
the entire Antarctic ice sheet. Hence this also explains the disparity
between their ICESat-derived mass budget and the mass-balance estimates of
many other studies (e.g. Shepherd et al., 2012; McMillan et al., 2014;
Martin-Espanol et al., 2016), especially in East Antarctica as documented in
Scambos and Shuman (2016) and Richter et al. (2016). Urban et al. (2013) (as
updated in Scambos and Shuman, 2016) obtained significantly smaller biases
using the global ocean as a reference surface. The 2016 paper also discusses
that due to different GLAS sensor saturation levels, those ocean-derived
biases are not applicable over a high-albedo ice sheet surface.</p>
      <p>After applying the laser campaign biases as corrections to the ICESat surface
elevations, we calculate the crossover differences with respect to the
kinematic GNSS profiles. The results in Fig. <xref ref-type="fig" rid="Ch1.F7"/>b show
the very high accuracy of the ICESat data, even in the coastal zone. The
crossover differences in the less sloping regions indicate that both data sets
have practically the same precision (compare Table <xref ref-type="table" rid="Ch1.T1"/>).
Here, the bias-corrections have only a minor influence on the standard
deviations (e.g. 11.1 cm for the uncorrected, 10.7 cm for the corrected
data over Lake Vostok) but become much more important when the temporal
distribution of the data is analysed. Close to the coast we observe a small
increase in standard deviation (approx. 30 cm for slopes exceeding
0.5<inline-formula><mml:math id="M235" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>). This might be an effect of the increased surface roughness
which affects the interpolation of the elevation to the crossover point. A
part of this increased noise could also be explained by topographic effects
within the 65 m laser footprint.</p>
      <p>To avoid the influence of surface elevation changes, previous studies as
<xref ref-type="bibr" rid="bib1.bibx57" id="text.91"/> or <xref ref-type="bibr" rid="bib1.bibx29" id="text.92"/> validated only laser campaigns
in very close temporal proximity (within some months) to their profiles. With
a standard deviation of 10–20 cm in the majority of the area, we can
confirm the results of <xref ref-type="bibr" rid="bib1.bibx29" id="text.93"/>. However, due to the different
ICESat release versions used, their mean offsets are not comparable to our
results. <xref ref-type="bibr" rid="bib1.bibx57" id="text.94"/> use measurements on snowmobiles near
Greenland summit for a similar validation. Their spread of ICESat – GPS
differences is significantly lower than in our study. However, their
assessment is limited to a single ICESat repeat pass section of 6 km length.
In contrast to those studies, our profiles cover a much longer temporal
range. This allows us to pinpoint the maximum range of elevation changes
<inline-formula><mml:math id="M236" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> in this area to very tight limits. Hence, we do not correct for
elevation changes in this comparison. Especially in the coastal zone, this
could explain the increased offset as well as the larger noise of the
crossovers. The obtained offset and standard deviation, in turn, constrain
the magnitude of possible elevation changes in these zones in addition to the
results in Sect. <xref ref-type="sec" rid="Ch1.S2.SS5"/>.</p>
      <p>A deeper view into the temporal variability of the crossover differences in
the Lake Vostok region is given in Fig. <xref ref-type="fig" rid="Ch1.F7"/>c. To show the
variability during the different GNSS seasons, we selected a single ICESat
campaign (L3C, which has the highest precision RMS<inline-formula><mml:math id="M237" display="inline"><mml:msub><mml:mi/><mml:mi>X</mml:mi></mml:msub></mml:math></inline-formula>; see
Table <xref ref-type="table" rid="Ch1.T3"/>) as reference and analysed the spread of the
crossovers over time. The monthly averages vary by less than 10 cm and,
within their standard deviations, nearly all of them can be considered to be
zero. The spread of the values is very likely a result of the remaining
uncertainties of the antenna height reduction in the GNSS profiles.
Interannual variations in accumulation <xref ref-type="bibr" rid="bib1.bibx14" id="paren.95"><named-content content-type="post"><inline-formula><mml:math id="M238" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> mm yr<inline-formula><mml:math id="M239" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula></named-content></xref> or a water discharge from Lake Vostok
<xref ref-type="bibr" rid="bib1.bibx45" id="paren.96"/> can be ruled out as possible causes. Due to the long
temporal base, those data sets nevertheless allow a precise trend
<inline-formula><mml:math id="M240" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> of <inline-formula><mml:math id="M241" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.4 <inline-formula><mml:math id="M242" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.4 cm yr<inline-formula><mml:math id="M243" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> to be derived. Together with the result of
Sect. <xref ref-type="sec" rid="Ch1.S2.SS5"/> and the estimate for the surface elevation change
rate <inline-formula><mml:math id="M244" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula>, obtained from Eq. (<xref ref-type="disp-formula" rid="Ch1.E4"/>) in the laser
campaign bias estimation, those are three very consistent results from
different methods of obtaining <inline-formula><mml:math id="M245" display="inline"><mml:mover accent="true"><mml:mi>h</mml:mi><mml:mo mathvariant="normal">˙</mml:mo></mml:mover></mml:math></inline-formula> from our GNSS profiles.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S4">
  <title>Validation of digital elevation models</title>
<sec id="Ch1.S4.SS1">
  <title>Data</title>
      <p>Our kinematic GNSS profiles allow us to validate not only altimetric surface
elevations but also derived products such as gridded digital elevation models
(DEMs). These products are used in a wide range of applications in polar
sciences. In some cases, such as the topographic correction in repeat track
analysis <xref ref-type="bibr" rid="bib1.bibx37" id="paren.97"/> or the estimation of drainage basins
<xref ref-type="bibr" rid="bib1.bibx65" id="paren.98"/>, only the precision of elevation differences between
neighbouring cells is important. Other applications, such as the derivation
of ice thickness at the grounding line <xref ref-type="bibr" rid="bib1.bibx48" id="paren.99"/>, depend on the
absolute accuracy.</p>
      <p>We validate four DEMs of Antarctica derived from satellite altimetry. The
500 m resolution DEM from data of the ICESat mission by
<xref ref-type="bibr" rid="bib1.bibx13" id="text.100"/> (further called ICESat-DEM) was a milestone for many
applications. Compared to previous, SRA-based DEMs, it provided a “greater
latitudinal extent and fewer slope-related effects”. Nevertheless, a weak
spot was the coarse cross-track spacing, especially for applications in
coastal regions. The DEM provided by <xref ref-type="bibr" rid="bib1.bibx3" id="text.101"/> (Bamber-DEM)
overcame this problem by combining the high accuracy of ICESat with the high
spatial resolution of ERS-1. The DEM produced by the Bedmap2 project
(Bedmap2-DEM) combined the Bamber-DEM with regional models in the margins,
the ice shelves and the Antarctic Peninsula <xref ref-type="bibr" rid="bib1.bibx19" id="paren.102"/>. To make
the Bedmap2-DEM comparable, we converted the elevations from the GL04C geoid
to the WGS-84 ellipsoid reference surface. Even though it should be identical
to the Bamber-DEM for the major part of the region, we included this model to
show the loss of accuracy by rounding the elevations towards integer metres
as has been done for Bedmap2.</p>
      <p>In addition to these ICESat-dominated DEMs, <xref ref-type="bibr" rid="bib1.bibx26" id="text.103"/> compiled the
first 3 years of the CryoSat-2 mission to a new DEM (CryoSat-DEM). With its
improved design, the radar altimeter of CryoSat-2 is capable to provide very
precise elevations in the margins. Furthermore, the high data density due to
the orbit configuration allows for a very homogeneous data set. There is
almost no need to fill data gaps due to the very small across-track spacing.</p>
</sec>
<sec id="Ch1.S4.SS2">
  <title>Methods</title>
      <p>By interpolating the DEM grid to the positions of the individual GNSS
measurements using bicubic interpolation, we obtain an elevation difference
for every single GNSS data location. Hence, the DEM validation relies on many
more elevation differences than the validation of the altimetry profiles
themselves, where the heights could only be compared at crossover locations.</p>
      <p>To facilitate the comparison with the results from
Sect. <xref ref-type="sec" rid="Ch1.S3"/>, we subdivide these elevation
differences into the same zones described in Sect. <xref ref-type="sec" rid="Ch1.S3.SS2.SSS1"/>.
In the validation of DEMs, special attention has to be paid to interpolation
errors. The high resolution of 500 m of the ICESat-DEM seems reasonable when
working with cells which contain measurements. However, no data exist within
the almost 20 km gaps between the altimeter tracks. Thus, for a closer look
into these interpolation errors, we examine the dependence of the elevation
differences from the distance to the nearest track.</p>
</sec>
<sec id="Ch1.S4.SS3">
  <title>Results</title>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><caption><p>Histograms, means and standard deviations of differences between
four different DEMs and kinematic GNSS profiles for four zones of
characteristic surface slope.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f08.pdf"/>

        </fig>

      <p>The results of the validation (Fig. <xref ref-type="fig" rid="Ch1.F8"/>) of the ICESat-DEM
show that over Lake Vostok the accuracy is close to that of the original
ICESat elevations. This indicates that in this case of exceptionally smooth
topography the interpolation error is negligible. However, with increasing
slope the standard deviation of this DEM grows fast due to the scarce
across-track spacing of the altimetric profiles. In the Bamber-DEM, the
inclusion of the additional ERS-1 data reduces this interpolation error
between the ICESat tracks by 50 % in terms of standard deviation. In the
coastal zone, the gain in accuracy is minor as the precision of the radar
altimetry data deteriorates.</p>
      <p>The comparison of the Bedmap2-DEM with the Bamber-DEM reveals remarkable
differences. Firstly, the rounding to integer elevations in Bedmap2 increases
the standard deviation by several decimetres. Secondly, a constant offset of
<inline-formula><mml:math id="M246" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1 m becomes evident in the Bedmap2 data set. This seems to be an issue in
the compilation procedure as the original Bamber-DEM shows a good agreement
in terms of mean difference with our GNSS profiles in all regions. Finally,
in the coastal zone the two models behave differently. In Bedmap2 regional
elevation models have been included here, but the sparse sampling of these
areas by our profiles (see Fig. <xref ref-type="fig" rid="Ch1.F3"/>) does not allow
for a representative evaluation.</p>
      <p>The comparison of the CryoSat-DEM with the ICESat-based models proves that
SRA with the advanced instrument design is able to provide accurate elevation
information even in steep topography too. As for the CryoSat-2 altimetry
data, a slope-dependent offset is observed which presumably results from the
systematic underrepresentation of local depressions.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9"><caption><p>Median of absolute differences between various DEMs and the
kinematic GNSS profiles binned by surface slope (thick black line).
<bold>(a–b)</bold> Additionally for DEMs based on ICESat – coloured lines show
the differences for several ranges of distances to the laser altimeter tracks
(colour coded). <bold>(c)</bold> For the CryoSat-DEM the magenta line shows the
estimated error given by the uncertainty map which comes with the DEM.</p></caption>
          <?xmltex \igopts{width=213.395669pt}?><graphic xlink:href="https://tc.copernicus.org/articles/11/1111/2017/tc-11-1111-2017-f09.pdf"/>

        </fig>

      <p>In order to shed light on the relation of the DEM accuracy with the surface
slope, the median absolute deviations (DEM vs. kinematic GNSS) are binned in
0.1 <inline-formula><mml:math id="M247" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> slope intervals (Fig. <xref ref-type="fig" rid="Ch1.F9"/>). The medians
of the entire set of deviations (thick black lines) reveal a significant
increase with the slope. Splitting the deviations into subsets according to
the distance to the nearest ICESat track the impact of the interpolation
error on a particular DEM becomes evident (panels a, b). It demonstrates the
much greater dependence of the ICESat-DEM on the across-track distance
compared to the Bamber-DEM. While the ICESat-DEM yields superior accuracy
close to the tracks (i.e. distances <inline-formula><mml:math id="M248" display="inline"><mml:mo>&lt;</mml:mo></mml:math></inline-formula> 1 km) due to its small grid
interval (500 m), its median deviations exceed 10 m at large slopes
(<inline-formula><mml:math id="M249" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 0.5<inline-formula><mml:math id="M250" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>) and distances (<inline-formula><mml:math id="M251" display="inline"><mml:mo>&gt;</mml:mo></mml:math></inline-formula> 6 km).</p>
      <p>The dense spatial sampling of the CryoSat-2 altimetry data usually yields
observed elevations for each cell of the CryoSat-DEM. According to the
histograms obtained for the four zones, the slightly larger deviations of
this DEM compared to the other models are mainly due to the slope-dependent
offset. <xref ref-type="bibr" rid="bib1.bibx26" id="text.104"/> provide an error map based on a validation with
ICESat and airborne elevation data. These uncertainties are shown in
Fig. <xref ref-type="fig" rid="Ch1.F9"/>c as a function of slope. Their good agreement
with our results confirms them as realistic.</p>
</sec>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <title>Conclusions</title>
      <p>Between 2001 and 2015 we logged kinematic GNSS data along nine scientific
convoys and derived more than 30,000 km of surface elevation profiles. We
resolved the challenges of the GNSS processing, such as the very long
baselines and peculiar vehicle dynamics in soft snow. Our elevation profiles
have accuracies between 4 and 9 cm for a single data point. Over Lake Vostok
crossover differences yield a mean elevation change rate of
<inline-formula><mml:math id="M252" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.1 <inline-formula><mml:math id="M253" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.5 cm yr<inline-formula><mml:math id="M254" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This confirms the results of
<xref ref-type="bibr" rid="bib1.bibx44" id="text.105"/> and qualifies this area as a calibration site for
satellite altimetry.</p>
      <p>A crossover analysis with three different Envisat elevation data sets reveals
the impact of different processing strategies in satellite radar altimetry.
Concerning the slope correction, the relocation method is clearly superior to
the direct method, reducing elevation errors by about 66 % in terms of
standard deviation. Threshold retrackers (ICE1/OCOG) outperform functional
fit retrackers by up to 50 % in standard deviation. A similar analysis with
CryoSat-2 LRM mode data confirms this finding. Hence, we recommend threshold
retrackers for the determination of elevation time series because of its
significant suppression of the snowpack-related pseudo elevation variations.</p>
      <p>ICESat elevation data and our kinematic GNSS profiles are comparable in their
accuracy, even close to the coast. This comparison also constrains the
magnitude of temporal elevation changes. A combined crossover adjustment
above Lake Vostok yields a new set of ICESat laser campaign biases that no
longer depends on an a priori assumption of a stable surface elevation. The
surface elevation change rate of 0.0 <inline-formula><mml:math id="M255" display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 0.2 cm yr<inline-formula><mml:math id="M256" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, obtained
here, nevertheless proves that this assumption is correct to a very high level of
certainty. The correction of ICESat elevation data for the laser campaign
biases is crucial for estimates of surface elevation change rates and the
according mass balance. The discrepancy of the bias-induced trend between
<xref ref-type="bibr" rid="bib1.bibx67" id="text.106"/> and our result as well as other recent studies
<xref ref-type="bibr" rid="bib1.bibx27 bib1.bibx44" id="paren.107"/> is approximately <inline-formula><mml:math id="M257" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>2 cm yr<inline-formula><mml:math id="M258" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. This
is very likely the cause for the significantly more positive Antarctic ice
mass balance estimate from ICESat obtained by <xref ref-type="bibr" rid="bib1.bibx67" id="text.108"/> compared to
other authors <xref ref-type="bibr" rid="bib1.bibx51" id="paren.109"><named-content content-type="pre">see</named-content></xref>.</p>
      <p>The validation of four digital elevation models demonstrates the reduction of
interpolation errors achieved by <xref ref-type="bibr" rid="bib1.bibx3" id="text.110"/> by complementing ICESat
elevations with radar altimetry data. The advanced instrument design and high
spatial resolution of CryoSat-2 now permits radar altimetry to provide DEMs
<xref ref-type="bibr" rid="bib1.bibx26" id="paren.111"/> of similar accuracy, avoiding extensive interpolation.
<?xmltex \hack{\newpage}?></p>
</sec>

      
      </body>
    <back><notes notes-type="dataavailability">

      <p>The full set of surface elevation profiles
obtained from kinematic GNSS measurements is available for download on the
data server PANGAEA (<uri>https://doi.org/10.1594/PANGAEA.869761</uri>).</p>
  </notes><notes notes-type="competinginterests">

      <p>The authors declare that they have no conflict of
interest.</p>
  </notes><ack><title>Acknowledgements</title><p>This work is supported by the Deutsche Bundesstiftung Umwelt (DBU, German
Federal Environmental Foundation). The fieldwork was partly funded by the
German Research Foundation DFG (grants DI 473/20; DI 473/34; DI 473/38;
SCHE1426/20-1) and the Russian Foundation for Basic Research (grant
10-05-91330-NNIO-a). We also thank the participants of the Russian Antarctic
Expedition, especially the convoy teams, for their valuable support. We thank
the NASA Goddard Space Flight Center, the European Space Agency and the
National Snow and Ice Data Center for providing the altimetry data products.
We are grateful for the contributions of the editor E. Berthier, the reviewer
J. Nilsson and two anonymous reviewers, which helped to improve and to
clarify the manuscript.<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>Edited by: E. Berthier
<?xmltex \hack{\newline}?> Reviewed by: J. N. Nilsson and two anonymous referees</p></ack><ref-list>
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