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  <front>
    <journal-meta>
<journal-id journal-id-type="publisher">GMD</journal-id>
<journal-title-group>
<journal-title>Geoscientific Model Development</journal-title>
<abbrev-journal-title abbrev-type="publisher">GMD</abbrev-journal-title>
<abbrev-journal-title abbrev-type="nlm-ta">Geosci. Model Dev.</abbrev-journal-title>
</journal-title-group>
<issn pub-type="epub">1991-9603</issn>
<publisher><publisher-name>Copernicus Publications</publisher-name>
<publisher-loc>Göttingen, Germany</publisher-loc>
</publisher>
</journal-meta>

    <article-meta>
      <article-id pub-id-type="doi">10.5194/gmd-9-2549-2016</article-id><title-group><article-title>Comparison of adjoint and nudging methods to initialise ice sheet model basal conditions</article-title>
      </title-group><?xmltex \runningtitle{Initialisation of ice sheet model basal conditions}?><?xmltex \runningauthor{C. Mosbeux et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1 aff2">
          <name><surname>Mosbeux</surname><given-names>Cyrille</given-names></name>
          <email>cyrille.mosbeux@lgge.obs.ujf-grenoble.fr</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Gillet-Chaulet</surname><given-names>Fabien</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff2">
          <name><surname>Gagliardini</surname><given-names>Olivier</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>CNRS, LGGE, 38041 Grenoble, France</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Univ. Grenoble Alpes, LGGE, 38401 Grenoble, France</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Cyrille Mosbeux (cyrille.mosbeux@lgge.obs.ujf-grenoble.fr)</corresp></author-notes><pub-date><day>27</day><month>July</month><year>2016</year></pub-date>
      
      <volume>9</volume>
      <issue>7</issue>
      <fpage>2549</fpage><lpage>2562</lpage>
      <history>
        <date date-type="received"><day>12</day><month>January</month><year>2016</year></date>
           <date date-type="rev-request"><day>28</day><month>January</month><year>2016</year></date>
           <date date-type="rev-recd"><day>20</day><month>May</month><year>2016</year></date>
           <date date-type="accepted"><day>6</day><month>June</month><year>2016</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://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016.html">This article is available from https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016.html</self-uri>
<self-uri xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016.pdf">The full text article is available as a PDF file from https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016.pdf</self-uri>


      <abstract>
    <p>Ice flow models are now routinely used to forecast the ice sheets'
contribution to 21st century sea-level rise. For such short term simulations,
the model response is greatly affected by the initial conditions. Data
assimilation algorithms have been developed to invert for the friction of the
ice on its bedrock using observed surface velocities. A drawback of these
methods is that remaining uncertainties, especially in the bedrock elevation,
lead to non-physical ice flux divergence anomalies resulting in undesirable
transient effects. In this study, we compare two different assimilation
algorithms based on adjoints and nudging to constrain both bedrock friction
and elevation. Using synthetic twin experiments with realistic observation
errors, we show that the two algorithms lead to similar performances in
reconstructing both variables and allow the flux divergence anomalies to be
significantly reduced.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>Robustly reproducing the responsible mechanisms and forecasting the
ice sheets' contribution to 21st century sea-level rise is one of the major
challenges in ice sheet and ice flow modelling as highlighted by
community-organised efforts such as SeaRISE (Sea-level Response to Ice Sheet
Evolution) <xref ref-type="bibr" rid="bib1.bibx5 bib1.bibx28 bib1.bibx29" id="paren.1"/> or ice2sea
<xref ref-type="bibr" rid="bib1.bibx15 bib1.bibx36 bib1.bibx9" id="paren.2"><named-content content-type="pre">e.g.</named-content></xref>.</p>
      <p>Such projections on decadal timescales are sensitive to the model initial
state which can account for an important source of uncertainty in the model
response <xref ref-type="bibr" rid="bib1.bibx1" id="paren.3"/>. Improving the reliability of the
model projections requires the model initial state to be better constrained
from observations. The problem is that observations are often uncertain,
sparse in time and space, and indirect, so that the model state depends on
many poorly determined physical parameters and boundary conditions.
Gradient-based optimisation methods, such as the control method
<xref ref-type="bibr" rid="bib1.bibx24" id="paren.4"/> or the Robin inverse method
<xref ref-type="bibr" rid="bib1.bibx2" id="paren.5"/>, are efficient means to constrain such
model parameters and boundary conditions. These methods have been implemented
and applied with success in ice flow models of different complexity in order
to infer the basal drag, one of the most uncertain model parameters
<xref ref-type="bibr" rid="bib1.bibx26 bib1.bibx19 bib1.bibx34 bib1.bibx15" id="paren.6"><named-content content-type="pre">e.g.</named-content></xref>.</p>
      <p>However, remaining uncertainties lead to non-physical ice flux divergence
anomalies <xref ref-type="bibr" rid="bib1.bibx35" id="paren.7"/> resulting in undesirable transient
effects in the free surface evolution. A solution to dissipate these
transients is to conduct a surface relaxation step prior to the projections
<xref ref-type="bibr" rid="bib1.bibx15" id="paren.8"/>. This allows admissible flux divergence
rates to be reached but at the expense of the accuracy of the modelled
surface elevation and surface velocities which can then depart significantly
from observations after the relaxation step.</p>
      <p>Among the remaining uncertainties, one of the most important is the
uncertainty related to the bedrock elevation. The basal topography is derived
from ice thickness measurements, mostly obtained from airborne ice-penetrating
radars. These measurements can have large uncertainties and are
usually at a lower resolution than required model grids
<xref ref-type="bibr" rid="bib1.bibx8" id="paren.9"/>. Standard bedrock elevation maps for Antarctica
and Greenland are then produced by interpolation or Kriging, and report
standard errors ranging from a few tens of metres to several hundreds of metres
depending on the distance to observations and local topographic variability
<xref ref-type="bibr" rid="bib1.bibx11 bib1.bibx3" id="paren.10"/>. For comparison, the
uncertainty on the surface elevation is usually 1 order of magnitude lower
<xref ref-type="bibr" rid="bib1.bibx11" id="paren.11"/>.</p>
      <p>Because of theses large uncertainties, several methods have been proposed to
consider the bedrock elevation as an optimisation variable. For example,
<xref ref-type="bibr" rid="bib1.bibx27" id="text.12"/> derived the adjoint of the continuity equation for
the ice thickness. The depth-averaged velocities and surface mass balance are
then optimised to minimise the mismatch between modelled and measured ice
thicknesses. Surface velocity measurements are used as initial guess for
depth-averaged velocities, and (by construction) the flux divergence produced
by this approach is in equilibrium with the prescribed surface mass balance.
However, there is no constraint that the optimised velocities are a solution
of the stress equilibrium equations, so that, in general, the above method
does not guarantee that the flow divergence anomalies resulting from an ice
flow model initialised with the optimised fields will be reduced.</p>
      <p>In their work, <xref ref-type="bibr" rid="bib1.bibx38" id="text.13"/> developed an iterative algorithm where the
discrepancy between the surface elevation predicted by the model and the
observations is used to correct the bedrock elevation. Thus, the method does
not rely on the accurate computation of the derivative of a cost function, as
in a control method, and is then more similar to nudging methods that have
been widely studied in the past decades in meteorology
<xref ref-type="bibr" rid="bib1.bibx18" id="paren.14"><named-content content-type="pre">e.g.</named-content></xref> and later in oceanography
<xref ref-type="bibr" rid="bib1.bibx39 bib1.bibx6" id="paren.15"/>. However, the method
proposed by <xref ref-type="bibr" rid="bib1.bibx38" id="text.16"/> does not use observed surface
velocities to control the model parameters.</p>
      <p>Several methods have been explored to construct model states where both the
basal friction and the basal topography are treated as optimisation
variables. In a pioneer work, <xref ref-type="bibr" rid="bib1.bibx37" id="text.17"/> developed a
least-squares inversion using analytical solutions for the transmission of
small-scale basal perturbations to the ice surface. This method has been
extended in a non-linear Bayesian framework by
<xref ref-type="bibr" rid="bib1.bibx33" id="text.18"/> and applied to an Antarctic ice stream by
<xref ref-type="bibr" rid="bib1.bibx32" id="text.19"/>. <xref ref-type="bibr" rid="bib1.bibx7" id="text.20"/> have tested the
performances of an ensemble Kalman filter on twin experiments using a
shallow-ice flowline model. The adjoint method has been tested by
<xref ref-type="bibr" rid="bib1.bibx16" id="text.21"/> and <xref ref-type="bibr" rid="bib1.bibx30" id="text.22"/> with models
of different complexity. All these methods usually show good performance in
reconstructing both basal friction and basal topography when using
observations of both surface elevation and surface velocities, so that mixing
between the two variables does not seem to be too problematic for realistic
applications <xref ref-type="bibr" rid="bib1.bibx17" id="paren.23"/>. In addition,
<xref ref-type="bibr" rid="bib1.bibx32" id="text.24"/> and <xref ref-type="bibr" rid="bib1.bibx30" id="text.25"/> show better
performance when the rates of surface elevation change are also constrained
from observations.</p>
      <p>In this paper, we explore two different algorithms to infer both the basal
friction and the basal topography and initialise the model state using
simultaneous observations at a given time. The first algorithm is in line
with <xref ref-type="bibr" rid="bib1.bibx16" id="text.26"/> and <xref ref-type="bibr" rid="bib1.bibx30" id="text.27"/> since it
uses the adjoint solution of the force balance equation. We use the shallow
shelf approximation to facilitate the derivation of the adjoint. Indeed, in
this case the ice thickness appears as a state variable, while it changes the
geometry of the domain for higher order approximations
<xref ref-type="bibr" rid="bib1.bibx30" id="paren.28"/>. In its simplest formulation, the algorithm
minimises the misfit between model and observed surface velocities, but an
additional constraint where the flux divergence is close to a given surface
mass balance can be added. The second method is an algorithm combining
inversion of basal friction using the adjoint method and nudging of the
bedrock topography. The control from the surface velocity observations is
imposed by the adjoint step while the nudging step allows to decrease the
discrepancy between the flux divergence and the surface mass balance. The
main motivation of this second algorithm is its ease of implementation as no
inversion of the model with respect to the ice thickness is required. Our
objective is then to illustrate its ability to reconstruct the bedrock
topography by comparison with the results of the more mathematically founded
first algorithm. Both algorithms are implemented in the finite element
ice sheet/ice flow model Elmer/Ice <xref ref-type="bibr" rid="bib1.bibx13" id="paren.29"/>. The
methods and algorithms are described in details in Sect. <xref ref-type="sec" rid="Ch1.S2"/>. To
test their performances, we design a twin experiment in Sect. <xref ref-type="sec" rid="Ch1.S3"/>. The
results are discussed in Sect. <xref ref-type="sec" rid="Ch1.S4"/>.</p>
</sec>
<sec id="Ch1.S2">
  <title>Methods</title>
<sec id="Ch1.S2.SS1">
  <title>Direct model</title>
      <p>For the force balance, we use the standard vertically integrated shallow
shelf approximation (SSA) equations <xref ref-type="bibr" rid="bib1.bibx23" id="paren.30"/>. This
approximation neglects the effects of vertical shearing and is, hence, more
adapted to model the flow in areas where the friction is low, resulting in an
ice motion dominated by sliding. The horizontal velocity field <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mi>u</mml:mi><mml:mo>,</mml:mo><mml:mi>v</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is a
solution of

                <disp-formula specific-use="align" content-type="numbered"><mml:math display="block"><mml:mtable displaystyle="true"><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mo>∂</mml:mo><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mfenced close=")" open="("><mml:mn mathvariant="normal">2</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mfenced close=")" open="("><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mo>∂</mml:mo><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mfenced open="(" close=")"><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mspace linebreak="nobreak" width="1em"/><mml:mo>-</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mi>u</mml:mi><mml:mo>=</mml:mo><mml:mi mathvariant="italic">ρ</mml:mi><mml:mi>g</mml:mi><mml:mi>H</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>s</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mo>∂</mml:mo><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mfenced close=")" open="("><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mo>∂</mml:mo><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mfenced open="(" close=")"><mml:mn mathvariant="normal">2</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced></mml:mrow></mml:mtd></mml:mtr><mml:mlabeledtr id="Ch1.E1"><mml:mtd/><mml:mtd/><mml:mtd><mml:mrow><mml:mspace width="1em" linebreak="nobreak"/><mml:mo>-</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mi>v</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>i</mml:mtext></mml:msub><mml:mi>g</mml:mi><mml:mi>H</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>s</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula>

            where <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> is the friction coefficient, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ν</mml:mi></mml:math></inline-formula> the vertically averaged
effective viscosity, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>i</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> the ice density, <inline-formula><mml:math display="inline"><mml:mi>g</mml:mi></mml:math></inline-formula> the gravity, and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>H</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>s</mml:mtext></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> the thickness, with <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>s</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> the top and bottom surface
elevations, respectively.</p>
      <p>Natural boundaries are the calving fronts where the Neumann condition results
from the difference between the ice pressure and the sea water pressure:

                <disp-formula specific-use="align" content-type="numbered"><mml:math display="block"><mml:mtable displaystyle="true"><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>n</mml:mi><mml:mi>x</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>n</mml:mi><mml:mi>x</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>(</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo><mml:msub><mml:mi>n</mml:mi><mml:mi>y</mml:mi></mml:msub></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mspace width="1em" linebreak="nobreak"/><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>i</mml:mtext></mml:msub><mml:mi>g</mml:mi><mml:mi>H</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>w</mml:mtext></mml:msub><mml:mi>g</mml:mi><mml:msub><mml:mi>H</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:msub><mml:mi>n</mml:mi><mml:mi>x</mml:mi></mml:msub></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mn mathvariant="normal">4</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>n</mml:mi><mml:mi>y</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>n</mml:mi><mml:mi>y</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:mi>H</mml:mi><mml:mi mathvariant="italic">ν</mml:mi><mml:mo>(</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>v</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo><mml:msub><mml:mi>n</mml:mi><mml:mi>x</mml:mi></mml:msub></mml:mrow></mml:mtd></mml:mtr><mml:mlabeledtr id="Ch1.E2"><mml:mtd/><mml:mtd/><mml:mtd><mml:mrow><mml:mspace linebreak="nobreak" width="1em"/><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>i</mml:mtext></mml:msub><mml:mi>g</mml:mi><mml:mi>H</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>w</mml:mtext></mml:msub><mml:mi>g</mml:mi><mml:msub><mml:mi>H</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:msub><mml:mi>n</mml:mi><mml:mi>y</mml:mi></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula>

            where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>w</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the water density, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> the ice thickness below sea
level, and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>n</mml:mi><mml:mi>x</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>n</mml:mi><mml:mi>y</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> the two components of the horizontal unit vector normal
to the calving front. Dirichlet boundary conditions are prescribed for other
non-natural boundaries. The continuity equation for the ice thickness is
given by
            <disp-formula id="Ch1.E3" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mo>(</mml:mo><mml:mi>u</mml:mi><mml:mi>H</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mo>(</mml:mo><mml:mi>v</mml:mi><mml:mi>H</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mi>a</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula> is the surface mass balance and accumulation/ablation at
the bedrock interface is neglected.</p>
</sec>
<sec id="Ch1.S2.SS2">
  <title>Inverse methods</title>
      <p>The objective of the methods is to produce a model state from
Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>) that best fits the observations of surface velocities and
the rates of change of ice thickness. To minimise the discrepancy between the
model and the observations, the optimisation parameter vector <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula>
contains both the basal friction coefficient <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> and the bedrock
elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">p</mml:mi><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mo>,</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>).</p>
<sec id="Ch1.S2.SS2.SSS1">
  <title>Cost functions</title>
      <p>The misfit between the model and the corresponding observations is evaluated
using cost functions. The first cost function measures the difference between
modelled (<inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">u</mml:mi></mml:math></inline-formula>) and observed (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">u</mml:mi><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>) surface velocities:
              <disp-formula id="Ch1.E4" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:munder><mml:mo movablelimits="false">∫</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi></mml:munder><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:mo>(</mml:mo><mml:mi mathvariant="normal">|</mml:mi><mml:mi mathvariant="bold-italic">u</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">u</mml:mi><mml:mtext>obs</mml:mtext></mml:msub><mml:mi mathvariant="normal">|</mml:mi><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mtext>d</mml:mtext><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Γ</mml:mi></mml:math></inline-formula> is the model domain.</p>
      <p>The second cost function measures the misfit between modelled and observed
thickness rates of change:
              <disp-formula id="Ch1.E5" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:munder><mml:mo movablelimits="false">∫</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi></mml:munder><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:msup><mml:mfenced close="]" open="["><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mo>-</mml:mo><mml:msub><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mtext>obs</mml:mtext></mml:msub></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mtext>d</mml:mtext><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>The modelled rate of change of ice thickness <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:math></inline-formula> is
evaluated from Eq. (<xref ref-type="disp-formula" rid="Ch1.E3"/>) as the difference between the flux
divergence solution of Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>) and the prescribed surface mass
balance. Observed rate of change of ice thickness <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> can be estimated from surface elevation trends extracted from
radar altimetry measurements <xref ref-type="bibr" rid="bib1.bibx10" id="paren.31"/>.</p>
      <p>In general, both Eqs. (<xref ref-type="disp-formula" rid="Ch1.E4"/>) and (<xref ref-type="disp-formula" rid="Ch1.E5"/>) could be weighted with
error covariance estimates such as the one of <xref ref-type="bibr" rid="bib1.bibx10" id="text.32"/>.
However, this information is not often available. In this paper, observed
ice surface velocities (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="bold-italic">u</mml:mi><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>) and observed rate of change of
ice thickness <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> are considered
perfectly known or perturbed with a Gaussian noise which would make
unnecessary the addition of a covariance term.</p>
      <p>The objective is then to find the parameter vector <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula> that minimises
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. This can be achieved in different ways as
illustrated in the following sections.</p>
</sec>
<sec id="Ch1.S2.SS2.SSS2">
  <title>Adjoint method</title>
      <p>The two cost functions have an implicit dependence on the parameter vector <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula>
through the model surface velocities <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">u</mml:mi></mml:math></inline-formula> which are solutions of
Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>). The gradient of the cost functions with respect to <inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula> can
be computed efficiently using the adjoint equations of Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>). The
derivation of the continuous adjoint equations and the gradient of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> with respect to the friction coefficient <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> can be found in
<xref ref-type="bibr" rid="bib1.bibx24" id="normal.33"/>. This can be easily extended for the
computation of the gradient with respect to <inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula>.</p>
      <p>The implementation in Elmer/Ice is carried out in a way that stays as close
as possible to the differentiation of the discrete implementation of the
direct equations. This method should lead to a better accuracy on the
gradient computation than the discretisation of the continuous equations.
Elmer/Ice uses programming features that are not supported by automatic
differentiation tools and the differentiation of the crucial parts of the
discrete source code (e.g. cost function computation, matrix assembly) has
been done manually. If the problem is non-linear, as here due to the
dependence of the viscosity to the strain rate, and the non-linearity solved
using a Picard iterative scheme, the iterations should be reversed (at least
partially) in the adjoint code to achieve a good accuracy of the computed
gradient <xref ref-type="bibr" rid="bib1.bibx25" id="paren.34"/>. However, as the present direct solver
is equipped with a Newton linearisation of the ice viscosity so that it
remains self-adjoint <xref ref-type="bibr" rid="bib1.bibx31" id="paren.35"/>, the Newton iterations are
not reversed in the adjoint code and we only keep the last iteration. The
adjoint code has been validated on standard tests by comparing the gradients
with those obtained from a finite difference evaluation. The agreement is
usually better than 0.1 %.</p>
      <p>Inverse problems are often ill-posed, leading to instabilities. It is then
necessary to add regularisation terms to the cost function to avoid
overfitting of data. This can be done in the form of a Tikhonov
regularisation. Here, we define two different regularisations. The first one
measures the norm of the first spatial derivative of the component <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> of
<inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula>, thus allowing to give preference to smooth solutions:</p>
      <p><?xmltex \hack{\newpage}?>
              <disp-formula id="Ch1.E6" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>reg</mml:mtext><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:munder><mml:mo movablelimits="false">∫</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi></mml:munder><mml:msup><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:msub><mml:mi>p</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mfenced close=")" open="("><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:msub><mml:mi>p</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mtext>d</mml:mtext><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            The second forces the optimisation variables to stay close to a certain prior
or background information <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. This background can be based on
observations or on empirical knowledge. This second regularisation term is
written as
              <disp-formula id="Ch1.E7" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>b</mml:mtext><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:munder><mml:mo movablelimits="false">∫</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi></mml:munder><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mtext>p</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>(</mml:mo><mml:msub><mml:mi>p</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>p</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mtext>b</mml:mtext></mml:mrow></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mtext>d</mml:mtext><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">σ</mml:mi><mml:mtext>p</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is a spatial parameter allowing to give more or
less weight to the prior information <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>p</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mtext>b</mml:mtext></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>The computation of the gradients of these two functionals with respect to
<inline-formula><mml:math display="inline"><mml:mi mathvariant="bold-italic">p</mml:mi></mml:math></inline-formula> is trivial. How these regularisation terms are weighted with
respect to the model–data misfit functionals Eqs. (<xref ref-type="disp-formula" rid="Ch1.E4"/>) and
(<xref ref-type="disp-formula" rid="Ch1.E5"/>) is described in more details with the description of the
algorithms in Sec. <xref ref-type="sec" rid="Ch1.S2.SS3"/>.</p>
      <p>This minimisation is achieved using the quasi-Newton routine M1QN3
<xref ref-type="bibr" rid="bib1.bibx14" id="paren.36"/> implemented in Elmer/Ice. This method uses an
approximation of the second derivatives of the cost function and is therefore
more efficient than a fixed-step gradient descent.</p>
</sec>
<sec id="Ch1.S2.SS2.SSS3">
  <title>Nudging method</title>
      <p>By definition, the steady-state solution of Eq. (<xref ref-type="disp-formula" rid="Ch1.E3"/>) where <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula>
is replaced by the apparent mass balance <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>a</mml:mi><mml:mo>-</mml:mo><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the minimum for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. Running the model forward in
time with a constant forcing is then a simple way to minimise <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>,
equivalent to a relaxation step. Here, we assume that the surface elevation is
known so that computed changes in ice thickness are used to correct the
bedrock elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. During this process, the ice thickness can
substantially deviate from observations. Nudging methods, also called
Newtonian relaxation, can remedy to this problem by constraining the
thickness to fit observations through an additional callback term in
Eq. (<xref ref-type="disp-formula" rid="Ch1.E3"/>), which now writes
              <disp-formula id="Ch1.E8" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mo>(</mml:mo><mml:mi>u</mml:mi><mml:mi>H</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mo>(</mml:mo><mml:mi>v</mml:mi><mml:mi>H</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mi>a</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi></mml:mrow><mml:mrow><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>-</mml:mo><mml:mi>k</mml:mi><mml:mo>(</mml:mo><mml:mi>H</mml:mi><mml:mo>-</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where the coefficient <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> defines the amplitude of the callback at each node
of the model. These methods imply a trade-off, adjustable through <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula>,
between model physics and observations. The callback term can depend on many
different criteria such as observation accuracy or distance to observation
<xref ref-type="bibr" rid="bib1.bibx18" id="paren.37"/>. Here, we take <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> as a Gaussian function of
the distance to the closest observation so that the callback is maximum
where an observation is available and decreases to zero far from all
observations. The choice of the variance for the Gaussian function is
discussed in Sect. <xref ref-type="sec" rid="Ch1.S4.SS2"/>.</p>
</sec>
</sec>
<sec id="Ch1.S2.SS3">
  <title>Algorithms</title>
      <p>From the methods presented in the previous section we design two algorithms
to infer simultaneously the friction coefficient <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> and the bedrock
elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. To ensure that the friction coefficient remains
positive during the inversion, we use the following change of variable
            <disp-formula id="Ch1.E9" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mi mathvariant="italic">α</mml:mi></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
<sec id="Ch1.S2.SS3.SSS1">
  <title>Adjoint method with two parameters (ATP)</title>
      <p>This algorithm uses the gradients of the cost functions derived using the
adjoint method to optimise both <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. For the
regularisation, a constraint on the smoothness is imposed for <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> using
Eq. (<xref ref-type="disp-formula" rid="Ch1.E6"/>) while a constraint on the background information is imposed
for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> using Eq. (<xref ref-type="disp-formula" rid="Ch1.E7"/>). The total cost function then
writes
              <disp-formula id="Ch1.E10" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>ATP</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:mo>,</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub><mml:mo>+</mml:mo><mml:mi mathvariant="italic">γ</mml:mi><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>reg</mml:mtext><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>b</mml:mtext><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> is a constant fixed to give a similar weight to <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>
and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> while <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> are
two constants allowing to adjust the weight given to the regularisation
terms. Following <xref ref-type="bibr" rid="bib1.bibx12" id="text.38"/>, several pairs
(<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) are tested using a L-curve
approach, and optimal values are taken from the combinations that avoid two
extremes: overfitting of the observations or excessive regularisation.</p>
</sec>
<sec id="Ch1.S2.SS3.SSS2">
  <title>Adjoint-nudging coupling (ANC)</title>
      <p>In this algorithm, the adjoint method is first used to optimise <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> only
by minimising the following total cost function
              <disp-formula id="Ch1.E11" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>ANC</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub><mml:mo>+</mml:mo><mml:mi mathvariant="italic">γ</mml:mi><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>reg</mml:mtext><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:msub><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            The bedrock elevation is then updated using the nudging method by solving
Eq. (<xref ref-type="disp-formula" rid="Ch1.E8"/>) for a given time period <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula>. <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> should be neither too
short nor too long to allow to reduce <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> without overfitting
observations. The sensitivity of the method to <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> is discussed in the
results section.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><caption><p>Reference (solid lines) and initial (dashed lines) state for
<bold>(a)</bold> the bedrock elevations <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, <bold>(b)</bold> the estimated
basal traction <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">β</mml:mi><mml:mi>u</mml:mi></mml:mrow></mml:math></inline-formula>, and <bold>(c)</bold> the surface velocities. In
<bold>(a)</bold>, synthetic observations every 10 km are the plain black
circles. In <bold>(c)</bold> the observed velocities are depicted by the
circles and the shaded green curve is the absolute difference between
observed and reference surface velocities (right axis).</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f01.png"/>

          </fig>

      <p>These two steps are then repeated iteratively until changes in <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>
and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> between two iterations are less than 1 %.</p>
</sec>
</sec>
</sec>
<sec id="Ch1.S3">
  <title>Manufactured data sets</title>
      <p>A twin experiment is designed to investigate the ability of the two methods
to reproduce simultaneously good estimates of the basal friction coefficient
and the bedrock elevation. A flowline geometry is preferred to reduce the
computational cost and easily test the method, however all the algorithms can
be applied to 2-D plane view simulations. A reference experiment for which
all the model parameters are prescribed is produced to generate synthetic
observations. These observations are then used to test the performances of
the two algorithms.</p>
<sec id="Ch1.S3.SS1">
  <title>Reference experiment</title>
      <p>A flowline of Jakobshavn Glacier, Greenland, is used to test the two
algorithms with realistic conditions. Jakobshavn Isbrae is one of Greenland's
three largest outlet glaciers and has one of the largest drainage basin on
the ice sheet's western margin <xref ref-type="bibr" rid="bib1.bibx4" id="paren.39"/>. It is
also the fastest Greenland glacier with a terminus velocity greater than
13 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">km</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx20 bib1.bibx22" id="paren.40"/>. The
flowline is 550 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> long and runs from the ice divide to the ice
front. The surface and bedrock elevations are taken from available digital
elevation models <xref ref-type="bibr" rid="bib1.bibx3" id="paren.41"/>. The basal friction coefficient
field is first adjusted so that the model velocities fit observed velocities
<xref ref-type="bibr" rid="bib1.bibx21" id="paren.42"/>. To have realistic thickness rates of change,
the free surface is relaxed to steady state. The surface mass balance <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula> in
Eq. (<xref ref-type="disp-formula" rid="Ch1.E3"/>) has been calibrated so that the steady state is close
to the initial geometry, and is meant to take into account the flow
convergence or divergence along the flowline. The steady-state solution is
used as the reference of the twin experiment.</p>
      <p>The geometry is discretised through a mesh of 500 linear elements,
increasingly refined to the front of the glacier. The element size decreases
from <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 2 km in the upper part of the glacier to <inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 400 m down to
the front.</p>
      <p>Results will only be presented on the first 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> upstream of the
glacier front where velocities are above 100 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and where the
SSA is more appropriate but the inversion is done all along the flowline up
to the ridge.</p><?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S3.SS2">
  <title>Synthetic observations</title>
      <p>Synthetic observations are generated by sampling and/or adding noise to the
reference simulation. Details for each required field are given below. These
synthetic observations and initial fields for the inverse methods are
compared to the reference in Fig. <xref ref-type="fig" rid="Ch1.F1"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2" specific-use="star"><caption><p>Mean error on the thickness rate of change (rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mtext>div</mml:mtext></mml:msub></mml:math></inline-formula>) as a
function of the mean error on velocity (rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mi>u</mml:mi></mml:msub></mml:math></inline-formula>) for the 255 pairs of
regularisation parameters (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>).
Colour scales show the normalised regularisation terms
<bold>(a)</bold> <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>reg</mml:mtext><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and <bold>(b)</bold> <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>
(0 corresponds with the lowest value and 1 with the highest value obtained
with the 255 pairs). The chosen value (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn>11</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn mathvariant="normal">7</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>) is shown with a black circle.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f02.png"/>

        </fig>

<sec id="Ch1.S3.SS2.SSS1">
  <title>Surface velocities</title>
      <p>Surface velocities are assumed to be observed at the same resolution as the
reference simulation but with a white Gaussian noise with a mean <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>
and a standard deviation <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn>50</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. This corresponds to
a root mean squared (rms) error of 47.8 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> for the entire
flowline. The reference and noisy observed surface velocities are shown in
Fig. <xref ref-type="fig" rid="Ch1.F1"/>c together with their absolute difference.</p>
</sec>
<sec id="Ch1.S3.SS2.SSS2">
  <title>Surface mass balance and thickness rate of change</title>
      <p>The surface mass balance, <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula>, and thickness rate of change, <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, in Eq. (<xref ref-type="disp-formula" rid="Ch1.E5"/>) are assumed to be perfectly
observed. As the reference simulation corresponds to a steady state, <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>. However, the methods are also tested in
Sect. <xref ref-type="sec" rid="Ch1.S4.SS3"/> for cases where <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>≠</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula> to show their ability to initialise the model when the
flux divergence is not in equilibrium with the surface mass balance.</p><?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S3.SS2.SSS3">
  <title>Surface and bedrock elevations</title>
      <p>The surface elevation is assumed to be perfectly observed. For the bedrock
elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, we simulate observations representing airborne radar
measurements crossing the flowline. Bedrock elevations are sampled every
10 km with a Gaussian noise centred on zero and with a standard deviation of
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn>50</mml:mn></mml:mrow></mml:math></inline-formula> m. This leads to a rms error of 62.4 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> on the
55 observation points of the entire flowline. This error is similar to the
errors given in practice on recent bedrock elevation maps
<xref ref-type="bibr" rid="bib1.bibx11 bib1.bibx3" id="paren.43"/>. For the mesh nodes between
the observations, the bedrock is linearly interpolated as shown in
Fig. <xref ref-type="fig" rid="Ch1.F1"/>a. This is used as the first guess for the
inverse methods and as the background information for the regularisation in
Eq. (<xref ref-type="disp-formula" rid="Ch1.E7"/>).</p>
</sec>
<sec id="Ch1.S3.SS2.SSS4">
  <title>Model parameters</title>
      <p>The ice viscosity is assumed to be perfectly known and corresponds to the
viscosity used in the reference experiment.</p>
      <p>Assuming that no observation of the friction coefficient is available, an
initial solution has to be postulated. A good first guess for <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> is
provided by using the driving stress to estimate the basal shear stress:
              <disp-formula id="Ch1.E12" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ini</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mi>g</mml:mi><mml:mi>H</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">|</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">|</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">|</mml:mi><mml:mi>u</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">|</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>H</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>u</mml:mi><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> are, respectively, the ice thickness, the
surface slope and the surface velocity at position <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>. The reference and
initial values are shown in Fig. <xref ref-type="fig" rid="Ch1.F1"/>b.</p>
      <p>The rms errors on the surface velocities and the rate of change of ice
thickness between the initial state and the synthetic observations are,
respectively, 761 and 357 m a<inline-formula><mml:math 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>The average relative error on the basal shear stress is measured as
              <disp-formula id="Ch1.E13" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mi>L</mml:mi></mml:mfrac></mml:mstyle><mml:munder><mml:mo movablelimits="false">∫</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi></mml:munder><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub><mml:mi mathvariant="normal">|</mml:mi><mml:mo>-</mml:mo><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub><mml:mi mathvariant="normal">|</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">|</mml:mi><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub><mml:mi mathvariant="normal">|</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mtext>d</mml:mtext><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
            where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the basal shear stress in the reference
experiment and <inline-formula><mml:math display="inline"><mml:mi>L</mml:mi></mml:math></inline-formula> the length of the flowline. The relative error on the
basal shear stress with our initial estimate of the basal friction
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ini</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is 394 %. The performances of the two algorithms in
reducing these initial errors are presented in the following section and will
be compared to these initial errors.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><caption><p>Results of the ATP algorithm with (orange) and without (red)
optimisation of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, i.e. <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>, respectively,
in Eq. (<xref ref-type="disp-formula" rid="Ch1.E10"/>): <bold>(a)</bold> absolute difference between observed and
model velocities, <bold>(b)</bold> estimated basal traction, and
<bold>(c)</bold> estimated bedrock elevation. The green shaded area is the
difference between the noisy reference velocities and the true velocities.
The green solid lines are the reference values and the black dashed line is
the initial guess for the bedrock elevation.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f03.png"/>

          </fig>

</sec>
</sec>
</sec>
<sec id="Ch1.S4">
  <title>Results</title>
<sec id="Ch1.S4.SS1">
  <title>Adjoint method with two parameters (ATP)</title>
      <p>A set of 255 pairs (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) is tested to
adjust the weighting of the regularisation terms of Eq. (<xref ref-type="disp-formula" rid="Ch1.E10"/>). The
misfits on the different cost functions of Eq. (<xref ref-type="disp-formula" rid="Ch1.E10"/>) for the
different pairs (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) is given in
Fig. <xref ref-type="fig" rid="Ch1.F2"/>. Both graphs show that most of the pairs
fitting well the observed velocities can also adequately reproduce the
observed rate of change of the ice thickness.
Figure <xref ref-type="fig" rid="Ch1.F2"/>b also shows that smaller misfits on
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> clearly involve higher rms misfits on the ice surface
velocities (rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mi>u</mml:mi></mml:msub></mml:math></inline-formula>) and on the rate of change of the ice thickness
(rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mtext>div</mml:mtext></mml:msub></mml:math></inline-formula>). On the contrary, Fig. <xref ref-type="fig" rid="Ch1.F2"/>a does
not show a clear relation between the magnitude of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mrow><mml:msub><mml:mtext>reg</mml:mtext><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>
and the magnitude of rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mi>u</mml:mi></mml:msub></mml:math></inline-formula> and rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mtext>div</mml:mtext></mml:msub></mml:math></inline-formula>. Both graphs also show a
high density of pairs for small rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mi>u</mml:mi></mml:msub></mml:math></inline-formula> and rms<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mtext>div</mml:mtext></mml:msub></mml:math></inline-formula>. However, the
pair (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn>11</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn mathvariant="normal">7</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>) seems to
come off the others, giving a good trade off between data fitting and
regularisation. Notice that the constant <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">γ</mml:mi></mml:math></inline-formula> is fixed to 1 since
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> have the same order of magnitude.</p>
      <p>The optimisation of both <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> simultaneously allows a
rms misfit of 49.7 m a<inline-formula><mml:math 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> on velocities to be reached, very similar to
the observation rms error, showing no overfitting of velocity data. The rate
of change of ice thickness misfit is also largely decreased with a rms value
of 19.2 m a<inline-formula><mml:math 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 resulting basal traction <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> as well as the misfit for the surface velocities are given in
Fig. <xref ref-type="fig" rid="Ch1.F3"/>. The basal traction variability is accurately reproduced
with a corresponding average relative misfit of only 25 % along the entire
flowline with respect to the reference basal shear stress
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, i.e. more than a 10-fold decrease of the initial misfit.
We only notice local overestimations of slipperiness in bedrock pits without
significant impacts on the flow velocities. Indeed, under a defined value of
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> corresponding to a nearly perfectly sliding case, an additional
reduction in friction has no impact on the flow. The same reasoning applies
to a nearly perfectly sticky case, where an increased friction would not
involve more decrease of the velocity. The bedrock elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is
well reconstructed in the first 50 km upstream of the glacier front. The
discrepancy with respect to the reference bedrock is larger upstream where
the cost function <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is less sensitive because of lower velocities.
This could possibly be improved by using a cost function measuring the
logarithm of the misfit as in <xref ref-type="bibr" rid="bib1.bibx26" id="text.44"/>, but with a
greater risk of fitting noise since the relative observation error is higher
in these regions.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><caption><p>Results of the ANC algorithm (purple): <bold>(a)</bold> absolute
difference between observed and model velocities, <bold>(b)</bold> estimated
basal traction, and <bold>(c)</bold> estimated bedrock elevation. The green shaded
area is the difference between the noisy reference velocities and the true
velocities. The green solid lines are the reference values and the black
dashed line is the initial guess for the bedrock
elevation.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f04.png"/>

        </fig>

      <p>In order to assess the influence of accounting for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> on the
method, the optimisation is repeated without the <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> term in the
total cost function Eq. (<xref ref-type="disp-formula" rid="Ch1.E10"/>). The pair (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>) is kept equal to the previous case since the optimum
is hardly affected by the absence of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> in the total cost
function. The result is given and compared to the previous one in
Fig. <xref ref-type="fig" rid="Ch1.F3"/>. The friction coefficient <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> is again pretty well
reconstructed, with a corresponding relative average misfit of 31 % on
basal shear stress <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> to be compared to the 25 % obtained with
the optimisation of the <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> term. However, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> shows
non-consistent high frequencies involving a higher discrepancy with respect
to the reference bedrock elevation in the case of optimising
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. Therefore, the optimisation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> has a clear
regularisation effect on the parameter <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, by reducing the
non-consistent high-frequency oscillations of the solution.</p>
      <p>Introduction of a Gaussian noise on <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>
has been investigated in order to assess its effect on the optimisation of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. Different levels of standard deviation <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> have been
tested. Results show that the optimisation is little affected by this noise
even for standard deviations <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> going up to the same order of magnitude
as the surface accumulation <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula>. Introduction of systematic bias on
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> in a physically acceptable range, i.e.
of the same order of magnitude as surface accumulation <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula>, also have
few consequences on the optimisation.</p>
</sec>
<sec id="Ch1.S4.SS2">
  <title>Adjoint-nudging coupling (ANC)</title>
      <p>The steps for the optimisation of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> only are conducted with a value
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">λ</mml:mi><mml:mi mathvariant="italic">α</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn mathvariant="normal">9</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, which allows a good agreement between the
different cost functions and a value <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">γ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>.</p>
      <p>In addition to the regularisation parameters of Eq. (<xref ref-type="disp-formula" rid="Ch1.E11"/>), ANC
algorithm depends on the time period for the nudging steps <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> and the
variance of the Gaussian <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> in Eq. (<xref ref-type="disp-formula" rid="Ch1.E8"/>). The nudging period <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula>
impacts the convergence on <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> after each cycle.
The convergence is substantially similar for <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> from 1 to 4 years. Longer
periods mainly involve a worse minimisation of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>v</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> since there is no
control on velocities during nudging. Shorter relaxation times do not involve
sufficient change of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> inducing a lower minimisation of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>J</mml:mi><mml:mtext>div</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> for a given number of cycles. Therefore, a relaxation time <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> year is adopted, which seems sufficient to allow significant changes of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> without too much adaptation to the previous intermediate value
of the friction coefficient. The algorithm is stopped after 10 cycles,
corresponding to the stopping criterion of Sect. <xref ref-type="sec" rid="Ch1.S2.SS3.SSS2"/>. For a
given <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> period, tests show that variance values of the Gaussian <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> in
Eq. (<xref ref-type="disp-formula" rid="Ch1.E8"/>) larger than 1 km are excessive and induce non-physical
callback amplitudes when departing from observations. After a few cycles,
the resulting bedrock induces an increase between modelled and observed
velocities that cannot be overcome by the basal drag inversion. Variance
smaller than 1 km has little impact on the final result in terms of cost
functions. However, among the acceptable values, the 1 km variance gives the
best agreement between misfit on the surface velocities and misfit on the
rate of change of the ice thickness.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><caption><p>The five new references build from a 5-year perturbation of the
initial reference by an increase of the friction parameter: <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (green), <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (red), <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (blue lines), <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (purple), and
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn>10</mml:mn><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (orange). New references for <bold>(a)</bold> the
thickness rate of change for the different perturbations,
<bold>(b)</bold> velocities (without observation noise), and
<bold>(c)</bold> friction coefficients <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f05.png"/>

        </fig>

      <p>The model is in good agreement with observations with a rms misfit of
46.1 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> in the range of observation noise for velocities, and
15.8 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> for thickness rates of change. The basal shear stress
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is close to the reference one despite exacerbated variations
at some locations. The corresponding relative average misfit with respect to
the reference <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is 30 % for the entire flowline. The
reconstructed bedrock elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is also close to the reference
on almost 100 km upstream of the front of the glacier. This reflects,
especially in fast flowing region, a real improvement of the basal knowledge
with respect to the first guess. Moreover, the use of nudging, instead of the
adjoint method, does not show the same problem of non-sensitivity in regions
of slower flow velocities, as mentioned in Sect. <xref ref-type="sec" rid="Ch1.S4.SS1"/>. Note,
however, that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> significantly departs from the reference bedrock
elevation from 80 to 100 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> to the front, strongly linked to the
poorer fit of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> (see Fig. <xref ref-type="fig" rid="Ch1.F4"/>).</p>
      <p>As for ATP, introduction of a Gaussian noise in the observed thickness rate
of change <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> has also been tested.
Results show no significant impacts on the optimisation. Nevertheless,
introduction of systematic bias in <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>
has direct consequences on the nudging steps inducing an offset of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> of the range of the systematic bias cumulated on the nudging
period <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula>. ANC is therefore more sensitive to systematic bias than ATP.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F6" specific-use="star"><caption><p>Range of values for ATP algorithm for the five perturbations of the
friction coefficient <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>. <bold>(a, b)</bold> Minimum (dark orange shade) and
maximum (light orange shade) of absolute difference between observed and
model velocities and relative error for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, respectively.
<bold>(c)</bold> Range of values for bedrock elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (orange
shade). The green solid line is the reference value and the black dashed line
is the initial guess for the bedrock elevation.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f06.png"/>

        </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F7" specific-use="star"><caption><p>Same as Fig. 5 but for the ANC algorithm.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f07.png"/>

        </fig>

</sec>
<sec id="Ch1.S4.SS3">
  <title>Further sensitivity experiments</title>
      <p>In order to evaluate the efficiency of both algorithms in transient states,
we construct new reference cases where <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>≠</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>. This is achieved by multiplying <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">β</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> by a
factor of 2, 3, 4, 5, and 10. As a consequence, increasing the basal friction
involves a disequilibrium of the glacier, an ice thickening, and a decrease of
ice flow velocities.</p>
      <p>The time period for the glacier to come back to equilibrium, after this
change of friction parameter, depends on the amplitude of the perturbation.
Here, the perturbation is only applied during 5 years in order to keep the
five cases in disequilibrium. Resulting thickness rates of change <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi><mml:msub><mml:mo>)</mml:mo><mml:mtext>obs</mml:mtext></mml:msub><mml:mo>≠</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula> are in the same order of magnitude as the
tuned surface mass balance <inline-formula><mml:math display="inline"><mml:mi>a</mml:mi></mml:math></inline-formula>. The five new reference cases are presented in
Fig. <xref ref-type="fig" rid="Ch1.F5"/>.</p>
      <p>The results of the optimisations for the five cases of perturbation are shown
in Fig. <xref ref-type="fig" rid="Ch1.F6"/> for ATP and
Fig. <xref ref-type="fig" rid="Ch1.F7"/> for ANC. The velocity misfit for ATP
increases with the amplitude of perturbation with rms values between 47.8 and
52.3 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> while the rms misfit for thickness rate of change
increases from 12.7 to 21.8 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. ANC reaches rms misfits from
45.9 to 47.2 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> for velocities and 12.5 to
21.5 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> for thickness rate of change. The friction coefficient
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> is well reconstructed for both methods. The corresponding average
relative error (with respect to each reference) on basal shear stress
varies from 22 to 30 % for ANC and 20 to 28 % for ATP, still according to
the amplitude of the perturbation. Both algorithms also allow to improve the
knowledge of the bedrock elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> with regard to the first
guess. We notice a tendency to overestimate the amplitude of bumps and pits
in some locations which generally corresponds to an underestimation in the
amplitude of variations of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>. This latter behaviour highlights the
limits of the algorithms and the difficulty of distinguishing the effects of
two basal parameters as closely linked as the friction and the bedrock
topography. This behaviour had been already highlighted in
<xref ref-type="bibr" rid="bib1.bibx16" id="text.45"/> and <xref ref-type="bibr" rid="bib1.bibx17" id="text.46"/> where a
higher ice thickness with respect to the reference is compensated by a higher
basal friction, and conversely as well.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><caption><p>Evolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∂</mml:mo><mml:mi>H</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>t</mml:mi></mml:mrow></mml:math></inline-formula> after 1 year <bold>(a)</bold> and
10 years <bold>(b)</bold> of prognostic simulation and the resulting mismatch
after 10 years between surfaces obtained with three different initial states
and reference surface <bold>(c)</bold>. The orange and purple lines give the
results for ATP and ANC. The red line gives the result for inversion of
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f08.png"/>

        </fig>

</sec>
<sec id="Ch1.S4.SS4">
  <title>Flow divergence in transient model</title>
      <p>In this section, we assess the impact of our initialisation algorithms on the
prognostic response of the model forward in time assuming the same constant
forcing used to build the reference state. By doing so, if the initialisation
was perfect, one would expect no change of the geometry and ice flow during
this prognostic simulation. The experiment is performed from ATP and ANC
initial states. A third initialisation state is constructed for which only
the friction coefficient has been optimised, keeping <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> equals to
the a priori <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mrow><mml:msub><mml:mtext>b</mml:mtext><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>. This third initialisation, called
“<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only” involves a rms misfit on velocities of
43.3 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">a</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and an average relative error
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mtext>b,ref</mml:mtext></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> of 36 % on basal shear stress, similar to
the ATP and ANC initial states. However, the rms misfit on the thickness rate
of change is significantly higher, 147.8 m a<inline-formula><mml:math 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>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9"><caption><p>Ice surface elevation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>s</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> after 10 years of prognostic
simulation for three different initial states: initialisation with ATP
algorithm (orange line), with ANC algorithm (purple line), and with the
inversion of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only (red line). The green line is the reference surface
elevation. The figure focuses on the first 50 km next to the front of the
glacier.</p></caption>
          <?xmltex \igopts{width=199.169291pt}?><graphic xlink:href="https://gmd.copernicus.org/articles/9/2549/2016/gmd-9-2549-2016-f09.png"/>

        </fig>

      <p>The prognostic simulations are conducted during a 10-year period in order to see
how the initial thickness rate evolves during this time and how it impacts
the final ice thickness and ice surface. The thickness rates of change after 1
and 10 years of simulation are shown in
Fig. <xref ref-type="fig" rid="Ch1.F8"/>a and b, respectively, while the mismatch
on the surface elevation after 10 years is shown in
Fig. <xref ref-type="fig" rid="Ch1.F8"/>c.</p>
      <p>ANC and ATP initial states involve thickness rates of change much closer to
zero than the optimisation of “<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only”. This also leads to a lower
mismatch <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mtext>s</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> on the surface elevation with respect to the
reference after 10 years of simulation. Indeed, this mismatch is well below
20 m for both ANC and ATP, except on a few kilometres in the upstream
region, whereas the optimisation of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only gives rise to a mismatch
globally above 20 m with some regions exceeding 50 m.</p>
      <p>In that way, the two algorithms implemented in this study show substantial
improvements compared to the optimisation of “<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> only”. We especially
notice a better reproduction of low-scale variations of the surface elevation
due to the transfer of similar variations from the bedrock elevation
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (Fig. <xref ref-type="fig" rid="Ch1.F9"/>). These variations tend to
disappear with the optimisation of the friction only, giving rise to a lower
resolution of the surface. However, we should point out that this direct
transfer of bedrock variations to the surface is a consequence of the SSA
ice flow model used and that a full Stokes model would produce a more
diffusive transfer response.</p>
</sec>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <title>Conclusions</title>
      <p>The presented algorithms allow the reconstruction of two poorly known
parameters: the bedrock topography <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and the friction coefficient
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> at the same time.</p>
      <p>The optimisation of these two parameters mainly relies on the knowledge of
some other data that are easier to measure: ice surface velocities and thickness rates
of change. Some local measurements of bedrock elevation and associated errors
are necessary in order to define a background <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>. The two
algorithms aim to infer the set of parameters which minimises the misfit
between the model and the corresponding observations of ice surface
velocities and thickness rates of change. If the optimisation of ice surface
velocities is usually sufficient to infer <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>, the inference of a second
parameter requires more information to distinguish the effects of each
parameters on the flow. Observations of rates of change of ice thickness are
necessary to allow optimising <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> as well.</p>
      <p>The two algorithms are based on the optimisation of the friction coefficient
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> with the adjoint method. The bedrock geometry <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is
reconstructed in two different ways, again with the adjoint method for the first
algorithm (ATP) and with a nudging method based on mass conservation equation
for the second one (ANC).</p>
      <p>We have shown that the ATP algorithm is capable to well reproduce <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula> and
the corresponding basal shear stresses, while the bedrock elevation
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is only well reproduced in high velocities regions. The lower
the velocity, the harder for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> to depart from its initial
background value. The iterative algorithm coupling adjoint method and nudging
(ANC) gives results that are just as good. Moreover, ANC allows a better reconstruction of
the bedrock geometry <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mtext>b</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> in most regions. This is a very good sign
for an adaptation of the method to non-depth-integrated flow models such as
full Stokes models where the bedrock topography is no more a state variable
but affects the domain geometry making the derivation of the adjoint even
more demanding <xref ref-type="bibr" rid="bib1.bibx30" id="paren.47"/>. Indeed, there is no need to
inverse a shape variable like bedrock topography which is a usual obstacle to
adjoint-based methods.</p>
      <p>Furthermore, the transient simulations over 10 years from initial states
reconstructed with the two algorithms developed give very encouraging
results. The model divergence is clearly decreased with respect to usual
inversion methods of the friction coefficient only. The integration of
observations like thickness rates variation through an optimisation of the
divergence during inversion or nudging steps, allows to regularise the
solution in a physical way and also clearly improves the results.</p>
      <p>Finally, the sensitivity experiments shows that the different algorithms can
take into account the disequilibrium of mass balance, which is particularly
interesting considering that a large amount of outlet glaciers in both
Greenland and Antarctica present this feature.</p>
</sec>
<sec id="Ch1.S6">
  <title>Data availability</title>
      <p>The construction of the twin experiment presented in this article is
partially based on real data. Surface velocities come from Joughin et
al. (2010), while surface and bedrock geometries come from Bamber et
al. (2013). Notice that surface topography slightly differs from Bamber et
al. (2013) in order to reach steady state. The simulations were performed
using the Elmer/Ice finite element model
(<uri>https://github.com/ElmerCSC/elmerfem</uri>). Some modules were specially
developed for this application.</p>
</sec>

      
      </body>
    <back><ack><title>Acknowledgements</title><p>We would like to thank the editor, A. Le Brocq, as well as the two referees,
S. L. Cornford and R. Arthern, for their positive and constructive comments
which greatly improved the initial version of the manuscript. This work was
supported by the French National Research Agency (ANR) under the SUMER
(Blanc SIMI 6) 2012 project ANR-12-BS06-0018. LGGE is part of Labex OSUG@2020
(ANR10 LABX56).<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?> Edited by:
A. Le Brocq<?xmltex \hack{\newline}?> Reviewed by: R. Arthern and S. L. Cornford</p></ack><ref-list>
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<abstract-html><p class="p">Ice flow models are now routinely used to forecast the ice sheets'
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