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    <identifier identifierType="DOI">10.5880/icgem.2017.006</identifier>
    <creators>
     <creator>
      <creatorName nameType="Personal">Wu, Hu</creatorName>
      <givenName>Hu</givenName>
      <familyName>Wu</familyName>
      <affiliation>Institut für Erdmessung (IfE), Leibniz Universität Hannover, Germany</affiliation>
     </creator>
     <creator>
      <creatorName nameType="Personal">Müller, Jürgen</creatorName>
      <givenName>Jürgen</givenName>
      <familyName>Müller</familyName>
      <affiliation>Institut für Erdmessung (IfE), Leibniz Universität Hannover</affiliation>
     </creator>
     <creator>
      <creatorName nameType="Personal">Brieden, Phillip</creatorName>
      <givenName>Phillip</givenName>
      <familyName>Brieden</familyName>
      <affiliation>Institut für Erdmessung (IfE), Leibniz Universität Hannover</affiliation>
     </creator>
    </creators>
    <titles>
     <title>The GOCE-only global gravity field model IfE_GOCE05s</title>
    </titles>
    <publisher>GFZ Data Services</publisher>
    <publicationYear>2017</publicationYear>
    <subjects>
     <subject>ICGEM</subject>
     <subject>global gravitational model</subject>
     <subject>GOCE</subject>
     <subject subjectScheme="NASA/GCMD Earth Science Keywords">EARTH SCIENCE &gt; SOLID EARTH &gt; GEODETICS &gt; GEOID CHARACTERISTICS</subject>
     <subject subjectScheme="NASA/GCMD Earth Science Keywords">EARTH SCIENCE &gt; SOLID EARTH &gt; GRAVITY/GRAVITATIONAL FIELD &gt; GRAVITATIONAL FIELD</subject>
    </subjects>
    <contributors>
     <contributor contributorType="DataCurator">
      <contributorName nameType="Personal">Ince, Sinem</contributorName>
      <givenName>Sinem</givenName>
      <familyName>Ince</familyName>
      <affiliation affiliationIdentifier="" affiliationIdentifierScheme="">GFZ German Research Centre for Geosciences, Potsdam, Germany</affiliation>
     </contributor>
     <contributor contributorType="DataManager">
      <contributorName nameType="Personal">Reißland, Sven</contributorName>
      <givenName>Sven</givenName>
      <familyName>Reißland</familyName>
      <affiliation affiliationIdentifier="" affiliationIdentifierScheme="">GFZ German Research Centre for Geosciences, Potsdam, Germany</affiliation>
     </contributor>
     <contributor contributorType="ContactPerson">
      <contributorName>Wu, Hu</contributorName>
      <affiliation>Institut für Erdmessung (IfE), Leibniz Universität Hannover</affiliation>
     </contributor>
    </contributors>
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     <relatedIdentifier relatedIdentifierType="URL" relationType="Cites">https://dgk.badw.de/fileadmin/user_upload/Files/DGK/docs/c-777.pdf</relatedIdentifier>
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    <rightsList>
     <rights rightsURI="http://creativecommons.org/licenses/by/4.0/">CC BY 4.0</rights>
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    <descriptions>
     <description descriptionType="Abstract">IfE_GOCE05s is a GOCE-only global gravity field model, which was developed at the Institut für Erdmessung (IfE), Leibniz Universität Hannover, Germany. The observations with a time span from 1 November 2009 to 20 October 2013 are used for the model recovery. The GOCE precise kinematic orbit with 1-s sampling rate is processed for the gravity field up to degree/order 150, while the three main diagonal gravity gradients are down-sampled to 2 s and used to recover the model up to degree/order 250. With two additional Kaula’s regularizations, the combined model “IfE_GOCE05s” is derived, with a maximum degree of 250.      <br/>
       <br/>
            <br/>
 To develop IfE_GOCE05s, the following GOCE data (01.11.2009 - 20.10.2013) was used:      <br/>
 * Orbits: SST_PKI_2, SST_IAQ_2;      <br/>
 * Gradients: EGG_GGT_2, EGG_IAQ_2.      <br/>
       <br/>
            <br/>
 None any priori gravity field information was used.      <br/>
       <br/>
          <br/>
     </description>
     <description descriptionType="TechnicalInfo">      <br/>
            <br/>
       <br/>
            <br/>
 Processing procedures:      <br/>
       <br/>
            <br/>
 Gravity from orbits (SST):      <br/>
 * Acceleration approach was applied to the kinematic orbit data;      <br/>
 * PKI data was at 1 s sampling rate;      <br/>
 * Model was derived up to d/o (degree/order) 150;      <br/>
 * VCM (Variance-Covariance Matrix) was derived arc-wisely from the post-fit residuals.      <br/>
       <br/>
            <br/>
 Gravity from gradients (SGG):      <br/>
 * Gradients Vxx, Vyy and Vzz in the GRF (Gradiometer Reference Frame) were used;      <br/>
 * Gradients were down-sampled to 2 s;      <br/>
 * Model was derived up to d/o 250;      <br/>
 * VCM was estimated arc-wisely from the post-fit residuals.      <br/>
       <br/>
            <br/>
 Regularization:      <br/>
 * A strong Kaula-regularization was applied to constrain the (near-)zonal coefficients that are degraded by the polar gap problem;      <br/>
 * A slight Kaula-regularization was applied to improve the signal-to-noise ratio of the coefficients between d/o 201 and 250;      <br/>
 * The regularization parameters were empirically determined.      <br/>
       <br/>
            <br/>
 Combined solution:      <br/>
 * The normal equations for SST and SGG were summed wih proper weighting factors;      <br/>
 * Weighting factors for SST and SGG were determined from variance component estimation;      <br/>
 * A direct inversion was applied on the final normal equation.      <br/>
     </description>
    </descriptions>
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