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      FDC help: VORerr
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    <h2>
      The radio-navigation block <i>VORerr</i>
    </h2>
    <p>The block <i>VORerr</i> from the sublibrary VOR of the
    block-library <i><a href="navlib.htm">NAVLIB</a></i> can be used to
    implement steady-state VOR errors. The user must specify the required error
    percentage.</p>
     <p><b>Note:</b> the nominal VOR signals can be determined with the block
    <i><a href="vor.htm">VOR</a></i> from the same block-library. The system
    <i><a href="vorxmpl.htm">VOR example</a></i> demonstrates how these blocks
    can be combined.</p> 
    <h3>
      Input signal
    </h3>
<pre>
 Gamma_VOR (nominal value, coming from block VOR), [rad]
</pre>
    <p><i>Gamma_VOR</i> is the angle between the line through the projection point
    of the aircraft&#39;s c.g. on the ground and the VOR antenna, and the
    nominal VOR bearing (see also the <a href="#References">references</a>
    below).</p> 
    <h3>
      Output signal
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<pre>
 Gamma_VOR (nominal value + steady-state error), [rad]
</pre>
    <h3>
      <a name="References">References</a>
    </h3>
    <p>For more information about the block <i>VORerr</i>, consult the FDC user-manual, and/or:</p> 
    <ol>
      <li>
        M.O. Rauw: <i>A Simulink environment for Flight Dynamics and Control
        analysis - Application to the DHC-2 &#39;Beaver&#39;</i>. MSc-thesis,
        Delft University of Technology, Faculty of Aerospace Engineering,
        Delft, The Netherlands, 1993.
      </li>
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