A380_AT.xml

<?xml version="1.0"?>


<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="a380" release="BETA" version="2.0"
    xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
    xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">



<!-- 
   This XML file is incomplete, since DATCOM+ doesn't know 
   enough to fill in all the values. It has filled in 
   that it knows, though. You can build this part of the 
   XML specification once, as it links in the aero part, 
   which is the stuff that is going to change.

   Search for 'unknown' and replace with real values before loading in JSBSim.
-->

   <fileheader>
      <author>DATCOM+</author>
      <filecreationdate> 01/05/13  14:16 </filecreationdate>
      <description>DATCOM model for a unknown</description>
      <version>  </version>
      <reference refID="None" author="n/a" title="n/a" date="n/a"/>
      <description>  </description>
   </fileheader>








<!-- **********************************************************************
        METRICS
     **********************************************************************
-->


   <metrics>
      <wingarea unit="FT2">     9095.5000  </wingarea>
      <wingspan unit="FT">       261.8000  </wingspan>
      <chord unit="FT">           47.9000  </chord>
      <htailarea unit="FT2">    2236.0200  </htailarea>
      <htailarm unit="FT">       106.4339  </htailarm>
      <vtailarea unit="FT2">    1314.4999  </vtailarea>
      <vtailarm unit="FT">       100.2985  </vtailarm>
      <location name="AERORP" unit="IN">
         <!-- x> 43.2 </x>   FIX THIS
         <y>  0.0 </y>   FIX THIS
	 <z> 59.4 </z>   FIX THIS -->
	 <x> 1640 </x>
            <y> 0 </y>
            <z> 0 </z>
	 <!-- x> 41.656 </x>
         <y> 0 </y>
         <z> 0 </z -->
      </location>
      <location name="EYEPOINT" unit="IN">
         <!-- x> 37.0 </x>   FIX THIS
         <y>  0.0 </y>   FIX THIS
	   <z> 48.0 </z>   FIX THIS -->
	   <x> 201.2 </x>
            <y> -32 </y>
            <z> 80 </z>
      </location>
      <location name="VRP" unit="IN">
         <!-- x> 42.6 </x>   FIX THIS
         <y>  0.0 </y>   FIX THIS
	   <z> 38.5 </z>   FIX THIS -->
	   <x> 30.0 </x>
            <y> 0 </y>
            <z> 0 </z>
      </location>
   </metrics>




<!-- **********************************************************************
        MASS_BALANCE
     **********************************************************************
-->


   <mass_balance>
      <!-- 
      <location name="CG" unit="IN">
            <x>  1200.00  </x>
            <y>      .00  </y>
            <z>   124.80  </z>
      </location -->
      <ixx unit="SLUG*FT2">  33222524 </ixx>
        <iyy unit="SLUG*FT2">  31184361 </iyy>
        <izz unit="SLUG*FT2">  65490122 </izz>
        <emptywt unit="LBS" >    610344 </emptywt>
	<location name="CG" unit="IN">
            <!-- x>  1200.00  </x -->
	    <x>1580.79</x>
            <y>     0.00  </y>
            <!-- z>   124.80  </z -->
	    <z>-71.85</z>
      </location>
        <!-- location name="CG" unit="M">
	  <x> 40.152066 </x>
	  <y> 0.0000 </y>
	  <z> -5.52 </z>
        </location -->
	<pointmass name="pilots" >
          <weight unit="KG">160</weight>
          <location name="crew" unit = "M">
            <x>  4.0710 </x>                      
            <y>  0.0000 </y>                      
            <z> -7.0326 </z>                      
          </location>                           
          <form shape="cylinder">
            <radius unit="M"> 1.0 </radius> <!-- wild guess -->
            <length unit="M"> 1.0 </length> <!-- wild guess -->
          </form> 
         </pointmass>                            

        <pointmass name="passenger main" >
          <weight unit="KG">43040</weight>
          <location name="passenger" unit = "M">
            <x>  37.4554 </x>
            <y>  0.0000 </y>
            <z>  -5.7104 </z>
          </location>
          <form shape="cylinder">
            <radius unit="M">  2.0 </radius> <!-- wild guess -->
            <length unit="M"> 30.0 </length> <!-- wild guess -->
          </form> 
        </pointmass>

        <pointmass name="passenger upper" >
          <weight unit="KG">25200</weight>
          <location name="passenger" unit = "M">
            <x>  37.4554 </x>
            <y>  0.0000 </y>
            <z>  -8.3097 </z>
          </location>
          <form shape="cylinder">
            <radius unit="M">  1.0 </radius> <!-- wild guess -->
            <length unit="M"> 30.0 </length> <!-- wild guess -->
          </form> 
        </pointmass>

        <pointmass name="cargo forward" >
          <weight unit="KG">28577</weight>
          <location name="POINTMASS" unit = "M">
            <x>  15.5171 </x>
            <y>  0.0000 </y>
            <z>  -3.7654 </z>
          </location>
          <form shape="cylinder">
            <radius unit="M">  2.0 </radius> <!-- wild guess -->
            <length unit="M"> 10.0 </length> <!-- wild guess -->
          </form> 
        </pointmass>

        <pointmass name="cargo aft" >
          <weight unit="KG">20310</weight>
          <location name="POINTMASS" unit = "M">
            <x>  45.6932 </x>
            <y>  0.0000 </y>
            <z>  -4.1767 </z>
	  </location>
          <form shape="cylinder">
            <radius unit="M">  2.0 </radius> <!-- wild guess -->
            <length unit="M"> 10.0 </length> <!-- wild guess -->
          </form> 
        </pointmass>

	<pointmass name="cargo bulk" >
          <weight unit="KG">2515</weight>
          <location name="POINTMASS" unit = "M">
            <x>  52.4356 </x>
            <y>  0.00 </y>
	    <z>  -4.3714 </z>
          </location>
          <form shape="cylinder">
            <radius unit="M">  2.0 </radius> <!-- wild guess -->
            <length unit="M">  1.0 </length> <!-- wild guess -->
          </form> 
        </pointmass>
   </mass_balance>




<!-- **********************************************************************
        UNDERCARRIAGE
     **********************************************************************
-->


<!--

   DATCOM does not calculate ground reactions parameters.

-->


   <ground_reactions>
<contact type="BOGEY" name="Nose Gear">
            <location unit="IN">
                <x> 488.52 </x>
                <y> 0 </y>
                <z> -344.9 </z>
            </location>
            <static_friction> 0.8 </static_friction>
            <dynamic_friction> 0.5 </dynamic_friction>
            <rolling_friction> 0.02 </rolling_friction>
            <spring_coeff unit="LBS/FT"> 362502 </spring_coeff>
            <damping_coeff unit="LBS/FT/SEC"> 120834 </damping_coeff>
            <max_steer unit="DEG"> 70 </max_steer>
            <brake_group> NONE </brake_group>
            <retractable>1</retractable>
        </contact>
        <contact type="BOGEY" name="Left Main gear">
            <location unit="IN">
                <x> 1644 </x>
                <!-- y> -282.8 </y -->
                <y>278.972441</y>
                <z> -344.9 </z>
            </location>
            <static_friction> 0.8 </static_friction>
            <dynamic_friction> 0.5 </dynamic_friction>
            <rolling_friction> 0.02 </rolling_friction>
            <spring_coeff unit="LBS/FT"> 1.20834e+06 </spring_coeff>
            <damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
            <max_steer unit="DEG"> 0.0 </max_steer>   <!-- was 0.0 -->
            <brake_group> RIGHT </brake_group>
            <retractable>1</retractable>
        </contact>
        <contact type="BOGEY" name="Right Main Gear">
            <location unit="IN">
                <x> 1644 </x>
                <!-- y> 282.8 </y -->
                <y>-278.972441</y>
                <z> -344.9 </z>
            </location>
            <static_friction> 0.8 </static_friction>
            <dynamic_friction> 0.5 </dynamic_friction>
            <rolling_friction> 0.02 </rolling_friction>
            <spring_coeff unit="LBS/FT"> 1.20834e+06 </spring_coeff>
            <damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
            <max_steer unit="DEG"> 0.0 </max_steer>   <!-- was 0.0 -->
            <brake_group> LEFT </brake_group>
            <retractable>1</retractable>
	</contact>
   </ground_reactions>




<!-- **********************************************************************
        PROPULSION
     **********************************************************************
-->


   <propulsion>
<engine file="TRENT-900">
            <location unit="M">
                <x>  46.9824 </x>
                <y>  26.2467 </y>
		<z>  -3.4 </z>
            </location>
            <orient unit="DEG">
                <roll> 0.0 </roll>
                <pitch> 0 </pitch>
                <yaw> 0 </yaw>
            </orient>
            <feed>0</feed>
	    <feed>4</feed>
	    <feed>6</feed>
	    <feed>10</feed>
	    <feed>8</feed>
            <thruster file="direct">
                <location unit="M">
                    <!-- x> 1580.79 </x>
                    <y> -523.648 </y>
                    <z> -40 </z -->
		    <x> 46.9824 </x>
		    <y> 26.2467 </y>
		    <z> -3.4 </z>
                </location>
                <orient unit="DEG">
                    <roll> 0.0 </roll>
                    <pitch> 0.0 </pitch>
                    <yaw> 0.0 </yaw>
                </orient>
            </thruster>
        </engine>
        <engine file="TRENT-900">
            <location unit="M">
                <x> 38.9500 </x>
                <y> 15.9365 </y>
		<z> -2.55 </z>
            </location>
            <orient unit="DEG">
                <roll> 0.0 </roll>
                <pitch> 0 </pitch>
                <yaw> 0 </yaw>
            </orient>
            <feed>1</feed>
	    <feed>4</feed>
	    <feed>6</feed>
	    <feed>10</feed>
	    <feed>8</feed>
            <thruster file="direct">
                <location unit="M">
                    <!-- x> 1580.79 </x>
                    <y> -523.648 </y>
                    <z> -40 </z -->
		    <x> 38.9500 </x>
		    <y> 15.9365 </y>
		    <z> -2.55 </z>
                </location>
                <orient unit="DEG">
                    <roll> 0.0 </roll>
                    <pitch> 0.0 </pitch>
                    <yaw> 0.0 </yaw>
                </orient>
            </thruster>
        </engine>
        <engine file="TRENT-900">
            <location unit="M">
                <x> 38.9500 </x>
		<y> -15.9365 </y>
		<z> -2.55 </z>
            </location>
            <orient unit="DEG">
                <roll> 0.0 </roll>
                <pitch> 0 </pitch>
                <yaw> 0 </yaw>
            </orient>
            <feed>2</feed>
	    <feed>5</feed>
	    <feed>7</feed>
	    <feed>10</feed>
	    <feed>9</feed>
            <thruster file="direct">
                <location unit="M">
                    <!-- x> 1580.79 </x>
                    <y> 523.648 </y>
                    <z> -40 </z -->
		    <x> 38.9500 </x>
		    <y> -15.9365 </y>
		    <z> -2.55 </z>
                </location>
                <orient unit="DEG">
                    <roll> 0.0 </roll>
                    <pitch> 0.0 </pitch>
                    <yaw> 0.0 </yaw>
                </orient>
            </thruster>
        </engine>
        <engine file="TRENT-900">
            <location unit="M">
                <x>  46.9824 </x>
                <y>  -26.2467 </y>
		<z>  -3.4 </z>
            </location>
            <orient unit="DEG">
                <roll> 0.0 </roll>
                <pitch> 0 </pitch>
                <yaw> 0 </yaw>
            </orient>
            <feed>3</feed>
	    <feed>5</feed>
	    <feed>7</feed>
	    <feed>10</feed>
	    <feed>9</feed>
            <thruster file="direct">
                <location unit="M">
                    <!-- x> 1580.79 </x>
                    <y> 523.648 </y>
                    <z> -40 </z -->
		    <x>  46.9824 </x>
                    <y>  -26.2467 </y>
		    <z>  -3.4 </z>
                </location>
                <orient unit="DEG">
                    <roll> 0.0 </roll>
                    <pitch> 0.0 </pitch>
                    <yaw> 0.0 </yaw>
                </orient>
            </thruster>
        </engine>

	<!--  APU type -->
      <engine file="APU">
            <location unit="IN">
                <x> 100 </x>
                <y> 0 </y>
                <z> 0 </z>
            </location>
            <orient unit="DEG">
                <roll> 0.0 </roll>
                <pitch> 0 </pitch>
                <yaw> 0 </yaw>
            </orient>
            <feed>1</feed>
	    <feed>4</feed>
            <thruster file="direct">
                <location unit="IN">
                <x> 100 </x>
                <y> 0 </y>
                <z> 0 </z>
                </location>
                <orient unit="DEG">
                    <roll> 0.0 </roll>
                    <pitch> 0.0 </pitch>
                    <yaw> 0.0 </yaw>
                </orient>
            </thruster>
        </engine>
        

    <!-- 
           The A380 has 11 tanks in all. The feed tanks feed each engine with
	   a cross-over valve to the next engine. The sequence for feeding the
	   feed tanks is;
	    1. inner tank -> feed
	    2. mid tank   -> feed
	    3. trim tank  -> feed
	    4. outer tank -> feed
	   The trim tank should be moved to the outer trim tank before approach.
    -->
      <tank type="FUEL">    <!-- feed number 0 -->
            <location unit="M">
                <!-- x> 1580.79 </x>
                <y> 200 </y>
                <z> -71.8539 </z -->
		<x> 48.5306 </x>
		<y> 23.4729 </y>
		<z> -5.01 </z>
            </location>
            <capacity unit="LBS"> 48390 </capacity>
            <contents unit="LBS"> 16775 </contents>
	    <priority>1</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.87 </radius> 
        </tank>
        <tank type="FUEL">    <!-- feed number 1 -->
            <location unit="M">
		<x> 37.4956 </x>
		<y> 7.6904 </y>
		<z> -3.3069 </z>
            </location>
            <capacity unit="LBS"> 50780 </capacity>
            <contents unit="LBS"> 18280 </contents>
 	    <priority>1</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.9 </radius> 
         </tank>
        <tank type="FUEL">    <!-- feed number 2 -->
            <location unit="M">
		<x> 37.4956 </x>
		<y> -7.6904 </y>
		<z> -3.3069 </z>
            </location>
            <capacity unit="LBS"> 50780 </capacity>
            <contents unit="LBS"> 18280 </contents>
	    <priority>1</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.9 </radius> 
         </tank>
        <tank type="FUEL">    <!-- feed number 3 -->
            <location unit="M">
		<x> 48.5306 </x>
		<y> -23.4729 </y>
		<z> -5.01 </z>
            </location>
            <capacity unit="LBS"> 48390 </capacity>
            <contents unit="LBS"> 16775 </contents>
	    <priority>1</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.87 </radius> 
         </tank>
	<tank type="FUEL">    <!-- innerL 4 -->
            <location unit="M">
		<x> 42.1149 </x>
		<y> 8.5886 </y>
		<z> -3.3069 </z>
            </location>
            <capacity unit="LBS"> 79850 </capacity>
            <contents unit="LBS"> 17034 </contents>
	    <priority>2</priority>
            <type>JET-A</type>
            <radius unit="M"> 2.21 </radius> 
         </tank>
	<tank type="FUEL">    <!-- innerR 5 -->
            <location unit="M">
		<x> 42.1149 </x>
		<y> -8.5886 </y>
		<z> -3.3069 </z>
            </location>
            <capacity unit="LBS"> 79850 </capacity>
            <contents unit="LBS"> 17034 </contents>
	    <priority>2</priority>
            <type>JET-A</type>
            <radius unit="M"> 2.21 </radius> 
         </tank>
	<tank type="FUEL">    <!-- midL 6 -->
            <location unit="M"> 
		<x> 44.0396 </x>
		<y> 15.0043 </y>
		<z> -4.67 </z>
            </location>
            <capacity unit="LBS"> 63100 </capacity>
            <contents unit="LBS"> 16826 </contents>
	    <priority>3</priority>
            <type>JET-A</type>
            <radius unit="M"> 2.04 </radius> 
         </tank>
	<tank type="FUEL">    <!-- midR 7 -->
            <location unit="M">
		<x> 44.0396 </x>
		<y> -15.0043 </y>
		<z> -4.67 </z>
            </location>
            <capacity unit="LBS"> 63100 </capacity>
            <contents unit="LBS"> 16826 </contents>
	    <priority>3</priority>
            <type>JET-A</type>
            <radius unit="M"> 2.04 </radius> 
         </tank>
	<tank type="FUEL">    <!-- outerL 8 -->
            <location unit="M">
		<x> 52.7169 </x>
		<y> 30.1754 </y>
		<z> -5.28 </z>
            </location>
            <capacity unit="LBS"> 18200 </capacity>
            <contents unit="LBS"> 10434 </contents>
	    <priority>4</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.35 </radius> 
         </tank>
	<tank type="FUEL">    <!-- outerR 9 -->
            <location unit="M">
		<x> 52.7169 </x>
		<y> -30.1754 </y>
		<z> -5.28 </z>
            </location>
            <capacity unit="LBS"> 18200 </capacity>
            <contents unit="LBS"> 10434 </contents>
	    <priority>4</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.35 </radius> 
         </tank>
	<tank type="FUEL">    <!-- trim 10 -->
            <location unit="M">
                <!-- x> 1580.79 </x>
                <y> 0 </y>
                <z> -71.8539 </z -->
		<x> 60.8777 </x>
		<y> 0.0000 </y>
		<z> -7.9141 </z>
            </location>
            <capacity unit="LBS"> 41020 </capacity>
            <contents unit="LBS"> 20000 </contents>
	    <priority>5</priority>
            <type>JET-A</type>
            <radius unit="M"> 1.77 </radius> 
         </tank>

   </propulsion>




<!-- **********************************************************************
        AUTOPILOT
     **********************************************************************
-->


   <!-- Autopilot is not a required section, and DATCOM does not calculate this -->


  <system file="pushback"/> 

<!-- **********************************************************************
        FLIGHT CONTROLS
     **********************************************************************
-->


   <!-- DATCOM does not calculate the flight control section -->
   <flight_control name="FCS: a380">
       <channel name="All">

        <summer name="Pitch Trim Sum">
            <input>fcs/elevator-cmd-norm</input>
            <input>fcs/pitch-trim-cmd-norm</input>
            <clipto>
                <min>-1</min>
                <max>1</max>
            </clipto>
        </summer>

        <aerosurface_scale name="Elevator Control">
            <input>fcs/pitch-trim-sum</input>
            <range>
                <min>-0.35</min>
                <max>0.3</max>
            </range>
            <output>fcs/elevator-pos-rad</output>
        </aerosurface_scale>

        <summer name="Roll Trim Sum">
            <input>fcs/aileron-cmd-norm</input>
            <input>fcs/roll-trim-cmd-norm</input>
            <clipto>
                <min>-1</min>
                <max>1</max>
            </clipto>
        </summer>

        <aerosurface_scale name="Left Aileron Control">
            <input>fcs/roll-trim-sum</input>
            <range>
                <min>-0.35</min>
                <max>0.35</max>
            </range>
            <output>fcs/left-aileron-pos-rad</output>
        </aerosurface_scale>

        <aerosurface_scale name="Right Aileron Control">
            <input>-fcs/roll-trim-sum</input>
            <range>
                <min>-0.35</min>
                <max>0.35</max>
            </range>
            <output>fcs/right-aileron-pos-rad</output>
        </aerosurface_scale>

        <summer name="Rudder Command Sum">
            <input>fcs/rudder-cmd-norm</input>
            <input>fcs/yaw-trim-cmd-norm</input>
            <clipto>
                <min>-1</min>
                <max>1</max>
            </clipto>
        </summer>

        <scheduled_gain name="Yaw Damper Rate">
            <input>velocities/r-aero-rad_sec</input>
            <table>
                <independentVar>aero/qbar-psf</independentVar>
                <tableData>
                    3.0000	0.0000
                    11.0000	2.0000
                </tableData>
            </table>
        </scheduled_gain>

        <scheduled_gain name="Yaw Damper Beta">
            <input>aero/beta-rad</input>
            <table>
                <independentVar>aero/qbar-psf</independentVar>
                <tableData>
                    3.0000	0.0000
                    11.0000	0.0000
                </tableData>
            </table>
        </scheduled_gain>

        <summer name="Yaw Damper Sum">
            <input>fcs/yaw-damper-beta</input>
            <input>fcs/yaw-damper-rate</input>
            <clipto>
                <min>-0.2000</min>
                <max>0.2000</max>
            </clipto>
        </summer>

        <scheduled_gain name="Yaw Damper Final">
            <input>fcs/yaw-damper-sum</input>
            <table>
                <independentVar>aero/qbar-psf</independentVar>
                <tableData>
                    2.9900	0.0000
                    3.0000	1.0000
                </tableData>
            </table>
        </scheduled_gain>

        <summer name="Rudder Sum">
            <input>fcs/rudder-command-sum</input>
            <input>fcs/yaw-damper-final</input>
            <clipto>
                <min>-1.0000</min>
                <max>1.0000</max>
            </clipto>
        </summer>

        <aerosurface_scale name="Rudder Control">
            <input>fcs/rudder-sum</input>
            <range>
                <min>-0.3500</min>
                <max>0.3500</max>
            </range>
            <output>fcs/rudder-pos-rad</output>
        </aerosurface_scale>

        <kinematic name="Flaps Control">
            <input>fcs/flap-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>7.2720</position>
                    <time>15.0</time>
                </setting>
                <setting>
                    <position>15.4530</position>
                    <time>5.0</time>
                </setting>
		<setting>
		  <position>23.6340</position>
		  <time>4.0</time>
		</setting>
                <setting>
                    <position>30.0000</position>
                    <time>5.0</time>
                </setting>
            </traverse>
            <output>fcs/flap-pos-deg</output>
	  </kinematic>

            <aerosurface_scale name="Flap Position Normalizer">
              <input>fcs/flap-pos-deg</input>
              <domain>
                <min>0</min>  <!-- Flaps actual minimum position -->
                <max>30</max>  <!-- Flaps actual maximum position -->
              </domain>
              <range>
                <min>0</min>  <!-- Flaps normalized minimum position -->
                <max>1</max>  <!-- Flaps normalized maximum position -->
              </range>
              <output>fcs/flap-pos-norm</output>
            </aerosurface_scale>

        <!-- kinematic name="Gear Control">
            <input>gear/gear-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>1.0000</position>
                    <time>15.0000</time>
                </setting>
            </traverse>
            <output>gear/gear-pos-norm</output>
        </kinematic -->
	<property>fcs/slat-cmd-norm</property>
	
	<kinematic name="fcs/leading-edge-flap-cmd-norm">
	  <input>fcs/slat-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>30.0</position>
                    <time>9.0</time>
                </setting>
	      </traverse>
	      <output>fcs/leading-edge-flap-pos-deg</output>
	</kinematic>
	
	<kinematic name="fcs/leading-edge-slat-cmd-norm">
	  <input>fcs/slat-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>20.0</position>
                    <time>5.0</time>
                </setting>
	      </traverse>
	      <output>fcs/leading-edge-slat-pos-deg</output>
	</kinematic>
	

	<kinematic name="gear/unit[0]/pos">
	    <input>gear/gear-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>  
                <setting>
                    <position>1.0000</position>
                    <time>16.0000</time>
                </setting>  
            </traverse>
            <output>gear/unit[0]/pos-norm</output>
        </kinematic>
        <kinematic name="gear/unit[1]/pos">
            <input>gear/gear-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting> 
                    <position>1.0000</position>
                    <time>13.0000</time>
                </setting>
            </traverse>
            <output>gear/unit[1]/pos-norm</output>
        </kinematic>
        <kinematic name="gear/unit[2]/pos">
            <input>gear/gear-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>1.0000</position>
                    <time>25.0000</time>
                </setting>
            </traverse>
            <output>gear/unit[2]/pos-norm</output>
        </kinematic>

        <kinematic name="Speedbrake Control">
            <input>fcs/speedbrake-cmd-norm</input>
            <traverse>
                <setting>
                    <position>0.0000</position>
                    <time>0.0000</time>
                </setting>
                <setting>
                    <position>1.0000</position>
                    <time>1.0000</time>
                </setting>
            </traverse>
            <output>fcs/speedbrake-pos-norm</output>
        </kinematic>
	
	    <aerosurface_scale name="Spoiler Normalizer">
              <input>fcs/speedbrake-cmd-norm</input>
              <domain>
                <min>0</min>  <!-- Flaps actual minimum position -->
                <max>80</max>  <!-- Flaps actual maximum position -->
              </domain>
              <range>
                <min>0</min>  <!-- Flaps normalized minimum position -->
                <max>1</max>  <!-- Flaps normalized maximum position -->
              </range>
              <output>fcs/ground-spoiler-pos-deg</output>
	      <output>fcs/flight-spoiler-pos-deg</output>
            </aerosurface_scale>

     </channel>
   </flight_control>




<!-- **********************************************************************
        AERODYNAMICS
     **********************************************************************
-->




   <!-- Link to the aerodynamics file -->

   <aerodynamics file="A380_AT_aero.xml"/>



<!-- ********************************************************************** -->


    <external_reactions>
 	  <force name="pushback" frame="BODY">
	      <location unit="IN">
		   <x>12.150</x>
		   <y>-0.875</y>
		   <z>1.641</z>
		</location>
	      <direction>
		   <x>1</x>
		   <y>0</y>
		   <z>0</z>
		</direction>
	 </force>
    </external_reactions>


<!--
   OUTPUT section definition

   The following specifies the way that JSBSim writes out data

   NAME is the filename you want the output to go to

   TYPE can be:

      CSV       Comma separated data. If a filename is supplied then the data
                goes to that file. If COUT or cout is specified, the data
                goes to stdout. If the filename is a null filename
                the data goes to stdout, as well

      SOCKET    Will eventually send data to a socket output, where NAME
                would then be the IP address of the machine the data 
                should be sent to. DON'T USE THIS YET!

      TABULAR   Columnar data. 

      TERMINAL  Output to terminal. NOT IMPLEMENTED YET!

      NONE      Specifies to do nothing. This setting makes it easy to turn 
                on and off the data output without having to mess with 
                anything else.


   NOTE that Time is always output with the data.

-->



   <output name="JSBout.rec" type="TABULAR" rate="20">
      <simulation>       OFF </simulation>
      <atmosphere>       ON  </atmosphere>
      <atmosphere>       ON  </atmosphere>
      <massprops>        ON  </massprops>
      <aerosurfaces>     ON  </aerosurfaces>
      <rates>            ON  </rates>
      <velocities>       ON  </velocities>
      <forces>           OFF </forces>
      <moments>          OFF </moments>
      <position>         ON  </position>
      <coefficients>     OFF </coefficients>
      <ground_reactions> OFF </ground_reactions>
      <fcs>              ON  </fcs>
      <propulsion>       OFF </propulsion>

      <!-- property>fcs/flap-pos-deg</property -->

   </output>



</fdm_config>