Aircraft-set.xml: Difference between revisions

m
m (→‎Visual aircraft model: fix formatting - don't know what is going on with the last example ending in </sim>... is it a failed import of that code???)
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<aircraft>
<aircraft>
   <performance>
   <performance>
<minimum>
    <minimum>
<takeoff-length-ft type="int">6000</takeoff-length-ft>
      <takeoff-length-ft type="int">6000</takeoff-length-ft>
<landing-length-ft type="int">4000</landing-length-ft>
      <landing-length-ft type="int">4000</landing-length-ft>
</minimum>
    </minimum>
<climb>
    <climb>
<!-- potential for climb data in the future  
      <!-- potential for climb data in the future  
<airspeed-knots type="int">280</airspeed-knots>
      <airspeed-knots type="int">280</airspeed-knots>
<vertical-speed-fpm type="int">2000</vertical-speed-fpm>
      <vertical-speed-fpm type="int">2000</vertical-speed-fpm>
-->
      -->
</climb>
    </climb>
<cruise>
    <cruise>
<airspeed-knots type="int">400</airspeed-knots>
      <airspeed-knots type="int">400</airspeed-knots>
<!--  <mach type="double">0.875</mach> -->
      <!--  <mach type="double">0.875</mach> -->
<altitude-ft type="int">4500</altitude-ft>
      <altitude-ft type="int">4500</altitude-ft>
<!-- <flight-level type="int">330</flight-level> -->
      <!-- <flight-level type="int">330</flight-level> -->
</cruise>
    </cruise>
<descent>
    <descent>
<!-- potential for descent data in the future  
      <!-- potential for descent data in the future  
<airspeed-knots type="int">330</airspeed-knots>
      <airspeed-knots type="int">330</airspeed-knots>
<vertical-speed-fpm type="int">-1200</vertical-speed-fpm>
      <vertical-speed-fpm type="int">-1200</vertical-speed-fpm>
-->
      -->
</descent>
    </descent>
<approach>
    <approach>
<airspeed-knots type="int">120</airspeed-knots>
      <airspeed-knots type="int">120</airspeed-knots>
</approach>
    </approach>
<maximum>
    <maximum>
<altitude-ft type="int">21000</altitude-ft> <!-- service ceiling -->
      <altitude-ft type="int">21000</altitude-ft> <!-- service ceiling -->
<mach type="double">0.875</mach>
      <mach type="double">0.875</mach>
<airspeed-knots type="int">180</airspeed-knots> <!-- VNe or similar airframe structural limit -->
      <airspeed-knots type="int">180</airspeed-knots> <!-- VNe or similar airframe structural limit -->
</maximum>
    </maximum>
   </performance >
   </performance >
</aircraft>
</aircraft>
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