fgdata/Aircraft-yasim/c172.xml

<airplane mass="1950">

<!-- Approach configuration -->
<approach speed="47" aoa="16">
  <control axis="/controls/throttle[0]" value="0.3"/>
  <control axis="/controls/mixture[0]" value="1.0"/>
  <control axis="/controls/flaps" value="1.0"/>
</approach>

<!-- Cruise configuration -->
<cruise speed="123" alt="0">
  <control axis="/controls/throttle[0]" value="1.0"/>
  <control axis="/controls/mixture[0]" value="1.0"/>
  <control axis="/controls/flaps" value="0.0"/>
</cruise>

<cockpit x="-1.88" y=".33" z="0.6"/>

<fuselage ax="-.17" ay="0" az="-.51" bx="-7.16" by="0" bz=".17"
          width="1.5" taper="0.2" midpoint="0.3"/>

<wing x="-2.47" y=".51" z=".68" taper=".78"
      length="5.37" chord="1.54" sweep="0" dihedral="0" camber="0.1">
  <stall aoa="16" width="6" peak="1.5"/>
  <flap0 start="0" end=".38" lift="1.6" drag="2.0"/>
  <flap1 start=".78" end="1" lift="1.5" drag="1.6"/>
  <control axis="/controls/flaps" output="FLAP0"/>
  <control axis="/controls/aileron" output="FLAP1" split="true"/>
  <control axis="/controls/aileron-trim" output="FLAP1" split="true"/>
</wing>

<hstab x="-7.16" y="0.08" z=".17" taper=".63"
       length="1.71" chord="1.36" sweep="0">
  <stall aoa="16" width="4" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.6" drag="1.8"/>
  <control axis="/controls/elevator" output="FLAP0"/>
  <control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>

<vstab x="-7.16" y="0" z=".17" taper=".5"
       length="1.71" chord="1.54" sweep="20">
  <stall aoa="16" width="4" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.3" drag="1.5"/>
  <control axis="/controls/rudder" output="FLAP0" invert="true"/>
  <control axis="/controls/rudder-trim" output="FLAP0" invert="true"/>
</vstab>

<propeller radius="1.0"
	   cruise-speed="86" cruise-rpm="2200"
           cruise-alt="10000" cruise-power="99"
           takeoff-power="160" takeoff-rpm="2500"
           eng-power="160" eng-rpm="2500"
           x="-.6" y="0" z="0" mass="400" moment="8">
  <actionpt x="0" y="0" z="0"/>
  <control axis="/controls/throttle[0]" output="THROTTLE"/>
  <control axis="/controls/mixture[0]" output="MIXTURE"/>
</propeller>

<gear x="-1" y="0" z="-1.5" compression=".4"> <!-- nose -->
  <control axis="/controls/rudder" output="STEER"/>
</gear>

<gear x="-2.82" y="1.15" z="-1.36" compression=".3"> <!-- left main -->
  <control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>

<gear x="-2.82" y="-1.15" z="-1.36" compression=".3"> <!-- left main -->
  <control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>

<tank x="-2.47" y="1.36" z=".68" capacity="75"/> 
<tank x="-2.47" y="-1.36" z=".68" capacity="75"/> 

<ballast x="-2.0" y=".33" z="0" mass="180"/> <!-- pilot -->
<ballast x="-2.0" y="-.33" z="0" mass="180"/> <!-- passenger -->
<ballast x="-1.0" y="-.33" z="0" mass="200"/> <!-- cockpit -->

</airplane>