fgdata/Aircraft-yasim/c310.xml

<airplane mass="3903">

<approach speed="70" aoa="16">
  <control axis="/controls/throttle[0]" value="0.4"/>
  <control axis="/controls/throttle[1]" value="0.4"/>
  <control axis="/controls/mixture[0]" value="1.0"/>
  <control axis="/controls/mixture[1]" value="1.0"/>
  <control axis="/controls/propeller-pitch[0]" value="0.5"/>
  <control axis="/controls/propeller-pitch[1]" value="0.5"/>
  <control axis="/controls/flaps" value="1.0"/>
</approach>
<cruise speed="223" alt="20000">
  <control axis="/controls/throttle[0]" value="1.0"/>
  <control axis="/controls/throttle[1]" value="1.0"/>
  <control axis="/controls/mixture[0]" value="1.0"/>
  <control axis="/controls/mixture[1]" value="1.0"/>
  <control axis="/controls/propeller-pitch[0]" value="1.0"/>
  <control axis="/controls/propeller-pitch[1]" value="1.0"/>
  <control axis="/controls/flaps" value="0.0"/>
</cruise>

<cockpit x="-2.78" y="0.26" z="0.95"/>

<fuselage ax="0.00"  ay="0" az="0" bx="-9.50" by="0" bz="0"
          width="1.5" taper="0" midpoint="0.4"/>

<wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68"
      sweep="0" dihedral="5" taper="0.8" camber="0.1">
  <stall aoa="16" width="4" peak="1.5"/>
  <flap0 start="0" end=".5" lift="1.5" drag="2.0"/>
  <flap1 start=".55" end=".94" lift="1.3" drag="1.5"/>
  <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="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24"
       sweep="0" dihedral="0" taper="0.6" camber="0.1">
  <stall aoa="16" width="4" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.5" drag="1.8"/>
  <control axis="/controls/elevator" output="FLAP0"/>
  <control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>

<vstab x="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61"
       sweep="36" taper="0.5">
  <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>

<!-- Late model 310's had 50 gallon tip tanks, and 31.5 gallon wing
     tanks.  Some also had nacelle tanks, but those aren't modeled
     here -->
<tank x="-3.62" y="5.30" z="0.44" capacity="300"/>
<tank x="-3.62" y="1.02" z="-0.15" capacity="189"/>
<tank x="-3.62" y="-1.02" z="-0.15" capacity="189"/>
<tank x="-3.62" y="-5.30" z="0.44" capacity="300"/>

<gear x="0.00" y="0.00" z="-1.35" compression=".5" retract-time="7">
  <control axis="/controls/rudder" output="STEER"/>
</gear>
<gear x="-4.02" y="1.32" z="-1.35" compression=".5" retract-time="7">
  <control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<gear x="-4.02" y="-1.32" z="-1.35" compression=".5" retract-time="7">
  <control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>

<propeller x="-2.56" y="1.83" z="0.07"
           mass="800" moment="12" radius="1.0"
           eng-power="285" eng-rpm="2700"
           turbo-mul="2" wastegate-mp="40"
           cruise-power="157" cruise-speed="195"
           cruise-rpm="2100" cruise-alt="20000"
           min-rpm="1600" max-rpm="2700">
  <actionpt x="-1.53" y="1.83" z="0.07"/>
  <control axis="/controls/throttle[0]" output="THROTTLE"/>
  <control axis="/controls/mixture[0]" output="MIXTURE"/>
  <control axis="/controls/propeller-pitch[0]" output="ADVANCE"/>
</propeller>

<propeller x="-2.56" y="-1.83" z="0.07"
           mass="800" moment="12" radius="1.0"
           eng-power="285" eng-rpm="2700"
           turbo-mul="2" wastegate-mp="40"
           cruise-power="157" cruise-speed="195"
           cruise-rpm="2100" cruise-alt="10000"
           min-rpm="1600" max-rpm="2700">
  <actionpt x="-1.53" y="-1.83" z="0.07"/>
  <control axis="/controls/throttle[1]" output="THROTTLE"/>
  <control axis="/controls/mixture[1]" output="MIXTURE"/>
  <control axis="/controls/propeller-pitch[1]" output="ADVANCE"/>
</propeller>

<ballast x="-2.78" y="0.26" z="0.0" mass="180"/> <!-- pilot -->
<ballast x="-2.2" y="0" z="0.0" mass="240"/>    <!-- cockpit -->

<weight x="-4.24" y="0" z="0" mass-prop="/yasim/c310/passenger-lbs"/>

</airplane>