fgdata/Aircraft-yasim/seahawkpair-yasim.xml

<!--  Hawker Sea Hawk yasim config.  This is a hack and not an
      authentic representation of the aircraft.  Having said
      that, the numbers, where I could find them, roughly match
      those of the original aircraft.
      Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
-->

<airplane mass="9720">

<!-- Approach configuration.
     I couldn't find any approach data but I think that the way
     the aircraft sits tail down on it's u/c indicates that it
     must land at a fairly shallow AoA to avoid hitting tail
     first.  The speed is a guess.

     I could see no sign or mention of spoilers or airbrakes in any
     of the docs or pictures I found.
-->
 <approach speed="110" aoa="7">
  <control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
  <control-setting axis="/controls/flight/flaps" value="1.0"/>
  <control-setting axis="/controls/gear/gear-down" value="1"/>
 </approach>

<!-- Cruise configuration.
     Max speed at sea level is 599 mph = 521 knots.  The same source
     also quoted 587 mph at 'altitude'.
-->
 <cruise speed="521" alt="0">
  <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
  <control-setting axis="/controls/flight/flaps" value="0.0"/>
  <control-setting axis="/controls/gear/gear-down" value="0"/>
 </cruise>

 <cockpit x="3.0" y="0.0" z="0.7"/>

 <fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
          width="1.3"/>

<!-- The wing length is from tips to fuselage, including intakes.
     The aileron figures are probably too low but the roll rate seemed
     too high otherwise.
-->
 <wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
      length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
  <stall aoa="17" width="3" peak="1.3"/>
  <flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
  <flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>

  <control-input axis="/controls/flight/flaps" control="FLAP0"/>
  <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
  <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>

  <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
  <control-output control="FLAP1" side="left"
      prop="/surface-positions/left-aileron-pos-norm"/>
  <control-output control="FLAP1" side="right"
      prop="/surface-positions/right-aileron-pos-norm"/>
  <control-output control="SPOILER" side="right"
      prop="/surface-positions/right-spoiler-pos-norm"/> -->

  <control-speed control="FLAP0" transition-time="5"/>

 </wing>

 <hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
       length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
  <stall aoa="17" width="5" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
  <control-input axis="/controls/flight/elevator" control="FLAP0"/>
  <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
  <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
 </hstab>

 <vstab x="-5.2" y="0.0" z="0.2" taper="0.8"
       length="1.4" chord="1.8" sweep="10.0">
  <stall aoa="16" width="5" peak="1.5"/>
  <flap0 start="0" end="1" lift="1.15" drag="1.3"/>
  <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
  <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
 </vstab>

<!-- Engines and tanks.
     1 x Roll-Royce Nene 103.  I've no idea how much it actually
     weighs.
-->
 <jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
  <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
 </jet>
<!-- Fuel tanks in front of and behind the engine.
-->
 <tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2600"/>
 <tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2600"/>

<!-- Undercarriage -->
<!-- nose -->
 <gear x="4.0" y="0.0" z="-1.39" retract-time="7" compression="0.6">
  <control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
  <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  <control-speed control="EXTEND" transition-time="7"/>
  <control-output control="EXTEND" prop="/gear/gear/position-norm"/>
 </gear>

<!-- left main -->
 <gear x="0.08" y="1.4" z="-1.3" retract-time="7" compression="0.6">
  <control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
  <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  <control-speed control="EXTEND" transition-time="7"/>
  <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
 </gear>

<!-- right main -->
 <gear x="0.08" y="-1.4" z="-1.3" retract-time="7" compression="0.6">
  <control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
  <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  <control-speed control="EXTEND" transition-time="7"/>
  <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
 </gear>

<!-- Canopy -->
 <gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
  <control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
  <control-speed control="EXTEND" transition-time="10"/>
  <control-output control="EXTEND" prop="/canopy/position-norm"/>
 </gear>

<!-- Wingman -->
 <gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
  <control-input axis="/controls/autoflight/wingman" control="EXTEND"/>
  <control-speed control="EXTEND" transition-time="10"/>
  <control-output control="EXTEND" prop="/wingman/position-norm"/>
 </gear>

<!-- Ballast -->
 <ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
 <ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
 <ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->

</airplane>