vampire/vampire-yasim.xml

<?xml version="1.0" encoding="UTF-8"?>

<!--  DH Vampire F3, StuartC

Crew: Pilot only
Length: 30 ft 9 in (9.37 m)
Wingspan: 38 ft 0 in (11.58 m)
Height: 6 ft 2 in (1.88 m)
Max takeoff weight: 12,385 lb (5,618 kg)
Engine Single 1,420 lbf (6.3 kN) de Havilland Goblin 2 turbojet
Maximum speed: 530 mph at sea level (855 km/h)
Range: 1,090 mi (1,755 km)
Service ceiling: 40,000 ft (12,200 m)

Armament:
Four 20 mm Hispano cannons
Two 500 lb (227 kg) or 1,000 lb (455 kg) bombs
Eight 60lb (27kg) 3 in (76 mm) unguided rocket projectiles
Some Vampires were retro-fitted with Sidewinder missile guidance systems 


-->

<airplane mass="7283">

  <approach speed="110" aoa="6" fuel="0.1">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
    <control-setting axis="/controls/flight/flaps" value="1"/>
    <control-setting axis="/controls/gear/gear-down" value="1"/>
    <solve-weight idx="0" weight="170"/>
  </approach>

  <cruise speed="476" alt="25000" fuel="0.4">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="1"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="1"/>
    <control-setting axis="/controls/flight/flaps" value="0"/>
    <control-setting axis="/controls/gear/gear-down" value="0"/>
    <solve-weight idx="0" weight="170"/>
  </cruise>

  <cockpit x="1.3" y="0.0" z="0.7"/>

  <!-- Fuselage with engine on top -->
  <!-- fuselage ax="3.25" ay="0" az="-0.25"  bx="-2.42" by="0" bz="-0.2" width="1.4" taper="0.3" midpoint="0.50"/ -->
  
  <fuselage ax="2.05" ay="0" az="0.35"  bx="0.55" by="0" bz="0.55" width="0.65" taper="0.22" midpoint="0.4"/>

  <fuselage ax="3.25" ay="0" az="-0.25"  bx="2.89" by="0" bz="-0.23" width="0.65" taper="0.28" midpoint="1"/>
  <fuselage ax="2.9" ay="0" az="-0.23"  bx="2.32" by="0" bz="-0.18" width="1.0" taper="0.64" midpoint="1"/>
  <fuselage ax="2.35" ay="0" az="-0.18"  bx="0.4" by="0" bz="-0.12" width="1.31" taper="0.76" midpoint="1"/>
  <fuselage ax="0.42" ay="0" az="-0.12"  bx="-0.57" by="0" bz="-0.12" width="1.31" taper="0.96" midpoint="0"/>
  <fuselage ax="-0.55" ay="0" az="-0.12"  bx="-1.32" by="0" bz="-0.14" width="1.258" taper="0.82" midpoint="0"/>
  <fuselage ax="-1.3" ay="0" az="-0.14"  bx="-2.42" by="0" bz="-0.2" width="1.03" taper="0.48" midpoint="0"/>

  <fuselage ax="0.05" ay="1.4" az="0.02"  bx="-5.45" by="1.4" bz="0.25" width="0.28" taper="1.0" midpoint="0.50"/>
  <fuselage ax="0.05" ay="-1.4" az="0.02"  bx="-5.45" by="-1.4" bz="0.25" width="0.28" taper="1.0" midpoint="0.50"/>
  
<!--
        incidence="1" 
        twist="-1"
-->
  <wing x="-0.38" y="2.94" z="-0"
        chord="1.92" 
        length="2.48"
        taper="0.55"
        sweep="1.8"
        incidence="2"
        dihedral="3.4"
        twist="-1"
        camber="0.015">
        <stall aoa="16" width="5" peak="1.5"/>
        <flap0 start="0" end="0.01" lift="1.6" drag="2.2"/>
        <flap1 start="0" end="1" lift="1.3" drag="1.0"/>

        <control-input axis="/controls/flight/aileron" control="FLAP1" square="true" split="true"/> 
        <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
		
		 <control-output control="FLAP0" side="left" prop="/surface-positions/left-flap-pos-norm"/>
        <control-output control="FLAP0" side="right" prop="/surface-positions/right-flap-pos-norm"/>
        <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="FLAP1" prop="/surface-positions/aileron-pos-norm"/>

		<control-speed control="FLAP0" transition-time="5"/>
        <control-speed control="FLAP1" transition-time="0.1"/>
   </wing>
   
   <!-- inner -->
  <mstab x="-0.21" y="0.4" z="-0.16"
        chord="3.38" 
        length="0.92"
        taper="0.78"
        sweep="11.4"
        incidence="2"
        dihedral="3.4"
        camber="0.022">
        <stall aoa="16" width="5" peak="1.5"/>
        <flap0 start="0.28" end="1" lift="1.1" drag="7.5"/>
        <!-- <flap0 start="0.28" end="1" lift="1.6" drag="2.2"/> -->

        <control-input axis="controls/flight/speedbrake" control="FLAP0"/>
       <!-- <control-input axis="/controls/flight/flaps" control="FLAP0"/> -->

        <control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>  
      <!--  <control-output control="FLAP0" side="left" prop="/surface-positions/left-flap-pos-norm"/>
        <control-output control="FLAP0" side="right" prop="/surface-positions/right-flap-pos-norm"/>
        <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>-->

        <control-speed control="FLAP0" transition-time="10"/>
   </mstab>
   
<!-- middle -->
  <mstab x="-0.39" y="1.3" z="-0.1"
        chord="2.64" 
        length="1.65"
        taper="0.73"
        sweep="-0.4"
        incidence="2"
        dihedral="3.4"
        camber="0.015">
        <stall aoa="16" width="5" peak="1.5"/>
        <spoiler start="0.18" end="0.74" lift="1.1" drag="7.5"/>
        <flap0 start="0.18" end="0.74" lift="1.6" drag="2.2"/>

        <control-input axis="controls/flight/speedbrake" control="SPOILER"/>
        <control-input axis="/controls/flight/flaps" control="FLAP0"/> 

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

        <control-speed control="FLAP0" transition-time="30"/>
   </mstab>
   
<!-- tip -->
  <mstab x="-0.46" y="5.42" z="0.14"
        chord="1.056" 
        length="0.36"
        taper="0.3"
        sweep="-4.4"
        incidence="1"
        dihedral="3.4"
        camber="0.015">
        <stall aoa="16" width="5" peak="1.5"/>
   </mstab>
   
   <hstab x="-4.83" y="0" z="0.48"
         chord="1.2"
         length="1.4"
         taper="1"
         sweep="0"
         camber="-0.0065"
         incidence="0">
         <stall aoa="20" width="9" peak="1.6"/>
         <flap0 start="0" end="0.88" lift="2.1" drag="1.2"/>

         <control-input axis="/controls/flight/elevator" square="false" control="FLAP0" />
         <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>

         <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
  </hstab>

  <vstab x="-4.792" y="1.4" z="0.1"
         chord="1.5" 
         length="1.4" 
         taper="0.2"
         sweep="26">
         <stall aoa="16" width="7" peak="1.5"/>
         <flap0 start="0" end="1" lift="1.7" drag="1.3"/>

         <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
  </vstab>
  
  <vstab x="-4.792" y="-1.4" z="0.1"
         chord="1.5" 
         length="1.4" 
         taper="0.2"
         sweep="26">
         <stall aoa="16" width="7" peak="1.5"/>
         <flap0 start="0" end="1" lift="1.7" drag="1.3"/>

         <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
  </vstab>

  <!-- 
   De havilland goblin 3. 3350lbf
  -->
  <jet x="-0.25" y="0" z="-0.2"
       n1-idle="30" 
       n1-max="90" 
       n2-idle="35" 
       n2-max="95"
       egt="850" 
       tsfc="1.39"
       mass="1550" 
       thrust="3350" >
    <actionpt x="-2.28" y="0" z="-0.2"/>
       <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
  </jet>
  

  <!-- Undercarriage -->
  <!-- nose -->
  <gear x="3.0" y="0" z="-1.28"
        retract-time="7"
        compression="0.7"
        spring="1.1"
        damp="1.4"
        sfric="0.79"
        dfric="0.69">

        <control-input axis="/controls/flight/rudder" control="STEER" src0="-1.0" src1="1.0" dst0="-0.078" dst1="0.078"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

  <!-- left main -->
  <gear x="-0.189" y="1.587" z="-1.35"
        retract-time="7"
       compression="0.8"
        spring="0.85"
        damp="2" 
        sfric="0.8"
        dfric="0.7">

        <control-input axis="/controls/gear/brake-left" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

  <!-- right main -->
  <gear x="-0.189" y="-1.587" z="-1.35"
        retract-time="7"
       compression="0.8"
        spring="0.85"
        damp="2"
        sfric="0.8"
        dfric="0.7">

        <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

  <weight x="1.46" y="0.0" z="0.21" mass-prop="/yasim/gloster-meteor/pilot-lb"/>
<!-- <ballast x="3.9" y="0" z="-0.05" mass="900"/> -->

  <!-- Internal tanks 
   2*280 liter wings
  -->
  <tank x="0.46" y="-1.86" z="-0.0" jet="true" capacity="1000"/>
  <tank x="0.46"  y="1.86" z="-0.0" jet="true" capacity="1000"/>
  
  <tank x="0.09" y="-2.93" z="-0.44" jet="true" capacity="250"/>
  <tank x="0.09"  y="2.93" z="-0.44" jet="true" capacity="250"/>

  <!-- CG Theorique x=1.358 y=0 z=-0.260 -->
  <!-- x a 1.536 pour etre en avant des roues -->
  <ballast x="2.65" y="0" z="-0.1" mass="2750"/>

</airplane>