FGR2Phantom/FGR-yasim.xml

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

<!-- FGR2 Phantom II
<airplane mass="31000" version="YASIM_VERSION_CURRENT">-->

<airplane mass="31000" version="YASIM_VERSION_CURRENT">

<!-- Approach configuration -->
<approach speed="130" aoa="8" 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="1.0"/>
<control-setting axis="/controls/flight/spoilers" value="0.5"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>

<!-- Cruise configuration -->
<!--
<cruise speed="1204" alt="40000" fuel="0.41">
-->
<cruise speed="1100	" alt="40000" fuel="0.41">
  <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="0.0"/>
  <control-setting axis="/controls/gear/gear-down" value="0"/>
 </cruise>

<!-- pilot eyepoint -->
<cockpit x="5.5" y="0.0" z="1.0"/>

<fuselage ax="9.3" ay="0" az="0" bx="4" by="0" bz="0.78" width="1.8" taper="0.2" midpoint="1" idrag="0.3"/>

  <fuselage ax="4" ay="0" az="0.78" bx="-4" by="0" bz="0.7" width="1.8" taper="1" midpoint="0" idrag="0.3"/>
  
   <fuselage ax="-4" ay="0" az="0.78" bx="-8.6" by="0" bz="1.3" width="1.8" taper="0.2" midpoint="0" idrag="0.2"/>
  
<!-- Engines -->
  <fuselage ax="4.5" ay="0.9" az="0.7" bx="-4.7" by="0.6" bz="0.3" width="1.0" taper= "1" midpoint= "0.8" idrag="0.3" />
  <fuselage ax="4.5" ay="-0.9" az="0.7" bx="-4.7" by="-0.6" bz="0.3" width="1.0" taper= "1" midpoint= "0.8" idrag="0.3" />





<wing x="0.4" y="1.2" z="-0.1"
chord="5.75" 
length="3.53"
taper="0.52" 
incidence="1.4"
twist="-2.0"
idrag="0.5"
sweep="34" 
dihedral="0">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.01" end="0.47" lift="1.9" drag="1.4"/>
<flap1 start="0.47" end="0.813" lift="1.2" drag="1.2"/>

<slat aoa="4" start="0.04" end="0.813" lift="1.4" drag="1.3"/>
<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-input axis="/controls/flight/flaps" control="SLAT"/>


<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
<control-output control="SLAT" prop="surface-positions/slat-pos-norm"/>

<control-speed control="SLAT" transition-time="1.9"/>
<control-speed control="FLAP0" transition-time="15"/>
<control-speed control="FLAP1" transition-time="0.25"/>

</wing>

<!-- Wing end -->
 
 <wing x="-1.55" y="4.13" z="-0.15" 
 chord="3.15" 
length="2.2"
taper="0.4" 
incidence="1.4"
sweep="37" 
dihedral="11"
camber="-0.05">
  <stall aoa="18" width="2" peak="1.3"/>
  
 </wing>
 
 <!-- body -->

<mstab x="0" y="0" z="0.173" chord="7" 
length="1.025"
taper="1" 
incidence="0"
sweep="0" 
dihedral="0"
camber="-0.05">
         <stall aoa="18" width="2" peak="1.3"/>
         <flap0 start="0.01" end="0.47" lift="1.1" drag="29.9"/>
         <control-input axis="/controls/flight/speedbrake" control="FLAP0"/>
         <control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
         <control-speed control="FLAP0" transition-time="4"/>
  </mstab>



<hstab x="-6.3" y="0.220" z="1.24"
taper="0.23"
length="2.65"
chord="2.6"
incidence="-1.7"
sweep="27"
dihedral="-19">
<stall aoa="35" width="33" peak="2"/>
<flap0 start="0.01" end="1.0" lift="2" drag="1.4"/>
<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"/>
<control-speed control="FLAP0" transition-time="0.4"/>


</hstab>


<vstab x="-5.45" y="0" z="1.5"
chord="5.5" 
length="2.7" 
taper="0.29"
incidence="0"
sweep="48">
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0.01" end=".94" lift="1.3" 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"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>



<!-- Engines   source            : http://en.wikipedia.org/wiki/Rolls-Royce_Spey

                 name              : Rolls-Royce Spey
                 type              : Turbofan
                 power cruise      : 12150 lbf  
                 adterburner       : 20515 lbf  
                 weight            : 4093 lb 
  -->
 <jet x="0" y="0.555" z="0.334"
mass="4093"
thrust="12140"
afterburner="20515"
n1-idle="1" 
n1-max="125" >
  <actionpt x="-4.561" y="0.483" z="-0.0"/>
  <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
  <control-input axis="/controls/engines/engine[0]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
  <control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
 </jet>

  
 <jet x="0" y="-0.555" z="0.334"
mass="4093"
thrust="12140"
afterburner="20515"
n1-idle="1" 
n1-max="125" >
  <actionpt x="-2.561" y="-0.483" z="-0.0"/>
  <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
  <control-input axis="/controls/engines/engine[1]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
  <control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
 </jet>

<!-- nose -->
 <gear x="6.423" y="0" z="-1.970" 
retract-time="8"
compression="0.7"
        spring="1.1"
        damp="1.4">
  <control-input axis="/controls/flight/rudder" control="STEER" square="false"/>
  <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="-0.664" y="2.695" z="-2.060"
retract-time="8"
compression="0.8"
        spring="0.85"
        damp="2">
  <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="-0.664" y="-2.695" z="-2.060"
retract-time="8"
compression="0.8"
        spring="0.85"
        damp="2">
  <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>

 <!-- FUEL tank0 -->
  <tank x="2.5" y=" 0.0" z="1.5" jet="true" capacity="1674"/>
  
  <!-- FUEL tank1 -->
  <tank x="0" y=" 0.0" z="1.5" jet="true" capacity="1510"/>
  
  <!-- FUEL tank2 -->
  <tank x="-1" y=" 0.0" z="1.5" jet="true" capacity="1175"/>
  
  <!-- FUEL tank3 -->
  <tank x="-2" y=" 0.0" z="1.5" jet="true" capacity="1558"/>
  
  <!-- FUEL tank4 -->
  <tank x="-2.5" y=" 0.0" z="1.5" jet="true" capacity="1408"/>
  
  <!-- FUEL tank5 -->
  <tank x="-3" y=" 0.0" z="1.5" jet="true" capacity="1640"/>
  
  <!-- FUEL tank6 not used in the FGR2 -->
  <tank x="-3.5" y=" 0.0" z="1.5" jet="true" capacity="0"/>
 

  <!-- FUEL Wing -->
  <tank x="0" y=" 1.5" z="-0.2" jet="true" capacity="2200"/>
  <tank x="0" y=" -1.5" z="-0.2" jet="true" capacity="2200"/>

  <!-- EXT TANK -->
  <tank x="0.0" y= " 0.0"  z="-0.8" jet="true" capacity="4114"/>
  <tank x="0.0" y= " 3.3"  z="-0.8" jet="true" capacity="2542"/>
  <tank x="0.0" y= "-3.3"  z="-0.8" jet="true" capacity="2542"/>


<!-- ballast -->
<ballast x="6.7" y="0" z="-1.59" mass="3000"/>

<ballast x="5.74" y="0" z="-0.35" mass="1200"/>

<ballast x="4" y="0" z="0.2" mass="4900"/>

<!-- ballast -->
<ballast x="5.05" y="0" z="-0.1" mass="200"/>

<ballast x="-0.8" y="3" z="-1.59" mass="200"/>

<ballast x="-0.8" y="-3" z="-1.59" mass="200"/>


<!-- Parachute -->
  <!-- X axis - force forward -->
  <thruster x="-7.015"  y="-0.108" z="0.720" vx="1" vy="0" vz="0"
        thrust="10000">
        <control-input axis="/controls/engines/thruster[1]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>
  <!-- Y axis - force left -->
  <thruster x="-7.015"  y="-0.108" z="0.720" vx="0" vy="1" vz="0"
        thrust="10000">
        <control-input axis="/controls/engines/thruster[2]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>
  <!-- Z axis - force up -->
  <thruster x="-7.015"  y="-0.108" z="0.720" vx="0" vy="0" vz="1"
        thrust="10000">
        <control-input axis="/controls/engines/thruster[3]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>

<!-- Hook -->
  <hook x="-4.8" y="0" z="-0.282" 
        length="2.571" 
        down-angle="60" 
        up-angle="-18.6">
    <control-input axis="/controls/gear/tailhook" control="HEXTEND"/>
    <control-speed control="HEXTEND" transition-time="1.35"/>
  </hook>
  
  <!-- Launch-bar 			-0.780453-->
	<launchbar 	x="6.8"
							y="0.0"
							z="-1.0"
							length="3.5052">
							<!--down-angle="90"
							up-angle="0"
							holdback-x="-16.3"
							holdback-y="0.0"
							holdback-z="0.1175"
							holdback-length="2.0"-->
		<control-input axis="/controls/gear/launchbar"
									 control="LEXTEND"/>
		<control-speed control="LEXTEND"
									 transition-time="1"/>
	<control-input axis="/controls/gear/launchbar/acceleration-norm"
									 control="LACCEL"/>
	</launchbar>


  <!-- Stores -->
  
<weight x="0"
y="3.65"
z="0"
size="0.9"
mass-prop="sim/weight[0]/weight-lb"/>



<weight x="1.5"
y="2.17"
z="-0.55"
size="0.6"
mass-prop="sim/weight[1]/weight-lb"/>

<weight x="3.5"
y="0.45"
z="-0.25"
size="0.3"
mass-prop="sim/weight[2]/weight-lb"/>



<weight x="-1.8"
y="1.1"
z="-0.36"
size="0.3"
mass-prop="sim/weight[3]/weight-lb"/>





<weight x="0"
y="0"
z="-0.8"
size="0.95"
mass-prop="sim/weight[4]/weight-lb"/>




<weight x="-1.8"
y="-1.1"
z="-0.36"
size="0.3"
mass-prop="sim/weight[5]/weight-lb"/>



<weight x="3.5"
y="0.45"
z="-0.25"
size="0.3"
mass-prop="sim/weight[6]/weight-lb"/>



<weight x="1.5"
y="-2.17"
z="-0.55"
size="0.6"
mass-prop="sim/weight[7]/weight-lb"/>

<weight x="0"
y="-3.65"
z="0"
size="0.9"
mass-prop="sim/weight[8]/weight-lb"/>
  

</airplane>