Robinson-R66/raven.xml

<?xml version="1.0" encoding="ISO-8859-1"?>

<!-- R44 FDM

     2011 BARANGER Emmanuel First for test
     2011 JM-26 First really R44 FDM
   -->

   <airplane mass="1505" version="YASIM_VERSION_CURRENT">

    <approach speed="47" aoa="16">
      <control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
    </approach>

    <cruise speed="100" alt="0">
      <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
    </cruise>

    <rotor name="main" 
     x="2.218" y="0.0" z="1.605" 
    nx="0.05" ny="0" nz="1"
     fx="0.99" fy="0" fz="-0.043" 
     ccw="1"
	 phi0="45"
     maxcollective="7.2"
     mincollective="0.0"
     mincyclicele="-12.5"
     maxcyclicele="17.5"
     mincyclicail="-13.5"
     maxcyclicail="8.7"
     diameter="10.0584"
    numblades="2"
     weightperblade="35"
     relbladecenter="0.3"
     dynamic="1"
     rpm="495"
     rellenflaphinge="0.2"
     delta3="0.0"
     delta=".25"
     pitch-a="10"
     pitch-b="15"
     flapmin="-13.0"
     flapmax="13.0"
     flap0="-2.0"
     flap0factor="0"
     notorque="0"
     dragfactor="0.30"
     translift-ve="20"
     translift-maxfactor="0.3"
     ground-effect-constant="0.1"
     twist="-6"
     taper="1"
     chord="0.18288"
     number-of-segments="8"
     number-of-parts="8"
     rel-len-where-incidence-is-measured="0.7"
     rel-len-blade-start="0.04"
     airfoil-lift-coefficient="5.67"
     airfoil-drag-coefficient0="0.01"
     airfoil-drag-coefficient1="0.05"
     incidence-stall-zero-speed="19"
     incidence-stall-half-sonic-speed="10"
     lift-factor-stall="0.15"
    stall-change-over="5.5"
    drag-factor-stall="4.0"
     cyclic-factor="1.0"
     rotor-correction-factor="0.9"
	  balance="0.97">
     <control-input axis="/controls/flight/aileron-trim" control="CYCLICAIL" split="true"/>
     <control-input axis="/controls/flight/aileron" control="CYCLICAIL" src0="-1.0" src1="1.0" dst0="-1.0" dst1="1.0"/>
     <control-input axis="/controls/flight/elevator-trim" control="CYCLICELE" split="true"/>
     <control-input axis="/controls/flight/elevator" control="CYCLICELE" src0="-1.0" src1="1.0" dst0="-1.0" dst1="1.0"/>
     <control-input axis="/controls/engines/engine[0]/throttle" control="COLLECTIVE" src0="0.0" src1="1.0" dst0="1.0" dst1="-1.0"/>
   </rotor>

   <rotor name="tail"
     x="-3.609" y="0.362" z="0.395"
     nx="0.0" ny="-1" nz="0.0"
     fx="1" fy="0" fz="0"
     ccw="1"
     maxcollective="22"
     mincollective="-34"
     diameter="1.47"
     numblades="2"
     weightperblade="1"
     relbladecenter="0.55"
     dynamic="1"
     rpm="3356"
     rellenflaphinge="0.0"
     delta3="1"
     translift="0" delta="0.8"
     pitch-a="10"
     pitch-b="15"
     airfoil-lift-coefficient="6.4"
     airfoil-drag-coefficient0="0.0035"
     airfoil-drag-coefficient1="0.10"
     incidence-stall-zero-speed="19.25"
     incidence-stall-half-sonic-speed="10.5"
     lift-factor-stall="0.26"
     stall-change-over="7"
     drag-factor-stall="8"
     notorque="0"
     taper="1"
     chord="0.116"
     number-of-segments="5"
     number-of-parts="4"
     rel-len-blade-start="0.2"
     rotor-correction-factor="0.9"
     downwashfactor="0.3">
     <control-input axis="/controls/flight/rudder" control="COLLECTIVE" invert="true" src0="-1.0" src1="1.0" dst0="-1.0" dst1="1.0"/>
     <control-input axis="/controls/flight/fcs/tail-rotor/throttle" control="COLLECTIVE" src0="-1.0" src1="1.0" dst0="-1.0" dst1="1.0"/>
   </rotor>

   <rotorgear max-power-engine="183"
     max-power-rotor-brake="50"
     rotorgear-friction="0.5"
     engine-prop-factor="0.005"
     engine-accel-limit="3"
     yasimdragfactor="10"
     yasimliftfactor="140">
     <!--<control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>-->
     <control-input axis="/engines/engine/clutch-engaged" control="ROTORGEARENGINEON"/>
     <control-input axis="/controls/rotor/brake" control="ROTORBRAKE" src0="0.0" src1="1.0" dst0="0.0" dst1="1.0"/>
   </rotorgear>

   <cockpit x="3.405" y="0.252" z="-0.140"/>

   <!-- Fuse -->
   <fuselage ax="4.538" ay="0" az="-0.759" bx=" 0.594" by="0" bz="-0.534" width="1.361" taper="0.5" midpoint="0.35"/>
   <fuselage ax="1.751" ay="0" az="-0.069" bx="-3.678" by="0" bz=" 0.352" width="0.380" taper="0.5" midpoint="0.00"/>

   <vstab x="-3.589" y="-0.182" z="0.320"
     chord="0.510" 
     length="1.080" 
     taper="0.5" 
     sweep="13">
     <stall aoa="16" width="4" peak="1.5"/>
   </vstab>

   <vstab x="-3.589" y="-0.182" z="0.320"
     chord="0.510" 
     length="0.700" 
     taper="0.6"
     dihedral="270" 
     sweep="24">
     <stall aoa="16" width="4" peak="1.5"/>
   </vstab>

   <hstab x="-3.597" y="-0.098" z="0.237"
     chord="0.52" 
     length="1.205" 
     taper="0.5"
     dihedral="180">
     <stall aoa="0" width="0" peak="1.5"/>
   </hstab>

   <!-- Avant gauche -->
   <gear x="3.603" y="1.043" z="-1.7" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1">
    <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>

  <!-- Avant droit -->
  <gear x="3.603" y="-1.043" z="-1.7" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1">
    <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>

  <!-- Arriere gauche -->
  <gear x="1.465" y="1.043" z="-1.75" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1">
	
    <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
    <control-speed control="EXTEND" transition-time="7"/>
    <control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
  </gear>

  <!-- Arriere droit -->
  <gear x="1.465" y="-1.043" z="-1.75" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1">
    <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
    <control-speed control="EXTEND" transition-time="7"/>
    <control-output control="EXTEND" prop="gear/gear[3]/position-norm"/>
  </gear>

  <!-- Patte de queue -->
  <gear x="-4.018" y="-0.183" z="-0.445"
    skid="1"
    compression="0.01"
    spring="0.1"
    sfric="1"
    dfric="1">
  </gear>

  <tank x="4" y="0" z="-0.31" capacity="189.6"/>
  <tank x="4" y="0" z="-0.31" capacity="111"/>

  <weight x="0.5588" y=" 0.270" z="-1.8" mass-prop="/sim/weight[0]/weight-lb"/> <!-- left seat  -->
  <weight x="0.5588" y="-0.236" z="-1.8" mass-prop="/sim/weight[1]/weight-lb"/> <!-- right seat -->

  <ballast x="3" y=" 0.0" z="-0.5" mass="450"/>
  <ballast x="2" y=" 1.1" z=" 1.1" mass="100"/>
  <ballast x="2" y="-1.1" z=" 1.1" mass="50"/>

  <thruster x="-0.75"  y="0" z="0" vx="-1" vy="0" vz="1" thrust="850">
    <control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>

  <thruster x="-0.75"  y="0" z="0" vx="0" vy="1" vz="0" thrust="300">
    <control-input axis="/sim/model/pushback/target-speed-fps-y" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  </thruster>

</airplane>