Robinson-R66/r66-yasim.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="1290" version="YASIM_VERSION_CURRENT">

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

    <cruise speed="117" alt="0">
      <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
    </cruise>

    <rotor name="main" 
     x="0.1" y="0.0" z="1.905" 
     nx="0.05" ny="0" nz="1"
     fx="0.99" fy="0" fz="-0.043" 
     ccw="1"
	 phi0="45"
     maxcollective="13"
     mincollective="0.0"
     mincyclicele="-30.5"
     maxcyclicele="30.5"
     mincyclicail="-10.5"
     maxcyclicail="15.7"
     diameter="10.0584"
    numblades="2"
     weightperblade="40"
     relbladecenter="0.3"
     dynamic="0.8"
     rpm="408"
     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="5"
     translift-maxfactor="0.7"
     ground-effect-constant="0.1"
     twist="-4"
     taper="0.95"
     chord="0.309"
     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="5.87"
     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="0.98">
     <control-input axis="/controls/flight/aileron-trim" control="CYCLICAIL"/>
  <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"/>
  <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="-5.75" y="0.362" z="0.6"
     nx="0.0" ny="-1" nz="0.0"
     fx="1" fy="0" fz="0"
     ccw="1"
     maxcollective="13"
     mincollective="-16"
     diameter="1.524"
     numblades="2"
     weightperblade="1"
     relbladecenter="0.55"
     dynamic="0.70"
     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="0.1397"
     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-trim" control="COLLECTIVE" invert="true"/>
  <control-input axis="/controls/flight/rudder" control="COLLECTIVE" invert="true"
                 src0="-1.0" src1="1.0"
                 dst0="-1.0" dst1="1.0"/>
   </rotor>

   <rotorgear max-power-engine="200"
    max-power-rotor-brake="50"
     rotorgear-friction="0.3"
     engine-prop-factor="0.005"
     engine-accel-limit="3"
     yasimdragfactor="5"
     yasimliftfactor="145">


    <control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>
    <control-input axis="/controls/rotor/brake" control="ROTORBRAKE"
             src0="0.0" src1="1.0"
             dst0="0.0" dst1="1.0"/>
    <control-input axis="/controls/rotor/reltarget" control="ROTORRELTARGET"
             src0="0.0" src1="1.0"
             dst0="0.0" dst1="1.0"/>
    <control-input axis="/controls/rotor/maxreltorque" control="ROTORENGINEMAXRELTORQUE"
             src0="0.0" src1="1.0"
             dst0="0.0" dst1="1.0"/>
   </rotorgear>

   <cockpit x="1.405" y="0.252" z="-0.140"/>

   <!-- Fuse -->
   <fuselage ax="2.438" ay="0" az="-0.559" bx=" -1.794" by="0" bz="-0.534" width="1.561" taper="0.5" midpoint="0.35"/>
   <fuselage ax="-0.4" ay="0" az="-0.0" bx="-5.7" by="0" bz=" 0.6" width="0.6" taper="0.3" midpoint="0.00"/>

   <vstab x="-5.8" y="-0.182" z="0.6"
     chord="0.510" 
     length="1.080" 
     taper="0.5" 
     sweep="16"
     incidence="0.5">
         <stall aoa="6" width="9" peak="2.3"/>
   </vstab>

   <vstab x="-5.8" y="-0.182" z="0.6"
     chord="0.510" 
     length="0.800" 
     taper="0.6"
     dihedral="-90" 
     sweep="18"
      incidence="-0.5">
         <stall aoa="6" width="9" peak="2.3"/>
   </vstab>

   <hstab x="-5.8" y="-0.098" z="0.637"
     chord="0.52" 
     length="1.15" 
     taper="0.5"
     dihedral="0">
     <stall aoa="0" width="0" peak="1.5"/>
   </hstab>

   <!-- Avant gauche -->
   <gear x="1.603" y="1.043" z="-1.6" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1"/>
   


  <!-- Avant droit -->
  <gear x="1.603" y="-1.043" z="-1.6" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1"/>
    


  <!-- Arriere gauche -->
  <gear x="-1" y="1.043" z="-1.6" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1"/>
   
 

  <!-- Arriere droit -->
  <gear x="-1" y="-1.043" z="-1.6" 
    skid="1" 
    compression="0.05"
    spring="1.0" 
    damp="0.2" 
    sfric="0.5" 
    dfric="0.4"
	stiction="1"/>
   


  <!-- Patte de queue -->
  <gear x="-7" y="-0.183" z="-0.445"
    skid="1"
    compression="0.01"
    spring="0.1"
    sfric="1"
    dfric="1"
	stiction="1"/>


  <tank x="1" y="0" z="-0.31" capacity="1700"/>
  <tank x="1" y="0" z="-0.31" capacity="163.72"/>

  <weight x="-2.5588" y=" 0.270" z="-1.8" mass-prop="/sim/weight[0]/weight-lb"/> <!-- left seat  -->
  <weight x="-2.5588" y="-0.236" z="-1.8" mass-prop="/sim/weight[1]/weight-lb"/> <!-- right seat -->

  <ballast x="1" y=" 0.0" z="-0.5" mass="450"/>
  <ballast x="-1" y=" 1.1" z=" 1.1" mass="100"/>
  <ballast x="-1" y="-1.1" z=" 1.1" mass="50"/>

   <thruster  x="0.1" y="0.0" z="1.905" vx="1" vy="0" vz="0" thrust="2000">
    <control-input axis="/rotors/main/vibration/longitudinal" src0="-1" src1="1" dst0="-1" dst1="1" control="THROTTLE"/>
  </thruster>

  <thruster  x="0.1" y="0.0" z="1.905" vx="0" vy="1" vz="0" thrust="2000">
    <control-input axis="/rotors/main/vibration/lateral" src0="-1" src1="1" dst0="-1" dst1="1" control="THROTTLE"/>
  </thruster>


</airplane>