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Mil-Mi-2.xml
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<?xml version="1.0" encoding="ISO-8859-1"?>
<!-- R44 FDM
2011 BARANGER Emmanuel First for test
2011 JM-26 First really R44 FDM
2019 Re-used as Mi2 FDM
-->
<airplane mass="1280">
<approach speed="47" aoa="16">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
</approach>
<cruise speed="125" 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="17"
mincollective="0.3"
mincyclicele="-9.5"
maxcyclicele="9.5"
mincyclicail="-2.5"
maxcyclicail="2.7"
diameter="10.1"
numblades="2"
weightperblade="60"
relbladecenter="0.5"
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="0.7"
ground-effect-constant="0.1"
twist="-8.5"
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="0.18"
stall-change-over="5.5"
drag-factor-stall="2.0"
cyclic-factor="1.0"
rotor-correction-factor="0.9">
<control-input axis="/controls/flight/aileron-trim" control="CYCLICAIL" split="true"/>
<control-input axis="/controls/flight/fcs/roll" 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/fcs/pitch" 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="24"
mincollective="-5"
diameter="1.47"
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="0.116"
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/fcs/yaw" 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="380"
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>
<!-- Nose -->
<gear x="3.72847" y="0.01353" z="-1.68243"
skid="0"
compression="0.05"
spring="1.0"
damp="0.2"
sfric="0.5"
dfric="0.4">
<control-input axis="/controls/flight/rudder" control="STEER" square="true" src0="-1" dst0="-1.0" src1="1" dst1="1.0"/>
<control-output control="STEER" prop="controls/gear/steering"/>
</gear>
<!-- Left -->
<gear x="1.08159" y="1.53904" z="-1.56537"
skid="0"
compression="0.05"
spring="1.0"
damp="0.2"
sfric="0.5"
dfric="0.4">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<!-- Right -->
<gear x="1.08159" y="-1.5126" z="-1.56537"
skid="0"
compression="0.05"
spring="1.0"
damp="0.2"
sfric="0.5"
dfric="0.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<!-- Tail -->
<gear x="-5.6643" y="0.01261" z="-0.50964"
skid="1"
compression="0.01"
spring="0.1"
sfric="1"
dfric="1">
</gear>
<tank x="1.85342" y="0" z="-0.996445" jet="1" capacity="1322.0"/>
<weight x="3.41157" y="0.506127" z="-0.175444" mass-prop="/sim/weight[0]/weight-lb"/> <!-- left seat -->
<weight x="3.41157" y="-0.506127" z="-0.175444" 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"/>
</airplane>