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v22.xml
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<?xml version="1.0" encoding="ISO-8859-1"?>
<!-- Bell Boeing V22 Osprey : 2007 Maik JUSTUS
Updated : 2010 Oliver Thurau
Updated : 2014 Emmanuel BARANGER
-->
<airplane mass="50000">
<approach speed="85" aoa="6">
<control-setting axis="/sim/model/v22/solver_throttle" value="0.2"/>
<control-setting axis="/sim/model/v22/tilt" value="90"/>
</approach>
<cruise speed="275" alt="15000">
<control-setting axis="/sim/model/v22/solver_throttle" value="1"/>
<control-setting axis="/sim/model/v22/tilt" value="90"/>
</cruise>
<cockpit x="-1.88" y=".33" z="0.6"/>
<!-- main fuselage front-->
<fuselage ax=" 8.1" ay=" 0.00" az="-1.90" bx=" 5.80" by=" 0.00" bz="-1.40" width="2.20" taper="0.25" midpoint="1.0" cx="0.150" cy="0.15" cz="0.35" idrag="0"/>
<!-- main fuselage center -->
<fuselage ax=" 6.0" ay=" 0.00" az="-1.40" bx="-2.50" by=" 0.00" bz="-1.40" width="2.30" taper="0.95" midpoint="0.5" cx="0.350" cy="1.60" cz="0.35" idrag="0"/>
<!-- top fuselage -->
<fuselage ax=" 1.0" ay=" 0.00" az="-0.80" bx="-2.50" by=" 0.00" bz="-0.80" width="2.30" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 3.0" ay=" 0.00" az="-0.80" bx=" 1.00" by=" 0.00" bz="-0.80" width="2.30" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 4.0" ay=" 0.00" az="-0.80" bx=" 3.00" by=" 0.00" bz="-0.80" width="2.30" taper="0.40" midpoint="1.0" cx="0.150" cy="0.15" cz="0.35" idrag="0"/>
<!-- top fuselage right wingbase-->
<fuselage ax=" 3.2" ay="-0.20" az=" 0.00" bx=" 2.20" by="-0.70" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 2.2" ay="-0.70" az=" 0.00" bx=" 0.00" by="-0.70" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 0.0" ay="-0.70" az=" 0.00" bx="-1.20" by="-0.20" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 3.2" ay="-0.50" az=" 0.00" bx=" 2.20" by="-1.00" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 2.2" ay="-1.00" az=" 0.00" bx=" 0.00" by="-1.00" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 0.0" ay="-1.00" az=" 0.00" bx="-1.20" by="-0.40" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<!-- top fuselage left wingbase-->
<fuselage ax=" 3.2" ay=" 0.20" az=" 0.00" bx=" 2.20" by=" 0.70" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 2.2" ay=" 0.70" az=" 0.00" bx=" 0.00" by=" 0.70" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 0.0" ay=" 0.70" az=" 0.00" bx="-1.20" by=" 0.20" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 3.2" ay=" 0.50" az=" 0.00" bx=" 2.20" by=" 1.00" bz=" 0.00" width="0.50" taper="0.40" midpoint="1.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 2.2" ay=" 1.00" az=" 0.00" bx=" 0.00" by=" 1.00" bz=" 0.00" width="0.50" taper="1.00" midpoint="0.5" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<fuselage ax=" 0.0" ay=" 1.00" az=" 0.00" bx="-1.20" by=" 0.40" bz="-0.20" width="0.50" taper="0.40" midpoint="0.0" cx="0.015" cy="0.15" cz="0.35" idrag="0"/>
<!-- side fuselage right-->
<fuselage ax=" 3.0" ay="-0.75" az="-2.10" bx=" 1.00" by="-1.75" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax=" 1.2" ay="-1.70" az="-2.10" bx="-1.50" by="-1.70" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax=" 1.7" ay="-1.00" az="-2.10" bx="-1.50" by="-1.00" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-1.3" ay="-1.70" az="-2.10" bx="-3.80" by="-0.70" bz="-1.60" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<!-- side fuselage left-->
<fuselage ax=" 3.0" ay=" 0.75" az="-2.10" bx=" 1.00" by=" 1.75" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax=" 1.2" ay=" 1.70" az="-2.10" bx="-1.50" by=" 1.70" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax=" 1.7" ay=" 1.00" az="-2.10" bx="-1.50" by=" 1.00" bz="-2.10" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-1.3" ay=" 1.70" az="-2.10" bx="-3.80" by=" 0.70" bz="-1.60" width="0.80" taper="1.00" midpoint="0.5" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<!-- back fuselage -->
<fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by="-0.45" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by=" 0.00" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-2.3" ay=" 0.00" az="-1.40" bx="-5.00" by=" 0.45" bz="-1.03" width="2.20" taper="0.55" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-4.8" ay="-0.45" az="-1.05" bx="-6.50" by="-0.75" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="2.00" cz="0.35" idrag="0"/>
<fuselage ax="-4.8" ay=" 0.00" az="-1.05" bx="-6.50" by=" 0.00" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-4.8" ay=" 0.45" az="-1.05" bx="-6.50" by=" 0.75" bz="-0.50" width="1.30" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-6.4" ay="-0.75" az="-0.51" bx="-7.70" by="-0.75" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-6.4" ay=" 0.00" az="-0.51" bx="-7.70" by=" 0.00" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<fuselage ax="-6.4" ay=" 0.75" az="-0.51" bx="-7.70" by=" 0.75" bz="-0.40" width="0.45" taper="0.35" midpoint="0.0" cx="0.015" cy="1.00" cz="0.35" idrag="0"/>
<!-- main wing -->
<wing x="0.90" y="0.4" z="0.30"
chord="2.65"
chord_real="2.65"
taper="1"
length_real="6.1"
length="6.1"
dihedral="1.8"
incidence="3.5"
camber="0.2"
sweep="-8">
<stall width="8" aoa="35" peak="1.5"/>
<flap0 drag="1.6" end="0.5" lift="2" start="0.02"/>
<flap1 drag="1.6" end="0.97" lift="2" start="0.5"/>
<control-input control="FLAP0" axis="/sim/model/v22/wing/flap"/>
<control-input control="FLAP1" axis="/sim/model/v22/wing/flap"/>
<control-input control="FLAP1" split="true" axis="sim/model/v22/wing/aileron"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/left-aileron-pos-norm" side="left"/>
<control-output control="FLAP1" prop="/surface-positions/right-aileron-pos-norm" side="right"/>
</wing>
<mstab x="-8.40" y="0.0" z="-0.45"
taper="1"
length="2.50"
chord="2.30"
sweep="0"
incidence="-0.5">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 drag="1.2" end="1" lift="1.9" start="0"/>
<control-input control="FLAP0" axis="/sim/model/v22/wing/elevator"/>
<control-output prop="/surface-positions/elevator-pos-norm" control="FLAP0"/>
</mstab>
<!-- Vertical wing - rudder -->
<vstab x="-7.90" y="2.52" z="-1.39"
taper="0.4"
length="3.20"
chord="2.72"
sweep="15"
incidence="0">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 drag="1.2" end="1" lift="1.4" start="0.4"/>
<control-input control="FLAP0" axis="/sim/model/v22/wing/rudder" invert="true"/>
<control-output prop="/surface-positions/rudder-pos-norm" control="FLAP0" min="1" max="-1"/>
</vstab>
<vstab x="-7.90" y="-2.52" z="-1.39"
taper="0.4"
length="3.20"
chord="2.72"
sweep="15"
incidence="0">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 drag="1.2" end="1" lift="1.4" start="0.4"/>
<control-input control="FLAP0" axis="/sim/model/v22/wing/rudder" invert="true"/>
<control-output prop="/surface-positions/rudder-pos-norm" control="FLAP0" min="1" max="-1"/>
</vstab>
<!-- main == right rotor (name=main for mp-protocol) -->
<!-- tail == left rotor (name=tail for mp-protocol) -->
<rotor name="main"
x="1.57" y="-7.041" z="2.550"
nx="0" ny="0" nz="1"
fx="1" fy="0" fz="0"
ccw="1"
maxcollective="180" mincollective="-180"
mincyclicele="-90" maxcyclicele="90"
mincyclicail="-90" maxcyclicail="90"
mintiltpitch="-180" maxtiltpitch="180"
tiltcenterx="1.75" tiltcentery="-2.1" tiltcenterz="0.30"
mintiltroll="-90" maxtiltroll="90"
diameter="11.58"
numblades="3"
weightperblade="675"
twist="-47.5"
chord="0.81"
rpm="412"
relbladecenter="0.5"
dynamic="1"
rellenflaphinge="0.13"
delta3="-0.26"
delta="0.25"
pitch-a="10" pitch-b="15"
flapmin="-15" flapmax="15"
flap0="-2"
flap0factor="0"
notorque="0"
dragfactor="0.30"
translift-ve="20"
translift-maxfactor="1.3"
ground-effect-constant="0.1"
taper="1"
number-of-segments="8"
number-of-parts="8"
rel-len-where-incidence-is-measured="0.6"
rel-len-blade-start="0.16"
airfoil-lift-coefficient="3.15"
airfoil-drag-coefficient0="0.38"
airfoil-drag-coefficient1="5.5"
incidence-stall-zero-speed="65"
incidence-stall-half-sonic-speed="55.0"
lift-factor-stall="0.45"
stall-change-over="11"
drag-factor-stall="4.0"
cyclic-factor="0.8"
rotor-correction-factor="1.7"
balance="1"
downwashfactor="0.3"
phi0="95">
<control-input axis="/sim/model/v22/tilt" control="TILTPITCH" src0="-180" src1="180" dst0="1" dst1="-1"/>
<control-input axis="/sim/model/v22/rotor/right/elevator" control="CYCLICELE" src0="-90" src1="90" dst0="-1" dst1="1"/>
<control-input axis="/sim/model/v22/rotor/right/collective" control="COLLECTIVE" src0="-180" src1="180" dst0="-1" dst1="1"/>
</rotor>
<rotor name="tail"
x="1.57" y="7.041" z="2.550"
nx="0" ny="0" nz="1"
fx="1" fy="0" fz="0"
ccw="0"
maxcollective="180" mincollective="-180"
mincyclicele="-90" maxcyclicele="90"
mincyclicail="-90" maxcyclicail="90"
mintiltpitch="-180" maxtiltpitch="180"
tiltcenterx="1.75" tiltcentery="2.1" tiltcenterz="0.30"
mintiltroll="-90" maxtiltroll="90"
diameter="11.58"
numblades="3"
weightperblade="675"
twist="-47.5"
chord="0.81"
rpm="412"
relbladecenter="0.5"
dynamic="1"
rellenflaphinge="0.13"
delta3="-0.26"
delta="0.25"
pitch-a="10" pitch-b="15"
flapmin="-15" flapmax="15"
flap0="-2"
flap0factor="0"
notorque="0"
dragfactor="0.30"
translift-ve="20"
translift-maxfactor="1.3"
ground-effect-constant="0.1"
taper="1"
number-of-segments="8"
number-of-parts="8"
rel-len-where-incidence-is-measured="0.6"
rel-len-blade-start="0.16"
airfoil-lift-coefficient="3.15"
airfoil-drag-coefficient0="0.38"
airfoil-drag-coefficient1="5.5"
incidence-stall-zero-speed="65"
incidence-stall-half-sonic-speed="55"
lift-factor-stall="0.45"
stall-change-over="11"
drag-factor-stall="4.0"
cyclic-factor="0.8"
rotor-correction-factor="1.7"
balance="1"
downwashfactor="0.3"
phi0="95">
<control-input axis="/sim/model/v22/tilt" control="TILTPITCH" src0="-180" src1="180" dst0="1" dst1="-1"/>
<control-input axis="/sim/model/v22/rotor/left/elevator" control="CYCLICELE" src0="-90" src1="90" dst0="-1" dst1="1"/>
<control-input axis="/sim/model/v22/rotor/left/collective" control="COLLECTIVE" src0="-180" src1="180" dst0="-1" dst1="1"/>
</rotor>
<rotorgear max-power-engine-real="9172"
max-power-engine="131720"
max-power-rotor-brake="4850"
rotorgear-friction="30"
engine-prop-factor="0.015"
engine-accel-limit="4"
yasimdragfactor="270"
yasimliftfactor="28">
<control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>
<control-input axis="/controls/rotor/brake" control="ROTORBRAKE" src0="0" src1="1" dst0="0" dst1="1"/>
<control-input axis="/controls/rotor/reltarget" control="ROTORRELTARGET" src0="0" src1="2" dst0="0" dst1="2"/>
<control-input axis="/controls/rotor/maxreltorque" control="ROTORENGINEMAXRELTORQUE" src0="0" src1="2" dst0="0" dst1="2"/>
</rotorgear>
<!-- front gear -->
<gear x="7.428" y="0" z="-2.949"
compression="0.2"
spring="0.65"
damp="0.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
<control-input axis="/controls/flight/rudder" control="STEER" square="true" src0="-1.0" src1="1.0" dst0="-0.8" dst1="0.8"/>
<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="5"/>
</gear>
<!-- left gear -->
<gear x="0.467" y="2.101" z="-2.949"
compression="0.2"
spring="0.65"
damp="0.4">
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
<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="5.1"/>
</gear>
<!-- right gear -->
<gear x="0.467" y="-2.101" z="-2.949"
compression="0.2"
spring="0.65"
damp="0.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
<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="5.2"/>
</gear>
<!-- CRASH LANDING FX - left skid -->
<gear x=" 6.00" y=" 1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x="-2.40" y=" 1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- CRASH LANDING FX - left skid -->
<gear x=" 6.00" y="-1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x="-2.40" y="-1.000" z="-2.50" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- CRASH FX - right ruder skid -->
<gear x="-7.50" y=" 2.500" z="-1.38" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x="-9.00" y=" 2.500" z="-1.32" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- CRASH FX - left ruder skid -->
<gear x="-7.50" y="-2.500" z="-1.38" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x="-9.00" y="-2.500" z="-1.32" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- CRASH FX - right engine skid ax="1.57" ay="7.041" az="2.550" -->
<gear x=" 2.52" y="-7.441" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x=" 1.40" y="-7.241" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- CRASH FX - left engine skid ax="1.57" ay="7.041" az="2.550" -->
<gear x=" 2.52" y="+7.441" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<gear x=" 1.40" y="+7.241" z="-1.87" skid="1" compression="0.1" spring="0.8" sfric="0.7" dfric="0.6" ignored-by-solver="1"/>
<!-- Forward sponson Fuel tank -->
<tank x="1.70" y=" 1.4" z="-2.10" capacity="75"/>
<tank x="1.70" y="-1.4" z="-2.10" capacity="75"/>
<!-- Wing feeder tank -->
<tank x="1.90" y=" 5.8" z=" 0.30" capacity="75"/>
<tank x="1.90" y="-5.8" z=" 0.30" capacity="75"/>
<!-- Wing aux tank -->
<tank x="1.90" y=" 3.6" z=" 0.10" capacity="75"/>
<tank x="1.90" y="-3.6" z=" 0.10" capacity="75"/>
<!-- work around bug in native-fdm.cxx:184 -->
<tank x="0" y="0" z="0" capacity="0"/>
<!-- ballast corections overall plane-->
<ballast x=" 4.25" y=" 0" z="-2.5" mass=" 9500"/>
<ballast x="-8.00" y=" 0" z=" 0.5" mass="-9800"/>
<!-- engine weight: 971 lbs, add some lbs for hydraulics and -->
<ballast x=" 1.91" yr=" 6" y=" 7" z="0.39" mass="1000"/>
<ballast x=" 1.91" yr="-6" y="-7" z="0.39" mass="1000"/>
<!-- gear weight: 230 lbs, add some lbs for hydraulics and -->
<ballast x=" 7.10" yr=" 0" y=" 0.0" z="-2.20" mass="180"/>
<ballast x="-1.10" yr=" 6" y=" 2.1" z="-2.40" mass="230"/>
<ballast x="-1.10" yr="-6" y="-2.1" z="-2.40" mass="230"/>
<!-- pilot -->
<weight x="6.0" y=" 0.6" z="-1.3" mass-prop="/sim/weight[0]/weight-lb"/>
<!-- co-pilot -->
<weight x="6.0" y="-0.6" z="-1.3" mass-prop="/sim/weight[1]/weight-lb"/>
<!-- right passenger -->
<weight x="4.2" y=" 0.6" z="-1.5" mass-prop="/sim/weight[2]/weight-lb"/>
<!-- left passenger -->
<weight x="4.2" y="-0.6" z="-1.5" mass-prop="/sim/weight[3]/weight-lb"/>
<!-- load -->
<weight x="0.2" y=" 0.0" z="-1.9" mass-prop="/sim/weight[4]/weight-lb"/>
<!-- pushback -->
<thruster x="7.105" y="0" z="-3.212"
vx="1" vy="0" vz="0"
thrust="5200">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<hitch name="aerotow"
x="-3.1" y="0" z="-2.525"
force-is-calculated-by-other="0">
<tow length="30"
weight-per-meter="0.035"
elastic-constant="9000"
break-force="80000"
mp-auto-connect-period="0"/>
<winch max-tow-length="100"
min-tow-length="30"
initial-tow-length="30"/>
<control-input axis="/controls/aerotow/find-aircraft" control="FINDAITOW"/>
</hitch>
</airplane>