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ac130-yasim.xml
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<?xml version="1.0" encoding="ISO-8859-1"?>
<!-- C130-H YASim config. - 2010 Jack Mermod
Source : http://en.wikipedia.org/wiki/C-130_Hercules
Envergure : 40.4 m (132 ft 7 in)
Longueur : 29.8 m (97 ft 9 in)
Hauteur : 11.6 m (38 ft 3 in)
Poids vide: 34600 kg (76120 lbs)
Moteurs : 4 Allison T56-A-15 turboprops 4591 CV, 13820 RPM, 1940 lb (880 kg)
Helices : Hamilton Standard 43E60-6901A (1074 lbs)
Vitesse : 644 km/h (348 kts)
-->
<airplane mass="76120">
<!-- Configuration d'approche -->
<approach speed="123" aoa="3.0" fuel="1.0">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[2]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[3]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.7"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>
<!-- Configuration de croisiere -->
<cruise speed="348" alt="28000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.8"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.8"/>
<control-setting axis="/controls/engines/engine[2]/propeller-pitch" value="0.8"/>
<control-setting axis="/controls/engines/engine[3]/propeller-pitch" value="0.8"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
<cockpit x="10.333" y="0.598" z="3.005"/>
<!-- Fuselage -->
<fuselage ax="13.224" ay="0" az="1.23" bx="11.80" by="0" bz="1.23" width="2.00" taper="0.40" midpoint="1.00"/>
<fuselage ax="12.00" ay="0" az="1.12" bx="8.90" by="0" bz="2.02" width="4.36" taper="0.42" midpoint="1.00"/>
<fuselage ax="9.50" ay="0" az="2.05" bx="-4.10" by="0" bz="2.05" width="4.304" taper="1.00" midpoint="1.00"/>
<fuselage ax="-3.80" ay="0" az="2.05" bx="-11.50" by="0" bz="3.50" width="4.304" taper="0.3" midpoint="0.00"/>
<fuselage ax="-11.50" ay="0" az="3.50" bx="-16.414" by="0" bz="4.175" width="1.30" taper="0.1" midpoint="0.00"/>
<!-- engines -->
<fuselage ax="3.533" ay="9.821" az="3.725" bx="-1.427" by="9.821" bz="3.725" width="1.05" taper="0.60" midpoint="0.15"/>
<fuselage ax="3.533" ay="4.929" az="3.725" bx="-1.427" by="4.929" bz="3.725" width="1.05" taper="0.60" midpoint="0.15"/>
<fuselage ax="3.533" ay="-4.929" az="3.725" bx="-1.427" by="-4.929" bz="3.725" width="1.05" taper="0.60" midpoint="0.15"/>
<fuselage ax="3.533" ay="-9.821" az="3.725" bx="-1.427" by="-9.821" bz="3.725" width="1.05" taper="0.60" midpoint="0.15"/>
<!-- fuel tank -->
<fuselage ax="2.910" ay="7.695" az="2.172" bx="-4.795" by="7.695" bz="2.172" width="1.1" taper="0.60" midpoint="0.15"/>
<fuselage ax="2.910" ay="-7.695" az="2.172" bx="-4.795" by="-7.695" bz="2.172" width="1.1" taper="0.60" midpoint="0.15"/>
<!-- Ailes taper 0.85, twist 3-->
<wing x="-1.486" y="1.240" z="3.660"
chord="5.201"
length="18.9"
taper="0.565"
camber="0.147"
sweep="-1.7"
dihedral="2.5"
twist="-3.0">
<stall aoa="16.0" width="5" peak="1.3"/>
<flap0 start="0.048" end="0.679" lift="1.52" drag="1.63"/>
<flap1 start="0.679" end="0.990" lift="1.27" drag="1.35"/>
<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-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
<control-speed control="FLAP0" transition-time="15"/>
<control-speed control="FLAP1" transition-time="1.0"/>
</wing>
<!-- Gouverne de profondeur -->
<hstab x="-12.648" y="0.370" z="4.090"
chord="4.494"
length="7.5"
taper="0.43"
sweep="5">
<stall aoa="20.0" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.53" drag="1.53"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" side="left" prop="/surface-positions/elevator-pos-norm"/>
<control-speed control="FLAP0" transition-time="2.5"/>
</hstab>
<!-- Gouverne de direction -->
<vstab x="-12.181" y="0" z="4.296"
chord="5.776"
length="6.704"
taper="0.32"
sweep="8">
<stall aoa="16.0" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.5"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" effectiveness="1.0" 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="2.0"/>
</vstab>
<!-- Sources : http://en.wikipedia.org/wiki/Allison_T56
Engines : Allison T56
Type : Turboprop
Power : 5565 ch
Masse : 1940 lb (880 kg)
RPM : 2400 - 2600
Propeller : Hamilton Standard 43E60-6901A (1074 lbs)
engine + propeller = 1940 + 1074 = 3014
-->
<!-- Exterieur gauche -->
<propeller x="2.22" y="9.821" z="3.307"
mass="3014"
moment="110"
radius="2.8"
cruise-speed="300"
cruise-rpm="920"
cruise-power="4500"
cruise-alt="25000"
min-rpm="220"
max-rpm="1020">
<actionpt x="3.764" y="9.821" z="3.622"/>
<control-input axis="/controls/engines/engine[0]/propeller-pitch" control="ADVANCE"/>
<turbine-engine eng-power="5565"
eng-rpm="1020"
alt="28000"
flat-rating="4150"
min-n2="70"
max-n2="100">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
</turbine-engine>
</propeller>
<!-- Interieur gauche -->
<propeller x="2.22" y="4.929" z="3.307"
mass="3014"
moment="110"
radius="2.8"
cruise-speed="300"
cruise-rpm="920"
cruise-power="4500"
cruise-alt="25000"
min-rpm="220"
max-rpm="1020">
<actionpt x="3.764" y="4.926" z="3.622"/>
<control-input axis="/controls/engines/engine[1]/propeller-pitch" control="ADVANCE"/>
<turbine-engine eng-power="5565"
eng-rpm="1020"
alt="28000"
flat-rating="4150"
min-n2="70"
max-n2="100">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[1]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[1]/boost" control="BOOST"/>
</turbine-engine>
</propeller>
<!-- Interieur droit -->
<propeller x="2.22" y="-4.929" z="3.307"
mass="3014"
moment="110"
radius="2.8"
cruise-speed="300"
cruise-rpm="920"
cruise-power="4500"
cruise-alt="25000"
min-rpm="220"
max-rpm="1020">
<actionpt x="3.764" y="-4.926" z="3.622"/>
<control-input axis="/controls/engines/engine[2]/propeller-pitch" control="ADVANCE"/>
<turbine-engine eng-power="5565"
eng-rpm="1020"
alt="28000"
flat-rating="4150"
min-n2="70"
max-n2="100">
<control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[2]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[2]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[2]/boost" control="BOOST"/>
</turbine-engine>
</propeller>
<!-- Exterieur droit -->
<propeller x="2.22" y="-9.821" z="3.307"
mass="3014"
moment="110"
radius="2.8"
cruise-speed="300"
cruise-rpm="920"
cruise-power="4500"
cruise-alt="25000"
min-rpm="220"
max-rpm="1020">
<actionpt x="3.764" y="-9.821" z="3.622"/>
<control-input axis="/controls/engines/engine[3]/propeller-pitch" control="ADVANCE"/>
<turbine-engine eng-power="5565"
eng-rpm="1020"
alt="28000"
flat-rating="4150"
min-n2="70"
max-n2="100">
<control-input axis="/controls/engines/engine[3]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[3]/starter" control="STARTER"/>
<control-input axis="/controls/engines/engine[3]/magnetos" control="MAGNETOS"/>
<control-input axis="/controls/engines/engine[3]/boost" control="BOOST"/>
</turbine-engine>
</propeller>
<!-- trusters for reverse -->
<thruster x="3.764" y="4.929" z="3.307"
vx="-1" vy="0" vz="0"
thrust="15000">
<control-input axis="/controls/engines/engine[0]/reverser" control="THROTTLE" src0="0" src1="1" dst0="0" dst1="1"/>
</thruster>
<thruster x="3.764" y="-4.929" z="3.307"
vx="-1" vy="0" vz="0"
thrust="15000">
<control-input axis="/controls/engines/engine[0]/reverser" control="THROTTLE" src0="0" src1="1" dst0="0" dst1="1"/>
</thruster>
<!-- Poition des roues au sol -->
<!-- Nez -->
<gear x="9.511" y="0" z="-0.878"
retract-time="7"
compression="0.45"
spring="0.78"
damp="1.35">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- Gauche avant -->
<gear x="0.831" y="2.125" z="-0.896"
retract-time="7"
compression="0.45"
spring="0.80"
damp="1.10">
<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="10"/>
</gear>
<!-- Droite avant -->
<gear x="0.831" y="-2.125" z="-0.896"
retract-time="7"
compression="0.45"
spring="0.80"
damp="1.10">
<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="10"/>
</gear>
<!-- Gauche arriere -->
<gear x="-0.702" y="2.125" z="-0.896"
retract-time="7"
compression="0.35"
spring="1.40"
damp="1.23">
<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[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="10"/>
</gear>
<!-- Droite arriere -->
<gear x="-0.702" y="-2.125" z="-0.896"
retract-time="7"
compression="0.35"
spring="1.40"
damp="1.23">
<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[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="10"/>
</gear>
<!-- Reservoirs de carburant -->
<!-- 1 et 4 - Reservoirs principaux d'extremites -->
<!-- adjusted tanks to get a balanced aircraft/approx position)-->
<tank x="-0.2" y="14.732" z="3.927" capacity="8710"/>
<tank x="-0.2" y="-14.732" z="3.927" capacity="8710"/>
<!-- 2 et 3 - Reservoirs principaux interieurs -->
<tank x="-0.4" y="7.041" z="3.796" capacity="7995"/>
<tank x="-0.4" y="-7.041" z="3.796" capacity="7995"/>
<!-- 5 et 6 - Reservoirs auxiliaires -->
<tank x="-0.4" y="2.451" z="3.770" capacity="5915"/>
<tank x="-0.4" y="-2.451" z="3.770" capacity="5915"/>
<!-- 7 et 8 - Reservoirs supplementaires sur pylones -->
<tank x="-0.133" y="7.701" z="2.179" capacity="5299"/>
<tank x="-0.133" y="-7.701" z="2.179" capacity="5299"/>
<!-- Ballast CG au centre de la corde des ailes x=1.486 -->
<ballast x="11" y="0" z="1" mass="8000"/>
<ballast x="-13.5" y="0" z="3.7" mass="-15000"/>
</airplane>