rendered paste body<?xml version="1.0" encoding="utf-8"?>
<airplane mass="728"> <!-- 330 kg, verifier la conversion kg/lb -->
<!-- Approach configuration -->
<approach speed="40" aoa="16" fuel="0.6"> <!-- 1,3 VSO mais 90 km/h en réalité -->
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.9"/>
<solve-weight idx="0" weight="120"/>
<solve-weight idx="1" weight="150"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="83" alt="2000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.9"/>
<control-setting axis="/engines/engine[0]/rpm" value="2200"/>
<control-setting axis="/controls/flight/elevator-trim" value="0.3"/>
<solve-weight idx="0" weight="120"/>
<solve-weight idx="1" weight="150"/>
</cruise>
<cockpit x="1.23" y="-0.26" z="-0.43"/>
<!-- Fuselage -->
<fuselage ax="2.9" ay="0" az="0.2" bx="-2.4" by="0" bz="0.1"
width="1.15" taper="0.3" midpoint="0.25"/>
<!-- Aile en une seule partie, on oublie la "cassure" -->
<wing x="1.05" y="0.54" z="-0.23" taper="0.6" incidence="2.0" twist="-1.0"
length="3.60" chord="1.71" sweep="3.0" dihedral="5.0" camber="0.15">
<stall aoa="18" width="4.0" peak="1.5"/>
<flap0 start="0.55" end="1.0" lift="1.3" drag="1.2"/>
<control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
<control-output control="FLAP0" side="left"
prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP0" side="right"
prop="/surface-positions/right-aileron-pos-norm"/>
</wing>
<hstab x="-2.35" y="0.03" z="0.27" taper="1.0" effectiveness="1.0"
length="1.39" chord="0.96" sweep="0">
<stall aoa="16" width="3.0"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-2.2" y="0" z="-1.0" taper="0.6" effectiveness="1.5"
length="0.8" chord="0.8" sweep="10">
<stall aoa="15" width="3.0"/>
<flap0 start="0" end="1" lift="2.0" drag="1.2"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<!-- Continental C90 -->
<propeller radius="1.0"
cruise-speed="70" cruise-rpm="2200"
cruise-alt="8000" cruise-power="70"
takeoff-power="80" takeoff-rpm="2200"
x="2.6" y="0.0" z="0.2" mass="180" moment="4">
<piston-engine eng-rpm="2450" alt="0" eng-power="90"/>
<actionpt x="3.05" y="0.0" z="0.2" />
<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]/mixture" control="MIXTURE"/>
</propeller>
<!-- Train principal / Main gear -->
<gear x="1.78" y="1.0" z="-1.0" compression="0.1" sfric="0.8" dfric="0.8"
spring=".6" damp="1.2">
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
</gear>
<gear x="1.78" y="-1.0" z="-1.0" compression="0.1" sfric="0.8" dfric="0.8"
spring=".6" damp="1.2">
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
</gear>
<!-- Roulette de queue -->
<gear x="-2.64" y="0" z="-0.415" compression=".05" sfric="0.6" dfric="0.8"
spring=".5" damp="0.8">
<control-input axis="/controls/flight/rudder" control="STEER"
src0="-1.0" src1="1.0"
dst0="0.2" dst1="-0.2"/>
</gear>
<!-- Centre de gravité -->
<ballast x="2.2" y="0" z="-0.70" mass="200"/>
<!-- Carburant -->
<tank x="2.0" y="0.0" z="0.0" capacity="60" />
<tank x="0.3" y="0" z="0" capacity="55" />
<!-- Pilote, copilote, 5kg de bagages -->
<weight x="1.3" y=".3" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="1.3" y="-.3" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="0.8" y="0" z="0" mass-prop="/sim/weight[2]/weight-lb"/>
</airplane>