/
p130ul.xml
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/
p130ul.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!-- Pottier P130 UL
3d model by hydroz.net; ported by legoboyvdlp; FDM by D-ECHO, based on p92 by Emmanuel Baranger
-->
<airplane mass="573" version="YASIM_VERSION_CURRENT">
<!-- Approach configuration -->
<approach speed="40" aoa="7" fuel="0.2"><!--guessed!!-->
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.0"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/sim/weight[0]/weight-lb" value ="180"/>
<control-setting axis="/sim/weight[1]/weight-lb" value ="0"/>
<control-setting axis="/sim/weight[2]/weight-lb" value ="0"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="98" alt="6000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/sim/weight[0]/weight-lb" value ="180"/>
<control-setting axis="/sim/weight[1]/weight-lb" value ="0"/>
<control-setting axis="/sim/weight[2]/weight-lb" value ="0"/>
</cruise>
<cockpit x="-0.6682" y="-0.2722" z="-0.104"/>
<!--fuselage-->
<fuselage ax="1.0867" ay="0" az="-0.4831" bx="-3.9308" by="0" bz="-0.1314" width="0.68" taper="0.50" midpoint="1"/>
<wing x="-1.0" y="0.5012" z="0.0066"
chord="1.2"
length="3.5"
sweep="-20"
taper="1"
camber="0.05">
<stall aoa="19" width="5.0" peak="1.5"/>
<flap0 start="0.053" end="0.485" lift="1.3" drag="1.7"/>
<flap1 start="0.485" end="0.920" lift="1.3" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true" src0="-1.0" src1="1.0" dst0="-0.2" dst1="0.2"/>
<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="2"/>
</wing>
<hstab x="-4.59335" y="0" z="0.6555"
chord="0.8"
length="1.3"
taper="1" >
<stall aoa="25" width="2" peak="1.5"/>
<flap0 start="0" end="1.00" lift="2" drag="1.7"/>
<flap1 start="0" end="0.66" lift="1.5" drag="1.3"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP1"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/elevator-trim-norm"/>
</hstab>
<vstab x="-4.0678" y="0" z="-0.1518"
chord="1.120"
length="1.400"
taper="0.5"
sweep="27">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="2.75" drag="0.6"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true" square="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>
<!-- Engines name : 1600 cc Volkswagen
-->
<propeller x="0.8374" y="0.0" z="-0.457"
radius="0.75"
mass="132.3"
moment="0.60"
cruise-speed="95"
cruise-rpm="2263"
cruise-alt="6000"
cruise-power="60"
takeoff-power="65"
takeoff-rpm="2387"
gear-ratio="0.412" >
<actionpt x="1.1601" y="0.0" z="-0.455"/>
<piston-engine eng-rpm="5800"
eng-power="65"
displacement="105.0"
compression="9"/>
<control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle" />
<control-input control="STARTER" axis="/controls/engines/engine[0]/starter" />
<control-input control="MAGNETOS" axis="/controls/engines/engine[0]/magnetos" />
<control-input control="MIXTURE" axis="/controls/engines/engine[0]/mixture" />
</propeller>
<!--If tricycle configuration-->
<!-- Noze wheel -->
<gear x="0.8442" y="0" z="-1.4962"
compression="0.07"
spring="3.2"
damp="0.2"
on-solid="1"
sfric="1"
dfric="1">
<control-input axis="/controls/gear/tricycle" control="EXTEND"/>
<control-input axis="/controls/flight/rudder" control="STEER" src0="-1.0" src1="1.0" dst0="-0.1" dst1="0.1"/>
</gear>
<!-- Left wheel -->
<gear x="-0.7977" y="1.2551" z="-1.5404"
compression="0.2"
spring="3.8"
damp="0.2"
on-solid="1" >
<control-input axis="/controls/gear/tricycle" control="EXTEND"/>
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true" src0="0.0" src1="1.0" dst0="0.0" dst1="0.4"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- Right wheel -->
<gear x="-0.7977" y="-1.2551" z="-1.5404"
compression="0.2"
spring="3.2"
damp="0.2"
on-solid="1" >
<control-input axis="/controls/gear/tricycle" control="EXTEND"/>
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true" src0="0.0" src1="1.0" dst0="0.0" dst1="0.4"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!--If taildragger configuration-->
<!-- Left wheel -->
<gear x="-0.1491" y="1.1824" z="-1.5969"
compression="0.2"
spring="3.8"
damp="0.2"
on-solid="1" >
<control-input axis="/controls/gear/taildragger" control="EXTEND"/>
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true" src0="0.0" src1="1.0" dst0="0.0" dst1="0.4"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- Right wheel -->
<gear x="-0.1491" y="-1.1824" z="-1.5969"
compression="0.2"
spring="3.2"
damp="0.2"
on-solid="1" >
<control-input axis="/controls/gear/taildragger" control="EXTEND"/>
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true" src0="0.0" src1="1.0" dst0="0.0" dst1="0.4"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
</gear>
<!-- Tail wheel -->
<gear x="-4.0541" y="0" z="-0.4596"
compression="0.07"
spring="3.2"
damp="0.2"
on-solid="1"
sfric="1"
dfric="1">
<control-input axis="/controls/gear/taildragger" control="EXTEND"/>
<control-input axis="/controls/flight/rudder" control="STEER" src0="-1.0" src1="1.0" dst0="-0.1" dst1="0.1"/>
</gear>
<tank x="1.460" y="-0.7" z="0.490" capacity="77"/>
<tank x="1.460" y="0.7" z="0.490" capacity="77"/>
<!-- pilot -->
<weight x="-0.6682" y="0.2722" z="-0.104" mass-prop="/sim/weight[0]/weight-lb"/>
<!-- copilot -->
<weight x="-0.6682" y="-0.2722" z="-0.104" mass-prop="/sim/weight[1]/weight-lb"/>
<!-- baggage -->
<weight x="-0.9745" y="0" z="-0.2535" mass-prop="/sim/weight[2]/weight-lb"/>
<!-- Mass distribution -->
<ballast x="0" y="0" z="0.0" mass="150"/>
</airplane>