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sr22-yasim.xml
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sr22-yasim.xml
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<?xml version="1.0" encoding="ISO-8859-1"?>
<!-- Cirrus SR22 - 2013 Emmanuel BARANGER
sources : http://en.wikipedia.org/wiki/Cirrus_SR22
wingspan : 11.68 m ( 38 ft 4 in )
length : 7.92 m ( 26 ft 0 in )
height : 2.72 m ( 8 ft 11 in )
empty weight : 1009 kg ( 2225 lb )
fuel capacity : 92 US gallons ( 348 litres )
engine : Continental IO-550-N Six cylinder horizontally opposed aircraft engine ( 310 hp )
Cruise speed : 343 km/h ( 185 kt )
-->
<airplane mass="2225" version="YASIM_VERSION_CURRENT">
<!-- Approach configuration -->
<approach speed="40" aoa="4" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="185" alt="6000" fuel="0.5">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.6"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
</cruise>
<cockpit x="1.176" y="0.300" z="0.440"/>
<fuselage ax="3.51758" ay="0" az="-0.11527" bx="-3.66646" by="0" bz="-0.12118" width="1.260" taper="0.3" midpoint="0.3"/>
<wing x="0.80762" y="0.339" z="-0.540"
chord="1.574"
length="5.461"
taper="0.50"
sweep="-2.7"
dihedral="4"
camber="0.01">
<stall aoa="18" width="1" peak="1.5"/>
<flap0 start="0.00" end="0.60" lift="1.2" drag="1.25"/>
<flap1 start="0.60" end="1.00" lift="1.2" drag="1.10"/>
<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-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
<control-speed control="FLAP0" transition-time="4"/>
</wing>
<hstab x="-3.02711" y="0" z="-0.10167"
chord="1.106"
length="1.965"
taper="0.7"
sweep="1">
<stall aoa="14" width="1" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1"/>
<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="-2.95241" y="0" z="-0.149"
chord="1.441"
length="1.650"
taper="0.4"
sweep="26">
<stall aoa="14" width="1" peak="1.5"/>
<flap0 start="0" end="1" lift="1.75" drag="1.35"/>
<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>
<!-- Engines source : http://en.wikipedia.org/wiki/Continental_IO-550
name : Continental IO-550
type : 6-cylinder air-cooled horizontally opposed aircraft piston engine
power cruise : 300 hp at 2700 rpm
weight : 430.72 lb ( 195.37 kg )
displacement : 552 in3 ( 9.05 L )
compression : 8.5:1
-->
<propeller x="3.17434" y="0" z="-0.12602"
radius="1"
mass="430.72"
moment="6"
cruise-speed="185"
cruise-rpm="2575"
cruise-alt="6000"
cruise-power="280"
takeoff-power="310"
takeoff-rpm="2600">
<actionpt x="3.59129" y="0" z="-0.12602"/>
<piston-engine eng-rpm="2700"
eng-power="310"
displacement="552"
compression="8.5">
<control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle" src0="0" src1="1" dst0="0" dst1="1"/>
<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" src0="0" src1="1" dst0="0.8" dst1="0.8"/>
</piston-engine>
</propeller>
<!-- Castering nose wheel -->
<gear x="3.093" y="0" z="-1.399"
compression="0.15"
spring="0.8"
on-solid="1"
castering="1"
sfric="1"
dfric="1">
<control-input axis="/controls/gear/tailwheel-lock" control="CASTERING"
src0="0" src1="1"
dst0="1" dst1="0"/>
</gear>
<!-- Left wheel -->
<gear x="0.92380" y="1.81669" z="-1.35894"
compression="0.2"
spring="1.8"
damp="0.03"
on-solid="1" >
<control-input control="BRAKE" axis="/controls/gear/brake-left"/>
<control-input control="BRAKE" axis="/controls/gear/brake-parking"/>
</gear>
<!-- Right wheel -->
<gear x="0.92380" y="-1.81669" z="-1.35894"
compression="0.2"
spring="1.8"
damp="0.03"
on-solid="1" >
<control-input control="BRAKE" axis="/controls/gear/brake-right"/>
<control-input control="BRAKE" axis="/controls/gear/brake-parking"/>
</gear>
<!-- Tail contact point -->
<gear x="-3.18197" y="0" z="-0.45408"
compression="0.01">
</gear>
<tank x="1.03" y=" 1.8" z="-0.42" capacity="200"/>
<tank x="0.46" y=" 0.0" z="-0.31" capacity="300"/>
<tank x="1.03" y="-1.8" z="-0.42" capacity="200"/>
<!-- Mass distribution -->
<ballast x="3" y="0" z="-1" mass="350"/>
</airplane>