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MD-11.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<airplane mass="286965">
<!-- Approach configuration based on stall chart http://tinypic.com/hsqd1l.jpg (from airliners.net thread http://www.airliners.net/aviation-forums/tech_ops/read.main/135496/) -->
<approach speed="132" aoa="4.0" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.6" />
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.6" />
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.6" />
<control-setting axis="/controls/flight/flaps" value="1.0" />
<control-setting axis="/controls/flight/slats" value="1.0" />
<control-setting axis="/controls/gear/gear-down" value="1.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="142700.0" />
</approach>
<!-- Cruise configuration -->
<cruise speed="530" alt="37000" fuel="0.8" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.95" />
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.95" />
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.95" />
<control-setting axis="/controls/flight/flaps" value="0.0" />
<control-setting axis="/controls/flight/slats" value="0.0" />
<control-setting axis="/controls/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="142700.0" />
</cruise>
<!-- <cockpit x="16.0" y="0.75" z="-0.8" />-->
<!-- Fuselage -->
<fuselage ax="17.74" ay="0.0" az="5.18" bx="-10.12" by="0.0" bz="5.133" width="6.0" taper="1.0" midpoint="1.0" />
<fuselage ax="27.67" ay="0.0" az="4.843" bx="17.74" by="0.0" bz="5.18" width="6.0" taper="0.14" midpoint="1.0" />
<fuselage ax="-10.12" ay="0.0" az="5.133" bx="-24.587" by="0.0" bz="6.101" width="6.0" taper="0.22" midpoint="0.0" />
<wing x="-3.114" y="9.219" z="4.235" length="18.8" chord="7.81" sweep="32.0" taper="0.3" camber="0.01" dihedral="6.4" incidence="3.0" twist="-2.9" idrag="2.0">
<stall aoa="8.0" width="5" peak="0.8" />
<flap0 start="0.0" end="0.52" lift="1.5" drag="2.0" />
<flap1 start="0.53" end="0.825" lift="1.1" drag="1.3" />
<slat start="0.0" end="0.85" aoa="3.0" drag="1.1" />
<spoiler start="0.03" end="0.45" lift="0.5" drag="1.6" />
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT" src0="0" dst0="0" src1="0.1428" dst1="1.0"/>
<control-output control="SLAT" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="78"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="SPOILER" transition-time="2"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<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="FLAP1" transition-time="3.0" />
</wing>
<!-- Horizontal stabilizers -->
<hstab x="-19.448" y="0.91" z="5.632" length="11.5" chord="8.0" sweep="30.0" taper="0.4"
dihedral="10.6" camber="-0.1" twist="-1.0" idrag="1.1">
<stall aoa="15.0" width="7" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.5" drag="1.3" />
<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" />
<control-speed control="FLAP0" transition-time="2.5" />
</hstab>
<!-- Vertical stabilizers -->
<vstab x="-17.8" y="0.0" z="7.68" length="12.0" chord="8.0" taper="0.4"
sweep="35.0" idrag="1.5">
<stall aoa="15" width="2" peak="1.5" />
<flap0 start="0.37" end="1.0" lift="1.4" drag="1.3" />
<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"/>
<control-speed control="FLAP0" transition-time="3.0" />
</vstab>
<!-- Engines -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="7.142" ay="8.138" az="2.536" bx="2.461" by="8.138" bz="2.536" width="2.742" taper="0.94" midpoint="0.0" />
<fuselage ax="7.142" ay="-8.138" az="2.536" bx="2.461" by="-8.138" bz="2.536" width="2.742" taper="0.94" midpoint="0.0" />
<fuselage ax="-14.534" ay="0.0" az="9.654" bx="-24.871" by="0.0" bz="9.293" width="2.84" taper="0.94" midpoint="0.0" />
<!-- Actual engines -->
<jet x="-2.125" y="8.138" z="3.541" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[0]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="2.461" y="8.138" z="2.536" />
</jet>
<jet x="28.0873" y="0.0" z="10.5002" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[1]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-24.871" y="0.0" z="9.293" />
</jet>
<jet x="-2.125" y="-8.138" z="3.541" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[2]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[2]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[2]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="2.461" y="-8.138" z="2.536" />
</jet>
<!-- Nosegear -->
<gear x="20.6395" y="0.0" z="0.7" compression="0.4" spring="0.8" damp="4.0">
<!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<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="15"/>
</gear>
<!-- Left main gears -->
<gear x="-3.1584" y="-5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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="19" />
</gear>
<gear x="-4.7637" y="-5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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[2]/position-norm" />
<control-speed control="EXTEND" transition-time="19" />
</gear>
<!-- Right main gears -->
<gear x="-3.1584" y="5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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[3]/position-norm" />
<control-speed control="EXTEND" transition-time="19" />
</gear>
<gear x="-4.7637" y="5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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="19" />
</gear>
<!-- Center gear -->
<gear x="-4.7637" y="0" z="0.5586" compression="0.7" spring="0.6" damp="1.0">
<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[5]/position-norm" />
<control-speed control="EXTEND" transition-time="15" />
</gear>
<!-- Fuel and payload -->
<!-- Left wing tanks-->
<tank x="0.8531" y="7.5" z="5.4676" jet="true" capacity="40602" />
<!-- Center tank -->
<tank x="0.7674" y="0.0" z="3.9503" jet="true" capacity="64038" />
<!-- Right wing tanks -->
<tank x="-3.1" y="-7.5" z="4.0" jet="true" capacity="40602" />
<tank x="0.7674" y="0.0" z="3.9503" jet="true" capacity="98108" />
<tank x="-25.4726" y="0" z="14.7597" jet="true" capacity="13400" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="25.0" y="0.0" z="4.0" mass="30000.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-2.0" y="0.0" z="3.0" mass="10000.0" />
<!-- Payload information from http://www.acp-logistics.com/DC-10-charter-mcdonnell-douglas.html -->
<!-- Crew -->
<weight x="25.0" y="0.0" z="5.0" mass-prop="/sim/weight[0]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="600.0" />
<!-- PAX/Cargo -->
<weight x="3.0" y="0.0" z="5.0" mass-prop="/sim/weight[1]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="142700.0" />
</airplane>