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KC-10M.xml
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KC-10M.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!-- MD-10 FDM, parts from Ryan Miller's DC-10, and Jormmapaappa1235, tikibar, and it0uchpods' MD-11 -->
<airplane version="YASIM_VERSION_32" mass="283975">
<!-- 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="134" 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="95000.0" />
</approach>
<!-- Cruise configuration -->
<cruise speed="485" alt="35000" fuel="0.8" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.85" />
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.85" />
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.85" />
<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="95000.0" />
</cruise>
<!-- <cockpit x="16.0" y="0.75" z="-0.8" />-->
<!-- Fuselage -->
<fuselage ax="17.74" ay="0.0" az="5.18" bx="-11.013" 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="-11.013" ay="0.0" az="5.133" bx="-32.48" by="0.0" bz="6.101" width="6.0" taper="0.22" midpoint="0.0" />
<wing x="-1.08" y="3.0" z="4.235" length="28.06" chord="12.0" sweep="35.0" taper="0.31" camber="0.05" dihedral="6.4" incidence="3.6" twist="-2.9" idrag="1.15">
<stall aoa="8.0" width="5" peak="0.8" />
<flap0 start="0.0" end="0.52" lift="1.2" drag="1.5" />
<flap1 start="0.53" end="0.825" lift="1.2" drag="1.6" />
<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-speed control="FLAP0" transition-time="78"/>
<!--control-input axis="/surface-positions/flap-pos-norm" control="SLAT" src0="0" dst0="0" src1="0.1428" dst1="1.0"/-->
<control-input axis="/controls/flight/slats" control="SLAT"/>
<control-output control="SLAT" prop="/surface-positions/slats"/>
<control-speed control="SLAT" transition-time="9"/>
<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-pos" 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-output control="FLAP0" prop="/surface-positions/flap-inner-pos-norm" />
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-inner-pos-norm" />
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-inner-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-inner-pos-norm" />
<control-output control="FLAP0" prop="/surface-positions/flap-outer-pos-norm" />
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-outer-pos-norm" />
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-outer-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-outer-pos-norm" />
</wing>
<!-- Horizontal stabilizers -->
<hstab x="-19.448" y="0.91" z="5.632" length="13.5" 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="1.7" drag="1.3" />
<control-input axis="/controls/flight/elevator-pos" control="FLAP0" src0="-1.0" dst0="-0.7" src1="1.0" dst1="0.7"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0" />
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm" />
</hstab>
<!-- Vertical stabilizers -->
<vstab x="-25.7" y="0.0" z="7.68" length="12.0" chord="8.0" taper="0.4"
sweep="35.0" idrag="1.5">
<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/rudder-pos" 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="1.5" />
</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="-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" />
<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" />
<!-- Actual engines -->
<jet x="3.541" y="8.138" z="3.541" mass="9047.0" thrust="52500.0" afterburner="0" rotate="0.0" n1-idle="23.4" n1-max="110.0" n2-idle="64.7" n2-max="108.0" tsfc="0.332" 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="-30.564" y="0.0" z="10.5002" mass="9047.0" thrust="52500.0" afterburner="0" rotate="0.0" n1-idle="23.4" n1-max="110.0" n2-idle="64.7" n2-max="108.0" tsfc="0.332" 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="3.541" y="-8.138" z="3.541" mass="9047.0" thrust="52500.0" afterburner="0" rotate="0.0" n1-idle="23.4" n1-max="110.0" n2-idle="64.7" n2-max="108.0" tsfc="0.332" 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>
<!-- Pushback -->
<thruster x="20.6395" y="0.00" z="0.7" vx="1" vy="0" vz="0" thrust="12000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- Nosegear -->
<gear x="18.8" y="0.0" z="-0.451" compression="0.4" spring="0.8" damp="4.0" sfric="1.2" dfric="1.0">
<!-- 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="gear/gear[0]/steering-norm" />
<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="8"/>
</gear>
<!-- Left main gears -->
<gear x="-2.65" y="5.25" z="-0.615" 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="12" />
</gear>
<!-- Right main gears -->
<gear x="-2.65" y="-5.25" z="-0.615" 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[2]/position-norm" />
<control-speed control="EXTEND" transition-time="12" />
</gear>
<!-- Fuel and payload -->
<!-- Left wing tanks-->
<tank x="3.0" y="7.5" z="3.5" jet="true" capacity="40602" />
<!-- Center tank -->
<tank x="1.08" y="0.0" z="3.0503" jet="true" capacity="64038" />
<!-- Right wing tanks -->
<tank x="3.0" y="-7.5" z="3.5" jet="true" capacity="40602" />
<tank x="-1.08" y="0.0" z="3.0503" jet="true" capacity="98108" />
<tank x="-27.341" y="0" z="14.7597" jet="true" capacity="13400" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="16.0" y="0.0" z="2.3" mass="50000.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-2.8" y="0.0" z="2.3" mass="150000.0" />
<!-- Payload information from http://www.acp-logistics.com/DC-10-charter-mcdonnell-douglas.html -->
<!-- Crew -->
<weight x="25.0" y="0.0" z="4.0" mass-prop="/sim/weight[0]/weight-lb" />
<!-- PAX/Cargo -->
<weight x="-2.75" y="0.0" z="3.2" mass-prop="/sim/weight[1]/weight-lb" />
</airplane>