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DC-9-32.xml
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DC-9-32.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Douglas DC-9-32 for FlightGear YASim FDM
By Skyop
Specifications can be viewed on Wikipedia:
http://en.wikipedia.org/wiki/McDonnell_Douglas_DC-9#Series_30
More can be found on airliners.net:
http://www.airliners.net/aircraft-data/stats.main?id=276
-->
<airplane mass="67190">
<approach speed="140" aoa="5.0" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.5" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.5" />
<control-setting axis="/controls/flight/flaps" value="1.0" />
<control-setting axis="/controls/gear/gear-down" value="1.0" />
<solve-weight idx="0" weight="600" />
<solve-weight idx="1" weight="17700" />
</approach>
<cruise speed="438" alt="34200" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.8" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.8" />
<control-setting axis="/controls/flight/flaps" value="0.0" />
<control-setting axis="/controls/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="600" />
<solve-weight idx="1" weight="17700" />
</cruise>
<cockpit x="-2.8" y="0.52" z="1.5" />
<!-- FUSELAGE -->
<!-- Main fuselage -->
<fuselage ax="-5.087" ay="0.0" az="0.746" bx="-22.392" by="0.0" bz="0.746" width="3.32" taper="1.0" midpoint="1.0" />
<!-- Nose cone -->
<fuselage ax="0.0" ay="0.0" az="0.0" bx="-5.087" by="0.0" bz="0.746" width="3.32" taper="0.14" midpoint="1.0" />
<!-- Rear cone -->
<fuselage ax="-22.392" ay="0.0" az="0.746" bx="-32.867" by="0.0" bz="1.54" width="3.32" taper="0.22" midpoint="0.0" />
<!-- WINGS -->
<wing x="-16.808" y="1.623" z="-0.363" length="13.7" chord="5.108" sweep="20.75" taper="0.22" camber="0.01" dihedral="2.0" incidence="1.0" twist="-2.5" idrag="1.2">
<stall aoa="17" width="5" peak="1.8" />
<flap0 start="0.009" end="0.440" lift="1.15" drag="2.78" />
<flap1 start="0.584" end="0.848" lift="1.3" drag="1.9" />
<slat start="0.02" end="0.95" aoa="3.0" drag="1.1" />
<spoiler start="0.18" end="0.52" lift="0.0" drag="1.3" />
<control-input axis="/controls/flight/flaps" control="FLAP0" />
<control-input axis="/controls/flight/flaps" control="SLAT" src0="0.0" src1="0.111" dst0="0.0" dst1="1.0" />
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/spoilers" control="SPOILER" />
<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="SLAT" prop="/surface-positions/slats" />
<control-output control="SPOILER" prop="/surface-positions/spoilers-pos-norm" />
<control-speed control="FLAP0" transition-time="20.0" />
<control-speed control="SLAT" transition-time="15.0" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!-- ELEVATORS -->
<hstab x="-32.953" y="0.22" z="5.991" length="6.2" chord="3.222" twist="-1.0" taper="0.4" sweep="27.0" camber="0.00" dihedral="-2.5" idrag="1.0">
<stall aoa="20" width="7" peak="1.5" />
<flap0 start="0" end="0.93" 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" />
</hstab>
<!-- TAIL -->
<vstab x="-29.765" y="0.0" z="2.12" length="6.0" chord="5.0" taper="0.7" sweep="43.0">
<stall aoa="15" width="2" peak="1.5" />
<flap0 start="0.0" end="0.73" lift="1.3" 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" />
</vstab>
<!-- ENGINES -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="-23.08" ay="2.832" az="0.941" bx="-28.437" by="2.832" bz="0.754" width="1.5" taper="0.9" midpoint="0.0" />
<fuselage ax="-23.08" ay="-2.832" az="0.941" bx="-28.437" by="-2.832" bz="0.754" width="1.5" taper="0.9" midpoint="0.0" />
<!-- Actual engine definitions -->
<jet x="-25.156" y="2.832" z="0.842" mass="3200.0" thrust="15000.0" afterburner="0.0" rotate="0.0" n1-idle="33.0" n1-max="102.0" n2-idle="53.0" n2-max="103.0" tsfc="0.4" egt="1050.0" epr="3.0" exhaust-speed="1655.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/surface-positions/left-reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-28.437" y="2.832" z="0.754" />
</jet>
<jet x="-25.156" y="-2.832" z="0.842" mass="3200.0" thrust="15000.0" afterburner="0.0" rotate="0.0" n1-idle="33.0" n1-max="102.0" n2-idle="53.0" n2-max="103.0" tsfc="0.4" egt="1050.0" epr="3.0" exhaust-speed="1655.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/surface-positions/right-reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-28.437" y="-2.832" z="0.754" />
</jet>
<!-- LANDING GEARS -->
<!-- Pushback -->
<thruster x="-2.337" y="0.0" z="-2.304" vx="1" vy="0" vz="0" thrust="5000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-25" src1="25" dst0="-1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="-2.337" y="0.0" z="-2.304" compression="0.25" spring="0.7" damp="4.0">
<control-input axis="/controls/flight/rudder" control="STEER" square="true" />
<control-input axis="/controls/gear/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm" />
<control-output control="STEER" prop="/gear/gear[0]/steering-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<!-- Left main gear -->
<gear x="-18.129" y="2.545" z="-2.741" compression="0.6">
<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="10.0" />
</gear>
<!-- Right main gear -->
<gear x="-18.129" y="-2.545" z="-2.741" compression="0.6">
<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="10.0" />
</gear>
<!-- landing gear drag right -->
<vstab x="-18.129" y="2.545" z="-1.941"
taper="0"
incidence="0"
twist="0"
chord="0.404"
sweep="0"
camber="0.0"
dihedral="6"
length="1.93">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="-0.24"
drag="2.96"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[2]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<!-- landing gear drag left -->
<vstab x="-18.129" y="-2.545" z="-1.941"
taper="0"
incidence="0"
twist="0"
chord="0.404"
sweep="0"
camber="0.0"
dihedral="6"
length="1.93">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="-0.24"
drag="2.96"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[1]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<!-- Nose gear drag -->
<vstab x="-2.337" y="0.0" z="-1.504"
taper="0"
incidence="0"
twist="0"
chord="0.394"
sweep="0"
camber="0.0"
dihedral="6"
length="1.53">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="-0.44"
drag="2.86"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[0]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<!-- FUEL AND PAYLOAD -->
<!-- Total fuel capacity: 4,260 gallons -->
<!-- Left wing fuel tank -->
<tank x="-18.85" y="6.75" z="-0.2" jet="true" capacity="9542" />
<!-- Right wing fuel tank -->
<tank x="-18.85" y="-6.75" z="-0.2" jet="true" capacity="9542" />
<!-- Main fuel tank -->
<tank x="-16.95" y="0.0" z="0.15" jet="true" capacity="9542" />
<!-- Ballast to adjust center of gravity -->
<ballast x="-0.8" y="0.0" z="0.0" mass="11000.0" />
<!-- Crew -->
<weight x="-2.8" y="0.0" z="0.0" mass-prop="/sim/weight[0]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="600.0" />
<!-- PAX -->
<weight x="-14.0" y="0.0" z="0.0" mass-prop="/sim/weight[1]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="30525.0" />
</airplane>