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C-32J-20.xml
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C-32J-20.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Boeing C-32J (757-200 VIP transport) with Pratt & Whitney
PW2040 engines for FlightGear YASim FDM
By J Maverick 16, Joshua Davidson, Jonathan Redpath (legoboyvdlp). Original work: tikibar.
Original specifications can be viewed on Boeing's website:
http://www.boeing.com/commercial/757family/pf/pf_200tech.html
http://www.boeing.com/commercial/airports/757.htm
http://www.aviamarket.org/reviews/civil-aircraft/1095-boeing-757-200.html
-->
<airplane version="YASIM_VERSION_32" mass="130875">
<approach speed="145" aoa="6" fuel="0.17">
<control-setting axis="/controls/engines/engine[0]/throttle-fdm" value="0.5" />
<control-setting axis="/controls/engines/engine[1]/throttle-fdm" 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="450" />
<solve-weight idx="1" weight="47931" />
</approach>
<cruise speed="503" alt="35000" fuel="0.69">
<control-setting axis="/controls/engines/engine[0]/throttle-fdm" value="0.85" />
<control-setting axis="/controls/engines/engine[1]/throttle-fdm" value="0.85" />
<control-setting axis="/controls/flight/flaps" value="0.0" />
<control-setting axis="/controls/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="450" />
<solve-weight idx="1" weight="47931" />
</cruise>
<cockpit x="-2.25" y="0.0" z="1.4" />
<!-- FUSELAGE -->
<!-- Main fuselage -->
<fuselage ax="-5.656" ay="0.0" az="0.991" bx="-36.338" by="0.0" bz="0.991" cx="1.066" cy="1.066" cz="1.0" width="3.760" taper="1.0" midpoint="1.0" />
<!-- Nose cone -->
<fuselage ax="0.112" ay="0.0" az="0.0" bx="-5.656" by="0.0" bz="0.991" cx="1.066" cy="1.066" cz="1.0" width="3.760" taper="0.2" midpoint="1.0" />
<!-- Rear cone -->
<fuselage ax="-36.338" ay="0.0" az="0.991" bx="-46.923" by="0.0" bz="1.656" cx="1.066" cy="1.066" cz="1.0" width="3.760" taper="0.25" midpoint="0.0" />
<!-- WINGS -->
<wing x="-22.009" y="1.880" z="0.076" length="18.122" chord="8.333" sweep="18.9" taper="0.227" dihedral="10.5" camber="0.1" incidence="2.0" twist="-3.0" idrag="1.18">
<stall aoa="12.0" width="3" peak="1.5" />
<flap0 start="0.01" end="0.72" lift="1.4" drag="1.8" />
<flap1 start="0.745" end="0.985" lift="1.55" drag="1.3" />
<slat start="0.02" end="0.985" aoa="3.0" drag="1.4" />
<spoiler start="0.11" end="0.7" lift="0.5" drag="1.8" />
<control-input axis="/controls/flight/flaps" control="FLAP0" />
<control-input axis="/controls/flight/flaps" control="SLAT" src0="0.0" src1="0.177" dst0="0.0" dst1="1.0" />
<control-input axis="/controls/flight/aileron-pos" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/fdm-speedbrake" 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/fdm-speedbrake-pos-norm" />
<control-speed control="FLAP0" transition-time="64.0" />
<control-speed control="SLAT" transition-time="15.0" />
<control-speed control="SPOILER" transition-time="1.5" />
</wing>
<!-- ELEVATORS -->
<hstab x="-42.085" y="1.88" z="1.723" length="6.531" chord="4.242" twist="0.0" taper="0.411" sweep="28.8" camber="0.1">
<stall aoa="20" width="7" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.7" drag="1.5" />
<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>
<!-- TAIL -->
<vstab x="-41.19" y="0.00" z="2.996" chord="6.56" length="8.84" taper="0.475" sweep="35.0" effectiveness="1.5">
<stall aoa="15" width="2" peak="1.3" />
<flap0 start="0.0" end="1.0" lift="1.4" 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" />
</vstab>
<!-- ENGINES -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="-16.498" ay="6.48" az="-0.985" bx="-19.059" by="6.48" bz="-0.97" cx="0.2" width="2.69" taper="0.9" midpoint="1.0" />
<fuselage ax="-19.059" ay="6.48" az="-0.97" bx="-21.522" by="6.48" bz="-0.801" cx="0.2" width="2.69" taper="0.65" midpoint="0.0" />
<fuselage ax="-16.498" ay="-6.48" az="-0.985" bx="-19.059" by="-6.48" bz="-0.97" cx="0.2" width="2.69" taper="0.9" midpoint="1.0" />
<fuselage ax="-19.059" ay="-6.48" az="-0.97" bx="-21.522" by="-6.48" bz="-0.801" cx="0.2" width="2.69" taper="0.65" midpoint="0.0" />
<!-- Actual engine definitions -->
<jet x="-18.391" y="6.48" z="-0.801" mass="7100.0" thrust="43734.0" afterburner="0.0" rotate="0.0" n1-idle="23.1" n1-max="109.4" n2-idle="69.2" n2-max="104.2" tsfc="0.358" egt="810.0" exhaust-speed="1255.0" spool-time="3.0" epr="2.00">
<control-input axis="/controls/engines/engine[0]/throttle-fdm" 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="-22.038" y="6.48" z="-0.801" />
</jet>
<jet x="-18.391" y="-6.48" z="-0.801" mass="7100.0" thrust="43734.0" afterburner="0.0" rotate="0.0" n1-idle="23.1" n1-max="109.4" n2-idle="69.2" n2-max="104.2" tsfc="0.358" egt="810.0" exhaust-speed="1255.0" spool-time="3.0" epr="2.00">
<control-input axis="/controls/engines/engine[1]/throttle-fdm" 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="-22.038" y="-6.48" z="-0.801" />
</jet>
<!-- LANDING GEARS -->
<!-- Pushback -->
<thruster x="-5.778" y="0.0" z="-3.3" vx="1" vy="0" vz="0" thrust="42000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="-5.778" y="0.0" z="-3.37" compression="0.25" spring="0.7" damp="4.0" sfric="0.99">
<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="8.0" />
</gear>
<!-- Left main gear forward -->
<gear x="-23.484" y="3.768" z="-3.37" compression="0.6">
<control-input axis="/autopilot/autobrake/left-brake-output" 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="8.0" />
</gear>
<!-- Left main gear aft -->
<gear x="-24.653" y="3.768" z="-3.37" compression="0.6">
<control-input axis="/autopilot/autobrake/left-brake-output" 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="8.0" />
</gear>
<!-- Right main gear forward -->
<gear x="-23.484" y="-3.768" z="-3.37" compression="0.6">
<control-input axis="/autopilot/autobrake/right-brake-output" 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="8.0" />
</gear>
<!-- Right main gear aft -->
<gear x="-24.653" y="-3.768" z="-3.37" compression="0.6">
<control-input axis="/autopilot/autobrake/right-brake-output" 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="8.0" />
</gear>
<!-- FUEL AND PAYLOAD -->
<!-- Total fuel capacity: 101,480 pounds (This is an extended range plane) -->
<!-- Left wing fuel tank -->
<tank x="-24.3" y="8.25" z="0.8" jet="true" capacity="15880" />
<!-- Right wing fuel tank -->
<tank x="-24.3" y="-8.25" z="0.8" jet="true" capacity="15880" />
<!-- Center fuel tank -->
<tank x="-22.0" y="0.0" z="-0.75" jet="true" capacity="52700" />
<!-- Aux fuel tanks -->
<!-- Step up to 8510, was 8310 -->
<tank x="-20.0" y="0.0" z="-0.75" jet="true" capacity="8510" />
<tank x="-24.0" y="0.0" z="-0.75" jet="true" capacity="8510" />
<!-- Crew -->
<weight x="-2.5" y="0.0" z="1.0" mass-prop="/sim/weight[0]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="600.0" />
<!-- PAX/Cargo -->
<weight x="-21.741" y="0.0" z="1.0" mass-prop="/sim/weight[1]/weight-lb" />
<!-- Ballast to adjust center of gravity -->
<ballast x="-11.0" y="0.0" z="1.0" mass="40000" />
<ballast x="-10.0" y="0.0" z="1.0" mass="700" />
</airplane>