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717-200HGW.xml
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717-200HGW.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Boeing 717-200 [Basic Gross Weight] for FlightGear YASim FDM
By Skyop
Specifications can be viewed on Boeing's website:
http://www.boeing.com/commercial/717/pf/pf_product.html
More can be found on airliners.net:
http://www.airliners.net/aircraft-data/stats.main?id=111
-->
<airplane mass="69830">
<approach speed="120" aoa="5.0" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.6" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.6" />
<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="16.0" y="0.75" z="-0.8" />
<!-- FUSELAGE -->
<!-- Main fuselage -->
<fuselage ax="14.337" ay="0.0" az="-1.554" bx="-6.1" by="0.0" bz="-1.554" width="3.32" taper="1.0" midpoint="1.0" />
<!-- Nose cone -->
<fuselage ax="18.886" ay="0.0" az="-2.3" bx="14.337" by="0.0" bz="-1.554" width="3.32" taper="0.14" midpoint="1.0" />
<!-- Rear cone -->
<fuselage ax="-6.1" ay="0.0" az="-1.554" bx="-15.448" by="0.0" bz="-0.943" width="3.32" taper="0.22" midpoint="0.0" />
<!-- WINGS -->
<wing x="0.609" y="1.45" z="-2.432" length="13.7" chord="4.978" sweep="20.75" taper="0.22" camber="0.09" incidence="3.0" twist="-1.0" idrag="1.0">
<stall aoa="15" width="5" peak="0.8" />
<flap0 start="0.0195" end="0.584" lift="1.5" drag="2.0" />
<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/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/speedbrake-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="-15.729" y="0.22" z="3.694" length="6.5" chord="3.602" twist="-1.0" taper="0.4" sweep="25.0" idrag="1.0" camber="0.09">
<stall aoa="20" width="7" peak="1.5" />
<flap0 start="0" end="0.93" lift="1.4" 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="-12.165" y="0.0" z="-0.26" length="6.0" chord="5.0" taper="0.65" sweep="40.0">
<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="-4.753" ay="2.915" az="-1.074" bx="-10.746" by="2.915" bz="-1.242" width="2.1" taper="0.55" midpoint="0.0" />
<fuselage ax="-4.753" ay="-2.915" az="-1.074" bx="-10.746" by="-2.915" bz="-1.242" width="2.1" taper="0.55" midpoint="0.0" />
<!-- Actual engine definitions -->
<jet x="-7.342" y="2.915" z="-1.257" mass="4912.0" thrust="21000.0" 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="1555.0" 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="/engines/engine[0]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-10.746" y="2.915" z="-1.242" />
</jet>
<jet x="-7.342" y="-2.915" z="-1.257" mass="4912.0" thrust="21000.0" 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="1555.0" 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="/engines/engine[1]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-10.746" y="-2.915" z="-1.242" />
</jet>
<!-- LANDING GEARS -->
<!-- Pushback -->
<thruster x="16.67" y="0.0" z="-4.245" vx="1" vy="0" vz="0" thrust="9000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="16.67" y="0.0" z="-4.245" 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="-0.99" y="2.125" z="-4.412" 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="10.0" />
</gear>
<!-- Right main gear -->
<gear x="-0.99" y="-2.125" z="-4.412" 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[2]/position-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<!-- FUEL AND PAYLOAD -->
<!-- Total fuel capacity: 3,670 gallons (27,280 pounds) -->
<!-- Left wing fuel tank -->
<tank x="-1.05" y="6.75" z="-2.2" jet="true" capacity="9093" />
<!-- Right wing fuel tank -->
<tank x="-1.05" y="-6.75" z="-2.2" jet="true" capacity="9094" />
<!-- Main fuel tank -->
<tank x="0.85" y="0.0" z="-2.15" jet="true" capacity="9093" />
<!-- Ballast to adjust center of gravity -->
<ballast x="16.0" y="0.0" z="-2.0" mass="10000.0" />
<!-- Crew -->
<weight x="16.0" 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 -->
<weight x="1.0" y="0.0" z="1.0" mass-prop="/sim/weight[1]/weight-lb" size="0.0" solve-weight="0.0" idx="0" weight="17700.0" />
</airplane>