127 lines
5.7 KiB
XML
127 lines
5.7 KiB
XML
<airplane mass="400000">
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<!-- Approach configuration -->
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<approach speed="136" aoa="7">
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<control-setting axis="/controls/throttle[0]" value="0.2"/>
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<control-setting axis="/controls/throttle[1]" value="0.2"/>
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<control-setting axis="/controls/flaps" value="1.0"/>
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<control-setting axis="/controls/slats" value="1.0"/>
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<control-setting axis="/controls/gear-down" value="1"/>
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</approach>
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<!-- Cruise configuration -->
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<cruise speed="490" alt="36000">
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<control-setting axis="/controls/throttle[0]" value="0.75"/>
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<control-setting axis="/controls/throttle[1]" value="0.75"/>
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<control-setting axis="/controls/flaps" value="0.0"/>
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<control-setting axis="/controls/gear-down" value="0"/>
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</cruise>
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<cockpit x="-5.42" y="1.81" z="15.06"/>
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<fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41"
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width="6" taper="0.3" midpoint="0.2"/>
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<wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
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taper=".27" dihedral="7" camber="0.15" incidence="-0.7">
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<stall aoa="15" width="2" peak="1.5"/>
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<flap0 start="0" end=".56" lift="1.8" drag="3"/>
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<flap1 start=".64" end=".88" lift="1.3" drag="1.5"/>
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<slat start="0" end="1" aoa="2" drag="1.1"/>
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<spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/>
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<control-input axis="/controls/flaps" control="FLAP0"/>
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<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
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<control-input axis="/controls/slats" control="SLAT"/>
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<control-input axis="/controls/spoilers" control="SPOILER"/>
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<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
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<control-output control="FLAP1" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP1" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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<control-speed control="FLAP0" transition-time="10"/>
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</wing>
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<hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
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sweep="28" dihedral="7" camber="-0.1" effectiveness="1.5">
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<stall aoa="15" width="2" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.6" drag="1.8"/>
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<control-input axis="/controls/elevator" control="FLAP0"/>
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<control-input axis="/controls/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
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</hstab>
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<vstab x="-62.63" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3"
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sweep="33">
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<stall aoa="15" width="2" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.2" drag="1.3"/>
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<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
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<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
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min="1" max="-1"/>
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</vstab>
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<!-- The CF6 engines are rated at 60000 lbs thrust, flat rated to 33 -->
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<!-- degrees C. Corrected to YASim's standard atmosphere temperature -->
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<!-- of 288.2 kelvins, that gives 63737 lbs of nominal thrust. -->
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<jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="63737">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="63737">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="63737">
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<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
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</jet>
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<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="63737">
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<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
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</jet>
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<gear x="-5.42" y="0.00" z="-5.42" compression="2"> <!-- nose -->
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<control-input axis="/controls/rudder" control="STEER" square="true"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-29.15" y="5.42" z="-5.42" compression="2"> <!-- fwd left main -->
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<control-input axis="/controls/brakes[0]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-31.32" y="1.81" z="-5.42" compression="2"> <!-- rear left main -->
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<control-input axis="/controls/brakes[0]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-31.32" y="-1.81" z="-5.42" compression="2"> <!-- rear right main -->
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<control-input axis="/controls/brakes[1]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-29.15" y="-5.42" z="-5.42" compression="2"> <!-- fwd right main -->
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<control-input axis="/controls/brakes[1]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/>
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<tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/>
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<tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/>
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<ballast x="-6" y="0" z="2.4" mass="30000"/> <!-- hump -->
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<ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump -->
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<ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump -->
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<ballast x="-24" y="0" z="2.4" mass="30000"/> <!-- hump -->
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</airplane>
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