184 lines
6.3 KiB
XML
184 lines
6.3 KiB
XML
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<!-- B52-H yasim config.
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Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
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-->
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<airplane mass="185000">
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<!-- Approach configuration -->
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<approach speed="100" aoa="0.0">
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<control-setting axis="/controls/throttle[0]" value="0.6"/>
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<control-setting axis="/controls/flaps" value="2.0"/>
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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="450" alt="0"> -->
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<control-setting axis="/controls/throttle[0]" value="1.0"/>
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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="-2.2" y="0.0" z="2.0"/>
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<fuselage ax="0" ay="0" az="0" bx="-49.05" by="0" bz=".64"
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width="3.2" taper="0.5" midpoint="0.3"/>
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<wing x="-16.0" y="1.6" z="1.2" taper="0.4"
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length="31.1" chord="10.0" sweep="35" dihedral="-4.0" camber="0.01">
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<stall aoa="15.0" width="3" peak="1.3"/>
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<flap0 start="0.0" end="0.7" lift="1.5" drag="1.2"/>
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<flap1 start="0.75" end="0.9" lift="1.5" drag="1.2"/>
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<spoiler start="0.5" end="0.75" lift="0.1" drag="20.0"/>
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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/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-output control="SPOILER" side="left"
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prop="/surface-positions/left-spoiler-pos-norm"/>
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<control-output control="SPOILER" side="right"
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prop="/surface-positions/right-spoiler-pos-norm"/>
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<control-speed control="FLAP0" transition-time="5"/>
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<control-speed control="SPOILER" transition-time="0.5"/>
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</wing>
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<hstab x="-41.5" y="1.0" z="0.8" taper="0.25" effectiveness="1.0"
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length="7.5" chord="7.5" sweep="40.0" dihedral="0.0">
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<stall aoa="15.0" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.7" drag="2.0"/>
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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="-41.5" y="0" z="2.0" taper="0.4"
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length="8.5" chord="7.5" sweep="35.0">
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<stall aoa="15.0" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
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<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
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</vstab>
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<!-- Left wing engines -->
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<!-- Left Outer Left -->
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<jet x="-23.0" y="20.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Left Outer Right -->
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<jet x="-23.0" y="18.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Left Inner Left -->
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<jet x="-15.0" y="12.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Left Inner Right -->
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<jet x="-15.0" y="10.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Right wing engines -->
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<!-- Right Inner Left -->
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<jet x="-15.0" y="-10.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Right Inner Right -->
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<jet x="-15.0" y="-12.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Right Outer Left -->
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<jet x="-23.0" y="-18.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Right Outer Right -->
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<jet x="-23.0" y="-20.0" z="-1.0"
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mass="4000"
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thrust="17000">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<!-- Front Left -->
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<gear x="-13.2" y="2.0" z="-2.8" retract-time="7" compression="1.0">
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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-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<!-- Front Right -->
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<gear x="-13.2" y="-2.0" z="-2.8" retract-time="7" compression="1.0">
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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-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<!-- Rear Left -->
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<gear x="-28.0" y="2.0" z="-2.8" retract-time="7" compression="1.2">
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<control-input axis="/controls/brakes" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<!-- Rear Right -->
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<gear x="-28.0" y="-2.0" z="-2.8" retract-time="7" compression="1.2">
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<control-input axis="/controls/brakes" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<!-- Left Wing -->
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<gear x="-31.0" y="23.0" z="-2.0" retract-time="7" compression="3.5">
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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-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<!-- Right Wing -->
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<gear x="-31.0" y="-23.0" z="-2.0" retract-time="7" compression="3.5">
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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-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
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</gear>
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<tank x="-20.0" y="6.0" z="2.0" capacity="80000"/>
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<tank x="-20.0" y="-6.0" z="2.0" capacity="80000"/>
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<ballast x="-10.0" y="0" z="1" mass="30000"/>
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</airplane>
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