222 lines
9 KiB
XML
222 lines
9 KiB
XML
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<!-- A10 yasim config. This is a hack and not an authentic
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representation of the aircraft. Having said that, the
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numbers, where I could find them, roughly match those of
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the original aircraft.
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Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
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-->
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<airplane mass="45860">
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<!-- Approach configuration -->
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<approach speed="110" aoa="14">
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<control-setting axis="/controls/throttle[0]" value="0.5"/>
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<control-setting axis="/controls/flaps" value="1.0"/>
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<control-setting axis="/controls/spoilers" 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="380" alt="35000">
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<control-setting axis="/controls/throttle[0]" value="0.8"/>
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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="-3.5" y="0.0" z="1.2"/>
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<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0"
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width="1.4"/>
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<!-- Left Engine -->
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<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8"
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width="1.5"/>
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<!-- Right Engine -->
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<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8"
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width="1.5"/>
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<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
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length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
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<stall aoa="14" width="3" peak="1.3"/>
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<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
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<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
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<spoiler start="0.54" end="0.86" 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/aileron-trim" 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="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="1.2"
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length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0.0">
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<stall aoa="20" width="5" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
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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="-15.0" y="2.5" z="-0.9" taper="0.7"
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length="2.8" chord="2.0" sweep="0.0">
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<stall aoa="16" width="5" 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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<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7"
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length="2.8" chord="2.0" sweep="0.0">
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<stall aoa="16" width="5" 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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<!-- Engines and tanks -->
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<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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</jet>
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<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
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<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
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</jet>
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<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
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<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
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<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/>
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<!-- Undercarriage -->
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<!-- nose -->
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<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
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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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<!-- left main -->
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<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
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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[0]/position-norm"/>
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</gear>
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<!-- right main -->
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<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
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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[1]/position-norm"/>
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</gear>
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<!-- Canopy -->
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<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6">
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<control-input axis="/controls/parking-brake" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="5"/>
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<control-output control="EXTEND" prop="/canopy/position-norm"/>
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</gear>
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<!-- Ballast -->
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<ballast x="-3.5" y="0" z="1.0" mass="800"/> <!-- C/pit + Pilot -->
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<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
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<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
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<ballast x="-7.0" y="0" z="-0.8" mass="2500"/> <!-- trim ballast -->
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<!-- Weapons load -->
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<!-- AGM65 x 16 objects and ballast (Left to Right) -->
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<!-- Positioned in line with the aircraft CG (x) - y and z locs approximate -->
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<!-- Left Wing Outer AGM65 -->
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<fuselage ax="-7.65" ay="4.71" az="-0.47" bx="-10.15" by="4.71" bz="-0.35" width="0.35"/>
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<ballast x="-8.6" y="4.71" z="-0.41" mass="485"/>
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<!-- Left Wing Mid Cluster Outer AGM65 -->
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<fuselage ax="-7.65" ay="3.89" az="-0.53" bx="-10.15" by="3.89" bz="-0.41" width="0.35"/>
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<ballast x="-8.6" y="3.89" z="-0.47" mass="485"/>
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<!-- Left Wing Mid Cluster Mid AGM65 -->
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<fuselage ax="-7.65" ay="3.59" az="-0.96" bx="-10.15" by="3.59" bz="-0.84" width="0.35"/>
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<ballast x="-8.6" y="3.89" z="-0.90" mass="485"/>
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<!-- Left Wing Mid Cluster Inner AGM65 -->
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<fuselage ax="-7.65" ay="3.21" az="-0.59" bx="-10.15" by="3.21" bz="-0.47" width="0.35"/>
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<ballast x="-8.6" y="3.21" z="-0.53" mass="485"/>
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<!-- Left Wing Inner Cluster Outer AGM65 -->
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<fuselage ax="-7.65" ay="1.97" az="-0.65" bx="-10.15" by="1.97" bz="-0.53" width="0.35"/>
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<ballast x="-8.6" y="1.97" z="-0.59" mass="485"/>
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<!-- Left Wing Inner Cluster Mid AGM65 -->
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<fuselage ax="-7.65" ay="1.63" az="-1.05" bx="-10.15" by="1.63" bz="-0.93" width="0.35"/>
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<ballast x="-8.6" y="1.63" z="-0.99" mass="485"/>
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<!-- Left Wing Inner Cluster Inner AGM65 -->
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<fuselage ax="-7.65" ay="1.29" az="-0.65" bx="-10.15" by="1.29" bz="-0.53" width="0.35"/>
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<ballast x="-8.6" y="1.29" z="-0.59" mass="485"/>
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<!-- Left Fuselage AGM65 -->
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<fuselage ax="-7.65" ay="0.53" az="-0.70" bx="-10.15" by="0.53" bz="-0.58" width="0.35"/>
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<ballast x="-8.6" y="0.53" z="-0.64" mass="485"/>
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<!-- Right Wing Outer AGM65 -->
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<fuselage ax="-7.65" ay="-4.71" az="-0.47" bx="-10.15" by="-4.71" bz="-0.35" width="0.35"/>
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<ballast x="-8.6" y="-4.71" z="-0.41" mass="485"/>
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<!-- Right Wing Mid Cluster Outer AGM65 -->
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<fuselage ax="-7.65" ay="-3.89" az="-0.53" bx="-10.15" by="-3.89" bz="-0.41" width="0.35"/>
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<ballast x="-8.6" y="-3.89" z="-0.47" mass="485"/>
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<!-- Right Wing Mid Cluster Mid AGM65 -->
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<fuselage ax="-7.65" ay="-3.59" az="-0.96" bx="-10.15" by="-3.59" bz="-0.84" width="0.35"/>
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<ballast x="-8.6" y="-3.89" z="-0.90" mass="485"/>
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<!-- Right Wing Mid Cluster Inner AGM65 -->
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<fuselage ax="-7.65" ay="-3.21" az="-0.59" bx="-10.15" by="-3.21" bz="-0.47" width="0.35"/>
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<ballast x="-8.6" y="-3.21" z="-0.53" mass="485"/>
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<!-- Right Wing Inner Cluster Outer AGM65 -->
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<fuselage ax="-7.65" ay="-1.97" az="-0.65" bx="-10.15" by="-1.97" bz="-0.53" width="0.35"/>
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<ballast x="-8.6" y="-1.97" z="-0.59" mass="485"/>
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<!-- Right Wing Inner Cluster Mid AGM65 -->
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<fuselage ax="-7.65" ay="-1.63" az="-1.05" bx="-10.15" by="-1.63" bz="-0.93" width="0.35"/>
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<ballast x="-8.6" y="-1.63" z="-0.99" mass="485"/>
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<!-- Right Wing Inner Cluster Inner AGM65 -->
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<fuselage ax="-7.65" ay="-1.29" az="-0.65" bx="-10.15" by="-1.29" bz="-0.53" width="0.35"/>
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<ballast x="-8.6" y="-1.29" z="-0.59" mass="485"/>
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<!-- Right Fuselage AGM65 -->
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<fuselage ax="-7.65" ay="-0.53" az="-0.70" bx="-10.15" by="-0.53" bz="-0.58" width="0.35"/>
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<ballast x="-8.6" y="-0.53" z="-0.64" mass="485"/>
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<!-- AIM9 x 2 objects and ballast (guessed) - (Left to Right) -->
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<!-- Positioned ahead of the aircraft CG (x) - y and z locs approximate -->
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<!-- Left Wing AIM9 -->
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<fuselage ax="-6.9" ay="5.76" az="-0.27" bx="-9.9" by="5.76" bz="-0.15" width="0.13"/>
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<ballast x="-7.9" y="5.76" z="-0.21" mass="200"/>
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<!-- Right Wing AIM9 -->
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<fuselage ax="-6.9" ay="-5.76" az="-0.27" bx="-9.9" by="-5.76" bz="-0.15" width="0.13"/>
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<ballast x="-7.9" y="-5.76" z="-0.21" mass="200"/>
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</airplane>
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