223 lines
9.4 KiB
XML
223 lines
9.4 KiB
XML
<!-- A10 yasim config. This is a hack and not an authentic
|
|
representation of the aircraft. Having said that, the
|
|
numbers, where I could find them, roughly match those of
|
|
the original aircraft.
|
|
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
|
-->
|
|
|
|
<airplane mass="45860">
|
|
|
|
<!-- Approach configuration -->
|
|
<approach speed="110" aoa="8">
|
|
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
|
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
|
|
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
|
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
|
</approach>
|
|
|
|
<!-- Cruise configuration -->
|
|
<cruise speed="380" alt="0">
|
|
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
|
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
|
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
|
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
|
</cruise>
|
|
|
|
<cockpit x="-3.5" y="0.0" z="1.2"/>
|
|
|
|
<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0"
|
|
width="1.4"/>
|
|
|
|
<!-- Left Engine -->
|
|
<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8"
|
|
width="1.5"/>
|
|
|
|
<!-- Right Engine -->
|
|
<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8"
|
|
width="1.5"/>
|
|
|
|
<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
|
|
length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
|
|
<stall aoa="17" width="6" peak="1.3"/>
|
|
<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
|
|
<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
|
|
<spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
|
|
|
|
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
|
<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/spoilers" 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="SPOILER" side="left"
|
|
prop="/surface-positions/left-spoiler-pos-norm"/>
|
|
<control-output control="SPOILER" side="right"
|
|
prop="/surface-positions/right-spoiler-pos-norm"/>
|
|
|
|
<control-speed control="FLAP0" transition-time="5"/>
|
|
<control-speed control="SPOILER" transition-time="0.5"/>
|
|
|
|
</wing>
|
|
|
|
<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
|
|
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
|
|
<stall aoa="18" width="5" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
|
<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>
|
|
|
|
<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
|
|
length="2.8" chord="2.0" sweep="0.0">
|
|
<stall aoa="16" width="5" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
|
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
|
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
|
</vstab>
|
|
|
|
<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
|
|
length="2.8" chord="2.0" sweep="0.0">
|
|
<stall aoa="16" width="5" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
|
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
|
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
|
</vstab>
|
|
|
|
<!-- Engines and tanks -->
|
|
<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
|
|
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
|
</jet>
|
|
|
|
<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
|
|
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
|
</jet>
|
|
|
|
<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
|
|
<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
|
|
<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/>
|
|
|
|
<!-- Undercarriage -->
|
|
<!-- nose -->
|
|
<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.8">
|
|
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
|
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="7"/>
|
|
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- left main -->
|
|
<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
|
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
|
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="7"/>
|
|
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- right main -->
|
|
<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
|
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
|
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="7"/>
|
|
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- Canopy -->
|
|
<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="5"/>
|
|
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- Ballast -->
|
|
<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- C/pit + Pilot -->
|
|
<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
|
|
<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
|
|
|
|
<!-- Weapons load -->
|
|
|
|
<!-- AGM65 x 16 objects and ballast (Left to Right) -->
|
|
<!-- Positioned just ahead of the aircraft CG (x) - y and z locs approximate -->
|
|
|
|
<!-- Left Wing Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="4.71" az="-0.47" bx="-10.15" by="4.71" bz="-0.35" width="0.35"/>
|
|
<ballast x="-8.9" y="4.71" z="-0.41" mass="485"/>
|
|
|
|
<!-- Left Wing Mid Cluster Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="3.89" az="-0.53" bx="-10.15" by="3.89" bz="-0.41" width="0.35"/>
|
|
<ballast x="-8.9" y="3.89" z="-0.47" mass="485"/>
|
|
|
|
<!-- Left Wing Mid Cluster Mid AGM65 -->
|
|
<fuselage ax="-7.65" ay="3.59" az="-0.96" bx="-10.15" by="3.59" bz="-0.84" width="0.35"/>
|
|
<ballast x="-8.9" y="3.89" z="-0.90" mass="485"/>
|
|
|
|
<!-- Left Wing Mid Cluster Inner AGM65 -->
|
|
<fuselage ax="-7.65" ay="3.21" az="-0.59" bx="-10.15" by="3.21" bz="-0.47" width="0.35"/>
|
|
<ballast x="-8.9" y="3.21" z="-0.53" mass="485"/>
|
|
|
|
<!-- Left Wing Inner Cluster Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="1.97" az="-0.65" bx="-10.15" by="1.97" bz="-0.53" width="0.35"/>
|
|
<ballast x="-8.9" y="1.97" z="-0.59" mass="485"/>
|
|
|
|
<!-- Left Wing Inner Cluster Mid AGM65 -->
|
|
<fuselage ax="-7.65" ay="1.63" az="-1.05" bx="-10.15" by="1.63" bz="-0.93" width="0.35"/>
|
|
<ballast x="-8.9" y="1.63" z="-0.99" mass="485"/>
|
|
|
|
<!-- Left Wing Inner Cluster Inner AGM65 -->
|
|
<fuselage ax="-7.65" ay="1.29" az="-0.65" bx="-10.15" by="1.29" bz="-0.53" width="0.35"/>
|
|
<ballast x="-8.9" y="1.29" z="-0.59" mass="485"/>
|
|
|
|
<!-- Left Fuselage AGM65 -->
|
|
<fuselage ax="-7.65" ay="0.53" az="-0.70" bx="-10.15" by="0.53" bz="-0.58" width="0.35"/>
|
|
<ballast x="-8.9" y="0.53" z="-0.64" mass="485"/>
|
|
|
|
<!-- Right Wing Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="-4.71" az="-0.47" bx="-10.15" by="-4.71" bz="-0.35" width="0.35"/>
|
|
<ballast x="-8.9" y="-4.71" z="-0.41" mass="485"/>
|
|
|
|
<!-- Right Wing Mid Cluster Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="-3.89" az="-0.53" bx="-10.15" by="-3.89" bz="-0.41" width="0.35"/>
|
|
<ballast x="-8.9" y="-3.89" z="-0.47" mass="485"/>
|
|
|
|
<!-- Right Wing Mid Cluster Mid AGM65 -->
|
|
<fuselage ax="-7.65" ay="-3.59" az="-0.96" bx="-10.15" by="-3.59" bz="-0.84" width="0.35"/>
|
|
<ballast x="-8.9" y="-3.89" z="-0.90" mass="485"/>
|
|
|
|
<!-- Right Wing Mid Cluster Inner AGM65 -->
|
|
<fuselage ax="-7.65" ay="-3.21" az="-0.59" bx="-10.15" by="-3.21" bz="-0.47" width="0.35"/>
|
|
<ballast x="-8.9" y="-3.21" z="-0.53" mass="485"/>
|
|
|
|
<!-- Right Wing Inner Cluster Outer AGM65 -->
|
|
<fuselage ax="-7.65" ay="-1.97" az="-0.65" bx="-10.15" by="-1.97" bz="-0.53" width="0.35"/>
|
|
<ballast x="-8.9" y="-1.97" z="-0.59" mass="485"/>
|
|
|
|
<!-- Right Wing Inner Cluster Mid AGM65 -->
|
|
<fuselage ax="-7.65" ay="-1.63" az="-1.05" bx="-10.15" by="-1.63" bz="-0.93" width="0.35"/>
|
|
<ballast x="-8.9" y="-1.63" z="-0.99" mass="485"/>
|
|
|
|
<!-- Right Wing Inner Cluster Inner AGM65 -->
|
|
<fuselage ax="-7.65" ay="-1.29" az="-0.65" bx="-10.15" by="-1.29" bz="-0.53" width="0.35"/>
|
|
<ballast x="-8.9" y="-1.29" z="-0.59" mass="485"/>
|
|
|
|
<!-- Right Fuselage AGM65 -->
|
|
<fuselage ax="-7.65" ay="-0.53" az="-0.70" bx="-10.15" by="-0.53" bz="-0.58" width="0.35"/>
|
|
<ballast x="-8.9" y="-0.53" z="-0.64" mass="485"/>
|
|
|
|
<!-- AIM9 x 2 objects and ballast (guessed) - (Left to Right) -->
|
|
<!-- Positioned ahead of the aircraft CG (x) - y and z locs approximate -->
|
|
|
|
<!-- Left Wing AIM9 -->
|
|
<fuselage ax="-6.9" ay="5.76" az="-0.27" bx="-9.9" by="5.76" bz="-0.15" width="0.13"/>
|
|
<ballast x="-8.9" y="5.76" z="-0.21" mass="200"/>
|
|
|
|
<!-- Right Wing AIM9 -->
|
|
<fuselage ax="-6.9" ay="-5.76" az="-0.27" bx="-9.9" by="-5.76" bz="-0.15" width="0.13"/>
|
|
<ballast x="-8.9" y="-5.76" z="-0.21" mass="200"/>
|
|
|
|
</airplane>
|