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fgdata/Aircraft-yasim/a10cl-yasim.xml
curt 3a71945920 Lee Elliott:
Initial revision of a10.
2002-12-06 18:41:03 +00:00

141 lines
5.6 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="37700">
<!-- Approach configuration -->
<approach speed="110" aoa="14">
<control-setting axis="/controls/throttle[0]" value="0.5"/>
<control-setting axis="/controls/flaps" value="1.0"/>
<control-setting axis="/controls/spoilers" value="1.0"/>
<control-setting axis="/controls/gear-down" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="380" alt="35000">
<control-setting axis="/controls/throttle[0]" value="0.8"/>
<control-setting axis="/controls/flaps" value="0.0"/>
<control-setting axis="/controls/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="14" width="3" 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/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
<control-input axis="/controls/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="1.2"
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0.0">
<stall aoa="20" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
<control-input axis="/controls/elevator" control="FLAP0"/>
<control-input axis="/controls/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"
length="2.8" chord="2.0" sweep="0.0">
<stall aoa="16" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
<control-input axis="/controls/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"
length="2.8" chord="2.0" sweep="0.0">
<stall aoa="16" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
<control-input axis="/controls/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/throttle[0]" control="THROTTLE"/>
</jet>
<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
<control-input axis="/controls/throttle[1]" 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="0.7">
<control-input axis="/controls/rudder" control="STEER" square="true"/>
<control-input axis="/controls/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/brakes[0]" control="BRAKE"/>
<control-input axis="/controls/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/brakes[1]" control="BRAKE"/>
<control-input axis="/controls/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/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="800"/> <!-- 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 -->
<ballast x="-7.0" y="0" z="-0.8" mass="2500"/> <!-- trim ballast -->
</airplane>