<!-- 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="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="4.5" y="0.0" z="1.2"/> <fuselage ax="8" ay="0" az="0" bx="-8.26" by="0" bz="0" width="1.4"/> <!-- Left Engine --> <fuselage ax="-2" ay="1.50" az="1" bx="-5.5" by="1.50" bz="0.8" width="1.5"/> <!-- Right Engine --> <fuselage ax="-2" ay="-1.50" az="1" bx="-5.5" by="-1.50" bz="0.8" width="1.5"/> <wing x="-0.8" 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="-7.5" 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="-7.0" 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="-7.0" 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="-3.8" y="-1.5" z="1.0" mass="1000" thrust="9065"> <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/> </jet> <jet x="-3.8" y="1.5" z="1.0" mass="1000" thrust="9065"> <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/> </jet> <tank x="-0.5" y="-1.5" z="0.0" jet="true" capacity="2000"/> <tank x="-0.5" y="1.5" z="0.0" jet="true" capacity="2000"/> <tank x="-0.5" y="0" z="0.0" jet="true" capacity="6700"/> <!-- Ferry Tanks --> <tank x="-0.5" y="1.29" z="-0.7" jet="true" capacity="4032"/> <tank x="-0.5" y="0" z="-0.7" jet="true" capacity="4032"/> <tank x="-0.5" y="-1.29" z="-0.7" jet="true" capacity="4032"/> <!-- Undercarriage --> <!-- nose --> <gear x="5.1" y="0.4" z="-2.8" retract-time="7" compression="0.7"> <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="-1.0" 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="-1.0" 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="5.4" 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="4.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit --> <ballast x="4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun --> <ballast x="3.0" y="0" z="0.0" mass="1000"/> <!-- avionics --> <!-- Ferry Tanks --> <fuselage ax="1.1" ay="0.0" az="-1.2" bx="-2.9" by="0.0" bz="-1.2" width="0.8"/> <fuselage ax="1.1" ay="1.29" az="-1.2" bx="-2.9" by="1.29" bz="-1.2" width="0.8"/> <fuselage ax="1.1" ay="-1.29" az="-1.2" bx="-2.9" by="-1.29" bz="-1.2" width="0.8"/> </airplane>