139 lines
6.3 KiB
XML
Executable file
139 lines
6.3 KiB
XML
Executable file
<!-- TSR2 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. Lee Elliott.
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The ailerons are a hack on this fdm - the real aircraft
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use all moving tail planes for roll and this model had a
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very high roll rate so they've been made relatively
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ineffective and in the model/anim file the aileron surface
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positions actually operate on the tailplanes.
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-->
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<airplane mass="54750">
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<!-- Approach configuration -->
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<approach speed="130" aoa="10.0">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
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<control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
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<control-setting axis="/controls/flight/flaps" value="1.0"/>
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<control-setting axis="/controls/flight/spoiler" value="0.2"/>
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<control-setting axis="/controls/gear/gear-down" value="1"/>
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</approach>
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<!-- Cruise configuration -->
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<!-- <cruise speed="840" alt="1000"> -->
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<cruise speed="1197" alt="35000">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
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<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
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<control-setting axis="/controls/engines/engine[0]/afterburner" value="1.0"/>
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<control-setting axis="/controls/engines/engine[1]/afterburner" value="1.0"/>
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<control-setting axis="/controls/flight/flaps" value="0.0"/>
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<control-setting axis="/controls/gear/gear-down" value="0"/>
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</cruise>
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<cockpit x="8.5" y="0.0" z="1.0"/>
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<fuselage ax="13.0" ay="0" az="0" bx="-14.13" by="0" bz=".64"
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width="2.0" taper="0.5" midpoint="0.3"/>
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<wing x="-3.0" y="1.5" z="1.7" taper="0.25"
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length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.003">
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<stall aoa="35.0" width="3" peak="1.3"/>
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<flap0 start="0.0" end="0.9" lift="1.4" drag="1.2"/>
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<flap1 start="0.0" end="0.4" lift="1.05" drag="1.2"/>
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<spoiler start="0.54" end="0.86" lift="0.0" drag="20.0"/>
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<control-input axis="/controls/flight/flaps" control="FLAP0"/>
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<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
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<control-input axis="/controls/flight/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="FLAP1" transition-time="0.5"/>
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<control-speed control="SPOILER" transition-time="0.5"/>
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</wing>
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<hstab x="-10.0" y="1.0" z="0.5" taper=".2" effectiveness="2.0"
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length="3.0" chord="4.0" sweep="55" dihedral="0.0">
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<stall aoa="35.0" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.4" drag="1.3"/>
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<control-input axis="/controls/flight/elevator" control="FLAP0"/>
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<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
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<control-speed control="FLAP0" transition-time="0.5"/>
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</hstab>
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<vstab x="-10.0" y="0" z="1.38" taper=".176" effectiveness="1.0"
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length="4.5" chord="4.0" sweep="50">
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<stall aoa="28.0" 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/flight/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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<!-- nose -->
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<gear x="3.0" y="0" z="-2.0" retract-time="7" compression="0.8">
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<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
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<control-input axis="/controls/gear/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="-4.0" y="2.5" z="-2.0" retract-time="7" compression="0.8">
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<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/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="-4.0" y="-2.5" z="-2.0" retract-time="7" compression="0.8">
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<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/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="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
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<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="10"/>
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<control-output control="EXTEND" prop="/canopy/position-norm"/>
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</gear>
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<jet x="-8.0" y="-1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
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<!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> -->
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<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
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<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
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</jet>
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<jet x="-8.0" y="1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
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<!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> -->
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<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
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<control-input axis="/controls/engines/engine[1]/afterburner" control="REHEAT"/>
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</jet>
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<tank x="-2.0" y="0.0" z="0.5" jet="true" capacity="13000"/>
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<tank x="-3.0" y="2.5" z="1.7" jet="true" capacity="11000"/>
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<tank x="-3.0" y="-2.5" z="1.7" jet="true" capacity="11000"/>
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<ballast x="8.5" y="0" z="0" mass="3000"/> <!-- Cockpit -->
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<ballast x="4.0" y="0" z="0" mass="3000"/> <!-- avionics -->
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<ballast x="-6.0" y="0" z="0" mass="100"/> <!-- Trim ballast -->
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</airplane>
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