141 lines
5.8 KiB
XML
Executable file
141 lines
5.8 KiB
XML
Executable file
<!-- Hawker Sea Hawk yasim config. This is a hack and not an
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authentic representation of the aircraft. Having said
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that, the numbers, where I could find them, roughly match
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those of 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="9720">
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<!-- Approach configuration.
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I couldn't find any approach data but I think that the way
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the aircraft sits tail down on it's u/c indicates that it
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must land at a fairly shallow AoA to avoid hitting tail
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first. The speed is a guess.
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I could see no sign or mention of spoilers or airbrakes in any
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of the docs or pictures I found.
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-->
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<approach speed="110" aoa="7">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
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<control-setting axis="/controls/flight/flaps" value="1.0"/>
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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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Max speed at sea level is 599 mph = 521 knots. The same source
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also quoted 587 mph at 'altitude'.
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-->
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<cruise speed="521" alt="0">
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<control-setting axis="/controls/engines/engine[0]/throttle" 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="3.0" y="0.0" z="0.7"/>
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<fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
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width="1.3"/>
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<!-- The wing length is from tips to fuselage, including intakes.
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The aileron figures are probably too low but the roll rate seemed
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too high otherwise.
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-->
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<wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
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length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
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<stall aoa="17" width="3" peak="1.3"/>
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<flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
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<flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>
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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-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="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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</wing>
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<hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
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length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
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<stall aoa="17" width="5" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
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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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</hstab>
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<vstab x="-5.2" y="0.0" z="0.2" taper="0.8"
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length="1.4" chord="1.8" sweep="10.0">
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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/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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<!-- Engines and tanks.
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1 x Roll-Royce Nene 103. I've no idea how much it actually
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weighs.
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-->
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<jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
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<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
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</jet>
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<!-- Fuel tanks in front of and behind the engine.
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-->
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<tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2600"/>
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<tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2600"/>
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<!-- Undercarriage -->
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<!-- nose -->
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<gear x="4.0" y="0.0" z="-1.39" retract-time="7" compression="0.6">
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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="0.08" y="1.4" z="-1.3" retract-time="7" compression="0.6">
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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="0.08" y="-1.4" z="-1.3" retract-time="7" compression="0.6">
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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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<!-- Wingman -->
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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/autoflight/wingman" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="10"/>
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<control-output control="EXTEND" prop="/wingman/position-norm"/>
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</gear>
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<!-- Ballast -->
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<ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
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<ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
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<ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->
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</airplane>
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