ca3963d865
The other stuff isn't really an update but something I did for a bit of a laugh. The idea ocurred to me after animating the folding wings on the seahawk and seeing that the aileron and flap axis still worked...
139 lines
5.4 KiB
XML
Executable file
139 lines
5.4 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/throttle[0]" value="0.5"/>
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<control-setting axis="/controls/flaps" value="1.0"/>
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<control-setting axis="/controls/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/throttle[0]" value="1.0"/>
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<control-setting axis="/controls/flaps" value="0.0"/>
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<control-setting axis="/controls/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/flaps" control="FLAP0"/>
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<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/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/elevator" control="FLAP0"/>
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<control-input axis="/controls/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/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/throttle[0]" 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/rudder" control="STEER" square="true"/>
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<control-input axis="/controls/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/brakes[0]" control="BRAKE"/>
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<control-input axis="/controls/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/brakes[1]" control="BRAKE"/>
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<control-input axis="/controls/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/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/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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