139 lines
5.6 KiB
XML
Executable file
139 lines
5.6 KiB
XML
Executable file
<!-- Hawker Sea Hawk 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="9720">
|
|
|
|
<!-- Approach configuration.
|
|
I couldn't find any approach data but I think that the way
|
|
the aircraft sits tail down on it's u/c indicates that it
|
|
must land at a fairly shallow AoA to avoid hitting tail
|
|
first. The speed is a guess.
|
|
|
|
I could see no sign or mention of spoilers or airbrakes in any
|
|
of the docs or pictures I found.
|
|
-->
|
|
<approach speed="110" aoa="7">
|
|
<control-setting axis="/controls/engines/engine[0]/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.
|
|
Max speed at sea level is 599 mph = 521 knots. The same source
|
|
also quoted 587 mph at 'altitude'.
|
|
-->
|
|
<cruise speed="521" alt="0">
|
|
<control-setting axis="/controls/engines/engine[0]/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="3.0" y="0.0" z="0.7"/>
|
|
|
|
<fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
|
|
width="1.3"/>
|
|
|
|
<!-- The wing length is from tips to fuselage, including intakes.
|
|
The aileron figures are probably too low but the roll rate seemed
|
|
too high otherwise.
|
|
-->
|
|
<wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
|
|
length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
|
|
<stall aoa="17" width="3" peak="1.3"/>
|
|
<flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
|
|
<flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>
|
|
|
|
<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-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="right"
|
|
prop="/surface-positions/right-spoiler-pos-norm"/> -->
|
|
|
|
<control-speed control="FLAP0" transition-time="5"/>
|
|
|
|
</wing>
|
|
|
|
<hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
|
|
length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
|
|
<stall aoa="17" 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="-5.2" y="0.0" z="0.2" taper="0.8"
|
|
length="1.4" chord="1.8" sweep="10.0">
|
|
<stall aoa="16" width="5" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.15" 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.
|
|
1 x Roll-Royce Nene 103. I've no idea how much it actually
|
|
weighs.
|
|
-->
|
|
<jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
|
|
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
|
</jet>
|
|
<!-- Fuel tanks in front of and behind the engine.
|
|
-->
|
|
<tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2600"/>
|
|
<tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2600"/>
|
|
|
|
<!-- Undercarriage -->
|
|
<!-- nose -->
|
|
<gear x="4.0" y="0.0" z="-1.39" retract-time="7" compression="0.6">
|
|
<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="0.08" y="1.4" z="-1.3" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/wheel[0]/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="0.08" y="-1.4" z="-1.3" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/wheel[1]/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="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="10"/>
|
|
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- Wingman -->
|
|
<gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
|
<control-input axis="/controls/autoflight/wingman" control="EXTEND"/>
|
|
<control-speed control="EXTEND" transition-time="10"/>
|
|
<control-output control="EXTEND" prop="/wingman/position-norm"/>
|
|
</gear>
|
|
|
|
<!-- Ballast -->
|
|
<ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
|
|
<ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
|
|
<ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->
|
|
|
|
</airplane>
|