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Lee Elliott:

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...
This commit is contained in:
curt 2003-01-09 15:04:55 +00:00
parent a2c511a47f
commit ca3963d865
2 changed files with 212 additions and 0 deletions

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<!-- 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/throttle[0]" value="0.5"/>
<control-setting axis="/controls/flaps" value="1.0"/>
<control-setting axis="/controls/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/throttle[0]" value="1.0"/>
<control-setting axis="/controls/flaps" value="0.0"/>
<control-setting axis="/controls/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/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/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/elevator" control="FLAP0"/>
<control-input axis="/controls/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/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/throttle[0]" 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/rudder" control="STEER" square="true"/>
<control-input axis="/controls/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/brakes[0]" control="BRAKE"/>
<control-input axis="/controls/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/brakes[1]" control="BRAKE"/>
<control-input axis="/controls/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/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/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>

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<?xml version="1.0"?>
<!--
************************************************************************
Hawker Sea Hawk pair simulation config.
2003-01-09 Lee Elliott leee-fgfs@spatial.freeserve.co.uk
************************************************************************
-->
<PropertyList>
<sim>
<flight-model>yasim</flight-model>
<aero>seahawkpair-yasim</aero>
<fuel-fraction>1.0</fuel-fraction>
<sound>
<audible>true</audible>
<path>Aircraft/a4/a4-sound.xml</path>
</sound>
<panel>
<path>Aircraft/c310/c310-vfr-panel.xml</path>
</panel>
<panel_2>
<path>Aircraft/c310/c310-mini-panel.xml</path>
</panel_2>
<hud>
<path>Huds/Default/default.xml</path>
<visibility>true</visibility>
</hud>
<model>
<path>Aircraft/seahawk/seahawkpair-model.xml</path>
</model>
<view n="1">
<config>
<z-offset-m type="double" archive="y">-80.0</z-offset-m>
</config>
</view>
</sim>
<autopilot>
<config>
<min-climb-speed-kt type="float">100.0</min-climb-speed-kt>
<best-climb-speed-kt type="float">550.0</best-climb-speed-kt>
<target-climb-rate-fpm type="float">6000.0</target-climb-rate-fpm>
<target-descent-rate-fpm type="float">6000.0</target-descent-rate-fpm>
<elevator-adj-factor type="float">300.0</elevator-adj-factor>
<integral-contribution type="float">0.005</integral-contribution>
<max-aileron type="float">0.5</max-aileron>
<max-roll-deg type="float">60.0</max-roll-deg>
<roll-out-deg type="float">8</roll-out-deg>
<roll-out-smooth-deg type="float">15.0</roll-out-smooth-deg>
<zero-pitch-throttle type="float">0.5</zero-pitch-throttle>
<zero-pitch-trim-full-throttle type="float">0.001</zero-pitch-trim-full-throttle>
</config>
</autopilot>
</PropertyList>