02b4b4a3f0
Here're some updates for some of the instruments, the TSR2 and the B52. The instruments are just parameterised/non-specific versions of the engine and fuel gauges. The old gauges will still be used by the a10s and the sea hawks until I get them done. There're a couple of tweaks to the tsr2 yasim config and amendments to the model file to change the angle at which the airbrakes operate, correct the direction that the nose gear retracts/extends and to rotate the main-gear carts during retraction/extention. There're also new panels, using the new instruments. The b52 yasim config has some big changes due to finding some more info i.e. wing incidence of 6 degrees, fuel capacities and aileron changes (removed from G & H versions!). It's now based on an 'F' model and I've put some comments in the yasim config about it. The b52-readme.txt includes a suggested method on getting airborne;). I've included an amended model - B52-F.3ds, which is the default in the new model file, and a couple of panels. I'm quite pleased with the b52 - the take-offs resemble the photographs I've seen and I think I've got reasonable values where I've had to guess at stuff, but the results from the yasim solver look as through the model is approaching the limits of acceptability for yasim. By this I mean that the model is probably a bit dodgy, not that the yasim solver is limited.
137 lines
5.9 KiB
XML
Executable file
137 lines
5.9 KiB
XML
Executable file
<!-- TSR2 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.
|
|
|
|
The ailerons are a hack on this fdm - the real aircraft
|
|
use all moving tail planes for roll and this model had a
|
|
very high roll rate so they've been made relatively
|
|
ineffective and in the model/anim file the aileron surface
|
|
positions actually operate on the tailplanes.
|
|
-->
|
|
|
|
<airplane mass="54750">
|
|
|
|
<!-- Approach configuration -->
|
|
<approach speed="130" aoa="10.0">
|
|
<control-setting axis="/controls/throttle[0]" value="0.2"/>
|
|
<control-setting axis="/controls/throttle[1]" value="0.2"/>
|
|
<control-setting axis="/controls/flaps" value="1.0"/>
|
|
<control-setting axis="/controls/spoiler" value="0.2"/>
|
|
<control-setting axis="/controls/gear-down" value="1"/>
|
|
</approach>
|
|
|
|
<!-- Cruise configuration -->
|
|
<!-- <cruise speed="840" alt="1000"> -->
|
|
<cruise speed="1197" alt="35000">
|
|
<control-setting axis="/controls/throttle[0]" value="1.0"/>
|
|
<control-setting axis="/controls/throttle[1]" value="1.0"/>
|
|
<control-setting axis="/controls/afterburner[0]" value="1.0"/>
|
|
<control-setting axis="/controls/afterburner[1]" value="1.0"/>
|
|
<control-setting axis="/controls/flaps" value="0.0"/>
|
|
<control-setting axis="/controls/gear-down" value="0"/>
|
|
</cruise>
|
|
|
|
<cockpit x="8.5" y="0.0" z="1.0"/>
|
|
|
|
<fuselage ax="13.0" ay="0" az="0" bx="-14.13" by="0" bz=".64"
|
|
width="2.0" taper="0.5" midpoint="0.3"/>
|
|
|
|
<wing x="-3.0" y="1.5" z="1.7" taper="0.25"
|
|
length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.003">
|
|
<stall aoa="35.0" width="3" peak="1.3"/>
|
|
<flap0 start="0.0" end="0.9" lift="1.4" drag="1.2"/>
|
|
<flap1 start="0.0" end="0.4" lift="1.05" drag="1.2"/>
|
|
<spoiler start="0.54" end="0.86" lift="0.0" drag="20.0"/>
|
|
|
|
<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-input axis="/controls/spoilers" control="SPOILER"/>
|
|
|
|
<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="left"
|
|
prop="/surface-positions/left-spoiler-pos-norm"/>
|
|
<control-output control="SPOILER" side="right"
|
|
prop="/surface-positions/right-spoiler-pos-norm"/>
|
|
|
|
<control-speed control="FLAP0" transition-time="5"/>
|
|
<control-speed control="FLAP1" transition-time="0.5"/>
|
|
<control-speed control="SPOILER" transition-time="0.5"/>
|
|
|
|
</wing>
|
|
|
|
<hstab x="-10.0" y="1.0" z="0.5" taper=".2" effectiveness="2.0"
|
|
length="3.0" chord="4.0" sweep="55" dihedral="0.0">
|
|
<stall aoa="35.0" width="3" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.4" drag="1.3"/>
|
|
<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"/>
|
|
<control-speed control="FLAP0" transition-time="0.5"/>
|
|
</hstab>
|
|
|
|
<vstab x="-10.0" y="0" z="1.38" taper=".176" effectiveness="1.0"
|
|
length="4.5" chord="4.0" sweep="50">
|
|
<stall aoa="28.0" width="3" 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>
|
|
|
|
<!-- nose -->
|
|
<gear x="3.0" y="0" z="-2.0" retract-time="7" compression="0.8">
|
|
<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="-4.0" y="2.5" z="-2.0" retract-time="7" compression="0.8">
|
|
<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="-4.0" y="-2.5" z="-2.0" retract-time="7" compression="0.8">
|
|
<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>
|
|
|
|
<jet x="-8.0" y="-1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
|
|
<!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> -->
|
|
<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
|
|
<control-input axis="/controls/afterburner[0]" control="REHEAT"/>
|
|
</jet>
|
|
|
|
<jet x="-8.0" y="1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
|
|
<!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> -->
|
|
<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
|
|
<control-input axis="/controls/afterburner[1]" control="REHEAT"/>
|
|
</jet>
|
|
|
|
<tank x="-2.0" y="0.0" z="0.5" jet="true" capacity="13000"/>
|
|
<tank x="-3.0" y="2.5" z="1.7" jet="true" capacity="11000"/>
|
|
<tank x="-3.0" y="-2.5" z="1.7" jet="true" capacity="11000"/>
|
|
|
|
<ballast x="8.5" y="0" z="0" mass="3000"/> <!-- Cockpit -->
|
|
<ballast x="4.0" y="0" z="0" mass="3000"/> <!-- avionics -->
|
|
<ballast x="-6.0" y="0" z="0" mass="100"/> <!-- Trim ballast -->
|
|
|
|
</airplane>
|