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Initial revision of YASim aircraft config files.

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curt 2001-12-06 19:16:30 +00:00
parent 9e0e36808d
commit aada4d7db3
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90
Aircraft-yasim/747.xml Normal file
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<airplane mass="400000">
<!-- Approach configuration -->
<approach speed="130" aoa="9">
<control axis="/controls/throttle[0]" value="0.5"/>
<control axis="/controls/throttle[1]" value="0.5"/>
<control axis="/controls/flaps" value="1.0"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="487" alt="41000">
<control axis="/controls/throttle[0]" value="1.0"/>
<control axis="/controls/throttle[1]" value="1.0"/>
<control axis="/controls/flaps" value="0.0"/>
</cruise>
<cockpit x="-5.42" y="1.81" z="15.06"/>
<fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41" width="6"/>
<wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
taper=".27" dihedral="7" camber="0.1">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.8" drag="3"/>
<flap1 start=".64" end=".88" lift="1.3" drag="1.5"/>
<control axis="/controls/flaps" output="FLAP0"/>
<control axis="/controls/aileron" output="FLAP1" split="true"/>
</wing>
<hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
sweep="28" dihedral="7" effectiveness="1">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
<control axis="/controls/elevator" output="FLAP0"/>
<control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>
<vstab x="-62.63" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3"
sweep="33" effectiveness="1">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.2" drag="1.3"/>
<control axis="/controls/rudder" output="FLAP0" invert="true"/>
</vstab>
<jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="60000">
<control axis="/controls/throttle[0]" output="THROTTLE"/>
</jet>
<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="60000">
<control axis="/controls/throttle[0]" output="THROTTLE"/>
</jet>
<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="60000">
<control axis="/controls/throttle[1]" output="THROTTLE"/>
</jet>
<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="60000">
<control axis="/controls/throttle[1]" output="THROTTLE"/>
</jet>
<gear x="-5.42" y="0.00" z="-5.42" retract-time="7" compression="2"> <!-- nose -->
<control axis="/controls/rudder" output="STEER" square="true"/>
</gear>
<gear x="-29.15" y="5.42" z="-5.42" retract-time="7" compression="2"> <!-- fwd left main -->
<control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<gear x="-31.32" y="1.81" z="-5.42" retract-time="7" compression="2"> <!-- rear left main -->
<control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<gear x="-31.32" y="-1.81" z="-5.42" retract-time="7" compression="2"> <!-- rear right main -->
<control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>
<gear x="-29.15" y="-5.42" z="-5.42" retract-time="7" compression="2"> <!-- fwd right main -->
<control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>
<tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/>
<tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/>
<tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/>
<ballast x="-6" y="0" z="2.4" mass="40000"/> <!-- hump -->
<ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump -->
<ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump -->
<ballast x="-24" y="0" z="2.4" mass="40000"/> <!-- hump -->
</airplane>

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Aircraft-yasim/X15set.xml Normal file
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<?xml version="1.0"?>
<!--
************************************************************************
X15 simulation config. This files ties together all the components
used by FGFS to represent the X15. Components include the flight data
model, instrument panel, and external 3D model.
3D models can be downloaded from http://home.t-online.de/home/Wolfram.Kuss/
October 23 2001 John Check, fgpanels@rockfish.net
************************************************************************
-->
<PropertyList>
<!-- these are the three main components -->
<sim>
<flight-model>jsb</flight-model>
<aircraft>X15</aircraft>
<sound>false</sound>
<panel>
<path>Aircraft/X15/Panels/X15-panel.xml</path>
</panel>
<!-- gear up -->
<model>
<path>Aircraft/X15/Models/X15_flight.ac</path>
</model>
<!-- gear down -->
<model_2>
<path>Aircraft/X15/Models/X15_landing.ac</path>
</model_2>
</sim>
</PropertyList>

77
Aircraft-yasim/a4.xml Normal file
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<airplane mass="10250">
<!-- Approach configuration -->
<approach speed="120" aoa="16.5">
<control axis="/controls/throttle[0]" value="0.5"/>
<control axis="/controls/flaps" value="1.0"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="517" alt="34000">
<control axis="/controls/throttle[0]" value="1.0"/>
<control axis="/controls/flaps" value="0.0"/>
</cruise>
<cockpit x="-2.9" y="0.0" z="1.0"/>
<fuselage ax="0" ay="0" az="0" bx="-12.2" by="0" bz=".64" width="1.47"/>
<wing x="-6.4" y=".55" z="0" taper=".186"
length="4.04" chord="3.95" sweep="28" dihedral="0" camber="0.1">
<stall aoa="25" width="10" peak="1.3"/>
<flap0 start="0.0" end="0.5" lift="1.5" drag="2.0"/>
<flap1 start="0.5" end="1.0" lift="1.15" drag="1.3"/>
<control axis="/controls/flaps" output="FLAP0"/>
<control axis="/controls/aileron" output="FLAP1" split="true"/>
</wing>
<hstab x="-11.01" y="0" z="1.38" taper=".3" effectiveness="2"
length="2.02" chord="2.02" sweep="26">
<stall aoa="25" width="10" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="2.0"/>
<control axis="/controls/elevator" output="FLAP0"/>
<control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>
<vstab x="-11.01" y="0" z="1.38" taper=".176"
length="2.57" chord="3.11" sweep="28">
<stall aoa="25" width="10" peak="1.5"/>
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
<control axis="/controls/rudder" output="FLAP0" invert="true"/>
</vstab>
<!-- NOTE: Skyhawks do NOT have afterburners. This one does for
testing purposes only -->
<jet x="-5.0" y="0" z=".44" mass="2050" thrust="10250" afterburner="16500">
<control axis="/controls/throttle[0]" output="THROTTLE"/>
<control axis="/controls/afterburner[0]" output="REHEAT"/>
</jet>
<!-- nose -->
<gear x="-2.29" y="0" z="-1.93" retract-time="7" compression=".96">
<control axis="/controls/rudder" output="STEER" square="true"/>
</gear>
<!-- left main -->
<gear x="-7" y="1.19" z="-1.56" retract-time="7" compression=".78">
<control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<!-- right main -->
<gear x="-7" y="-1.19" z="-1.56" retract-time="7" compression=".78">
<control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>
<!-- A4-M had 800 gallons of in-fuselage fuel capacity in three tanks,
one in each wing and one behind the cockpit. TA-4F had "only" 100
gallons in the fuselage due to the second seat, so the wings must
have 0-350 gallons each. Call the tanks 260/280/260 gallons, and
use 6.72 lbs/gal for Jet-A fuel. -->
<tank x="-5.50" y="0" z="0.5" jet="true" capacity="1880"/>
<tank x="-6.0" y="1" z="0" jet="true" capacity="1750"/>
<tank x="-6.0" y="-1" z="0" jet="true" capacity="1750"/>
<ballast x="-1.5" y="0" z="1" mass="650"/> <!-- cockpit -->
<ballast x="-3.0" y="0" z="1" mass="650"/> <!-- cockpit -->
<ballast x="-11.01" y="0" z="1.38" mass="-300"/> <!-- lighten the tail -->
</airplane>

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Aircraft-yasim/c172.xml Normal file
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<airplane mass="1950">
<!-- Approach configuration -->
<approach speed="40" aoa="16">
<control axis="/controls/throttle[0]" value="0.3"/>
<control axis="/controls/mixture[0]" value="1.0"/>
<control axis="/controls/flaps" value="1.0"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="115" alt="8000">
<control axis="/controls/throttle[0]" value="1.0"/>
<control axis="/controls/mixture[0]" value="1.0"/>
<control axis="/controls/flaps" value="0.0"/>
</cruise>
<cockpit x="-1.88" y=".33" z="0.6"/>
<fuselage ax="-.17" ay="0" az="-.51" bx="-7.16" by="0" bz=".17" width="1"/>
<!-- Extra fuselage to handle the "bulge" at the front -->
<fuselage ax="-1.36" ay="0" az=".17" bx="-4.09" by="0" bz=".17" width="1"/>
<wing x="-2.47" y=".51" z=".68" taper=".78"
length="5.37" chord="1.54" sweep="0" dihedral="0" camber="0.1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end=".38" lift="1.6" drag="2.0"/>
<flap1 start=".78" end="1" lift="1.5" drag="1.6"/>
<control axis="/controls/flaps" output="FLAP0"/>
<control axis="/controls/aileron" output="FLAP1" split="true"/>
</wing>
<hstab x="-7.16" y="0.08" z=".17" taper=".63" effectiveness="2"
length="1.71" chord="1.36" sweep="0">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.8"/>
<control axis="/controls/elevator" output="FLAP0"/>
<control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>
<vstab x="-7.16" y="0" z=".17" taper=".5" effectiveness="3"
length="1.71" chord="1.54" sweep="20">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
<control axis="/controls/rudder" output="FLAP0" invert="true" square="true"/>
</vstab>
<propeller radius="1.0"
cruise-speed="86" cruise-rpm="2200"
cruise-alt="10000" cruise-power="99"
takeoff-power="180" takeoff-rpm="2500"
eng-power="180" eng-rpm="2500"
x="-.6" y="0" z="0" mass="400" moment="11">
<actionpt x="0" y="0" z="0"/>
<control axis="/controls/throttle[0]" output="THROTTLE"/>
<control axis="/controls/mixture[0]" output="MIXTURE"/>
</propeller>
<gear x="-1" y="0" z="-1.5" compression=".4"> <!-- nose -->
<control axis="/controls/rudder" output="STEER"/>
</gear>
<gear x="-2.73" y="1.15" z="-1.36" compression=".3"> <!-- left main -->
<control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<gear x="-2.73" y="-1.15" z="-1.36" compression=".3"> <!-- left main -->
<control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>
<tank x="-2.47" y="1.36" z=".68" capacity="75"/>
<tank x="-2.47" y="-1.36" z=".68" capacity="75"/>
<ballast x="-2.0" y=".33" z="0" mass="180"/> <!-- pilot -->
<ballast x="-2.0" y="-.33" z="0" mass="180"/> <!-- passenger -->
<ballast x="-1.0" y="-.33" z="0" mass="200"/> <!-- cockpit -->
</airplane>

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Aircraft-yasim/c310.xml Normal file
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<airplane mass="3903">
<approach speed="70" aoa="16">
<control axis="/controls/throttle[0]" value="0.4"/>
<control axis="/controls/throttle[1]" value="0.4"/>
<control axis="/controls/mixture[0]" value="1.0"/>
<control axis="/controls/mixture[1]" value="1.0"/>
<control axis="/controls/propellor-pitch[0]" value="0.5"/>
<control axis="/controls/propellor-pitch[1]" value="0.5"/>
<control axis="/controls/flaps" value="1.0"/>
</approach>
<cruise speed="223" alt="20000">
<control axis="/controls/throttle[0]" value="1.0"/>
<control axis="/controls/throttle[1]" value="1.0"/>
<control axis="/controls/mixture[0]" value="1.0"/>
<control axis="/controls/mixture[1]" value="1.0"/>
<control axis="/controls/propellor-pitch[0]" value="1.0"/>
<control axis="/controls/propellor-pitch[1]" value="1.0"/>
<control axis="/controls/flaps" value="0.0"/>
</cruise>
<cockpit x="-2.78" y="0.26" z="0.95"/>
<fuselage ax="0.00" ay="0" az="0"
bx="-9.50" by="0" bz="0" width="0.8"/>
<wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68"
sweep="0" dihedral="5" taper="0.8" camber="0.1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end=".5" lift="1.5" drag="2.0"/>
<flap1 start=".55" end=".94" lift="1.3" drag="1.5"/>
<control axis="/controls/flaps" output="FLAP0"/>
<control axis="/controls/aileron" output="FLAP1" split="true"/>
</wing>
<hstab x="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24"
sweep="0" dihedral="0" taper="0.6" camber="0.1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.8"/>
<control axis="/controls/elevator" output="FLAP0"/>
<control axis="/controls/elevator-trim" output="FLAP0"/>
</hstab>
<vstab x="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61"
sweep="36" taper="0.5">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
<control axis="/controls/rudder" output="FLAP0" invert="true" square="true"/>
</vstab>
<!-- Late model 310's had 50 gallon tip tanks, and 31.5 gallon wing
tanks. Some also had nacelle tanks, but those aren't modeled
here -->
<tank x="-3.62" y="5.30" z="0.44" capacity="300"/>
<tank x="-3.62" y="1.02" z="-0.15" capacity="189"/>
<tank x="-3.62" y="-1.02" z="-0.15" capacity="189"/>
<tank x="-3.62" y="-5.30" z="0.44" capacity="300"/>
<gear x="0.00" y="0.00" z="-1.35" compression=".5" retract-time="7">
<control axis="/controls/rudder" output="STEER"/>
</gear>
<gear x="-4.02" y="1.32" z="-1.35" compression=".5" retract-time="7">
<control axis="/controls/brakes[0]" output="BRAKE"/>
</gear>
<gear x="-4.02" y="-1.32" z="-1.35" compression=".5" retract-time="7">
<control axis="/controls/brakes[1]" output="BRAKE"/>
</gear>
<propeller x="-2.56" y="1.83" z="0.07"
mass="800" moment="20" radius="1.0"
eng-power="285" eng-rpm="2700"
turbo-mul="2" wastegate-mp="40"
cruise-power="157" cruise-speed="195"
cruise-rpm="2100" cruise-alt="20000"
min-rpm="1600" max-rpm="2700">
<actionpt x="-1.53" y="1.83" z="0.07"/>
<control axis="/controls/throttle[0]" output="THROTTLE"/>
<control axis="/controls/mixture[0]" output="MIXTURE"/>
<control axis="/controls/propellor-pitch[0]" output="ADVANCE"/>
</propeller>
<propeller x="-2.56" y="-1.83" z="0.07"
mass="800" moment="20" radius="1.0"
eng-power="285" eng-rpm="2700"
turbo-mul="2" wastegate-mp="40"
cruise-power="157" cruise-speed="195"
cruise-rpm="2100" cruise-alt="10000"
min-rpm="1600" max-rpm="2700">
<actionpt x="-1.53" y="-1.83" z="0.07"/>
<control axis="/controls/throttle[1]" output="THROTTLE"/>
<control axis="/controls/mixture[1]" output="MIXTURE"/>
<control axis="/controls/propellor-pitch[1]" output="ADVANCE"/>
</propeller>
<ballast x="-2.78" y="0.26" z="0.0" mass="180"/> <!-- pilot -->
<ballast x="-8.5" y="0" z="0" mass="-150"/>
<ballast x="-7" y="0" z="0" mass="-300"/>
<weight x="-4.24" y="0" z="0" mass-prop="/yasim/c310/passenger-lbs"/>
</airplane>