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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
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<!--
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# Copyright (c) A3XX Development Team #
#######################################
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-->
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<fdm_config name= "A320family" version= "2.0" release= "BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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<fileheader >
<author > Joshua Davidson (it0uchpods)</author>
<version > Pre V1.0</version>
<description > A3XX FDE</description>
</fileheader>
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<metrics >
<wingarea unit= "FT2" > 1319.79 </wingarea>
<wingspan unit= "FT" > 111.26 </wingspan>
<wing_incidence > 1.03 </wing_incidence>
<chord unit= "FT" > 13.76 </chord>
<htailarea unit= "FT2" > 334.24 </htailarea>
<htailarm unit= "FT" > 57.88 </htailarm>
<vtailarea unit= "FT2" > 248.79 </vtailarea>
<vtailarm unit= "FT" > 57.33 </vtailarm>
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<location name= "AERORP" unit= "IN" >
<x > 690.00 </x>
<y > 0 </y>
<z > 0.00 </z>
</location>
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<location name= "EYEPOINT" unit= "IN" >
<x > 80 </x>
<y > -30 </y>
<z > 70 </z>
</location>
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<location name= "VRP" unit= "IN" >
<x > 661.1 </x>
<y > 0 </y>
<z > -37 </z>
</location>
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</metrics>
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<mass_balance >
<ixx unit= "SLUG*FT2" > 611903</ixx>
<iyy unit= "SLUG*FT2" > 1735389</iyy>
<izz unit= "SLUG*FT2" > 2301293</izz>
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<ixy unit= "SLUG*FT2" > 0</ixy>
<ixz unit= "SLUG*FT2" > 0</ixz>
<iyz unit= "SLUG*FT2" > 0</iyz>
<emptywt unit= "LBS" > 80431</emptywt>
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<location name= "CG" unit= "IN" >
<x > 656.00 </x>
<y > 0 </y>
<z > 0.00 </z>
</location>
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<pointmass name= "Cockpit Crew" >
<weight unit= "LBS" > 400</weight>
<!-- MAX: 400lbs, two pilots -->
<location name= "POINTMASS" unit= "IN" >
<x > 200</x>
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
<pointmass name= "Engine 1" >
<weight unit= "LBS" > 5200.7</weight>
<location name= "POINTMASS" unit= "IN" >
<x > 530.86</x>
<y > -5.755</y>
<z > -78.56019</z>
</location>
</pointmass>
<pointmass name= "Engine 2" >
<weight unit= "LBS" > 5200.7</weight>
<location name= "POINTMASS" unit= "IN" >
<x > 530.86</x>
<y > 5.755</y>
<z > -78.56019</z>
</location>
</pointmass>
<pointmass name= "PAX 0A (60 seats)" >
<weight unit= "LBS" > 6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 470.1711</x>
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
<pointmass name= "PAX 0B (60 seats)" >
<weight unit= "LBS" > 6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 809.5669</x>
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
<pointmass name= "PAX 0C (54 seats)" >
<weight unit= "LBS" > 5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 1163.2729</x>
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
<pointmass name= "Cargo Hold 1" >
<weight unit= "LBS" > 2000</weight>
<!-- MAX: 7500.126lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 383.4792</x>
<y > 0</y>
<z > -29.5</z>
<!-- 1.5m and now half of it for the center point of the load -->
</location>
</pointmass>
<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
<pointmass name= "Cargo Hold 3" >
<weight unit= "LBS" > 2000</weight>
<!-- MAX: 5384.414lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 849.1324</x>
<y > 0</y>
<z > -29.5</z>
</location>
</pointmass>
<pointmass name= "Cargo Hold 4" >
<weight unit= "LBS" > 1500</weight>
<!-- MAX: 4651.754lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 931.0653</x>
<y > 0</y>
<z > -29.5</z>
</location>
</pointmass>
<pointmass name= "Cargo Hold 5" >
<weight unit= "LBS" > 2000</weight>
<!-- MAX: 3300.320lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 1068.2634</x>
<y > 0</y>
<z > 0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
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</mass_balance>
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<ground_reactions >
<!-- REF - 1 page 165 + 271 -->
<contact type= "BOGEY" name= "NOSE_LG" >
<location unit= "IN" >
<x > 197.6772 </x>
<y > 0 </y>
<z > -137.9617 </z>
</location>
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 30935.5 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 16978.5 </damping_coeff>
<max_steer unit= "DEG" > 70 </max_steer>
<!-- REF - 1 page 133 -->
<brake_group > NOSE </brake_group>
<retractable > 1</retractable>
</contact>
<contact type= "BOGEY" name= "LEFT_MLG" >
<location unit= "IN" >
<!-- <x> 699.9243 </x> -->
<x > 695.3149 </x>
<y > -149.4094 </y>
<z > -150.4824 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction? -->
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 59785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 23957 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > LEFT </brake_group>
<retractable > 1</retractable>
</contact>
<contact type= "BOGEY" name= "RIGHT_MLG" >
<location unit= "IN" >
<!-- <x> 697.3425 </x> It should be right left simetric
<x > 699.9243 </x> -->
<x > 695.3149 </x>
<y > 149.4094 </y>
<z > -150.4824 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction? -->
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<!-- spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 33957 </damping_coeff-->
<spring_coeff unit= "LBS/FT" > 59785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 23957 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > RIGHT </brake_group>
<retractable > 1</retractable>
</contact>
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<contact type= "STRUCTURE" name= "NOSE_1" >
<location unit= "IN" >
<x > 37.7953 </x>
<y > 0 </y>
<z > -38.1374 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "NOSE_2" >
<location unit= "IN" >
<x > 128.1102 </x>
<y > 0 </y>
<z > -55.0271 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "CENTER_1" >
<location unit= "IN" >
<x > 274.0157 </x>
<y > 0 </y>
<z > -60.0665 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "CENTER_2" >
<location unit= "IN" >
<x > 930 </x>
<y > 0 </y>
<z > -60.0665 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
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<contact type= "STRUCTURE" name= "ENG_1" >
<location unit= "IN" >
<x > 589.735</x>
<y > -226.575</y>
<z > -95.567</z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "ENG_2" >
<location unit= "IN" >
<x > 589.735</x>
<y > 226.575</y>
<z > -95.567</z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
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<contact type= "STRUCTURE" name= "TAIL_1" >
<location unit= "IN" >
<x > 1097.9921 </x>
<y > 0 </y>
<z > -44.7722 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_2" >
<location unit= "IN" >
<x > 1225 </x>
<y > 0 </y>
<z > -18.8067 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_3" >
<location unit= "IN" >
<x > 1341.6142 </x>
<y > 0 </y>
<z > -10.2599 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_4" >
<location unit= "IN" >
<x > 1469.0945 </x>
<y > 0 </y>
<z > 47.4138 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 1 </dynamic_friction>
<rolling_friction > 1 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "WING_TIP_1" >
<location unit= "IN" >
<x > 838.8898 </x>
<y > -667.5197 </y>
<z > 35.7926 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "WING_TIP_2" >
<location unit= "IN" >
<x > 838.8898 </x>
<y > 667.5197 </y>
<z > 35.7926 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 1 </dynamic_friction>
<rolling_friction > 1 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
</ground_reactions>
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<propulsion >
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<engine file= "cfm56_5b6" >
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<location unit= "IN" >
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<x > 620.0683 </x>
<y > -226.575 </y>
<z > -45.567 </z>
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</location>
<orient unit= "DEG" >
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<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > 1 </yaw>
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</orient>
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<feed > 7</feed>
<thruster file= "direct" >
<location unit= "IN" >
<x > 655.4820 </x>
<y > -226.575 </y>
<z > 0.000 </z>
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > 1 </yaw>
</orient>
</thruster>
</engine>
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<engine file= "cfm56_5b6" >
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<location unit= "IN" >
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<x > 620.0683 </x>
<y > 226.575 </y>
<z > -45.567 </z>
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</location>
<orient unit= "DEG" >
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<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > -1 </yaw>
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</orient>
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<feed > 8</feed>
<thruster file= "direct" >
<location unit= "IN" >
<x > 655.4820 </x>
<y > 226.575 </y>
<z > 0.000 </z>
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > -1 </yaw>
</orient>
</thruster>
</engine>
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<tank type= "FUEL" > <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
<location unit= "IN" >
<x > 783.0709 </x>
<y > -574.4148 </y>
<z > 3.1080 </z>
</location>
<capacity unit= "LBS" > 412 </capacity> <!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
<contents unit= "LBS" > 0 </contents>
<priority > 4</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Left Tank (Outer) 1 -->
<location unit= "IN" >
<x > 739.5669 </x>
<y > -457.4259 </y>
<z > -8.0898 </z>
</location>
<capacity unit= "LBS" > 1520.00 </capacity> <!-- need review -->
<contents unit= "LBS" > 1520 </contents> <!-- outer filled first than inner -->
<standpipe unit= "LBS" > 21</standpipe> <!-- minimun fuel on pipes -->
<priority > 2</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Left Tank (Inner) 2 -->
<location unit= "IN" >
<x > 652.5591 </x>
<y > -236.2992 </y>
<z > -33.9470 </z>
</location>
<capacity unit= "LBS" > 11982 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 4480 </contents>
<standpipe unit= "LBS" > 31</standpipe> <!-- minimun fuel on pipes -->
<priority > 3</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Center Tank 3 -->
<location unit= "IN" >
<x > 522.0473 </x>
<y > 0 </y>
<z > -47.0 </z>
</location>
<capacity unit= "LBS" > 14281 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 0 </contents> <!-- wing tanks always filled first -->
<standpipe unit= "LBS" > 43</standpipe> <!-- minimun fuel on pipes -->
<priority > 1</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Right Tank (Inner) 4 -->
<location unit= "IN" >
<x > 652.5591 </x>
<y > 236.2992 </y>
<z > -33.9470 </z>
</location>
<capacity unit= "LBS" > 11982 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 4480 </contents>
<standpipe unit= "LBS" > 31</standpipe> <!-- minimum fuel on pipes -->
<priority > 3</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Right Tank (Outer) 5 -->
<location unit= "IN" >
<x > 739.5669 </x>
<y > 457.4259 </y>
<z > -8.0898 </z>
</location>
<capacity unit= "LBS" > 1520 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 1520 </contents> <!-- outer filled before inner -->
<standpipe unit= "LBS" > 21</standpipe> <!-- minimun fuel on pipes -->
<priority > 2</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
<location unit= "IN" >
<x > 783.0709 </x>
<y > 574.4148 </y>
<z > 3.1080 </z>
</location>
<capacity unit= "LBS" > 412 </capacity> <!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
<contents unit= "LBS" > 0 </contents>
<priority > 4</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
<tank type= "FUEL" > <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
<location unit= "IN" >
<x > 589.735</x>
<y > 0</y>
<z > -45.567</z>
</location>
<capacity unit= "LBS" > 100 </capacity> <!-- need review -->
<contents unit= "LBS" > 0 </contents>
<priority > 1</priority>
<type > JET-A1</type>
</tank>
<tank type= "FUEL" > <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
<location unit= "IN" >
<x > 589.735</x>
<y > 0</y>
<z > -45.567</z>
</location>
<capacity unit= "LBS" > 100 </capacity> <!-- need review -->
<contents unit= "LBS" > 0 </contents>
<priority > 1</priority>
<type > JET-A1</type>
</tank>
</propulsion>
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<system file= "pushback" />
<system file= "fuel" />
<system file= "glass-effect1" />
<system file= "fmgc" />
<system file= "fcs" />
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<flight_control name= "none" />
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<aerodynamics file= "Systems/a319-aerodynamics.xml" />
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<external_reactions >
<force name= "pushback" frame= "BODY" >
<location unit= "IN" >
<x > 294</x>
<y > 0</y>
<z > -149</z>
</location>
<direction >
<x > 1</x>
<y > 0</y>
<z > 0</z>
</direction>
</force>
</external_reactions>
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</fdm_config>
