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IDG-A32X/A320-100-CFM.xml

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A32X: New A320-100 with Old style GPWS, fix FMGC speeds
2017-06-19 02:53:08 +00:00
<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<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">
<fileheader>
<author>Joshua Davidson (it0uchpods)</author>
<version>Pre V1.0</version>
<description>A3XX FDE</description>
</fileheader>
<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>
<!-- location name="AERORP" unit="IN">
<x> 642.122 </x>
<y> 0 </y>
<z> -25.2091 </z>
</location -->
<location name="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
<z> 0.00 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 80 </x>
<y> -30 </y>
<z> 70 </z>
</location>
<location name="VRP" unit="IN">
<x> 661.1 </x>
<y> 0 </y>
<z> -37 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 611903 </ixx>
<iyy unit="SLUG*FT2"> 1735389 </iyy>
<izz unit="SLUG*FT2"> 2301293 </izz>
<!--
___________________A320_________A330__________A340
BOW_____________178000________270000________283925
SPAN______________144___________198___________209
LENGTH____________153___________209___________209
ROLL MOI_________1725000______5727777_______10613448
PITCH MOI________2550000______19040141_______13904249
YAW MOI_________3950000______23089847_______24848934
<ixx unit="SLUG*FT2"> 2262183 </ixx>
<iyy unit="SLUG*FT2"> 3172439 </iyy>
<izz unit="SLUG*FT2"> 3337024 </izz>
<ixx unit="SLUG*FT2">1725000</ixx>
<iyy unit="SLUG*FT2">2550000</iyy>
<izz unit="SLUG*FT2">3950000</izz> -->
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- location name="CG" unit="IN">
<! - -x> 642.122 </x- - >
<x> 650.122 </x><! - - At zero load of fuel and cargo/pax the CG goes to 642 - - >
<y> 0 </y>
<z> -41.7398 </z>
</location -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
<z> 0.00 </z>
</location>
<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="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</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>
</mass_balance>
<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> NONE </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>
<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>
<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>
<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>
<propulsion>
<engine file="cfm56_5a1">
<location unit="IN">
<x> 620.0683 </x>
<y> -226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
<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>
<engine file="cfm56_5a1">
<location unit="IN">
<x> 620.0683 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
<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>
<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><!-- 1 percent of total capacity, needs 20C to be filled -->
<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><!-- correct by FCOM -->
<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 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><!-- need review -->
<contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
<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><!-- 1 percent of total fuel capacity, needs 20C-->
<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>-226.575</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>226.575</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>
<system file="pushback" />
<system file="fuel" />
<system file="glass-effect1" />
<system file="it-fbw" />
<system file="fmgc" />
<system file="fcs" />
<flight_control name="none"/>
<aerodynamics file="Systems/a320-aerodynamics.xml" />
<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>
</fdm_config>
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