IDG-A32X/A319-100-CFM.xml

<?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_5b6">
	<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_5b6">
	<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><!-- 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>-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/a319-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>