IDG-A32X/A320-200-IAE.xml

<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>

<!--
##############################################################
# Copyright (c) A3XX Development Team - All Rights Reserved. #
##############################################################
-->

<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> 690.00 </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>

		<ixy unit="SLUG*FT2">0</ixy>
		<ixz unit="SLUG*FT2">0</ixz>
		<iyz unit="SLUG*FT2">0</iyz>
		<emptywt unit="LBS">80431</emptywt>

		<location name="CG" unit="IN">
			<x> 656.00 </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="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>


	</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> 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>

		<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="v2527_a5">
		<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="v2527_a5">
		<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>0</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>0</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>

	<system file="pushback" />
	<system file="fuel" />
	<system file="glass-effect1" />
	<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>