A321-211.xml

<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="A320-211" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">

<fileheader>
	<author> Unknown </author>
	<filecreationdate> 2003-01-01 </filecreationdate>
	<version> Version </version>
	<description> Airbus A320 </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="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" >     87274 </emptywt>
	<location name="CG" unit="IN">
	<x> 642.122 </x>
	<y> 0 </y>
	<z> -41.7398 </z>
	</location>

	<pointmass name="Crew">
		<weight unit="LBS">600</weight>
		<location name="POINTMASS" unit="IN">
			<x>400</x>
			<y>0</y>
			<z>0</z>
		</location>
	</pointmass>
	<pointmass name="PAX">
		<weight unit="LBS">75500</weight>
		<location name="POINTMASS" unit="IN">
			<x>705</x>
			<y>0</y>
			<z>0</z>
		</location>
	</pointmass>
</mass_balance>

<ground_reactions>
	<contact type="BOGEY" name="NOSE_LG">
	<location unit="IN">
		<x> 29.566964</x>
		<y> 0 </y>
		<z> -137.9617 </z>
	</location>
	<static_friction> 0.5 </static_friction>
	<dynamic_friction> 0.8 </dynamic_friction>
	<rolling_friction> 0.02 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 75000 </spring_coeff>
	<damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
	<max_steer unit="DEG"> 75 </max_steer>
	<brake_group> NONE </brake_group>
	<retractable>1</retractable>
	</contact>
	<contact type="BOGEY" name="LEFT_MLG">
	<location unit="IN">
		<x> 699.9243 </x>
		<y> -149.4094 </y>
		<z> -152.6824 </z>
	</location>
	<static_friction> 0.5 </static_friction>
	<dynamic_friction> 0.8 </dynamic_friction>
	<rolling_friction> 0.02 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 180000 </spring_coeff>
	<damping_coeff unit="LBS/FT/SEC"> 33957 </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>
		<y> 149.4094 </y>
		<z> -152.6824</z>
	</location>
	<static_friction> 0.5 </static_friction>
	<dynamic_friction> 0.8 </dynamic_friction>
	<rolling_friction> 0.02 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 180000 </spring_coeff>
	<damping_coeff unit="LBS/FT/SEC"> 33957 </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> 205.905536 </x>
		<y> 0 </y>
		<z> -38.1374 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 296.220436 </x>
		<y> 0 </y>
		<z> -55.0271 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 992.87399 </x>
		<y> 0 </y>
		<z> -44.7722 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1119.88189 </x>
		<y> 0 </y>
		<z> -18.8067 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1236.49609 </x>
		<y> 0 </y>
		<z> -10.2599 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 232.59841 </x>
		<y> 0 </y>
		<z> 47.4138 </z>
	</location>
	<static_friction> 1.0 </static_friction>
	<dynamic_friction> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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> 1.4 </dynamic_friction>
	<rolling_friction> 1.0 </rolling_friction>
	<spring_coeff unit="LBS/FT"> 1.5e+06 </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_5b3">
	<location unit="IN">
		<x> 589.735 </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>0</feed>
	<feed>1</feed>
	<feed>3</feed>
	<feed>4</feed>
	<feed>5</feed>
	<thruster file="direct">
		<location unit="IN">
		<x> 589.735 </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>
	</thruster>
	</engine>
	<engine file="cfm56_5b3">
	<location unit="IN">
		<x> 589.735 </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>0</feed>
	<feed>1</feed>
	<feed>3</feed>
	<feed>4</feed>
	<feed>5</feed>
	<thruster file="direct">
		<location unit="IN">
		<x> 589.735 </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>
	</thruster>
	</engine>
	<tank type="FUEL">    <!-- Left Tank (Inner) -->
		<location unit="IN">
			<x> 630.6588 </x>
			<y> -236.2992 </y>
			<z> -33.9470 </z>
		</location>
		<capacity unit="LBS"> 12186.9 </capacity>
		<contents unit="LBS"> 2437.38 </contents>
	</tank>
	<tank type="FUEL">    <!-- Left Tank (Outer) -->
		<location unit="IN">
			<x> 737.4190 </x>
			<y> -457.4259 </y>
			<z> -8.0898 </z>
		</location>
		<capacity unit="LBS"> 1548.8 </capacity>
		<contents unit="LBS"> 154.88 </contents>
	</tank>
	<tank type="FUEL">    <!-- Left Tank (Surge) -->
		<location unit="IN">
			<x> 788.4322 </x>
			<y> -574.4148 </y>
			<z> 3.1080 </z>
		</location>
		<capacity unit="LBS"> 328.13 </capacity>
		<contents unit="LBS"> 0 </contents>
	</tank>
	<tank type="FUEL">    <!-- Center Tank -->
		<location unit="IN">
			<x> 580.9955 </x>
			<y> 0 </y>
			<z> -47.0 </z>
		</location>
		<capacity unit="LBS"> 14520 </capacity>
		<contents unit="LBS"> 0 </contents>
	</tank>
	<tank type="FUEL">    <!-- Right Tank (Inner) -->
		<location unit="IN">
			<x> 630.6588 </x>
			<y> 236.2992 </y>
			<z> -33.9470 </z>
		</location>
		<capacity unit="LBS"> 12186.9 </capacity>
		<contents unit="LBS"> 2437.38 </contents>
	</tank>
	<tank type="FUEL">    <!-- Right Tank (Outer) -->
		<location unit="IN">
			<x> 737.4190 </x>
			<y> 457.4259 </y>
			<z> -8.0898 </z>
		</location>
		<capacity unit="LBS"> 1548.8 </capacity>
		<contents unit="LBS"> 154.88 </contents>
	</tank>
	<tank type="FUEL">    <!-- Right Tank (Surge) -->
		<location unit="IN">
			<x> 788.4322 </x>
			<y> 574.4148 </y>
			<z> 3.1080 </z>
		</location>
		<capacity unit="LBS"> 328.13 </capacity>
		<contents unit="LBS"> 0 </contents>
	</tank>
</propulsion>

<system file="pushback" />

<flight_control name="FCS: A320">
	<channel name="Pitch">
	<summer name="Pitch Trim Sum">
		<input>fcs/elevator-cmd-norm</input>
		<input>fcs/pitch-trim-cmd-norm</input>
		<clipto>
		<min>-1</min>
		<max>1</max>
		</clipto>
	</summer>

	<aerosurface_scale name="Elevator Control">
		<input>fcs/pitch-trim-sum</input>
		<gain>0.018</gain>
		<range>
		<min>-30</min>
		<max>15</max>
		</range>
		<output>fcs/elevator-pos-rad</output>
	</aerosurface_scale>

	<aerosurface_scale name="Elevator position normalized">
		<input>fcs/elevator-pos-deg</input>
		<domain>
		<min>-30</min>
		<max>15</max>
		</domain>
		<range>
		<min>-1</min>
		<max>1</max>
		</range>
		<output>fcs/elevator-pos-norm</output>
	</aerosurface_scale>
	</channel>
	<channel name="Roll">
	<summer name="Roll Trim Sum">
		<input>fcs/aileron-cmd-norm</input>
		<input>fcs/roll-trim-cmd-norm</input>
		<clipto>
		<min>-1</min>
		<max>1</max>
		</clipto>
	</summer>

	<aerosurface_scale name="Left Aileron Control">
		<input>fcs/roll-trim-sum</input>
		<gain>0.02</gain>
		<range>
		<min>-25</min>
		<max>25</max>
		</range>
		<output>fcs/left-aileron-pos-rad</output>
	</aerosurface_scale>

	<aerosurface_scale name="Right Aileron Control">
		<input>-fcs/roll-trim-sum</input>
		<gain>0.02</gain>
		<range>
		<min>-25</min>
		<max>25</max>
		</range>
		<output>fcs/right-aileron-pos-rad</output>
	</aerosurface_scale>

	<aerosurface_scale name="Left Aileron position normalized">
		<input>fcs/left-aileron-pos-deg</input>
		<domain>
		<min>-25</min>
		<max>25</max>
		</domain>
		<range>
		<min>-0.75</min>
		<max>1</max>
		</range>
		<output>fcs/left-aileron-pos-norm</output>
	</aerosurface_scale>

	<aerosurface_scale name="Right Aileron position normalized">
		<input>fcs/right-aileron-pos-deg</input>
		<domain>
		<min>-25</min>
		<max>25</max>
		</domain>
		<range>
		<min>-0.75</min>
		<max>1</max>
		</range>
		<output>fcs/right-aileron-pos-norm</output>
	</aerosurface_scale>
	</channel>
	<channel name="Yaw">
	<pure_gain name="Yaw Damper Rate">
		<input>velocities/r-rad_sec</input>
		<gain>2</gain>
	</pure_gain>

	<pure_gain name="Yaw Damper Beta">
		<input>aero/beta-rad</input>
		<gain>-5</gain>
	</pure_gain>

	<summer name="Yaw Trim Sum">
		<input>fcs/rudder-cmd-norm</input>
		<input>fcs/yaw-trim-cmd-norm</input>
		<clipto>
		<min>-1</min>
		<max>1</max>
		</clipto>
	</summer>

	<summer name="Rudder Sum">
		<input>fcs/yaw-trim-sum</input>
		<input>fcs/yaw-damper-rate</input>
		<input>fcs/yaw-damper-beta</input>
		<clipto>
		<min>-1</min>
		<max>1</max>
		</clipto>
	</summer>

	<aerosurface_scale name="Rudder Control">
		<input>fcs/rudder-sum</input>
		<gain>0.01745</gain>
		<range>
		<min>-25</min>
		<max>25</max>
		</range>
		<output>fcs/rudder-pos-rad</output>
	</aerosurface_scale>

	<aerosurface_scale name="Rudder position normalized">
		<input>fcs/rudder-pos-deg</input>
		<domain>
		<min>-25</min>
		<max>25</max>
		</domain>
		<range>
		<min>-1</min>
		<max>1</max>
		</range>
		<output>fcs/rudder-pos-norm</output>
	</aerosurface_scale>
	</channel>
	<channel name="Flaps">
	<kinematic name="Flaps Control">
		<input>fcs/flap-cmd-norm</input>
		<traverse>
		<setting>
			<position>0</position>
			<time>0</time>
		</setting>
		<setting>
			<position>40</position>
			<time>40</time>
		</setting>
		</traverse>
		<output>fcs/flap-pos-deg</output>
	</kinematic>

	<aerosurface_scale name="Flap position normalized">
		<input>fcs/flap-pos-deg</input>
		<domain>
		<min>0</min>
		<max>40</max>
		</domain>
		<range>
		<min>0</min>
		<max>1</max>
		</range>
		<output>fcs/flap-pos-norm</output>
	</aerosurface_scale>
	</channel>
	<channel name="Landing Gear">
	<kinematic name="Gear Control">
		<input>gear/gear-cmd-norm</input>
		<traverse>
		<setting>
			<position>0</position>
			<time>0</time>
		</setting>
		<setting>
			<position>1</position>
			<time>10</time>
		</setting>
		</traverse>
		<output>gear/gear-pos-norm</output>
	</kinematic>
	</channel>
	<channel name="Speedbrake">
	<kinematic name="Speedbrake">
		<input>fcs/speedbrake-cmd-norm</input>
		<traverse>
		<setting>
			<position>0</position>
			<time>0</time>
		</setting>
		<setting>
			<position>1</position>
			<time>2</time>
		</setting>
		</traverse>
		<output>fcs/speedbrake-pos-norm</output>
	</kinematic>
	</channel>
</flight_control>
<aerodynamics>

	<axis name="DRAG">
	<function name="aero/coefficient/CDo">
		<description>Drag_at_zero_lift</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<value>0.016</value>
		</product>
	</function>
	<function name="aero/coefficient/CDalpha">
		<description>Drag_due_to_alpha</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<table>
			<independentVar lookup="row">aero/alpha-rad</independentVar>
			<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
			<tableData>
				0.0000	1.0000	25.0000	40.0000
			-0.0873	0.0041	0.0000	0.0005	0.0014
			-0.0698	0.0013	0.0004	0.0025	0.0041
			-0.0524	0.0001	0.0023	0.0059	0.0084
			-0.0349	0.0003	0.0057	0.0108	0.0141
			-0.0175	0.0020	0.0105	0.0172	0.0212
			0.0000	0.0052	0.0168	0.0251	0.0399
			0.0175	0.0099	0.0248	0.0346	0.0502
			0.0349	0.0162	0.0342	0.0457	0.0621
			0.0524	0.0240	0.0452	0.0583	0.0755
			0.0698	0.0334	0.0577	0.0724	0.0904
			0.0873	0.0442	0.0718	0.0881	0.1068
			0.1047	0.0566	0.0874	0.1053	0.1248
			0.1222	0.0706	0.1045	0.1240	0.1443
			0.1396	0.0860	0.1232	0.1442	0.1654
			0.1571	0.0962	0.1353	0.1573	0.1790
			0.1745	0.1069	0.1479	0.1708	0.1930
			0.1920	0.1180	0.1610	0.1849	0.2075
			0.2094	0.1298	0.1746	0.1995	0.2226
			0.2269	0.1424	0.1892	0.2151	0.2386
			0.2443	0.1565	0.2054	0.2323	0.2564
			0.2618	0.1727	0.2240	0.2521	0.2767
			0.2793	0.1782	0.2302	0.2587	0.2835
			0.2967	0.1716	0.2227	0.2507	0.2753
			0.3142	0.1618	0.2115	0.2388	0.2631
			0.3316	0.1475	0.1951	0.2214	0.2451
			0.3491	0.1097	0.1512	0.1744	0.1966
			</tableData>
		</table>
		</product>
	</function>
	<function name="aero/coefficient/CDde">
		<description>Drag_due_to_elevator_Deflection</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>fcs/mag-elevator-pos-rad</property>
		<value>0.0500</value>
		</product>
	</function>
	<function name="aero/coefficient/CDbeta">
		<description>Drag_due_to_sideslip</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>aero/mag-beta-rad</property>
		<value>0.2000</value>
		</product>
	</function>
	<function name="aero/coefficient/CDgear">
		<description>Drag_due_to_landing_gear</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>gear/gear-pos-norm</property>
		<value>0.0400</value>
		</product>
	</function>
	<function name="aero/coefficient/CDspeedbrake">
		<description>Drag_due_to_speedbrake</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>fcs/speedbrake-pos-norm</property>
		<value>0.0400</value>
		</product>
	</function>
	</axis>

	<axis name="SIDE">
	<function name="aero/coefficient/CYb">
		<description>Side_force_due_to_beta</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<table>
			<independentVar>aero/beta-rad</independentVar>
			<tableData>
			-0.3500	0.5000
			0.0000	0.0000
			0.3500	-0.5000
			</tableData>
		</table>
		</product>
	</function>
	</axis>

	<axis name="LIFT">
	<function name="aero/coefficient/CLalpha">
		<description>Lift_due_to_alpha</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<table>
			<independentVar lookup="row">aero/alpha-rad</independentVar>
			<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
			<tableData>
				0.0000	1.0000	9.0000	10.0000	40.0000
			-0.0900	-0.2200	-0.2200	-0.1200	-0.1200	0.3200
			0.0000	0.2500	0.2500	0.3500	0.3500	0.7500
			0.0900	0.7300	0.7300	0.8300	0.8300	1.2300
			0.1000	0.8300	0.8300	0.9300	0.9300	1.3300
			0.1200	0.9200	0.9200	1.0200	1.0200	1.4200
			0.1400	1.0200	1.0200	1.1200	1.1200	1.5200
			0.1600	1.0800	1.0800	1.1800	1.1800	1.5800
			0.1700	1.1300	1.1300	1.2300	1.2300	1.6300
			0.1900	1.1900	1.1900	1.2900	1.2900	1.6900
			0.2100	1.2500	1.2500	1.3500	1.3500	1.7700
			0.2400	1.3500	1.3700	1.4700	1.4800	1.9300
			0.2600	1.4400	1.4700	1.5700	1.6200	2.1200
			0.2800	1.4700	1.5100	1.6100	1.7800	2.4000
			0.3000	1.5000	1.5600	1.6600	1.9000	2.3000
			0.3200	1.4700	1.6100	1.6000	1.7000	2.0300
			0.3400	1.3500	1.5000	1.4100	1.5000	1.5300
			0.3600	1.1500	1.2000	1.2000	1.2000	1.2000
			</tableData>
		</table>
		</product>
	</function>
	<function name="aero/coefficient/CLDe">
		<description>Lift_due_to_Elevator_Deflection</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>fcs/elevator-pos-rad</property>
		<value>0.1930</value>
		</product>
	</function>
	</axis>

	<axis name="ROLL">
	<function name="aero/coefficient/Clb">
		<description>Roll_moment_due_to_beta</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<table>
			<independentVar>aero/beta-rad</independentVar>
			<tableData>
			-0.3500	0.0100
			0.0000	0.0000
			0.3500	-0.0100
			</tableData>
		</table>
		</product>
	</function>
	<function name="aero/coefficient/Clp">
		<description>Roll_moment_due_to_roll_rate_(roll_damping)</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>aero/bi2vel</property>
		<property>velocities/p-aero-rad_sec</property>
		<value>-0.5000</value>
		</product>
	</function>
	<function name="aero/coefficient/Clr">
		<description>Roll_moment_due_to_yaw_rate</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>aero/bi2vel</property>
		<property>velocities/r-aero-rad_sec</property>
		<value>0.0050</value>
		</product>
	</function>
	<function name="aero/coefficient/Clda">
		<description>Roll_moment_due_to_aileron</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>fcs/left-aileron-pos-rad</property>
		<value>0.2000</value>
		</product>
	</function>
	<function name="aero/coefficient/Cldr">
		<description>Roll_moment_due_to_rudder</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>fcs/rudder-pos-rad</property>
		<value>0.0050</value>
		</product>
	</function>
	</axis>

	<axis name="PITCH">
	<function name="aero/coefficient/Cmo">
		<description>Pitching_moment_at_zero_alpha</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/cbarw-ft</property>
		<table>
			<independentVar>fcs/flap-pos-deg</independentVar>
			<tableData>
			0.0000	0.0400
			40.0000	-0.1000
			</tableData>
		</table>
		</product>
	</function>
	<function name="aero/coefficient/Cmalpha">
		<description>Pitch_moment_due_to_alpha</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/cbarw-ft</property>
		<property>aero/alpha-rad</property>
		<value>-4.0000</value>
		</product>
	</function>
	<function name="aero/coefficient/CmDe">
		<description>Pitch_moment_due_to_elevator_Deflection</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/cbarw-ft</property>
		<property>fcs/elevator-pos-rad</property>
		<value>-1.5000</value>
		</product>
	</function>
	<function name="aero/coefficient/Cmq">
		<description>Pitch_moment_due_to_pitch_rate</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/cbarw-ft</property>
		<property>aero/ci2vel</property>
		<property>velocities/q-aero-rad_sec</property>
		<value>-10.0000</value>
		</product>
	</function>
	<function name="aero/coefficient/Cmadot">
		<description>Pitch_moment_due_to_alpha_rate</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/cbarw-ft</property>
		<property>aero/ci2vel</property>
		<property>aero/alphadot-rad_sec</property>
		<value>-12.0000</value>
		</product>
	</function>
	</axis>

	<axis name="YAW">
	<function name="aero/coefficient/Cnr">
		<description>Yaw_moment_due_to_yaw_rate</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>aero/bi2vel</property>
		<property>velocities/r-aero-rad_sec</property>
		<value>-0.0400</value>
		</product>
	</function>
	<function name="aero/coefficient/Cnb">
		<description>Yaw_moment_due_to_beta</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>aero/beta-rad</property>
		<value>0.2000</value>
		</product>
	</function>
	<function name="aero/coefficient/Cndr">
		<description>Yaw_moment_due_to_rudder</description>
		<product>
		<property>aero/qbar-psf</property>
		<property>metrics/Sw-sqft</property>
		<property>metrics/bw-ft</property>
		<property>fcs/rudder-pos-rad</property>
		<value>-0.5000</value>
		</product>
	</function>
	</axis>
</aerodynamics>

	<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>