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A330-343.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="A330-343" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author>Narendran Muraleedharan</author>
<email>[email protected]</email>
<filecreationdate>2012-06-16</filecreationdate>
<version>2.0</version>
<description>Airbus A330-343 (A330-300 with Rolls Royce Trent 772B-60 Engines)</description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 3892.00 </wingarea>
<wingspan unit="FT" > 197.83 </wingspan>
<wing_incidence> 1.03 </wing_incidence>
<chord unit="FT" > 31.03 </chord>
<htailarea unit="FT2"> 222.16 </htailarea>
<htailarm unit="FT" > 107.29 </htailarm>
<vtailarea unit="FT2"> 496.25 </vtailarea>
<vtailarm unit="FT" > 0.00 </vtailarm>
<location name="AERORP" unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="VRP" unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 7675399 </ixx>
<iyy unit="SLUG*FT2"> 1904014 </iyy>
<izz unit="SLUG*FT2"> 2308984 </izz>
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS"> 274000 </emptywt>
<location name="CG" unit="IN">
<x> -95 </x>
<y> 0 </y>
<z> -60 </z>
</location>
<pointmass name="Crew">
<weight unit="LBS">1080</weight>
<location name="POINTMASS" unit="IN">
<x>-235.2</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="PAX">
<weight unit="LBS">41000</weight>
<location name="POINTMASS" unit="IN">
<x>110.936</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="Fwd Cargo">
<weight unit="LBS">3000</weight>
<location name="POINTMASS" unit="IN">
<x>-538.216</x>
<y>0</y>
<z>-52.13</z>
</location>
</pointmass>
<pointmass name="Aft Cargo">
<weight unit="LBS">3000</weight>
<location name="POINTMASS" unit="IN">
<x>120</x>
<y>0</y>
<z>-59.05</z>
</location>
</pointmass>
<pointmass name="Rear Bulk Cargo">
<weight unit="LBS">6500</weight>
<location name="POINTMASS" unit="IN">
<x>617</x>
<y>0</y>
<z>-59.05</z>
</location>
</pointmass>
<pointmass name="Engine1">
<weight unit="LBS">9820</weight>
<location name="POINTMASS" unit="IN">
<x>-45.31</x>
<y>-370.36</y>
<z>-97.71</z>
</location>
</pointmass>
<pointmass name="Engine2">
<weight unit="LBS">9280</weight>
<location name="POINTMASS" unit="IN">
<x>-45.31</x>
<y>370.36</y>
<z>-97.71</z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE_LG">
<location unit="IN">
<x> -736.92 </x>
<y> 0 </y>
<z> -215.91 </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"> 48124 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 38900 </damping_coeff>
<max_steer unit="DEG"> 50 </max_steer>
<brake_group> NONE </brake_group>
<retractable>1</retractable>
</contact>
<!-- I put 2 gear configs for each main gear to help with the gear base angle animation, so I dividded spring and damping coeffs into 2 for each (hope this works well) -->
<contact type="BOGEY" name="LEFT_MLG1">
<location unit="IN">
<x> 192.92 </x>
<y> -216.932 </y>
<z> -222.61 </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"> 35785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 30957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MLG1">
<location unit="IN">
<x> 192.92 </x>
<y> 216.932 </y>
<z> -222.61 </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"> 35785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 30957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MLG2">
<location unit="IN">
<x> 266.74 </x>
<y> -216.932 </y>
<z> -210.79 </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"> 35785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 30957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MLG2">
<location unit="IN">
<x> 266.74 </x>
<y> 216.932 </y>
<z> -210.79 </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"> 35785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 30957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="STRUCTURE" name="NOSE">
<location unit="IN">
<x> -848 </x>
<y> 0 </y>
<z> -85.104 </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>-71.71</x>
<y>-377.45</y>
<z>-167.84</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>-71.71</x>
<y>377.45</y>
<z>-167.84</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">
<location unit="IN">
<x> 923.65 </x>
<y> 0 </y>
<z> -70.53 </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_1">
<location unit="IN">
<x> 545.69 </x>
<y> -1135.51 </y>
<z> 35.06 </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> 545.69 </x>
<y> 1135.51 </y>
<z> 35.06 </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="cf6-80e1">
<location unit="IN">
<x>-45.31</x>
<y>-370.36</y>
<z>-97.71</z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
<!-- <feed>1</feed>
<feed>2</feed>
<feed>3</feed>
<feed>4</feed>
<feed>5</feed> -->
<feed>7</feed>
<thruster file="direct">
<location unit="IN">
<x>-45.31</x>
<y>-370.36</y>
<z>-97.71</z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
</thruster>
</engine>
<engine file="cf6-80e1">
<location unit="IN">
<x>-45.31</x>
<y>370.36</y>
<z>-97.71</z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
<!-- <feed>1</feed>
<feed>2</feed>
<feed>3</feed>
<feed>4</feed>
<feed>5</feed> -->
<feed>8</feed>
<thruster file="direct">
<location unit="IN">
<x>-45.31</x>
<y>370.36</y>
<z>-97.71</z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
</thruster>
</engine>
<!-- Main and Trimmer Tank Quantities from http://www.smartcockpit.com/pdf/plane/airbus/A330/systems/0011/ -->
<tank type="FUEL"> <!-- Left Tank (Vent) -->
<location unit="IN">
<x> 479.50 </x>
<y> -1022.04 </y>
<z> 32.72 </z>
</location>
<capacity unit="LBS"> 800 </capacity> <!-- Needs to be reviewed -->
<contents unit="LBS"> 0 </contents>
<priority>0</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Left Tank (Outer) -->
<location unit="IN">
<x> 364.45 </x>
<y> -761.21 </y>
<z> 11.82 </z>
</location>
<capacity unit="LBS"> 6317 </capacity>
<contents unit="LBS"> 3000 </contents>
<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) -->
<location unit="IN">
<x> 167.06 </x>
<y> -316.38 </y>
<z> -19.70 </z>
</location>
<capacity unit="LBS"> 60686 </capacity>
<contents unit="LBS"> 30000 </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 -->
<location unit="IN">
<x> 167.06 </x>
<y> 0 </y>
<z> -53.58 </z>
</location>
<capacity unit="LBS"> 60925 </capacity>
<contents unit="LBS"> 35000 </contents>
<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) -->
<location unit="IN">
<x> 167.06 </x>
<y> 316.38 </y>
<z> -19.70 </z>
</location>
<capacity unit="LBS"> 60686 </capacity>
<contents unit="LBS"> 30000 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<priority>3</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Right Tank (Outer) -->
<location unit="IN">
<x> 364.45 </x>
<y> 761.21 </y>
<z> 11.82 </z>
</location>
<capacity unit="LBS"> 6317 </capacity>
<contents unit="LBS"> 3000 </contents>
<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 (Vent) -->
<location unit="IN">
<x> 479.50 </x>
<y> 1022.04 </y>
<z> 32.72 </z>
</location>
<capacity unit="LBS"> 800 </capacity> <!-- Needs to be reviewed -->
<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>75.65</x>
<y>-365.24</y>
<z>-27.58</z>
</location>
<capacity unit="LBS"> 700 </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>75.65</x>
<y>365.24</y>
<z>-27.58</z>
</location>
<capacity unit="LBS"> 700 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>1</priority>
<type>JET-A1</type>
</tank>
</propulsion>
<system file="pushback" />
<system file="a333-fuel" />
<flight_control name="FCS: A333">
<channel name="Pitch">
<summer name="Pitch Trim Sum">
<input>fcs/elevator-fbw-output</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-fbw-output</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">
<!-- Testing on Ground steering Rudder bug
<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> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min> -0.25 </min>
<max> 0.25 </max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper Rate">
<input>velocities/r-aero-rad_sec</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.00
60 2.00
</tableData>
</table>
</scheduled_gain>
<scheduled_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.00
60 0.00
</tableData>
</table>
</scheduled_gain>
<summer name="Yaw Damper Sum">
<input>fcs/yaw-damper-beta</input>
<input>fcs/yaw-damper-rate</input>
<clipto>
<min> -0.1 </min>
<max> 0.1 </max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper Final">
<input>fcs/yaw-damper-sum</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.0
31 1.0
</tableData>
</table>
</scheduled_gain>
<summer name="Rudder Sum">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-final</input>
<clipto>
<min> -1 </min>
<max> 1 </max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<range>
<min> -0.35 </min>
<max> 0.35 </max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="rudder normalization">
<input>fcs/rudder-pos-rad</input>
<domain>
<min> -0.35 </min>
<max> 0.35 </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>
<channel name="Tiller">
<switch name="/controls/gear/tiller-disabled">
<default value="0"/>
<test logic="AND" value="1">
/controls/gear/tiller-enabled == 0
</test>
</switch>
<fcs_function name="Nose Wheel Steering 0">
<function name="fcs/steer-nose-deg[0]">
<description>Steering command for nose gear</description>
<sum>
<product>
<table>
<independentVar lookup="row">/controls/gear/tiller-cmd-norm</independentVar>
<independentVar lookup="column">/controls/flight/rudder</independentVar>
<tableData>
-1 0 1
-1 -70 -70 -70
0 -7 0 7
1 70 70 70
</tableData>
</table>
<property>/controls/gear/tiller-enabled</property>
</product>
<product>
<product>
<property>/controls/flight/rudder</property>
<value>70</value>
</product>
<property>/controls/gear/tiller-disabled</property>
</product>
</sum>
</function>
</fcs_function>
<!-- simulate rotational friction -->
<actuator name="Gear Nose Actuator">
<input>fcs/steer-nose-deg[0]</input>
<rate_limit>70</rate_limit>
<output>fcs/steer-pos-deg[0]</output>
</actuator>
</channel>
</flight_control>
<aerodynamics>
<function name="aero/function/kCDge">
<description>Change_in_drag_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 0.4800
0.1000 0.5150
0.1500 0.6290
0.2000 0.7090
0.3000 0.8150
0.4000 0.8820
0.5000 0.9280
0.6000 0.9620
0.7000 0.9880
0.8000 1.0000
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<function name="aero/function/kCLge">
<description>Change_in_lift_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 1.3030
0.1000 1.1270
0.1500 1.0900
0.2000 1.0730
0.3000 1.0460
0.4000 1.0550
0.5000 1.0190
0.6000 1.0130
0.7000 1.0080
0.8000 1.0060
0.9000 1.0030
1.0000 1.0020
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<axis name="LIFT">
<function name="aero/force/Lift_gain">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.30</value>
</product>
</function>
<!--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/force/Lift_alpha">
<description>Lift_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</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 0.2500
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>-->
<function name="aero/force/Lift_elevator">
<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>0.2530</value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_zero_lift">
<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