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737-400.xml
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737-400.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="737" release="BETA" version="2.0" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Dave Culp </author>
<author> Aeromatic </author>
<author> SP-NTX (737-300 to 737-400 and new autopilot, cockpit, ...) </author>
<filecreationdate> 2006-01-04 </filecreationdate>
<version>$Revison: 1.1 $</version>
<description> Models a 737. </description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 1171.00 </wingarea>
<wingspan unit="FT"> 94.70 </wingspan>
<chord unit="FT"> 12.31 </chord>
<htailarea unit="FT2"> 348.00 </htailarea>
<htailarm unit="FT"> 48.04 </htailarm>
<vtailarea unit="FT2"> 297.00 </vtailarea>
<vtailarm unit="FT"> 44.50 </vtailarm>
<location name="AERORP" unit="IN">
<x> 610 </x>
<y> 0 </y>
<z> 24 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 80 </x>
<y> -30 </y>
<z> 70 </z>
</location>
<location name="VRP" unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 562000 </ixx>
<iyy unit="SLUG*FT2"> 1.473e+06 </iyy>
<izz unit="SLUG*FT2"> 1.894e+06 </izz>
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 8000 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS"> 72490 </emptywt>
<location name="CG" unit="IN">
<x> 624 </x>
<y> 0 </y>
<z> -40 </z>
</location>
<pointmass name="Pilot">
<weight unit="LBS"> 200.0 </weight>
<location name="POINTMASS" unit="IN">
<x> 101.5 </x>
<y> -18.88 </y>
<z> 16.52 </z>
</location>
</pointmass>
<pointmass name="Co Pilot">
<weight unit="LBS"> 200.0 </weight>
<location name="POINTMASS" unit="IN">
<x> 101.5 </x>
<y> 18.88 </y>
<z> 16.52 </z>
</location>
</pointmass>
<pointmass name="Cabin Zone 0a">
<weight unit="LBS"> 2000 </weight>
<location name="POINTMASS" unit="IN">
<x> 252 </x>
<y> 0 </y>
<z> 27.5 </z>
</location>
</pointmass>
<pointmass name="Cabin Zone 0b">
<weight unit="LBS"> 2400 </weight>
<location name="POINTMASS" unit="IN">
<x> 430 </x>
<y> 0 </y>
<z> 27.5 </z>
</location>
</pointmass>
<pointmass name="Cabin Zone 0c">
<weight unit="LBS"> 3400 </weight>
<location name="POINTMASS" unit="IN">
<x> 610 </x>
<y> 0 </y>
<z> 27.5 </z>
</location>
</pointmass>
<pointmass name="Cabin Zone 0d">
<weight unit="LBS"> 3000 </weight>
<location name="POINTMASS" unit="IN">
<x> 790 </x>
<y> 0 </y>
<z> 27.5 </z>
</location>
</pointmass>
<pointmass name="Cabin Zone 0e">
<weight unit="LBS"> 1800</weight>
<location name="POINTMASS" unit="IN">
<x> 975 </x>
<y> 0 </y>
<z> 27.5 </z>
</location>
</pointmass>
<!--cargo compartment!-->
<pointmass name="Cargo1">
<weight unit="LBS"> 763 </weight>
<location name="POINTMASS" unit="IN">
<x> 256 </x>
<y> 0 </y>
<z> -27.7 </z>
</location>
</pointmass>
<pointmass name="Cargo2">
<weight unit="LBS"> 388 </weight>
<location name="POINTMASS" unit="IN">
<x>340 </x>
<y> 0 </y>
<z> -27.7 </z>
</location>
</pointmass>
<pointmass name="Cargo3">
<weight unit="LBS"> 1131 </weight>
<location name="POINTMASS" unit="IN">
<x> 424 </x>
<y> 0 </y>
<z> -27.7 </z>
</location>
</pointmass>
<pointmass name="Cargo4">
<weight unit="LBS"> 2337 </weight>
<location name="POINTMASS" unit="IN">
<x> 748 </x>
<y> 0 </y>
<z> -27.7 </z>
</location>
</pointmass>
<pointmass name="Cargo5">
<weight unit="LBS"> 212 </weight>
<location name="POINTMASS" unit="IN">
<x> 852 </x>
<y> 0 </y>
<z> -27.7 </z>
</location>
</pointmass>
<pointmass name="Cargo6">
<weight unit="LBS"> 359 </weight>
<location name="POINTMASS" unit="IN">
<x> 956 </x>
<y> 0 </y>
<z> -23.2 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact name="Nose Gear" type="BOGEY">
<location unit="IN">
<x> 158 </x>
<y> 0 </y>
<z> -97.6 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT">240000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side>120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 35 </max_steer>
<brake_group> NONE </brake_group>
<retractable>1</retractable>
</contact>
<contact name="Left Main Gear" type="BOGEY">
<location unit="IN">
<x> 648 </x>
<y> -100 </y>
<z> -108.6 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact name="Right Main Gear" type="BOGEY">
<location unit="IN">
<x> 648 </x>
<y> 100 </y>
<z> -108.6 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact name="fuselage_belly" type="STRUCTURE">
<location unit="IN">
<x> 240 </x>
<y> 0 </y>
<z> -64.92 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact name="fuselage_nose" type="STRUCTURE">
<location unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact name="fuselage_tail1" type="STRUCTURE">
<location unit="IN">
<x> 885.32 </x>
<y> 0 </y>
<z> -57.28 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact name="fuselage_tail1" type="STRUCTURE">
<location unit="IN">
<x> 1274.8 </x>
<y> 0 </y>
<z>48 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact name="left wing tip" type="STRUCTURE">
<location unit="IN">
<x>801 </x>
<y> 572 </y>
<z> 19.5 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact name="right wing tip" type="STRUCTURE">
<location unit="IN">
<x>801 </x>
<y>-572 </y>
<z> 19.5 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.50 </rolling_friction>
<spring_coeff unit="LBS/FT"> 120000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC">20000</damping_coeff_rebound>
<relaxation_velocity>
<rolling unit="FT/SEC">0.7</rolling>
<side unit="FT/SEC">0.7</side>
</relaxation_velocity>
<force_lag_filter>
<rolling> 120.0 </rolling>
<side> 120.0 </side>
</force_lag_filter>
<wheel_slip_filter> 120.0 </wheel_slip_filter>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>
<propulsion>
<engine file="CFM56">
<location unit="IN">
<x> 540 </x>
<y> -193 </y>
<z> -40 </z>
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> -5 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>0</feed>
<feed>2</feed>
<thruster file="direct">
<location unit="IN">
<x> 540 </x>
<y> -193 </y>
<z> -40 </z>
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> -5 </pitch>
<yaw> 0 </yaw>
</orient>
</thruster>
</engine>
<engine file="CFM56">
<location unit="IN">
<x> 540 </x>
<y> 193 </y>
<z> -40 </z>
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> -5 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>1</feed>
<feed>2</feed>
<thruster file="direct">
<location unit="IN">
<x> 540 </x>
<y> 193 </y>
<z> -40 </z>
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> -5 </pitch>
<yaw> 0 </yaw>
</orient>
</thruster>
</engine>
<tank type="FUEL">
<!-- Left wing tank -->
<location unit="IN">
<x> 550</x>
<y> -80 </y>
<z> -18 </z>
</location>
<capacity unit="LBS"> 10200 </capacity>
<contents unit="LBS"> 6300 </contents>
<temperature> 59.0 </temperature>
<!-- Fuel temp in degrees F -->
</tank>
<tank type="FUEL">
<!-- Right wing tank -->
<location unit="IN">
<x> 550 </x>
<y> 80 </y>
<z> -18 </z>
</location>
<capacity unit="LBS"> 10200 </capacity>
<contents unit="LBS"> 6300 </contents>
</tank>
<tank type="FUEL">
<!-- Center tank -->
<location unit="IN">
<x> 550 </x>
<y> 0 </y>
<z> -18 </z>
</location>
<capacity unit="LBS"> 15000 </capacity>
<contents unit="LBS"> 10500 </contents>
</tank>
</propulsion>
<system file="pushback"/>
<flight_control name="FCS: 737">
<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>
<range>
<min>-0.336</min>
<max> 0.3875</max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Elevator Normalized">
<input>fcs/elevator-pos-rad</input>
<domain>
<min>-0.336</min>
<max> 0.3875</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>
<range>
<min>-0.25</min>
<max> 0.25</max>
</range>
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron Control">
<input>-fcs/roll-trim-sum</input>
<range>
<min>-0.25</min>
<max> 0.25</max>
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left aileron Normalized">
<input>fcs/left-aileron-pos-rad</input>
<domain>
<min>-0.3577924967</min>
<max> 0.2705260341</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
<aerosurface_scale name="Right aileron Normalized">
<input>fcs/right-aileron-pos-rad</input>
<domain>
<min>-0.3577924967</min>
<max> 0.2705260341</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Yaw">
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max> 1</max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper">
<input>velocities/r-aero-rad_sec</input>
<table>
<independentVar>velocities/mach</independentVar>
<tableData>
0.00 0.0
0.10 0.0
0.11 1.0
</tableData>
</table>
</scheduled_gain>
<scheduled_gain name="Yaw Damper Final">
<input>fcs/yaw-damper</input>
<table>
<independentVar>velocities/mach</independentVar>
<tableData>
0.00 0.0
0.10 0.0
0.11 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>-0.500</min>
<max> 0.500</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder Normalized">
<input>fcs/rudder-pos-rad</input>
<domain>
<min>-0.500</min>
<max> 0.500</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>0.025</position>
<time>5.7</time>
</setting>
<setting>
<position>0.050</position>
<time>12.7</time>
</setting>
<setting>
<position>0.125</position>
<time>5.7</time>
</setting>
<setting>
<position>0.25</position>
<time>5.7</time>
</setting>
<setting>
<position>0.625</position>
<time>1.5</time>
</setting>
<setting>
<position>0.750</position>
<time>2.4</time>
</setting>
<setting>
<position>0.750</position>
<time>2.4</time>
</setting>
<setting>
<position>1</position>
<time>3.3</time>
</setting>
</traverse>
<output>fcs/flap-pos-norm</output>
</kinematic>
</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>7</time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic>
</channel>
<channel name="Flight Spoilers">
<!-- operated by the speedbrake handle and roll control -->
<kinematic name="Flight Spoilers Control">
<input>fcs/speedbrake-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.6</time>
</setting>
</traverse>
<output>fcs/speedbrake-pos-norm</output>
</kinematic>
</channel>
<channel name="Ground Spoilers">
<!-- these only operate on the ground -->
<kinematic name="Ground Spoilers Control">
<input>fcs/spoiler-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.6</time>
</setting>
</traverse>
<output>fcs/spoiler-pos-norm</output>
</kinematic>
</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
</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 1.2030
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>
<function name="aero/function/kCLsb">
<description>Change_in_lift_due_to_speed_brake</description>
<product>
<table>
<independentVar>fcs/speedbrake-pos-norm</independentVar>
<tableData>
0.0000 1.0
0.1000 0.85
</tableData>
</table>
</product>
</function>
<function name="aero/function/kCLsp">
<description>Change_in_lift_due_to_spoilers</description>
<product>
<table>
<independentVar>fcs/spoiler-pos-norm</independentVar>
<tableData>
0.0000 1.0
0.1000 0.6
</tableData>
</table>
</product>
</function>
<axis name="DRAG">
<function name="aero/coefficient/CD0">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-1.57 1.5000
-0.26 0.0420
0.00 0.0210
0.26 0.0420
1.57 1.5000
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDi">
<description>Induced_drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<property>aero/function/kCDge</property>
<value>0.043</value>
</product>
</function>
<function name="aero/coefficient/CDmach">
<description>Drag_due_to_mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>velocities/mach</independentVar>
<tableData>
0.00 0.0000
0.79 0.0000
1.10 0.0230
1.80 0.0150
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDflap">
<description>Drag_due_to_flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-norm</property>
<value>0.059</value>
</product>
</function>
<function name="aero/coefficient/CDgear">
<description>Drag_due_to_gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.017</value>
</product>
</function>
<function name="aero/coefficient/CDsb">
<description>Drag_due_to_flight_spoilers</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.03</value>
</product>
</function>
<function name="aero/coefficient/CDsp">
<description>Drag_due_to_ground_spoilers</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/spoiler-pos-norm</property>
<value>0.05</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>
<table>
<independentVar>aero/beta-rad</independentVar>
<tableData>
-1.57 1.2300
-0.26 0.0500
0.00 0.0000
0.26 0.0500
1.57 1.2300
</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/elevator-pos-norm</property>
<value>0.059</value>
</product>
</function>
<function name="aero/coefficient/CDrv">
<description>Drag_due_to_reverse</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>/engines/engine/reverser-pos-norm</property>
<value>0.018</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>
<property>aero/beta-rad</property>
<value>-1</value>
</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>
<property>aero/function/kCLge</property>
<property>aero/function/kCLsb</property>
<property>aero/function/kCLsp</property>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.68
0.00 0.20
0.23 1.20
0.46 0.20
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/dCLflap">
<description>Delta_Lift_due_to_flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-norm</property>
<property>aero/function/kCLge</property>
<property>aero/function/kCLsb</property>
<property>aero/function/kCLsp</property>
<value>0.9</value>
</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>0.1</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>
<property>aero/beta-rad</property>
<value>-0.09</value>
</product>
</function>
<function name="aero/coefficient/Clp">
<description>Roll_moment_due_to_roll_rate</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>-0.4</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>0.09</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>
<table>
<independentVar>velocities/mach</independentVar>
<tableData>
0.0 0.100
2.0 0.033
</tableData>
</table>
</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>