jsbsim.js
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JSBSim flight dynamics model ported to JavaScript
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text/xml
<fdm_config name="f15" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Erik Hofman </author>
<filecreationdate> 2005-01-01 </filecreationdate>
<version> $Revision: 1.31 $ </version>
<description> McDonnell Douglas F-15 Eagle </description>
<note>
This model was created using publicly available data, publicly available
technical reports, textbooks, and guesses. It contains no proprietary or
restricted data. If this model has been validated at all, it would be
only to the extent that it seems to "fly right", and that it possibly
complies with published, publicly known, performance data (maximum speed,
endurance, etc.). Thus, this model is meant for educational and entertainment
purposes only.
This simulation model is not endorsed by the manufacturer. This model is not
to be sold.
</note>
</fileheader>
<metrics>
<wingarea unit="FT2"> 608 </wingarea>
<wingspan unit="FT"> 42.83 </wingspan>
<chord unit="FT"> 15.95 </chord>
<htailarea unit="FT2"> 45.01 </htailarea>
<htailarm unit="FT"> 20 </htailarm>
<vtailarea unit="FT2"> 46.96 </vtailarea>
<vtailarm unit="FT"> 0 </vtailarm>
<location name="AERORP" unit="IN">
<x> -234.15 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> -398.45 </x>
<y> 0 </y>
<z> 37 </z>
</location>
<location name="VRP" unit="IN">
<x> -237.25 </x>
<y> 0 </y>
<z> 4.58 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 28700 </ixx>
<iyy unit="SLUG*FT2"> 165100 </iyy>
<izz unit="SLUG*FT2"> 187900 </izz>
<ixz unit="SLUG*FT2"> 520 </ixz>
<emptywt unit="LBS"> 28000 </emptywt>
<location name="CG" unit="IN">
<x> -236.39 </x>
<y> 0 </y>
<z> 4.5 </z>
</location>
<pointmass name="Pilot">
<weight unit="LBS"> 230 </weight>
<location name="POINTMASS" unit="IN">
<x> -398.45 </x>
<y> 0 </y>
<z> 20 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x> -393.2 </x>
<y> 0 </y>
<z> -89.2 </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"> 12200 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 5000 </damping_coeff>
<max_steer unit="DEG"> 5 </max_steer>
<brake_group> NONE </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="MLG_LEFT">
<location unit="IN">
<x> -187 </x>
<y> -54 </y>
<z> -85.4 </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"> 22704 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 9000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="MLG_RIGHT">
<location unit="IN">
<x> -187 </x>
<y> 54 </y>
<z> -85.4 </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"> 22704 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 9000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="WT_LEFT">
<location unit="IN">
<x> -92.2 </x>
<y> -257 </y>
<z> 10 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="WT_RIGHT">
<location unit="IN">
<x> -92.2 </x>
<y> 257 </y>
<z> 10 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="VT_LEFT">
<location unit="IN">
<x> 47.4 </x>
<y> -69.7 </y>
<z> 133.8 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="VT_RIGHT">
<location unit="IN">
<x> 47.4 </x>
<y> 69.7 </y>
<z> 133.8 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="RADOME">
<location unit="IN">
<x> -648.7 </x>
<y> 0 </y>
<z> -17 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="BELLY">
<location unit="IN">
<x> -187 </x>
<y> 0 </y>
<z> -37 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>
<propulsion>
<engine file="F100-PW-229">
<location unit="IN">
<x> 0 </x>
<y> -25.5 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>0</feed>
<feed>1</feed>
<thruster file="direct">
<location unit="IN">
<x> 50 </x>
<y> -25.5 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<engine file="F100-PW-229">
<location unit="IN">
<x> 0 </x>
<y> 25.5 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>0</feed>
<feed>1</feed>
<thruster file="direct">
<location unit="IN">
<x> 50 </x>
<y> 25.5 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<tank type="FUEL"> <!-- Tank number 0 -->
<location unit="IN">
<x> -236.39 </x>
<y> 0 </y>
<z> 4.5 </z>
</location>
<capacity unit="LBS"> 6561.5 </capacity>
<contents unit="LBS"> 2500 </contents>
</tank>
<tank type="FUEL"> <!-- Tank number 1 -->
<location unit="IN">
<x> -236.39 </x>
<y> 0 </y>
<z> 4.5 </z>
</location>
<capacity unit="LBS"> 6561.5 </capacity>
<contents unit="LBS"> 2500 </contents>
</tank>
</propulsion>
<flight_control name="FCS: f15">
<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>
<kinematic name="elevator position">
<input>fcs/pitch-trim-sum</input>
<traverse>
<setting>
<position>-1</position>
<time>0.6</time>
</setting>
<setting>
<position>1</position>
<time>0.6</time>
</setting>
</traverse>
<output>fcs/elevator-pos-norm</output>
</kinematic>
<aerosurface_scale name="elevator position">
<input>fcs/pitch-trim-sum</input>
<gain>0.01745</gain>
<domain>
<min>-1</min>
<max>1</max>
</domain>
<range>
<min>-26</min>
<max>15</max>
</range>
<output>fcs/elevator-pos-rad</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>
<kinematic name="aileron pos norm">
<input>fcs/roll-trim-sum</input>
<traverse>
<setting>
<position>-1</position>
<time>0.3</time>
</setting>
<setting>
<position>1</position>
<time>0.3</time>
</setting>
</traverse>
<output>fcs/left-aileron-pos-norm</output>
</kinematic>
<aerosurface_scale name="Left Aileron Control">
<input>fcs/aileron-pos-norm</input>
<gain>0.01745</gain>
<range>
<min>-20</min>
<max>20</max>
</range>
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron Control">
<input>fcs/aileron-pos-norm</input>
<gain>-0.01745</gain>
<range>
<min>-20</min>
<max>20</max>
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
</channel>
<channel name="Yaw">
<pure_gain name="Yaw Damper Gain">
<input>velocities/r-rad_sec</input>
<gain>-0.001745</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<input>fcs/yaw-damper-gain</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<kinematic name="rudder position">
<input>fcs/yaw-trim-sum</input>
<traverse>
<setting>
<position>-1</position>
<time>0.4</time>
</setting>
<setting>
<position>1</position>
<time>0.4</time>
</setting>
</traverse>
<output>fcs/rudder-pos-norm</output>
</kinematic>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-pos-norm</input>
<gain>0.01745</gain>
<range>
<min>-30</min>
<max>30</max>
</range>
<output>fcs/rudder-pos-rad</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>5</time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic>
</channel>
<channel name="Speedbrake">
<kinematic name="Speedbrake Control">
<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>
<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 1.0610
0.1000 1.0330
0.1500 1.0310
0.2000 1.0330
0.3000 1.0280
0.4000 1.0110
0.5000 1.0090
0.6000 1.0050
0.7000 1.0020
0.8000 1.0000
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<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 0.8100
0.1000 0.9900
0.1500 0.9500
0.2000 0.9800
0.3000 0.9900
0.4000 1.0000
0.5000 1.0400
0.6000 1.0100
0.7000 0.9900
0.8000 1.0100
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<function name="aero/function/kCmge">
<description>Change_in_pitch_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 0.9920
0.1000 0.9960
0.1500 0.9990
0.2000 0.9970
0.3000 1.0000
0.4000 1.0000
0.5000 1.0020
0.6000 1.0010
0.7000 0.9980
0.8000 0.9990
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<axis name="DRAG">
<function name="aero/coefficient/CDalpha">
<description>Drag_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.5000 1.4000
-0.4190 0.3800 0.0970
-0.2790 0.2200 0.0250
-0.1400 0.0700 0.0180
-0.0700 0.0400 0.0100
0.0000 0.0147 0.0074
0.0700 0.0400 0.0100
0.1400 0.0700 0.0180
0.2790 0.2200 0.0250
0.4190 0.3800 0.0970
0.5590 0.8000 0.2030
0.6980 1.0100 0.2570
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDi">
<description>Drag_induced</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 0.2270
-0.2620 0.0670
-0.1750 0.0480
-0.0870 0.0060
0.0000 0.0060
0.0700 0.0130
0.1400 0.0200
0.2090 0.0470
0.2790 0.0670
0.3490 0.2120
0.4190 0.2270
0.4890 0.3310
0.5590 0.4740
0.6980 0.2120
0.7850 0.9130
0.8730 0.7210
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDbeta">
<description>Drag_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/mag-beta-rad</property>
<property>aero/function/kCDge</property>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 2.5954
-0.2620 3.2686
-0.1750 3.3563
-0.0870 3.0533
0.0000 3.8228
0.0700 4.3450
0.1400 4.1909
0.2090 3.7331
0.2790 3.1268
0.3490 2.8246
0.4190 2.4657
0.4890 2.2127
0.5590 1.9317
0.6980 1.2283
0.7850 0.9522
0.8730 0.7015
</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>
<abs><property>fcs/mag-elevator-pos-rad</property></abs>
<value>0.0438</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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 -0.8594
0.0700 -0.0974
0.5590 -0.0115
0.8730 -0.3552
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CYda">
<description>Side_force_due_to_aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>-0.0012</value>
</product>
</function>
<function name="aero/coefficient/CYdr">
<description>Side_force_due_to_rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.3724</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>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.5000 1.4000
-0.3490 -0.9300 -0.2500
-0.2620 -0.8600 -0.2300
-0.1750 -0.5800 -0.1600
-0.0870 -0.2600 -0.0700
0.0000 0.0600 0.0200
0.0700 0.3000 0.0800
0.1400 0.5800 0.1600
0.2090 0.7800 0.2100
0.2790 0.8800 0.2400
0.3490 1.0100 0.2700
0.4190 1.0800 0.2900
0.4890 1.1600 0.3100
0.5590 1.1900 0.3200
0.6980 1.1700 0.3100
0.7850 1.0900 0.2900
0.8730 1.0500 0.2800
</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>0.5730</value>
</product>
</function>
<function name="aero/coefficient/CLadot">
<description>Lift_due_to_alpha_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alphadot-rad_sec</property>
<property>aero/ci2vel</property>
<value>17.2232</value>
</product>
</function>
<function name="aero/coefficient/CLq">
<description>Lift_due_to_pitch_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>velocities/q-aero-rad_sec</property>
<property>aero/ci2vel</property>
<value>-17.2232</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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 0.0286
-0.1750 -0.2292
0.0000 -0.0573
0.2090 -0.1719
0.3140 -0.1146
0.4190 -0.1719
0.6980 -0.0745
0.7850 -0.1146
0.8730 -0.1203
</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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
0.0000 -0.4000
0.3490 -0.3100
</tableData>
</table>
</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>0.0001</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>aero/alpha-rad</independentVar>
<tableData>
-0.3490 0.0172
-0.0870 0.0372
0.1400 0.0401
0.5590 0.0057
0.8730 0.0057
</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>
<value>0.0115</value>
</product>
</function>
</axis>
<axis name="PITCH">
<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>
<property>aero/function/kCmge</property>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 -1.1459
-0.2620 -0.5730
-0.1310 -0.0573
0.0000 -0.2292
0.2790 -0.5157
0.4190 -0.8594
0.5590 -0.4584
0.8730 -0.5157
</tableData>
</table>
</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>-11.8870</value>
</product>
</function>
<function name="aero/coefficient/CmM">
<description>Pitch_moment_due_to_Mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>velocities/mach</property>
<value>-0.0000</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>-4.7000</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>-0.4580</value>
</product>
</function>
</axis>
<axis name="YAW">
<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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 0.0745
0.0000 0.1776
0.3490 0.0057
0.5240 -0.0974
0.8730 -0.0286
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Cnp">
<description>Yaw_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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 0.1100
-0.0870 -0.1400
0.0000 -0.1000
0.2790 0.0100
0.4190 -0.1300
0.8730 -0.1800
</tableData>
</table>
</product>
</function>
<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>-0.4447</value>
</product>
</function>
<function name="aero/coefficient/Cnda">
<description>Yaw_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>0.0022</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>
<table>
<independentVar>aero/alpha-rad</independentVar>
<tableData>
-0.3490 -0.0688
0.8730 -0.0115
</tableData>
</table>
</product>
</function>
</axis>
</aerodynamics>
</fdm_config>