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Loreley-B.xml
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Loreley-B.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="Loreley-B" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Peter Brendt / Aeromatic v 0.95 </author>
<filecreationdate>2014-11-18</filecreationdate>
<version>$Revision: 1.15 $</version>
<description>Loreley-B Voodoomaster</description>
</fileheader>
<!--
File: Loreley-B.xml
Inputs:
name: Loreley-B
type: two-engine transonic/supersonic fighter
max weight: 74955 lb
wing span: 48.17 ft
length: 72.83 ft
wing area: unspecified
gear type: tricycle
retractable?: yes
# engines: 2
engine type: turbine
engine layout: aft fuselage
yaw damper? yes
Outputs:
wing loading: 95.00 lb/sq-ft
payload: 22027.3 lbs
CL-alpha: 3.5 per radian
CL-0: 0.08
CL-max: 1
CD-0: 0.021
K: 0.12
-->
<metrics>
<wingarea unit="FT2"> 789.00 </wingarea>
<wingspan unit="FT" > 48.17 </wingspan>
<wing_incidence> 2.00 </wing_incidence>
<chord unit="FT" > 16.38 </chord>
<htailarea unit="FT2"> 157.80 </htailarea>
<htailarm unit="FT" > 29.13 </htailarm>
<vtailarea unit="FT2"> 94.68 </vtailarea>
<vtailarm unit="FT" > 29.13 </vtailarm>
<location name="AERORP" unit="IN">
<x> 424.38 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 174.79 </x>
<y> 0.00 </y>
<z> 36.00 </z>
</location>
<location name="VRP" unit="IN">
<x>0</x>
<y>0</y>
<z>0</z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 43563 </ixx>
<iyy unit="SLUG*FT2"> 185751 </iyy>
<izz unit="SLUG*FT2"> 175445 </izz>
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS" > 40785 </emptywt>
<location name="CG" unit="IN">
<x> 424.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
<pointmass name="Pilot">
<description>Weight of pilot</description>
<weight unit="LBS">200</weight>
<location name="POINTMASS" unit="IN">
<x> 24.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon1l">
<description>Weight on pylon 1 left</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y>-180.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon2l">
<description>Weight on pylon 2 left</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y>-150.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon3l">
<description>Weight on pylon 3 left</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y>-120.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon4l">
<description>Weight on pylon 4 left</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y>-90.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon5l">
<description>Weight on pylon 5 left</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> -60.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="PylonC">
<description>Weight on center pylon</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon5r">
<description>Weight on pylon 5 right</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 60.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon4r">
<description>Weight on pylon 4 right</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 90.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon3r">
<description>Weight on pylon 3 right</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 120.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon2r">
<description>Weight on pylon 2 right</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 150.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
<pointmass name="Pylon1r">
<description>Weight on pylon 1 right</description>
<weight unit="LBS">0</weight>
<location name="POINTMASS" unit="IN">
<x> 524.38 </x>
<y> 180.00 </y>
<z> -21.85 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x> 113.61 </x>
<y> 0.00 </y>
<z> -104.88 </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"> 15000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 27477.50 </damping_coeff>
<max_steer unit="DEG"> 65.00 </max_steer>
<brake_group>NONE</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="IN">
<x> 545.35 </x>
<y> -52.02 </y>
<z> -104.88 </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"> 74955.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 37477.50 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>LEFT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="IN">
<x> 545.35 </x>
<y> 52.02 </y>
<z> -104.88 </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"> 74955.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 37477.50 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>RIGHT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="STRUCTURE" name="LEFT_WING">
<location unit="IN">
<x> 524.38 </x>
<y> -24.09 </y>
<z> -21.85 </z>
</location>
<static_friction> 1.00 </static_friction>
<dynamic_friction> 1.00 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 74955.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 74955.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="IN">
<x> 524.38 </x>
<y> 24.09 </y>
<z> -21.85 </z>
</location>
<static_friction> 1.00 </static_friction>
<dynamic_friction> 1.00 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 74955.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 74955.00 </damping_coeff>
</contact>
</ground_reactions>
<propulsion>
<engine file="Saturn_127">
<location unit="IN">
<x> 813.96 </x>
<y> -25.00 </y>
<z> 36.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>0</feed>
<thruster file="direct">
<location unit="IN">
<x> 813.96 </x>
<y> -25.00 </y>
<z> 36.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="Saturn_127">
<location unit="IN">
<x> 813.96 </x>
<y> 25.00 </y>
<z> 36.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>1</feed>
<thruster file="direct">
<location unit="IN">
<x> 813.96 </x>
<y> 25.00 </y>
<z> 36.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="RR800">
<location unit="IN">
<x> 513.96 </x>
<y> -120.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>0</feed>
<thruster file="direct">
<location unit="IN">
<x> 513.96 </x>
<y> -120.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="RR800">
<location unit="IN">
<x> 513.96 </x>
<y> 120.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>1</feed>
<thruster file="direct">
<location unit="IN">
<x> 513.96 </x>
<y> 120.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="RR1000">
<location unit="IN">
<x> 513.96 </x>
<y> -90.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>0</feed>
<thruster file="direct">
<location unit="IN">
<x> 513.96 </x>
<y> -90.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="RR1000">
<location unit="IN">
<x> 513.96 </x>
<y> 90.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>1</feed>
<thruster file="direct">
<location unit="IN">
<x> 513.96 </x>
<y> 90.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<tank type="FUEL" number="0">
<location unit="IN">
<x> 424.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
<capacity unit="LBS"> 4047.57 </capacity>
<contents unit="LBS"> 2023.79 </contents>
</tank>
<tank type="FUEL" number="1">
<location unit="IN">
<x> 424.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
<capacity unit="LBS"> 4047.57 </capacity>
<contents unit="LBS"> 2023.79 </contents>
</tank>
<tank type="FUEL" number="2">
<location unit="IN">
<x> 424.38 </x>
<y> 0.00 </y>
<z> -21.85 </z>
</location>
<capacity unit="LBS"> 4047.57 </capacity>
<contents unit="LBS"> 2023.79 </contents>
</tank>
</propulsion>
<system file="TriCycle_PushbackJSBSIM"/>
<flight_control name="FCS: Loreley-B">
<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> -0.35 </min>
<max> 0.35 </max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="elevator normalization">
<input>fcs/elevator-pos-rad</input>
<domain>
<min> -0.35 </min>
<max> 0.35 </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> -0.35 </min>
<max> 0.35 </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> -0.35 </min>
<max> 0.35 </max>
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="left aileron normalization">
<input>fcs/left-aileron-pos-rad</input>
<domain>
<min> -0.35 </min>
<max> 0.35 </max>
</domain>
<range>
<min> -1 </min>
<max> 1 </max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
<aerosurface_scale name="right aileron normalization">
<input>fcs/right-aileron-pos-rad</input>
<domain>
<min> -0.35 </min>
<max> 0.35 </max>
</domain>
<range>
<min> -1 </min>
<max> 1 </max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
</channel>
<property value="1">fcs/yaw-damper-enable</property>
<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 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>
<gain>fcs/yaw-damper-enable</gain>
</scheduled_gain>
<summer name="Rudder Sum">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-rate</input>
<clipto>
<min> -1.1 </min>
<max> 1.1 </max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<domain>
<min> -1.1 </min>
<max> 1.1 </max>
</domain>
<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> 10 </position>
<time> 4 </time>
</setting>
<setting>
<position> 15 </position>
<time> 4 </time>
</setting>
<setting>
<position> 20 </position>
<time> 3 </time>
</setting>
<setting>
<position> 25 </position>
<time> 3 </time>
</setting>
<setting>
<position> 30 </position>
<time> 3 </time>
</setting>
<setting>
<position> 35 </position>
<time> 3 </time>
</setting>
<setting>
<position> 40 </position>
<time> 3 </time>
</setting>
<setting>
<position> 45 </position>
<time> 3 </time>
</setting>
</traverse>
<output>fcs/flap-pos-deg</output>
</kinematic>
<aerosurface_scale name="flap normalization">
<input>fcs/flap-pos-deg</input>
<domain>
<min> 0 </min>
<max> 30 </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> 5 </time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic>
<scheduled_gain name="Scheduled Steer Pos Deg">
<input>fcs/steer-cmd-norm</input>
<table>
<independentVar>velocities/vg-fps</independentVar>
<tableData>
10.0 65.0
50.0 5.0
150.0 1.0
</tableData>
</table>
<output>fcs/steer-pos-deg</output>
</scheduled_gain>
</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> 1 </time>
</setting>
</traverse>
<output>fcs/speedbrake-pos-norm</output>
</kinematic>
</channel>
</flight_control>
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<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>
<tableData>
-0.20 -0.620
0.00 0.080
0.26 1.000
0.60 0.448
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.01167 </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>0.2</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>0.2</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.500
-0.26 0.027
0.00 0.021
0.26 0.027
1.57 1.500
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.12</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.81 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00267 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.02</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.2</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<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="ROLL">
<function name="aero/moment/Roll_beta">
<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>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<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/moment/Roll_yaw">
<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>0.15</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<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>0.11</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<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>0.01</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<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>-0.3</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -0.800
2.0 -0.200