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C-5-JSB.xml
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C-5-JSB.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="C-5 Galaxy" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Jon Bourgeois </author>
<filecreationdate> 2010-03-14 </filecreationdate>
<version>2.0</version>
<description> Models a C-5 Galaxy. </description>
</fileheader>
<!--
File: C-5.xml
Inputs:
name: C-5_Galaxy
type: four-engine transonic transport
manufacturer: Lockheed
first flight: 30 June 1968
max weight: 840000 lb (381,000 kg)
empty weight: 380,000 lb (172,370 kg)
loaded weight: 769,000 lb (348,800 kg)
wing span: 222.74709 ft (67.89 m)
length: 247.09211 ft (75.31 m)
height: 65 ft (19.84 m)
wing area: 6200 sq-ft
gear type: tricycle
retractable?: yes
# engines: 4
engine type: fan-jet
engine layout: wings
yaw damper? yes
Outputs:
wing loading: 27.75 lb/sq-ft
CL-alpha: 4.4 per radian
CL-0: 0.2
CL-max: 1.2
CD-0: 0.017
K: 0.042
General Characteristics:
Crew: 8 typical (pilot, first pilot, 1st Officer, two flight engineers, three loadmasters) 4 minimum (pilot, copilot, two flight engineers)
Payload: 270,000 lb (122,470 kg) M Model: 285,000 lb (129,274 kg)
Engines A/B/C Models: GE TF-39 43,000 lbs thrust
Engines M Model: GE CF6-80C2L1F 50,580 lbs thrust
Fuel Capacity: 51,450 gallons or 332,500 lb (150,819 kg)
Fuel Tanks: 12 integral tanks in wings
Normal Cruise Speed: Mach 0.77
Cargo Bay: 121 ft (37 m) long, 13.5 ft (4.1 m) high, and 19 ft (5.8 m) wide, or just over 31,000 cu ft (880 m3)
Cargo Bay Capacity: 36 463L Pallets
Tires 49 X 17 inches or 1.2446 X 0.4318 meters
-->
<metrics>
<wingarea unit="FT2"> 6200.00 </wingarea>
<wingspan unit="FT" > 222.75 </wingspan>
<wing_incidence> 3.00 </wing_incidence>
<chord unit="FT" > 35.70 </chord>
<htailarea unit="FT2"> 966 </htailarea>
<htailarm unit="FT" > 139.31 </htailarm>
<vtailarea unit="FT2"> 961 </vtailarea>
<vtailarm unit="FT" > 111.71 </vtailarm>
<location name="AERORP" unit="FT">
<x> 107.31 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 232.12 </x>
<y> -27.85 </y>
<z> 154.75 </z>
</location>
<location name="VRP" unit="IN">
<x>0</x>
<y>0</y>
<z>0</z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 14067811.7032 </ixx>
<iyy unit="SLUG*FT2"> 19614209.0022 </iyy>
<izz unit="SLUG*FT2"> 32969644.0486 </izz>
<emptywt unit="LBS" > 380000 </emptywt>
<location name="CG" unit="FT">
<x> 111.70 </x> <!-- 111.70 -->
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<pointmass name="Pilot">
<weight unit="LBS"> 180 </weight>
<location name="POINTMASS" unit="IN">
<x> 232.12 </x>
<y> -27.85 </y>
<z> 154.75 </z>
</location>
</pointmass>
<pointmass name="Copilot">
<weight unit="LBS"> 180 </weight>
<location name="POINTMASS" unit="IN">
<x> 232.12 </x>
<y> 27.85 </y>
<z> 154.75 </z>
</location>
</pointmass>
<pointmass name="payload">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 20.784 </x>
<y> 0 </y>
<z> -2.36235 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSEGEAR">
<location unit="IN">
<x> 504.48 </x>
<y> 0.00 </y>
<z> -222.84 </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"> 570000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 171000.00 </damping_coeff>
<max_steer unit="DEG"> 60.00 </max_steer>
<brake_group>NOSE</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Main1_Left Front">
<location unit="IN">
<x> 1278.23 </x>
<y> -147.01 </y>
<z> -222.84 </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"> 570000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 114000.00 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>LEFT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Main2_Left Rear">
<location unit="IN">
<x> 1505.71 </x>
<y> -147.01 </y>
<z> -222.84 </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"> 570000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 114000.00 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>LEFT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Main3_Right Front">
<location unit="IN">
<x> 1278.23 </x>
<y> 147.01 </y>
<z> -222.84 </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"> 570000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 114000.00 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>RIGHT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Main4_Right Rear">
<location unit="IN">
<x> 1505.71 </x>
<y> 147.01 </y>
<z> -222.84 </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"> 570000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 114000.00 </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> 1584.63 </x>
<y> -1445.36 </y>
<z> 60.24 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="IN">
<x> 1584.63 </x>
<y> -1445.36 </y>
<z> 60.24 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="NG_POD">
<location unit="IN">
<x> 510.67 </x>
<y> 0 </y>
<z> 151.65 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="Nosetip">
<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>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="MLG_PODLT">
<location unit="IN">
<x> 1391.97 </x>
<y> -147.01 </y>
<z> -148.56 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="MLG_PODRT">
<location unit="IN">
<x> 1391.97 </x>
<y> 147.01 </y>
<z> -148.56 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="Rear_Fuselage">
<location unit="IN">
<x> 2429.57 </x>
<y> 0 </y>
<z> 12.38 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 500000.0 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 500000.0 </damping_coeff>
</contact>
</ground_reactions>
<propulsion>
<engine file="CF6-80C2"> <!-- Engine1 -->
<location unit="IN">
<x> 1293.71 </x>
<y> -804.70 </y>
<z> -21.66 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>0</feed>
<feed>1</feed>
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 1374.18 </x>
<y> -804.70 </y>
<z> -21.66 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="CF6-80C2"> <!-- Engine2 -->
<location unit="IN">
<x> 1148.24 </x>
<y> -213.77 </y>
<z> 6.19 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>3</feed>
<feed>2</feed>
<feed>5</feed>
<thruster file="direct">
<location unit="IN">
<x> 1228.71 </x>
<y> -213.77 </y>
<z> 6.19 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="CF6-80C2"> <!-- Engine3 -->
<location unit="IN">
<x> 1148.24 </x>
<y> 213.77 </y>
<z> 6.19 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>8</feed>
<feed>9</feed>
<feed>6</feed>
<thruster file="direct">
<location unit="IN">
<x> 1228.71 </x>
<y> 213.77 </y>
<z> 6.19 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="CF6-80C2"> <!-- Engine4 -->
<location unit="IN">
<x> 1293.71 </x>
<y> 804.70 </y>
<z> -21.66 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed>11</feed>
<feed>10</feed>
<feed>7</feed>
<thruster file="direct">
<location unit="IN">
<x> 1374.18 </x>
<y> 804.70 </y>
<z> -21.66 </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"> <!-- Main1 -->
<location unit="IN">
<x> 1584.63 </x>
<y> -1157.53 </y>
<z> 64.99 </z>
</location>
<capacity unit="LBS"> 26556.75 </capacity>
<contents unit="LBS"> 13000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="1"> <!-- Aux1 -->
<location unit="IN">
<x> 1494.88 </x>
<y> -894.45 </y>
<z> 102.13 </z>
</location>
<capacity unit="LBS"> 30119.27 </capacity>
<contents unit="LBS"> 15000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="2"> <!-- Aux2 -->
<location unit="IN">
<x> 1293.71 </x>
<y> -544.72 </y>
<z> 142.37 </z>
</location>
<capacity unit="LBS"> 24461.86 </capacity>
<contents unit="LBS"> 12000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="3"> <!-- Main2 -->
<location unit="IN">
<x> 1176.10 </x>
<y> -300.21 </y>
<z> 164.03 </z>
</location>
<capacity unit="LBS"> 43521.73 </capacity>
<contents unit="LBS"> 22000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="4"> <!-- ExtRng1 -->
<location unit="IN">
<x> 1417.51 </x>
<y> -526.15 </y>
<z> 142.37 </z>
</location>
<capacity unit="LBS"> 15566.64 </capacity>
<contents unit="LBS"> 8000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="5"> <!-- ExtRng2 -->
<location unit="IN">
<x> 1358.70 </x>
<y> -287.83 </y>
<z> 164.03 </z>
</location>
<capacity unit="LBS"> 26024.97 </capacity>
<contents unit="LBS"> 13000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="6"> <!-- ExtRng3 -->
<location unit="IN">
<x> 1358.70 </x>
<y> 287.33 </y>
<z> 164.03 </z>
</location>
<capacity unit="LBS"> 26024.97 </capacity>
<contents unit="LBS"> 13000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="7"> <!-- ExtRng4 -->
<location unit="IN">
<x> 1417.51 </x>
<y> 526.15 </y>
<z> 142.37 </z>
</location>
<capacity unit="LBS"> 15566.64 </capacity>
<contents unit="LBS"> 8000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="8"> <!-- Main3 -->
<location unit="IN">
<x> 1176.10 </x>
<y> 300.21 </y>
<z> 164.03 </z>
</location>
<capacity unit="LBS"> 43521.73 </capacity>
<contents unit="LBS"> 22000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="9"> <!-- Aux3 -->
<location unit="IN">
<x> 1293.71 </x>
<y> 544.72 </y>
<z> 142.37 </z>
</location>
<capacity unit="LBS"> 24461.86 </capacity>
<contents unit="LBS"> 12000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="10"> <!-- Aux4 -->
<location unit="IN">
<x> 1494.88 </x>
<y> 894.45 </y>
<z> 102.13 </z>
</location>
<capacity unit="LBS"> 30119.27 </capacity>
<contents unit="LBS"> 15000 </contents>
<type> JP-8 </type>
</tank>
<tank type="FUEL" number="11"> <!-- Main4 -->
<location unit="IN">
<x> 1584.63 </x>
<y> 1157.53 </y>
<z> 64.99 </z>
</location>
<capacity unit="LBS"> 26566.75 </capacity>
<contents unit="LBS"> 13000 </contents>
<type> JP-8 </type>
</tank>
</propulsion>
<flight_control name="FCS: C-5">
<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>
<channel name="Yaw">
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min> -0.35 </min>
<max> 0.35 </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> 15 </position>
<time> 4 </time>
</setting>
<setting>
<position> 30 </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>
</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>
<scheduled_gain name="Scheduled Steer Pos Deg">
<input>fcs/steer-cmd-norm</input>
<table>
<independentVar>velocities/vg-fps</independentVar>
<tableData>
10.0 80.0
50.0 7.5
150.0 1.0
</tableData>
</table>
<output>fcs/steer-pos-deg</output>
</scheduled_gain>
</flight_control>
<aerodynamics>
<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>
<tableData>
-0.20 -0.680
0.00 0.200
0.23 1.200
0.60 0.600
</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-deg</property>
<value> 0.05000 </value>
</product>
</function>
<function name="aero/coefficient/dCLsb">
<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>-0.08</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>0.2</value>
</product>
</function>
</axis>
<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 lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.500
-0.26 0.022
0.00 0.017
0.26 0.022
1.57 1.500
</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>
<value>0.042</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 lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData> <!-- Original Aeromatic Table -->
</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-deg</property>
<value> 0.00183 </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>0.011</value>
</product>
</function>
<function name="aero/coefficient/CDsb">
<description>Drag_due_to_speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.017</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 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/coefficient/CDde">
<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/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="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>-0.1</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>