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A380_RJ.xml
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<?xml version="1.0"?>
<?xml-stylesheet href="http://jsbsim.sourceforge.net/JSBSim.xsl" type="text/xsl"?>
<fdm_config name="a380" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<!--
This is the Airbus A380 double-deck wide body subsonic general passenger transport aircraft.
Modification History:
When Who What
2007 ICunningram Initial
2008 KAmpere update
2008 FDalvi update
APR-2009 SHamilton update
Jun-2010 SHamilton tweak high-lift devices to match CLmax
-->
<fileheader>
<author>Cunningham, Ampere, Hamilton, et al</author>
<filecreationdate> Creation Date </filecreationdate>
<version>V1.0.3</version>
<description>Models an A380</description>
</fileheader>
<metrics>
<!-- wingarea unit="FT2"> 8934.95 </wingarea>
<wingspan unit="FT"> 261.82 </wingspan>
<chord unit="FT"> 34.13 </chord>
<htailarea unit="FT2"> 2233.74 </htailarea>
<htailarm unit="FT"> 102.66 </htailarm>
<vtailarea unit="FT2"> 1786.99 </vtailarea>
<vtailarm unit="FT"> 0 </vtailarm -->
<wingarea unit="FT2"> 9096.43 </wingarea>
<wingspan unit="FT" > 261.82 </wingspan>
<wing_incidence> 2.00 </wing_incidence>
<!-- chord unit="FT" > 33.5 </chord -->
<chord unit="FT" > 34.88 </chord>
<htailarea unit="FT2"> 2274.11 </htailarea>
<htailarm unit="FT" > 107.78 </htailarm>
<vtailarea unit="FT2"> 1819.29 </vtailarea>
<vtailarm unit="FT" > 107.78 </vtailarm>
<location name="AERORP" unit="IN">
<x> 1640 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 201.2 </x>
<y> -32 </y>
<z> 80 </z>
</location>
<location name="VRP" unit="M">
<!-- x> 30.0 </x>
<y> 0 </y>
<z> 0.00 </z -->
<x> 0.0 </x>
<y> 0 </y>
<z> -5.56 </z>
</location>
</metrics>
<mass_balance>
<!-- ixx unit="SLUG*FT2"> 9.87831e+07 </ixx>
<iyy unit="SLUG*FT2"> 9.33213e+07 </iyy>
<izz unit="SLUG*FT2"> 1.95326e+08 </izz>
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS"> 725004 </emptywt>
<location name="CG" unit="IN">
<x> 1580.8 </x>
<y> 0 </y>
<z> -71.9 </z>
</location -->
<ixx unit="SLUG*FT2"> 40378502 </ixx>
<iyy unit="SLUG*FT2"> 38145914 </iyy>
<izz unit="SLUG*FT2"> 79841172 </izz>
<emptywt unit="LBS" > 740880 </emptywt>
<location name="CG" unit="IN">
<x> 1580.79 </x>
<y> 0.00 </y>
<z> -71.85 </z>
<!-- x> 40.152066 </x>
<y> 0.0000 </y>
<z> -5.52 </z -->
</location>
<pointmass name="pilots" >
<weight unit="KG">160</weight>
<location name="crew" unit = "M">
<x> 4.0710 </x>
<y> 0.0000 </y>
<z> -7.0326 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 1.0 </radius> <!-- wild guess -->
<length unit="M"> 1.0 </length> <!-- wild guess -->
</form>
</pointmass>
<pointmass name="passenger main" >
<weight unit="KG">43040</weight>
<location name="passenger" unit = "M">
<x> 37.4554 </x>
<y> 0.0000 </y>
<z> -5.7104 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 2.0 </radius> <!-- wild guess -->
<length unit="M"> 30.0 </length> <!-- wild guess -->
</form>
</pointmass>
<pointmass name="passenger upper" >
<weight unit="KG">25200</weight>
<location name="passenger" unit = "M">
<x> 37.4554 </x>
<y> 0.0000 </y>
<z> -8.3097 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 2.0 </radius> <!-- wild guess -->
<length unit="M"> 30.0 </length> <!-- wild guess -->
</form>
</pointmass>
<pointmass name="cargo forward" >
<weight unit="KG">28577</weight>
<location name="POINTMASS" unit = "M">
<x> 15.5171 </x>
<y> 0.0000 </y>
<z> -3.7654 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 2.0 </radius> <!-- wild guess -->
<length unit="M"> 10.0 </length> <!-- wild guess -->
</form>
</pointmass>
<pointmass name="cargo aft" >
<weight unit="KG">20310</weight>
<location name="POINTMASS" unit = "M">
<x> 45.6932 </x>
<y> 0.0000 </y>
<z> -4.1767 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 2.0 </radius> <!-- wild guess -->
<length unit="M"> 10.0 </length> <!-- wild guess -->
</form>
</pointmass>
<pointmass name="cargo bulk" >
<weight unit="KG">2515</weight>
<location name="POINTMASS" unit = "M">
<x> 52.4356 </x>
<y> 0.00 </y>
<z> -4.3714 </z>
</location>
<form shape="cylinder">
<radius unit="M"> 2.0 </radius> <!-- wild guess -->
<length unit="M"> 1.0 </length> <!-- wild guess -->
</form>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="Nose Gear">
<location unit="IN">
<x> 488.52 </x>
<y> 0 </y>
<z> -344.9 </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"> 362502 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 120834 </damping_coeff>
<max_steer unit="DEG"> 70 </max_steer>
<brake_group> NOSE </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Left Main gear">
<location unit="IN">
<x> 1644 </x>
<!-- y> -282.8 </y -->
<y>278.972441</y>
<z> -344.9 </z>
</location>
<static_friction> 0.85 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 1.20834e+06 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer> <!-- was 0.0 -->
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Right Main Gear">
<location unit="IN">
<x> 1644 </x>
<!-- y> 282.8 </y -->
<y>-278.972441</y>
<z> -344.9 </z>
</location>
<static_friction> 0.85 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 1.20834e+06 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer> <!-- was 0.0 -->
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<!--
<contact type="STRUCTURE" name="ELG">
<location unit="IN">
<x> 488,52 </x>
<y> 0 </y>
<z> -322.9 </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"> 362502 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 120834 </damping_coeff>
<max_steer unit="DEG"> 30 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="EMLG1">
<location unit="IN">
<x> 1644 </x>
<y> -282.8 </y>
<z> -322.9 </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"> 1.20834e+06 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="EMLG2">
<location unit="IN">
<x> 1644 </x>
<y> 282.8 </y>
<z> -322.9 </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"> 1.20834e+06 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 241668 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
-->
</ground_reactions>
<propulsion>
<engine file="TRENT-900">
<location unit="M">
<x> 46.9824 </x>
<y> 26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>0</feed>
<feed>4</feed>
<feed>6</feed>
<feed>10</feed>
<feed>8</feed>
<thruster file="direct">
<location unit="M">
<!-- x> 1580.79 </x>
<y> -523.648 </y>
<z> -40 </z -->
<x> 46.9824 </x>
<y> 26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<engine file="TRENT-900">
<location unit="M">
<x> 38.9500 </x>
<y> 15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>1</feed>
<feed>4</feed>
<feed>6</feed>
<feed>10</feed>
<feed>8</feed>
<thruster file="direct">
<location unit="M">
<!-- x> 1580.79 </x>
<y> -523.648 </y>
<z> -40 </z -->
<x> 38.9500 </x>
<y> 15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<engine file="TRENT-900">
<location unit="M">
<x> 38.9500 </x>
<y> -15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>2</feed>
<feed>5</feed>
<feed>7</feed>
<feed>10</feed>
<feed>9</feed>
<thruster file="direct">
<location unit="M">
<!-- x> 1580.79 </x>
<y> 523.648 </y>
<z> -40 </z -->
<x> 38.9500 </x>
<y> -15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<engine file="TRENT-900">
<location unit="M">
<x> 46.9824 </x>
<y> -26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>3</feed>
<feed>5</feed>
<feed>7</feed>
<feed>10</feed>
<feed>9</feed>
<thruster file="direct">
<location unit="M">
<!-- x> 1580.79 </x>
<y> 523.648 </y>
<z> -40 </z -->
<x> 46.9824 </x>
<y> -26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<!-- APU type -->
<engine file="APU">
<location unit="IN">
<x> 100 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>1</feed>
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 100 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<!--
The A380 has 11 tanks in all. The feed tanks feed each engine with
a cross-over valve to the next engine. The sequence for feeding the
feed tanks is;
1. inner tank -> feed
2. mid tank -> feed
3. trim tank -> feed
4. outer tank -> feed
The trim tank should be moved to the outer trim tank before approach.
-->
<tank type="FUEL"> <!-- feed number 0 -->
<location unit="M">
<!-- x> 1580.79 </x>
<y> 200 </y>
<z> -71.8539 </z -->
<x> 48.5306 </x>
<y> 23.4729 </y>
<z> -5.01 </z>
</location>
<capacity unit="LBS"> 48390 </capacity>
<contents unit="LBS"> 16775 </contents>
<priority>1</priority>
<type>JET-A</type>
<radius unit="M"> 1.87 </radius>
</tank>
<tank type="FUEL"> <!-- feed number 1 -->
<location unit="M">
<x> 37.4956 </x>
<y> 7.6904 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 50780 </capacity>
<contents unit="LBS"> 18280 </contents>
<priority>1</priority>
<type>JET-A</type>
<radius unit="M"> 1.9 </radius>
</tank>
<tank type="FUEL"> <!-- feed number 2 -->
<location unit="M">
<x> 37.4956 </x>
<y> -7.6904 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 50780 </capacity>
<contents unit="LBS"> 18280 </contents>
<priority>1</priority>
<type>JET-A</type>
<radius unit="M"> 1.9 </radius>
</tank>
<tank type="FUEL"> <!-- feed number 3 -->
<location unit="M">
<x> 48.5306 </x>
<y> -23.4729 </y>
<z> -5.01 </z>
</location>
<capacity unit="LBS"> 48390 </capacity>
<contents unit="LBS"> 16775 </contents>
<priority>1</priority>
<type>JET-A</type>
<radius unit="M"> 1.87 </radius>
</tank>
<tank type="FUEL"> <!-- innerL 4 -->
<location unit="M">
<x> 42.1149 </x>
<y> 8.5886 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 79850 </capacity>
<contents unit="LBS"> 17034 </contents>
<priority>2</priority>
<type>JET-A</type>
<radius unit="M"> 2.21 </radius>
</tank>
<tank type="FUEL"> <!-- innerR 5 -->
<location unit="M">
<x> 42.1149 </x>
<y> -8.5886 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 79850 </capacity>
<contents unit="LBS"> 17034 </contents>
<priority>2</priority>
<type>JET-A</type>
<radius unit="M"> 2.21 </radius>
</tank>
<tank type="FUEL"> <!-- midL 6 -->
<location unit="M">
<x> 44.0396 </x>
<y> 15.0043 </y>
<z> -4.67 </z>
</location>
<capacity unit="LBS"> 63100 </capacity>
<contents unit="LBS"> 16826 </contents>
<priority>3</priority>
<type>JET-A</type>
<radius unit="M"> 2.04 </radius>
</tank>
<tank type="FUEL"> <!-- midR 7 -->
<location unit="M">
<x> 44.0396 </x>
<y> -15.0043 </y>
<z> -4.67 </z>
</location>
<capacity unit="LBS"> 63100 </capacity>
<contents unit="LBS"> 16826 </contents>
<priority>3</priority>
<type>JET-A</type>
<radius unit="M"> 2.04 </radius>
</tank>
<tank type="FUEL"> <!-- outerL 8 -->
<location unit="M">
<x> 52.7169 </x>
<y> 30.1754 </y>
<z> -5.28 </z>
</location>
<capacity unit="LBS"> 18200 </capacity>
<contents unit="LBS"> 10434 </contents>
<priority>4</priority>
<type>JET-A</type>
<radius unit="M"> 1.35 </radius>
</tank>
<tank type="FUEL"> <!-- outerR 9 -->
<location unit="M">
<x> 52.7169 </x>
<y> -30.1754 </y>
<z> -5.28 </z>
</location>
<capacity unit="LBS"> 18200 </capacity>
<contents unit="LBS"> 10434 </contents>
<priority>4</priority>
<type>JET-A</type>
<radius unit="M"> 1.35 </radius>
</tank>
<tank type="FUEL"> <!-- trim 10 -->
<location unit="M">
<!-- x> 1580.79 </x>
<y> 0 </y>
<z> -71.8539 </z -->
<x> 60.8777 </x>
<y> 0.0000 </y>
<z> -7.9141 </z>
</location>
<capacity unit="LBS"> 41020 </capacity>
<contents unit="LBS"> 20000 </contents>
<priority>5</priority>
<type>JET-A</type>
<radius unit="M"> 1.77 </radius>
</tank>
</propulsion>
<system file="pushback"/>
<flight_control name="FCS: a380">
<channel name="All">
<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>0.3</max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<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>
<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>aero/qbar-psf</independentVar>
<tableData>
3.0000 0.0000
11.0000 2.0000
</tableData>
</table>
</scheduled_gain>
<scheduled_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<table>
<independentVar>aero/qbar-psf</independentVar>
<tableData>
3.0000 0.0000
11.0000 0.0000
</tableData>
</table>
</scheduled_gain>
<summer name="Yaw Damper Sum">
<input>fcs/yaw-damper-beta</input>
<input>fcs/yaw-damper-rate</input>
<clipto>
<min>-0.2000</min>
<max>0.2000</max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper Final">
<input>fcs/yaw-damper-sum</input>
<table>
<independentVar>aero/qbar-psf</independentVar>
<tableData>
2.9900 0.0000
3.0000 1.0000
</tableData>
</table>
</scheduled_gain>
<summer name="Rudder Sum">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-final</input>
<clipto>
<min>-1.0000</min>
<max>1.0000</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<range>
<min>-0.3500</min>
<max>0.3500</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<kinematic name="Flaps Control">
<input>fcs/flap-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>7.2720</position>
<time>15.0</time>
</setting>
<setting>
<position>15.4530</position>
<time>5.0</time>
</setting>
<setting>
<position>23.6340</position>
<time>4.0</time>
</setting>
<setting>
<position>30.0000</position>
<time>5.0</time>
</setting>
</traverse>
<output>fcs/flap-pos-deg</output>
<aerosurface_scale name="Flap Position Normalizer">
<input>fcs/flap-pos-deg</input>
<domain>
<min>0</min> <!-- Flaps actual minimum position -->
<max>30</max> <!-- Flaps actual maximum position -->
</domain>
<range>
<min>0</min> <!-- Flaps normalized minimum position -->
<max>1</max> <!-- Flaps normalized maximum position -->
</range>
<output>fcs/flap-pos-norm</output>
</aerosurface_scale>
</kinematic>
<kinematic name="Slats Control">
<input>fcs/slat-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>30.0000</position>
<time>12.0</time>
</setting>
</traverse>
<output>fcs/leading-edge-slat-pos-deg</output>
<output>fcs/leading-edge-flap-pos-deg</output>
</kinematic>
<!-- kinematic name="Gear Control">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>1.0000</position>
<time>15.0000</time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic -->
<kinematic name="gear/unit[0]/pos">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>1.0000</position>
<time>16.0000</time>
</setting>
</traverse>
<output>gear/unit[0]/pos-norm</output>
</kinematic>
<kinematic name="gear/unit[1]/pos">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>1.0000</position>
<time>13.0000</time>
</setting>
</traverse>
<output>gear/unit[1]/pos-norm</output>
</kinematic>
<kinematic name="gear/unit[2]/pos">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>1.0000</position>
<time>25.0000</time>
</setting>
</traverse>
<output>gear/unit[2]/pos-norm</output>
</kinematic>
<kinematic name="Speedbrake Control">
<input>fcs/speedbrake-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>1.0000</position>
<time>1.0000</time>
</setting>
</traverse>
<output>fcs/speedbrake-pos-norm</output>
</kinematic>
</channel>
</flight_control>
<!--
The aerodynamics section
-->
<aerodynamics>
<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>
-1.5700 1.5000
-0.2600 0.0340
0.0000 0.0170
0.2600 0.0340
1.5700 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>
<!-- value>0.0420</value -->
<value>0.0350</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>
0.0000 0.0000
0.7900 0.0000
1.1000 0.0230
1.8000 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>0.0550</value>
</product>
</function -->
<function name="aero/coefficient/CDflap">
<description>Drag_due_to_flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>fcs/flap-pos-norm</independentVar>
<tableData>
0.00 0.00
0.25 0.00
0.53 0.001 <!-- 0.00 -->
0.79 0.025 <!-- 0.03, 0.015 -->
1.00 0.043 <!-- 0.05, 0.023 -->
</tableData>
</table>
</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/unit[2]/pos-norm</property><!-- FIXME -->
<value>0.0110</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>0.0170</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>
-1.5700 1.2300
-0.2600 0.0500
0.0000 0.0000
0.2600 0.0500
1.5700 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>0.0550</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>
<sin><property>aero/beta-rad</property></sin>
<!-- property>aero/beta-rad</property -->
<value>-1.0000</value>
</product>
</function>
</axis>
<function name="aero/function/ground-effect-factor-lift">
<description>Change in lift due to ground effect factor</description>
<product>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.0 1.203
0.1 1.127
0.15 1.090
0.2 1.073
0.3 1.046
0.4 1.055
0.5 1.019
0.6 1.013
0.7 1.008
0.8 1.006
0.9 1.003
1.0 1.002
1.1 1.0
</tableData>
</table>
</product>
</function>
<function name="aero/function/ground-effect-factor-drag">
<description>Change in drag due to ground effect</description>
<product>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.0 0.480
0.1 0.515
0.15 0.629
0.2 0.709