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A380.xml
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A380.xml
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<?xml version="1.0"?><!-- minor changes by ph-cor jan2016 -->
<?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">
<fileheader>
<author>Muraleedharn, Cunningham, Ampere, Hamilton, et al</author>
<filecreationdate> 20140709 </filecreationdate>
<version>1.0</version>
<description>Updated Airbus A380-800 Flight Dynamics - largely based of scotth1's A380 flight dynamics</description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 9095.5000 </wingarea>
<wingspan unit="FT"> 261.8000 </wingspan>
<chord unit="FT"> 47.9000 </chord>
<htailarea unit="FT2"> 2236.0200 </htailarea>
<htailarm unit="FT"> 106.4339 </htailarm>
<vtailarea unit="FT2"> 1314.4999 </vtailarea>
<vtailarm unit="FT"> 100.2985 </vtailarm>
<location name="AERORP" unit="M">
<x> 41.656 </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 </z>
</location>
</metrics>
<mass_balance>
<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>
</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"> 1.0 </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="M">
<x> 12.40 </x>
<y> 0 </y>
<z> -9.19 </z>
</location>
<static_friction> 0.95 </static_friction>
<dynamic_friction> 0.86 </dynamic_friction><!-- 0.76 -->
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 140000 </spring_coeff><!-- 44000 -->
<damping_coeff unit="LBS/FT/SEC"> 60000 </damping_coeff><!-- 8000 -->
<max_steer unit="DEG"> 50 </max_steer>
<brake_group> NONE </brake_group>
<retractable>1</retractable>
</contact><!-- All main wheels 2 meters back -->
<contact type="BOGEY" name="Left Fwd Main gear REAR WHEELS">
<location unit="M">
<x> 43.02 </x>
<y> -6.23</y>
<z> -9.44 </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"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Right Fwd Main Gear REAR WHEELS">
<location unit="M">
<x> 43.02 </x>
<y> 6.23</y>
<z> -9.44 </z><!-- -9.44 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Left Aft Main gear FWD WHEELS">
<location unit="M">
<x> 43.95 </x>
<y> -3.45</y>
<z> -10.44 </z><!-- -8.9152 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Right Fwd Main Gear FWD WHEELS">
<location unit="M">
<x> 43.95 </x>
<y> 3.45</y>
<z> -10.44 </z><!-- -8.9152 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<!-- Additional Gears for rotate animation parameters -->
<contact type="BOGEY" name="Left Fwd Main gear FWD WHEELS">
<location unit="M">
<x> 41.60 </x>
<y> -6.23</y>
<z> -9.44 </z><!-- -9.44 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Right Fwd Main Gear FWD WHEELS">
<location unit="M">
<x> 41.60 </x>
<y> 6.23</y>
<z> -9.44 </z><!-- -9.44 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Left Aft Main gear REAR WHEELS">
<location unit="M">
<x> 46.95 </x>
<y> -3.45</y>
<z> -10.44 </z><!-- -8.9152 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="Right Fwd Main Gear REAR WHEELS"><!-- Fwd altered in Aft -->
<location unit="M">
<x> 46.95 </x>
<y> 3.45</y>
<z> -10.44 </z><!-- -8.9152 -->
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 130000 </spring_coeff><!-- 120000 -->
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff><!-- 7000 -->
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<!-- STRUCTURE POINTS -->
<contact type="STRUCTURE" name="TAIL">
<location unit="M">
<x> 63.1620 </x>
<y> 0 </y>
<z> -4.7 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 0.4 </dynamic_friction>
<rolling_friction> 0.4 </rolling_friction>
<spring_coeff unit="LBS/FT"> 200000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="NOSE">
<location unit="M">
<x> 9.5775 </x>
<y> 0 </y>
<z> -5.7 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 0.4 </dynamic_friction>
<rolling_friction> 0.4 </rolling_friction>
<spring_coeff unit="LBS/FT"> 200000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="LEFT">
<location unit="M">
<x> 58.4195 </x>
<y> -39.5 </y>
<z> -1.7 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 0.4 </dynamic_friction>
<rolling_friction> 0.4 </rolling_friction>
<spring_coeff unit="LBS/FT"> 200000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="RIGHT">
<location unit="M">
<x> 58.4195 </x>
<y> 39.5 </y>
<z> -1.7 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 0.4 </dynamic_friction>
<rolling_friction> 0.4 </rolling_friction>
<spring_coeff unit="LBS/FT"> 200000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 50000 </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>
<thruster file="direct">
<location unit="M">
<x> 46.9824 </x>
<y> -26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </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>
<thruster file="direct">
<location unit="M">
<x> 38.9500 </x>
<y> -15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </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>
<thruster file="direct">
<location unit="M">
<x> 38.9500 </x>
<y> 15.9365 </y>
<z> -2.55 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </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>
<thruster file="direct">
<location unit="M">
<x> 46.9824 </x>
<y> 26.2467 </y>
<z> -3.4 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
</thruster>
</engine>
<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>0</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>
<!--
There are 11 actual fuel tanks on the A380. In addition to the 11 tanks, there are 2 vent tanks (at the wing tips) -
L VENT TANK
L OUTER TANK
FEED TANK 1 - engine 1 feed
L MID TANK
L INNER TANK
FEED TANK 2 - engine 2 feed
TRIM TANK
FEED TANK 3 - engine 3 feed
R INNER TANK - apu feed
R MID TANK
FEED TANK 4 - engine 4 feed
R OUTER TANK
R VENT TANK
During normal operation, the fuel flow is like -
L OUTER TANK - FEED TANK 1
L MID TANK - FEED TANK 1
L MID TANK - L INNER TANK
L INNER TANK - FEED TANK 2
R INNER TANK - FEED TANK 3
R MID TANK - R INNER TANK
R MID TANK - FEED TANK 4
R OUTER TNAK - FEED TANK 4
Cross-feed balances fuel between the engine feed tanks and the R INNER TANK for APU
During flight, fuel is constantly being moved between to/from the trim tanks to maintain optimum aircraft cg (different for t/o, clb, crz and app)
R INNER TANK - TRIM TANK
L INNER TANK - TRIM TANK
-->
<tank type="FUEL"> <!-- FEED TANK 1 -->
<location unit="M">
<x> 48.5306 </x>
<y> -23.4729 </y>
<z> -5.01 </z>
</location>
<capacity unit="LBS"> 49455 </capacity> <!-- 7390 US gal -->
<contents unit="LBS"> 16775 </contents>
<type>JET-A</type>
<radius unit="M"> 1.87 </radius>
</tank>
<tank type="FUEL"> <!-- FEED TANK 2 -->
<location unit="M">
<x> 37.4956 </x>
<y> -7.6904 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 51896 </capacity> <!-- 7760 US gal -->
<contents unit="LBS"> 18280 </contents>
<type>JET-A</type>
<radius unit="M"> 1.9 </radius>
</tank>
<tank type="FUEL"> <!-- FEED TANK 3 -->
<location unit="M">
<x> 37.4956 </x>
<y> 7.6904 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 51896 </capacity> <!-- 7760 US gal -->
<contents unit="LBS"> 18280 </contents>
<type>JET-A</type>
<radius unit="M"> 1.9 </radius>
</tank>
<tank type="FUEL"> <!-- FEED TANK 4 -->
<location unit="M">
<x> 48.5306 </x>
<y> 23.4729 </y>
<z> -5.01 </z>
</location>
<capacity unit="LBS"> 49455 </capacity> <!-- 7390 US gal -->
<contents unit="LBS"> 16775 </contents>
<type>JET-A</type>
<radius unit="M"> 1.87 </radius>
</tank>
<tank type="FUEL"> <!-- L INNER TANK -->
<location unit="M">
<x> 42.1149 </x>
<y> -8.5886 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 81612 </capacity> <!-- 12190 US gal -->
<contents unit="LBS"> 17034 </contents>
<type>JET-A</type>
<radius unit="M"> 2.21 </radius>
</tank>
<tank type="FUEL"> <!-- R INNER TANK -->
<location unit="M">
<x> 42.1149 </x>
<y> 8.5886 </y>
<z> -3.3069 </z>
</location>
<capacity unit="LBS"> 81612 </capacity> <!-- 12190 US gal -->
<contents unit="LBS"> 17034 </contents>
<type>JET-A</type>
<radius unit="M"> 2.21 </radius>
</tank>
<tank type="FUEL"> <!-- L MID TANK -->
<location unit="M">
<x> 44.0396 </x>
<y> -15.0043 </y>
<z> -4.67 </z>
</location>
<capacity unit="LBS"> 69690 </capacity> <!-- 9630 US gal -->
<contents unit="LBS"> 16826 </contents>
<type>JET-A</type>
<radius unit="M"> 2.04 </radius>
</tank>
<tank type="FUEL"> <!-- R MID TANK -->
<location unit="M">
<x> 44.0396 </x>
<y> 15.0043 </y>
<z> -4.67 </z>
</location>
<capacity unit="LBS"> 69690 </capacity> <!-- 9630 US gal -->
<contents unit="LBS"> 16826 </contents>
<type>JET-A</type>
<radius unit="M"> 2.04 </radius>
</tank>
<tank type="FUEL"> <!-- L OUTER TANK -->
<location unit="M">
<x> 52.7169 </x>
<y> -30.1754 </y>
<z> -5.28 </z>
</location>
<capacity unit="LBS"> 18607 </capacity> <!-- 2760 US gal -->
<contents unit="LBS"> 10434 </contents>
<type>JET-A</type>
<radius unit="M"> 1.35 </radius>
</tank>
<tank type="FUEL"> <!-- R OUTER TANK -->
<location unit="M">
<x> 52.7169 </x>
<y> 30.1754 </y>
<z> -5.28 </z>
</location>
<capacity unit="LBS"> 18607 </capacity> <!-- 2760 US gal -->
<contents unit="LBS"> 10434 </contents>
<type>JET-A</type>
<radius unit="M"> 1.35 </radius>
</tank>
<tank type="FUEL"> <!-- TRIM TANK -->
<location unit="M">
<x> 60.8777 </x>
<y> 0.0000 </y>
<z> -7.9141 </z>
</location>
<capacity unit="LBS"> 41920 </capacity> <!-- 8280 US gal -->
<contents unit="LBS"> 20000 </contents>
<type>JET-A</type>
<radius unit="M"> 1.77 </radius>
</tank>
<tank type="FUEL"> <!-- L VENT -->
<location unit="M">
<x> 53 </x>
<y> -35 </y>
<z> -5.32 </z>
</location>
<capacity unit="LBS"> 2025 </capacity> <!-- 400 US gal -->
<contents unit="LBS"> 0 </contents>
<type>JET-A</type>
<radius unit="M"> 0.8 </radius>
</tank>
<tank type="FUEL"> <!-- R VENT -->
<location unit="M">
<x> 53 </x>
<y> 35 </y>
<z> -5.32 </z>
</location>
<capacity unit="LBS"> 2025 </capacity> <!-- 400 US gal -->
<contents unit="LBS"> 0 </contents>
<type>JET-A</type>
<radius unit="M"> 1.77 </radius>
</tank>
</propulsion>
<system file="pushback"/>
<flight_control name="FCS: A380">
<channel name="All">
<!-- All properties used in the flight control system are fly-by-wire output properties -->
<!-- FCS: Flight Control System - PITCH AXIS -->
<!-- 5 pitch control surfaces - HSTB, LOB ELEV, LIB ELEV, RIB ELEV, ROB ELEV -->
<summer name="Pitch Trim Sum"> <!-- FIXME - Is this really required anymore? -->
<input>fcs/hstb-fbw-output</input> <!-- Horizontal Stabilizer - between -0.4 and 0.4 -->
<input>fcs/elev-lob-output</input> <!-- Left Outboard Elevator output - between -0.18 and 0.18 -->
<input>fcs/elev-lib-output</input> <!-- Left Inboard Elevator output - between -0.12 and 0.12 -->
<input>fcs/elev-rob-output</input> <!-- Right Outboard Elevator output - between -0.18 and 0.18 -->
<input>fcs/elev-rib-output</input> <!-- Right Inboard Elevator output - between -0.12 and 0.12 -->
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Elevator Trim Control">
<input>fcs/hstb-fbw-output</input>
<range>
<min>-0.35</min>
<max>0.3</max>
</range>
<output>fcs/hstab-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Outboard elevator Control">
<input>fcs/elev-lob-output</input>
<range>
<min>-0.52</min>
<max>0.52</max>
</range>
<output>fcs/elev-lob-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Outboard elevator Control">
<input>fcs/elev-rob-output</input>
<range>
<min>-0.52</min>
<max>0.52</max>
</range>
<output>fcs/elev-rob-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Inboard elevator Control">
<input>fcs/elev-lib-output</input>
<range>
<min>-0.60</min>
<max>0.60</max>
</range>
<output>fcs/elev-lib-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Inboard elevator Control">
<input>fcs/elev-rib-output</input>
<range>
<min>-0.60</min>
<max>0.60</max>
</range>
<output>fcs/elev-rib-pos-rad</output>
</aerosurface_scale>
<!-- FCS: Flight Control System - ROLL AXIS -->
<!-- 10 roll control surfaces - ALRN-LOB, ALRN-LMD, ALRN-LIB, LSP8, LSP7, RSP7, RSP8, ALRN-RIB, ALRN-RMD, ALRN-ROB -->
<summer name="Roll Trim Sum">
<input>fcs/alrn-lob-fbw-output</input> <!-- Left Outboard Aileron - between -0.14 and 0.14 -->
<input>fcs/alrn-lmd-fbw-output</input> <!-- Left Outboard Aileron - between -0.10 and 0.10 -->
<input>fcs/alrn-lib-fbw-output</input> <!-- Left Outboard Aileron - between -0.09 and 0.09 -->
<input>fcs/lsp8-fbw-output</input> <!-- Left Spoiler 8 - between -0.09 and 0.00 -->
<input>fcs/lsp7-fbw-output</input> <!-- Left Spoiler 7 - between -0.08 and 0.00 -->
<input>fcs/alrn-rob-fbw-output</input> <!-- Left Outboard Aileron - between -0.14 and 0.14 -->
<input>fcs/alrn-rmd-fbw-output</input> <!-- Left Outboard Aileron - between -0.10 and 0.10 -->
<input>fcs/alrn-rib-fbw-output</input> <!-- Left Outboard Aileron - between -0.09 and 0.09 -->
<input>fcs/rsp8-fbw-output</input> <!-- Right Spoiler 8 - between 0.00 and 0.09 -->
<input>fcs/rsp7-fbw-output</input> <!-- Right Spoiler 7 - between 0.00 and 0.08-->
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Left Outboard Aileron Control">
<input>fcs/alrn-lob-fbw-output</input>
<range>
<min>-0.35</min>
<max>0.35</max>
</range>
<output>fcs/alrn-lob-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Middle Aileron Control">
<input>fcs/alrn-lmd-fbw-output</input>
<range>
<min>-0.35</min>
<max>0.35</max>
</range>
<output>fcs/alrn-lmd-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Inboard Aileron Control">
<input>fcs/alrn-lib-fbw-output</input>
<range>
<min>-0.40</min>
<max>0.40</max>
</range>
<output>fcs/alrn-lib-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Outboard Aileron Control">
<input>fcs/alrn-rob-fbw-output</input>
<range>
<min>-0.35</min>
<max>0.35</max>
</range>
<output>fcs/alrn-rob-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Middle Aileron Control">
<input>fcs/alrn-rmd-fbw-output</input>
<range>
<min>-0.35</min>
<max>0.35</max>
</range>
<output>fcs/alrn-rmd-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Inboard Aileron Control">
<input>fcs/alrn-rib-fbw-output</input>
<range>
<min>-0.40</min>
<max>0.40</max>
</range>
<output>fcs/alrn-rib-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Spoiler 8 Control">
<input>fcs/lsp8-fbw-output</input>
<range>
<min>0</min>
<max>1</max>
</range>
<output>fcs/lsp8-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Spoiler 8 Control">
<input>fcs/rsp8-fbw-output</input>
<range>
<min>0</min>
<max>1</max>
</range>
<output>fcs/rsp8-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Spoiler 7 Control">
<input>fcs/lsp7-fbw-output</input>
<range>
<min>0</min>
<max>0.94</max>
</range>
<output>fcs/lsp7-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Spoiler 7 Control">
<input>fcs/rsp7-fbw-output</input>
<range>
<min>0</min>
<max>0.94</max>
</range>
<output>fcs/rsp7-pos-rad</output>
</aerosurface_scale>
<!-- FCS: Flight Control System - YAW -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-fbw-output</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>
<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>
<!-- All the flaps (excluding slats ofcourse) are controlled by all 3 hydraulic systems, so a combined controller can be used as it has been so far -->
<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>
</kinematic>
<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 name="fcs/leading-edge-flap-cmd-norm">
<input>fcs/slat-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>30.0</position>
<time>9.0</time>
</setting>
</traverse>
<output>fcs/leading-edge-flap-pos-deg</output>
</kinematic>
<kinematic name="fcs/leading-edge-slat-cmd-norm">
<input>fcs/slat-cmd-norm</input>
<traverse>
<setting>
<position>0.0000</position>
<time>0.0000</time>
</setting>
<setting>
<position>20.0</position>
<time>5.0</time>
</setting>
</traverse>
<output>fcs/leading-edge-slat-pos-deg</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>25.0000</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>