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Su-27.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="Su-27SK" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<metrics>
<wingarea unit="M2"> 62.0 </wingarea>
<wingspan unit="M" > 14.7 </wingspan>
<wing_incidence> 2.0 </wing_incidence>
<chord unit="M" > 4.2 </chord>
<htailarea unit="FT2"> 133.49 </htailarea>
<htailarm unit="M" > 18.0 </htailarm>
<vtailarea unit="FT2"> 120.14 </vtailarea>
<vtailarm unit="M" > 17.5 </vtailarm>
<location name="AERORP" unit="M">
<x> 13.3 </x>
<y> 0.0 </y>
<z> -0.5 </z>
</location>
<location name="EYEPOINT" unit="M">
<x> 5.0 </x>
<y> 0.0 </y>
<z> 1.5 </z>
</location>
<location name="VRP" unit="M">
<x>0</x>
<y>0</y>
<z>0</z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 54859 </ixx>
<iyy unit="SLUG*FT2"> 167365 </iyy>
<izz unit="SLUG*FT2"> 169937 </izz>
<emptywt unit="KG" > 16380 </emptywt>
<location name="CG" unit="M">
<x> 13.2 </x>
<y> 0.0 </y>
<z> -0.5 </z>
</location>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE_GEAR">
<location unit="M">
<x> 7.80 </x>
<y> 0.00 </y>
<z> -2.30 </z>
</location>
<static_friction> 0.9 </static_friction>
<dynamic_friction> 0.6 </dynamic_friction>
<rolling_friction> 0.01 </rolling_friction>
<spring_coeff unit="LBS/FT"> 20000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<max_steer unit="DEG"> 35.00 </max_steer>
<brake_group>NONE</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_GEAR">
<location unit="M">
<x> 13.70 </x>
<y> -2.20 </y>
<z> -2.52 </z>
</location>
<static_friction> 0.9 </static_friction>
<dynamic_friction> 0.6 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 35000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>LEFT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_GEAR">
<location unit="M">
<x> 13.7 </x>
<y> 2.2 </y>
<z> -2.5 </z>
</location>
<static_friction> 0.9 </static_friction>
<dynamic_friction> 0.6 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 35000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10000 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group>RIGHT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="STRUCTURE" name="NOSE">
<location unit="M">
<x> 0.0 </x>
<y> 0.0 </y>
<z> 0.0 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="LEFT_BODY">
<location unit="M">
<x> 11.0 </x>
<y> -1.3 </y>
<z> -1.0 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_BODY">
<location unit="M">
<x> 11.0 </x>
<y> 1.3 </y>
<z> -1.0 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="LEFT_WING">
<location unit="M">
<x> 16.0 </x>
<y> -7.6 </y>
<z> 0.3 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="M">
<x> 16.0 </x>
<y> 7.6 </y>
<z> 0.3 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="LEFT_VSTAB">
<location unit="M">
<x> 17.6 </x>
<y> -2.2 </y>
<z> 3.8 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_VSTAB">
<location unit="M">
<x> 17.6 </x>
<y> 2.2 </y>
<z> 3.8 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 81585.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16317.00 </damping_coeff>
</contact>
</ground_reactions>
<propulsion>
<engine file="Saturn-AL-31">
<feed>0</feed>
<feed>1</feed>
<feed>2</feed>
<feed>3</feed>
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 802.25 </x>
<y> -20.00 </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="Saturn-AL-31">
<feed>0</feed>
<feed>1</feed>
<feed>2</feed>
<feed>3</feed>
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 802.25 </x>
<y> 20.00 </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"> <!-- Tank1 fuselage afterproue -->
<location unit="IN">
<x> 260.35 </x>
<y> 0.00 </y>
<z> -21.56 </z>
</location>
<capacity unit="LBS"> 7010.70 </capacity>
<contents unit="LBS"> 3505.35 </contents>
</tank>
<tank type="FUEL" number="1"> <!-- Tank2 Main center fuselage -->
<location unit="IN">
<x> 517.35 </x>
<y> 0.00 </y>
<z> -21.56 </z>
</location>
<capacity unit="LBS"> 9171.23 </capacity>
<contents unit="LBS"> 4585.61 </contents>
</tank>
<tank type="FUEL" number="2"> <!-- Tank3L L.wing -->
<location unit="IN">
<x> 517.35 </x>
<y> -137 </y>
<z> -21.56 </z>
</location>
<capacity unit="LBS"> 1168.45 </capacity>
<contents unit="LBS"> 584.22 </contents>
</tank>
<tank type="FUEL" number="3"> <!-- Tank3R R.wing -->
<location unit="IN">
<x> 517.35 </x>
<y> 137 </y>
<z> -21.56 </z>
</location>
<capacity unit="LBS"> 1168.45 </capacity>
<contents unit="LBS"> 584.22 </contents>
</tank>
<tank type="FUEL" number="4"> <!-- Tank4 rear fuselage -->
<location unit="IN">
<x> 669.29 </x>
<y> 0.00 </y>
<z> -21.56 </z>
</location>
<capacity unit="LBS"> 2204.62 </capacity>
<contents unit="LBS"> 1102.31 </contents>
</tank>
</propulsion>
<system file="jsb-electrical"/>
<flight_control file="Systems/jsb-controls"/>
<aerodynamics file="Systems/jsb-aerodynamics.xml"/>
</fdm_config>