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CS100-JSB.xml
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CS100-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="A320family" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author>D-ECHO based on A318 by Joshua Davidson (it0uchpods)</author>
<version>Pre V1.0</version>
<description>Bombardier CSeries CS100</description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 1209 </wingarea>
<wingspan unit="FT" > 115 </wingspan>
<wing_incidence> 1.03 </wing_incidence>
<chord unit="M" > 6.3 </chord>
<htailarea unit="FT2"> 334.24 </htailarea>
<htailarm unit="FT" > 57.88 </htailarm>
<vtailarea unit="FT2"> 248.79 </vtailarea>
<vtailarm unit="FT" > 57.33 </vtailarm>
<location name="AERORP" unit="M">
<x> -3.5 </x>
<y> 0 </y>
<z> -3 </z>
</location>
<location name="EYEPOINT" unit="M">
<x> -14.5 </x>
<y> -0.5 </y>
<z> -1.5 </z>
</location>
<location name="VRP" unit="IN">
<x> 0.0 </x>
<y> 0.0 </y>
<z> 0.0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 611903</ixx>
<iyy unit="SLUG*FT2">1735389</iyy>
<izz unit="SLUG*FT2">2301293</izz>
<ixy unit="SLUG*FT2">0</ixy>
<ixz unit="SLUG*FT2">0</ixz>
<iyz unit="SLUG*FT2">0</iyz>
<emptywt unit="KG">77650</emptywt>
<location name="CG" unit="M">
<x> -4.5 </x>
<y> 0 </y>
<z> -3 </z>
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight>
<!-- MAX: 7500.126lbs -->
<location name="POINTMASS" unit="IN">
<x>383.4792</x>
<y>0</y>
<z>-29.5</z>
<!-- 1.5m and now half of it for the center point of the load -->
</location>
</pointmass>
<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
<pointmass name="Cargo Hold 3">
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
<z>-29.5</z>
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
<z>-29.5</z>
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight>
<!-- MAX: 3300.320lbs -->
<location name="POINTMASS" unit="IN">
<x>1068.2634</x>
<y>0</y>
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<!-- REF-1 page 165 + 271 -->
<contact type="BOGEY" name="NOSE_LG">
<location unit="M">
<x> -13.95082 </x>
<y> 0 </y>
<z> -5.60434 </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"> 30935.5 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
<max_steer unit="DEG"> 70 </max_steer>
<!-- REF-1 page 133 -->
<brake_group> NOSE </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MLG">
<location unit="M">
<x> -1.14043 </x>
<y> -2.99817 </y>
<z> -5.73159 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MLG">
<location unit="M">
<x> -1.14043 </x>
<y> 2.99817 </y>
<z> -5.73159 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>1</retractable>
</contact>
<contact type="STRUCTURE" name="NOSE_1">
<location unit="M">
<x> -17.3523 </x>
<y> 0 </y>
<z> -3 </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"> 50000 </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_2">
<location unit="M">
<x> -14.96695 </x>
<y> 0 </y>
<z> -3.89475 </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"> 50000 </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="CENTER_1">
<location unit="M">
<x> -4.30219 </x>
<y> 0 </y>
<z> -4.51197 </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"> 50000 </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="CENTER_2">
<location unit="M">
<x> 0.53396 </x>
<y> 0 </y>
<z> -4.50047 </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"> 50000 </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="ENG_1">
<location unit="M">
<x>-5.76446</x>
<y>-5.53916</y>
<z>-5.18418</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"> 50000 </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="ENG_2">
<location unit="M">
<x>-5.76446</x>
<y>5.53916</y>
<z>-5.18418</z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.4 </rolling_friction>
<spring_coeff unit="LBS/FT"> 50000 </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="TAIL_1">
<location unit="M">
<x> 6.71252 </x>
<y> 0 </y>
<z> -3.95646 </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"> 50000 </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="TAIL_2">
<location unit="M">
<x> 17.6725 </x>
<y> 0 </y>
<z> -1.49885 </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"> 50000 </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="TAIL_3">
<location unit="M">
<x> 17 </x>
<y> 0 </y>
<z> 5.86 </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"> 50000 </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="TAIL_4">
<location unit="M">
<x> 15 </x>
<y> 0 </y>
<z> 5.65</z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<rolling_friction> 1 </rolling_friction>
<spring_coeff unit="LBS/FT"> 50000 </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="WING_TIP_1">
<location unit="M">
<x> 3.2 </x>
<y> -16 </y>
<z> -1.1 </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"> 50000 </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="WING_TIP_2">
<location unit="M">
<x> 4.65 </x>
<y> -17.3 </y>
<z> 0.35 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<rolling_friction> 1 </rolling_friction>
<spring_coeff unit="LBS/FT"> 50000 </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="WING_TIP_3">
<location unit="M">
<x> 3.2 </x>
<y> 16 </y>
<z> -1.1 </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"> 50000 </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="WING_TIP_4">
<location unit="M">
<x> 4.65 </x>
<y> 17.3 </y>
<z> 0.35 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<rolling_friction> 1 </rolling_friction>
<spring_coeff unit="LBS/FT"> 50000 </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="pw1524g">
<location unit="M">
<x> -5.87913 </x>
<y> -5.53646 </y>
<z> -4.01434 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
<feed>7</feed>
<thruster file="direct">
<location unit="M">
<x> -5.08913 </x>
<y> -5.53646 </y>
<z> -4.01434 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
</thruster>
</engine>
<engine file="pw1524g">
<location unit="M">
<x> -5.87913 </x>
<y> 5.53646 </y>
<z> -4.01434 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
<feed>8</feed>
<thruster file="direct">
<location unit="M">
<x> -5.08913 </x>
<y> 5.53646 </y>
<z> -4.01434 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
</thruster>
</engine>
<!--Tanks: 13,785.63 litres of fuel-->
<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
<location unit="IN">
<x> 783.0709 </x>
<y> -574.4148 </y>
<z> 3.1080 </z>
</location>
<capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
<contents unit="LBS"> 0 </contents>
<priority>4</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
<location unit="IN">
<x> 739.5669 </x>
<y> -457.4259 </y>
<z> -8.0898 </z>
</location>
<capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
<contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
<location unit="IN">
<x> 652.5591 </x>
<y> -236.2992 </y>
<z> -33.9470 </z>
</location>
<capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
<contents unit="LBS"> 4480 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<priority>3</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Center Tank 3 -->
<location unit="IN">
<x> 522.0473 </x>
<y> 0 </y>
<z> -47.0 </z>
</location>
<capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
<contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
<priority>1</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
<location unit="IN">
<x> 652.5591 </x>
<y> 236.2992 </y>
<z> -33.9470 </z>
</location>
<capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
<contents unit="LBS"> 4480 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
<priority>3</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
<location unit="IN">
<x> 739.5669 </x>
<y> 457.4259 </y>
<z> -8.0898 </z>
</location>
<capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
<contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
<location unit="IN">
<x> 783.0709 </x>
<y> 574.4148 </y>
<z> 3.1080 </z>
</location>
<capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
<contents unit="LBS"> 0 </contents>
<priority>4</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
<location unit="IN">
<x>589.735</x>
<y>0</y>
<z>-45.567</z>
</location>
<capacity unit="LBS"> 100 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>1</priority>
<type>JET-A1</type>
</tank>
<tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
<location unit="IN">
<x>589.735</x>
<y>0</y>
<z>-45.567</z>
</location>
<capacity unit="LBS"> 100 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>1</priority>
<type>JET-A1</type>
</tank>
</propulsion>
<system file="pushback" /><!--
<system file="fuel" />-->
<system file="glass-effect1" />
<system file="fmgc" />
<system file="fcs" />
<flight_control name="none"/>
<aerodynamics file="Systems/cs100-aerodynamics.xml" />
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>