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c182t.xml
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c182t.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<!-- Source: http://forum.flightgear.org/viewtopic.php?f=25&t=21664&start=45 -->
<fdm_config name="c182t" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Unknown, HHS, Dany93 </author>
<filecreationdate> 2021-02-19 </filecreationdate>
<version> $Id: c172p.xml,v 1.40 June 2015 $ </version>
<!-- experimental stall and spin, up to flat spin March 2014 -->
<!-- Source: http://forum.flightgear.org/viewtopic.php?f=25&t=21664&start=45 -->
<!-- this file with comments for stall and spin to help -->
<!-- from further modifications for c172p-detailed 2015 -->
<!--many coefficients from David Megginson: http://www.megginson.com/Aviation/roskam-coefficients.html#sec.data-->
<description> Cessna C-182S </description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 174 </wingarea>
<wingspan unit="FT"> 36 </wingspan>
<chord unit="FT"> 4.9 </chord>
<htailarea unit="FT2"> 21.9 </htailarea>
<htailarm unit="FT"> 17.7 </htailarm>
<vtailarea unit="FT2"> 16.5 </vtailarea>
<vtailarm unit="FT">17.7 </vtailarm>
<location name="AERORP" unit="IN">
<x>37.37 </x>
<y> 0 </y>
<z>32.94 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> -13 </x>
<y> 0 </y>
<z> 23.68 </z>
</location>
<location name="VRP" unit="IN"><!--Datum according POH -->
<x>-3.25</x>
<y> 0 </y>
<z>0 </z>
</location>
</metrics>
<mass_balance> <!--SLUG*FT2 from http://www.megginson.com/Aviation/roskam-coefficients.html#sec.data-->
<ixx unit="SLUG*FT2"> 948 </ixx>
<iyy unit="SLUG*FT2"> 1346 </iyy>
<izz unit="SLUG*FT2"> 1967</izz>
<ixy unit="SLUG*FT2"> -0 </ixy>
<ixz unit="SLUG*FT2"> -0 </ixz>
<iyz unit="SLUG*FT2"> -0 </iyz>
<emptywt unit="LBS"> 1925 </emptywt>
<location name="CG" unit="IN">
<x>40.31</x><!--according to POH and W&B calculator http://www.freechecklists.net/Resources/Cessna/182S+Skylane/-->
<y> 0 </y>
<z> 0 </z>
</location>
<pointmass name="Pilot">
<weight unit="LBS"> 180 </weight>
<location name="POINTMASS" unit="IN">
<x> 37 </x>
<y>-9.88</y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="Co-Pilot">
<weight unit="LBS"> 0 </weight> <!-- <weight unit="LBS">180</weight> -->
<location name="POINTMASS" unit="IN">
<x> 37 </x>
<y> 9.88 </y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="Left Passenger">
<weight unit="LBS"> 0 </weight> <!-- <weight unit="LBS">180</weight> -->
<location name="POINTMASS" unit="IN">
<x> 74 </x>
<y> -9.88 </y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="Right Passenger">
<weight unit="LBS"> 0 </weight> <!-- <weight unit="LBS">180</weight> -->
<location name="POINTMASS" unit="IN">
<x> 74 </x>
<y> 9.88 </y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="BaggageA">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 97 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="BaggageB">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 116 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</pointmass>
<pointmass name="Ice">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x>37.37 </x>
<y> 0 </y>
<z>32.94 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<!-- based on: https://www.researchgate.net/figure/Typical-air-spring-and-oil-damper-force-curves-for-a-light-aircraft_fig3_224989810-->
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x>-10.31 </x>
<y> 0 </y>
<z>-47.09</z><!--includes offset due to gear compression animation, should be -47.17-->
</location>
<static_friction> 1.4 </static_friction>
<dynamic_friction> 0.6 </dynamic_friction>
<rolling_friction> 0.03 </rolling_friction>
<strut_force>
<function>
<sum>
<product>
<value>-1</value>
<table>
<independentVar>gear/unit[0]/compression-ft</independentVar>
<tableData>
0.00 000
0.005 258
0.05 516
0.15 774
0.40 2400
</tableData>
</table>
</product>
<ifthen>
<ge>
<property> gear/unit[0]/compression-velocity-fps </property>
<value> 0.0 </value>
</ge>
<product>
<value>-1</value>
<table>
<independentVar> gear/unit[0]/compression-velocity-fps </independentVar>
<tableData>
-18.00 -13500
-9.18 -4500
0.00 0
9.18 4500
18.0 13500
</tableData>
</table>
</product>
<product>
<value>-1</value>
<property> fcs/gear-compression-velocity-dep-nose</property>
<property> gear/unit[0]/compression-velocity-fps </property>
</product>
</ifthen>
</sum>
</function>
</strut_force>
<!--<spring_coeff unit="LBS/FT">2400 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">490 </damping_coeff>
<damping_coeff_rebound type="SQUARE" unit="LBS/FT2/SEC2">0</damping_coeff_rebound>-->
<max_steer unit="DEG"> 29 </max_steer><!-- limited to 10 deg NWS, but can turn up to 30 with side force -->
<table name="CORNERING_COEFF" type="internal">
<tableData> <!-- jsbsim-pacejka.py 5.0 0.03 2.85 1.4 1.03 1.4 https://github.com/JSBSim-Team/jsbsim/issues/127 https://github.com/JSBSim-Team/jsbsim/issues/127-->
-90.0 -0.6276256632207626
-85.0 -0.6417393571173159
-80.0 -0.6578124074897472
-75.0 -0.6761339658692869
-70.0 -0.6970340668693019
-65.0 -0.7208796953965572
-60.0 -0.7480586200367123
-55.0 -0.7789376993218241
-50.0 -0.8137693871814174
-45.0 -0.852494972166421
-40.0 -0.8943455737614107
-35.0 -0.9370583530652546
-30.0 -0.9754028875043508
-25.0 -0.9986292585314367
-20.0 -0.9867956894252938
-15.0 -0.9078708239414398
-10.0 -0.722622440415344
-5.0 -0.4088092889390962
0.0 0.0
5.0 0.4088092889390962
10.0 0.722622440415344
15.0 0.9078708239414398
20.0 0.9867956894252938
25.0 0.9986292585314367
30.0 0.9754028875043508
35.0 0.9370583530652546
40.0 0.8943455737614107
45.0 0.852494972166421
50.0 0.8137693871814174
55.0 0.7789376993218241
60.0 0.7480586200367123
65.0 0.7208796953965572
70.0 0.6970340668693019
75.0 0.6761339658692869
80.0 0.6578124074897472
85.0 0.6417393571173159
90.0 0.6276256632207626
</tableData>
</table>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="IN">
<x>54.43 </x>
<y>-51.56 </y>
<z>-43.67 </z><!--includes offset due to gear compression animation, should be -41.56-->
</location>
<static_friction> 0.5 </static_friction>
<dynamic_friction> 0.4</dynamic_friction>
<rolling_friction> 0.03 </rolling_friction>
<!--<strut_force>
<function>
<sum>
<product>
<value>-1</value>
<table>
<independentVar>gear/unit[1]/compression-ft</independentVar>
<tableData>
0.00 000
0.4 3600
</tableData>
</table>
</product>
<ifthen>
<ge>
<property> gear/unit[1]/compression-velocity-fps </property>
<value> 0</value>
</ge>
<product>
<value>-1</value>
<table>
<independentVar> gear/unit[1]/compression-velocity-fps </independentVar>
<tableData>
-1 -442
0.00 0
1 442
</tableData>
</table>
</product>
<product>
<value>-1</value>
<property> fcs/gear-compression-velocity-dep</property>
<property> gear/unit[1]/compression-velocity-fps </property>
</product>
</ifthen>
</sum>
</function>
</strut_force>-->
<spring_coeff unit="LBS/FT">3600 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">295</damping_coeff>
<damping_coeff_rebound type="SQUARE" unit="LBS/FT2/SEC2">295 </damping_coeff_rebound>
<max_steer unit="DEG"> 0.0 </max_steer>
<table name="CORNERING_COEFF" type="internal">
<tableData> <!-- jsbsim-pacejka.py 5.0 0.06 2.8 0.5 1.03 0.5 -->
-90.0 -0.5760395836174765
-85.0 -0.5776440181093163
-80.0 -0.5803918992801416
-75.0 -0.584501031700121
-70.0 -0.5902476568617109
-65.0 -0.5979865464058901
-60.0 -0.6081793463286825
-55.0 -0.6214348494943271
-50.0 -0.6385661913510731
-45.0 -0.6606706311692149
-40.0 -0.6892340269266315
-35.0 -0.726240829612553
-30.0 -0.7741813043425955
-25.0 -0.8355026710967953
-20.0 -0.9097416834082445
-15.0 -0.9818532434458513
-10.0 -0.9824937511496707
-5.0 -0.7127565569007203
0.0 0.0
5.0 0.7127565569007203
10.0 0.9824937511496707
15.0 0.9818532434458513
20.0 0.9097416834082445
25.0 0.8355026710967953
30.0 0.7741813043425955
35.0 0.726240829612553
40.0 0.6892340269266315
45.0 0.6606706311692149
50.0 0.6385661913510731
55.0 0.6214348494943271
60.0 0.6081793463286825
65.0 0.5979865464058901
70.0 0.5902476568617109
75.0 0.584501031700121
80.0 0.5803918992801416
85.0 0.5776440181093163
90.0 0.5760395836174765
</tableData>
</table>
<brake_group> LEFT </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="IN">
<x>54.43 </x>
<y>51.56 </y>
<z>-43.67 </z><!--includes offset due to gear compression animation, should be -41.56-->
</location>
<static_friction> 0.5</static_friction>
<dynamic_friction> 0.4 </dynamic_friction>
<rolling_friction> 0.03 </rolling_friction>
<!--<strut_force>
<function>
<sum>
<product>
<value>-1</value>
<table>
<independentVar>gear/unit[2]/compression-ft</independentVar>
<tableData>
0.00 000
0.4 3600
</tableData>
</table>
</product>
<ifthen>
<ge>
<property> gear/unit[2]/compression-velocity-fps </property>
<value> 0.1 </value>
</ge>
<product>
<value>-1</value>
<table>
<independentVar> gear/unit[2]/compression-velocity-fps </independentVar>
<tableData>
-1 -442
0.00 0
1 442
</tableData>
</table>
</product>
<product>
<value>-1</value>
<property> fcs/gear-compression-velocity-dep</property>
<property> gear/unit[2]/compression-velocity-fps </property>
</product>
</ifthen>
</sum>
</function>
</strut_force>-->
<spring_coeff unit="LBS/FT">3600 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">295</damping_coeff>
<damping_coeff_rebound type="SQUARE" unit="LBS/FT2/SEC2">295</damping_coeff_rebound>
<max_steer unit="DEG"> 0.0 </max_steer>
<table name="CORNERING_COEFF" type="internal">
<tableData> <!-- jsbsim-pacejka.py 5.0 0.06 2.8 0.5 1.03 0.5 -->
-90.0 -0.5760395836174765
-85.0 -0.5776440181093163
-80.0 -0.5803918992801416
-75.0 -0.584501031700121
-70.0 -0.5902476568617109
-65.0 -0.5979865464058901
-60.0 -0.6081793463286825
-55.0 -0.6214348494943271
-50.0 -0.6385661913510731
-45.0 -0.6606706311692149
-40.0 -0.6892340269266315
-35.0 -0.726240829612553
-30.0 -0.7741813043425955
-25.0 -0.8355026710967953
-20.0 -0.9097416834082445
-15.0 -0.9818532434458513
-10.0 -0.9824937511496707
-5.0 -0.7127565569007203
0.0 0.0
5.0 0.7127565569007203
10.0 0.9824937511496707
15.0 0.9818532434458513
20.0 0.9097416834082445
25.0 0.8355026710967953
30.0 0.7741813043425955
35.0 0.726240829612553
40.0 0.6892340269266315
45.0 0.6606706311692149
50.0 0.6385661913510731
55.0 0.6214348494943271
60.0 0.6081793463286825
65.0 0.5979865464058901
70.0 0.5902476568617109
75.0 0.584501031700121
80.0 0.5803918992801416
85.0 0.5776440181093163
90.0 0.5760395836174765
</tableData>
</table>
<brake_group> RIGHT </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="TAIL_SKID">
<location unit="IN">
<x> 219.33 </x>
<y> 0 </y>
<z> 4.15 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT"> 1900 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 540 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="belly_front">
<location unit="IN">
<x>0.021 </x>
<y>0.0 </y>
<z> -15.29 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">100 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="belly_aft_left">
<location unit="IN">
<x>62 </x>
<y>-10.36 </y>
<z> -21.31 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="belly_aft_right">
<location unit="IN">
<x>62 </x>
<y>10.36 </y>
<z> -21.31 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000</damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="LEFT_WINGTIP">
<location unit="IN">
<x>12.03 </x>
<y>-212.86 </y>
<z> 33.37 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="RIGHT_WINGTIP">
<location unit="IN">
<x> 12.03 </x>
<y> 212.86 </y>
<z> 33.37 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="NOSETIP">
<location unit="IN">
<x> -92.50 </x>
<y> 0</y>
<z> 0 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT"> 100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="ROOF_FRONT">
<location unit="IN">
<x> -4.82 </x>
<y> 0</y>
<z> 31.37 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="ROOF_BACK">
<location unit="IN">
<x>58.47</x>
<y> 0</y>
<z>30.62 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="STRUCTURE" name="HSTAB_TIP">
<location unit="IN">
<x> 214.47 </x>
<y> 0</y>
<z>79.41 </z>
</location>
<static_friction> 1.0 </static_friction>
<dynamic_friction> 1.0 </dynamic_friction>
<rolling_friction> 1.0 </rolling_friction>
<spring_coeff unit="LBS/FT">100 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC">1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>
<propulsion>
<engine file="engIO540AB1A5">
<location unit="IN">
<x>-40.94 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>5</feed>
<thruster file="prop_79in3v">
<location unit="IN">
<x> -73.62 </x>
<y> 0 </y>
<z> 0</z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
<sense> 1 </sense>
<p_factor>15 </p_factor>
</thruster>
</engine>
<!-- 0: left wing -->
<tank type="FUEL"> <!-- Tank number 0 with 44 gallons =290.5lbs ?? kerosin but should be AVGas!-->
<location unit="IN">
<x> 36.27 </x>
<y>-59.49 </y>
<z> 31.21</z>
</location>
<drain_location unit="M">
<x> 1.057 </x>
<y>-1.11821 </y>
<z> 0.68779 </z>
</drain_location>
<capacity unit="LBS"> 264.88 </capacity>
<contents unit="LBS"> 264.88</contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<standpipe>2</standpipe>
<type>AVGAS</type>
</tank>
<!-- 1: right wing -->
<tank type="FUEL"> <!-- Tank number 1 with 44 gallons =290.5lbs kerosin but should be AVGas!-->
<location unit="IN">
<x> 36.27 </x>
<y> 59.49 </y>
<z> 31.21 </z>
</location>
<drain_location unit="M">
<x> 1.057 </x>
<y> 1.11821 </y>
<z> 0.68779 </z>
</drain_location>
<capacity unit="LBS"> 264.88 </capacity>
<contents unit="LBS"> 264.88 </contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<standpipe>2</standpipe>
<type>AVGAS</type>
</tank>
<!-- 2: Fuel selector sump -->
<tank type="FUEL">
<location unit="IN">
<x>0.45</x>
<y>0</y>
<z>-0.40</z>
</location>
<drain_location unit="M">
<x>0.45</x>
<y>0</y>
<z>-0.45</z>
</drain_location>
<capacity unit="LBS">0.1</capacity> <!-- todo: arbitrary numer as i dont know exact ones -->
<contents unit="LBS">0</contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<type>AVGAS</type>
</tank>
<!-- 3: Strainer sump -->
<tank type="FUEL">
<location unit="IN">
<x>-0.28</x>
<y>0</y>
<z>-0.30</z>
</location>
<drain_location unit="M">
<x>-0.28</x>
<y>0</y>
<z>-0.50</z>
</drain_location>
<capacity unit="LBS">0.1</capacity>
<contents unit="LBS">0</contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<type>AVGAS</type>
</tank>
<!-- 4: Fuel pipe -->
<tank type="FUEL">
<location unit="IN">
<x>-0.35</x>
<y>0</y>
<z>-0.30</z>
</location>
<drain_location unit="M">
<x>-0.35</x>
<y>0</y>
<z>-0.50</z>
</drain_location>
<capacity unit="LBS">0.05</capacity>
<contents unit="LBS">0</contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<type>AVGAS</type>
</tank>
<!-- 5: engine manifold (engine feeds from here) -->
<tank type="FUEL">
<location unit="IN">
<x>-0.60</x>
<y>0</y>
<z>-0.30</z>
</location>
<drain_location unit="M">
<x>-0.60</x>
<y>0</y>
<z>-0.50</z>
</drain_location>
<capacity unit="LBS">0.1</capacity>
<contents unit="LBS">0</contents>
<temperature>50</temperature>
<density unit="LBS/GAL"> 6.02 </density>
<type>AVGAS</type>
</tank>
<!-- 6: "virtual" mix-to-engine tank (workaround for starter mixture) -->
<tank type="FUEL">
<location unit="IN">
<x>0</x>
<y>0</y>
<z>0</z>
</location>
<drain_location unit="M">
<x>0</x>
<y>0</y>
<z>0</z>
</drain_location>
<capacity unit="LBS">0.001</capacity>
<contents unit="LBS">0</contents>
<priority>0</priority>
</tank>
</propulsion>
<system file="fuel"/> <!-- integrate advanced fuel system -->
<system file="external-heat"/> <!-- integrate external-heater -->
<system file="electrical"/> <!-- load electrical system -->
<system file="cabin-heat_and_air"/> <!-- cabin heat and air -->
<system file="damage"/> <!-- integrate damage detection -->
<system file="static-sources"/> <!-- integrate alternate static source simulation -->
<system file="towbar"/> <!-- integrate towbar -->
<flight_control name="FCS: c182s">
<!--Cessna 182S POH Page 7-12: nose gear steer deg=11deg, by applying left or right brake increasing steer deg up to 29deg-->
<!-- Control input channel, inspired from PA28 -->
<!-- https://sourceforge.net/p/flightgear/fgaddon/HEAD/tree/trunk/Aircraft/PA28/Systems/pa28-fcs.xml#l11 -->
<!-- see discussion in https://github.com/HHS81/c182s/pull/582#issuecomment-2030922438 -->
<channel name="Control Inputs">
<lag_filter name="fcs/aileron-yoke">
<input>/controls/flight/aileron</input>
<c1>20</c1>
</lag_filter>
<lag_filter name="fcs/elevator-yoke">
<input>/controls/flight/elevator</input>
<c1>20</c1>
</lag_filter>
<lag_filter name="fcs/elevator-trim-knob">
<input>/controls/flight/elevator-trim</input>
<c1>20</c1>
</lag_filter>
<lag_filter name="fcs/rudder-pedal">
<input>/controls/flight/rudder</input>
<c1>20</c1>
</lag_filter>
<lag_filter name="fcs/rudder-trim-knob">
<input>/controls/flight/rudder-trim</input>
<c1>20</c1>
</lag_filter>
</channel>
<channel name="ground reaction">
<!-- can be used for idividuell damping as an example based on velocity or anything else-->
<fcs_function name="fcs/gear-compression-velocity-dep-nose">
<function>
<table>
<independentVar>velocities/u-fps</independentVar>
<tableData>
0.0 0
110 0
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="fcs/gear-compression-velocity-dep">
<function>
<table>
<independentVar>velocities/u-fps</independentVar>
<tableData>
0.0 442
110 442
</tableData>
</table>
</function>
</fcs_function>
</channel>
<!-- following code by Jonathan Redpath aka legoboyvdlp-->
<channel name="NWS">
<switch name="fcs/nws-enabled">
<default value="0"/>
<test logic="OR" value="1"> <!-- NWS mechanically centered if gear is fully extended -->
/gear/gear[0]/compression-norm gt 0.001
</test>
</switch>
<fcs_function name="left brake nose-gear">
<function name="fcs/nose-gear-left-brake-steer-factor">
<product>
<property>fcs/left-brake-cmd-norm</property>
<value>-1</value>
</product>
</function>
</fcs_function>
<fcs_function name="right brake nose-gear">
<function name="fcs/nose-gear-right-brake-steer-factor">
<product>
<property>fcs/right-brake-cmd-norm</property>
<value>1</value>
</product>
</function>
</fcs_function>
<summer name="fcs/brake-sum">
<input>fcs/nose-gear-right-brake-steer-factor</input>
<input>fcs/nose-gear-left-brake-steer-factor</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<switch name="fcs/brake-influence-enabled"> <!-- brake should not influence nws if the aircraft is not moving -->
<default value="0"/>
<test logic="OR" value="1">
/gear/gear[0]/rollspeed-ms gt 0.25
</test>
</switch>
<fcs_function name="fcs/brake-sum-adjusted">
<function>
<product>
<property>fcs/brake-influence-enabled</property>
<property>fcs/brake-sum</property>
</product>
</function>
</fcs_function>
<fcs_function name="fcs/nws-cmd-deg"> <!-- Drive the nose wheel with the rudder and brakes -->
<function>
<table>
<independentVar lookup="row">fcs/brake-sum-adjusted</independentVar>
<independentVar lookup="column">/controls/flight/rudder</independentVar>
<tableData>
-1 0 1
-1 -29 0 11
0 -11 0 11
1 -11 0 29
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="fcs/nws-cmd-deg-adjusted">
<function>
<product>
<property>fcs/nws-cmd-deg</property>
<property>fcs/nws-enabled</property>
</product>
</function>
</fcs_function>
<actuator name="fcs/steer-deg-actuator">
<input>fcs/nws-cmd-deg-adjusted</input>
<rate_limit>80</rate_limit> <!-- 80 deg / s , or 1/8 second to full deflection with NWS -->
<output>fcs/steer-pos-deg-actuator</output>
</actuator>
<switch name="fcs/steer-pos-deg">
<default value="fcs/steer-pos-deg-actuator"/>
<test value="external_reactions/towbar/steer-deg">
external_reactions/towbar/attached eq 1
gear/unit[0]/WOW eq 1
</test>
</switch>
</channel>
<channel name="Pitch">
<summer name="Pitch Trim Sum">
<input>fcs/elevator-yoke</input>
<input>fcs/elevator-trim-knob</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Elevator Control">
<input>fcs/pitch-trim-sum</input>
<gain>0.01745</gain>
<range>
<min>-28</min>
<max>21</max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Elevator Position Normalized">
<input>fcs/elevator-pos-deg</input>
<domain>
<min>-28</min>
<max>21</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-yoke</input>
<input>fcs/roll-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
<output>fcs/roll-trim-sum</output>
</summer>
<summer name="Aileron Norm Left">
<input>fcs/roll-trim-sum</input>
<clipto>
<min>-1.0</min>
<max>1.0</max>
</clipto>
<output>fcs/left-aileron-pos-norm</output>
</summer>
<aerosurface_scale name="Left Aileron Control">
<input>fcs/roll-trim-sum</input>
<range>
<min>-0.366519</min>
<max>0.261799</max>
</range>
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
<summer name="Aileron Norm Right">
<input>fcs/roll-trim-sum</input>
<clipto>
<min>-1.0</min>
<max>1.0</max>
</clipto>
<output>fcs/right-aileron-pos-norm</output>
</summer>
<aerosurface_scale name="Right Aileron Control">
<input>fcs/roll-trim-sum</input>
<range>
<min>0.261799 </min>
<max>-0.366519</max>
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
</channel>
<channel name="Yaw">
<summer name="Yaw Trim Sum">
<input>-fcs/rudder-pedal</input>
<input>-fcs/rudder-trim-knob</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control"><!-- Perpendicular to hinge line-->
<input>fcs/yaw-trim-sum</input>
<gain>0.01745</gain>
<range>
<min>-27</min>
<max>27</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder Position Normalized">
<input>fcs/rudder-pos-deg</input><!-- Perpendicular to hinge line-->
<domain>
<min>-27</min>
<max>27</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>