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IDG-A32X/A320-200-IAE.xml

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First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
fix autospoiler, bugfixes, Upper-ECAM finished, except warnings and flap/slat indicator
2016-11-06 04:38:16 +00:00
<fdm_config name="A320family" version="2.0" release="BETA"
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Bicyus (Jon Ortuondo) </author>
<email> bicyus@gmail.com </email>
<filecreationdate> 2012-02-15 </filecreationdate>
<version> 0.99 </version>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<description> Airbus A320-200 with IAE V2500 Engines </description>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<note> Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<limitation></limitation>
</fileheader>
<metrics>
<wingarea unit="FT2"> 1319.79 </wingarea>
<wingspan unit="FT" > 111.26 </wingspan>
<wing_incidence> 1.03 </wing_incidence>
<chord unit="FT" > 13.76 </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="IN">
<x> 642.122 </x>
<y> 0 </y>
<z> -25.2091 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 80 </x>
<y> -30 </y>
<z> 70 </z>
</location>
<location name="VRP" unit="IN">
<x> 661.1 </x>
<y> 0 </y>
<z> -37 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 611903 </ixx>
<iyy unit="SLUG*FT2"> 1735389 </iyy>
<izz unit="SLUG*FT2"> 2301293 </izz>
<!--
___________________A320_________A330__________A340
BOW_____________178000________270000________283925
SPAN______________144___________198___________209
LENGTH____________153___________209___________209
ROLL MOI_________1725000______5727777_______10613448
PITCH MOI________2550000______19040141_______13904249
YAW MOI_________3950000______23089847_______24848934
<ixx unit="SLUG*FT2"> 2262183 </ixx>
<iyy unit="SLUG*FT2"> 3172439 </iyy>
<izz unit="SLUG*FT2"> 3337024 </izz>
<ixx unit="SLUG*FT2">1725000</ixx>
<iyy unit="SLUG*FT2">2550000</iyy>
<izz unit="SLUG*FT2">3950000</izz> -->
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<location name="CG" unit="IN">
<!--x> 642.122 </x-->
<x> 650.122 </x><!-- At zero load of fuel and cargo/pax the CG goes to 642 -->
<y> 0 </y>
<z> -41.7398 </z>
</location>
<pointmass name="Crew">
<weight unit="LBS">400</weight> <!-- MAX: 600lbs-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<pointmass name="PAX">
<weight unit="LBS">19750</weight> <!-- MAX: 39500 lbs ** looks too heavy. maybe low it and give a long cilinder shape. need to do some maths-->
<form shape="cylinder">
<radius unit="M"> 2.13 </radius>
<length unit="M"> 24.44 </length>
</form>
<location name="POINTMASS" unit="IN">
<x>705</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<!-- NEW Pointmasses Start Weights for good CG -->
<pointmass name="Fwd Cargo">
<weight unit="LBS">3750</weight> <!-- #REF-3 page 19, MAX 3402 kilograms = 7500.12616 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 4.95 </length>
</form>
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98,
x= (door form nose(8.16m))-(door with(1.816m)/2)+(Cargo compartment lenght(4.953m)/2)
x= 9.7285 meters = 383.011811 in
-->
<x>383.01</x>
<y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
</location>
</pointmass>
<pointmass name="Aft Cargo">
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 4536 kilograms = 10000.1682 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 6.6 </length>
</form>
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98,
x= (door form nose(22.69m))-(door with(1.816m)/2)
x= 21.78200 meters = 857.559055 in
-->
<x>857.55</x>
<y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
</location>
</pointmass>
<pointmass name="Rear Bulk Cargo">
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 1497 kilograms = 3300.32006 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 2 </length>
</form>
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+102,
x= (door form nose(22.69m))+(door with(1.816m)/2)+( Dist. between rear doors(2.19))+(Aprox to compartment center (2m))
x= 27.78800 meters = 1 094.01575 in
-->
<x>1094</x>
<y>0</y>
<z>-39.37</z> <!-- Aprox bulk lower deck 1 meter = 39.3700787 in -->
</location>
</pointmass>
<pointmass name="Engine1">
<weight unit="LBS">5248</weight>
<form shape="cylinder">
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<location name="POINTMASS" unit="IN">
<x>589.735</x>
<y>-226.575</y>
<z>-45.567</z>
</location>
</pointmass>
<pointmass name="Engine2">
<weight unit="LBS">5248</weight>
<form shape="cylinder">
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<location name="POINTMASS" unit="IN">
<x>589.735</x>
<y>226.575</y>
<z>-45.567</z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<!-- REF-1 page 165 + 271 -->
<contact type="BOGEY" name="NOSE_LG">
<location unit="IN">
<x> 197.6772 </x>
<y> 0 </y>
<z> -137.9617 </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> NONE </brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MLG">
<location unit="IN">
<!--<x> 699.9243 </x>-->
<x> 695.3149 </x>
<y> -149.4094 </y>
<z> -150.4824 </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="IN">
<!-- <x> 697.3425 </x> It should be right left simetric
<x> 699.9243 </x> -->
<x> 695.3149 </x>
<y> 149.4094 </y>
<z> -150.4824 </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="IN">
<x> 37.7953 </x>
<y> 0 </y>
<z> -38.1374 </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="IN">
<x> 128.1102 </x>
<y> 0 </y>
<z> -55.0271 </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="IN">
<x> 274.0157 </x>
<y> 0 </y>
<z> -60.0665 </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="IN">
<x> 930 </x>
<y> 0 </y>
<z> -60.0665 </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="IN">
<x>589.735</x>
<y>-226.575</y>
<z>-95.567</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="IN">
<x>589.735</x>
<y>226.575</y>
<z>-95.567</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="IN">
<x> 1097.9921 </x>
<y> 0 </y>
<z> -44.7722 </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="IN">
<x> 1225 </x>
<y> 0 </y>
<z> -18.8067 </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="IN">
<x> 1341.6142 </x>
<y> 0 </y>
<z> -10.2599 </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="IN">
<x> 1469.0945 </x>
<y> 0 </y>
<z> 47.4138 </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="IN">
<x> 838.8898 </x>
<y> -667.5197 </y>
<z> 35.7926 </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="IN">
<x> 838.8898 </x>
<y> 667.5197 </y>
<z> 35.7926 </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>
AP STILL BROKE, FDM STILL FUNNY, much fixes and improvements, AP panel mapped mostly, except button lights.
2016-11-05 03:39:28 +00:00
<engine file="v2527_a5">
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 589.735 </x>
<y> -226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
<feed>3</feed>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<feed>1</feed>
<feed>2</feed>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<thruster file="direct">
<location unit="IN">
<x> 589.735 </x>
<y> -226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> 1 </yaw>
</orient>
</thruster>
</engine>
AP STILL BROKE, FDM STILL FUNNY, much fixes and improvements, AP panel mapped mostly, except button lights.
2016-11-05 03:39:28 +00:00
<engine file="v2527_a5">
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 589.735 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<feed>3</feed>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<feed>5</feed>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<feed>4</feed>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<thruster file="direct">
<location unit="IN">
<x> 589.735 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 2.2 </pitch>
<yaw> -1 </yaw>
</orient>
</thruster>
</engine>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 788.4322 </x>
<y> -574.4148 </y>
<z> 3.1080 </z>
</location>
<capacity unit="LBS"> 328.13 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>4</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 737.4190 </x>
<y> -457.4259 </y>
<z> -8.0898 </z>
</location>
<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
<contents unit="LBS"> 154.88 </contents>
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 630.6588 </x>
<y> -236.2992 </y>
<z> -33.9470 </z>
</location>
<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
<contents unit="LBS"> 2437.38 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<priority>3</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Center Tank 3 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 580.9955 </x>
<y> 0 </y>
<z> -47.0 </z>
</location>
<capacity unit="LBS"> 14520 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
<priority>1</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 630.6588 </x>
<y> 236.2992 </y>
<z> -33.9470 </z>
</location>
<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
<contents unit="LBS"> 2437.38 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<priority>3</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 737.4190 </x>
<y> 457.4259 </y>
<z> -8.0898 </z>
</location>
<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
<contents unit="LBS"> 154.88 </contents>
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<priority>2</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
mew ecam halfway done, improments
2016-11-06 01:46:53 +00:00
<tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<location unit="IN">
<x> 788.4322 </x>
<y> 574.4148 </y>
<z> 3.1080 </z>
</location>
<capacity unit="LBS"> 328.13 </capacity><!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>4</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
</propulsion>
<system file="pushback" />
<!--system file="a320-fuel" /-->
<system file="glass-effect1"/>
<flight_control name="FCS: A320">
<channel name="Pitch">
<summer name="Pitch Trim Sum">
<input>/controls/flight/elevator</input>
<input>/controls/flight/elevator-trim</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Elevator Control">
<input>fcs/pitch-trim-sum</input>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<gain>0.025</gain>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<range>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-10</min>
<max>10</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Elevator position normalized">
<input>fcs/elevator-pos-deg</input>
<domain>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-10</min>
<max>10</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</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>/controls/flight/aileron</input>
<input>/controls/flight/aileron-trim</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Left Aileron Control">
<input>fcs/roll-trim-sum</input>
<gain>0.02</gain>
<range>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-15</min>
<max>15</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</range>
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron Control">
<input>-fcs/roll-trim-sum</input>
<gain>0.02</gain>
<range>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-15</min>
<max>15</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Aileron position normalized">
<input>fcs/left-aileron-pos-deg</input>
<domain>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-15</min>
<max>15</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</domain>
<range>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-1</min>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<max>1</max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron position normalized">
<input>fcs/right-aileron-pos-deg</input>
<domain>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-15</min>
<max>15</max>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</domain>
<range>
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<min>-1</min>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<max>1</max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
</channel>
AP STILL BROKE, FDM STILL FUNNY, much fixes and improvements, AP panel mapped mostly, except button lights.
2016-11-05 03:39:28 +00:00
<channel name="Throttle">
<pure_gain name="fcs/throttle1">
<input>/controls/engines/engine[0]/throttle-fdm</input>
<gain>1</gain>
<output>fcs/throttle-cmd-norm</output>
<output>fcs/throttle-pos-norm</output>
</pure_gain>
<pure_gain name="fcs/throttle2">
<input>/controls/engines/engine[1]/throttle-fdm</input>
<gain>1</gain>
<output>fcs/throttle-cmd-norm[1]</output>
<output>fcs/throttle-pos-norm[1]</output>
</pure_gain>
</channel>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
<channel name="Yaw">
<!-- Testing on Ground steering Rudder bug
<pure_gain name="Yaw Damper Rate">
<input>velocities/r-rad_sec</input>
<gain>2</gain>
</pure_gain>
<pure_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<gain>-5</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<summer name="Rudder Sum">
<input>fcs/yaw-trim-sum</input>
<input>fcs/yaw-damper-rate</input>
<input>fcs/yaw-damper-beta</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<gain>0.01745</gain>
<range>
<min>-25</min>
<max>25</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder position normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-25</min>
<max>25</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min> -0.35 </min>
<max> 0.35 </max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper Rate">
<input>velocities/r-aero-rad_sec</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.00
60 2.00
</tableData>
</table>
</scheduled_gain>
<scheduled_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.00
60 0.00
</tableData>
</table>
</scheduled_gain>
<summer name="Yaw Damper Sum">
<input>fcs/yaw-damper-beta</input>
<input>fcs/yaw-damper-rate</input>
<clipto>
<min> -0.1 </min>
<max> 0.1 </max>
</clipto>
</summer>
<scheduled_gain name="Yaw Damper Final">
<input>fcs/yaw-damper-sum</input>
<table>
<independentVar lookup="row">velocities/ve-kts</independentVar>
<tableData>
30 0.0
31 1.0
</tableData>
</table>
</scheduled_gain>
<summer name="Rudder Sum">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-final</input>
<clipto>
<min> -1 </min>
<max> 1 </max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<range>
<min> -0.35 </min>
<max> 0.35 </max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="rudder normalization">
<input>fcs/rudder-pos-rad</input>
<domain>
<min> -0.35 </min>
<max> 0.35 </max>
</domain>
<range>
<min> -1 </min>
<max> 1 </max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Flaps">
<kinematic name="Flaps Control">
<input>fcs/flap-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>40</position>
<time>40</time>
</setting>
</traverse>
<output>fcs/flap-pos-deg</output>
</kinematic>
<aerosurface_scale name="Flap position normalized">
<input>fcs/flap-pos-deg</input>
<domain>
<min>0</min>
<max>40</max>
</domain>
<range>
<min>0</min>
<max>1</max>
</range>
<output>fcs/flap-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Landing Gear">
<kinematic name="Gear Control">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>10</time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic>
</channel>
<channel name="Speedbrake">
<kinematic name="Speedbrake">
<input>fcs/speedbrake-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>2</time>
</setting>
</traverse>
<output>fcs/speedbrake-pos-norm</output>
</kinematic>
</channel>
<channel name="Tiller">
<switch name="/controls/gear/tiller-disabled">
<default value="0"/>
<test logic="AND" value="1">
/controls/gear/tiller-enabled == 0
</test>
</switch>
<fcs_function name="Nose Wheel Steering 0">
<function name="fcs/steer-nose-deg[0]">
<description>Steering command for nose gear</description>
<sum>
<product>
<table>
<independentVar lookup="row">/controls/gear/tiller-cmd-norm</independentVar>
<independentVar lookup="column">/controls/flight/rudder</independentVar>
<tableData>
-1 0 1
-1 -70 -70 -70
0 -7 0 7
1 70 70 70
</tableData>
</table>
<property>/controls/gear/tiller-enabled</property>
</product>
<product>
<product>
<property>/controls/flight/rudder</property>
<value>70</value>
</product>
<property>/controls/gear/tiller-disabled</property>
</product>
</sum>
</function>
</fcs_function>
<!-- simulate rotational friction -->
<actuator name="Gear Nose Actuator">
<input>fcs/steer-nose-deg[0]</input>
<rate_limit>70</rate_limit>
<output>fcs/steer-pos-deg[0]</output>
</actuator>
</channel>
</flight_control>
<aerodynamics>
<function name="aero/function/kCDge">
<description>Change_in_drag_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 0.4800
0.1000 0.5150
0.1500 0.6290
0.2000 0.7090
0.3000 0.8150
0.4000 0.8820
0.5000 0.9280
0.6000 0.9620
0.7000 0.9880
0.8000 1.0000
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<function name="aero/function/kCLge">
<description>Change_in_lift_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 1.2030
0.1000 1.1270
0.1500 1.0900
0.2000 1.0730
0.3000 1.0460
0.4000 1.0550
0.5000 1.0190
0.6000 1.0130
0.7000 1.0080
0.8000 1.0060
0.9000 1.0030
1.0000 1.0020
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<axis name="LIFT">
<function name="aero/force/Lift_gain">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
A321 added: Rembrandt users: I am still working on the glass animation for the A321, so the windows will appear not see through from outside.
2016-11-06 16:03:42 +00:00
<value>0.30</value>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</product>
</function>
<!--function name="aero/coefficient/CLalpha">
<description>Lift_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 1.0000 9.0000 10.0000 40.0000
-0.0900 -0.2200 -0.2200 -0.1200 -0.1200 0.3200
0.0000 0.2500 0.2500 0.3500 0.3500 0.7500
0.0900 0.7300 0.7300 0.8300 0.8300 1.2300
0.1000 0.8300 0.8300 0.9300 0.9300 1.3300
0.1200 0.9200 0.9200 1.0200 1.0200 1.4200
0.1400 1.0200 1.0200 1.1200 1.1200 1.5200
0.1600 1.0800 1.0800 1.1800 1.1800 1.5800
0.1700 1.1300 1.1300 1.2300 1.2300 1.6300
0.1900 1.1900 1.1900 1.2900 1.2900 1.6900
0.2100 1.2500 1.2500 1.3500 1.3500 1.7700
0.2400 1.3500 1.3700 1.4700 1.4800 1.9300
0.2600 1.4400 1.4700 1.5700 1.6200 2.1200
0.2800 1.4700 1.5100 1.6100 1.7800 2.4000
0.3000 1.5000 1.5600 1.6600 1.9000 2.3000
0.3200 1.4700 1.6100 1.6000 1.7000 2.0300
0.3400 1.3500 1.5000 1.4100 1.5000 1.5300
0.3600 1.1500 1.2000 1.2000 1.2000 1.2000
</tableData>
</table>
</product>
</function-->
<function name="aero/force/Lift_alpha">
<description>Lift_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 1.0000 9.0000 10.0000 40.0000
-0.0900 -0.2200 -0.2200 -0.1200 -0.1200 0.2500
0.0000 0.2500 0.2500 0.3500 0.3500 0.7500
0.0900 0.7300 0.7300 0.8300 0.8300 1.2300
0.1000 0.8300 0.8300 0.9300 0.9300 1.3300
0.1200 0.9200 0.9200 1.0200 1.0200 1.4200
0.1400 1.0200 1.0200 1.1200 1.1200 1.5200
0.1600 1.0800 1.0800 1.1800 1.1800 1.5800
0.1700 1.1300 1.1300 1.2300 1.2300 1.6300
0.1900 1.1900 1.1900 1.2900 1.2900 1.6900
0.2100 1.2500 1.2500 1.3500 1.3500 1.7700
0.2400 1.3500 1.3700 1.4700 1.4800 1.9300
0.2600 1.4400 1.4700 1.5700 1.6200 2.1200
0.2800 1.4700 1.5100 1.6100 1.7800 2.4000
0.3000 1.5000 1.5600 1.6600 1.9000 2.3000
0.3200 1.4700 1.6100 1.6000 1.7000 2.0300
0.3400 1.3500 1.5000 1.4100 1.5000 1.5300
0.3600 1.1500 1.2000 1.2000 1.2000 1.2000
</tableData>
</table>
</product>
</function>
<!--function name="aero/coefficient/CLDe">
<description>Lift_due_to_Elevator_Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.1930</value>
</product>
</function>-->
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.1930</value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_zero_lift">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.016</value>
</product>
</function>
<!--function name="aero/coefficient/CDalpha">
<description>Drag_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 1.0000 25.0000 40.0000
-0.0873 0.0041 0.0000 0.0005 0.0014
-0.0698 0.0013 0.0004 0.0025 0.0041
-0.0524 0.0001 0.0023 0.0059 0.0084
-0.0349 0.0003 0.0057 0.0108 0.0141
-0.0175 0.0020 0.0105 0.0172 0.0212
0.0000 0.0052 0.0168 0.0251 0.0399
0.0175 0.0099 0.0248 0.0346 0.0502
0.0349 0.0162 0.0342 0.0457 0.0621
0.0524 0.0240 0.0452 0.0583 0.0755
0.0698 0.0334 0.0577 0.0724 0.0904
0.0873 0.0442 0.0718 0.0881 0.1068
0.1047 0.0566 0.0874 0.1053 0.1248
0.1222 0.0706 0.1045 0.1240 0.1443
0.1396 0.0860 0.1232 0.1442 0.1654
0.1571 0.0962 0.1353 0.1573 0.1790
0.1745 0.1069 0.1479 0.1708 0.1930
0.1920 0.1180 0.1610 0.1849 0.2075
0.2094 0.1298 0.1746 0.1995 0.2226
0.2269 0.1424 0.1892 0.2151 0.2386
0.2443 0.1565 0.2054 0.2323 0.2564
0.2618 0.1727 0.2240 0.2521 0.2767
0.2793 0.1782 0.2302 0.2587 0.2835
0.2967 0.1716 0.2227 0.2507 0.2753
0.3142 0.1618 0.2115 0.2388 0.2631
0.3316 0.1475 0.1951 0.2214 0.2451
0.3491 0.1097 0.1512 0.1744 0.1966
</tableData>
</table>
</product>
</function-->
<function name="aero/force/Drag_alpha">
<description>Drag_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 1.0000 25.0000 40.0000
-0.0873 0.0041 0.0000 0.0005 0.0014
-0.0698 0.0013 0.0004 0.0025 0.0041
-0.0524 0.0001 0.0023 0.0059 0.0084
-0.0349 0.0003 0.0057 0.0108 0.0141
-0.0175 0.0020 0.0105 0.0172 0.0212
0.0000 0.0052 0.0168 0.0251 0.0399
0.0175 0.0099 0.0248 0.0346 0.0502
0.0349 0.0162 0.0342 0.0457 0.0621
0.0524 0.0240 0.0452 0.0583 0.0755
0.0698 0.0334 0.0577 0.0724 0.0904
0.0873 0.0442 0.0718 0.0881 0.1068
0.1047 0.0566 0.0874 0.1053 0.1248
0.1222 0.0706 0.1045 0.1240 0.1443
0.1396 0.0860 0.1232 0.1442 0.1654
0.1571 0.0962 0.1353 0.1573 0.1790
0.1745 0.1069 0.1479 0.1708 0.1930
0.1920 0.1180 0.1610 0.1849 0.2075
0.2094 0.1298 0.1746 0.1995 0.2226
0.2269 0.1424 0.1892 0.2151 0.2386
0.2443 0.1565 0.2054 0.2323 0.2564
0.2618 0.1727 0.2240 0.2521 0.2767
0.2793 0.1782 0.2302 0.2587 0.2835
0.2967 0.1716 0.2227 0.2507 0.2753
0.3142 0.1618 0.2115 0.2388 0.2631
0.3316 0.1475 0.1951 0.2214 0.2451
0.3491 0.1097 0.1512 0.1744 0.1966
</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/mag-elevator-pos-rad</property>
<value>0.0500</value>
</product>
</function-->
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.055</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>
<property>aero/mag-beta-rad</property>
<value>0.2000</value>
</product>
</function-->
<function name="aero/force/Drag_beta">
<description>Drag_due_to_sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/mag-beta-rad</property>
<value>0.2000</value>
</product>
</function>
<!--function name="aero/coefficient/CDgear">
<description>Drag_due_to_landing_gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.0400</value>
</product>
</function-->
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.04</value>
</product>
</function>
<!--function name="aero/coefficient/CDspeedbrake">
<description>Drag_due_to_speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.0400</value>
</product>
</function-->
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.04</value>
</product>
</function>
<!--function name="aero/coefficient/CDo">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.016</value>
</product>
</function-->
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</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>
<table>
<independentVar>aero/beta-rad</independentVar>
<tableData>
-0.3500 0.5000
0.0000 0.0000
0.3500 -0.5000
</tableData>
</table>
</product>
</function -->
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<!--function name="aero/coefficient/Clb">
<description>Roll_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<table>
<independentVar>aero/beta-rad</independentVar>
<tableData>
-0.3500 0.0100
0.0000 0.0000
0.3500 -0.0100
</tableData>
</table>
</product>
</function-->
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<!--function name="aero/coefficient/Clp">
<description>Roll_moment_due_to_roll_rate_(roll_damping)</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.5000</value>
</product>
</function-->
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.4</value>
</product>
</function>
<!--function name="aero/coefficient/Clr">
<description>Roll_moment_due_to_yaw_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.0050</value>
</product>
</function-->
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<!--function name="aero/coefficient/Clda">
<description>Roll_moment_due_to_aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<!- value>0.2000</value -> <!- Excesive roll !!! ->
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.100
2.0 0.033
</tableData>
</table>
</product>
</function-->
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
<!-- 0.0 0.100 -->
0.0 0.080
2.0 0.033
</tableData>
</table>
</product>
</function>
<!--function name="aero/coefficient/Cldr">
<description>Roll_moment_due_to_rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.0050</value>
</product>
</function-->
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.005</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_zero_alpha_and_flaps">
<description>Pitching_moment_at_zero_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<table>
<independentVar>fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 0.0000
40.0000 -0.1000
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_alpha">
<description>Pitch_moment_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<!-- value>-4.0000</value> -->
some changes and fixes, AP DISABLED DUE TO FDM ISSUES
2016-11-05 04:53:20 +00:00
<value>-0.8</value>
First commit, not yet flyable, does load however. Only A320-200 with IAE engines for the moment, more coming later
2016-11-04 22:13:12 +00:00
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch_moment_due_to_elevator_Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<!-- <value>-1.5000</value> Excesive Pitch -->
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
<!-- 0.0 -1.200 -->
0.0 -1.000
2.0 -0.300
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch_moment_due_to_pitch_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<!--value>-10.0000</value-->
<value>-10</value>
</product>
</function>
<function name="aero/moment/Pitch_alpha_rate">
<description>Pitch_moment_due_to_alpha_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<!--value>-12.0000</value-->
<value>-12</value>
</product>
</function>
</axis>
<axis name="YAW">
<!--function name="aero/coefficient/Cnr">
<description>Yaw_moment_due_to_yaw_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.0400</value>
</product>
</function-->
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.15</value>
</product>
</function>
<!--function name="aero/coefficient/Cnb">
<description>Yaw_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.2000</value>
</product>
</function-->
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<!--function name="aero/coefficient/Cndr">
<description>Yaw_moment_due_to_rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<!- <value>-0.5000</value> Excesive Yaw->
<value>-0.3</value>
</product>
</function-->
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<!--value>-0.2</value-->
<value>-0.15</value>
</product>
</function>
<!--function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function-->
</axis>
</aerodynamics>
<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>
Reference in a new issue Copy permalink