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A32X: FDE Improvements by Richard, fix FBW, FCS

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This commit is contained in:
Joshua Davidson 2017-06-25 10:24:50 -04:00
parent 1f6ce5044a
commit f77895e644
16 changed files with 3751 additions and 3913 deletions
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78
A318-100-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A319-100-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A319-100-IAE.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A320-100-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

156
A320-200-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">
@ -458,114 +440,140 @@ YAW MOI_________3950000______23089847_______24848934
</engine>
<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
<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><!-- 1 percent of total capacity, needs 20C to be filled -->
<capacity unit="LBS"> 412 </capacity>
<!-- 1 percent of total capacity, needs 20C to be filled -->
<contents unit="LBS"> 0 </contents>
<priority>4</priority>
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
<tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
<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><!-- correct by FCOM -->
<contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<capacity unit="LBS"> 1520.00 </capacity>
<!-- correct by FCOM -->
<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 -->
<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 -->
<capacity unit="LBS"> 11982 </capacity>
<!-- correct by FCOM -->
<contents unit="LBS"> 4480 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
<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 -->
<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 filled first -->
<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
<capacity unit="LBS"> 14281 </capacity>
<!-- correct by FCOM -->
<contents unit="LBS"> 0 </contents>
<!-- wing tanks 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 -->
<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 -->
<capacity unit="LBS"> 11982 </capacity>
<!-- correct by FCOM -->
<contents unit="LBS"> 4480 </contents>
<standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
<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 -->
<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><!-- need review -->
<contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
<capacity unit="LBS"> 1520 </capacity>
<!-- need review -->
<contents unit="LBS"> 1520 </contents>
<!-- outer tank filled first than inner tank -->
<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 -->
<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><!-- 1 percent of total fuel capacity, needs 20C-->
<capacity unit="LBS"> 412 </capacity>
<!-- 1 percent of total fuel capacity, needs 20C-->
<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) -->
<tank type="FUEL">
<!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
<location unit="IN">
<x>589.735</x>
<y>-226.575</y>
<z>-45.567</z>
</location>
<capacity unit="LBS"> 100 </capacity><!-- need review -->
<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) -->
<tank type="FUEL">
<!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
<location unit="IN">
<x>589.735</x>
<y>226.575</y>
<z>-45.567</z>
</location>
<capacity unit="LBS"> 100 </capacity><!-- need review -->
<capacity unit="LBS"> 100 </capacity>
<!-- need review -->
<contents unit="LBS"> 0 </contents>
<priority>1</priority>
<type>JET-A1</type>

78
A320-200-IAE.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

88
A320neo-CFM.xml
View file

@ -10,21 +10,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<description>A3XX FDE</description>
</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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +31,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +47,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +56,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +65,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +74,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +83,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +92,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +112,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +121,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +147,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A321-200-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A321-200-IAE.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

78
A321neo-CFM.xml
View file

@ -20,11 +20,6 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<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="AERORP" unit="IN">
<x> 700.00 </x>
<y> 0 </y>
@ -46,40 +41,15 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</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> -->
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<ixz unit="SLUG*FT2">8000</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<emptywt unit="LBS">80431</emptywt>
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- 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 -->
<location name="CG" unit="IN">
<x> 652.00 </x>
<y> 0 </y>
@ -87,7 +57,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
<pointmass name="Cockpit Crew">
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
<weight unit="LBS">400</weight>
<!-- MAX: 400lbs, two pilots-->
<location name="POINTMASS" unit="IN">
<x>200</x>
<y>0</y>
@ -95,7 +66,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
@ -103,7 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>470.1711</x>
<y>0</y>
@ -111,7 +84,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<weight unit="LBS">6600</weight>
<!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>809.5669</x>
<y>0</y>
@ -119,7 +93,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<weight unit="LBS">5940</weight>
<!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>1163.2729</x>
<y>0</y>
@ -127,16 +102,19 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<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 -->
<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 -->
<weight unit="LBS">2000</weight>
<!-- MAX: 5384.414lbs -->
<location name="POINTMASS" unit="IN">
<x>849.1324</x>
<y>0</y>
@ -144,7 +122,8 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 4">
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
<weight unit="LBS">1500</weight>
<!-- MAX: 4651.754lbs -->
<location name="POINTMASS" unit="IN">
<x>931.0653</x>
<y>0</y>
@ -152,11 +131,13 @@ YAW MOI_________3950000______23089847_______24848934
</location>
</pointmass>
<pointmass name="Cargo Hold 5">
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
<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 -->
<z>0</z>
<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
</location>
</pointmass>
@ -176,8 +157,9 @@ YAW MOI_________3950000______23089847_______24848934
<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>
<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">

10
Systems/a318-aerodynamics.xml
View file

@ -3,6 +3,7 @@
<aerodynamics>
<property value="0.0">ice/wing</property>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
@ -71,7 +72,7 @@
</product>
</function>
<function name="aero/force/Lift_wingice">
<function name="aero/coefficient/CLicew">
<description>Lift_decrease_due_to_ice_on_wing</description>
<product>
<property>aero/qbar-psf</property>
@ -219,7 +220,6 @@
</table>
</product>
</function>
</axis>
<axis name="SIDE">
@ -257,7 +257,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
<value>-1.1</value>
</product>
</function>
@ -306,7 +306,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
<value>-0.5</value>
</product>
</function>
@ -335,7 +335,7 @@
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
<value>-150</value>
</product>
</function>

10
Systems/a319-aerodynamics.xml
View file

@ -3,6 +3,7 @@
<aerodynamics>
<property value="0.0">ice/wing</property>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
@ -71,7 +72,7 @@
</product>
</function>
<function name="aero/force/Lift_wingice">
<function name="aero/coefficient/CLicew">
<description>Lift_decrease_due_to_ice_on_wing</description>
<product>
<property>aero/qbar-psf</property>
@ -219,7 +220,6 @@
</table>
</product>
</function>
</axis>
<axis name="SIDE">
@ -257,7 +257,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
<value>-1.1</value>
</product>
</function>
@ -306,7 +306,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
<value>-0.5</value>
</product>
</function>
@ -335,7 +335,7 @@
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
<value>-150</value>
</product>
</function>

35
Systems/a320-aerodynamics.xml
View file

@ -3,6 +3,7 @@
<aerodynamics>
<property value="0.0">ice/wing</property>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
@ -203,20 +204,6 @@
</product>
</function>
</axis>
<axis name="SIDE">
<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>
<function name="aero/force/Drag_wingice">
<description>Drag_due_to_ice_on_wing</description>
<product>
@ -235,6 +222,20 @@
</function>
</axis>
<axis name="SIDE">
<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/moment/Roll_beta">
@ -256,7 +257,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
<value>-1.1</value>
</product>
</function>
@ -305,7 +306,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
<value>-0.5</value>
</product>
</function>
@ -334,7 +335,7 @@
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
<value>-150</value>
</product>
</function>

7
Systems/a321-aerodynamics.xml
View file

@ -3,6 +3,7 @@
<aerodynamics>
<property value="0.0">ice/wing</property>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
@ -256,7 +257,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
<value>-1.1</value>
</product>
</function>
@ -305,7 +306,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
<value>-0.5</value>
</product>
</function>
@ -334,7 +335,7 @@
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
<value>-150</value>
</product>
</function>

8
Systems/fcs.xml
View file

@ -14,7 +14,7 @@
<aerosurface_scale name="Elevator Control">
<input>fcs/pitch-trim-sum</input>
<gain>0.02</gain>
<gain>0.021</gain>
<range>
<min>-20</min>
<max>20</max>
@ -42,7 +42,7 @@
<aerosurface_scale name="Left Aileron Control">
<input>fcs/roll-trim-sum</input>
<gain>0.022</gain>
<gain>0.025</gain>
<range>
<min>-15</min>
<max>15</max>
@ -52,7 +52,7 @@
<aerosurface_scale name="Right Aileron Control">
<input>-fcs/roll-trim-sum</input>
<gain>0.022</gain>
<gain>0.025</gain>
<range>
<min>-15</min>
<max>15</max>
@ -330,7 +330,7 @@
<!-- simulate rotational friction -->
<actuator name="Gear Nose Actuator">
<input>fcs/steer-nose-deg[0]</input>
<rate_limit>70</rate_limit>
<rate_limit>90</rate_limit>
<output>fcs/steer-pos-deg[0]</output>
</actuator>

4
Systems/it-fbw-b.xml
View file

@ -137,7 +137,7 @@
<alpha>0.1</alpha>
<gamma>0</gamma>
<Ti>5</Ti>
<Td>0.005</Td>
<Td>0.002</Td>
<u_min>-1</u_min>
<u_max>1</u_max>
</config>
@ -392,7 +392,7 @@
<property>/controls/flight/elevator-fbw-cmd</property>
</output>
<config>
<Kp>-0.21</Kp>
<Kp>-0.20</Kp>
<beta>1</beta>
<alpha>0.1</alpha>
<gamma>0</gamma>