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Revert "A32X: Update inertia"

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This reverts commit b366549f03.
This commit is contained in:
Joshua Davidson 2017-06-24 16:55:07 -04:00
parent 430924c777
commit 4626dff4e5
9 changed files with 297 additions and 63 deletions
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40
A318-100-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A319-100-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A319-100-IAE.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A320-100-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A320-200-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A320-200-IAE.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A320neo-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A321-200-CFM.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>

40
A321-200-IAE.xml
View file

@ -46,14 +46,40 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2">1248922</ixx>
<iyy unit="SLUG*FT2">1800728</iyy>
<izz unit="SLUG*FT2">2894800</izz>
<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
<ixy unit="SLUG*FT2"> 0</ixy>
<ixz unit="SLUG*FT2">5800</ixz>
<iyz unit="SLUG*FT2"> 0</iyz>
<emptywt unit="LBS">80431</emptywt>
<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-->
<!-- #### 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>