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A32X: Add Engine weights to FDE, tries to fix gear....

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This commit is contained in:
Joshua Davidson 2017-06-27 14:47:38 -04:00
parent f3dad9af41
commit 3d85b5f4d6
14 changed files with 138 additions and 64 deletions
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19
A318-100-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A319-100-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A319-100-IAE.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A320-100-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A320-200-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A320-200-IAE.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A320neo-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A321-200-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A321-200-IAE.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

19
A321neo-CFM.xml
View file

@ -65,13 +65,20 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<z>0</z>
</location>
</pointmass>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight>
<!-- MAX: 1320lbs, up to six flight-attendants-->
<pointmass name="Engine 1">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>696</x>
<y>0</y>
<z>0</z>
<x>530.86</x>
<y>-5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="Engine 2">
<weight unit="LBS">5200.7</weight>
<location name="POINTMASS" unit="IN">
<x>530.86</x>
<y>5.755</y>
<z>-78.56019</z>
</location>
</pointmass>
<pointmass name="PAX 0A (60 seats)">

3
Systems/a318-aerodynamics.xml
View file

@ -319,7 +319,8 @@
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
0.0 -2.200
0.2 -2.100
2.0 -0.900
</tableData>
</table>

3
Systems/a319-aerodynamics.xml
View file

@ -319,7 +319,8 @@
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
0.0 -2.200
0.2 -2.100
2.0 -0.900
</tableData>
</table>

3
Systems/a320-aerodynamics.xml
View file

@ -319,7 +319,8 @@
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
0.0 -2.200
0.2 -2.100
2.0 -0.900
</tableData>
</table>

3
Systems/a321-aerodynamics.xml
View file

@ -319,7 +319,8 @@
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
0.0 -2.200
0.2 -2.100
2.0 -0.900
</tableData>
</table>