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A320-200 FLYABLE! Others coming soon!

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This commit is contained in:
Joshua Davidson 2016-11-08 23:05:30 -05:00
parent d044f1d39a
commit 98d24aa62f
8 changed files with 46 additions and 51 deletions
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2
A319-200-IAE-set.xml
View file

@ -8,7 +8,7 @@
<path>Aircraft/A320Family/Sounds/v2500-sound.xml</path>
</sound>
<description>Airbus A319 (IAE V2500)</description>
<description>NOT READY: Airbus A319 (IAE V2500)</description>
<flight-model>jsb</flight-model>
<aero>A319-200-IAE</aero>
<model>

2
A319-200-IAE.xml
View file

@ -10,7 +10,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<filecreationdate> 2012-03-02 </filecreationdate>
<version> 0.99 </version>
<description> Airbus A319-200 with IAE V2500 Engines </description>
<note> Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<note> Revised and fixed by Peter Brendt (jwocky) and Joshua Davidson (it0uchpods). Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<limitation></limitation>
</fileheader>

30
A320-200-IAE.xml
View file

@ -10,7 +10,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<filecreationdate> 2012-02-15 </filecreationdate>
<version> 0.99 </version>
<description> Airbus A320-200 with IAE V2500 Engines </description>
<note> Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<note> Revised and fixed by Peter Brendt (jwocky) and Joshua Davidson (it0uchpods). Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<limitation></limitation>
</fileheader>
@ -109,7 +109,7 @@ YAW MOI_________3950000______23089847_______24848934
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>400.1711</x>
<x>470.1711</x>
<y>0</y>
<z>0</z>
</location>
@ -117,7 +117,7 @@ YAW MOI_________3950000______23089847_______24848934
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<x>689.5669</x>
<x>809.5669</x>
<y>0</y>
<z>0</z>
</location>
@ -125,7 +125,7 @@ YAW MOI_________3950000______23089847_______24848934
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<x>993.2729</x>
<x>1163.2729</x>
<y>0</y>
<z>0</z>
</location>
@ -425,9 +425,9 @@ YAW MOI_________3950000______23089847_______24848934
<feed>2</feed>
<thruster file="direct">
<location unit="IN">
<x> 640.4820 </x>
<x> 655.4820 </x>
<y> -226.575 </y>
<z> -45.567 </z>
<z> 0.000 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
@ -453,9 +453,9 @@ YAW MOI_________3950000______23089847_______24848934
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 640.4820 </x>
<x> 655.4820 </x>
<y> 226.575 </y>
<z> -45.567 </z>
<z> 0.000 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
@ -965,8 +965,8 @@ YAW MOI_________3950000______23089847_______24848934
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.780
0.00 0.375
0.23 1.300
0.00 0.345
0.23 1.100
0.60 0.700
</tableData>
</table>
@ -979,7 +979,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.01000 </value>
<value> 0.00700 </value>
</product>
</function>
@ -988,8 +988,8 @@ YAW MOI_________3950000______23089847_______24848934
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.02300 </value>
<property>fcs/slat-pos-deg</property>
<value> 0.02000 </value>
</product>
</function>
@ -1068,7 +1068,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00150 </value>
<value> 0.00120 </value>
</product>
</function>
@ -1078,7 +1078,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00150 </value>
<value> 0.00120 </value>
</product>
</function>

25
A320-main.xml
View file

@ -33,9 +33,9 @@
<electrical>
<path></path>
</electrical>
<!--autopilot>AP is commented out on purpose! The FDM is not ready yet, once it is, I will allow the AP
<autopilot>
<path>Aircraft/A320Family/Systems/it-autoflight.xml</path>
</autopilot-->
</autopilot>
<!-- Uses slightly modified IT-AUTOFLIGHT Thrust controller. -->
<autopilot>
<path>Aircraft/A320Family/Systems/custom-autothrust.xml</path>
@ -232,22 +232,18 @@
<roll>
<umin>-0.40</umin>
<umax>0.40</umax>
<kp>0.06</kp>
<kp-vorloc>0.07</kp-vorloc>
<ti>0.0001</ti>
<ti-vorloc>0.0001</ti-vorloc>
<kp>0.09</kp>
<kp-vorloc>0.06</kp-vorloc>
</roll>
<pitch>
<umin>-0.18</umin>
<umax>0.18</umax>
<kp>-0.05</kp>
<ti>0.0001</ti>
<umin>-0.25</umin>
<umax>0.25</umax>
<kp>-0.07</kp>
</pitch>
<flch>
<umin>-0.18</umin>
<umax>0.18</umax>
<kp>-0.05</kp>
<ti>0.0001</ti>
<umin>-0.25</umin>
<umax>0.25</umax>
<kp>-0.08</kp>
</flch>
<gs>
<kp>0.10</kp>
@ -470,6 +466,7 @@
<minimums-mode>DH</minimums-mode>
<ILS1>false</ILS1>
<ILS2>false</ILS2>
<stallvls>-10</stallvls>
<fma>
<athr-box>O </athr-box>
</fma>

2
A321-200-IAE-set.xml
View file

@ -8,7 +8,7 @@
<path>Aircraft/A320Family/Sounds/v2500-sound.xml</path>
</sound>
<description>Airbus A321 (IAE V2500)</description>
<description>NOT READY: Airbus A321 (IAE V2500)</description>
<flight-model>jsb</flight-model>
<aero>A321-200-IAE</aero>
<model>

2
A321-200-IAE.xml
View file

@ -10,7 +10,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<filecreationdate> 2012-02-22 </filecreationdate>
<version> 0.99 </version>
<description> Airbus A320-200 with IAE V2500 Engines </description>
<note> Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<note> Revised and fixed by Peter Brendt (jwocky) and Joshua Davidson (it0uchpods). Fork from the A320-Family aircraft project (Thanks to all authors) </note>
<limitation></limitation>
</fileheader>

17
Models/Instruments/PFD/PFD1.xml
View file

@ -174,7 +174,7 @@
<type>texmultiple</type>
<object-name>vls-tape</object-name>
<transform>
<property>/flight-management/fmgc-values/indicated-vls-speed</property>
<property>/modes/pfd/stallvls</property>
<subtype>textranslate</subtype>
<factor>0.002001953</factor>
<axis>
@ -199,7 +199,7 @@
<type>texmultiple</type>
<object-name>stall-tape</object-name>
<transform>
<property>/flight-management/fmgc-values/ind-stall-speed</property>
<property>/modes/pfd/stallvls</property>
<subtype>textranslate</subtype>
<factor>0.002001953</factor>
<axis>
@ -251,15 +251,14 @@
</axis>
</transform>
<transform>
<property>/controls/flight/flaps</property>
<property>/controls/flight/flap-lever</property>
<subtype>textranslate</subtype>
<interpolation>
<entry><ind>0</ind><dep>0</dep></entry>
<entry><ind>0.20</ind><dep>0.0703125</dep></entry>
<entry><ind>0.29</ind><dep>0.140625</dep></entry>
<entry><ind>0.596</ind><dep>0.2109375</dep></entry>
<entry><ind>0.645</ind><dep>0.28125</dep></entry>
<entry><ind>1</ind><dep>0.333984375</dep></entry>
<entry><ind>1</ind><dep>0.090625</dep></entry>
<entry><ind>2</ind><dep>0.1609375</dep></entry>
<entry><ind>3</ind><dep>0.23125</dep></entry>
<entry><ind>4</ind><dep>0.303984375</dep></entry>
</interpolation>
<axis>
<x>1</x>
@ -274,7 +273,7 @@
<object-name>vfe-tape</object-name>
<condition>
<greater-than>
<property>controls/flight/flaps</property>
<property>/controls/flight/flap-lever</property>
<value>0</value>
</greater-than>
</condition>

17
Models/Instruments/PFD/PFD2.xml
View file

@ -174,7 +174,7 @@
<type>texmultiple</type>
<object-name>vls-tape</object-name>
<transform>
<property>/flight-management/fmgc-values/indicated-vls-speed</property>
<property>/modes/pfd/stallvls</property>
<subtype>textranslate</subtype>
<factor>0.002001953</factor>
<axis>
@ -199,7 +199,7 @@
<type>texmultiple</type>
<object-name>stall-tape</object-name>
<transform>
<property>/flight-management/fmgc-values/ind-stall-speed</property>
<property>/modes/pfd/stallvls</property>
<subtype>textranslate</subtype>
<factor>0.002001953</factor>
<axis>
@ -251,15 +251,14 @@
</axis>
</transform>
<transform>
<property>/controls/flight/flaps</property>
<property>/controls/flight/flap-lever</property>
<subtype>textranslate</subtype>
<interpolation>
<entry><ind>0</ind><dep>0</dep></entry>
<entry><ind>0.20</ind><dep>0.0703125</dep></entry>
<entry><ind>0.29</ind><dep>0.140625</dep></entry>
<entry><ind>0.596</ind><dep>0.2109375</dep></entry>
<entry><ind>0.645</ind><dep>0.28125</dep></entry>
<entry><ind>1</ind><dep>0.333984375</dep></entry>
<entry><ind>1</ind><dep>0.090625</dep></entry>
<entry><ind>2</ind><dep>0.1609375</dep></entry>
<entry><ind>3</ind><dep>0.23125</dep></entry>
<entry><ind>4</ind><dep>0.303984375</dep></entry>
</interpolation>
<axis>
<x>1</x>
@ -274,7 +273,7 @@
<object-name>vfe-tape</object-name>
<condition>
<greater-than>
<property>controls/flight/flaps</property>
<property>/controls/flight/flap-lever</property>
<value>0</value>
</greater-than>
</condition>