A3XX: Fix PFD Conditions
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parent
3a3a25956d
commit
f5029de068
4 changed files with 102 additions and 43 deletions
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@ -26,7 +26,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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<z> -25.2091 </z>
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</location -->
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<location name="AERORP" unit="IN">
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<x> 700.00 </x>
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<x> 680.00 </x>
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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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@ -81,7 +81,7 @@ YAW MOI_________3950000______23089847_______24848934
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<z> -41.7398 </z>
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</location -->
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<location name="CG" unit="IN">
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<x> 652.00 </x>
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<x> 620.00 </x>
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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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@ -89,7 +89,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="Cockpit Crew">
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<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
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<location name="POINTMASS" unit="IN">
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<x>200</x>
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<x>150</x>
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<y>0</y>
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<z>0</z>
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</location>
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@ -97,7 +97,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="Cabin Crew">
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<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
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<location name="POINTMASS" unit="IN">
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<x>696</x>
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<x>666</x>
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<y>0</y>
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<z>0</z>
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</location>
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@ -105,7 +105,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="PAX 0A (60 seats)">
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<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
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<location name="POINTMASS" unit="IN">
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<x>470.1711</x>
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<x>460.1711</x>
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<y>0</y>
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<z>0</z>
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</location>
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@ -113,7 +113,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="PAX 0B (60 seats)">
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<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
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<location name="POINTMASS" unit="IN">
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<x>809.5669</x>
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<x>789.5669</x>
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<y>0</y>
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<z>0</z>
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</location>
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@ -121,7 +121,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="PAX 0C (54 seats)">
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<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
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<location name="POINTMASS" unit="IN">
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<x>1163.2729</x>
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<x>1123.2729</x>
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<y>0</y>
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<z>0</z>
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</location>
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@ -129,7 +129,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="Cargo Hold 1">
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<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
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<location name="POINTMASS" unit="IN">
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<x>383.4792</x>
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<x>363.4792</x>
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<y>0</y>
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<z>-29.5</z> <!-- 1.5m and now half of it for the center point of the load -->
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</location>
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@ -138,7 +138,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="Cargo Hold 3">
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<weight unit="LBS">2000</weight> <!-- MAX: 5384.414lbs -->
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<location name="POINTMASS" unit="IN">
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<x>849.1324</x>
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<x>821.1324</x>
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<y>0</y>
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<z>-29.5</z>
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</location>
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@ -146,7 +146,7 @@ YAW MOI_________3950000______23089847_______24848934
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<pointmass name="Cargo Hold 4">
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<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
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<location name="POINTMASS" unit="IN">
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<x>931.0653</x>
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<x>911.0653</x>
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<y>0</y>
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<z>-29.5</z>
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</location>
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@ -167,7 +167,7 @@ YAW MOI_________3950000______23089847_______24848934
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<!-- REF-1 page 165 + 271 -->
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<contact type="BOGEY" name="NOSE_LG">
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<location unit="IN">
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<x> 197.6772 </x>
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<x> 275.6772 </x>
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<y> 0 </y>
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<z> -137.9617 </z>
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</location>
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@ -33,31 +33,59 @@
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<animation>
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<type>select</type>
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<object-name>sidestick-max</object-name>
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<object-name>sidestick-pos</object-name>
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<object-name>sidestick-pos</object-name>
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<condition>
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<and>
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<property>/options/pfd/sidestick-pos</property>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<or>
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<and>
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<or>
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<property>/gear/gear[1]/wow</property>
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<property>/gear/gear[2]/wow</property>
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<and>
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<property>/options/pfd/sidestick-pos</property>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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</and>
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</or>
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<or>
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<and>
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<or>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>1</value>
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</equals>
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</or>
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<equals>
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<property>/engines/engine[0]/state</property>
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<value>3</value>
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</equals>
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</and>
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<and>
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<or>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>1</value>
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</equals>
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</or>
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<equals>
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<property>/engines/engine[1]/state</property>
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<value>3</value>
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</equals>
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<not><property>/gear/gear[1]/wow</property></not>
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<not><property>/gear/gear[2]/wow</property></not>
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</or>
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</and>
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</and>
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</or>
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</and>
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</condition>
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</animation>
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@ -667,6 +695,7 @@
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<animation>
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<type>textranslate</type>
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<object-name>alt-tape-2</object-name>
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<property>octal</property>
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<property>instrumentation/altimeter/indicated-altitude-ft</property>
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<factor>0.009999725</factor>
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<axis>
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@ -33,31 +33,59 @@
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<animation>
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<type>select</type>
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<object-name>sidestick-max</object-name>
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<object-name>sidestick-pos</object-name>
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<object-name>sidestick-pos</object-name>
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<condition>
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<and>
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<property>/options/pfd/sidestick-pos</property>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<or>
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<and>
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<or>
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<property>/gear/gear[1]/wow</property>
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<property>/gear/gear[2]/wow</property>
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<and>
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<property>/options/pfd/sidestick-pos</property>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>0</value>
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</equals>
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</and>
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</or>
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<or>
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<and>
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<or>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>1</value>
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</equals>
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</or>
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<equals>
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<property>/engines/engine[0]/state</property>
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<value>3</value>
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</equals>
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</and>
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<and>
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<or>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/FMGC/status/phase</property>
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<value>1</value>
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</equals>
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</or>
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<equals>
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<property>/engines/engine[1]/state</property>
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<value>3</value>
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</equals>
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<not><property>/gear/gear[1]/wow</property></not>
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<not><property>/gear/gear[2]/wow</property></not>
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</or>
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</and>
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</and>
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</or>
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</and>
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</condition>
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</animation>
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@ -667,6 +695,7 @@
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<animation>
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<type>textranslate</type>
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<object-name>alt-tape-2</object-name>
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<property>octal</property>
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<property>instrumentation/altimeter/indicated-altitude-ft</property>
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<factor>0.009999725</factor>
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<axis>
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@ -320,6 +320,7 @@
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -1.900
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0.2 -1.800
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2.0 -0.900
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</tableData>
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</table>
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