This commit is contained in:
omega13a
commit
e8c40d685a
43 changed files with 1553 additions and 37 deletions
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@ -7,7 +7,7 @@
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<sound>
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<path>Aircraft/A320Family/Sounds/cfm56-sound.xml</path>
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</sound>
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<checklists include="A3XX-Checklists.xml"/>
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||||
<description>Airbus A319-112 (CFM56)</description>
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||||
<flight-model>jsb</flight-model>
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<aero>A319-100-CFM</aero>
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@ -103,9 +103,10 @@
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</sim>
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<options>
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<options n="0">
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<EIS2 type="bool">0</EIS2>
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<eng>CFM</eng>
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<maxblock>52.3</maxblock>
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</options>
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<sharklet type="bool">0</sharklet>
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@ -7,7 +7,7 @@
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<sound>
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<path>Aircraft/A320Family/Sounds/v2500-sound.xml</path>
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</sound>
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<checklists include="A3XX-Checklists.xml"/>
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<description>Airbus A319-131 (IAE V2500)</description>
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<flight-model>jsb</flight-model>
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<aero>A319-100-IAE</aero>
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@ -103,9 +103,10 @@
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</sim>
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<options>
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<options n="0">
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<EIS2 type="bool">0</EIS2>
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<eng>IAE</eng>
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<maxblock>52.3</maxblock>
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</options>
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<sharklet type="bool">0</sharklet>
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@ -7,7 +7,7 @@
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<sound>
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<path>Aircraft/A320Family/Sounds/cfm56-sound.xml</path>
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</sound>
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<checklists include="A3XX-Checklists.xml"/>
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<description>Airbus A320-214 (CFM56)</description>
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<flight-model>jsb</flight-model>
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<aero>A320-200-CFM</aero>
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@ -103,9 +103,10 @@
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</sim>
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<options>
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<options n="0">
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<EIS2 type="bool">0</EIS2>
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<eng>CFM</eng>
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<maxblock>52.3</maxblock>
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</options>
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<sharklet type="bool">0</sharklet>
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@ -120,5 +121,4 @@
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<file>Aircraft/A320Family/Nasal/a320livery-cfm.nas</file>
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</specific>
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</nasal>
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</PropertyList>
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@ -7,7 +7,7 @@
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<sound>
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<path>Aircraft/A320Family/Sounds/v2500-sound.xml</path>
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</sound>
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<checklists include="A3XX-Checklists.xml"/>
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<description>Airbus A320-232 (IAE V2500)</description>
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<flight-model>jsb</flight-model>
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<aero>A320-200-IAE</aero>
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@ -103,9 +103,10 @@
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</sim>
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<options>
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<options n="0">
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<EIS2 type="bool">0</EIS2>
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<eng>IAE</eng>
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<maxblock>52.3</maxblock>
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</options>
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<sharklet type="bool">0</sharklet>
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@ -324,7 +324,7 @@
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</cmd>
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<autoland>
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<kp-pitch>0.035</kp-pitch>
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<kp-rudder>-0.15</kp-rudder>
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<kp-rudder>-0.05</kp-rudder>
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</autoland>
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</config>
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<output>
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@ -7,7 +7,7 @@
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<sound>
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<path>Aircraft/A320Family/Sounds/leapx-sound.xml</path>
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</sound>
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<checklists include="A3XX-Checklists.xml"/>
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<description>Airbus A320-251N (LEAP-1A)</description>
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<flight-model>jsb</flight-model>
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<aero>A320-200-CFM</aero>
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@ -103,9 +103,10 @@
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</sim>
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<options>
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<options n="0">
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<EIS2 type="bool">1</EIS2>
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<eng>CFM</eng>
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<maxblock>52.3</maxblock>
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</options>
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<sharklet type="bool">1</sharklet>
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600
A320neo-CFM.xml
Normal file
600
A320neo-CFM.xml
Normal file
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@ -0,0 +1,600 @@
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<?xml version="1.0"?>
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<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
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<fdm_config name="A320family" version="2.0" release="BETA"
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xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
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xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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<fileheader>
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<author>Joshua Davidson (it0uchpods)</author>
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<version>Pre V1.0</version>
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<description>A3XX FDE</description>
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</fileheader>
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<metrics>
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<wingarea unit="FT2"> 1319.79 </wingarea>
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<wingspan unit="FT" > 111.26 </wingspan>
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<wing_incidence> 1.03 </wing_incidence>
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<chord unit="FT" > 13.76 </chord>
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<htailarea unit="FT2"> 334.24 </htailarea>
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<htailarm unit="FT" > 57.88 </htailarm>
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<vtailarea unit="FT2"> 248.79 </vtailarea>
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<vtailarm unit="FT" > 57.33 </vtailarm>
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<!-- location name="AERORP" unit="IN">
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<x> 642.122 </x>
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<y> 0 </y>
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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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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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<location name="EYEPOINT" unit="IN">
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<x> 80 </x>
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<y> -30 </y>
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<z> 70 </z>
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</location>
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<location name="VRP" unit="IN">
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<x> 661.1 </x>
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<y> 0 </y>
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<z> -37 </z>
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</location>
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</metrics>
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<mass_balance>
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<ixx unit="SLUG*FT2"> 611903 </ixx>
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<iyy unit="SLUG*FT2"> 1735389 </iyy>
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<izz unit="SLUG*FT2"> 2301293 </izz>
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<!--
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___________________A320_________A330__________A340
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BOW_____________178000________270000________283925
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SPAN______________144___________198___________209
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LENGTH____________153___________209___________209
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||||
ROLL MOI_________1725000______5727777_______10613448
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||||
PITCH MOI________2550000______19040141_______13904249
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||||
YAW MOI_________3950000______23089847_______24848934
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||||
|
||||
<ixx unit="SLUG*FT2"> 2262183 </ixx>
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||||
<iyy unit="SLUG*FT2"> 3172439 </iyy>
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||||
<izz unit="SLUG*FT2"> 3337024 </izz>
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||||
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||||
<ixx unit="SLUG*FT2">1725000</ixx>
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||||
<iyy unit="SLUG*FT2">2550000</iyy>
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<izz unit="SLUG*FT2">3950000</izz> -->
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||||
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<ixy unit="SLUG*FT2"> 0 </ixy>
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<ixz unit="SLUG*FT2"> 0 </ixz>
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<iyz unit="SLUG*FT2"> 0 </iyz>
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<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
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<!-- #### 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%
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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
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-->
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<!-- location name="CG" unit="IN">
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<! - -x> 642.122 </x- - >
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<x> 650.122 </x><! - - At zero load of fuel and cargo/pax the CG goes to 642 - - >
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<y> 0 </y>
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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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<y> 0 </y>
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<z> 0.00 </z>
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</location>
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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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<y>0</y>
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||||
<z>0</z>
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||||
</location>
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||||
</pointmass>
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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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<y>0</y>
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||||
<z>0</z>
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||||
</location>
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</pointmass>
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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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||||
<y>0</y>
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||||
<z>0</z>
|
||||
</location>
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||||
</pointmass>
|
||||
<pointmass name="PAX 0B (60 seats)">
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||||
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>809.5669</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="PAX 0C (54 seats)">
|
||||
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
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||||
<location name="POINTMASS" unit="IN">
|
||||
<x>1163.2729</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 1">
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<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 -->
|
||||
</location>
|
||||
</pointmass>
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||||
<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
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||||
<pointmass name="Cargo Hold 3">
|
||||
<weight unit="LBS">2000</weight> <!-- MAX: 5384.414lbs -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>849.1324</x>
|
||||
<y>0</y>
|
||||
<z>-29.5</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 4">
|
||||
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>931.0653</x>
|
||||
<y>0</y>
|
||||
<z>-29.5</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 5">
|
||||
<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>1068.2634</x>
|
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<y>0</y>
|
||||
<z>0</z> <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
|
||||
</location>
|
||||
</pointmass>
|
||||
|
||||
|
||||
</mass_balance>
|
||||
|
||||
<ground_reactions>
|
||||
<!-- REF-1 page 165 + 271 -->
|
||||
<contact type="BOGEY" name="NOSE_LG">
|
||||
<location unit="IN">
|
||||
<x> 197.6772 </x>
|
||||
<y> 0 </y>
|
||||
<z> -137.9617 </z>
|
||||
</location>
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<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>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
<contact type="BOGEY" name="LEFT_MLG">
|
||||
<location unit="IN">
|
||||
<!--<x> 699.9243 </x>-->
|
||||
<x> 695.3149 </x>
|
||||
<y> -149.4094 </y>
|
||||
<z> -150.4824 </z>
|
||||
</location>
|
||||
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.02 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> LEFT </brake_group>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
<contact type="BOGEY" name="RIGHT_MLG">
|
||||
<location unit="IN">
|
||||
<!-- <x> 697.3425 </x> It should be right left simetric
|
||||
<x> 699.9243 </x> -->
|
||||
<x> 695.3149 </x>
|
||||
<y> 149.4094 </y>
|
||||
<z> -150.4824 </z>
|
||||
</location>
|
||||
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.02 </rolling_friction>
|
||||
<!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
|
||||
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> RIGHT </brake_group>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
|
||||
<contact type="STRUCTURE" name="NOSE_1">
|
||||
<location unit="IN">
|
||||
<x> 37.7953 </x>
|
||||
<y> 0 </y>
|
||||
<z> -38.1374 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="NOSE_2">
|
||||
<location unit="IN">
|
||||
<x> 128.1102 </x>
|
||||
<y> 0 </y>
|
||||
<z> -55.0271 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="CENTER_1">
|
||||
<location unit="IN">
|
||||
<x> 274.0157 </x>
|
||||
<y> 0 </y>
|
||||
<z> -60.0665 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="CENTER_2">
|
||||
<location unit="IN">
|
||||
<x> 930 </x>
|
||||
<y> 0 </y>
|
||||
<z> -60.0665 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
|
||||
<contact type="STRUCTURE" name="ENG_1">
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>-226.575</y>
|
||||
<z>-95.567</z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="ENG_2">
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>226.575</y>
|
||||
<z>-95.567</z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
|
||||
|
||||
<contact type="STRUCTURE" name="TAIL_1">
|
||||
<location unit="IN">
|
||||
<x> 1097.9921 </x>
|
||||
<y> 0 </y>
|
||||
<z> -44.7722 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_2">
|
||||
<location unit="IN">
|
||||
<x> 1225 </x>
|
||||
<y> 0 </y>
|
||||
<z> -18.8067 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_3">
|
||||
<location unit="IN">
|
||||
<x> 1341.6142 </x>
|
||||
<y> 0 </y>
|
||||
<z> -10.2599 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_4">
|
||||
<location unit="IN">
|
||||
<x> 1469.0945 </x>
|
||||
<y> 0 </y>
|
||||
<z> 47.4138 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 1 </dynamic_friction>
|
||||
<rolling_friction> 1 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="WING_TIP_1">
|
||||
<location unit="IN">
|
||||
<x> 838.8898 </x>
|
||||
<y> -667.5197 </y>
|
||||
<z> 35.7926 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="WING_TIP_2">
|
||||
<location unit="IN">
|
||||
<x> 838.8898 </x>
|
||||
<y> 667.5197 </y>
|
||||
<z> 35.7926 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 1 </dynamic_friction>
|
||||
<rolling_friction> 1 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
</ground_reactions>
|
||||
|
||||
<propulsion>
|
||||
|
||||
<engine file="leap1a26">
|
||||
<location unit="IN">
|
||||
<x> 620.0683 </x>
|
||||
<y> -226.575 </y>
|
||||
<z> -45.567 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> 1 </yaw>
|
||||
</orient>
|
||||
<feed>7</feed>
|
||||
<thruster file="direct">
|
||||
<location unit="IN">
|
||||
<x> 655.4820 </x>
|
||||
<y> -226.575 </y>
|
||||
<z> 0.000 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> 1 </yaw>
|
||||
</orient>
|
||||
</thruster>
|
||||
</engine>
|
||||
|
||||
<engine file="leap1a26">
|
||||
<location unit="IN">
|
||||
<x> 620.0683 </x>
|
||||
<y> 226.575 </y>
|
||||
<z> -45.567 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> -1 </yaw>
|
||||
</orient>
|
||||
<feed>8</feed>
|
||||
<thruster file="direct">
|
||||
<location unit="IN">
|
||||
<x> 655.4820 </x>
|
||||
<y> 226.575 </y>
|
||||
<z> 0.000 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> -1 </yaw>
|
||||
</orient>
|
||||
</thruster>
|
||||
</engine>
|
||||
|
||||
|
||||
<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 -->
|
||||
<contents unit="LBS"> 0 </contents>
|
||||
|
||||
<priority>4</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<priority>2</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<contents unit="LBS"> 4480 </contents>
|
||||
<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 -->
|
||||
<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 -->
|
||||
<priority>1</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<contents unit="LBS"> 4480 </contents>
|
||||
<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 -->
|
||||
<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 -->
|
||||
<priority>2</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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-->
|
||||
<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) -->
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>-226.575</y>
|
||||
<z>-45.567</z>
|
||||
</location>
|
||||
<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) -->
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>226.575</y>
|
||||
<z>-45.567</z>
|
||||
</location>
|
||||
<capacity unit="LBS"> 100 </capacity><!-- need review -->
|
||||
<contents unit="LBS"> 0 </contents>
|
||||
<priority>1</priority>
|
||||
<type>JET-A1</type>
|
||||
</tank>
|
||||
</propulsion>
|
||||
|
||||
<system file="pushback" />
|
||||
<system file="fuel" />
|
||||
<system file="glass-effect1" />
|
||||
<system file="it-fbw" />
|
||||
<system file="fmgc" />
|
||||
<system file="fcs" />
|
||||
|
||||
<flight_control name="none"/>
|
||||
|
||||
<aerodynamics file="Systems/a320-aerodynamics.xml" />
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
|
|
@ -7,7 +7,7 @@
|
|||
<sound>
|
||||
<path>Aircraft/A320Family/Sounds/cfm56-sound.xml</path>
|
||||
</sound>
|
||||
|
||||
<checklists include="A3XX-Checklists.xml"/>
|
||||
<description>Airbus A321-211 (CFM56)</description>
|
||||
<flight-model>jsb</flight-model>
|
||||
<aero>A321-200-CFM</aero>
|
||||
|
|
@ -103,9 +103,10 @@
|
|||
|
||||
</sim>
|
||||
|
||||
<options>
|
||||
<options n="0">
|
||||
<EIS2 type="bool">0</EIS2>
|
||||
<eng>CFM</eng>
|
||||
<maxblock>52.0</maxblock>
|
||||
</options>
|
||||
|
||||
<sharklet type="bool">0</sharklet>
|
||||
|
|
|
|||
|
|
@ -103,9 +103,10 @@
|
|||
|
||||
</sim>
|
||||
|
||||
<options>
|
||||
<options n="0">
|
||||
<EIS2 type="bool">0</EIS2>
|
||||
<eng>IAE</eng>
|
||||
<maxblock>52.0</maxblock>
|
||||
</options>
|
||||
|
||||
<sharklet type="bool">0</sharklet>
|
||||
|
|
|
|||
|
|
@ -103,9 +103,10 @@
|
|||
|
||||
</sim>
|
||||
|
||||
<options>
|
||||
<options n="0">
|
||||
<EIS2 type="bool">1</EIS2>
|
||||
<eng>CFM</eng>
|
||||
<maxblock>52.0</maxblock>
|
||||
</options>
|
||||
|
||||
<sharklet type="bool">1</sharklet>
|
||||
|
|
|
|||
600
A321neo-CFM.xml
Normal file
600
A321neo-CFM.xml
Normal file
|
|
@ -0,0 +1,600 @@
|
|||
<?xml version="1.0"?>
|
||||
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
|
||||
<fdm_config name="A320family" version="2.0" release="BETA"
|
||||
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
|
||||
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
||||
|
||||
<fileheader>
|
||||
<author>Joshua Davidson (it0uchpods)</author>
|
||||
<version>Pre V1.0</version>
|
||||
<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>
|
||||
<z> 0.00 </z>
|
||||
</location>
|
||||
|
||||
<location name="EYEPOINT" unit="IN">
|
||||
<x> 80 </x>
|
||||
<y> -30 </y>
|
||||
<z> 70 </z>
|
||||
</location>
|
||||
|
||||
<location name="VRP" unit="IN">
|
||||
<x> 661.1 </x>
|
||||
<y> 0 </y>
|
||||
<z> -37 </z>
|
||||
</location>
|
||||
|
||||
</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> -->
|
||||
|
||||
<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>
|
||||
<z> 0.00 </z>
|
||||
</location>
|
||||
|
||||
<pointmass name="Cockpit Crew">
|
||||
<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>200</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cabin Crew">
|
||||
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>696</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="PAX 0A (60 seats)">
|
||||
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>470.1711</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="PAX 0B (60 seats)">
|
||||
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>809.5669</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="PAX 0C (54 seats)">
|
||||
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>1163.2729</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 1">
|
||||
<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 -->
|
||||
</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 -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>849.1324</x>
|
||||
<y>0</y>
|
||||
<z>-29.5</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 4">
|
||||
<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
|
||||
<location name="POINTMASS" unit="IN">
|
||||
<x>931.0653</x>
|
||||
<y>0</y>
|
||||
<z>-29.5</z>
|
||||
</location>
|
||||
</pointmass>
|
||||
<pointmass name="Cargo Hold 5">
|
||||
<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 -->
|
||||
</location>
|
||||
</pointmass>
|
||||
|
||||
|
||||
</mass_balance>
|
||||
|
||||
<ground_reactions>
|
||||
<!-- REF-1 page 165 + 271 -->
|
||||
<contact type="BOGEY" name="NOSE_LG">
|
||||
<location unit="IN">
|
||||
<x> 197.6772 </x>
|
||||
<y> 0 </y>
|
||||
<z> -137.9617 </z>
|
||||
</location>
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<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>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
<contact type="BOGEY" name="LEFT_MLG">
|
||||
<location unit="IN">
|
||||
<!--<x> 699.9243 </x>-->
|
||||
<x> 695.3149 </x>
|
||||
<y> -149.4094 </y>
|
||||
<z> -150.4824 </z>
|
||||
</location>
|
||||
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.02 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> LEFT </brake_group>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
<contact type="BOGEY" name="RIGHT_MLG">
|
||||
<location unit="IN">
|
||||
<!-- <x> 697.3425 </x> It should be right left simetric
|
||||
<x> 699.9243 </x> -->
|
||||
<x> 695.3149 </x>
|
||||
<y> 149.4094 </y>
|
||||
<z> -150.4824 </z>
|
||||
</location>
|
||||
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
|
||||
<static_friction> 0.8 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.02 </rolling_friction>
|
||||
<!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
|
||||
<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> RIGHT </brake_group>
|
||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
|
||||
<contact type="STRUCTURE" name="NOSE_1">
|
||||
<location unit="IN">
|
||||
<x> 37.7953 </x>
|
||||
<y> 0 </y>
|
||||
<z> -38.1374 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="NOSE_2">
|
||||
<location unit="IN">
|
||||
<x> 128.1102 </x>
|
||||
<y> 0 </y>
|
||||
<z> -55.0271 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="CENTER_1">
|
||||
<location unit="IN">
|
||||
<x> 274.0157 </x>
|
||||
<y> 0 </y>
|
||||
<z> -60.0665 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="CENTER_2">
|
||||
<location unit="IN">
|
||||
<x> 930 </x>
|
||||
<y> 0 </y>
|
||||
<z> -60.0665 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
|
||||
<contact type="STRUCTURE" name="ENG_1">
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>-226.575</y>
|
||||
<z>-95.567</z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="ENG_2">
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>226.575</y>
|
||||
<z>-95.567</z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.5 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
|
||||
|
||||
<contact type="STRUCTURE" name="TAIL_1">
|
||||
<location unit="IN">
|
||||
<x> 1097.9921 </x>
|
||||
<y> 0 </y>
|
||||
<z> -44.7722 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_2">
|
||||
<location unit="IN">
|
||||
<x> 1225 </x>
|
||||
<y> 0 </y>
|
||||
<z> -18.8067 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_3">
|
||||
<location unit="IN">
|
||||
<x> 1341.6142 </x>
|
||||
<y> 0 </y>
|
||||
<z> -10.2599 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="TAIL_4">
|
||||
<location unit="IN">
|
||||
<x> 1469.0945 </x>
|
||||
<y> 0 </y>
|
||||
<z> 47.4138 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 1 </dynamic_friction>
|
||||
<rolling_friction> 1 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="WING_TIP_1">
|
||||
<location unit="IN">
|
||||
<x> 838.8898 </x>
|
||||
<y> -667.5197 </y>
|
||||
<z> 35.7926 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 0.4 </dynamic_friction>
|
||||
<rolling_friction> 0.4 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
<contact type="STRUCTURE" name="WING_TIP_2">
|
||||
<location unit="IN">
|
||||
<x> 838.8898 </x>
|
||||
<y> 667.5197 </y>
|
||||
<z> 35.7926 </z>
|
||||
</location>
|
||||
<static_friction> 1.0 </static_friction>
|
||||
<dynamic_friction> 1 </dynamic_friction>
|
||||
<rolling_friction> 1 </rolling_friction>
|
||||
<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
|
||||
<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
|
||||
<max_steer unit="DEG"> 0.0 </max_steer>
|
||||
<brake_group> NONE </brake_group>
|
||||
<retractable>0</retractable>
|
||||
</contact>
|
||||
</ground_reactions>
|
||||
|
||||
<propulsion>
|
||||
|
||||
<engine file="leap1a32">
|
||||
<location unit="IN">
|
||||
<x> 620.0683 </x>
|
||||
<y> -226.575 </y>
|
||||
<z> -45.567 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> 1 </yaw>
|
||||
</orient>
|
||||
<feed>7</feed>
|
||||
<thruster file="direct">
|
||||
<location unit="IN">
|
||||
<x> 655.4820 </x>
|
||||
<y> -226.575 </y>
|
||||
<z> 0.000 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> 1 </yaw>
|
||||
</orient>
|
||||
</thruster>
|
||||
</engine>
|
||||
|
||||
<engine file="leap1a32">
|
||||
<location unit="IN">
|
||||
<x> 620.0683 </x>
|
||||
<y> 226.575 </y>
|
||||
<z> -45.567 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> -1 </yaw>
|
||||
</orient>
|
||||
<feed>8</feed>
|
||||
<thruster file="direct">
|
||||
<location unit="IN">
|
||||
<x> 655.4820 </x>
|
||||
<y> 226.575 </y>
|
||||
<z> 0.000 </z>
|
||||
</location>
|
||||
<orient unit="DEG">
|
||||
<roll> 0.0 </roll>
|
||||
<pitch> 2.2 </pitch>
|
||||
<yaw> -1 </yaw>
|
||||
</orient>
|
||||
</thruster>
|
||||
</engine>
|
||||
|
||||
|
||||
<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 -->
|
||||
<contents unit="LBS"> 0 </contents>
|
||||
|
||||
<priority>4</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<priority>2</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<contents unit="LBS"> 4480 </contents>
|
||||
<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 -->
|
||||
<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 -->
|
||||
<priority>1</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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 -->
|
||||
<contents unit="LBS"> 4480 </contents>
|
||||
<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 -->
|
||||
<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 -->
|
||||
<priority>2</priority>
|
||||
<type>JET-A1</type>
|
||||
<temperature>50</temperature>
|
||||
</tank>
|
||||
<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-->
|
||||
<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) -->
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>-226.575</y>
|
||||
<z>-45.567</z>
|
||||
</location>
|
||||
<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) -->
|
||||
<location unit="IN">
|
||||
<x>589.735</x>
|
||||
<y>226.575</y>
|
||||
<z>-45.567</z>
|
||||
</location>
|
||||
<capacity unit="LBS"> 100 </capacity><!-- need review -->
|
||||
<contents unit="LBS"> 0 </contents>
|
||||
<priority>1</priority>
|
||||
<type>JET-A1</type>
|
||||
</tank>
|
||||
</propulsion>
|
||||
|
||||
<system file="pushback" />
|
||||
<system file="fuel" />
|
||||
<system file="glass-effect1" />
|
||||
<system file="it-fbw" />
|
||||
<system file="fmgc" />
|
||||
<system file="fcs" />
|
||||
|
||||
<flight_control name="none"/>
|
||||
|
||||
<aerodynamics file="Systems/a321-aerodynamics.xml" />
|
||||
|
||||
<external_reactions>
|
||||
<force name="pushback" frame="BODY">
|
||||
<location unit="IN">
|
||||
<x>294</x>
|
||||
<y>0</y>
|
||||
<z>-149</z>
|
||||
</location>
|
||||
<direction>
|
||||
<x>1</x>
|
||||
<y>0</y>
|
||||
<z>0</z>
|
||||
</direction>
|
||||
</force>
|
||||
</external_reactions>
|
||||
</fdm_config>
|
||||
133
A3XX-Checklists.xml
Normal file
133
A3XX-Checklists.xml
Normal file
|
|
@ -0,0 +1,133 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<checklist>
|
||||
<title>BEFORE START</title>
|
||||
<page>
|
||||
<item>
|
||||
<name>COCKPIT PREP</name>
|
||||
<value>COMPLET(BOTH)</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>PINS AND COVERS</name>
|
||||
<value>REMOVED</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>SIGNS</name>
|
||||
<value>ON/AUTO</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>ADIRS</name>
|
||||
<value>NAV</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>FUEL QUANTITY</name>
|
||||
<value>____KG</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>TO DATA/V.BUGS</name>
|
||||
<value>____SET (BOTH)</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>BARO REF</name>
|
||||
<value>____SET (BOTH)</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>MOBILE PHONES</name>
|
||||
<value>OFF</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>A/SKID + N/W STEERING</name>
|
||||
<value>AS RQRD</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>WINDOWS/DOORS</name>
|
||||
<value>CLOSED (BOTH)</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>BEACON</name>
|
||||
<value>ON/(AUTO)</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>THR LEVERS</name>
|
||||
<value>IDLE</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>PARKING BRAKE</name>
|
||||
<value>AS RQRD</value>
|
||||
</item>
|
||||
</page>
|
||||
</checklist>
|
||||
<checklist>
|
||||
<title>ENG START PROCEDURE</title>
|
||||
<item>
|
||||
<name>Eng Mstr Swtch</name>
|
||||
<value>OFF</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>Eng Start Selector</name>
|
||||
<value>NORM</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>ENG Man Start PB</name>
|
||||
<value>OFF</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>Check ECAM oil 10 qts ++</name>
|
||||
</item>
|
||||
<item>
|
||||
<name>Eng Start Selector</name>
|
||||
<value>IGN/Start</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>Eng 1 Mstr Swtch</name>
|
||||
<value>ON</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>wait 30 sec</name>
|
||||
</item>
|
||||
<item>
|
||||
<name>Eng 2 Mstr Swtch</name>
|
||||
<value>ON</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>wait 30 sec</name>
|
||||
</item>
|
||||
</checklist>
|
||||
<checklist>
|
||||
<title>AFTER START</title>
|
||||
<item>
|
||||
<name>ANTI-ICE</name>
|
||||
<value>AS RQRD</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>ECAM STATUS</name>
|
||||
<value>CHECKED</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>APU</name>
|
||||
<value>AS RQRD</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>PITCH TRIM</name>
|
||||
<value>____SET</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>RUDDER TRIM</name>
|
||||
<value>ZERO</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>GROUND CREW</name>
|
||||
<value>CLEAR</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>A/SKID + N/W STEERING</name>
|
||||
<value>ON</value>
|
||||
</item>
|
||||
<item>
|
||||
<name>Eng Start Selector</name>
|
||||
<value>NORM</value>
|
||||
</item>
|
||||
</checklist>
|
||||
</PropertyList>
|
||||
51
Engines/leap1a26.xml
Normal file
51
Engines/leap1a26.xml
Normal file
|
|
@ -0,0 +1,51 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<turbine_engine name="leap1a26">
|
||||
<milthrust> 27120 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
|
||||
<bypassratio> 7.2 </bypassratio>
|
||||
<tsfc> 0.8 </tsfc>
|
||||
<bleed> 0.029 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 2.0 </n2spinup>
|
||||
<maxn1> 105.8 </maxn1>
|
||||
<maxn2> 102.1 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
|
||||
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
|
||||
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
|
||||
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
|
||||
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
|
||||
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
|
||||
0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
|
||||
0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
|
||||
0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
|
||||
0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
|
||||
1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
|
||||
1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
|
||||
1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
51
Engines/leap1a32.xml
Normal file
51
Engines/leap1a32.xml
Normal file
|
|
@ -0,0 +1,51 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<turbine_engine name="leap1a32">
|
||||
<milthrust> 32160 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
|
||||
<bypassratio> 7.2 </bypassratio>
|
||||
<tsfc> 0.8 </tsfc>
|
||||
<bleed> 0.029 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 2.0 </n2spinup>
|
||||
<maxn1> 105.8 </maxn1>
|
||||
<maxn2> 102.1 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
|
||||
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
|
||||
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
|
||||
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
|
||||
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
|
||||
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
|
||||
0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
|
||||
0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
|
||||
0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
|
||||
0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
|
||||
1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
|
||||
1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
|
||||
1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
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|
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|
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|
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|
|
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|
|||
<axis-alignment>yz-plane</axis-alignment>
|
||||
<type type="string">text-value</type>
|
||||
<format type="string">%s</format>
|
||||
<property>/it-autoflight/internal/alt</property>
|
||||
<property>/it-autoflight/internal/alt-mng</property>
|
||||
<truncate type="bool">false</truncate>
|
||||
<font type="string">helvetica_bold.txf</font>
|
||||
<draw-text type="bool">true</draw-text>
|
||||
|
|
@ -2768,7 +2768,7 @@
|
|||
<axis-alignment>yz-plane</axis-alignment>
|
||||
<type type="string">text-value</type>
|
||||
<format type="string">%s</format>
|
||||
<property>/it-autoflight/internal/alt</property>
|
||||
<property>/it-autoflight/internal/alt-mng</property>
|
||||
<truncate type="bool">false</truncate>
|
||||
<font type="string">helvetica_bold.txf</font>
|
||||
<draw-text type="bool">true</draw-text>
|
||||
|
|
|
|||
|
|
@ -2744,7 +2744,7 @@
|
|||
<axis-alignment>yz-plane</axis-alignment>
|
||||
<type type="string">text-value</type>
|
||||
<format type="string">%s</format>
|
||||
<property>/it-autoflight/internal/alt</property>
|
||||
<property>/it-autoflight/internal/alt-mng</property>
|
||||
<truncate type="bool">false</truncate>
|
||||
<font type="string">helvetica_bold.txf</font>
|
||||
<draw-text type="bool">true</draw-text>
|
||||
|
|
@ -2768,7 +2768,7 @@
|
|||
<axis-alignment>yz-plane</axis-alignment>
|
||||
<type type="string">text-value</type>
|
||||
<format type="string">%s</format>
|
||||
<property>/it-autoflight/internal/alt</property>
|
||||
<property>/it-autoflight/internal/alt-mng</property>
|
||||
<truncate type="bool">false</truncate>
|
||||
<font type="string">helvetica_bold.txf</font>
|
||||
<draw-text type="bool">true</draw-text>
|
||||
|
|
|
|||
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|
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|
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|
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|
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|
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|
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|
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|
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|
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BIN
Models/Liveries/A320/CFM-NEO/KZR.png
Normal file
BIN
Models/Liveries/A320/CFM-NEO/KZR.png
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 407 KiB |
14
Models/Liveries/A320/CFM-NEO/KZR.xml
Normal file
14
Models/Liveries/A320/CFM-NEO/KZR.xml
Normal file
|
|
@ -0,0 +1,14 @@
|
|||
<?xml version="1.0" encoding="UTF-8" ?>
|
||||
<!-- Deutsche Lufthansa AG livery for Airbus Industries A320neo mady by D-SVEN. Have fun! -->
|
||||
<PropertyList>
|
||||
<sim>
|
||||
<model>
|
||||
<livery>
|
||||
<name>Air Astana (P4-KBH)</name>
|
||||
<texture>Liveries/A320/CFM-NEO/KZR.png</texture>
|
||||
</livery>
|
||||
</model>
|
||||
</sim>
|
||||
</PropertyList>
|
||||
|
||||
|
||||
BIN
Models/Liveries/A320/IAE/STAR_WARS.png
Normal file
BIN
Models/Liveries/A320/IAE/STAR_WARS.png
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 1.1 MiB |
18
Models/Liveries/A320/IAE/STAR_WARS.xml
Normal file
18
Models/Liveries/A320/IAE/STAR_WARS.xml
Normal file
|
|
@ -0,0 +1,18 @@
|
|||
<?xml version="1.0" encoding="UTF-8" ?>
|
||||
|
||||
<PropertyList>
|
||||
<sim>
|
||||
<model>
|
||||
<livery>
|
||||
<name>Star Wards</name>
|
||||
<texture>Liveries/A320/IAE/STAR_WARS.png</texture>
|
||||
</livery>
|
||||
</model>
|
||||
</sim>
|
||||
|
||||
<options>
|
||||
<EIS2 type="bool">1</EIS2>
|
||||
</options>
|
||||
|
||||
<sharklet type="bool">0</sharklet>
|
||||
</PropertyList>
|
||||
BIN
Models/Liveries/A320/IAE/TIGER_airways.png
Normal file
BIN
Models/Liveries/A320/IAE/TIGER_airways.png
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 479 KiB |
18
Models/Liveries/A320/IAE/TIGER_airways.xml
Normal file
18
Models/Liveries/A320/IAE/TIGER_airways.xml
Normal file
|
|
@ -0,0 +1,18 @@
|
|||
<?xml version="1.0" encoding="UTF-8" ?>
|
||||
|
||||
<PropertyList>
|
||||
<sim>
|
||||
<model>
|
||||
<livery>
|
||||
<name>TIGER Airways</name>
|
||||
<texture>Liveries/A320/IAE/TIGER_airways.png</texture>
|
||||
</livery>
|
||||
</model>
|
||||
</sim>
|
||||
|
||||
<options>
|
||||
<EIS2 type="bool">1</EIS2>
|
||||
</options>
|
||||
|
||||
<sharklet type="bool">0</sharklet>
|
||||
</PropertyList>
|
||||
|
|
@ -151,7 +151,7 @@ var phasecheck = maketimer(0.2, func {
|
|||
setprop("/FMGC/status/phase", "2");
|
||||
}
|
||||
|
||||
if ((wowl and wowr) and (gs < 20) and (phase == "5")) {
|
||||
if ((wowl and wowr) and (gs < 20) and (phase == "2" or phase == "3" or phase == "4" or phase == "5" or phase == "6")) {
|
||||
setprop("/FMGC/status/phase", "7");
|
||||
var fd1 = getprop("/it-autoflight/input/fd1");
|
||||
var fd2 = getprop("/it-autoflight/input/fd2");
|
||||
|
|
|
|||
|
|
@ -453,8 +453,9 @@ var initInputB = func(key) {
|
|||
setprop("/MCDU[0]/scratchpad", "");
|
||||
} else {
|
||||
var tfs = size(scratchpad);
|
||||
if (tfs == 2 or tfs == 4) {
|
||||
if (scratchpad >= 1.0 and scratchpad <= 45.0) {
|
||||
var maxblock = getprop("/options/maxblock");
|
||||
if (tfs == 2 or tfs == 4 or tfs == 5) {
|
||||
if (scratchpad >= 1.0 and scratchpad <= maxblock) {
|
||||
setprop("/FMGC/internal/block", scratchpad);
|
||||
setprop("/FMGC/internal/block-set", 1);
|
||||
setprop("/MCDU[0]/scratchpad", "");
|
||||
|
|
|
|||
|
|
@ -453,8 +453,9 @@ var initInputB = func(key) {
|
|||
setprop("/MCDU[1]/scratchpad", "");
|
||||
} else {
|
||||
var tfs = size(scratchpad);
|
||||
if (tfs == 2 or tfs == 4) {
|
||||
if (scratchpad >= 1.0 and scratchpad <= 45.0) {
|
||||
var maxblock = getprop("/options/maxblock");
|
||||
if (tfs == 2 or tfs == 4 or tfs == 5) {
|
||||
if (scratchpad >= 1.0 and scratchpad <= maxblock) {
|
||||
setprop("/FMGC/internal/block", scratchpad);
|
||||
setprop("/FMGC/internal/block-set", 1);
|
||||
setprop("/MCDU[1]/scratchpad", "");
|
||||
|
|
|
|||
|
|
@ -45,6 +45,12 @@ var pneu_init = func {
|
|||
setprop("/systems/pressurization/diff-to-target", "0");
|
||||
setprop("/systems/pressurization/ditchingpb", 0);
|
||||
setprop("/systems/pressurization/targetvs", "0");
|
||||
setprop("/systems/ventilation/cabin/fans", 0); # aircon fans
|
||||
setprop("/systems/ventilation/avionics/fan", 0);
|
||||
setprop("/systems/ventilation/avionics/extractvalve", "0");
|
||||
setprop("/systems/ventilation/avionics/inletvalve", "0");
|
||||
setprop("/systems/ventilation/lavatory/extractfan", 0);
|
||||
setprop("/systems/ventilation/lavatory/extractvalve", "0");
|
||||
pneu_timer.start();
|
||||
}
|
||||
|
||||
|
|
@ -188,6 +194,20 @@ var master_pneu = func {
|
|||
|
||||
if (ditch and auto) {
|
||||
setprop("/systems/pressurization/outflowpos", "1");
|
||||
setprop("/systems/ventilation/avionics/extractvalve", "1");
|
||||
setprop("/systems/ventilation/avionics/inletvalve", "1");
|
||||
}
|
||||
|
||||
var dcess = getprop("/systems/electrical/bus/dc-ess");
|
||||
var acess = getprop("/systems/electrical/bus/ac-ess");
|
||||
var fanon = getprop("/systems/ventilation/avionics/fan");
|
||||
|
||||
if ((dcess > 25) or (acess > 110)) {
|
||||
setprop("/systems/ventilation/avionics/fan", 1);
|
||||
setprop("/systems/ventilation/lavatory/extractfan", 1);
|
||||
} else if ((dcess == 0) and (acess == 0)) {
|
||||
setprop("/systems/ventilation/avionics/fan", 0);
|
||||
setprop("/systems/ventilation/lavatory/extractfan", 0);
|
||||
}
|
||||
}
|
||||
|
||||
|
|
|
|||
BIN
Paintkit/airastana.xcf
Normal file
BIN
Paintkit/airastana.xcf
Normal file
Binary file not shown.
|
|
@ -871,12 +871,12 @@
|
|||
<property>/controls/flight/rudder-fbw-cmd</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.03</Kp>
|
||||
<Kp>0.025</Kp>
|
||||
<beta>1</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0</gamma>
|
||||
<Ti>1.5</Ti>
|
||||
<Td>0.0001</Td>
|
||||
<Ti>3.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>-0.2</u_min>
|
||||
<u_max>0.2</u_max>
|
||||
</config>
|
||||
|
|
|
|||
|
|
@ -409,17 +409,19 @@
|
|||
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
||||
<entry><ind>-50000</ind><dep>-50000</dep></entry>
|
||||
<entry><ind>-10000</ind><dep> -5000</dep></entry>
|
||||
<entry><ind> -5000</ind><dep> -1230</dep></entry>
|
||||
<entry><ind> -4000</ind><dep> -1025</dep></entry>
|
||||
<entry><ind> -3000</ind><dep> -820</dep></entry>
|
||||
<entry><ind> -2000</ind><dep> -615</dep></entry>
|
||||
<entry><ind> -5000</ind><dep> -3200</dep></entry>
|
||||
<entry><ind> -4000</ind><dep> -2000</dep></entry>
|
||||
<entry><ind> -3000</ind><dep> -1640</dep></entry>
|
||||
<entry><ind> -2000</ind><dep> -1230</dep></entry>
|
||||
<entry><ind> -1000</ind><dep> -410</dep></entry>
|
||||
<entry><ind> 0</ind><dep> 0</dep></entry>
|
||||
<entry><ind> 1000</ind><dep> 205</dep></entry>
|
||||
<entry><ind> 2000</ind><dep> 410</dep></entry>
|
||||
<entry><ind> 3000</ind><dep> 615</dep></entry>
|
||||
<entry><ind> 4000</ind><dep> 820</dep></entry>
|
||||
<entry><ind> 5000</ind><dep> 1025</dep></entry>
|
||||
<entry><ind> 1000</ind><dep> 410</dep></entry>
|
||||
<entry><ind> 2000</ind><dep> 820</dep></entry>
|
||||
<entry><ind> 3000</ind><dep> 1230</dep></entry>
|
||||
<entry><ind> 4000</ind><dep> 1640</dep></entry>
|
||||
<entry><ind> 5000</ind><dep> 2000</dep></entry>
|
||||
<entry><ind>10000</ind><dep> 5000</dep></entry>
|
||||
<entry><ind>50000</ind><dep> 50000</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
|
|||
Reference in a new issue