MAN THR added, EPR updated, Shadow removed forever
This commit is contained in:
Joshua Davidson
parent
d3e253084d
commit
154e78643d
16 changed files with 352 additions and 367 deletions
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@ -55,10 +55,10 @@
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<name>Spoilers</name>
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<path>Aircraft/A320Family/Systems/a320-spoilers.xml</path>
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</autopilot>
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<property-rule n="101">
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<autopilot>
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<path>Systems/fl2070_sound.xml</path>
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</property-rule>
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<property-rule n="102">
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</autopilot>
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<property-rule n="100">
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<path>Systems/pfd.xml</path>
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</property-rule>
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</systems>
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@ -298,15 +298,6 @@
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<starter-switch type="bool">false</starter-switch>
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<max-athr-thrust type="float">0.94</max-athr-thrust>
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</engine>
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<detents>
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<current type="string">none</current>
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<throttle type="float">0</throttle>
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<rev type="float">-0.59</rev>
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<idle type="float">0</idle>
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<clb type="float">0.72</clb>
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<flex type="float">0.98</flex>
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<toga type="float">1</toga>
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</detents>
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</engines>
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<flight>
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<ground-spoilers-armed type="bool">false</ground-spoilers-armed>
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@ -14,17 +14,7 @@
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<name>Fuselage</name>
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<path>Aircraft/A320Family/Models/Fuselages/a319.fuselage.xml</path>
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</model>
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<!-- effects -->
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<model>
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<name>shadow</name>
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<path>Aircraft/A320Family/Models/Effects/shadow.xml</path>
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<offsets>
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<x-m>20.38</x-m>
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<z-m>-4.26</z-m>
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<pitch-deg>1.5</pitch-deg>
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</offsets>
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</model>
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</model>
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<!-- Separate Flightdeck to fit the modified nose -->
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<model>
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<name>Flightdeck</name>
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@ -14,16 +14,6 @@
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<name>Fuselage</name>
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<path>Aircraft/A320Family/Models/Fuselages/a320.fuselage.xml</path>
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</model>
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<!-- effects -->
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<model>
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<name>shadow</name>
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<path>Aircraft/A320Family/Models/Effects/shadow.xml</path>
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<offsets>
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<x-m>20.38</x-m>
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<z-m>-4.26</z-m>
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<pitch-deg>1.5</pitch-deg>
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</offsets>
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</model>
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<!-- Separate Flightdeck to fit the modified nose -->
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<model>
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@ -15,16 +15,6 @@
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<path>Aircraft/A320Family/Models/Fuselages/a321.fuselage.xml</path>
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</model>
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<!-- effects -->
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<model>
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<name>shadow</name>
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<path>Aircraft/A320Family/Models/Effects/shadow.xml</path>
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<offsets>
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<x-m>20.38</x-m>
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<z-m>-4.26</z-m>
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<pitch-deg>1.5</pitch-deg>
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</offsets>
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</model>
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<!-- Separate Flightdeck to fit the modified nose -->
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<model>
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<name>Flightdeck</name>
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@ -1,6 +1,6 @@
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<?xml version="1.0" encoding="utf-8"?>
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<PropertyList>
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<name>Aircraft/A320neo/Models/Effects/NEOreflect</name>
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<name>Aircraft/A320Family/Models/Effects/NEOreflect</name>
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<inherits-from>Effects/reflect</inherits-from>
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<parameters>
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@ -1,23 +0,0 @@
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AC3Db
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MATERIAL "ac3dmat14" rgb 0.8 0.8 0.8 amb 0.2 0.2 0.2 emis 0 0 0 spec 0.2 0.2 0.2 shi 128 trans 0
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OBJECT world
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kids 1
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OBJECT poly
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name "shadow"
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loc 0 0 6.09085e-007
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texture "shadow.png"
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crease 45.000000
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numvert 4
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-18.785 0 17.05
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18.785 0 17.05
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18.785 0 -17.05
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-18.785 0 -17.05
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numsurf 1
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SURF 0x10
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mat 0
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refs 4
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0 0 0
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1 1 0
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2 1 1
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3 0 1
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kids 0
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Binary file not shown.
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Before Width: | Height: | Size: 9.9 KiB |
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@ -1,73 +0,0 @@
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<?xml version="1.0"?>
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<PropertyList>
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<path>res/shadow.ac</path>
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<animation>
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<!-- opaque objects -->
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<!-- transparent objects -->
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<object-name>shadow</object-name>
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<type>select</type>
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<condition>
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<not>
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<property>/sim/rendering/rembrandt/enabled</property>
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</not>
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</condition>
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</animation>
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<effect>
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<inherits-from>Effects/model-transparent</inherits-from>
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<object-name>shadow</object-name>
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</effect>
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<!-- ALS shadow effect -->
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<effect>
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<inherits-from>Effects/shadow</inherits-from>
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<object-name>shadow</object-name>
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</effect>
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<!--Translate to ground level -->
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<animation>
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<type>translate</type>
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<object-name>shadow</object-name>
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<property>/controls/lighting/shad-light-alt</property>
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<factor>0.301</factor>
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<axis>
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<x>0</x>
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<y>0</y>
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<z>-1</z>
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</axis>
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</animation>
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<animation>
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<type>rotate</type>
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<object-name>shadow</object-name>
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<property>/orientation/roll-deg</property>
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<center>
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<x>0</x>
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<y>0</y>
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<z>0</z>
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</center>
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<axis>
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<x>-1</x>
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<y>0</y>
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<z>0</z>
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</axis>
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</animation>
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<animation>
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<type>rotate</type>
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<object-name>shadow</object-name>
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<property>/orientation/pitch-deg</property>
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<center>
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<x>0</x>
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<y>0</y>
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<z>0</z>
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</center>
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<axis>
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<x>0</x>
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<y>1</y>
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<z>0</z>
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</axis>
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</animation>
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</PropertyList>
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@ -1956,9 +1956,13 @@
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<entry><ind>0.00000</ind><dep>10</dep></entry>
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<entry><ind>0.59999</ind><dep>33</dep></entry>
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<entry><ind>0.60000</ind><dep>35</dep></entry>
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<entry><ind>0.79999</ind><dep>35</dep></entry>
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<entry><ind>0.80000</ind><dep>46</dep></entry>
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<entry><ind>0.94999</ind><dep>46</dep></entry>
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<entry><ind>0.64999</ind><dep>35</dep></entry>
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<entry><ind>0.65000</ind><dep>37</dep></entry>
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<entry><ind>0.77999</ind><dep>44</dep></entry>
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<entry><ind>0.78000</ind><dep>46</dep></entry>
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<entry><ind>0.82999</ind><dep>46</dep></entry>
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<entry><ind>0.83000</ind><dep>48</dep></entry>
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<entry><ind>0.94999</ind><dep>53</dep></entry>
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<entry><ind>0.95000</ind><dep>55</dep></entry>
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<entry><ind>1.00000</ind><dep>55</dep></entry>
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</interpolation>
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@ -2009,9 +2013,13 @@
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<entry><ind>0.00000</ind><dep>10</dep></entry>
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<entry><ind>0.59999</ind><dep>33</dep></entry>
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<entry><ind>0.60000</ind><dep>35</dep></entry>
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<entry><ind>0.79999</ind><dep>35</dep></entry>
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<entry><ind>0.80000</ind><dep>46</dep></entry>
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<entry><ind>0.94999</ind><dep>46</dep></entry>
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<entry><ind>0.64999</ind><dep>35</dep></entry>
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<entry><ind>0.65000</ind><dep>37</dep></entry>
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<entry><ind>0.77999</ind><dep>44</dep></entry>
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<entry><ind>0.78000</ind><dep>46</dep></entry>
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<entry><ind>0.82999</ind><dep>46</dep></entry>
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<entry><ind>0.83000</ind><dep>48</dep></entry>
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<entry><ind>0.94999</ind><dep>53</dep></entry>
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<entry><ind>0.95000</ind><dep>55</dep></entry>
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<entry><ind>1.00000</ind><dep>55</dep></entry>
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</interpolation>
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@ -799,7 +799,7 @@
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<offsets>
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<x-m>0.00091828</x-m>
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<y-m>0.0326226</y-m>
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<z-m>0.0531781</z-m>
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<z-m>0.0581781</z-m>
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</offsets>
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<alignment>center-center</alignment>
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<axis-alignment>yz-plane</axis-alignment>
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@ -823,7 +823,7 @@
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<offsets>
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<x-m>0.00091828</x-m>
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<y-m>0.0436226</y-m>
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<z-m>0.0531781</z-m>
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<z-m>0.0581781</z-m>
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</offsets>
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<alignment>center-center</alignment>
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<axis-alignment>yz-plane</axis-alignment>
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@ -998,6 +998,14 @@
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<property>/it-autoflight/output/athr</property>
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<value>1</value>
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</equals>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>MAN THR</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state2</property>
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<value>MAN THR</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>MCT</value>
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@ -1006,14 +1014,6 @@
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<property>/systems/thrust/state2</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state3</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state4</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>TOGA</value>
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@ -1022,14 +1022,6 @@
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<property>/systems/thrust/state2</property>
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<value>TOGA</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state3</property>
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<value>TOGA</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state4</property>
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<value>TOGA</value>
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</not-equals>
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</and>
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</condition>
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</animation>
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@ -1295,14 +1287,6 @@
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<property>/systems/thrust/state2</property>
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<value>CL</value>
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</equals>
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<equals>
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<property>/systems/thrust/state3</property>
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<value>CL</value>
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</equals>
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<equals>
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<property>/systems/thrust/state4</property>
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<value>CL</value>
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</equals>
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</or>
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</and>
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</condition>
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@ -1326,14 +1310,6 @@
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<property>/systems/thrust/state2</property>
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<value>MAN</value>
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</equals>
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<equals>
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<property>/systems/thrust/state3</property>
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<value>MAN</value>
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</equals>
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<equals>
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<property>/systems/thrust/state4</property>
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<value>MAN</value>
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</equals>
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<equals>
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<property>/systems/thrust/state1</property>
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<value>CL</value>
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@ -1342,15 +1318,15 @@
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<property>/systems/thrust/state2</property>
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<value>CL</value>
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</equals>
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<equals>
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<property>/systems/thrust/state3</property>
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<value>CL</value>
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</equals>
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<equals>
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<property>/systems/thrust/state4</property>
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<value>CL</value>
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</equals>
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</or>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>MAN THR</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state2</property>
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<value>MAN THR</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>MCT</value>
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@ -1359,14 +1335,6 @@
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<property>/systems/thrust/state2</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state3</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state4</property>
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<value>MCT</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state1</property>
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<value>TOGA</value>
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@ -1375,14 +1343,6 @@
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<property>/systems/thrust/state2</property>
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<value>TOGA</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state3</property>
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<value>TOGA</value>
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</not-equals>
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<not-equals>
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<property>/systems/thrust/state4</property>
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<value>TOGA</value>
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||||
</not-equals>
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||||
</and>
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||||
</condition>
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</animation>
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@ -1397,6 +1357,14 @@
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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>/systems/thrust/state1</property>
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<value>MAN THR</value>
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</equals>
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<equals>
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<property>/systems/thrust/state2</property>
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||||
<value>MAN THR</value>
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</equals>
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<equals>
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||||
<property>/systems/thrust/state1</property>
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||||
<value>MCT</value>
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@ -1405,14 +1373,6 @@
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<property>/systems/thrust/state2</property>
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||||
<value>MCT</value>
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||||
</equals>
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||||
<equals>
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||||
<property>/systems/thrust/state3</property>
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||||
<value>MCT</value>
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||||
</equals>
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||||
<equals>
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||||
<property>/systems/thrust/state4</property>
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||||
<value>MCT</value>
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||||
</equals>
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||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
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||||
<value>TOGA</value>
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||||
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@ -1421,14 +1381,6 @@
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<property>/systems/thrust/state2</property>
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||||
<value>TOGA</value>
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||||
</equals>
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||||
<equals>
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||||
<property>/systems/thrust/state3</property>
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||||
<value>TOGA</value>
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||||
</equals>
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||||
<equals>
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||||
<property>/systems/thrust/state4</property>
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||||
<value>TOGA</value>
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||||
</equals>
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||||
</or>
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||||
</and>
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||||
</condition>
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||||
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@ -1532,6 +1484,29 @@
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</font-resolution>
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</text>
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|
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<text>
|
||||
<name>athr-thr-fma</name>
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<offsets>
|
||||
<x-m>0.00091828</x-m>
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||||
<y-m>-0.0546226</y-m>
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||||
<z-m>0.0630781</z-m>
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||||
</offsets>
|
||||
<alignment>center-center</alignment>
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||||
<axis-alignment>yz-plane</axis-alignment>
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||||
<type type="string">text-value</type>
|
||||
<format type="string">THR</format>
|
||||
<property>autopilot/serviceable</property>
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||||
<font type="string">helvetica_medium.txf</font>
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||||
<draw-text type="bool">true</draw-text>
|
||||
<draw-alignment type="bool">false</draw-alignment>
|
||||
<draw-boundingbox type="bool">false</draw-boundingbox>
|
||||
<character-size>0.0055</character-size>
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||||
<font-resolution>
|
||||
<width type="int">32</width>
|
||||
<height type="int">32</height>
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||||
</font-resolution>
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||||
</text>
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||||
|
||||
<text>
|
||||
<name>athr-box-fma</name>
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<offsets>
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|
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@ -1583,6 +1558,14 @@
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<property>/systems/thrust/state2</property>
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||||
<value>MCT</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -1642,6 +1625,45 @@
|
|||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>athr-thr-fma</object-name>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<text>
|
||||
<name>athr-lvrclb-fma</name>
|
||||
<offsets>
|
||||
|
|
@ -1815,6 +1837,7 @@
|
|||
<object-name>athr-man-fma</object-name>
|
||||
<object-name>athr-toga-fma</object-name>
|
||||
<object-name>athr-mct-fma</object-name>
|
||||
<object-name>athr-thr-fma</object-name>
|
||||
<object-name>athr-box-fma</object-name>
|
||||
<object-name>athr-lvrclb-fma</object-name>
|
||||
<object-name>vs-num</object-name>
|
||||
|
|
|
|||
|
|
@ -799,7 +799,7 @@
|
|||
<offsets>
|
||||
<x-m>0.00091828</x-m>
|
||||
<y-m>0.0326226</y-m>
|
||||
<z-m>0.0531781</z-m>
|
||||
<z-m>0.0581781</z-m>
|
||||
</offsets>
|
||||
<alignment>center-center</alignment>
|
||||
<axis-alignment>yz-plane</axis-alignment>
|
||||
|
|
@ -823,7 +823,7 @@
|
|||
<offsets>
|
||||
<x-m>0.00091828</x-m>
|
||||
<y-m>0.0436226</y-m>
|
||||
<z-m>0.0531781</z-m>
|
||||
<z-m>0.0581781</z-m>
|
||||
</offsets>
|
||||
<alignment>center-center</alignment>
|
||||
<axis-alignment>yz-plane</axis-alignment>
|
||||
|
|
@ -998,6 +998,14 @@
|
|||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
|
|
@ -1006,14 +1014,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>TOGA</value>
|
||||
|
|
@ -1022,14 +1022,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
|
@ -1295,14 +1287,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -1326,14 +1310,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
|
|
@ -1342,15 +1318,15 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
</or>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
|
|
@ -1359,14 +1335,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>MCT</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>TOGA</value>
|
||||
|
|
@ -1375,14 +1343,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
<not-equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>TOGA</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
|
@ -1397,6 +1357,14 @@
|
|||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
|
|
@ -1405,14 +1373,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>TOGA</value>
|
||||
|
|
@ -1421,14 +1381,6 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>TOGA</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state3</property>
|
||||
<value>TOGA</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state4</property>
|
||||
<value>TOGA</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -1532,6 +1484,29 @@
|
|||
</font-resolution>
|
||||
</text>
|
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|
||||
<text>
|
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<name>athr-thr-fma</name>
|
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<offsets>
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<x-m>0.00091828</x-m>
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<y-m>-0.0546226</y-m>
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</offsets>
|
||||
<alignment>center-center</alignment>
|
||||
<axis-alignment>yz-plane</axis-alignment>
|
||||
<type type="string">text-value</type>
|
||||
<format type="string">THR</format>
|
||||
<property>autopilot/serviceable</property>
|
||||
<font type="string">helvetica_medium.txf</font>
|
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<draw-text type="bool">true</draw-text>
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|
||||
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|
||||
<font-resolution>
|
||||
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|
||||
<height type="int">32</height>
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||||
</font-resolution>
|
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|
||||
|
||||
<text>
|
||||
<name>athr-box-fma</name>
|
||||
<offsets>
|
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|
|
@ -1583,6 +1558,14 @@
|
|||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
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</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
|
|
@ -1642,6 +1625,45 @@
|
|||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
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<condition>
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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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|
||||
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|
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|
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|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<text>
|
||||
<name>athr-lvrclb-fma</name>
|
||||
<offsets>
|
||||
|
|
@ -1815,6 +1837,7 @@
|
|||
<object-name>athr-man-fma</object-name>
|
||||
<object-name>athr-toga-fma</object-name>
|
||||
<object-name>athr-mct-fma</object-name>
|
||||
<object-name>athr-thr-fma</object-name>
|
||||
<object-name>athr-box-fma</object-name>
|
||||
<object-name>athr-lvrclb-fma</object-name>
|
||||
<object-name>vs-num</object-name>
|
||||
|
|
|
|||
|
|
@ -1085,15 +1085,20 @@
|
|||
<object-name>thrpos1</object-name>
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<property>controls/engines/engine[0]/throttle</property>
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|
@ -1112,15 +1117,20 @@
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<object-name>thrpos2</object-name>
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<property>controls/engines/engine[1]/throttle</property>
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|
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|
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|
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<entry><ind>0.78000</ind><dep>89</dep></entry>
|
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|
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<entry><ind>0.83000</ind><dep>90</dep></entry>
|
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<entry><ind>0.94999</ind><dep>92</dep></entry>
|
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|
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|
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</interpolation>
|
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<center>
|
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<x-m>0</x-m>
|
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|
|
@ -1185,7 +1195,7 @@
|
|||
<object-name>n11</object-name>
|
||||
<property>engines/engine/n1</property>
|
||||
<interpolation>
|
||||
<entry><ind> 23</ind><dep> 0</dep></entry>
|
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<entry><ind> 20</ind><dep> 0</dep></entry>
|
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<entry><ind> 40</ind><dep> 47</dep></entry>
|
||||
<entry><ind>100</ind><dep>159</dep></entry>
|
||||
<entry><ind>110</ind><dep>170</dep></entry>
|
||||
|
|
@ -1207,7 +1217,7 @@
|
|||
<object-name>n12</object-name>
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<property>engines/engine[1]/n1</property>
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<interpolation>
|
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<entry><ind> 23</ind><dep> 0</dep></entry>
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<entry><ind> 40</ind><dep> 47</dep></entry>
|
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<entry><ind>100</ind><dep>159</dep></entry>
|
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<entry><ind>110</ind><dep>170</dep></entry>
|
||||
|
|
|
|||
|
|
@ -185,7 +185,7 @@ setlistener("/sim/signals/fdm-initialized", func {
|
|||
setprop("/it-autoflight/settings/land-enable", 1); # Enable or disable automatic landing.
|
||||
setprop("/it-autoflight/autoland/flare-altitude", 40); # Altitude when the flare mode starts in an autoland.
|
||||
setprop("/controls/engines/thrust-limit", "TOGA");
|
||||
setprop("/controls/engines/epr-limit", 1.379);
|
||||
setprop("/controls/engines/epr-limit", 1.301);
|
||||
setprop("/controls/engines/n1-limit", 97.8);
|
||||
});
|
||||
|
||||
|
|
|
|||
|
|
@ -6,7 +6,7 @@ setlistener("/sim/signals/fdm-initialized", func {
|
|||
setprop("/systems/thrust/state1", "IDLE");
|
||||
setprop("/systems/thrust/state2", "IDLE");
|
||||
setprop("/systems/thrust/lvrclb", "0");
|
||||
setprop("/systems/thrust/clbreduc-ft", "2000");
|
||||
setprop("/systems/thrust/clbreduc-ft", "1500");
|
||||
lvrclb();
|
||||
print("Thrust System ... Done!")
|
||||
});
|
||||
|
|
@ -16,17 +16,22 @@ setlistener("/controls/engines/engine[0]/throttle", func {
|
|||
if (thrr < 0.05) {
|
||||
setprop("/systems/thrust/state1", "IDLE");
|
||||
atoff_request();
|
||||
} else if (thrr >= 0.05 and thrr < 0.60) {
|
||||
} else if (thrr >= 0.01 and thrr < 0.60) {
|
||||
setprop("/systems/thrust/state1", "MAN");
|
||||
} else if (thrr >= 0.60 and thrr < 0.80) {
|
||||
} else if (thrr >= 0.60 and thrr < 0.65) {
|
||||
setprop("/systems/thrust/state1", "CL");
|
||||
} else if (thrr >= 0.80 and thrr < 0.95) {
|
||||
} else if (thrr >= 0.65 and thrr < 0.78) {
|
||||
setprop("/systems/thrust/state1", "MAN THR");
|
||||
} else if (thrr >= 0.78 and thrr < 0.83) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/controls/engines/engine[0]/throttle-fdm", 0.94);
|
||||
setprop("/controls/engines/engine[0]/throttle-fdm", 0.90);
|
||||
setprop("/systems/thrust/state1", "MCT");
|
||||
} else if (thrr >= 0.83 and thrr < 0.95) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/systems/thrust/state1", "MAN THR");
|
||||
} else if (thrr >= 0.95) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/controls/engines/engine[0]/throttle-fdm", 0.98);
|
||||
setprop("/controls/engines/engine[0]/throttle-fdm", 0.95);
|
||||
setprop("/systems/thrust/state1", "TOGA");
|
||||
}
|
||||
});
|
||||
|
|
@ -36,17 +41,22 @@ setlistener("/controls/engines/engine[1]/throttle", func {
|
|||
if (thrr < 0.05) {
|
||||
setprop("/systems/thrust/state2", "IDLE");
|
||||
atoff_request();
|
||||
} else if (thrr >= 0.05 and thrr < 0.60) {
|
||||
} else if (thrr >= 0.01 and thrr < 0.60) {
|
||||
setprop("/systems/thrust/state2", "MAN");
|
||||
} else if (thrr >= 0.60 and thrr < 0.80) {
|
||||
} else if (thrr >= 0.60 and thrr < 0.65) {
|
||||
setprop("/systems/thrust/state2", "CL");
|
||||
} else if (thrr >= 0.80 and thrr < 0.95) {
|
||||
} else if (thrr >= 0.65 and thrr < 0.78) {
|
||||
setprop("/systems/thrust/state2", "MAN THR");
|
||||
} else if (thrr >= 0.78 and thrr < 0.83) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/controls/engines/engine[1]/throttle-fdm", 0.94);
|
||||
setprop("/controls/engines/engine[1]/throttle-fdm", 0.90);
|
||||
setprop("/systems/thrust/state2", "MCT");
|
||||
} else if (thrr >= 0.83 and thrr < 0.95) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/systems/thrust/state2", "MAN THR");
|
||||
} else if (thrr >= 0.95) {
|
||||
setprop("/it-autoflight/input/athr", 1);
|
||||
setprop("/controls/engines/engine[1]/throttle-fdm", 0.98);
|
||||
setprop("/controls/engines/engine[1]/throttle-fdm", 0.95);
|
||||
setprop("/systems/thrust/state2", "TOGA");
|
||||
}
|
||||
});
|
||||
|
|
|
|||
|
|
@ -14,7 +14,7 @@
|
|||
<entry><ind> 18</ind><dep>0.988</dep></entry>
|
||||
<entry><ind> 23</ind><dep>1.000</dep></entry>
|
||||
<entry><ind> 35</ind><dep>1.060</dep></entry>
|
||||
<entry><ind>105.0</ind><dep>1.380</dep></entry>
|
||||
<entry><ind>105.0</ind><dep>1.322</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
@ -33,7 +33,7 @@
|
|||
<entry><ind> 18</ind><dep>0.988</dep></entry>
|
||||
<entry><ind> 23</ind><dep>1.000</dep></entry>
|
||||
<entry><ind> 35</ind><dep>1.060</dep></entry>
|
||||
<entry><ind>105.0</ind><dep>1.380</dep></entry>
|
||||
<entry><ind>105.0</ind><dep>1.322</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
|
|||
|
|
@ -1,7 +1,7 @@
|
|||
<?xml version="1.0" encoding="UTF-8"?>
|
||||
|
||||
<!-- Joshua Davidson (it0uchpods/411) -->
|
||||
<!-- This file adjustes the value for the manual thrust/autothrottle input for the engines. It is then sent to thrust.nas. -->
|
||||
<!-- This file adjustes the value for the manual thrust/autothrottle input for the engines. -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
|
|
@ -14,8 +14,12 @@
|
|||
<expression>
|
||||
<table>
|
||||
<property>/controls/engines/engine[0]/throttle</property>
|
||||
<entry><ind>0.0</ind><dep>0.00</dep></entry>
|
||||
<entry><ind>0.6</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.00</ind><dep>0.00</dep></entry>
|
||||
<entry><ind>0.60</ind><dep>0.83</dep></entry>
|
||||
<entry><ind>0.65</ind><dep>0.83</dep></entry>
|
||||
<entry><ind>0.78</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.83</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.95</ind><dep>0.95</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
@ -31,8 +35,12 @@
|
|||
<expression>
|
||||
<table>
|
||||
<property>/controls/engines/engine[1]/throttle</property>
|
||||
<entry><ind>0.0</ind><dep>0.00</dep></entry>
|
||||
<entry><ind>0.6</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.00</ind><dep>0.00</dep></entry>
|
||||
<entry><ind>0.60</ind><dep>0.83</dep></entry>
|
||||
<entry><ind>0.65</ind><dep>0.83</dep></entry>
|
||||
<entry><ind>0.78</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.83</ind><dep>0.90</dep></entry>
|
||||
<entry><ind>0.95</ind><dep>0.95</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
@ -47,6 +55,10 @@
|
|||
<enable>
|
||||
<condition>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
|
|
@ -64,26 +76,32 @@
|
|||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[0]/throttle-man</property>
|
||||
</input>
|
||||
|
|
@ -112,6 +130,15 @@
|
|||
<property>/controls/engines/engine[0]/throttle-fdm</property>
|
||||
</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>1</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
|
|
@ -168,7 +195,7 @@
|
|||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
<value>0.2</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
|
|
@ -189,6 +216,10 @@
|
|||
<enable>
|
||||
<condition>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
|
|
@ -206,26 +237,32 @@
|
|||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[1]/throttle-man</property>
|
||||
</input>
|
||||
|
|
@ -254,6 +291,15 @@
|
|||
<property>/controls/engines/engine[1]/throttle-fdm</property>
|
||||
</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>1</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
|
|
@ -310,7 +356,7 @@
|
|||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
<value>0.2</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
|
|
|
|||
Reference in a new issue