some fixes, and new ITAF
This commit is contained in:
Joshua Davidson
parent
ae9969fd2a
commit
71ec680bc5
25 changed files with 663 additions and 1009 deletions
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@ -70,8 +70,6 @@
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<A320>
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<file>Aircraft/A320Family/Nasal/engines.nas</file>
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<file>Aircraft/A320Family/Nasal/electrical.nas</file>
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<file>Aircraft/A320Family/Nasal/v-speeds.nas</file>
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<file>Aircraft/A320Family/Nasal/tyresmoke.nas</file>
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<file>Aircraft/A320Family/Nasal/systems.nas</file>
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<file>Aircraft/A320Family/Nasal/a319livery.nas</file>
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<file>Aircraft/A320Family/Models/Instruments/ND/ND.nas</file>
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@ -79,13 +77,11 @@
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<file>Aircraft/A320Family/Nasal/efis.nas</file>
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<file>Aircraft/A320Family/Nasal/PFD_FMA.nas</file>
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<file>Aircraft/A320Family/Nasal/fctl.nas</file>
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file>
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</A320>
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<itaf>
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<file>Aircraft/A320Family/Nasal/it-autoflight.nas</file>
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</itaf>
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<lgciu>
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file>
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</lgciu>
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<thrust>
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<file>Aircraft/A320Family/Nasal/thrust.nas</file>
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</thrust>
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@ -70,8 +70,6 @@
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<A320>
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<file>Aircraft/A320Family/Nasal/engines.nas</file>
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<file>Aircraft/A320Family/Nasal/electrical.nas</file>
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<file>Aircraft/A320Family/Nasal/v-speeds.nas</file>
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<file>Aircraft/A320Family/Nasal/tyresmoke.nas</file>
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<file>Aircraft/A320Family/Nasal/systems.nas</file>
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<file>Aircraft/A320Family/Nasal/a320livery.nas</file>
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<file>Aircraft/A320Family/Models/Instruments/ND/ND.nas</file>
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@ -79,12 +77,11 @@
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<file>Aircraft/A320Family/Nasal/efis.nas</file>
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<file>Aircraft/A320Family/Nasal/PFD_FMA.nas</file>
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<file>Aircraft/A320Family/Nasal/fctl.nas</file>
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file> <!-- it0uchpods please leave this here! -->
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file>
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</A320>
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<itaf>
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<file>Aircraft/A320Family/Nasal/it-autoflight.nas</file>
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</itaf>
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<thrust>
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<file>Aircraft/A320Family/Nasal/thrust.nas</file>
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</thrust>
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@ -223,44 +223,49 @@
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<max-lb type="double">3300.320</max-lb>
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</weight>
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</payload>
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<it-autoflight>
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<config>
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<altitude-dial-mode>0</altitude-dial-mode>
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<roll>
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<umin>-0.40</umin>
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<umax>0.40</umax>
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<kp>0.09</kp>
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<ti>10.0</ti>
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<td>0.00001</td>
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</roll>
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<vorloc>
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<kp>0.06</kp>
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<kp-vloc>0.09</kp-vloc>
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<ti>10.0</ti>
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<td>0.00001</td>
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</vorloc>
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<kp-cws>0.09</kp-cws>
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</roll>
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<pitch>
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<umin>-0.25</umin>
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<umax>0.25</umax>
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<umin>-0.30</umin>
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<umax>0.30</umax>
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<kp>-0.05</kp>
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<ti>10.0</ti>
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<td>0.0001</td>
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<kp-cws>-0.07</kp-cws>
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</pitch>
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<flch>
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<umin>-0.25</umin>
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<umax>0.25</umax>
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<kp>-0.03</kp>
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<ti>10.0</ti>
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<td>0.00001</td>
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</flch>
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<gs>
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<kp>0.10</kp>
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</gs>
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<cmd>
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<roll-scale>5</roll-scale>
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<vorloc>-4.0</vorloc>
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<alt>0.025</alt>
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<vs>0.07</vs>
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<flch>-0.30</flch>
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<gs>0.10</gs>
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</cmd>
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<autoland>
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<kp-roll>0.10</kp-roll>
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<kp-pitch>0.01</kp-pitch>
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<kp-rudder>-0.3</kp-rudder>
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</autoland>
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</config>
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<settings>
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<flare-altitude>40</flare-altitude>
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<land-enable>1</land-enable>
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<land-flap>0.645</land-flap>
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<retard-ft>40</retard-ft>
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<retard-enable>0</retard-enable>
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<toga-pitch>15</toga-pitch>
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</settings>
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</it-autoflight>
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<autopilot>
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@ -70,8 +70,6 @@
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<A320>
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<file>Aircraft/A320Family/Nasal/engines.nas</file>
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<file>Aircraft/A320Family/Nasal/electrical.nas</file>
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<file>Aircraft/A320Family/Nasal/v-speeds.nas</file>
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<file>Aircraft/A320Family/Nasal/tyresmoke.nas</file>
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<file>Aircraft/A320Family/Nasal/systems.nas</file>
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<file>Aircraft/A320Family/Nasal/a321livery.nas</file>
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<file>Aircraft/A320Family/Models/Instruments/ND/ND.nas</file>
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@ -79,13 +77,11 @@
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<file>Aircraft/A320Family/Nasal/efis.nas</file>
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<file>Aircraft/A320Family/Nasal/PFD_FMA.nas</file>
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<file>Aircraft/A320Family/Nasal/fctl.nas</file>
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file>
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</A320>
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<itaf>
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<file>Aircraft/A320Family/Nasal/it-autoflight.nas</file>
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</itaf>
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<lgciu>
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<file>Aircraft/A320Family/Nasal/LGCIU.nas</file>
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</lgciu>
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<thrust>
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<file>Aircraft/A320Family/Nasal/thrust.nas</file>
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</thrust>
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@ -17,9 +17,9 @@
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<tsfc> 0.8 </tsfc>
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<bleed> 0.03</bleed>
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<idlen1> 23.4 </idlen1>
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<idlen2> 63.7 </idlen2>
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<idlen2> 62.7 </idlen2>
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<maxn1> 105.8 </maxn1>
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<maxn2> 112.5 </maxn2>
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<maxn2> 102.1 </maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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@ -13,13 +13,13 @@
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<turbine_engine name="V2527_A5">
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<milthrust> 26600 </milthrust>
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<bypassratio> 0.1 </bypassratio>
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<bypassratio> 2.0 </bypassratio>
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<tsfc> 0.8 </tsfc>
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<bleed> 0.03</bleed>
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<idlen1> 23.4 </idlen1>
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<idlen2> 63.7 </idlen2>
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<idlen2> 62.7 </idlen2>
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<maxn1> 105.8 </maxn1>
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<maxn2> 112.5 </maxn2>
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<maxn2> 102.1 </maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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@ -17,9 +17,9 @@
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<tsfc> 0.8 </tsfc>
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<bleed> 0.03</bleed>
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<idlen1> 23.4 </idlen1>
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<idlen2> 63.7 </idlen2>
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<idlen2> 62.7 </idlen2>
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<maxn1> 105.8 </maxn1>
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<maxn2> 112.5 </maxn2>
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<maxn2> 102.1</maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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@ -265,6 +265,14 @@
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<property>/it-autoflight/output/lat</property>
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<value>2</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>4</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>5</value>
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</equals>
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</or>
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</condition>
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</animation>
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@ -444,7 +444,7 @@ refs 4
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numvert 4
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@ -1,558 +0,0 @@
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AC3Db
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name "gsscale"
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loc 0.00091828 0.0004113 -0.0352752
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texture "symbols.png"
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crease 45.000000
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||||
numvert 4
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name "locscale"
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||||
texture "symbols.png"
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mat 0
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OBJECT poly
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name "gspointer"
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loc 0.00226889 9.10088e-006 -0.0356073
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texture "symbols.png"
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crease 45.000000
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||||
numvert 4
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numsurf 1
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SURF 0x30
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||||
mat 0
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||||
refs 4
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kids 0
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OBJECT poly
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||||
name "locpointer"
|
||||
loc 0.00226889 -0.0482638 0.00541306
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||||
texture "symbols.png"
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crease 45.000000
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numvert 4
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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kids 0
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OBJECT poly
|
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name "vls-tape"
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||||
loc 0.00091828 -0.000281699 0.0476063
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||||
texture "vls-tape.png"
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||||
crease 45.000000
|
||||
numvert 4
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||||
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-1e-005 -0.0424935 -0.00136903
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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1 0 0.321832
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3 1 0.0448185
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kids 0
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OBJECT poly
|
||||
name "stall-tape"
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||||
loc 0.00091828 -0.000281699 0.0476063
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||||
texture "spd-tape.png"
|
||||
crease 45.000000
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||||
numvert 4
|
||||
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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3 0.598403 0.0448185
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kids 0
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OBJECT poly
|
||||
name "vfe-tape"
|
||||
loc 0.00091828 -0.000281699 0.0476063
|
||||
texture "spd-tape.png"
|
||||
crease 45.000000
|
||||
numvert 4
|
||||
0 -0.0424935 -0.00136903
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||||
0 -0.0424935 0.00136901
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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2 0.605455 0.321965
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1 0.605455 0.0450599
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0 0.66857 0.0450599
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kids 0
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OBJECT poly
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||||
name "bank"
|
||||
loc 0.00147448 0.0381779 0.00511426
|
||||
texture "symbols.png"
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crease 45.000000
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||||
numvert 4
|
||||
0 -0.00444023 -0.00535177
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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2 0.505593 0.567016
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1 0.505593 0.295057
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0 0.348876 0.295057
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kids 0
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OBJECT poly
|
||||
name "alt-tape-2"
|
||||
loc 0.00091828 0.000295199 -0.0595814
|
||||
texture "alt-tape-2.png"
|
||||
crease 45.000000
|
||||
numvert 4
|
||||
0 -0.00598263 -0.00278856
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0 -0.00598263 0.00278853
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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1 0.0568116 -0.130193
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0 0.962665 -0.130193
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kids 0
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OBJECT poly
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name "radar-alt"
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||||
loc 0.000360576 -0.000264099 -0.0474465
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texture "radar-alt.png"
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crease 45.000000
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numvert 4
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0 0.0428304 -0.00806341
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0 -0.0428304 -0.00806341
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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3 0.990386 0.0507198
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kids 0
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OBJECT poly
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name "landing-elev"
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||||
loc 0.000360576 -0.000264099 -0.0474465
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||||
texture "arpt-elev.png"
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||||
crease 45.000000
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||||
numvert 4
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0 0.0428304 -0.00806341
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0 -0.0428304 -0.00806341
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numsurf 1
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SURF 0x30
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mat 0
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refs 4
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0 0.990386 0.217208
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3 0.990386 0.0507198
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kids 0
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OBJECT poly
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name "rect"
|
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loc 0.0643506 4.65661e-010 2.32831e-010
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||||
texture "mask.png"
|
||||
crease 45.000000
|
||||
numvert 4
|
||||
-0.0639733 0.0784821 -0.0784821
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||||
-0.0639733 0.0784821 0.0784821
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||||
-0.0639733 -0.0784821 0.0784821
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||||
-0.0639733 -0.0784821 -0.0784821
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numsurf 1
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||||
SURF 0x30
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||||
mat 0
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refs 4
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0 1 1
|
||||
1 0 1
|
||||
2 0 0
|
||||
3 1 0
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||||
kids 0
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||||
OBJECT poly
|
||||
name "spdtrnd-down"
|
||||
loc 0.00133822 -0.0211824 0.0513713
|
||||
texture "spdtrend.png"
|
||||
crease 45.000000
|
||||
numvert 4
|
||||
0 0.0210118 0.00234548
|
||||
0 0.0210118 -0.00234545
|
||||
0 -0.0210118 -0.00234544
|
||||
0 -0.0210118 0.00234548
|
||||
numsurf 1
|
||||
SURF 0x30
|
||||
mat 0
|
||||
refs 4
|
||||
3 0 0.496308
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||||
2 1.03601 0.496308
|
||||
1 1.03601 -0.00461811
|
||||
0 0 -0.00461811
|
||||
kids 0
|
||||
OBJECT poly
|
||||
name "fd_roll"
|
||||
loc 0.00132974 0.000720247 0.00491576
|
||||
texture "symbols.png"
|
||||
crease 45.000000
|
||||
numvert 4
|
||||
0 0.0195466 -0.000502482
|
||||
0 -0.0195466 -0.000502482
|
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0 -0.0195466 0.000502482
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||||
0 0.0195466 0.000502482
|
||||
numsurf 1
|
||||
SURF 0x30
|
||||
mat 0
|
||||
refs 4
|
||||
3 0.510324 0.464321
|
||||
2 0.762653 0.464321
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1 0.762653 0.461267
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0 0.510324 0.461267
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kids 0
|
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|
|
@ -14,7 +14,7 @@
|
|||
</overlay>
|
||||
</model>
|
||||
|
||||
<model>
|
||||
<!--model>
|
||||
<name>Port tire smoke</name>
|
||||
<path>Aircraft/Generic/Effects/tyre-smoke-port.xml</path>
|
||||
<offsets>
|
||||
|
|
@ -22,7 +22,7 @@
|
|||
<y-m>0</y-m>
|
||||
<z-m>-0.572</z-m>
|
||||
</offsets>
|
||||
</model>
|
||||
</model-->
|
||||
|
||||
<!-- Gear compression -->
|
||||
<animation>
|
||||
|
|
|
|||
|
|
@ -14,7 +14,7 @@
|
|||
</overlay>
|
||||
</model>
|
||||
|
||||
<model>
|
||||
<!--model>
|
||||
<name>Starboard tire smoke</name>
|
||||
<path>Aircraft/Generic/Effects/tyre-smoke-stbd.xml</path>
|
||||
<offsets>
|
||||
|
|
@ -22,7 +22,7 @@
|
|||
<y-m>0</y-m>
|
||||
<z-m>-0.572</z-m>
|
||||
</offsets>
|
||||
</model>
|
||||
</model-->
|
||||
|
||||
<!-- Gear compression -->
|
||||
<animation>
|
||||
|
|
|
|||
|
|
@ -14,7 +14,7 @@
|
|||
</offsets>
|
||||
</model>
|
||||
|
||||
<model>
|
||||
<!--model>
|
||||
<name>Nose tire smoke</name>
|
||||
<path>Aircraft/Generic/Effects/tyre-smoke-nose.xml</path>
|
||||
<offsets>
|
||||
|
|
@ -22,7 +22,7 @@
|
|||
<y-m>0</y-m>
|
||||
<z-m>-2.314</z-m>
|
||||
</offsets>
|
||||
</model>
|
||||
</model-->
|
||||
|
||||
<!-- Gear compression -->
|
||||
<animation>
|
||||
|
|
|
|||
|
|
@ -3,7 +3,7 @@
|
|||
|
||||
# Speed or Mach?
|
||||
var speedmach = func {
|
||||
if (getprop("/it-autoflight/output/vert") == 4) {
|
||||
if ((getprop("/it-autoflight/output/vert") == 4) or (getprop("/it-autoflight/output/vert") == 6) or (getprop("/it-autoflight/output/vert") == 7)) {
|
||||
# Do nothing because it's in FLCH mode.
|
||||
} else {
|
||||
if (getprop("/it-autoflight/input/kts-mach") == 0) {
|
||||
|
|
@ -42,6 +42,8 @@ setlistener("/it-autoflight/mode/lat", func {
|
|||
setprop("/modes/pfd/fma/roll-mode", "LOC");
|
||||
} else if (lat == "ALGN") {
|
||||
setprop("/modes/pfd/fma/roll-mode", "ALN");
|
||||
} else if (lat == "T/O") {
|
||||
setprop("/modes/pfd/fma/roll-mode", " ");
|
||||
}
|
||||
});
|
||||
|
||||
|
|
@ -60,10 +62,16 @@ setlistener("/it-autoflight/mode/vert", func {
|
|||
setprop("/modes/pfd/fma/pitch-mode", "OP CLB");
|
||||
} else if (vert == "SPD DES") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "OP DES");
|
||||
} else if (vert == "FPA") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "FPA");
|
||||
} else if (vert == "LAND 3") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "LAND");
|
||||
} else if (vert == "FLARE") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "FLARE");
|
||||
} else if (vert == "T/O CLB") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "SRS");
|
||||
} else if (vert == "G/A CLB") {
|
||||
setprop("/modes/pfd/fma/pitch-mode", "SRS");
|
||||
}
|
||||
});
|
||||
|
||||
|
|
|
|||
|
|
@ -1,18 +1,15 @@
|
|||
# IT AUTOFLIGHT System Controller by Joshua Davidson (it0uchpods/411).
|
||||
# V3.0.0 Milestone 3 Build 78
|
||||
# V3.0.0 Build 110
|
||||
# This program is 100% GPL!
|
||||
|
||||
print("IT-AUTOFLIGHT: Please Wait!");
|
||||
setprop("/it-autoflight/settings/retard-enable", 1); # Do not change this here! See IT-AUTOFLIGHT's Help.txt
|
||||
setprop("/it-autoflight/settings/retard-ft", 50); # Do not change this here! See IT-AUTOFLIGHT's Help.txt
|
||||
setprop("/it-autoflight/settings/land-flap", 0.6); # Do not change this here! See IT-AUTOFLIGHT's Help.txt
|
||||
setprop("/it-autoflight/settings/land-enable", 1); # Do not change this here! See IT-AUTOFLIGHT's Help.txt
|
||||
setprop("/it-autoflight/autoland/flare-altitude", 20); # Do not change this here! See IT-AUTOFLIGHT's Help.txt
|
||||
|
||||
var ap_init = func {
|
||||
setprop("/it-autoflight/input/kts-mach", 0);
|
||||
setprop("/it-autoflight/input/ap1", 0);
|
||||
setprop("/it-autoflight/input/ap2", 0);
|
||||
setprop("/it-autoflight/input/athr", 0);
|
||||
setprop("/it-autoflight/input/cws", 0);
|
||||
setprop("/it-autoflight/input/fd1", 0);
|
||||
setprop("/it-autoflight/input/fd2", 0);
|
||||
setprop("/it-autoflight/input/spd-kts", 200);
|
||||
|
|
@ -20,25 +17,31 @@ var ap_init = func {
|
|||
setprop("/it-autoflight/input/hdg", 360);
|
||||
setprop("/it-autoflight/input/alt", 10000);
|
||||
setprop("/it-autoflight/input/vs", 0);
|
||||
setprop("/it-autoflight/input/lat", 0);
|
||||
setprop("/it-autoflight/input/vert", 4);
|
||||
setprop("/it-autoflight/input/lat", 5);
|
||||
setprop("/it-autoflight/input/vert", 7);
|
||||
setprop("/it-autoflight/input/bank-limit", 30);
|
||||
setprop("/it-autoflight/input/trk", 0);
|
||||
setprop("/it-autoflight/input/toga", 0);
|
||||
setprop("/it-autoflight/output/ap1", 0);
|
||||
setprop("/it-autoflight/output/ap2", 0);
|
||||
setprop("/it-autoflight/output/at", 0);
|
||||
setprop("/it-autoflight/output/athr", 0);
|
||||
setprop("/it-autoflight/output/cws", 0);
|
||||
setprop("/it-autoflight/output/fd1", 0);
|
||||
setprop("/it-autoflight/output/fd2", 0);
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/thr-mode", 0);
|
||||
setprop("/it-autoflight/output/retard", 0);
|
||||
setprop("/it-autoflight/settings/min-pitch", -4);
|
||||
setprop("/it-autoflight/settings/min-pitch", -8);
|
||||
setprop("/it-autoflight/settings/max-pitch", 8);
|
||||
setprop("/it-autoflight/internal/min-pitch", -4);
|
||||
setprop("/it-autoflight/internal/min-pitch", -8);
|
||||
setprop("/it-autoflight/internal/max-pitch", 8);
|
||||
setprop("/it-autoflight/internal/alt", 10000);
|
||||
setprop("/it-autoflight/autoland/target-vs", "-500");
|
||||
setprop("/it-autoflight/internal/cwsr", 0);
|
||||
setprop("/it-autoflight/internal/cwsp", 0);
|
||||
setprop("/it-autoflight/autoland/target-vs", "-650");
|
||||
setprop("/it-autoflight/mode/lat", "T/O");
|
||||
setprop("/it-autoflight/mode/vert", "T/O CLB");
|
||||
update_arms();
|
||||
print("IT-AUTOFLIGHT: Done!");
|
||||
}
|
||||
|
|
@ -48,6 +51,7 @@ setlistener("/it-autoflight/input/ap1", func {
|
|||
var apmas = getprop("/it-autoflight/input/ap1");
|
||||
if (apmas == 0) {
|
||||
setprop("/it-autoflight/output/ap1", 0);
|
||||
setprop("/controls/flight/rudder", 0);
|
||||
if (getprop("/it-autoflight/sound/enableapoffsound") == 1) {
|
||||
setprop("/it-autoflight/sound/apoffsound", 1);
|
||||
setprop("/it-autoflight/sound/enableapoffsound", 0);
|
||||
|
|
@ -65,6 +69,7 @@ setlistener("/it-autoflight/input/ap2", func {
|
|||
var apmas = getprop("/it-autoflight/input/ap2");
|
||||
if (apmas == 0) {
|
||||
setprop("/it-autoflight/output/ap2", 0);
|
||||
setprop("/controls/flight/rudder", 0);
|
||||
if (getprop("/it-autoflight/sound/enableapoffsound2") == 1) {
|
||||
setprop("/it-autoflight/sound/apoffsound2", 1);
|
||||
setprop("/it-autoflight/sound/enableapoffsound2", 0);
|
||||
|
|
@ -87,6 +92,29 @@ setlistener("/it-autoflight/input/athr", func {
|
|||
}
|
||||
});
|
||||
|
||||
# CWS Master System
|
||||
setlistener("/it-autoflight/input/cws", func {
|
||||
var cwsmas = getprop("/it-autoflight/input/cws");
|
||||
if (cwsmas == 1) {
|
||||
setprop("/it-autoflight/sound/enableapoffsound", 1);
|
||||
setprop("/it-autoflight/sound/apoffsound", 0);
|
||||
setprop("/it-autoflight/sound/enableapoffsound2", 1);
|
||||
setprop("/it-autoflight/sound/apoffsound2", 0);
|
||||
setprop("/it-autoflight/output/ap1", 0);
|
||||
setprop("/it-autoflight/output/ap2", 0);
|
||||
setprop("/it-autoflight/internal/cws-roll-deg", getprop("/orientation/roll-deg"));
|
||||
setprop("/it-autoflight/internal/cws-pitch-deg", getprop("/orientation/pitch-deg"));
|
||||
cwsrollt.start();
|
||||
cwspitcht.start();
|
||||
setprop("/it-autoflight/output/cws", 1);
|
||||
} else if (cwsmas == 0) {
|
||||
cwsrollt.stop();
|
||||
cwspitcht.stop();
|
||||
setprop("/it-autoflight/output/cws", 0);
|
||||
setprop("/controls/flight/aileron-trim", 0);
|
||||
}
|
||||
});
|
||||
|
||||
# Flight Director 1 Master System
|
||||
setlistener("/it-autoflight/input/fd1", func {
|
||||
var fdmas = getprop("/it-autoflight/input/fd1");
|
||||
|
|
@ -109,14 +137,22 @@ setlistener("/it-autoflight/input/fd2", func {
|
|||
|
||||
# Master Lateral
|
||||
setlistener("/it-autoflight/input/lat", func {
|
||||
lateral();
|
||||
});
|
||||
|
||||
var lateral = func {
|
||||
var latset = getprop("/it-autoflight/input/lat");
|
||||
if (latset == 0) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/lat", 0);
|
||||
setprop("/it-autoflight/mode/lat", "HDG");
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
} else if (latset == 1) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/lat", 1);
|
||||
|
|
@ -128,6 +164,8 @@ setlistener("/it-autoflight/input/lat", func {
|
|||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/mode/arm", "LOC");
|
||||
} else if (latset == 3) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/lat", 0);
|
||||
|
|
@ -138,13 +176,21 @@ setlistener("/it-autoflight/input/lat", func {
|
|||
} else if (latset == 4) {
|
||||
setprop("/it-autoflight/output/lat", 4);
|
||||
setprop("/it-autoflight/mode/lat", "ALGN");
|
||||
} else if (latset == 5) {
|
||||
setprop("/it-autoflight/output/lat", 5);
|
||||
}
|
||||
});
|
||||
}
|
||||
|
||||
# Master Vertical
|
||||
setlistener("/it-autoflight/input/vert", func {
|
||||
vertical();
|
||||
});
|
||||
|
||||
var vertical = func {
|
||||
var vertset = getprop("/it-autoflight/input/vert");
|
||||
if (vertset == 0) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/vert", 0);
|
||||
setprop("/it-autoflight/mode/vert", "ALT HLD");
|
||||
|
|
@ -156,8 +202,10 @@ setlistener("/it-autoflight/input/vert", func {
|
|||
var altnow = int((getprop("/instrumentation/altimeter/indicated-altitude-ft")+50)/100)*100;
|
||||
setprop("/it-autoflight/input/alt", altnow);
|
||||
setprop("/it-autoflight/internal/alt", altnow);
|
||||
flchthrust();
|
||||
thrustmode();
|
||||
} else if (vertset == 1) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
var altinput = getprop("/it-autoflight/input/alt");
|
||||
setprop("/it-autoflight/internal/alt", altinput);
|
||||
var vsnow = int(getprop("/velocities/vertical-speed-fps")*0.6)*100;
|
||||
|
|
@ -170,14 +218,21 @@ setlistener("/it-autoflight/input/vert", func {
|
|||
} else {
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
}
|
||||
flchthrust();
|
||||
thrustmode();
|
||||
} else if (vertset == 2) {
|
||||
setprop("/instrumentation/nav/signal-quality-norm", 0);
|
||||
setprop("/it-autoflight/output/loc-armed", 1);
|
||||
if (getprop("/it-autoflight/output/lat") == 2) {
|
||||
# Do nothing because VORLOC is active
|
||||
} else {
|
||||
setprop("/instrumentation/nav/signal-quality-norm", 0);
|
||||
setprop("/it-autoflight/output/loc-armed", 1);
|
||||
}
|
||||
setprop("/instrumentation/nav/gs-rate-of-climb", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 1);
|
||||
setprop("/it-autoflight/mode/arm", "ILS");
|
||||
setprop("/it-autoflight/autoland/target-vs", "-650");
|
||||
} else if (vertset == 3) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
var pitchdeg = getprop("/orientation/pitch-deg");
|
||||
var calt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
||||
var alt = getprop("/it-autoflight/internal/alt");
|
||||
|
|
@ -190,7 +245,10 @@ setlistener("/it-autoflight/input/vert", func {
|
|||
minmaxtimer.start();
|
||||
setprop("/it-autoflight/output/vert", 0);
|
||||
setprop("/it-autoflight/mode/vert", "ALT CAP");
|
||||
thrustmode();
|
||||
} else if (vertset == 4) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
var altinput = getprop("/it-autoflight/input/alt");
|
||||
setprop("/it-autoflight/internal/alt", altinput);
|
||||
var calt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
||||
|
|
@ -207,29 +265,36 @@ setlistener("/it-autoflight/input/vert", func {
|
|||
setprop("/it-autoflight/mode/arm", " ");
|
||||
}
|
||||
} else if (vertset == 5) {
|
||||
# VNAV not ready yet, so do nothing
|
||||
# FPA not ready yet, so do nothing
|
||||
} else if (vertset == 6) {
|
||||
setprop("/it-autoflight/output/vert", 6);
|
||||
setprop("/it-autoflight/mode/vert", "LAND 3");
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
flchthrust();
|
||||
thrustmode();
|
||||
alandt.stop();
|
||||
alandt1.start();
|
||||
setprop("/it-autoflight/autoland/target-vs", "-500");
|
||||
setprop("/it-autoflight/autoland/target-vs", "-650");
|
||||
} else if (vertset == 7) {
|
||||
setprop("/it-autoflight/output/vert", 7);
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
togasel();
|
||||
thrustmode();
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
}
|
||||
});
|
||||
}
|
||||
|
||||
var flch_on = func {
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/vert", 4);
|
||||
flchtimer.start();
|
||||
thrustmodet.start();
|
||||
}
|
||||
var alt_on = func {
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/vert", 0);
|
||||
setprop("/it-autoflight/mode/vert", "ALT CAP");
|
||||
setprop("/it-autoflight/internal/max-pitch", 8);
|
||||
setprop("/it-autoflight/internal/min-pitch", -4);
|
||||
setprop("/it-autoflight/internal/min-pitch", -8);
|
||||
}
|
||||
|
||||
setlistener("/it-autoflight/input/kts-mach", func {
|
||||
|
|
@ -256,10 +321,36 @@ setlistener("/it-autoflight/output/vert", func {
|
|||
});
|
||||
|
||||
var altcapt = func {
|
||||
var vsnow = getprop("/it-autoflight/internal/vert-speed-fpm");
|
||||
if ((vsnow >= 0 and vsnow < 500) or (vsnow < 0 and vsnow > -500)) {
|
||||
setprop("/it-autoflight/internal/captvs", 100);
|
||||
setprop("/it-autoflight/internal/captvsneg", -100);
|
||||
} else if ((vsnow >= 500 and vsnow < 1000) or (vsnow < -500 and vsnow > -1000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 150);
|
||||
setprop("/it-autoflight/internal/captvsneg", -150);
|
||||
} else if ((vsnow >= 1000 and vsnow < 1500) or (vsnow < -1000 and vsnow > -1500)) {
|
||||
setprop("/it-autoflight/internal/captvs", 200);
|
||||
setprop("/it-autoflight/internal/captvsneg", -200);
|
||||
} else if ((vsnow >= 1500 and vsnow < 2000) or (vsnow < -1500 and vsnow > -2000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 300);
|
||||
setprop("/it-autoflight/internal/captvsneg", -300);
|
||||
} else if ((vsnow >= 2000 and vsnow < 3000) or (vsnow < -2000 and vsnow > -3000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 450);
|
||||
setprop("/it-autoflight/internal/captvsneg", -450);
|
||||
} else if ((vsnow >= 3000 and vsnow < 4000) or (vsnow < -3000 and vsnow > -4000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 650);
|
||||
setprop("/it-autoflight/internal/captvsneg", -650);
|
||||
} else if ((vsnow >= 4000 and vsnow < 5000) or (vsnow < -4000 and vsnow > -5000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 1000);
|
||||
setprop("/it-autoflight/internal/captvsneg", -1000);
|
||||
} else if ((vsnow >= 5000) or (vsnow < -5000)) {
|
||||
setprop("/it-autoflight/internal/captvs", 1250);
|
||||
setprop("/it-autoflight/internal/captvsneg", -1250);
|
||||
}
|
||||
var calt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
||||
var alt = getprop("/it-autoflight/internal/alt");
|
||||
var dif = calt - alt;
|
||||
if (dif < 500 and dif > -500) {
|
||||
if (dif < getprop("/it-autoflight/internal/captvs") and dif > getprop("/it-autoflight/internal/captvsneg")) {
|
||||
setprop("/it-autoflight/input/vert", 3);
|
||||
setprop("/it-autoflight/output/thr-mode", 0);
|
||||
}
|
||||
|
|
@ -267,8 +358,8 @@ var altcapt = func {
|
|||
setprop("/it-autoflight/internal/alt", altinput);
|
||||
}
|
||||
|
||||
# FLCH Thrust Mode Selector
|
||||
var flchthrust = func {
|
||||
# Thrust Mode Selector
|
||||
var thrustmode = func {
|
||||
var calt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
||||
var alt = getprop("/it-autoflight/internal/alt");
|
||||
var vertm = getprop("/it-autoflight/output/vert");
|
||||
|
|
@ -276,20 +367,23 @@ var flchthrust = func {
|
|||
if (calt < alt) {
|
||||
setprop("/it-autoflight/output/thr-mode", 2);
|
||||
setprop("/it-autoflight/mode/thr", " PITCH");
|
||||
setprop("/it-autoflight/mode/vert", "SPD CLB");
|
||||
setprop("/it-autoflight/mode/vert", "SPD CLB");
|
||||
} else if (calt > alt) {
|
||||
setprop("/it-autoflight/output/thr-mode", 1);
|
||||
setprop("/it-autoflight/mode/thr", " PITCH");
|
||||
setprop("/it-autoflight/mode/vert", "SPD DES");
|
||||
setprop("/it-autoflight/mode/vert", "SPD DES");
|
||||
} else {
|
||||
setprop("/it-autoflight/output/thr-mode", 0);
|
||||
setprop("/it-autoflight/mode/thr", "THRUST");
|
||||
setprop("/it-autoflight/input/vert", 3);
|
||||
}
|
||||
} else if (vertm == 7) {
|
||||
setprop("/it-autoflight/output/thr-mode", 2);
|
||||
setprop("/it-autoflight/mode/thr", " PITCH");
|
||||
} else {
|
||||
setprop("/it-autoflight/output/thr-mode", 0);
|
||||
setprop("/it-autoflight/mode/thr", "THRUST");
|
||||
flchtimer.stop();
|
||||
setprop("/it-autoflight/mode/thr", "THRUST");
|
||||
thrustmodet.stop();
|
||||
}
|
||||
}
|
||||
|
||||
|
|
@ -300,9 +394,9 @@ var minmax = func {
|
|||
var dif = calt - alt;
|
||||
if (dif < 100 and dif > -100) {
|
||||
setprop("/it-autoflight/internal/max-pitch", 8);
|
||||
setprop("/it-autoflight/internal/min-pitch", -4);
|
||||
setprop("/it-autoflight/internal/min-pitch", -5);
|
||||
var vertmode = getprop("/it-autoflight/output/vert");
|
||||
if (vertmode == 1 or vertmode == 2 or vertmode == 4) {
|
||||
if (vertmode == 1 or vertmode == 2 or vertmode == 4 or vertmode == 5 or vertmode == 6 or vertmode == 7) {
|
||||
# Do not change the vertical mode because we are not trying to capture altitude.
|
||||
} else {
|
||||
setprop("/it-autoflight/mode/vert", "ALT HLD");
|
||||
|
|
@ -334,7 +428,7 @@ var retardchk = func {
|
|||
atofft.start();
|
||||
} else {
|
||||
setprop("/it-autoflight/output/retard", 0);
|
||||
flchthrust();
|
||||
thrustmode();
|
||||
}
|
||||
}
|
||||
}
|
||||
|
|
@ -362,6 +456,26 @@ setlistener("/it-autoflight/input/hdg", func {
|
|||
setprop("/autopilot/settings/heading-bug-deg", getprop("/it-autoflight/input/hdg"));
|
||||
});
|
||||
|
||||
# TOGA
|
||||
setlistener("/it-autoflight/input/toga", func {
|
||||
if (getprop("/it-autoflight/input/toga") == 1) {
|
||||
setprop("/it-autoflight/input/vert", 7);
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/input/toga", 0);
|
||||
}
|
||||
});
|
||||
|
||||
var togasel = func {
|
||||
if ((getprop("/gear/gear[1]/wow") == 0) and (getprop("/gear/gear[2]/wow") == 0)) {
|
||||
setprop("/it-autoflight/mode/vert", "G/A CLB");
|
||||
} else {
|
||||
setprop("/it-autoflight/input/lat", 5);
|
||||
setprop("/it-autoflight/mode/lat", "T/O");
|
||||
setprop("/it-autoflight/mode/vert", "T/O CLB");
|
||||
}
|
||||
}
|
||||
|
||||
# LOC and G/S arming
|
||||
var update_arms = func {
|
||||
update_locarmelec();
|
||||
|
|
@ -383,9 +497,6 @@ var update_apparmelec = func {
|
|||
var appra = getprop("/it-autoflight/output/appr-armed");
|
||||
if (appra) {
|
||||
apparmcheck();
|
||||
if (getprop("/it-autoflight/settings/land-enable") == 1){
|
||||
alandt.start();
|
||||
}
|
||||
} else {
|
||||
return 0;
|
||||
}
|
||||
|
|
@ -414,7 +525,10 @@ var apparmcheck = func {
|
|||
setprop("/it-autoflight/output/vert", 2);
|
||||
setprop("/it-autoflight/mode/vert", "G/S");
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
flchthrust();
|
||||
if (getprop("/it-autoflight/settings/land-enable") == 1){
|
||||
alandt.start();
|
||||
}
|
||||
thrustmode();
|
||||
} else {
|
||||
return 0;
|
||||
}
|
||||
|
|
@ -424,19 +538,35 @@ var apparmcheck = func {
|
|||
var aland = func {
|
||||
var ap1 = getprop("/it-autoflight/output/ap1");
|
||||
var ap2 = getprop("/it-autoflight/output/ap2");
|
||||
if (ap1 or ap2) {
|
||||
if (getprop("/position/gear-agl-ft") <= 150) {
|
||||
if (getprop("/position/gear-agl-ft") <= 100) {
|
||||
if (ap1 or ap2) {
|
||||
setprop("/it-autoflight/input/lat", 4);
|
||||
setprop("/it-autoflight/input/vert", 6);
|
||||
} else {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
var aland1 = func {
|
||||
var aglal = getprop("/position/gear-agl-ft");
|
||||
var flarealt = getprop("/it-autoflight/autoland/flare-altitude");
|
||||
var flarealt = getprop("/it-autoflight/settings/flare-altitude");
|
||||
if (aglal <= flarealt and aglal > 5) {
|
||||
setprop("/it-autoflight/mode/vert", "FLARE");
|
||||
setprop("/it-autoflight/autoland/target-vs", "-120");
|
||||
}
|
||||
if ((getprop("/it-autoflight/output/ap1") == 0) and (getprop("/it-autoflight/output/ap2") == 0)) {
|
||||
alandt.stop();
|
||||
alandt1.stop();
|
||||
setprop("/it-autoflight/output/loc-armed", 0);
|
||||
setprop("/it-autoflight/output/lat", 2);
|
||||
setprop("/it-autoflight/mode/lat", "LOC");
|
||||
setprop("/it-autoflight/output/appr-armed", 0);
|
||||
setprop("/it-autoflight/output/vert", 2);
|
||||
setprop("/it-autoflight/mode/vert", "G/S");
|
||||
setprop("/it-autoflight/mode/arm", " ");
|
||||
}
|
||||
var gear1 = getprop("/gear/gear[1]/wow");
|
||||
var gear2 = getprop("/gear/gear[2]/wow");
|
||||
if (gear1 == 1 or gear2 == 1) {
|
||||
|
|
@ -447,13 +577,40 @@ var aland1 = func {
|
|||
}
|
||||
|
||||
# Autoland Stage 2 Logic (Rollout)
|
||||
# Coming soon, for now we just disconnect the AP on touch down.
|
||||
|
||||
|
||||
# CWS
|
||||
var cwsroll = func {
|
||||
var ail = getprop("/controls/flight/aileron");
|
||||
if (ail < 0.05 and ail > -0.05) {
|
||||
if (getprop("/it-autoflight/internal/cwsr") == 0) {
|
||||
setprop("/it-autoflight/internal/cws-roll-deg", getprop("/orientation/roll-deg"));
|
||||
}
|
||||
setprop("/it-autoflight/internal/cwsr", 1);
|
||||
} else {
|
||||
setprop("/it-autoflight/internal/cwsr", 0);
|
||||
}
|
||||
}
|
||||
|
||||
var cwspitch = func {
|
||||
var elv = getprop("/controls/flight/elevator");
|
||||
if (elv < 0.05 and elv > -0.05) {
|
||||
if (getprop("/it-autoflight/internal/cwsp") == 0) {
|
||||
setprop("/it-autoflight/internal/cws-pitch-deg", getprop("/orientation/pitch-deg"));
|
||||
}
|
||||
setprop("/it-autoflight/internal/cwsp", 1);
|
||||
} else {
|
||||
setprop("/it-autoflight/internal/cwsp", 0);
|
||||
}
|
||||
}
|
||||
|
||||
# Timers
|
||||
var altcaptt = maketimer(0.5, altcapt);
|
||||
var flchtimer = maketimer(0.5, flchthrust);
|
||||
var thrustmodet = maketimer(0.5, thrustmode);
|
||||
var minmaxtimer = maketimer(0.5, minmax);
|
||||
var retardt = maketimer(0.5, retardchk);
|
||||
var atofft = maketimer(0.5, atoffchk);
|
||||
var alandt = maketimer(0.5, aland);
|
||||
var alandt1 = maketimer(0.5, aland1);
|
||||
var alandt1 = maketimer(0.5, aland1);
|
||||
var cwsrollt = maketimer(0.1, cwsroll);
|
||||
var cwspitcht = maketimer(0.1, cwspitch);
|
||||
|
|
|
|||
|
|
@ -179,14 +179,11 @@ var triggerDoor = func(door, doorName, doorDesc)
|
|||
setlistener("/sim/signals/fdm-initialized", func {
|
||||
itaf.ap_init();
|
||||
var autopilot = gui.Dialog.new("sim/gui/dialogs/autopilot/dialog", "Aircraft/A320Family/Systems/autopilot-dlg.xml");
|
||||
setprop("/it-autoflight/settings/retard-enable", 0); # Enable or disable automatic autothrottle retard.
|
||||
setprop("/it-autoflight/settings/retard-ft", 50); # Add this to change the retard altitude.
|
||||
setprop("/it-autoflight/settings/land-flap", 0.645); # Define the landing flaps here. This is needed for autoland, and retard.
|
||||
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", 1.301);
|
||||
setprop("/controls/engines/n1-limit", 97.8);
|
||||
setprop("/it-autoflight/input/fd1", 1);
|
||||
setprop("/it-autoflight/input/fd2", 1);
|
||||
});
|
||||
|
||||
var aglgears = func {
|
||||
|
|
|
|||
|
|
@ -1,52 +0,0 @@
|
|||
var nose_wow_sav = 0;
|
||||
var left_wow_sav = 0;
|
||||
var right_wow_sav = 0;
|
||||
|
||||
var tyresmoke = func() {
|
||||
|
||||
if ((getprop("/sim/replay/time") == 0) or (getprop("/sim/replay/time") == nil)) {
|
||||
|
||||
if (getprop("/position/altitude-agl-ft") < 30) {
|
||||
|
||||
var nose_wow_cur = getprop("/gear/gear/wow");
|
||||
var left_wow_cur = getprop("/gear/gear[3]/wow");
|
||||
var right_wow_cur = getprop("/gear/gear[4]/wow");
|
||||
|
||||
if (nose_wow_cur and !nose_wow_sav)
|
||||
setprop("/aircraft/tyresmoke/nose", 1);
|
||||
else
|
||||
setprop("/aircraft/tyresmoke/nose", 0);
|
||||
|
||||
if (left_wow_cur and !left_wow_sav)
|
||||
setprop("/aircraft/tyresmoke/left", 1);
|
||||
else
|
||||
setprop("/aircraft/tyresmoke/left", 0);
|
||||
|
||||
if (right_wow_cur and !right_wow_sav)
|
||||
setprop("/aircraft/tyresmoke/right", 1);
|
||||
else
|
||||
setprop("/aircraft/tyresmoke/right", 0);
|
||||
|
||||
nose_wow_sav = nose_wow_cur;
|
||||
left_wow_sav = left_wow_cur;
|
||||
right_wow_sav = right_wow_cur;
|
||||
|
||||
if (left_wow_cur and (getprop("/velocities/airspeed-kt") > 70) and (getprop("controls/gear/brake-left") > 0.5)) {
|
||||
setprop("/aircraft/tyresmoke/left", 1);
|
||||
}
|
||||
|
||||
if (right_wow_cur and (getprop("/velocities/airspeed-kt") > 70) and (getprop("controls/gear/brake-right") > 0.5)) {
|
||||
setprop("/aircraft/tyresmoke/right", 1);
|
||||
}
|
||||
|
||||
} else {
|
||||
|
||||
setprop("/aircraft/tyresmoke/nose", 0);
|
||||
setprop("/aircraft/tyresmoke/left", 0);
|
||||
setprop("/aircraft/tyresmoke/right", 0);
|
||||
|
||||
}
|
||||
|
||||
}
|
||||
|
||||
};
|
||||
|
|
@ -1,38 +0,0 @@
|
|||
# Create initial announced variables at startup of the sim
|
||||
V1 = "";
|
||||
VR = "";
|
||||
V2 = "";
|
||||
|
||||
# The actual function
|
||||
var vspeeds = func {
|
||||
|
||||
# Create/populate variables at each function cycle
|
||||
# Retrieve total aircraft weight and convert to kg.
|
||||
WT = getprop("/fdm/jsbsim/inertia/weight-lbs")*0.00045359237;
|
||||
flaps = getprop("/instrumentation/fmc/to-flap");
|
||||
|
||||
# Calculate V-speeds with flaps 10
|
||||
if (flaps == 10) {
|
||||
V1 = (0.3*(WT-80))+125;
|
||||
VR = (0.3*(WT-80))+140;
|
||||
V2 = (0.3*(WT-80))+150;
|
||||
}
|
||||
|
||||
# Calculate V-speeds with flaps 15
|
||||
elsif (flaps == 15) {
|
||||
V1 = (0.3*(WT-80))+115;
|
||||
VR = (0.3*(WT-80))+130;
|
||||
V2 = (0.3*(WT-80))+140;
|
||||
}
|
||||
|
||||
# Export the calculated V-speeds to the property-tree, for further use
|
||||
setprop("/instrumentation/fmc/vspeeds/V1",V1);
|
||||
setprop("/instrumentation/fmc/vspeeds/VR",VR);
|
||||
setprop("/instrumentation/fmc/vspeeds/V2",V2);
|
||||
|
||||
# Repeat the function each second
|
||||
settimer(vspeeds, 1);
|
||||
}
|
||||
|
||||
# Only start the function when the FDM is initialized, to prevent the problem of not-yet-created properties.
|
||||
_setlistener("/sim/signals/fdm-initialized", vspeeds);
|
||||
|
|
@ -1,2 +1,2 @@
|
|||
# A320Family
|
||||
Airbus A320 Family for FlightGear. A320-200 Flyable! A319-200/A321-200 Flyable soon! Note: Flaps indicator still missing from ECAM, coming soon!
|
||||
Airbus A320 Family for FlightGear. Note: Flaps indicator still missing from ECAM, coming soon!
|
||||
Binary file not shown.
Binary file not shown.
|
|
@ -1,6 +1,6 @@
|
|||
<?xml version="1.0" encoding="UTF-8" ?>
|
||||
|
||||
<!-- IT-AUTOFLIGHT Autoflight Control Dialog -->
|
||||
<!-- IT-AUTOFLIGHT Autopilot Control Dialog -->
|
||||
|
||||
|
||||
<PropertyList>
|
||||
|
|
@ -13,7 +13,7 @@
|
|||
<layout>hbox</layout>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>IT-AUTOFLIGHT V3.0.0 Beta</label>
|
||||
<label>IT-AUTOFLIGHT System</label>
|
||||
</text>
|
||||
<button>
|
||||
<halign>right</halign>
|
||||
|
|
@ -56,17 +56,17 @@
|
|||
</binding>
|
||||
</button>
|
||||
<button>
|
||||
<legend>CWS</legend>
|
||||
<pref-width>35</pref-width>
|
||||
<enable>
|
||||
<equals>
|
||||
<property>/it-autoflight/settings/CWS-allowed</property>
|
||||
<value>blahblahblahblah</value>
|
||||
<property>/it-autoflight/settings/enable-cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</enable>
|
||||
<legend>CWS</legend>
|
||||
<pref-width>35</pref-width>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>/it-autoflight/unused/input/cws</property>
|
||||
<property>/it-autoflight/input/cws</property>
|
||||
</binding>
|
||||
</button>
|
||||
<button>
|
||||
|
|
@ -120,7 +120,7 @@
|
|||
<label>[CWS]</label>
|
||||
<visible>
|
||||
<equals>
|
||||
<property>/it-autoflight/unused/output/cws</property>
|
||||
<property>/it-autoflight/output/cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</visible>
|
||||
|
|
@ -240,16 +240,9 @@
|
|||
<row>0</row>
|
||||
<col>1</col>
|
||||
<legend>TOGA</legend>
|
||||
<enable>
|
||||
<equals>
|
||||
<property>/it-autoflight/unused/toga</property>
|
||||
<value>blahblahblahblah</value>
|
||||
</equals>
|
||||
</enable>
|
||||
<binding>
|
||||
<command>property-cycle</command>
|
||||
<property>/it-autoflight/toga</property>
|
||||
<value>0</value>
|
||||
<command>property-assign</command>
|
||||
<property>/it-autoflight/input/toga</property>
|
||||
<value>1</value>
|
||||
</binding>
|
||||
</button>
|
||||
|
|
@ -763,7 +756,7 @@
|
|||
|
||||
<button>
|
||||
<pref-width>40</pref-width>
|
||||
<legend>VNAV</legend>
|
||||
<legend>FPA</legend>
|
||||
<enable>
|
||||
<equals>
|
||||
<property>/it-autoflight/settings/disabled-button</property>
|
||||
|
|
@ -772,8 +765,8 @@
|
|||
</enable>
|
||||
<binding>
|
||||
<command>property-assign</command>
|
||||
<property>/it-autoflight/unused/vnav</property>
|
||||
<value>1</value>
|
||||
<property>/it-autoflight/input/vert</property>
|
||||
<value>5</value>
|
||||
</binding>
|
||||
</button>
|
||||
|
||||
|
|
|
|||
|
|
@ -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>1.322</dep></entry>
|
||||
<entry><ind>105.8</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>1.322</dep></entry>
|
||||
<entry><ind>105.8</ind><dep>1.322</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
|
|||
|
|
@ -219,6 +219,14 @@
|
|||
<property>/it-autoflight/output/lat</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>5</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
|
|
@ -236,7 +244,9 @@
|
|||
</and>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/heading-bug-error-deg</property>
|
||||
<scale>6.3</scale>
|
||||
<scale>
|
||||
<property>/it-autoflight/config/cmd/roll-scale</property>
|
||||
</scale>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
|
|
@ -252,7 +262,9 @@
|
|||
</and>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/true-heading-error-deg</property>
|
||||
<scale>6.3</scale>
|
||||
<scale>
|
||||
<property>/it-autoflight/config/cmd/roll-scale</property>
|
||||
</scale>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
|
|
@ -262,7 +274,24 @@
|
|||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/lnav-hdg-error-deg</property>
|
||||
<scale>6.3</scale>
|
||||
<scale>
|
||||
<property>/it-autoflight/config/cmd/roll-scale</property>
|
||||
</scale>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>5</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
<value>0</value>
|
||||
</input>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-roll-deg</property>
|
||||
|
|
@ -307,67 +336,6 @@
|
|||
</u_max>
|
||||
</filter>
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: ROLL</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/orientation/roll-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/internal/target-roll-deg</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/aileron-cmd</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/roll/kp</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>
|
||||
<property>/it-autoflight/config/roll/ti</property>
|
||||
</Ti>
|
||||
<Td>
|
||||
<property>/it-autoflight/config/roll/td</property>
|
||||
</Td>
|
||||
<u_min>
|
||||
<property>/it-autoflight/config/roll/umin</property>
|
||||
</u_min>
|
||||
<u_max>
|
||||
<property>/it-autoflight/config/roll/umax</property>
|
||||
</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
|
||||
<pid-controller>
|
||||
<name>VORLOC TRK</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -389,38 +357,34 @@
|
|||
<property>/it-autoflight/internal/target-roll-deg</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>-5.0</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>1.0</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>10.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>-30.0</u_min>
|
||||
<u_max>30.0</u_max>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/cmd/vorloc</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>10.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>-30</u_min>
|
||||
<u_max>30</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: VORLOC</name>
|
||||
<name>IT-CONTROLLER: ROLL</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>2</value>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
|
|
@ -434,17 +398,41 @@
|
|||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/vorloc/kp</property>
|
||||
<condition>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>2</value>
|
||||
</not-equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/config/roll/kp</property>
|
||||
</Kp>
|
||||
<Kp>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>2</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/config/roll/kp-vloc</property>
|
||||
</Kp>
|
||||
<Kp>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/config/autoland/kp-roll</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>
|
||||
<property>/it-autoflight/config/vorloc/ti</property>
|
||||
</Ti>
|
||||
<property>/it-autoflight/config/roll/ti</property>
|
||||
</Ti>
|
||||
<Td>
|
||||
<property>/it-autoflight/config/vorloc/td</property>
|
||||
</Td>
|
||||
<property>/it-autoflight/config/roll/td</property>
|
||||
</Td>
|
||||
<u_min>
|
||||
<property>/it-autoflight/config/roll/umin</property>
|
||||
</u_min>
|
||||
|
|
@ -453,9 +441,9 @@
|
|||
</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: ROLL FILTER</name>
|
||||
<name>IT-CONTROLLER: ROLL CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
|
|
@ -478,7 +466,7 @@
|
|||
</input>
|
||||
<output>/controls/flight/aileron</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>0.8</max-rate-of-change>
|
||||
<max-rate-of-change>0.9</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
|
|
@ -506,7 +494,9 @@
|
|||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.025</Kp>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/cmd/alt</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.5</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
|
|
@ -543,7 +533,9 @@
|
|||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.07</Kp>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/cmd/vs</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
|
|
@ -570,11 +562,11 @@
|
|||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/it-autoflight/internal/vert-speed-fpm</prop>
|
||||
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
||||
<scale>0.2</scale>
|
||||
</input>
|
||||
<reference>
|
||||
<prop>/it-autoflight/autoland/target-vs</prop>
|
||||
<property>/it-autoflight/autoland/target-vs</property>
|
||||
<scale>0.2</scale>
|
||||
</reference>
|
||||
<output>
|
||||
|
|
@ -621,14 +613,14 @@
|
|||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/gs/kp</property>
|
||||
<property>/it-autoflight/config/cmd/gs</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.5</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>10.0</Ti>
|
||||
<Td>0.0001</Td>
|
||||
<u_min>-10</u_min>
|
||||
<u_min>-5</u_min>
|
||||
<u_max>7</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
|
@ -638,10 +630,16 @@
|
|||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>7</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
|
|
@ -686,11 +684,12 @@
|
|||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>-0.30</Kp>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/cmd/flch</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
|
||||
<Ti>10.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>
|
||||
|
|
@ -709,7 +708,7 @@
|
|||
<property>/instrumentation/altimeter/indicated-altitude-ft</property>
|
||||
</less-than>
|
||||
</condition>
|
||||
<value>-15.0</value>
|
||||
<value>-7.0</value>
|
||||
</u_min>
|
||||
<u_max>
|
||||
<condition>
|
||||
|
|
@ -732,103 +731,44 @@
|
|||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: FLCH</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/orientation/pitch-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/elevator-cmd</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/flch/kp</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>
|
||||
<property>/it-autoflight/config/flch/ti</property>
|
||||
</Ti>
|
||||
<Td>
|
||||
<property>/it-autoflight/config/flch/td</property>
|
||||
</Td>
|
||||
<u_min>
|
||||
<property>/it-autoflight/config/flch/umin</property>
|
||||
</u_min>
|
||||
<u_max>
|
||||
<property>/it-autoflight/config/flch/umax</property>
|
||||
</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: PITCH</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>2</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>6</value>
|
||||
</equals>
|
||||
</or>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/orientation/pitch-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<condition>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>7</value>
|
||||
</not-equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</reference>
|
||||
<reference>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>7</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/settings/toga-pitch</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/elevator-cmd</property>
|
||||
</output>
|
||||
|
|
@ -855,7 +795,7 @@
|
|||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: PITCH FILTER</name>
|
||||
<name>IT-CONTROLLER: PITCH CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
|
|
@ -878,9 +818,236 @@
|
|||
</input>
|
||||
<output>/controls/flight/elevator</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>0.15</max-rate-of-change>
|
||||
<max-rate-of-change>0.3</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Rudder Control -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<pi-simple-controller>
|
||||
<name>RUDDER VORLOC TRK</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/nav1-heading-error-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0</value>
|
||||
</reference>
|
||||
<output>/it-autoflight/internal/rudder-cmd</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/autoland/kp-rudder</property>
|
||||
</Kp>
|
||||
<Ki>0</Ki>
|
||||
</config>
|
||||
<min>-0.25</min>
|
||||
<max>0.25</max>
|
||||
</pi-simple-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: RUDDER CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<enable>
|
||||
<condition>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</not-equals>
|
||||
</condition>
|
||||
<value>0</value>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/rudder-cmd</property>
|
||||
</input>
|
||||
<output>/controls/flight/rudder</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>0.20</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Control Wheel Steering -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: CWS ROLL</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/internal/cwsr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/orientation/roll-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/internal/cws-roll-deg</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/cws-ail-cmd</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/roll/kp</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>
|
||||
<property>/it-autoflight/config/roll/ti</property>
|
||||
</Ti>
|
||||
<Td>
|
||||
<property>/it-autoflight/config/roll/td</property>
|
||||
</Td>
|
||||
<u_min>-1.0</u_min>
|
||||
<u_max>1.0</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: CWS ROLL CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<enable>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/internal/cwsr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/cws-ail-cmd</property>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/internal/cwsr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0</value>
|
||||
</input>
|
||||
<output>/controls/flight/aileron-trim</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>0.9</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: CWS PITCH</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/internal/cwsp</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/orientation/pitch-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/internal/cws-pitch-deg</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/cws-elv-cmd</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<property>/it-autoflight/config/pitch/kp-cws</property>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>
|
||||
<property>/it-autoflight/config/pitch/ti</property>
|
||||
</Ti>
|
||||
<Td>
|
||||
<property>/it-autoflight/config/pitch/td</property>
|
||||
</Td>
|
||||
<u_min>-1.0</u_min>
|
||||
<u_max>1.0</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: CWS PITCH CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<enable>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/cws</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/cws-elv-cmd</property>
|
||||
</input>
|
||||
<output>/controls/flight/elevator-trim</output>
|
||||
<type>noise-spike</type>
|
||||
<max-rate-of-change>0.5</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Autotrim -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<pid-controller>
|
||||
<name>AP PITCH HELPER PLUS</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -970,7 +1137,7 @@
|
|||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: PITCH TRIM FILTER</name>
|
||||
<name>IT-CONTROLLER: PITCH TRIM CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
|
|
@ -1008,48 +1175,6 @@
|
|||
<max-rate-of-change>0.01</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Rudder Control -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<pid-controller>
|
||||
<name>IT-CONTROLLER: RUDDER ZERO</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<condition>
|
||||
<or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap1</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/ap2</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
</or>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<value>/controls/flight/rudder</value>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/controls/flight/rudder</property>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>5</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>10</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>-0.1</u_min>
|
||||
<u_max>0.1</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Flight Director -->
|
||||
<!-- =============================================================== -->
|
||||
|
|
@ -1077,6 +1202,12 @@
|
|||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>
|
||||
<condition>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>7</value>
|
||||
</not-equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<dif>
|
||||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
|
|
@ -1084,6 +1215,20 @@
|
|||
</dif>
|
||||
</expression>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>7</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<dif>
|
||||
<property>/it-autoflight/settings/toga-pitch</property>
|
||||
<property>/orientation/pitch-deg</property>
|
||||
</dif>
|
||||
</expression>
|
||||
</input>
|
||||
<output>/it-autoflight/fd/pitch-bar</output>
|
||||
</filter>
|
||||
|
||||
|
|
|
|||
|
|
@ -231,7 +231,7 @@
|
|||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: THRUST FILTER</name>
|
||||
<name>IT-CONTROLLER: THRUST CMD</name>
|
||||
<debug>false</debug>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
|
|
@ -285,7 +285,7 @@
|
|||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
<value>0.20</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
|
|
|
|||
Reference in a new issue