fly/IDG-A32X
Archived
1
0
Fork 0
Code Issues Pull requests Projects Releases Wiki Activity

Merge branch 'dev' of https://github.com/it0uchpods/IDG-A32X into dev

Browse source
This commit is contained in:
merspieler 2018-10-21 17:16:33 +02:00
commit 6a3d4fbeb6
6 changed files with 350 additions and 544 deletions

195
Systems/a320-fcs.xml
View file

@ -82,7 +82,7 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/roll/gain-switch</independentVar> <independentVar lookup="column">fbw/roll/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -26.2 0.0 0.2 -26.2 0.0
0.9 -15.5 0.0 0.9 -15.5 0.0
</tableData> </tableData>
@ -96,7 +96,7 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/roll/gain-switch</independentVar> <independentVar lookup="column">fbw/roll/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -45.5 0.0 0.2 -45.5 0.0
0.9 -36.0 0.0 0.9 -36.0 0.0
</tableData> </tableData>
@ -110,7 +110,7 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/roll/gain-switch</independentVar> <independentVar lookup="column">fbw/roll/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -2.1 0.0 0.2 -2.1 0.0
0.9 -1.1 0.0 0.9 -1.1 0.0
</tableData> </tableData>
@ -124,9 +124,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar> <independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 28 0 0.2 28 0
0.9 23 0 0.9 23 0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -138,9 +138,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar> <independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 61 0 0.2 61 0
0.9 45 0 0.9 45 0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -152,9 +152,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar> <independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 2.9 0.0 0.2 2.9 0.0
0.9 1.3 0.0 0.9 1.3 0.0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -166,7 +166,7 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar> <independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -7.5 0.0 0.2 -7.5 0.0
0.9 -1.5 0.0 0.9 -1.5 0.0
</tableData> </tableData>
@ -180,9 +180,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar> <independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 5.01 0.00 0.2 5.01 0.00
0.9 1.05 0.00 0.9 1.05 0.00
</tableData> </tableData>
</table> </table>
</function> </function>
@ -194,9 +194,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar> <independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 1.03 0.00 0.2 1.03 0.00
0.9 0.79 0.00 0.9 0.79 0.00
</tableData> </tableData>
</table> </table>
</function> </function>
@ -279,11 +279,11 @@
<independentVar lookup="row">attitude/roll-rad</independentVar> <independentVar lookup="row">attitude/roll-rad</independentVar>
<independentVar lookup="column">fbw/roll/a-i</independentVar> <independentVar lookup="column">fbw/roll/a-i</independentVar>
<tableData> <tableData>
-1 0 1 -1 0 1
-0.575959 0.261799 0.000000 0.000000 -0.575959 0.261799 0.000000 0.000000
-0.575958 0.000000 0.000000 0.000000 -0.575958 0.000000 0.000000 0.000000
0.575958 0.000000 0.000000 0.000000 0.575958 0.000000 0.000000 0.000000
0.575959 0.000000 0.000000 -0.261799 0.575959 0.000000 0.000000 -0.261799
</tableData> </tableData>
</table> </table>
<table> <table>
@ -310,11 +310,11 @@
<independentVar lookup="row">attitude/roll-rad</independentVar> <independentVar lookup="row">attitude/roll-rad</independentVar>
<independentVar lookup="column">fbw/roll/a-i</independentVar> <independentVar lookup="column">fbw/roll/a-i</independentVar>
<tableData> <tableData>
-1 0 1 -1 0 1
-1.169370 0.261799 0.000000 0.000000 -1.169370 0.261799 0.000000 0.000000
-1.169369 0.000000 0.000000 0.000000 -1.169369 0.000000 0.000000 0.000000
1.169369 0.000000 0.000000 0.000000 1.169369 0.000000 0.000000 0.000000
1.169370 0.000000 0.000000 -0.261799 1.169370 0.000000 0.000000 -0.261799
</tableData> </tableData>
</table> </table>
<table> <table>
@ -369,11 +369,11 @@
<independentVar lookup="row">attitude/roll-rad</independentVar> <independentVar lookup="row">attitude/roll-rad</independentVar>
<independentVar lookup="column">fbw/roll/a-i</independentVar> <independentVar lookup="column">fbw/roll/a-i</independentVar>
<tableData> <tableData>
-1 0 1 -1 0 1
-0.698132 0.261799 0.000000 0.000000 -0.698132 0.261799 0.000000 0.000000
-0.698131 0.000000 0.000000 0.000000 -0.698131 0.000000 0.000000 0.000000
0.698131 0.000000 0.000000 0.000000 0.698131 0.000000 0.000000 0.000000
0.698132 0.000000 0.000000 -0.261799 0.698132 0.000000 0.000000 -0.261799
</tableData> </tableData>
</table> </table>
</sum> </sum>
@ -523,9 +523,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">position/wow</independentVar> <independentVar lookup="column">position/wow</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 0.5 1.0 0.2 0.5 1.0
0.9 0.1 1.0 0.9 0.1 1.0
</tableData> </tableData>
</table> </table>
</product> </product>
@ -615,8 +615,8 @@
<table> <table>
<independentVar lookup="row">/position/gear-agl-ft</independentVar> <independentVar lookup="row">/position/gear-agl-ft</independentVar>
<tableData> <tableData>
5 0.2 5 0.2
30 0.1 30 0.1
</tableData> </tableData>
</table> </table>
</sum> </sum>
@ -779,11 +779,11 @@
<independentVar lookup="row">attitude/pitch-rad</independentVar> <independentVar lookup="row">attitude/pitch-rad</independentVar>
<independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar> <independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar>
<tableData> <tableData>
-1 0 1 -1 0 1
-0.261799 0.000000 0.000000 0.087266 -0.261799 0.000000 0.000000 0.087266
-0.261798 0.000000 0.000000 0.000000 -0.261798 0.000000 0.000000 0.000000
0.523598 0.000000 0.000000 0.000000 0.523598 0.000000 0.000000 0.000000
0.523599 -0.087266 0.000000 0.000000 0.523599 -0.087266 0.000000 0.000000
</tableData> </tableData>
</table> </table>
<table> <table>
@ -818,9 +818,9 @@
<independentVar lookup="row">attitude/pitch-rad</independentVar> <independentVar lookup="row">attitude/pitch-rad</independentVar>
<independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar> <independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar>
<tableData> <tableData>
-1 0 -1 0
0.523598 -0.026180 0.000000 0.523598 -0.026180 0.000000
0.523599 -0.087266 0.000000 0.523599 -0.087266 0.000000
</tableData> </tableData>
</table> </table>
<table> <table>
@ -1066,7 +1066,7 @@
<independentVar lookup="row">/controls/flight/rudder</independentVar> <independentVar lookup="row">/controls/flight/rudder</independentVar>
<independentVar lookup="column">fbw/fmgc/enabled</independentVar> <independentVar lookup="column">fbw/fmgc/enabled</independentVar>
<tableData> <tableData>
0 1 0 1
-1.00 -1 0 -1.00 -1 0
-0.04 0 0 -0.04 0 0
0.04 0 0 0.04 0 0
@ -1192,8 +1192,8 @@
<table> <table>
<independentVar lookup="row">/velocities/airspeed-kt</independentVar> <independentVar lookup="row">/velocities/airspeed-kt</independentVar>
<tableData> <tableData>
62 1.0 62 1.0
116 0.0 116 0.0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -1204,8 +1204,8 @@
<table> <table>
<independentVar lookup="row">/velocities/airspeed-kt</independentVar> <independentVar lookup="row">/velocities/airspeed-kt</independentVar>
<tableData> <tableData>
72 1.0 72 1.0
121 0.0 121 0.0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -1222,8 +1222,8 @@
<table> <table>
<independentVar lookup="row">spoilers/anti-droop-cmd</independentVar> <independentVar lookup="row">spoilers/anti-droop-cmd</independentVar>
<tableData> <tableData>
0.5 0.0 0.5 0.0
1.0 1.0 1.0 1.0
</tableData> </tableData>
</table> </table>
</function> </function>
@ -1521,9 +1521,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData> <tableData>
0 43000 0 43000
0.0 1.00 0.850 0.0 1.00 0.850
0.9 0.02 0.750 0.9 0.02 0.750
</tableData> </tableData>
</table> </table>
</scheduled_gain> </scheduled_gain>
@ -1534,9 +1534,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData> <tableData>
0 43000 0 43000
0.0 1.00 0.850 0.0 1.00 0.850
0.9 0.02 0.750 0.9 0.02 0.750
</tableData> </tableData>
</table> </table>
</scheduled_gain> </scheduled_gain>
@ -1547,9 +1547,9 @@
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData> <tableData>
0 43000 0 43000
0.0 1.00 0.850 0.0 1.00 0.850
0.9 0.02 0.750 0.9 0.02 0.750
</tableData> </tableData>
</table> </table>
</scheduled_gain> </scheduled_gain>
@ -1563,34 +1563,34 @@
<table> <table>
<independentVar lookup="row">/velocities/airspeed-kt</independentVar> <independentVar lookup="row">/velocities/airspeed-kt</independentVar>
<tableData> <tableData>
160.00 25.000 160.00 25.000
162.15 23.649 162.15 23.649
165.02 22.226 165.02 22.226
168.64 21.015 168.64 21.015
172.25 19.734 172.25 19.734
176.59 18.595 176.59 18.595
181.67 17.525 181.67 17.525
186.75 16.385 186.75 16.385
191.83 15.316 191.83 15.316
197.65 14.318 197.65 14.318
205.65 13.247 205.65 13.247
212.93 12.318 212.93 12.318
219.48 11.462 219.48 11.462
227.48 10.533 227.48 10.533
236.96 9.7450 236.96 9.7450
246.43 8.8863 246.43 8.8863
255.18 8.0990 255.18 8.0990
266.12 7.4525 266.12 7.4525
277.06 6.7704 277.06 6.7704
288.00 6.0884 288.00 6.0884
299.67 5.5124 299.67 5.5124
311.35 5.0075 311.35 5.0075
323.03 4.5736 323.03 4.5736
335.44 4.2104 335.44 4.2104
347.13 3.9186 347.13 3.9186
358.81 3.6979 358.81 3.6979
370.50 3.5482 370.50 3.5482
380.00 3.4000 380.00 3.4000
</tableData> </tableData>
</table> </table>
</function> </function>
@ -1737,7 +1737,8 @@
</channel> </channel>
<channel name="Flaps"> <channel name="SFCC">
<switch name="fcs/sfcc/unit1-avail"> <switch name="fcs/sfcc/unit1-avail">
<default value="0"/> <default value="0"/>
<test logic="OR" value="1"> <test logic="OR" value="1">
@ -1751,6 +1752,10 @@
/systems/electrical/bus/dc2 ge 25 /systems/electrical/bus/dc2 ge 25
</test> </test>
</switch> </switch>
</channel>
<channel name="Flaps">
<pure_gain name="fcs/flap-pos-gain"> <pure_gain name="fcs/flap-pos-gain">
<input>/controls/flight/flaps</input> <input>/controls/flight/flaps</input>
@ -1900,9 +1905,9 @@
<independentVar lookup="row">/velocities/groundspeed-kt</independentVar> <independentVar lookup="row">/velocities/groundspeed-kt</independentVar>
<independentVar lookup="column">hydraulics/tiller/switch</independentVar> <independentVar lookup="column">hydraulics/tiller/switch</independentVar>
<tableData> <tableData>
-1 0 1 -1 0 1
30.000 -70.0 0 70.0 30.000 -70.0 0 70.0
30.001 -10.0 0 10.0 30.001 -10.0 0 10.0
</tableData> </tableData>
</table> </table>
</function> </function>

264
Systems/fmgc-drivers.xml
View file

@ -9,11 +9,9 @@
<!-- IT-AUTOFLIGHT --> <!-- IT-AUTOFLIGHT -->
<PropertyList> <PropertyList>
<!-- =============================================================== --> <!-- Predictors -->
<!-- Predictors -->
<!-- =============================================================== -->
<predict-simple> <predict-simple>
<name>IAS 5 SECOND PREDICTOR</name> <name>IAS 5 SECOND PREDICTOR</name>
<debug>false</debug> <debug>false</debug>
@ -22,7 +20,7 @@
<seconds>5.0</seconds> <seconds>5.0</seconds>
<filter-gain>0.0</filter-gain> <filter-gain>0.0</filter-gain>
</predict-simple> </predict-simple>
<predict-simple> <predict-simple>
<name>IAS 10 SECOND PREDICTOR</name> <name>IAS 10 SECOND PREDICTOR</name>
<debug>false</debug> <debug>false</debug>
@ -49,7 +47,7 @@
<seconds>5.0</seconds> <seconds>5.0</seconds>
<filter-gain>0.0</filter-gain> <filter-gain>0.0</filter-gain>
</predict-simple> </predict-simple>
<predict-simple> <predict-simple>
<name>MACH 10 SECOND PREDICTOR</name> <name>MACH 10 SECOND PREDICTOR</name>
<debug>false</debug> <debug>false</debug>
@ -67,16 +65,13 @@
<seconds>15.0</seconds> <seconds>15.0</seconds>
<filter-gain>0.0</filter-gain> <filter-gain>0.0</filter-gain>
</predict-simple> </predict-simple>
<!-- =============================================================== --> <!-- Autopilot Helpers/Calculators -->
<!-- Autopilot Helpers/Calculators -->
<!-- =============================================================== -->
<filter> <filter>
<name>AUTOLAND FD FPM</name> <name>AUTOLAND FD FPM</name>
<type>gain</type> <type>gain</type>
<gain>1.0</gain> <gain>1.0</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input> <input>
<expression> <expression>
<table> <table>
@ -89,12 +84,11 @@
</input> </input>
<output>/it-autoflight/internal/target-fpm-c2</output> <output>/it-autoflight/internal/target-fpm-c2</output>
</filter> </filter>
<filter> <filter>
<name>AUTOLAND FPM</name> <name>AUTOLAND FPM</name>
<type>gain</type> <type>gain</type>
<gain>1.0</gain> <gain>1.0</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input> <input>
<expression> <expression>
<table> <table>
@ -111,12 +105,11 @@
</input> </input>
<output>/it-autoflight/internal/target-fpm-c</output> <output>/it-autoflight/internal/target-fpm-c</output>
</filter> </filter>
<filter> <filter>
<name>FMGC MNG SPD</name> <name>FMGC MNG SPD</name>
<type>gain</type> <type>gain</type>
<gain>1.0</gain> <gain>1.0</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input> <input>
<expression> <expression>
<product> <product>
@ -138,7 +131,6 @@
<name>FMGC MNG MACH</name> <name>FMGC MNG MACH</name>
<type>gain</type> <type>gain</type>
<gain>1.0</gain> <gain>1.0</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input> <input>
<expression> <expression>
<product> <product>
@ -164,7 +156,6 @@
<name>FMGC Target IAS PFD</name> <name>FMGC Target IAS PFD</name>
<type>gain</type> <type>gain</type>
<gain>1.0</gain> <gain>1.0</gain>
<update-interval-secs type="double">0.1</update-interval-secs>
<input> <input>
<condition> <condition>
<equals> <equals>
@ -193,10 +184,11 @@
</input> </input>
<output>/FMGC/internal/target-ias-pfd</output> <output>/FMGC/internal/target-ias-pfd</output>
</filter> </filter>
<filter> <filter>
<name>KTS INPUT FILTER</name> <name>KTS INPUT FILTER</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>
@ -218,32 +210,6 @@
<property>/it-autoflight/settings/togaspd</property> <property>/it-autoflight/settings/togaspd</property>
</input> </input>
<output>/it-autoflight/internal/flch-kts</output> <output>/it-autoflight/internal/flch-kts</output>
<type>noise-spike</type>
<max-rate-of-change>
<condition>
<or>
<and>
<not-equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</not-equals>
</and>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>100</value>
</max-rate-of-change>
<max-rate-of-change> <max-rate-of-change>
<condition> <condition>
<and> <and>
@ -257,6 +223,10 @@
<value>7</value> <value>7</value>
</equals> </equals>
</or> </or>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>0</value>
</equals>
<equals> <equals>
<property>/gear/gear[1]/wow</property> <property>/gear/gear[1]/wow</property>
<value>0</value> <value>0</value>
@ -269,43 +239,33 @@
</condition> </condition>
<value>5</value> <value>5</value>
</max-rate-of-change> </max-rate-of-change>
<max-rate-of-change>100</max-rate-of-change>
</filter> </filter>
<filter> <filter>
<name>MACH INPUT FILTER</name> <name>MACH INPUT FILTER</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>/it-autoflight/input/spd-mach</input>
<property>/it-autoflight/input/spd-mach</property>
</input>
<output>/it-autoflight/internal/flch-mach</output> <output>/it-autoflight/internal/flch-mach</output>
<type>noise-spike</type>
<max-rate-of-change>
<condition>
<or>
<not-equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</not-equals>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>1</value>
</max-rate-of-change>
<max-rate-of-change> <max-rate-of-change>
<condition> <condition>
<and> <and>
<or>
<equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</equals>
</or>
<equals> <equals>
<property>/it-autoflight/output/vert</property> <property>/it-autoflight/input/kts-mach</property>
<value>4</value> <value>1</value>
</equals> </equals>
<equals> <equals>
<property>/gear/gear[1]/wow</property> <property>/gear/gear[1]/wow</property>
@ -319,8 +279,9 @@
</condition> </condition>
<value>0.05</value> <value>0.05</value>
</max-rate-of-change> </max-rate-of-change>
<max-rate-of-change>1</max-rate-of-change>
</filter> </filter>
<filter> <filter>
<name>IAS SYNC</name> <name>IAS SYNC</name>
<type>gain</type> <type>gain</type>
@ -333,8 +294,16 @@
</equals> </equals>
</condition> </condition>
</enable> </enable>
<update-interval-secs type="double">0.5</update-interval-secs> <input>
<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input> <expression>
<floor>
<sum>
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
<value>0.5</value>
</sum>
</floor>
</expression>
</input>
<output>/it-autoflight/input/spd-kts</output> <output>/it-autoflight/input/spd-kts</output>
</filter> </filter>
@ -350,8 +319,22 @@
</equals> </equals>
</condition> </condition>
</enable> </enable>
<update-interval-secs type="double">0.5</update-interval-secs> <input>
<input>/instrumentation/airspeed-indicator/indicated-mach</input> <expression>
<div>
<floor>
<sum>
<product>
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
<value>1000</value>
</product>
<value>0.5</value>
</sum>
</floor>
<value>1000</value>
</div>
</expression>
</input>
<output>/it-autoflight/input/spd-mach</output> <output>/it-autoflight/input/spd-mach</output>
</filter> </filter>
@ -365,9 +348,7 @@
</condition> </condition>
<property>/orientation/heading-deg</property> <property>/orientation/heading-deg</property>
</input> </input>
<input> <input>/orientation/heading-magnetic-deg</input>
<property>/orientation/heading-magnetic-deg</property>
</input>
<reference>0</reference> <reference>0</reference>
<output>/it-autoflight/internal/heading-deg</output> <output>/it-autoflight/internal/heading-deg</output>
<output>/instrumentation/pfd/heading-deg</output> <output>/instrumentation/pfd/heading-deg</output>
@ -484,21 +465,7 @@
</sum> </sum>
</expression> </expression>
</input> </input>
<input> <input>0</input>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>0</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</not-equals>
</and>
</condition>
<value>0</value>
</input>
<output>/it-autoflight/internal/heading-error-deg</output> <output>/it-autoflight/internal/heading-error-deg</output>
<period> <period>
<min>-180</min> <min>-180</min>
@ -522,7 +489,10 @@
<input> <input>
<expression> <expression>
<floor> <floor>
<property>/it-autoflight/internal/vert-speed-fpm</property> <sum>
<property>/it-autoflight/internal/vert-speed-fpm</property>
<value>0.5</value>
</sum>
</floor> </floor>
</expression> </expression>
</input> </input>
@ -532,31 +502,18 @@
<filter> <filter>
<name>VERT SPEED FILTER</name> <name>VERT SPEED FILTER</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>/it-autoflight/input/vs</input>
<property>/it-autoflight/input/vs</property>
</input>
<output>/it-autoflight/internal/vs</output> <output>/it-autoflight/internal/vs</output>
<type>noise-spike</type>
<max-rate-of-change>
<condition>
<or>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>2000</value>
</max-rate-of-change>
<max-rate-of-change> <max-rate-of-change>
<condition> <condition>
<and> <and>
<equals>
<property>/it-autoflight/output/vert</property>
<value>1</value>
</equals>
<equals> <equals>
<property>/gear/gear[1]/wow</property> <property>/gear/gear[1]/wow</property>
<value>0</value> <value>0</value>
@ -569,8 +526,9 @@
</condition> </condition>
<value>300</value> <value>300</value>
</max-rate-of-change> </max-rate-of-change>
<max-rate-of-change>2000</max-rate-of-change>
</filter> </filter>
<filter> <filter>
<name>NAV ERROR DEG</name> <name>NAV ERROR DEG</name>
<debug>false</debug> <debug>false</debug>
@ -589,7 +547,7 @@
<max>180</max> <max>180</max>
</period> </period>
</filter> </filter>
<filter> <filter>
<name>INTERNAL VERTICAL SPEED COMPUTER</name> <name>INTERNAL VERTICAL SPEED COMPUTER</name>
<debug>false</debug> <debug>false</debug>
@ -830,49 +788,13 @@
</input> </input>
<output>/it-autoflight/internal/fpa</output> <output>/it-autoflight/internal/fpa</output>
</filter> </filter>
<!-- =============================================================== --> <!-- Flight Director -->
<!-- Flight Director -->
<!-- =============================================================== -->
<filter> <filter>
<name>IT-CONTROLLER: TARGET ROLL CMD</name> <name>IT-CONTROLLER: TARGET ROLL CMD</name>
<debug>false</debug> <debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<input>
<property>/it-autoflight/internal/target-roll-deg</property>
</input>
<output>/it-autoflight/internal/target-roll-fd</output>
<type>noise-spike</type> <type>noise-spike</type>
<max-rate-of-change>15</max-rate-of-change>
</filter>
<filter>
<name>FD: ROLL</name>
<debug>false</debug>
<type>gain</type>
<gain>1.0</gain>
<input>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>5</value>
</not-equals>
</and>
</condition>
<expression>
<dif>
<property>/it-autoflight/internal/target-roll-fd</property>
<property>/orientation/roll-deg</property>
</dif>
</expression>
</input>
<input> <input>
<condition> <condition>
<or> <or>
@ -886,9 +808,37 @@
</equals> </equals>
</or> </or>
</condition> </condition>
<value>0</value>
</input>
<input>/it-autoflight/internal/target-roll-deg</input>
<output>/it-autoflight/internal/target-roll-fd</output>
<max-rate-of-change>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</not-equals>
</and>
</condition>
<value>50</value>
</max-rate-of-change>
<max-rate-of-change>15</max-rate-of-change>
</filter>
<filter>
<name>FD: ROLL</name>
<debug>false</debug>
<type>gain</type>
<gain>1.0</gain>
<input>
<expression> <expression>
<dif> <dif>
<value>0</value> <property>/it-autoflight/internal/target-roll-fd</property>
<property>/orientation/roll-deg</property> <property>/orientation/roll-deg</property>
</dif> </dif>
</expression> </expression>
@ -897,7 +847,7 @@
<min>-30</min> <min>-30</min>
<max>30</max> <max>30</max>
</filter> </filter>
<filter> <filter>
<name>FD: PITCH</name> <name>FD: PITCH</name>
<debug>false</debug> <debug>false</debug>

78
Systems/fmgc-pitch.xml
View file

@ -9,10 +9,8 @@
<!-- IT-AUTOFLIGHT --> <!-- IT-AUTOFLIGHT -->
<PropertyList> <PropertyList>
<!-- =============================================================== --> <!-- Pitch Axis -->
<!-- Vertical Modes -->
<!-- =============================================================== -->
<filter> <filter>
<name>ALTITUDE CAPTURE/HOLD</name> <name>ALTITUDE CAPTURE/HOLD</name>
@ -29,33 +27,19 @@
</input> </input>
<reference> <reference>
<condition> <condition>
<not-equals> <equals>
<property>/it-autoflight/output/vert</property> <property>/it-autoflight/output/vert</property>
<value>8</value> <value>8</value>
</not-equals> </equals>
</condition> </condition>
<property>/it-autoflight/internal/alt</property>
</reference>
<reference>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>8</value>
</equals>
</condition>
<property>/it-autoflight/internal/mng-alt</property> <property>/it-autoflight/internal/mng-alt</property>
</reference> </reference>
<output> <reference>/it-autoflight/internal/alt</reference>
<property>/it-autoflight/internal/target-fpm</property> <output>/it-autoflight/internal/target-fpm</output>
</output> <min>/it-autoflight/internal/min-vs</min>
<min> <max>/it-autoflight/internal/max-vs</max>
<property>/it-autoflight/internal/min-vs</property>
</min>
<max>
<property>/it-autoflight/internal/max-vs</property>
</max>
</filter> </filter>
<pid-controller> <pid-controller>
<name>FPA HOLD</name> <name>FPA HOLD</name>
<debug>false</debug> <debug>false</debug>
@ -87,15 +71,9 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>/it-autoflight/internal/fpa</input>
<property>/it-autoflight/internal/fpa</property> <reference>/it-autoflight/input/fpa</reference>
</input> <output>/it-autoflight/internal/target-fpm-d</output>
<reference>
<property>/it-autoflight/input/fpa</property>
</reference>
<output>
<property>/it-autoflight/internal/target-fpm-d</property>
</output>
<config> <config>
<Kp> <Kp>
<expression> <expression>
@ -106,9 +84,6 @@
</table> </table>
</expression> </expression>
</Kp> </Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>2.0</Ti> <Ti>2.0</Ti>
<Td>0.002</Td> <Td>0.002</Td>
<u_min> <u_min>
@ -215,9 +190,7 @@
<property>/it-autoflight/internal/flch-mach</property> <property>/it-autoflight/internal/flch-mach</property>
<scale>1000.0</scale> <scale>1000.0</scale>
</reference> </reference>
<output> <output>/it-autoflight/internal/target-fpm-b</output>
<property>/it-autoflight/internal/target-fpm-b</property>
</output>
<config> <config>
<Kp> <Kp>
<condition> <condition>
@ -237,9 +210,6 @@
</condition> </condition>
<value>-60</value> <value>-60</value>
</Kp> </Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>2.5</Ti> <Ti>2.5</Ti>
<Td>0.001</Td> <Td>0.001</Td>
<u_min> <u_min>
@ -505,9 +475,7 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>/it-autoflight/internal/vert-speed-fpm</input>
<property>/it-autoflight/internal/vert-speed-fpm</property>
</input>
<reference> <reference>
<condition> <condition>
<or> <or>
@ -590,9 +558,7 @@
</condition> </condition>
<property>/it-autoflight/internal/nav1-rate-of-climb-fpm</property> <property>/it-autoflight/internal/nav1-rate-of-climb-fpm</property>
</reference> </reference>
<output> <output>/it-autoflight/internal/target-pitch-deg</output>
<property>/it-autoflight/internal/target-pitch-deg</property>
</output>
<config> <config>
<Kp> <Kp>
<condition> <condition>
@ -711,21 +677,15 @@
<min>-15</min> <min>-15</min>
<max>30</max> <max>30</max>
</filter> </filter>
<filter> <filter>
<name>System Command: Pitch Rate</name> <name>System Command: Pitch Rate</name>
<debug>false</debug> <debug>false</debug>
<type>gain</type> <type>gain</type>
<gain>0.15</gain> <gain>0.15</gain>
<input> <input>/orientation/pitch-deg</input>
<property>/orientation/pitch-deg</property> <reference>/it-autoflight/internal/target-pitch-deg</reference>
</input> <output>/fdm/jsbsim/fbw/fmgc/pitch-cmd</output> <!-- Inputs to the FBW Pitch -->
<reference>
<property>/it-autoflight/internal/target-pitch-deg</property>
</reference>
<output>
<property>/fdm/jsbsim/fbw/fmgc/pitch-cmd</property> <!-- Inputs to the FBW Pitch Rate -->
</output>
<min>-0.3</min> <min>-0.3</min>
<max>0.3</max> <max>0.3</max>
</filter> </filter>

211
Systems/fmgc-roll-yaw.xml
View file

@ -9,11 +9,9 @@
<!-- IT-AUTOFLIGHT --> <!-- IT-AUTOFLIGHT -->
<PropertyList> <PropertyList>
<!-- =============================================================== --> <!-- Roll Axis -->
<!-- Lateral Modes -->
<!-- =============================================================== -->
<pi-simple-controller> <pi-simple-controller>
<name>ROLL CONTROLLER: HDG/LNAV</name> <name>ROLL CONTROLLER: HDG/LNAV</name>
<debug>false</debug> <debug>false</debug>
@ -51,15 +49,9 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>/it-autoflight/internal/heading-error-deg</input>
<property>/it-autoflight/internal/heading-error-deg</property> <reference>0</reference>
</input> <output>/it-autoflight/internal/target-roll-deg</output>
<reference>
<value>0</value>
</reference>
<output>
<property>/it-autoflight/internal/target-roll-deg</property>
</output>
<config> <config>
<Kp>-1.8</Kp> <Kp>-1.8</Kp>
<Ki>-0.000001</Ki> <Ki>-0.000001</Ki>
@ -67,9 +59,7 @@
<property>/it-autoflight/internal/bank-limit</property> <property>/it-autoflight/internal/bank-limit</property>
<scale>-1</scale> <scale>-1</scale>
</min> </min>
<max> <max>/it-autoflight/internal/bank-limit</max>
<property>/it-autoflight/internal/bank-limit</property>
</max>
</config> </config>
</pi-simple-controller> </pi-simple-controller>
@ -104,30 +94,9 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>/it-autoflight/internal/nav-heading-error-deg</input>
<condition> <reference>0</reference>
<equals> <output>/it-autoflight/internal/target-roll-deg</output>
<property>/it-autoflight/settings/use-backcourse</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/internal/nav-heading-error-deg</property>
</input>
<input>
<condition>
<equals>
<property>/it-autoflight/settings/use-backcourse</property>
<value>1</value>
</equals>
</condition>
<property>/it-autoflight/internal/nav-bc-heading-error-deg</property>
</input>
<reference>
<value>0.0</value>
</reference>
<output>
<property>/it-autoflight/internal/target-roll-deg</property>
</output>
<config> <config>
<Kp>-2.8</Kp> <Kp>-2.8</Kp>
<Ki>-0.0001</Ki> <Ki>-0.0001</Ki>
@ -135,12 +104,10 @@
<property>/it-autoflight/internal/bank-limit</property> <property>/it-autoflight/internal/bank-limit</property>
<scale>-1</scale> <scale>-1</scale>
</min> </min>
<max> <max>/it-autoflight/internal/bank-limit</max>
<property>/it-autoflight/internal/bank-limit</property>
</max>
</config> </config>
</pi-simple-controller> </pi-simple-controller>
<filter> <filter>
<name>ROLL DEG SYNC</name> <name>ROLL DEG SYNC</name>
<debug>false</debug> <debug>false</debug>
@ -174,48 +141,14 @@
<property>/it-autoflight/internal/bank-limit</property> <property>/it-autoflight/internal/bank-limit</property>
<scale>-1</scale> <scale>-1</scale>
</min> </min>
<max> <max>/it-autoflight/internal/bank-limit</max>
<property>/it-autoflight/internal/bank-limit</property>
</max>
</filter> </filter>
<filter> <filter>
<name>IT-CONTROLLER: TARGET ROLL CMD</name> <name>IT-CONTROLLER: TARGET ROLL CMD</name>
<debug>false</debug> <debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<input>
<property>/it-autoflight/internal/target-roll-deg</property>
</input>
<output>/it-autoflight/internal/target-roll</output>
<type>noise-spike</type> <type>noise-spike</type>
<max-rate-of-change>6</max-rate-of-change>
</filter>
<filter>
<name>System Command: Roll Rate</name>
<debug>false</debug>
<type>gain</type>
<gain>-0.1</gain>
<input> <input>
<property>/orientation/roll-deg</property>
</input>
<reference>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>5</value>
</not-equals>
</and>
</condition>
<property>/it-autoflight/internal/target-roll</property>
</reference>
<reference>
<condition> <condition>
<or> <or>
<equals> <equals>
@ -229,17 +162,63 @@
</or> </or>
</condition> </condition>
<value>0</value> <value>0</value>
</reference> </input>
<output> <input>/it-autoflight/internal/target-roll-deg</input>
<property>/fdm/jsbsim/fbw/fmgc/roll-cmd</property> <!-- Inputs to the FBW Roll Rate --> <output>/it-autoflight/internal/target-roll</output>
</output> <max-rate-of-change>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</not-equals>
</and>
</condition>
<value>50</value>
</max-rate-of-change>
<max-rate-of-change>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</not-equals>
</and>
</condition>
<value>15</value>
</max-rate-of-change>
<max-rate-of-change>6</max-rate-of-change>
</filter>
<filter>
<name>System Command: Roll Rate</name>
<debug>false</debug>
<type>gain</type>
<gain>-0.1</gain>
<input>/orientation/roll-deg</input>
<reference>/it-autoflight/internal/target-roll</reference>
<output>/fdm/jsbsim/fbw/fmgc/roll-cmd</output> <!-- Inputs to the FBW Roll -->
<min>-0.32</min> <min>-0.32</min>
<max>0.32</max> <max>0.32</max>
</filter> </filter>
<!-- =============================================================== --> <!-- Yaw Axis -->
<!-- Yaw Control -->
<!-- =============================================================== -->
<pi-simple-controller> <pi-simple-controller>
<name>RUDDER VORLOC TRK</name> <name>RUDDER VORLOC TRK</name>
@ -252,12 +231,8 @@
</equals> </equals>
</condition> </condition>
</enable> </enable>
<input> <input>/it-autoflight/internal/nav-heading-error-deg</input>
<property>/it-autoflight/internal/nav-heading-error-deg</property> <reference>0</reference>
</input>
<reference>
<value>0</value>
</reference>
<output>/it-autoflight/internal/rudder-cmd</output> <output>/it-autoflight/internal/rudder-cmd</output>
<config> <config>
<Kp> <Kp>
@ -275,21 +250,7 @@
</condition> </condition>
<value>-0.05</value> <value>-0.05</value>
</Kp> </Kp>
<Kp> <Kp>-0.02</Kp>
<condition>
<or>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>-0.02</value>
</Kp>
<Ki>0</Ki> <Ki>0</Ki>
</config> </config>
<min>-0.15</min> <min>-0.15</min>
@ -299,28 +260,32 @@
<filter> <filter>
<name>IT-CONTROLLER: RUDDER CMD</name> <name>IT-CONTROLLER: RUDDER CMD</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>
<condition> <condition>
<not-equals> <and>
<property>/it-autoflight/output/lat</property> <or>
<value>4</value> <equals>
</not-equals> <property>/it-autoflight/output/ap1</property>
</condition> <value>1</value>
<value>0</value> </equals>
</input> <equals>
<input> <property>/it-autoflight/output/ap2</property>
<condition> <value>1</value>
<equals> </equals>
<property>/it-autoflight/output/lat</property> </or>
<value>4</value> <equals>
</equals> <property>/it-autoflight/output/lat</property>
<value>4</value>
</equals>
</and>
</condition> </condition>
<property>/it-autoflight/internal/rudder-cmd</property> <property>/it-autoflight/internal/rudder-cmd</property>
</input> </input>
<output>/fdm/jsbsim/fbw/fmgc/yaw-cmd</output> <input>0</input>
<type>noise-spike</type> <output>/fdm/jsbsim/fbw/fmgc/yaw-cmd</output> <!-- Inputs to the FBW Yaw -->
<max-rate-of-change>0.6</max-rate-of-change> <max-rate-of-change>0.6</max-rate-of-change>
</filter> </filter>

144
Systems/fmgc-thrust.xml
View file

@ -7,54 +7,31 @@
--> -->
<PropertyList> <PropertyList>
<!-- =============================================================== --> <!-- Thrust Axis -->
<!-- Thrust Modes -->
<!-- =============================================================== -->
<filter> <filter>
<name>KTS INPUT FILTER</name> <name>KTS INPUT FILTER</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>/it-autoflight/input/spd-kts</input>
<property>/it-autoflight/input/spd-kts</property>
</input>
<output>/it-autoflight/internal/kts</output> <output>/it-autoflight/internal/kts</output>
<type>noise-spike</type>
<max-rate-of-change>
<condition>
<or>
<not-equals>
<property>/it-autoflight/output/thr-mode</property>
<value>0</value>
</not-equals>
<equals>
<property>/it-autoflight/output/athr</property>
<value>0</value>
</equals>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>200</value>
</max-rate-of-change>
<max-rate-of-change> <max-rate-of-change>
<condition> <condition>
<and> <and>
<equals>
<property>/it-autoflight/output/athr</property>
<value>1</value>
</equals>
<equals> <equals>
<property>/it-autoflight/output/thr-mode</property> <property>/it-autoflight/output/thr-mode</property>
<value>0</value> <value>0</value>
</equals> </equals>
<equals> <equals>
<property>/it-autoflight/output/athr</property> <property>/it-autoflight/input/kts-mach</property>
<value>1</value> <value>0</value>
</equals> </equals>
<equals> <equals>
<property>/gear/gear[1]/wow</property> <property>/gear/gear[1]/wow</property>
@ -68,50 +45,30 @@
</condition> </condition>
<value>10</value> <value>10</value>
</max-rate-of-change> </max-rate-of-change>
<max-rate-of-change>200</max-rate-of-change>
</filter> </filter>
<filter> <filter>
<name>MACH INPUT FILTER</name> <name>MACH INPUT FILTER</name>
<debug>false</debug> <debug>false</debug>
<type>noise-spike</type>
<feedback-if-disabled>true</feedback-if-disabled> <feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to> <initialize-to>output</initialize-to>
<input> <input>/it-autoflight/input/spd-mach</input>
<property>/it-autoflight/input/spd-mach</property>
</input>
<output>/it-autoflight/internal/mach</output> <output>/it-autoflight/internal/mach</output>
<type>noise-spike</type>
<max-rate-of-change>
<condition>
<or>
<not-equals>
<property>/it-autoflight/output/thr-mode</property>
<value>0</value>
</not-equals>
<equals>
<property>/it-autoflight/output/athr</property>
<value>0</value>
</equals>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>2</value>
</max-rate-of-change>
<max-rate-of-change> <max-rate-of-change>
<condition> <condition>
<and> <and>
<equals>
<property>/it-autoflight/output/athr</property>
<value>1</value>
</equals>
<equals> <equals>
<property>/it-autoflight/output/thr-mode</property> <property>/it-autoflight/output/thr-mode</property>
<value>0</value> <value>0</value>
</equals> </equals>
<equals> <equals>
<property>/it-autoflight/output/athr</property> <property>/it-autoflight/input/kts-mach</property>
<value>1</value> <value>1</value>
</equals> </equals>
<equals> <equals>
@ -126,6 +83,7 @@
</condition> </condition>
<value>0.1</value> <value>0.1</value>
</max-rate-of-change> </max-rate-of-change>
<max-rate-of-change>2</max-rate-of-change>
</filter> </filter>
<filter> <filter>
@ -250,28 +208,15 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property> <reference>/it-autoflight/internal/kts</reference>
</input> <output>/controls/engines/throttle-cmd-pid</output>
<reference>
<property>/it-autoflight/internal/kts</property>
</reference>
<output>
<property>/controls/engines/throttle-cmd-pid</property>
</output>
<config> <config>
<Kp>0.055</Kp> <Kp>0.055</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>9.0</Ti> <Ti>9.0</Ti>
<Td>0.00001</Td> <Td>0.00001</Td>
<u_min> <u_min>/controls/engines/idle-limit</u_min>
<property>/controls/engines/idle-limit</property> <u_max>/controls/engines/throttle-pid-max</u_max>
</u_min>
<u_max>
<property>/controls/engines/throttle-pid-max</property>
</u_max>
</config> </config>
</pid-controller> </pid-controller>
@ -390,22 +335,13 @@
<property>/it-autoflight/internal/mach</property> <property>/it-autoflight/internal/mach</property>
<scale>1000.0</scale> <scale>1000.0</scale>
</reference> </reference>
<output> <output>/controls/engines/throttle-cmd-pid</output>
<property>/controls/engines/throttle-cmd-pid</property>
</output>
<config> <config>
<Kp>0.055</Kp> <Kp>0.055</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>9.0</Ti> <Ti>9.0</Ti>
<Td>0.00001</Td> <Td>0.00001</Td>
<u_min> <u_min>/controls/engines/idle-limit</u_min>
<property>/controls/engines/idle-limit</property> <u_max>/controls/engines/throttle-pid-max</u_max>
</u_min>
<u_max>
<property>/controls/engines/throttle-pid-max</property>
</u_max>
</config> </config>
</pid-controller> </pid-controller>
@ -512,12 +448,8 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>0.0</input>
<value>0.0</value> <output>/controls/engines/throttle-cmd-pid</output>
</input>
<output>
<property>/controls/engines/throttle-cmd-pid</property>
</output>
</filter> </filter>
<filter> <filter>
@ -623,12 +555,8 @@
</and> </and>
</condition> </condition>
</enable> </enable>
<input> <input>1.0</input>
<value>1.0</value> <output>/controls/engines/throttle-cmd-pid</output>
</input>
<output>
<property>/controls/engines/throttle-cmd-pid</property>
</output>
</filter> </filter>
<filter> <filter>
@ -725,12 +653,10 @@
</not-equals> </not-equals>
</and> </and>
</condition> </condition>
<value>1</value> <value>1.0</value>
</input> </input>
<input>0</input> <input>0.0</input>
<output> <output>/controls/engines/throttle-cmd-pid</output>
<property>/controls/engines/throttle-cmd-pid</property>
</output>
</filter> </filter>
</PropertyList> </PropertyList>

2
revision.txt
View file

@ -1 +1 @@
4679 4681