Merge branch 'dev' of https://github.com/it0uchpods/IDG-A32X into dev
This commit is contained in:
commit
6a3d4fbeb6
6 changed files with 350 additions and 544 deletions
|
|
@ -82,7 +82,7 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0 1
|
||||
0.2 -26.2 0.0
|
||||
0.9 -15.5 0.0
|
||||
</tableData>
|
||||
|
|
@ -96,7 +96,7 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0 1
|
||||
0.2 -45.5 0.0
|
||||
0.9 -36.0 0.0
|
||||
</tableData>
|
||||
|
|
@ -110,7 +110,7 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0 1
|
||||
0.2 -2.1 0.0
|
||||
0.9 -1.1 0.0
|
||||
</tableData>
|
||||
|
|
@ -124,9 +124,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 28 0
|
||||
0.9 23 0
|
||||
0 1
|
||||
0.2 28 0
|
||||
0.9 23 0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -138,9 +138,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 61 0
|
||||
0.9 45 0
|
||||
0 1
|
||||
0.2 61 0
|
||||
0.9 45 0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -152,9 +152,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/pitch/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 2.9 0.0
|
||||
0.9 1.3 0.0
|
||||
0 1
|
||||
0.2 2.9 0.0
|
||||
0.9 1.3 0.0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -166,7 +166,7 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0 1
|
||||
0.2 -7.5 0.0
|
||||
0.9 -1.5 0.0
|
||||
</tableData>
|
||||
|
|
@ -180,9 +180,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 5.01 0.00
|
||||
0.9 1.05 0.00
|
||||
0 1
|
||||
0.2 5.01 0.00
|
||||
0.9 1.05 0.00
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -194,9 +194,9 @@
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|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 1.03 0.00
|
||||
0.9 0.79 0.00
|
||||
0 1
|
||||
0.2 1.03 0.00
|
||||
0.9 0.79 0.00
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
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@ -279,11 +279,11 @@
|
|||
<independentVar lookup="row">attitude/roll-rad</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/a-i</independentVar>
|
||||
<tableData>
|
||||
-1 0 1
|
||||
-0.575959 0.261799 0.000000 0.000000
|
||||
-0.575958 0.000000 0.000000 0.000000
|
||||
0.575958 0.000000 0.000000 0.000000
|
||||
0.575959 0.000000 0.000000 -0.261799
|
||||
-1 0 1
|
||||
-0.575959 0.261799 0.000000 0.000000
|
||||
-0.575958 0.000000 0.000000 0.000000
|
||||
0.575958 0.000000 0.000000 0.000000
|
||||
0.575959 0.000000 0.000000 -0.261799
|
||||
</tableData>
|
||||
</table>
|
||||
<table>
|
||||
|
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@ -310,11 +310,11 @@
|
|||
<independentVar lookup="row">attitude/roll-rad</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/a-i</independentVar>
|
||||
<tableData>
|
||||
-1 0 1
|
||||
-1.169370 0.261799 0.000000 0.000000
|
||||
-1.169369 0.000000 0.000000 0.000000
|
||||
1.169369 0.000000 0.000000 0.000000
|
||||
1.169370 0.000000 0.000000 -0.261799
|
||||
-1 0 1
|
||||
-1.169370 0.261799 0.000000 0.000000
|
||||
-1.169369 0.000000 0.000000 0.000000
|
||||
1.169369 0.000000 0.000000 0.000000
|
||||
1.169370 0.000000 0.000000 -0.261799
|
||||
</tableData>
|
||||
</table>
|
||||
<table>
|
||||
|
|
@ -369,11 +369,11 @@
|
|||
<independentVar lookup="row">attitude/roll-rad</independentVar>
|
||||
<independentVar lookup="column">fbw/roll/a-i</independentVar>
|
||||
<tableData>
|
||||
-1 0 1
|
||||
-0.698132 0.261799 0.000000 0.000000
|
||||
-0.698131 0.000000 0.000000 0.000000
|
||||
0.698131 0.000000 0.000000 0.000000
|
||||
0.698132 0.000000 0.000000 -0.261799
|
||||
-1 0 1
|
||||
-0.698132 0.261799 0.000000 0.000000
|
||||
-0.698131 0.000000 0.000000 0.000000
|
||||
0.698131 0.000000 0.000000 0.000000
|
||||
0.698132 0.000000 0.000000 -0.261799
|
||||
</tableData>
|
||||
</table>
|
||||
</sum>
|
||||
|
|
@ -523,9 +523,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">position/wow</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 0.5 1.0
|
||||
0.9 0.1 1.0
|
||||
0 1
|
||||
0.2 0.5 1.0
|
||||
0.9 0.1 1.0
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
|
|
@ -615,8 +615,8 @@
|
|||
<table>
|
||||
<independentVar lookup="row">/position/gear-agl-ft</independentVar>
|
||||
<tableData>
|
||||
5 0.2
|
||||
30 0.1
|
||||
5 0.2
|
||||
30 0.1
|
||||
</tableData>
|
||||
</table>
|
||||
</sum>
|
||||
|
|
@ -779,11 +779,11 @@
|
|||
<independentVar lookup="row">attitude/pitch-rad</independentVar>
|
||||
<independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar>
|
||||
<tableData>
|
||||
-1 0 1
|
||||
-0.261799 0.000000 0.000000 0.087266
|
||||
-0.261798 0.000000 0.000000 0.000000
|
||||
0.523598 0.000000 0.000000 0.000000
|
||||
0.523599 -0.087266 0.000000 0.000000
|
||||
-1 0 1
|
||||
-0.261799 0.000000 0.000000 0.087266
|
||||
-0.261798 0.000000 0.000000 0.000000
|
||||
0.523598 0.000000 0.000000 0.000000
|
||||
0.523599 -0.087266 0.000000 0.000000
|
||||
</tableData>
|
||||
</table>
|
||||
<table>
|
||||
|
|
@ -818,9 +818,9 @@
|
|||
<independentVar lookup="row">attitude/pitch-rad</independentVar>
|
||||
<independentVar lookup="column">fbw/pitch/g-pi-switched</independentVar>
|
||||
<tableData>
|
||||
-1 0
|
||||
0.523598 -0.026180 0.000000
|
||||
0.523599 -0.087266 0.000000
|
||||
-1 0
|
||||
0.523598 -0.026180 0.000000
|
||||
0.523599 -0.087266 0.000000
|
||||
</tableData>
|
||||
</table>
|
||||
<table>
|
||||
|
|
@ -1066,7 +1066,7 @@
|
|||
<independentVar lookup="row">/controls/flight/rudder</independentVar>
|
||||
<independentVar lookup="column">fbw/fmgc/enabled</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0 1
|
||||
-1.00 -1 0
|
||||
-0.04 0 0
|
||||
0.04 0 0
|
||||
|
|
@ -1192,8 +1192,8 @@
|
|||
<table>
|
||||
<independentVar lookup="row">/velocities/airspeed-kt</independentVar>
|
||||
<tableData>
|
||||
62 1.0
|
||||
116 0.0
|
||||
62 1.0
|
||||
116 0.0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -1204,8 +1204,8 @@
|
|||
<table>
|
||||
<independentVar lookup="row">/velocities/airspeed-kt</independentVar>
|
||||
<tableData>
|
||||
72 1.0
|
||||
121 0.0
|
||||
72 1.0
|
||||
121 0.0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -1222,8 +1222,8 @@
|
|||
<table>
|
||||
<independentVar lookup="row">spoilers/anti-droop-cmd</independentVar>
|
||||
<tableData>
|
||||
0.5 0.0
|
||||
1.0 1.0
|
||||
0.5 0.0
|
||||
1.0 1.0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -1521,9 +1521,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
</tableData>
|
||||
</table>
|
||||
</scheduled_gain>
|
||||
|
|
@ -1534,9 +1534,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
</tableData>
|
||||
</table>
|
||||
</scheduled_gain>
|
||||
|
|
@ -1547,9 +1547,9 @@
|
|||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
0 43000
|
||||
0.0 1.00 0.850
|
||||
0.9 0.02 0.750
|
||||
</tableData>
|
||||
</table>
|
||||
</scheduled_gain>
|
||||
|
|
@ -1563,34 +1563,34 @@
|
|||
<table>
|
||||
<independentVar lookup="row">/velocities/airspeed-kt</independentVar>
|
||||
<tableData>
|
||||
160.00 25.000
|
||||
162.15 23.649
|
||||
165.02 22.226
|
||||
168.64 21.015
|
||||
172.25 19.734
|
||||
176.59 18.595
|
||||
181.67 17.525
|
||||
186.75 16.385
|
||||
191.83 15.316
|
||||
197.65 14.318
|
||||
205.65 13.247
|
||||
212.93 12.318
|
||||
219.48 11.462
|
||||
227.48 10.533
|
||||
236.96 9.7450
|
||||
246.43 8.8863
|
||||
255.18 8.0990
|
||||
266.12 7.4525
|
||||
277.06 6.7704
|
||||
288.00 6.0884
|
||||
299.67 5.5124
|
||||
311.35 5.0075
|
||||
323.03 4.5736
|
||||
335.44 4.2104
|
||||
347.13 3.9186
|
||||
358.81 3.6979
|
||||
370.50 3.5482
|
||||
380.00 3.4000
|
||||
160.00 25.000
|
||||
162.15 23.649
|
||||
165.02 22.226
|
||||
168.64 21.015
|
||||
172.25 19.734
|
||||
176.59 18.595
|
||||
181.67 17.525
|
||||
186.75 16.385
|
||||
191.83 15.316
|
||||
197.65 14.318
|
||||
205.65 13.247
|
||||
212.93 12.318
|
||||
219.48 11.462
|
||||
227.48 10.533
|
||||
236.96 9.7450
|
||||
246.43 8.8863
|
||||
255.18 8.0990
|
||||
266.12 7.4525
|
||||
277.06 6.7704
|
||||
288.00 6.0884
|
||||
299.67 5.5124
|
||||
311.35 5.0075
|
||||
323.03 4.5736
|
||||
335.44 4.2104
|
||||
347.13 3.9186
|
||||
358.81 3.6979
|
||||
370.50 3.5482
|
||||
380.00 3.4000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -1737,7 +1737,8 @@
|
|||
|
||||
</channel>
|
||||
|
||||
<channel name="Flaps">
|
||||
<channel name="SFCC">
|
||||
|
||||
<switch name="fcs/sfcc/unit1-avail">
|
||||
<default value="0"/>
|
||||
<test logic="OR" value="1">
|
||||
|
|
@ -1751,6 +1752,10 @@
|
|||
/systems/electrical/bus/dc2 ge 25
|
||||
</test>
|
||||
</switch>
|
||||
|
||||
</channel>
|
||||
|
||||
<channel name="Flaps">
|
||||
|
||||
<pure_gain name="fcs/flap-pos-gain">
|
||||
<input>/controls/flight/flaps</input>
|
||||
|
|
@ -1900,9 +1905,9 @@
|
|||
<independentVar lookup="row">/velocities/groundspeed-kt</independentVar>
|
||||
<independentVar lookup="column">hydraulics/tiller/switch</independentVar>
|
||||
<tableData>
|
||||
-1 0 1
|
||||
30.000 -70.0 0 70.0
|
||||
30.001 -10.0 0 10.0
|
||||
-1 0 1
|
||||
30.000 -70.0 0 70.0
|
||||
30.001 -10.0 0 10.0
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
|
|||
|
|
@ -9,11 +9,9 @@
|
|||
<!-- IT-AUTOFLIGHT -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Predictors -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
|
||||
<!-- Predictors -->
|
||||
|
||||
<predict-simple>
|
||||
<name>IAS 5 SECOND PREDICTOR</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -22,7 +20,7 @@
|
|||
<seconds>5.0</seconds>
|
||||
<filter-gain>0.0</filter-gain>
|
||||
</predict-simple>
|
||||
|
||||
|
||||
<predict-simple>
|
||||
<name>IAS 10 SECOND PREDICTOR</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -49,7 +47,7 @@
|
|||
<seconds>5.0</seconds>
|
||||
<filter-gain>0.0</filter-gain>
|
||||
</predict-simple>
|
||||
|
||||
|
||||
<predict-simple>
|
||||
<name>MACH 10 SECOND PREDICTOR</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -67,16 +65,13 @@
|
|||
<seconds>15.0</seconds>
|
||||
<filter-gain>0.0</filter-gain>
|
||||
</predict-simple>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Autopilot Helpers/Calculators -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
|
||||
<!-- Autopilot Helpers/Calculators -->
|
||||
|
||||
<filter>
|
||||
<name>AUTOLAND FD FPM</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<update-interval-secs type="double">0.05</update-interval-secs>
|
||||
<input>
|
||||
<expression>
|
||||
<table>
|
||||
|
|
@ -89,12 +84,11 @@
|
|||
</input>
|
||||
<output>/it-autoflight/internal/target-fpm-c2</output>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>AUTOLAND FPM</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<update-interval-secs type="double">0.05</update-interval-secs>
|
||||
<input>
|
||||
<expression>
|
||||
<table>
|
||||
|
|
@ -111,12 +105,11 @@
|
|||
</input>
|
||||
<output>/it-autoflight/internal/target-fpm-c</output>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>FMGC MNG SPD</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<update-interval-secs type="double">0.05</update-interval-secs>
|
||||
<input>
|
||||
<expression>
|
||||
<product>
|
||||
|
|
@ -138,7 +131,6 @@
|
|||
<name>FMGC MNG MACH</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<update-interval-secs type="double">0.05</update-interval-secs>
|
||||
<input>
|
||||
<expression>
|
||||
<product>
|
||||
|
|
@ -164,7 +156,6 @@
|
|||
<name>FMGC Target IAS PFD</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<update-interval-secs type="double">0.1</update-interval-secs>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
|
|
@ -193,10 +184,11 @@
|
|||
</input>
|
||||
<output>/FMGC/internal/target-ias-pfd</output>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>KTS INPUT FILTER</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<input>
|
||||
|
|
@ -218,32 +210,6 @@
|
|||
<property>/it-autoflight/settings/togaspd</property>
|
||||
</input>
|
||||
<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>
|
||||
<condition>
|
||||
<and>
|
||||
|
|
@ -257,6 +223,10 @@
|
|||
<value>7</value>
|
||||
</equals>
|
||||
</or>
|
||||
<equals>
|
||||
<property>/it-autoflight/input/kts-mach</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/gear/gear[1]/wow</property>
|
||||
<value>0</value>
|
||||
|
|
@ -269,43 +239,33 @@
|
|||
</condition>
|
||||
<value>5</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>100</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>MACH INPUT FILTER</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<input>
|
||||
<property>/it-autoflight/input/spd-mach</property>
|
||||
</input>
|
||||
<input>/it-autoflight/input/spd-mach</input>
|
||||
<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>
|
||||
<condition>
|
||||
<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>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>4</value>
|
||||
<property>/it-autoflight/input/kts-mach</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/gear/gear[1]/wow</property>
|
||||
|
|
@ -319,8 +279,9 @@
|
|||
</condition>
|
||||
<value>0.05</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>1</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>IAS SYNC</name>
|
||||
<type>gain</type>
|
||||
|
|
@ -333,8 +294,16 @@
|
|||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<update-interval-secs type="double">0.5</update-interval-secs>
|
||||
<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
|
||||
<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>
|
||||
</filter>
|
||||
|
||||
|
|
@ -350,8 +319,22 @@
|
|||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<update-interval-secs type="double">0.5</update-interval-secs>
|
||||
<input>/instrumentation/airspeed-indicator/indicated-mach</input>
|
||||
<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>
|
||||
</filter>
|
||||
|
||||
|
|
@ -365,9 +348,7 @@
|
|||
</condition>
|
||||
<property>/orientation/heading-deg</property>
|
||||
</input>
|
||||
<input>
|
||||
<property>/orientation/heading-magnetic-deg</property>
|
||||
</input>
|
||||
<input>/orientation/heading-magnetic-deg</input>
|
||||
<reference>0</reference>
|
||||
<output>/it-autoflight/internal/heading-deg</output>
|
||||
<output>/instrumentation/pfd/heading-deg</output>
|
||||
|
|
@ -484,21 +465,7 @@
|
|||
</sum>
|
||||
</expression>
|
||||
</input>
|
||||
<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>
|
||||
<input>0</input>
|
||||
<output>/it-autoflight/internal/heading-error-deg</output>
|
||||
<period>
|
||||
<min>-180</min>
|
||||
|
|
@ -522,7 +489,10 @@
|
|||
<input>
|
||||
<expression>
|
||||
<floor>
|
||||
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
||||
<sum>
|
||||
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
||||
<value>0.5</value>
|
||||
</sum>
|
||||
</floor>
|
||||
</expression>
|
||||
</input>
|
||||
|
|
@ -532,31 +502,18 @@
|
|||
<filter>
|
||||
<name>VERT SPEED FILTER</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<input>
|
||||
<property>/it-autoflight/input/vs</property>
|
||||
</input>
|
||||
<input>/it-autoflight/input/vs</input>
|
||||
<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>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/gear/gear[1]/wow</property>
|
||||
<value>0</value>
|
||||
|
|
@ -569,8 +526,9 @@
|
|||
</condition>
|
||||
<value>300</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>2000</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>NAV ERROR DEG</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -589,7 +547,7 @@
|
|||
<max>180</max>
|
||||
</period>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>INTERNAL VERTICAL SPEED COMPUTER</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -830,49 +788,13 @@
|
|||
</input>
|
||||
<output>/it-autoflight/internal/fpa</output>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Flight Director -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
|
||||
<!-- Flight Director -->
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: TARGET ROLL CMD</name>
|
||||
<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>
|
||||
<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>
|
||||
<condition>
|
||||
<or>
|
||||
|
|
@ -886,9 +808,37 @@
|
|||
</equals>
|
||||
</or>
|
||||
</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>
|
||||
<dif>
|
||||
<value>0</value>
|
||||
<property>/it-autoflight/internal/target-roll-fd</property>
|
||||
<property>/orientation/roll-deg</property>
|
||||
</dif>
|
||||
</expression>
|
||||
|
|
@ -897,7 +847,7 @@
|
|||
<min>-30</min>
|
||||
<max>30</max>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>FD: PITCH</name>
|
||||
<debug>false</debug>
|
||||
|
|
|
|||
|
|
@ -9,10 +9,8 @@
|
|||
<!-- IT-AUTOFLIGHT -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Vertical Modes -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<!-- Pitch Axis -->
|
||||
|
||||
<filter>
|
||||
<name>ALTITUDE CAPTURE/HOLD</name>
|
||||
|
|
@ -29,33 +27,19 @@
|
|||
</input>
|
||||
<reference>
|
||||
<condition>
|
||||
<not-equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/vert</property>
|
||||
<value>8</value>
|
||||
</not-equals>
|
||||
</equals>
|
||||
</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>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-fpm</property>
|
||||
</output>
|
||||
<min>
|
||||
<property>/it-autoflight/internal/min-vs</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/it-autoflight/internal/max-vs</property>
|
||||
</max>
|
||||
<reference>/it-autoflight/internal/alt</reference>
|
||||
<output>/it-autoflight/internal/target-fpm</output>
|
||||
<min>/it-autoflight/internal/min-vs</min>
|
||||
<max>/it-autoflight/internal/max-vs</max>
|
||||
</filter>
|
||||
|
||||
|
||||
<pid-controller>
|
||||
<name>FPA HOLD</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -87,15 +71,9 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/fpa</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/input/fpa</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-fpm-d</property>
|
||||
</output>
|
||||
<input>/it-autoflight/internal/fpa</input>
|
||||
<reference>/it-autoflight/input/fpa</reference>
|
||||
<output>/it-autoflight/internal/target-fpm-d</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<expression>
|
||||
|
|
@ -106,9 +84,6 @@
|
|||
</table>
|
||||
</expression>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>2.0</Ti>
|
||||
<Td>0.002</Td>
|
||||
<u_min>
|
||||
|
|
@ -215,9 +190,7 @@
|
|||
<property>/it-autoflight/internal/flch-mach</property>
|
||||
<scale>1000.0</scale>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-fpm-b</property>
|
||||
</output>
|
||||
<output>/it-autoflight/internal/target-fpm-b</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<condition>
|
||||
|
|
@ -237,9 +210,6 @@
|
|||
</condition>
|
||||
<value>-60</value>
|
||||
</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>2.5</Ti>
|
||||
<Td>0.001</Td>
|
||||
<u_min>
|
||||
|
|
@ -505,9 +475,7 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
||||
</input>
|
||||
<input>/it-autoflight/internal/vert-speed-fpm</input>
|
||||
<reference>
|
||||
<condition>
|
||||
<or>
|
||||
|
|
@ -590,9 +558,7 @@
|
|||
</condition>
|
||||
<property>/it-autoflight/internal/nav1-rate-of-climb-fpm</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-pitch-deg</property>
|
||||
</output>
|
||||
<output>/it-autoflight/internal/target-pitch-deg</output>
|
||||
<config>
|
||||
<Kp>
|
||||
<condition>
|
||||
|
|
@ -711,21 +677,15 @@
|
|||
<min>-15</min>
|
||||
<max>30</max>
|
||||
</filter>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>System Command: Pitch Rate</name>
|
||||
<debug>false</debug>
|
||||
<type>gain</type>
|
||||
<gain>0.15</gain>
|
||||
<input>
|
||||
<property>/orientation/pitch-deg</property>
|
||||
</input>
|
||||
<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>
|
||||
<input>/orientation/pitch-deg</input>
|
||||
<reference>/it-autoflight/internal/target-pitch-deg</reference>
|
||||
<output>/fdm/jsbsim/fbw/fmgc/pitch-cmd</output> <!-- Inputs to the FBW Pitch -->
|
||||
<min>-0.3</min>
|
||||
<max>0.3</max>
|
||||
</filter>
|
||||
|
|
|
|||
|
|
@ -9,11 +9,9 @@
|
|||
<!-- IT-AUTOFLIGHT -->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Lateral Modes -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
|
||||
<!-- Roll Axis -->
|
||||
|
||||
<pi-simple-controller>
|
||||
<name>ROLL CONTROLLER: HDG/LNAV</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -51,15 +49,9 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/heading-error-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/it-autoflight/internal/target-roll-deg</property>
|
||||
</output>
|
||||
<input>/it-autoflight/internal/heading-error-deg</input>
|
||||
<reference>0</reference>
|
||||
<output>/it-autoflight/internal/target-roll-deg</output>
|
||||
<config>
|
||||
<Kp>-1.8</Kp>
|
||||
<Ki>-0.000001</Ki>
|
||||
|
|
@ -67,9 +59,7 @@
|
|||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
<scale>-1</scale>
|
||||
</min>
|
||||
<max>
|
||||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
</max>
|
||||
<max>/it-autoflight/internal/bank-limit</max>
|
||||
</config>
|
||||
</pi-simple-controller>
|
||||
|
||||
|
|
@ -104,30 +94,9 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<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>
|
||||
<input>/it-autoflight/internal/nav-heading-error-deg</input>
|
||||
<reference>0</reference>
|
||||
<output>/it-autoflight/internal/target-roll-deg</output>
|
||||
<config>
|
||||
<Kp>-2.8</Kp>
|
||||
<Ki>-0.0001</Ki>
|
||||
|
|
@ -135,12 +104,10 @@
|
|||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
<scale>-1</scale>
|
||||
</min>
|
||||
<max>
|
||||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
</max>
|
||||
<max>/it-autoflight/internal/bank-limit</max>
|
||||
</config>
|
||||
</pi-simple-controller>
|
||||
|
||||
|
||||
<filter>
|
||||
<name>ROLL DEG SYNC</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -174,48 +141,14 @@
|
|||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
<scale>-1</scale>
|
||||
</min>
|
||||
<max>
|
||||
<property>/it-autoflight/internal/bank-limit</property>
|
||||
</max>
|
||||
<max>/it-autoflight/internal/bank-limit</max>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>IT-CONTROLLER: TARGET ROLL CMD</name>
|
||||
<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>
|
||||
<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>
|
||||
<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>
|
||||
<or>
|
||||
<equals>
|
||||
|
|
@ -229,17 +162,63 @@
|
|||
</or>
|
||||
</condition>
|
||||
<value>0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/fdm/jsbsim/fbw/fmgc/roll-cmd</property> <!-- Inputs to the FBW Roll Rate -->
|
||||
</output>
|
||||
</input>
|
||||
<input>/it-autoflight/internal/target-roll-deg</input>
|
||||
<output>/it-autoflight/internal/target-roll</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>
|
||||
<max>0.32</max>
|
||||
</filter>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Yaw Control -->
|
||||
<!-- =============================================================== -->
|
||||
<!-- Yaw Axis -->
|
||||
|
||||
<pi-simple-controller>
|
||||
<name>RUDDER VORLOC TRK</name>
|
||||
|
|
@ -252,12 +231,8 @@
|
|||
</equals>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/it-autoflight/internal/nav-heading-error-deg</property>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0</value>
|
||||
</reference>
|
||||
<input>/it-autoflight/internal/nav-heading-error-deg</input>
|
||||
<reference>0</reference>
|
||||
<output>/it-autoflight/internal/rudder-cmd</output>
|
||||
<config>
|
||||
<Kp>
|
||||
|
|
@ -275,21 +250,7 @@
|
|||
</condition>
|
||||
<value>-0.05</value>
|
||||
</Kp>
|
||||
<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>
|
||||
<Kp>-0.02</Kp>
|
||||
<Ki>0</Ki>
|
||||
</config>
|
||||
<min>-0.15</min>
|
||||
|
|
@ -299,28 +260,32 @@
|
|||
<filter>
|
||||
<name>IT-CONTROLLER: RUDDER CMD</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<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>
|
||||
<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>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/lat</property>
|
||||
<value>4</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<property>/it-autoflight/internal/rudder-cmd</property>
|
||||
</input>
|
||||
<output>/fdm/jsbsim/fbw/fmgc/yaw-cmd</output>
|
||||
<type>noise-spike</type>
|
||||
<input>0</input>
|
||||
<output>/fdm/jsbsim/fbw/fmgc/yaw-cmd</output> <!-- Inputs to the FBW Yaw -->
|
||||
<max-rate-of-change>0.6</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
|
|
|
|||
|
|
@ -7,54 +7,31 @@
|
|||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Thrust Modes -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
|
||||
<!-- Thrust Axis -->
|
||||
|
||||
<filter>
|
||||
<name>KTS INPUT FILTER</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<input>
|
||||
<property>/it-autoflight/input/spd-kts</property>
|
||||
</input>
|
||||
<input>/it-autoflight/input/spd-kts</input>
|
||||
<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>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
<property>/it-autoflight/input/kts-mach</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/gear/gear[1]/wow</property>
|
||||
|
|
@ -68,50 +45,30 @@
|
|||
</condition>
|
||||
<value>10</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>200</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>MACH INPUT FILTER</name>
|
||||
<debug>false</debug>
|
||||
<type>noise-spike</type>
|
||||
<feedback-if-disabled>true</feedback-if-disabled>
|
||||
<initialize-to>output</initialize-to>
|
||||
<input>
|
||||
<property>/it-autoflight/input/spd-mach</property>
|
||||
</input>
|
||||
<input>/it-autoflight/input/spd-mach</input>
|
||||
<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>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<property>/it-autoflight/input/kts-mach</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
|
|
@ -126,6 +83,7 @@
|
|||
</condition>
|
||||
<value>0.1</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>2</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
|
|
@ -250,28 +208,15 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
|
||||
</input>
|
||||
<reference>
|
||||
<property>/it-autoflight/internal/kts</property>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
|
||||
<reference>/it-autoflight/internal/kts</reference>
|
||||
<output>/controls/engines/throttle-cmd-pid</output>
|
||||
<config>
|
||||
<Kp>0.055</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>9.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</u_min>
|
||||
<u_max>
|
||||
<property>/controls/engines/throttle-pid-max</property>
|
||||
</u_max>
|
||||
<u_min>/controls/engines/idle-limit</u_min>
|
||||
<u_max>/controls/engines/throttle-pid-max</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
|
|
@ -390,22 +335,13 @@
|
|||
<property>/it-autoflight/internal/mach</property>
|
||||
<scale>1000.0</scale>
|
||||
</reference>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<output>/controls/engines/throttle-cmd-pid</output>
|
||||
<config>
|
||||
<Kp>0.055</Kp>
|
||||
<beta>1.0</beta>
|
||||
<alpha>0.1</alpha>
|
||||
<gamma>0.0</gamma>
|
||||
<Ti>9.0</Ti>
|
||||
<Td>0.00001</Td>
|
||||
<u_min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</u_min>
|
||||
<u_max>
|
||||
<property>/controls/engines/throttle-pid-max</property>
|
||||
</u_max>
|
||||
<u_min>/controls/engines/idle-limit</u_min>
|
||||
<u_max>/controls/engines/throttle-pid-max</u_max>
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
|
|
@ -512,12 +448,8 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<value>0.0</value>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<input>0.0</input>
|
||||
<output>/controls/engines/throttle-cmd-pid</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
|
|
@ -623,12 +555,8 @@
|
|||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<value>1.0</value>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<input>1.0</input>
|
||||
<output>/controls/engines/throttle-cmd-pid</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
|
|
@ -725,12 +653,10 @@
|
|||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>1</value>
|
||||
<value>1.0</value>
|
||||
</input>
|
||||
<input>0</input>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<input>0.0</input>
|
||||
<output>/controls/engines/throttle-cmd-pid</output>
|
||||
</filter>
|
||||
|
||||
</PropertyList>
|
||||
|
|
|
|||
|
|
@ -1 +1 @@
|
|||
4679
|
||||
4681
|
||||
Reference in a new issue