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IDG-A32X/Systems/fmgc-roll-yaw.xml
2018-12-19 20:55:02 -05:00

296 lines
6.9 KiB
XML

<?xml version="1.0"?>
<!-- Copyright (c) 2018 Joshua Davidson (it0uchpods) -->
<!-- IT-AUTOFLIGHT -->
<PropertyList>
<!-- Roll Axis -->
<pi-simple-controller>
<name>ROLL CONTROLLER: HDG/LNAV</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>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>/it-autoflight/internal/heading-error-deg</input>
<reference>0</reference>
<output>/it-autoflight/internal/target-roll-deg</output>
<config>
<Kp>
<expression>
<table>
<property>/fdm/jsbsim/velocities/vc-kts</property>
<entry><ind>140</ind><dep>-1.8</dep></entry>
<entry><ind>360</ind><dep>-2.8</dep></entry>
</table>
</expression>
</Kp>
<Ki>-0.000001</Ki>
<min>
<property>/it-autoflight/internal/bank-limit</property>
<scale>-1.0</scale>
</min>
<max>/it-autoflight/internal/bank-limit</max>
</config>
</pi-simple-controller>
<pi-simple-controller>
<name>VORLOC TRK</name>
<debug>false</debug>
<enable>
<condition>
<and>
<equals>
<property>/it-autoflight/output/lat</property>
<value>2</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>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<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>
<min>
<property>/it-autoflight/internal/bank-limit</property>
<scale>-1.0</scale>
</min>
<max>/it-autoflight/internal/bank-limit</max>
</config>
</pi-simple-controller>
<filter>
<name>ROLL DEG SYNC</name>
<debug>false</debug>
<type>gain</type>
<gain>1.0</gain>
<enable>
<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>
</enable>
<input>/orientation/roll-deg</input>
<output>/it-autoflight/internal/target-roll-deg</output>
<min>
<property>/it-autoflight/internal/bank-limit</property>
<scale>-1.0</scale>
</min>
<max>/it-autoflight/internal/bank-limit</max>
</filter>
<filter>
<name>IT-CONTROLLER: TARGET ROLL CMD</name>
<debug>false</debug>
<type>noise-spike</type>
<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>
<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 Axis -->
<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>/it-autoflight/internal/nav-heading-error-deg</input>
<reference>0</reference>
<output>/it-autoflight/internal/rudder-cmd</output>
<config>
<Kp>
<condition>
<and>
<equals>
<property>/gear/gear[1]/wow</property>
<value>0</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>0</value>
</equals>
</and>
</condition>
<value>-0.05</value>
</Kp>
<Kp>-0.02</Kp>
<Ki>0</Ki>
</config>
<min>-0.15</min>
<max>0.15</max>
</pi-simple-controller>
<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>
<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>
<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>
</PropertyList>