292 lines
6.8 KiB
XML
292 lines
6.8 KiB
XML
<?xml version="1.0"?>
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<!-- Copyright (c) 2019 Joshua Davidson (it0uchpods) -->
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<!-- IT-AUTOFLIGHT -->
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<PropertyList>
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<!-- Roll Axis -->
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<filter>
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<name>IT-CONTROLLER: HDG/LNAV ROLL</name>
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<debug>false</debug>
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<type>gain</type>
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<gain>
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<expression>
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<table>
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<property>/fdm/jsbsim/velocities/vc-kts</property>
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<entry><ind>140</ind><dep>1.8</dep></entry>
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<entry><ind>360</ind><dep>2.8</dep></entry>
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</table>
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</expression>
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</gain>
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<enable>
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<condition>
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<and>
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<or>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>1</value>
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</equals>
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</or>
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<or>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/fd1</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/fd2</property>
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<value>1</value>
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</equals>
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</or>
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</and>
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</condition>
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</enable>
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<input>/it-autoflight/internal/heading-error-deg</input>
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<reference>0</reference>
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<output>/it-autoflight/internal/target-roll-deg</output>
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<min>
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<property>/it-autoflight/internal/bank-limit</property>
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<scale>-1.0</scale>
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</min>
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<max>/it-autoflight/internal/bank-limit</max>
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</filter>
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<filter>
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<name>IT-CONTROLLER: VORLOC ROLL</name>
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<debug>false</debug>
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<type>gain</type>
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<gain>2.8</gain>
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<enable>
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<condition>
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<and>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>2</value>
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</equals>
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<or>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/fd1</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/fd2</property>
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<value>1</value>
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</equals>
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</or>
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</and>
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</condition>
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</enable>
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<input>/it-autoflight/internal/nav-heading-error-deg</input>
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<reference>0</reference>
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<output>/it-autoflight/internal/target-roll-deg</output>
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<min>
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<property>/it-autoflight/internal/bank-limit</property>
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<scale>-1.0</scale>
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</min>
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<max>/it-autoflight/internal/bank-limit</max>
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</filter>
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<filter>
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<name>ROLL DEG SYNC</name>
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<debug>false</debug>
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<type>gain</type>
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<gain>1.0</gain>
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<enable>
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<condition>
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<and>
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<not-equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/fd1</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/fd2</property>
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<value>1</value>
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</not-equals>
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</and>
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</condition>
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</enable>
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<input>/orientation/roll-deg</input>
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<output>/it-autoflight/internal/target-roll-deg</output>
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<min>
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<property>/it-autoflight/internal/bank-limit</property>
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<scale>-1.0</scale>
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</min>
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<max>/it-autoflight/internal/bank-limit</max>
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</filter>
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<filter>
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<name>IT-CONTROLLER: TARGET ROLL CMD</name>
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<debug>false</debug>
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<type>noise-spike</type>
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<input>
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<condition>
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<or>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>4</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>5</value>
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</equals>
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</or>
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</condition>
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<value>0</value>
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</input>
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<input>/it-autoflight/internal/target-roll-deg</input>
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<output>/it-autoflight/internal/target-roll</output>
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<max-rate-of-change>
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<condition>
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<and>
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<not-equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/fd1</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/fd2</property>
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<value>1</value>
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</not-equals>
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</and>
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</condition>
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<value>50</value>
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</max-rate-of-change>
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<max-rate-of-change>
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<condition>
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<and>
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<not-equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</not-equals>
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<not-equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</not-equals>
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</and>
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</condition>
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<value>15</value>
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</max-rate-of-change>
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<max-rate-of-change>6</max-rate-of-change>
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</filter>
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<filter>
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<name>System Command: Roll Rate</name>
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<debug>false</debug>
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<type>gain</type>
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<gain>-0.1</gain>
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<input>/orientation/roll-deg</input>
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<reference>/it-autoflight/internal/target-roll</reference>
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<output>/fdm/jsbsim/fbw/fmgc/roll-cmd</output> <!-- Inputs to the FBW Roll -->
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<min>-0.32</min>
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<max>0.32</max>
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</filter>
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<!-- Yaw Axis -->
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<pi-simple-controller>
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<name>RUDDER VORLOC TRK</name>
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<debug>false</debug>
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<enable>
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<condition>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>4</value>
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</equals>
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</condition>
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</enable>
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<input>/it-autoflight/internal/nav-heading-error-deg</input>
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<reference>0</reference>
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<output>/it-autoflight/internal/rudder-cmd</output>
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<config>
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<Kp>
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<condition>
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<and>
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<equals>
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<property>/gear/gear[1]/wow</property>
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<value>0</value>
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</equals>
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<equals>
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<property>/gear/gear[2]/wow</property>
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<value>0</value>
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</equals>
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</and>
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</condition>
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<value>-0.05</value>
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</Kp>
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<Kp>-0.02</Kp>
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<Ki>0</Ki>
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</config>
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<min>-0.15</min>
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<max>0.15</max>
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</pi-simple-controller>
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<filter>
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<name>IT-CONTROLLER: RUDDER CMD</name>
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<debug>false</debug>
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<type>noise-spike</type>
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<feedback-if-disabled>true</feedback-if-disabled>
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<initialize-to>output</initialize-to>
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<input>
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<condition>
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<and>
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<or>
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<equals>
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<property>/it-autoflight/output/ap1</property>
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<value>1</value>
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</equals>
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<equals>
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<property>/it-autoflight/output/ap2</property>
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<value>1</value>
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</equals>
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</or>
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<equals>
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<property>/it-autoflight/output/lat</property>
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<value>4</value>
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</equals>
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</and>
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</condition>
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<property>/it-autoflight/internal/rudder-cmd</property>
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</input>
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<input>0</input>
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<output>/fdm/jsbsim/fbw/fmgc/yaw-cmd</output> <!-- Inputs to the FBW Yaw -->
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<max-rate-of-change>0.6</max-rate-of-change>
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</filter>
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</PropertyList>
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