FMGC: Improve speed on pitch control loop
This commit is contained in:
Josh Davidson
parent
7b0180fec7
commit
11e8d34608
2 changed files with 161 additions and 115 deletions
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@ -237,7 +237,7 @@
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<type>exponential</type>
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<input>/velocities/airspeed-kt</input>
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<output>/it-autoflight/internal/kts-input-lag</output>
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<filter-time>0.16</filter-time>
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<filter-time>0.04</filter-time>
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</filter>
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<filter>
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@ -270,7 +270,7 @@
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</input>
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<input>/it-autoflight/internal/kts-rate-raw</input>
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<output>/it-autoflight/internal/kts-rate</output>
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<filter-time>0.16</filter-time>
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<filter-time>0.04</filter-time>
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</filter>
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<filter>
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@ -278,7 +278,7 @@
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<type>exponential</type>
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<input>/velocities/mach</input>
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<output>/it-autoflight/internal/mach-input-lag</output>
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<filter-time>0.16</filter-time>
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<filter-time>0.04</filter-time>
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</filter>
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<filter>
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@ -319,7 +319,7 @@
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</input>
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<input>/it-autoflight/internal/mach-rate-gain</input>
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<output>/it-autoflight/internal/mach-rate</output>
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<filter-time>0.16</filter-time>
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<filter-time>0.04</filter-time>
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</filter>
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<filter>
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@ -868,110 +868,6 @@
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<output>/it-autoflight/internal/fpa</output>
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</filter>
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<!-- Flight Director -->
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<filter>
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<name>FD Target Roll Filter</name>
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<type>noise-spike</type>
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<input>/it-autoflight/internal/target-roll-deg</input>
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<output>/it-autoflight/internal/target-roll-fd</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/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/fd1</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>1000</value>
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</max-rate-of-change>
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<max-rate-of-change>15</max-rate-of-change>
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</filter>
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<filter>
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<name>FD Roll</name>
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<type>noise-spike</type>
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<input>
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<expression>
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<difference>
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<property>/it-autoflight/internal/target-roll-fd</property>
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<property>/orientation/roll-deg</property>
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</difference>
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</expression>
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</input>
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<output>/it-autoflight/fd/roll-bar</output>
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<min>-30</min>
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<max>30</max>
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<max-rate-of-change>20</max-rate-of-change>
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</filter>
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<filter>
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<name>FD Pitch Takeoff</name>
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<type>gain</type>
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<gain>1.0</gain>
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<input>
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<condition>
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<equals>
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<property>/it-autoflight/mode/vert</property>
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<value>T/O CLB</value>
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</equals>
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</condition>
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<expression>
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<product>
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<table>
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<property>/orientation/pitch-deg</property>
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<entry><ind> 1</ind><dep>1</dep></entry>
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<entry><ind>10</ind><dep>0</dep></entry>
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</table>
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<table>
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<property>/position/gear-agl-ft</property>
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<entry><ind> 5</ind><dep>1</dep></entry>
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<entry><ind>30</ind><dep>0</dep></entry>
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</table>
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</product>
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</expression>
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</input>
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<input>0</input>
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<output>/it-autoflight/fd/pitch-bar-takeoff</output>
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</filter>
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<filter>
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<name>FD Pitch</name>
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<type>noise-spike</type>
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<input>
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<expression>
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<sum>
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<rad2deg>
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<asin>
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<div>
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<difference>
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<property>/it-autoflight/internal/target-common-fpm</property>
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<property>/it-autoflight/internal/vert-speed-fpm</property>
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</difference>
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<product>
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<max>
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<property>/instrumentation/airspeed-indicator[0]/true-speed-kt</property>
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<value>100</value>
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</max>
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<value>151.90288713910761</value> <!-- FPM to Knot * 1.5 -->
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</product>
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</div>
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</asin>
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</rad2deg>
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<property>/it-autoflight/fd/pitch-bar-takeoff</property>
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</sum>
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</expression>
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</input>
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<output>/it-autoflight/fd/pitch-bar</output>
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<min>-15</min>
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<max>15</max>
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<max-rate-of-change>10</max-rate-of-change>
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</filter>
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<filter>
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<name>Accel Altitude</name>
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<type>gain</type>
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@ -1017,4 +913,108 @@
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<output>/it-autoflight/settings/accel-ft</output>
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</filter>
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<!-- Flight Director -->
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<filter>
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<name>FD Target Roll Filter</name>
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<type>noise-spike</type>
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<input>/it-autoflight/internal/target-roll-deg</input>
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<output>/it-autoflight/internal/target-roll-fd</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/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/fd1</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>1000</value>
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</max-rate-of-change>
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<max-rate-of-change>15</max-rate-of-change>
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</filter>
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<filter>
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<name>FD Roll</name>
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<type>noise-spike</type>
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<input>
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<expression>
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<difference>
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<property>/it-autoflight/internal/target-roll-fd</property>
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<property>/orientation/roll-deg</property>
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</difference>
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</expression>
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</input>
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<output>/it-autoflight/fd/roll-bar</output>
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<min>-30</min>
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<max>30</max>
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<max-rate-of-change>20</max-rate-of-change>
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</filter>
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<filter>
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<name>FD Pitch Takeoff</name>
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<type>noise-spike</type>
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<input>
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<condition>
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<equals>
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<property>/it-autoflight/mode/vert</property>
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<value>T/O CLB</value>
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</equals>
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</condition>
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<expression>
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<product>
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<table>
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<property>/orientation/pitch-deg</property>
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<entry><ind> 1</ind><dep>1</dep></entry>
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<entry><ind>10</ind><dep>0</dep></entry>
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</table>
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<table>
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<property>/position/gear-agl-ft</property>
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<entry><ind> 5</ind><dep>1</dep></entry>
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<entry><ind>30</ind><dep>0</dep></entry>
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</table>
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</product>
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</expression>
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</input>
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<input>0</input>
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<output>/it-autoflight/fd/pitch-bar-takeoff</output>
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<max-rate-of-change>7.5</max-rate-of-change>
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</filter>
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<filter>
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<name>FD Pitch</name>
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<type>noise-spike</type>
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<input>
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<expression>
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<sum>
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<rad2deg>
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<asin>
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<div>
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<difference>
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<property>/it-autoflight/internal/target-common-fpm</property>
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<property>/it-autoflight/internal/vert-speed-fpm</property>
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</difference>
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<product>
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<max>
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<property>/instrumentation/airspeed-indicator[0]/true-speed-kt</property>
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<value>100</value>
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</max>
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<value>151.90288713910761</value> <!-- FPM to Knot * 1.5 -->
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</product>
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</div>
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</asin>
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</rad2deg>
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<property>/it-autoflight/fd/pitch-bar-takeoff</property>
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</sum>
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</expression>
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</input>
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<output>/it-autoflight/fd/pitch-bar</output>
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<min>-15</min>
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<max>15</max>
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<max-rate-of-change>10</max-rate-of-change>
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</filter>
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</PropertyList>
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@ -230,6 +230,25 @@
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<max-rate-of-change>10000</max-rate-of-change>
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</filter>
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<logic>
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<input>
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<and>
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<property>/it-autoflight/output/apfd-on</property>
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<or>
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<equals>
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<property>/it-autoflight/output/vert</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/vert</property>
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<value>7</value>
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</equals>
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</or>
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</and>
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</input>
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<output>/it-autoflight/internal/flch-active</output>
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</logic>
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<filter>
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<name>IT-CONTROLLER: Speed By Pitch Delta</name>
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<type>gain</type>
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@ -254,27 +273,54 @@
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<input>/it-autoflight/internal/kts-rate</input>
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<reference>/it-autoflight/internal/flch-kts-error</reference>
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<output>/it-autoflight/internal/flch-raw</output>
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<min>
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<condition>
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<or>
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<equals>
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<property>/gear/gear[1]/wow</property>
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<value>1</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>1</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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</min>
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<min>-2000</min>
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<max>2000</max>
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</filter>
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<filter>
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<name>IT-CONTROLLER: Speed By Pitch Delta Lag</name>
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<type>exponential</type>
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<input>/it-autoflight/internal/flch-raw</input>
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<output>/it-autoflight/internal/flch-lag</output>
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<filter-time>0.16</filter-time>
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<name>Speed By Pitch Filter</name>
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<type>noise-spike</type>
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<input>
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<condition>
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<property>/it-autoflight/internal/flch-active</property>
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</condition>
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<property>/it-autoflight/internal/flch-raw</property>
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</input>
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<input>/it-autoflight/internal/vert-speed-fpm</input>
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<output>/it-autoflight/internal/flch-filtered</output>
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<max-rate-of-change>
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<condition>
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<property>/it-autoflight/internal/flch-active</property>
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</condition>
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<value>1500</value>
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</max-rate-of-change>
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<max-rate-of-change>10000</max-rate-of-change>
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</filter>
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<filter>
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<name>IT-CONTROLLER: Speed By Pitch</name>
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<name>Speed By Pitch Final</name>
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<type>gain</type>
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<gain>1.0</gain>
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<input>
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<expression>
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<sum>
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<property>/it-autoflight/internal/vert-speed-fpm</property>
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<property>/it-autoflight/internal/flch-lag</property>
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<property>/it-autoflight/internal/flch-filtered</property>
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</sum>
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</expression>
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</input>
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