880 lines
21 KiB
XML
880 lines
21 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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<!-- Predictors -->
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<predict-simple>
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<name>IAS 5 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
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<output>/it-autoflight/internal/lookahead-5-sec-airspeed-kt</output>
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<seconds>5.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<predict-simple>
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<name>IAS 10 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
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<output>/it-autoflight/internal/lookahead-10-sec-airspeed-kt</output>
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<seconds>10.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<predict-simple>
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<name>IAS 15 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-speed-kt</input>
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<output>/it-autoflight/internal/lookahead-15-sec-airspeed-kt</output>
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<seconds>15.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<predict-simple>
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<name>MACH 5 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-mach</input>
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<output>/it-autoflight/internal/lookahead-5-sec-mach</output>
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<seconds>5.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<predict-simple>
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<name>MACH 10 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-mach</input>
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<output>/it-autoflight/internal/lookahead-10-sec-mach</output>
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<seconds>10.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<predict-simple>
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<name>MACH 15 SECOND PREDICTOR</name>
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<debug>false</debug>
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<input>/instrumentation/airspeed-indicator/indicated-mach</input>
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<output>/it-autoflight/internal/lookahead-15-sec-mach</output>
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<seconds>15.0</seconds>
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<filter-gain>0.0</filter-gain>
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</predict-simple>
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<!-- Autopilot Helpers/Calculators -->
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<filter>
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<name>AUTOLAND FD FPM</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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<table>
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<property>/position/gear-agl-ft</property>
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<entry><ind>100</ind><dep>-650</dep></entry>
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<entry><ind> 50</ind><dep>-500</dep></entry>
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<entry><ind> 45</ind><dep> -70</dep></entry>
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</table>
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</expression>
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</input>
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<output>/it-autoflight/internal/target-fpm-c2</output>
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</filter>
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<filter>
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<name>AUTOLAND FPM</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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<table>
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<property>/position/gear-agl-ft</property>
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<entry><ind>100</ind><dep>-650</dep></entry>
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<entry><ind> 50</ind><dep>-500</dep></entry>
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<entry><ind> 40</ind><dep>-400</dep></entry>
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<entry><ind> 30</ind><dep>-300</dep></entry>
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<entry><ind> 20</ind><dep>-180</dep></entry>
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<entry><ind> 10</ind><dep>-100</dep></entry>
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<entry><ind> 5</ind><dep> -70</dep></entry>
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</table>
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</expression>
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</input>
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<output>/it-autoflight/internal/target-fpm-c</output>
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</filter>
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<filter>
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<name>FMGC MNG SPD</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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<product>
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<value>266</value>
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<table>
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<property>/FMGC/internal/cost-index</property>
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<entry><ind> 0</ind><dep>1.00</dep></entry>
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<entry><ind>120</ind><dep>1.19</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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<output>/FMGC/internal/mng-alt-spd</output>
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<min>250</min>
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<max>345</max>
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</filter>
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<filter>
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<name>FMGC MNG MACH</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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<product>
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<table>
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<property>/instrumentation/altimeter/indicated-altitude-ft</property>
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<entry><ind>20000</ind><dep>0.625</dep></entry>
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<entry><ind>42000</ind><dep>0.805</dep></entry>
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</table>
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<table>
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<property>/FMGC/internal/cost-index</property>
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<entry><ind> 0</ind><dep>0.97</dep></entry>
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<entry><ind>120</ind><dep>1.05</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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<output>/FMGC/internal/mng-alt-mach</output>
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<min>0.500</min>
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<max>0.815</max>
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</filter>
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<filter>
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<name>FMGC Target IAS PFD</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/input/kts-mach</property>
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<value>0</value>
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</equals>
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</condition>
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<property>/it-autoflight/input/spd-kts</property>
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</input>
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<input>
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<condition>
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<equals>
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<property>/it-autoflight/input/kts-mach</property>
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<value>1</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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<div>
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<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
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<property>/instrumentation/airspeed-indicator/indicated-mach</property>
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</div>
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<property>/it-autoflight/input/spd-mach</property>
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</product>
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</expression>
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</input>
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<output>/FMGC/internal/target-ias-pfd</output>
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</filter>
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<filter>
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<name>KTS INPUT FILTER</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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<not-equals>
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<property>/it-autoflight/mode/vert</property>
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<value>T/O CLB</value>
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</not-equals>
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</condition>
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<property>/it-autoflight/input/spd-kts</property>
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</input>
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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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<property>/it-autoflight/settings/togaspd</property>
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</input>
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<output>/it-autoflight/internal/flch-kts</output>
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<max-rate-of-change>
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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/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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<equals>
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<property>/it-autoflight/input/kts-mach</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[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>5</value>
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</max-rate-of-change>
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<max-rate-of-change>100</max-rate-of-change>
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</filter>
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<filter>
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<name>MACH INPUT FILTER</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>/it-autoflight/input/spd-mach</input>
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<output>/it-autoflight/internal/flch-mach</output>
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<max-rate-of-change>
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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/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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<equals>
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<property>/it-autoflight/input/kts-mach</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[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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</max-rate-of-change>
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<max-rate-of-change>1</max-rate-of-change>
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</filter>
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<filter>
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<name>IAS SYNC</name>
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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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<equals>
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<property>/it-autoflight/input/kts-mach</property>
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<value>1</value>
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</equals>
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</condition>
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</enable>
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<input>
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<expression>
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<floor>
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<sum>
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<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
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<value>0.5</value>
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</sum>
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</floor>
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</expression>
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</input>
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<output>/it-autoflight/input/spd-kts</output>
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</filter>
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<filter>
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<name>MACH SYNC</name>
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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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<equals>
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<property>/it-autoflight/input/kts-mach</property>
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<value>0</value>
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</equals>
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</condition>
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</enable>
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<input>
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<expression>
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<div>
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<floor>
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<sum>
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<product>
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<property>/instrumentation/airspeed-indicator/indicated-mach</property>
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<value>1000</value>
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</product>
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<value>0.5</value>
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</sum>
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</floor>
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<value>1000</value>
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</div>
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</expression>
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</input>
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<output>/it-autoflight/input/spd-mach</output>
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</filter>
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<filter>
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<name>HEADING DEG</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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<property>/instrumentation/efis/mfd/true-north</property>
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</condition>
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<property>/orientation/heading-deg</property>
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</input>
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<input>/orientation/heading-magnetic-deg</input>
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<reference>0</reference>
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<output>/it-autoflight/internal/heading-deg</output>
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<output>/instrumentation/pfd/heading-deg</output>
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</filter>
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<filter>
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<name>TRACK DEG</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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<and>
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<property>/instrumentation/efis/mfd/true-north</property>
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<greater-than>
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<property>/velocities/groundspeed-kt</property>
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<value>1</value>
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</greater-than>
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</and>
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</condition>
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<property>/orientation/track-deg</property>
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</input>
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<input>
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<condition>
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<and>
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<not><property>/instrumentation/efis/mfd/true-north</property></not>
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<greater-than>
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<property>/velocities/groundspeed-kt</property>
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<value>1</value>
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</greater-than>
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</and>
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</condition>
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<property>/orientation/track-magnetic-deg</property>
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</input>
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<input>/it-autoflight/internal/heading-deg</input>
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<reference>0</reference>
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<output>/it-autoflight/internal/track-deg</output>
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<output>/instrumentation/pfd/track-deg</output>
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</filter>
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<filter>
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<name>DRIFT ANGLE</name>
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<type>gain</type>
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<gain>1.0</gain>
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<input>/orientation/track-magnetic-deg</input>
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<reference>/orientation/heading-magnetic-deg</reference>
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<output>/it-autoflight/internal/drift-angle-deg</output>
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<period>
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<min>-180</min>
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<max>180</max>
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</period>
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</filter>
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<filter>
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<name>HEADING ERROR DEG</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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<input>
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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>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/input/trk</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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<property>/it-autoflight/input/hdg</property>
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<offset>
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<property>/it-autoflight/internal/heading-deg</property>
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<scale>-1.0</scale>
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</offset>
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</input>
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<input>
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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>0</value>
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</equals>
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<equals>
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<property>/it-autoflight/input/trk</property>
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<value>1</value>
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</equals>
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</and>
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</condition>
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<property>/it-autoflight/input/hdg</property>
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<offset>
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<property>/it-autoflight/internal/track-deg</property>
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<scale>-1.0</scale>
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</offset>
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</input>
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<input>
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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>1</value>
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</equals>
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</condition>
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<expression>
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<sum>
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<property>/autopilot/route-manager/wp[0]/true-bearing-deg</property>
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<product>
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<property>/it-autoflight/internal/drift-angle-deg</property>
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<value>-1.0</value>
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</product>
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<product>
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<property>/orientation/heading-deg</property>
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<value>-1.0</value>
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</product>
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</sum>
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</expression>
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</input>
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<input>0</input>
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<output>/it-autoflight/internal/heading-error-deg</output>
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<period>
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<min>-180</min>
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<max>180</max>
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</period>
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</filter>
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<filter>
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<name>VERT SPEED 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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<not-equals>
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<property>/it-autoflight/output/vert</property>
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<value>1</value>
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</not-equals>
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</condition>
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</enable>
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<input>
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<expression>
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<floor>
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<sum>
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<property>/it-autoflight/internal/vert-speed-fpm</property>
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<value>0.5</value>
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</sum>
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</floor>
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</expression>
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</input>
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<output>/it-autoflight/input/vs</output>
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</filter>
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<filter>
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<name>VERT SPEED FILTER</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>/it-autoflight/input/vs</input>
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<output>/it-autoflight/internal/vs</output>
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<max-rate-of-change>
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<condition>
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<and>
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<equals>
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<property>/it-autoflight/output/vert</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[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>300</value>
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</max-rate-of-change>
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<max-rate-of-change>2000</max-rate-of-change>
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</filter>
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<filter>
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|
<name>NAV ERROR DEG</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>
|
|
<property>/instrumentation/nav[0]/radials/target-auto-hdg-deg</property>
|
|
<offset>
|
|
<property>/orientation/heading-deg</property>
|
|
<scale>-1.0</scale>
|
|
</offset>
|
|
</input>
|
|
<output>/it-autoflight/internal/nav-heading-error-deg</output>
|
|
<period>
|
|
<min>-180</min>
|
|
<max>180</max>
|
|
</period>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>INTERNAL VERTICAL SPEED COMPUTER</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>/instrumentation/gps/indicated-vertical-speed</input>
|
|
<output>/it-autoflight/internal/vert-speed-fpm</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>INTERNAL VERTICAL SPEED COMPUTER SYNC 4</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<enable>
|
|
<condition>
|
|
<not>
|
|
<or>
|
|
<equals>
|
|
<property>/it-autoflight/output/vert</property>
|
|
<value>4</value>
|
|
</equals>
|
|
<equals>
|
|
<property>/it-autoflight/output/vert</property>
|
|
<value>7</value>
|
|
</equals>
|
|
<and>
|
|
<equals>
|
|
<property>/it-autoflight/output/vert</property>
|
|
<value>8</value>
|
|
</equals>
|
|
<equals>
|
|
<property>/it-autoflight/output/vert-mng</property>
|
|
<value>4</value>
|
|
</equals>
|
|
</and>
|
|
</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>
|
|
</not>
|
|
</condition>
|
|
</enable>
|
|
<input>/it-autoflight/internal/vert-speed-fpm</input>
|
|
<output>/it-autoflight/internal/target-fpm-b</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>INTERNAL VERTICAL SPEED COMPUTER SYNC 5</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<enable>
|
|
<condition>
|
|
<not>
|
|
<equals>
|
|
<property>/it-autoflight/output/vert</property>
|
|
<value>5</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>
|
|
</not>
|
|
</condition>
|
|
</enable>
|
|
<input>/it-autoflight/internal/vert-speed-fpm</input>
|
|
<output>/it-autoflight/internal/target-fpm-d</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>NAV1 G/S FPM Calc</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>/instrumentation/nav[0]/gs-rate-of-climb-fpm</input>
|
|
<output>/it-autoflight/internal/nav1-rate-of-climb-fpm</output>
|
|
<min>
|
|
<condition>
|
|
<not-equals>
|
|
<property>/options/steep-ils</property>
|
|
<value>1</value>
|
|
</not-equals>
|
|
</condition>
|
|
<value>-1200</value>
|
|
</min>
|
|
<min>
|
|
<condition>
|
|
<equals>
|
|
<property>/options/steep-ils</property>
|
|
<value>1</value>
|
|
</equals>
|
|
</condition>
|
|
<value>-2200</value>
|
|
</min>
|
|
<max>0</max>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>HEADING PREDICTOR STAGE 1</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>
|
|
<condition>
|
|
<equals>
|
|
<property>/it-autoflight/input/trk</property>
|
|
<value>0</value>
|
|
</equals>
|
|
</condition>
|
|
<expression>
|
|
<sum>
|
|
<div>
|
|
<property>/orientation/roll-deg</property>
|
|
<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>
|
|
</div>
|
|
<property>/it-autoflight/internal/heading-deg</property>
|
|
</sum>
|
|
</expression>
|
|
</input>
|
|
<input>
|
|
<condition>
|
|
<equals>
|
|
<property>/it-autoflight/input/trk</property>
|
|
<value>1</value>
|
|
</equals>
|
|
</condition>
|
|
<expression>
|
|
<sum>
|
|
<div>
|
|
<property>/orientation/roll-deg</property>
|
|
<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>
|
|
</div>
|
|
<property>/it-autoflight/internal/track-deg</property>
|
|
</sum>
|
|
</expression>
|
|
</input>
|
|
<output>/it-autoflight/internal/heading-predicted-cmd</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>HEADING PREDICTOR STAGE 2</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>
|
|
<condition>
|
|
<greater-than>
|
|
<property>/it-autoflight/internal/heading-predicted-cmd</property>
|
|
<value>360</value>
|
|
</greater-than>
|
|
</condition>
|
|
<expression>
|
|
<dif>
|
|
<property>/it-autoflight/internal/heading-predicted-cmd</property>
|
|
<value>360</value>
|
|
</dif>
|
|
</expression>
|
|
</input>
|
|
<input>
|
|
<condition>
|
|
<less-than>
|
|
<property>/it-autoflight/internal/heading-predicted-cmd</property>
|
|
<value>0.5</value>
|
|
</less-than>
|
|
</condition>
|
|
<expression>
|
|
<sum>
|
|
<property>/it-autoflight/internal/heading-predicted-cmd</property>
|
|
<value>360</value>
|
|
</sum>
|
|
</expression>
|
|
</input>
|
|
<input>/it-autoflight/internal/heading-predicted-cmd</input>
|
|
<output>/it-autoflight/internal/heading-predicted</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>ALTITUDE PREDICTOR</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>
|
|
<expression>
|
|
<sum>
|
|
<div>
|
|
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
|
<value>5</value>
|
|
</div>
|
|
<property>/instrumentation/altimeter/indicated-altitude-ft</property>
|
|
</sum>
|
|
</expression>
|
|
</input>
|
|
<output>/it-autoflight/internal/altitude-predicted</output>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>INTERNAL FPA COMPUTER</name>
|
|
<debug>false</debug>
|
|
<type>gain</type>
|
|
<gain>1.0</gain>
|
|
<input>
|
|
<expression>
|
|
<dif>
|
|
<property>/orientation/pitch-deg</property>
|
|
<property>/orientation/alpha-deg</property>
|
|
</dif>
|
|
</expression>
|
|
</input>
|
|
<output>/it-autoflight/internal/fpa</output>
|
|
</filter>
|
|
|
|
<!-- Flight Director -->
|
|
|
|
<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-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>
|
|
<property>/it-autoflight/internal/target-roll-fd</property>
|
|
<property>/orientation/roll-deg</property>
|
|
</dif>
|
|
</expression>
|
|
</input>
|
|
<output>/it-autoflight/fd/roll-bar</output>
|
|
<min>-30</min>
|
|
<max>30</max>
|
|
</filter>
|
|
|
|
<filter>
|
|
<name>FD: PITCH</name>
|
|
<debug>false</debug>
|
|
<type>noise-spike</type>
|
|
<input>
|
|
<expression>
|
|
<product>
|
|
<dif>
|
|
<property>/it-autoflight/internal/target-common-fpm</property>
|
|
<property>/it-autoflight/internal/vert-speed-fpm</property>
|
|
</dif>
|
|
<table>
|
|
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
|
|
<entry><ind>0.20</ind><dep>0.004</dep></entry>
|
|
<entry><ind>0.95</ind><dep>0.002</dep></entry>
|
|
</table>
|
|
</product>
|
|
</expression>
|
|
</input>
|
|
<output>/it-autoflight/fd/pitch-bar</output>
|
|
<min>-15</min>
|
|
<max>30</max>
|
|
<max-rate-of-change>10</max-rate-of-change>
|
|
</filter>
|
|
|
|
</PropertyList>
|