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Update PX4 Firmware metadata Fri Nov 25 21:28:27 UTC 2022

QGC4.4
PX4BuildBot 2 years ago
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8463a9d629
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b6935630e2
1 changed files with 69 additions and 29 deletions
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  1. 98
      src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml

98
src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
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@ -3107,7 +3107,7 @@ @@ -3107,7 +3107,7 @@
<parameter name="FW_LND_FL_PMIN" default="2.5" type="FLOAT">
<short_desc>Flare, minimum pitch</short_desc>
<long_desc>Minimum pitch during flare, a positive sign means nose up Applied once flaring is triggered</long_desc>
<min>0</min>
<min>-5</min>
<max>15.0</max>
<unit>deg</unit>
<decimal>1</decimal>
@ -3117,9 +3117,9 @@ @@ -3117,9 +3117,9 @@
<short_desc>Landing flare sink rate</short_desc>
<long_desc>TECS will attempt to control the aircraft to this sink rate via pitch angle (throttle killed during flare)</long_desc>
<min>0.0</min>
<max>1.0</max>
<max>2</max>
<unit>m/s</unit>
<decimal>1</decimal>
<decimal>2</decimal>
<increment>0.1</increment>
</parameter>
<parameter name="FW_LND_FL_TIME" default="1.0" type="FLOAT">
@ -3252,18 +3252,28 @@ @@ -3252,18 +3252,28 @@
</parameter>
</group>
<group name="FW Launch detection">
<parameter name="LAUN_ALL_ON" default="0" type="INT32" boolean="true">
<short_desc>Launch detection</short_desc>
<parameter name="FW_LAUN_AC_T" default="0.05" type="FLOAT">
<short_desc>Trigger time</short_desc>
<long_desc>Launch is detected when acceleration in body forward direction is above FW_LAUN_AC_THLD for FW_LAUN_AC_T seconds.</long_desc>
<min>0.0</min>
<max>5.0</max>
<unit>s</unit>
<decimal>2</decimal>
<increment>0.05</increment>
</parameter>
<parameter name="LAUN_CAT_A" default="30.0" type="FLOAT">
<short_desc>Catapult accelerometer threshold</short_desc>
<long_desc>LAUN_CAT_A for LAUN_CAT_T serves as threshold to trigger launch detection.</long_desc>
<parameter name="FW_LAUN_AC_THLD" default="30.0" type="FLOAT">
<short_desc>Trigger acceleration threshold</short_desc>
<long_desc>Launch is detected when acceleration in body forward direction is above FW_LAUN_AC_THLD for FW_LAUN_AC_T seconds.</long_desc>
<min>0</min>
<unit>m/s^2</unit>
<decimal>1</decimal>
<increment>0.5</increment>
</parameter>
<parameter name="LAUN_CAT_MDEL" default="0.0" type="FLOAT">
<parameter name="FW_LAUN_DETCN_ON" default="0" type="INT32" boolean="true">
<short_desc>FW Launch detection</short_desc>
<long_desc>Enables automatic launch detection based on measured acceleration. Use for hand- or catapult-launched vehicles. Only available for fixed-wing vehicles. Not compatible with runway takeoff.</long_desc>
</parameter>
<parameter name="FW_LAUN_MOT_DEL" default="0.0" type="FLOAT">
<short_desc>Motor delay</short_desc>
<long_desc>Delay between starting attitude control and powering up the throttle (giving throttle control to the controller) Before this timespan is up the throttle will be set to FW_THR_IDLE, set to 0 to deactivate</long_desc>
<min>0.0</min>
@ -3272,24 +3282,6 @@ @@ -3272,24 +3282,6 @@
<decimal>1</decimal>
<increment>0.5</increment>
</parameter>
<parameter name="LAUN_CAT_PMAX" default="30.0" type="FLOAT">
<short_desc>Maximum pitch before the throttle is powered up (during motor delay phase)</short_desc>
<long_desc>This is an extra limit for the maximum pitch which is imposed in the phase before the throttle turns on. This allows to limit the maximum pitch angle during a bungee launch (make the launch less steep).</long_desc>
<min>0.0</min>
<max>45.0</max>
<unit>deg</unit>
<decimal>1</decimal>
<increment>0.5</increment>
</parameter>
<parameter name="LAUN_CAT_T" default="0.05" type="FLOAT">
<short_desc>Catapult time threshold</short_desc>
<long_desc>LAUN_CAT_A for LAUN_CAT_T serves as threshold to trigger launch detection.</long_desc>
<min>0.0</min>
<max>5.0</max>
<unit>s</unit>
<decimal>2</decimal>
<increment>0.05</increment>
</parameter>
</group>
<group name="FW NPFG Control">
<parameter name="FW_USE_NPFG" default="0" type="INT32" boolean="true">
@ -4052,6 +4044,14 @@ @@ -4052,6 +4044,14 @@
<unit>m/s</unit>
<decimal>1</decimal>
</parameter>
<parameter name="LNDFW_TRIG_TIME" default="2." type="FLOAT">
<short_desc>Fixed-wing land detection trigger time</short_desc>
<long_desc>Time the land conditions (speeds and acceleration) have to be satisfied to detect a landing.</long_desc>
<min>0.1</min>
<unit>s</unit>
<decimal>1</decimal>
<reboot_required>true</reboot_required>
</parameter>
<parameter name="LNDFW_VEL_XY_MAX" default="5.0" type="FLOAT">
<short_desc>Fixed-wing land detector: Max horizontal velocity threshold</short_desc>
<long_desc>Maximum horizontal velocity allowed in the landed state. A factor of 0.7 is applied in case of airspeed-less flying (either because no sensor is present or sensor data got invalid in flight).</long_desc>
@ -4060,9 +4060,9 @@ @@ -4060,9 +4060,9 @@
<unit>m/s</unit>
<decimal>1</decimal>
</parameter>
<parameter name="LNDFW_VEL_Z_MAX" default="2.0" type="FLOAT">
<parameter name="LNDFW_VEL_Z_MAX" default="1.0" type="FLOAT">
<short_desc>Fixed-wing land detector: Max vertiacal velocity threshold</short_desc>
<long_desc>Maximum vertical velocity allowed in the landed state. A factor of 0.7 is applied in case of airspeed-less flying (either because no sensor is present or sensor data got invalid in flight).</long_desc>
<long_desc>Maximum vertical velocity allowed in the landed state.</long_desc>
<min>0.1</min>
<max>20</max>
<unit>m/s</unit>
@ -8205,6 +8205,41 @@ @@ -8205,6 +8205,41 @@
<value code="400">400 Hz</value>
</values>
</parameter>
<parameter name="INA220_CONFIG" default="8607" type="INT32">
<short_desc>INA220 Power Monitor Config</short_desc>
<min>0</min>
<max>65535</max>
<decimal>1</decimal>
<increment>1</increment>
</parameter>
<parameter name="INA220_CUR_BAT" default="164.0" type="FLOAT">
<short_desc>INA220 Power Monitor Battery Max Current</short_desc>
<min>0.1</min>
<max>500.0</max>
<decimal>2</decimal>
<increment>0.1</increment>
</parameter>
<parameter name="INA220_CUR_REG" default="164.0" type="FLOAT">
<short_desc>INA220 Power Monitor Regulator Max Current</short_desc>
<min>0.1</min>
<max>500.0</max>
<decimal>2</decimal>
<increment>0.1</increment>
</parameter>
<parameter name="INA220_SHUNT_BAT" default="0.0005" type="FLOAT">
<short_desc>INA220 Power Monitor Battery Shunt</short_desc>
<min>0.000000001</min>
<max>0.1</max>
<decimal>10</decimal>
<increment>.000000001</increment>
</parameter>
<parameter name="INA220_SHUNT_REG" default="0.0005" type="FLOAT">
<short_desc>INA220 Power Monitor Regulator Shunt</short_desc>
<min>0.000000001</min>
<max>0.1</max>
<decimal>10</decimal>
<increment>.000000001</increment>
</parameter>
<parameter name="INA226_CONFIG" default="18139" type="INT32">
<short_desc>INA226 Power Monitor Config</short_desc>
<min>0</min>
@ -8374,6 +8409,11 @@ @@ -8374,6 +8409,11 @@
<short_desc>Eagle Tree airspeed sensor (external I2C)</short_desc>
<reboot_required>true</reboot_required>
</parameter>
<parameter name="SENS_EN_INA220" default="0" type="INT32" boolean="true">
<short_desc>Enable INA220 Power Monitor</short_desc>
<long_desc>For systems a INA220 Power Monitor, this should be set to true</long_desc>
<reboot_required>true</reboot_required>
</parameter>
<parameter name="SENS_EN_INA226" default="0" type="INT32" boolean="true">
<short_desc>Enable INA226 Power Monitor</short_desc>
<long_desc>For systems a INA226 Power Monitor, this should be set to true</long_desc>

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