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Commit 37cb521c authored by PX4 Jenkins's avatar PX4 Jenkins Committed by Daniel Agar
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Update PX4 Firmware metadata Wed May 23 00:37:06 EDT 2018

parent b79d884c
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Showing with 29 additions and 8 deletions
src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml
View file @ 37cb521c
......@@ -329,6 +329,11 @@
<maintainer>Michael Schaeuble</maintainer>
<type>Quadrotor x</type>
</airframe>
<airframe id="4014" maintainer="Lorenz Meier &lt;lorenz@px4.io&gt;" name="S500">
<class>Copter</class>
<maintainer>Lorenz Meier &lt;lorenz@px4.io&gt;</maintainer>
<type>Quadrotor x</type>
</airframe>
<airframe id="4020" maintainer="Thomas Gubler &lt;thomas@px4.io&gt;" name="Hobbyking Micro PCB">
<class>Copter</class>
<maintainer>Thomas Gubler &lt;thomas@px4.io&gt;</maintainer>
......
src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
View file @ 37cb521c
......@@ -199,6 +199,7 @@ Set to 2 to use heading from motion capture</short_desc>
</parameter>
<parameter default="0.1" name="ATT_W_MAG" type="FLOAT">
<short_desc>Complimentary filter magnetometer weight</short_desc>
<long_desc>Set to 0 to avoid using the magnetometer.</long_desc>
<min>0</min>
<max>1</max>
<decimal>2</decimal>
......@@ -2159,7 +2160,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
</parameter>
<parameter default="60.0" name="FW_P_RMAX_NEG" type="FLOAT">
<short_desc>Maximum negative / down pitch rate</short_desc>
<long_desc>This limits the maximum pitch down up angular rate the controller will output (in degrees per second). Setting a value of zero disables the limit.</long_desc>
<long_desc>This limits the maximum pitch down up angular rate the controller will output (in degrees per second).</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg/s</unit>
......@@ -2169,7 +2170,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
</parameter>
<parameter default="60.0" name="FW_P_RMAX_POS" type="FLOAT">
<short_desc>Maximum positive / up pitch rate</short_desc>
<long_desc>This limits the maximum pitch up angular rate the controller will output (in degrees per second). Setting a value of zero disables the limit.</long_desc>
<long_desc>This limits the maximum pitch up angular rate the controller will output (in degrees per second).</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg/s</unit>
......@@ -2255,7 +2256,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
</parameter>
<parameter default="70.0" name="FW_R_RMAX" type="FLOAT">
<short_desc>Maximum roll rate</short_desc>
<long_desc>This limits the maximum roll rate the controller will output (in degrees per second). Setting a value of zero disables the limit.</long_desc>
<long_desc>This limits the maximum roll rate the controller will output (in degrees per second).</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg/s</unit>
......@@ -2317,9 +2318,9 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<boolean />
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_W_RMAX" type="FLOAT">
<parameter default="30.0" name="FW_W_RMAX" type="FLOAT">
<short_desc>Maximum wheel steering rate</short_desc>
<long_desc>This limits the maximum wheel steering rate the controller will output (in degrees per second). Setting a value of zero disables the limit.</long_desc>
<long_desc>This limits the maximum wheel steering rate the controller will output (in degrees per second).</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg/s</unit>
......@@ -2337,7 +2338,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<increment>0.05</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_YR_I" type="FLOAT">
<parameter default="0.01" name="FW_YR_I" type="FLOAT">
<short_desc>Yaw rate integrator gain</short_desc>
<long_desc>This gain defines how much control response will result out of a steady state error. It trims any constant error.</long_desc>
<min>0.0</min>
......@@ -2366,9 +2367,9 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<increment>0.005</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_Y_RMAX" type="FLOAT">
<parameter default="50.0" name="FW_Y_RMAX" type="FLOAT">
<short_desc>Maximum yaw rate</short_desc>
<long_desc>This limits the maximum yaw rate the controller will output (in degrees per second). Setting a value of zero disables the limit.</long_desc>
<long_desc>This limits the maximum yaw rate the controller will output (in degrees per second).</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg/s</unit>
......@@ -8592,6 +8593,7 @@ This is used for gathering replay logs for the ekf2 module</short_desc>
<value code="1921600">ESP8266 (921600 baud, 8N1)</value>
<value code="3115200">Normal Telemetry (115200 baud, 8N1)</value>
<value code="5115200">Minimal Telemetry (115200 baud, 8N1)</value>
<value code="6460800">RTPS Client (460800 baud)</value>
</values>
</parameter>
<parameter default="0" name="SYS_FMU_TASK" type="INT32">
......@@ -8601,6 +8603,20 @@ This is used for gathering replay logs for the ekf2 module</short_desc>
<reboot_required>true</reboot_required>
<scope>drivers/px4fmu</scope>
</parameter>
<parameter default="1" name="SYS_HAS_BARO" type="INT32">
<short_desc>Control if the vehicle has a barometer</short_desc>
<long_desc>Disable this if the board has no barometer, such as some of the the Omnibus F4 SD variants. If disabled, the preflight checks will not check for the presence of a barometer.</long_desc>
<boolean />
<reboot_required>true</reboot_required>
<scope>modules/systemlib</scope>
</parameter>
<parameter default="1" name="SYS_HAS_MAG" type="INT32">
<short_desc>Control if the vehicle has a magnetometer</short_desc>
<long_desc>Disable this if the board has no magnetometer, such as the Omnibus F4 SD. If disabled, the preflight checks will not check for the presence of a magnetometer.</long_desc>
<boolean />
<reboot_required>true</reboot_required>
<scope>modules/systemlib</scope>
</parameter>
<parameter default="0" name="SYS_HITL" type="INT32">
<short_desc>Enable HITL mode on next boot</short_desc>
<long_desc>While enabled the system will boot in HITL mode and not enable all sensors and checks. When disabled the same vehicle can be normally flown outdoors.</long_desc>
......
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