From 3d18ce8999ec67a704aa38f88805bc935e05d7ce Mon Sep 17 00:00:00 2001 From: PX4BuildBot Date: Sat, 14 Aug 2021 19:14:46 +0000 Subject: [PATCH] Update PX4 Firmware metadata Sat Aug 14 19:14:46 UTC 2021 --- src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml | 14 +++++ .../PX4/PX4ParameterFactMetaData.xml | 71 ++++++++++++++++------ 2 files changed, 65 insertions(+), 20 deletions(-) diff --git a/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml b/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml index 94263d3..60bd155 100644 --- a/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml +++ b/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml @@ -433,6 +433,15 @@ James Goppert <james.goppert@gmail.com> Quadrotor x + + Copter + + Quadrotor x + motor 1 + motor 2 + motor 3 + motor 4 + Copter Hyon Lim <lim@uvify.com> @@ -709,6 +718,11 @@ flaps gear + + Plane + Romain Chiappinelli <romain.chiap@gmail.com> + Simulation + diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 37f0bc0..ebe6796 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -716,7 +716,6 @@ norm 2 0.01 - true Emergency threshold @@ -726,7 +725,6 @@ norm 2 0.01 - true Low threshold @@ -736,7 +734,6 @@ norm 2 0.01 - true This parameter is deprecated. Please use BAT1_N_CELLS instead @@ -928,7 +925,6 @@ Setting this parameter to 22027 will disable IO safety. WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK 0 22027 - true Circuit breaker for rate controller output @@ -942,28 +938,24 @@ Setting this parameter to 894281 will disable the power valid checks in the commander. WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK 0 894281 - true Circuit breaker for USB link check Setting this parameter to 197848 will disable the USB connected checks in the commander, setting it to 0 keeps them enabled (recommended). We are generally recommending to not fly with the USB link connected and production vehicles should set this parameter to zero to prevent users from flying USB powered. However, for R&D purposes it has proven over the years to work just fine. 0 197848 - true Circuit breaker for position error check Setting this parameter to 201607 will disable the position and velocity accuracy checks in the commander. WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK 0 201607 - true Circuit breaker for arming in fixed-wing mode check Setting this parameter to 159753 will enable arming in fixed-wing mode for VTOLs. WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK 0 159753 - true @@ -1392,7 +1384,6 @@ 1 100 s - true Horizontal position error threshold @@ -1415,7 +1406,6 @@ 1 100 s - true Required number of redundant power modules @@ -2806,6 +2796,23 @@ 3 + + + Required esc bootloader version + 0 + 65535 + + + Required esc firmware version + 0 + 65535 + + + Required esc hardware version + 0 + 65535 + + RC Loss Alarm @@ -3688,7 +3695,6 @@ Enable checks on ESCs that report their arming state If enabled, failure detector will verify that all the ESCs have successfully armed when the vehicle has transitioned to the armed state. Timeout for receiving an acknowledgement from the ESCs is 0.3s, if no feedback is received the failure detector will auto disarm the vehicle. - true Enable PWM input on for engaging failsafe from an external automatic trigger system (ATS) @@ -3855,13 +3861,14 @@ - Dump GPS communication to a file - If this is set to 1, all GPS communication data will be published via uORB, and written to the log file as gps_dump message. + Log GPS communication data + If this is set to 1, all GPS communication data will be published via uORB, and written to the log file as gps_dump message. If this is set to 2, the main GPS is configured to output RTCM data, which is then logged as gps_dump and can be used for PPK. 0 - 1 + 2 Disable - Enable + Full communication + RTCM output (PPK) @@ -4156,7 +4163,7 @@ Landing target measurement uncertainty - Variance of the landing target measurement from the driver. Higher values results in less agressive following of the measurement and a smoother output as well as fewer rejected measurements. + Variance of the landing target measurement from the driver. Higher values result in less aggressive following of the measurement and a smoother output as well as fewer rejected measurements. tan(rad)^2 4 @@ -4191,7 +4198,7 @@ Initial landing target velocity uncertainty - Initial variance of the relative landing target velocity in x and y direction + Initial variance of the relative landing target velocity in x and y directions 0.001 (m/s)^2 3 @@ -4443,7 +4450,7 @@ 4 - Vision delay compensaton + Vision delay compensation Set to zero to enable automatic compensation from measurement timestamps 0 0.1 @@ -4795,7 +4802,7 @@ Maximal horizontal distance from home to first waypoint - Failsafe check to prevent running mission stored from previous flight at a new takeoff location. Set a value of zero or less to disable. The mission will not be started if the current waypoint is more distant than MIS_DIS_1WP from the home position. + Failsafe check to prevent running mission stored from previous flight at a new takeoff location. Set a value of zero or less to disable. The mission will not be started if the current waypoint is more distant than MIS_DIST_1WP from the home position. 0 10000 m @@ -7154,7 +7161,7 @@ Maximum number of search attempts - Maximum number of times to seach for the landing target if it is lost during the precision landing. + Maximum number of times to search for the landing target if it is lost during the precision landing. 0 100 @@ -10731,6 +10738,10 @@ SMBUS Smart battery driver BQ40Z50 and BQ40Z80 true + + Eagle Tree airspeed sensor (external I2C) + true + Lidar-Lite (LL40LS) 0 @@ -10756,6 +10767,14 @@ Autodetect + + TE MS4525 differential pressure sensor (external I2C) + true + + + TE MS5525 differential pressure sensor (external I2C) + true + PAW3902 & PAW3903 Optical Flow true @@ -10772,6 +10791,10 @@ PX4 Flow Optical Flow true + + Sensirion SDP3X differential pressure sensor (external I2C) + true + Lightware Laser Rangefinder hardware model (serial) true @@ -12010,6 +12033,14 @@ the time taken for the thruster to step from 0 to 100% should be about 4 times tau s + + Vehicle type + true + + MC + FW + +