From 37cb521c4310511a004c51041f4823cfe9d92f74 Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Wed, 23 May 2018 00:37:06 -0400 Subject: [PATCH] Update PX4 Firmware metadata Wed May 23 00:37:06 EDT 2018 --- src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml | 5 ++++ .../PX4/PX4ParameterFactMetaData.xml | 32 ++++++++++++++++------ 2 files changed, 29 insertions(+), 8 deletions(-) diff --git a/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml b/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml index adcbccd..c762c5d 100644 --- a/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml +++ b/src/AutoPilotPlugins/PX4/AirframeFactMetaData.xml @@ -329,6 +329,11 @@ Michael Schaeuble Quadrotor x + + Copter + Lorenz Meier <lorenz@px4.io> + Quadrotor x + Copter Thomas Gubler <thomas@px4.io> diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 6425236..eee5b8e 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -199,6 +199,7 @@ Set to 2 to use heading from motion capture Complimentary filter magnetometer weight + Set to 0 to avoid using the magnetometer. 0 1 2 @@ -2159,7 +2160,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi Maximum negative / down pitch rate - 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. + This limits the maximum pitch down up angular rate the controller will output (in degrees per second). 0.0 90.0 deg/s @@ -2169,7 +2170,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi Maximum positive / up pitch rate - This limits the maximum pitch up angular rate the controller will output (in degrees per second). Setting a value of zero disables the limit. + This limits the maximum pitch up angular rate the controller will output (in degrees per second). 0.0 90.0 deg/s @@ -2255,7 +2256,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi Maximum roll rate - This limits the maximum roll rate the controller will output (in degrees per second). Setting a value of zero disables the limit. + This limits the maximum roll rate the controller will output (in degrees per second). 0.0 90.0 deg/s @@ -2317,9 +2318,9 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi modules/fw_att_control - + Maximum wheel steering rate - This limits the maximum wheel steering rate the controller will output (in degrees per second). Setting a value of zero disables the limit. + This limits the maximum wheel steering rate the controller will output (in degrees per second). 0.0 90.0 deg/s @@ -2337,7 +2338,7 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi 0.05 modules/fw_att_control - + Yaw rate integrator gain This gain defines how much control response will result out of a steady state error. It trims any constant error. 0.0 @@ -2366,9 +2367,9 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi 0.005 modules/fw_att_control - + Maximum yaw rate - This limits the maximum yaw rate the controller will output (in degrees per second). Setting a value of zero disables the limit. + This limits the maximum yaw rate the controller will output (in degrees per second). 0.0 90.0 deg/s @@ -8592,6 +8593,7 @@ This is used for gathering replay logs for the ekf2 module ESP8266 (921600 baud, 8N1) Normal Telemetry (115200 baud, 8N1) Minimal Telemetry (115200 baud, 8N1) + RTPS Client (460800 baud) @@ -8601,6 +8603,20 @@ This is used for gathering replay logs for the ekf2 module true drivers/px4fmu + + Control if the vehicle has a barometer + 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. + + true + modules/systemlib + + + Control if the vehicle has a magnetometer + 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. + + true + modules/systemlib + Enable HITL mode on next boot 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.