From b6935630e2737f24d43a88003284f0f4bb4c5973 Mon Sep 17 00:00:00 2001 From: PX4BuildBot Date: Fri, 25 Nov 2022 21:28:27 +0000 Subject: [PATCH] Update PX4 Firmware metadata Fri Nov 25 21:28:27 UTC 2022 --- .../PX4/PX4ParameterFactMetaData.xml | 98 +++++++++++++++------- 1 file changed, 69 insertions(+), 29 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 0f32a03..ec007b0 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -3107,7 +3107,7 @@ Flare, minimum pitch Minimum pitch during flare, a positive sign means nose up Applied once flaring is triggered - 0 + -5 15.0 deg 1 @@ -3117,9 +3117,9 @@ Landing flare sink rate TECS will attempt to control the aircraft to this sink rate via pitch angle (throttle killed during flare) 0.0 - 1.0 + 2 m/s - 1 + 2 0.1 @@ -3252,18 +3252,28 @@ - - Launch detection + + Trigger time + Launch is detected when acceleration in body forward direction is above FW_LAUN_AC_THLD for FW_LAUN_AC_T seconds. + 0.0 + 5.0 + s + 2 + 0.05 - - Catapult accelerometer threshold - LAUN_CAT_A for LAUN_CAT_T serves as threshold to trigger launch detection. + + Trigger acceleration threshold + Launch is detected when acceleration in body forward direction is above FW_LAUN_AC_THLD for FW_LAUN_AC_T seconds. 0 m/s^2 1 0.5 - + + FW Launch detection + 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. + + Motor delay 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 0.0 @@ -3272,24 +3282,6 @@ 1 0.5 - - Maximum pitch before the throttle is powered up (during motor delay phase) - 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). - 0.0 - 45.0 - deg - 1 - 0.5 - - - Catapult time threshold - LAUN_CAT_A for LAUN_CAT_T serves as threshold to trigger launch detection. - 0.0 - 5.0 - s - 2 - 0.05 - @@ -4052,6 +4044,14 @@ m/s 1 + + Fixed-wing land detection trigger time + Time the land conditions (speeds and acceleration) have to be satisfied to detect a landing. + 0.1 + s + 1 + true + Fixed-wing land detector: Max horizontal velocity threshold 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). @@ -4060,9 +4060,9 @@ m/s 1 - + Fixed-wing land detector: Max vertiacal velocity threshold - 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). + Maximum vertical velocity allowed in the landed state. 0.1 20 m/s @@ -8205,6 +8205,41 @@ 400 Hz + + INA220 Power Monitor Config + 0 + 65535 + 1 + 1 + + + INA220 Power Monitor Battery Max Current + 0.1 + 500.0 + 2 + 0.1 + + + INA220 Power Monitor Regulator Max Current + 0.1 + 500.0 + 2 + 0.1 + + + INA220 Power Monitor Battery Shunt + 0.000000001 + 0.1 + 10 + .000000001 + + + INA220 Power Monitor Regulator Shunt + 0.000000001 + 0.1 + 10 + .000000001 + INA226 Power Monitor Config 0 @@ -8374,6 +8409,11 @@ Eagle Tree airspeed sensor (external I2C) true + + Enable INA220 Power Monitor + For systems a INA220 Power Monitor, this should be set to true + true + Enable INA226 Power Monitor For systems a INA226 Power Monitor, this should be set to true