From 85506fa5244c9923c8b6d6e49bfb4a4ed5f14e9d Mon Sep 17 00:00:00 2001 From: PX4BuildBot Date: Mon, 3 Jul 2023 08:41:32 +0000 Subject: [PATCH] Update PX4 Firmware metadata Mon Jul 3 08:41:32 UTC 2023 --- .../PX4/PX4ParameterFactMetaData.xml | 24 +++++++++++----------- 1 file changed, 12 insertions(+), 12 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 8eaafd2..a78627e 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -5100,10 +5100,10 @@ s 2 - + Maximum downwards acceleration in climb rate controlled modes - 2.0 - 15.0 + 2 + 15 m/s^2 1 1 @@ -5126,10 +5126,10 @@ 2 1 - + Maximum upwards acceleration in climb rate controlled modes - 2.0 - 15.0 + 2 + 15 m/s^2 1 1 @@ -5245,8 +5245,8 @@ Minimum collective thrust in Stabilized mode The value is mapped to the lowest throttle stick position in Stabilized mode. Too low collective thrust leads to loss of roll/pitch/yaw torque control authority. Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE). - 0.0 - 1.0 + 0 + 1 norm 2 0.01 @@ -5270,8 +5270,8 @@ Manual yaw rate input filter time constant Not used in Stabilized mode Setting this parameter to 0 disables the filter - 0.0 - 5.0 + 0 + 5 s 2 0.01 @@ -5323,7 +5323,7 @@ Horizontal thrust margin Margin that is kept for horizontal control when higher priority vertical thrust is saturated. To avoid completely starving horizontal control with high vertical error. - 0.0 + 0 0.5 norm 2 @@ -5367,7 +5367,7 @@ Numerical velocity derivative low pass cutoff frequency - 0.0 + 0 10 Hz 1