From 1513ec55ba3209f0933a6479613b93b6ad8375da Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Fri, 23 Mar 2018 00:37:06 -0400 Subject: [PATCH] Update PX4 Firmware metadata Fri Mar 23 00:37:06 EDT 2018 --- .../PX4/PX4ParameterFactMetaData.xml | 50 +++++++++++++++++-- 1 file changed, 45 insertions(+), 5 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 4fd9a8141b..543dbcf88d 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -9524,11 +9524,6 @@ tailsitter, tiltrotor: main throttle 1 modules/vtol_att_control - - Optimal recovery strategy for pitch-weak tailsitters - - modules/vtol_att_control - Defines the time window during which the pusher throttle will be ramped up linearly to VT_F_TRANS_THR during a transition to fixed wing mode. Zero or negative values will produce an instant throttle rise to VT_F_TRANS_THR @@ -9611,6 +9606,51 @@ to fixed wing mode. Zero or negative values will produce an instant throttle ris modules/vtol_att_control + + + Gate size for true sideslip fusion + Sets the number of standard deviations used by the innovation consistency test. + 1 + 5 + SD + modules/wind_estimator + + + Wind estimator sideslip measurement noise + 0 + 1 + rad + modules/wind_estimator + + + Wind estimator true airspeed scale process noise + 0 + 0.1 + modules/wind_estimator + + + Gate size for true airspeed fusion + Sets the number of standard deviations used by the innovation consistency test. + 1 + 5 + SD + modules/wind_estimator + + + Wind estimator true airspeed measurement noise + 0 + 4 + m/s + modules/wind_estimator + + + Wind estimator wind process noise + 0 + 1 + m/s/s + modules/wind_estimator + + EXFW_HDNG_P -- GitLab