diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index dc727fdd4362de4fd48baa2a152334edd2187fa1..79855cb9e658175f6ca567df6b4c7a7862da7fe5 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -1227,6 +1227,14 @@ Set -1 to disable the check s 0.1 + + Timeout for detecting a failure after takeoff + A non-zero, positive value specifies the timeframe in seconds within failure detector is allowed to put the vehicle into a lockdown state if attitude exceeds the limits defined in FD_FAIL_P and FD_FAIL_R. The check is not executed for flight modes that do support acrobatic maneuvers, e.g: Acro (MC/FW), Rattitude and Manual (FW). A zero or negative value means that the check is disabled. + -1.0 + 5.0 + s + 3 + Battery failsafe mode Action the system takes at critical battery. See also BAT_CRIT_THR and BAT_EMERGEN_THR for definition of battery states. @@ -3152,6 +3160,12 @@ Set to 0 to disable heading hold + + 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 AUX5 or MAIN5 (depending on board) for engaging failsafe from an external automatic trigger system (ATS)