diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index dc727fd..79855cb 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)