uint32 control_mode_flags # Bitmask to indicate EKF logic state
# 0 - true if the filter tilt alignment is complete
@ -41,6 +42,9 @@ uint32 control_mode_flags # Bitmask to indicate EKF logic state
@@ -41,6 +42,9 @@ uint32 control_mode_flags # Bitmask to indicate EKF logic state
# 14 - true when height data from external vision measurements is being fused
# 15 - true when synthetic sideslip measurements are being fused
# 16 - true when only the magnetic field states are updated by the magnetometer
# 17 - true when the vehicle is operating as a fixed wing vehicle
# 18 - true when the magnetomer has been declared faulty and is no longer being used
# 19 - true when airspeed measurements are being fused
uint16 filter_fault_flags # Bitmask to indicate EKF internal faults
# 0 - true if the fusion of the magnetometer X-axis has encountered a numerical error
@ -95,6 +99,7 @@ uint16 solution_status_flags # Bitmask indicating which filter kinematic state o
@@ -95,6 +99,7 @@ uint16 solution_status_flags # Bitmask indicating which filter kinematic state o
# 8 - True if the EKF has sufficient data to enter a mode that will provide a (relative) position estimate
# 9 - True if the EKF has sufficient data to enter a mode that will provide a (absolute) position estimate
# 10 - True if the EKF has detected a GPS glitch
# 11 - True if the EKF has detected bad accelerometer data
float32 time_slip # cumulative amount of time in seconds that the EKF inertial calculation has slipped relative to system time