Patent ID: 11952142
Assignee: HONEYWELL INTERNATIONAL INC.
Field: Control (Instruments)
Classification: CPC B  G | IPC B  G

Claim 6:
7. The method of claim 1, comprising:
determining, via the at least one processor, at the future time that the at least one avionics data source is considered to be in the anomalous condition when the major anomaly threshold has been crossed;
depicting, on the display device, a failure flag depicting an anomalous status flag for the at least one avionics data source at the future time;
predicting, via the at least one processor, a second time following the future time when a functioning threshold will be crossed based on the time series data received at the second time, the second time representing when the at least one avionics data source will be deemed no longer anomalous and functioning; and
depicting, on the display device associated with the aircraft, the second time when the functioning threshold will be crossed.