Methods and systems for depicting avionics data anomalies

Patent metadata

Field	Value
Publication number	US-11952142-B2
Application number	US-202117315785-A
Country	US
Kind code	B2
Filing date	May 10, 2021
Priority date	May 10, 2021
Publication date	Apr 9, 2024
Grant date	Apr 9, 2024

Abstract

Methods and systems for depicting avionics data anomalies in an aircraft. Time series data is received from the avionics data source, a future time is predicted when a first anomaly threshold will be crossed based on the time series data, and the future time when the first anomaly threshold will be crossed is depicted on a display device associated with the aircraft.

First claim

What is claimed is:

1. A method for depicting avionics data anomalies in an aircraft, the method comprising:
receiving, via at least one processor, current time series data from at least one avionics data source;
determining current anomaly metric data based on the current time series data; and
upon a determination that the current anomaly metric data crosses a minor anomaly threshold:
predicting, via the at least one processor, a future time when a major anomaly threshold will be crossed by future anomaly metric data associated with future time series data received at the future time based on an extrapolation of the current time series data; and
depicting, on a display device associated with the aircraft, an indication that the at least one avionics data source will be considered to be in an anomalous condition at the future time when the major anomaly threshold will be crossed.

2. The method of claim 1 , wherein the predicting step provides a time uncertainty associated with the future time when the major anomaly threshold will be crossed and wherein the depicting step includes depicting the future time when the major anomaly threshold will be crossed and the time uncertainty.

3. The method of claim 2 , wherein the time uncertainty is depicted using one or more error bars.

4. The method of claim 1 , wherein the depicting step includes depicting an anomaly flag on a time scale, wherein the position of the anomaly flag on the time scale is set based on the future time.

5. The method of claim 4 , wherein the time scale auto-scales as the future time approaches.

6. The method of claim 4 , wherein the depicting step includes animation to move the anomaly flag relative to the time scale as the future time approaches.

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.

8. The method of claim 1 , wherein depicting the future time includes moving an anomaly flag along a time graph as the future time approaches and moving the anomaly flag into a static gutter portion adjacent the time graph when the at least one avionics data source is determined to be in the anomalous condition.

9. The method of claim 1 , wherein determining the current anomaly metric data comprises:
determining the current anomaly metric data representing data jump;
determining the current anomaly metric data representing frozen data source;
determining the current anomaly metric data representing gradual data drift; or
determining the current anomaly metric data representing data variance.

10. The method of claim 1 , wherein the predicting the future time is performed by linear extrapolation, polynomial extrapolation, or autoregressive methods.

11. The method of claim 1 , wherein the at least one avionics data source comprises:
distance measuring data source;
flight path vector source;
aircraft speed data source;
aircraft altitude data source;
instrument landing system data source;
aircraft heading data source;
aircraft attitude data source;
glideslope data source;
flight director data source; or
vertical speed data source.

12. The method of claim 1 , comprising displaying one or more display elements based on the time series data and removing the one or more display elements when the at least one avionics data source is determined to be in the anomalous condition.

13. A system for depicting avionics data anomalies in an aircraft, the system comprising:
a display device associated with the aircraft;
an avionics data source; and
a processor in operable communication with the display device and the avionics data source, the processor configured to execute program instructions, wherein the program instructions are configured to cause the processor to:
receive current time series data from the avionics data source;
determine current anomaly metric data based on the current time series data;
upon a determination that the current anomaly metric data crosses a minor anomaly threshold;
predict a future time when major anomaly threshold will be crossed by future anomaly metric data associated with future time series data received at the future time based on an extrapolation of the current time series data; and
depict, via the display device associated with the aircraft, an indication that the avionics data source will be considered to be in an anomalous condition at the future time when the major anomaly threshold will be crossed.

14. The system of claim 13 , wherein the program instructions are configured to cause the processor to provide a time uncertainty associated with the future time when the major anomaly threshold will be crossed and to depict the future time when the major anomaly threshold will be crossed and the time uncertainty.

15. The system of claim 14 , wherein the time uncertainty is depicted using one or more error bars.

16. The system of claim 13 , wherein the program instructions are configured to cause the processor to depict an anomaly flag on a time scale, wherein the position of the anomaly flag on the time scale is set based on the future time.

17. The method of claim 16 , wherein the program instructions are configured to cause the processor to include animation to move the failure flag relative to the time scale as the future time approaches.

Assignees

• Honeywell Int Inc

Inventors

• Dillard Michael
• Orhan Umut
• Whitlow Stephen

Classifications

• G06T11/26

  Drawing of charts or graphs · CPC title

• G06T13/80

  Two-dimensional [2D] animation, e.g. using sprites · CPC title

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G06T11/206

  Physics · mapped topic

• G05B23/0232 Primary

  based on qualitative trend analysis, e.g. system evolution · CPC title