Electronic avionics systems and methods
View Patent ↗The present general inventive concept relates to a system of method having an electronic flight display that meets the FAR 23.1311(b) regulatory requirement for redundant backup instruments in the cockpit. The present general inventive concept also provides a system and method to detect failures, obstructions, or improper operation of the aircraft pitot pressure sensing system using a combination of dissimilar sensor data that is independent from each other, e.g., allocated from different sources and employed for different purposes on different displays, and displays information on an avionics display screen.
1. An electronic avionics system comprising:
a comparator operably connected to a data source that derives real-time flight data regarding predetermined flight parameters and operably connected to one or more downstream critical systems that utilize the real-time flight data regarding predetermined flight parameters; and
a database accessible by said comparator, said database including ideal flight data regarding said predetermined flight parameters;
wherein said comparator categorizes said predetermined flight parameters and compares data from said data source and said ideal flight data regarding said predetermined flight parameters and determines if said data source is deriving corrupt data; and
wherein upon determining said data source is deriving corrupt data said comparator takes action to mitigate the effect of said corrupt data on one or more critical systems that utilize the data.
2. The electronic avionics system of claim 1 , wherein said ideal flight data comprises a value of real-time flight data from said data source that would be expected based upon real-time flight data derived from at least one of said data source or an other data source.
3. The electronic avionics system of claim 1 , wherein a predetermined flight parameter from said data source is pitot pressure.
4. The electronic avionics system of claim 1 , wherein a predetermined flight parameter from said data source is ground speed.
5. The electronic avionics system of claim 1 , wherein a predetermined flight parameter from said data source is air speed.
6. The electronic avionics system of claim 1 , wherein a predetermined flight parameter from said data source is ground speed and an other predetermined flight parameter from at least one of said data source or an other data source is air speed.
7. The electronic avionics system of claim 1 , wherein a predetermined flight parameter from said data source is ground speed and an other predetermined flight parameter from at least one of said data source or an other data source is pitot pressure.
8. The electronic avionics system of claim 1 , wherein said comparator alters said corrupt data by complete removal of said corrupt data prior to passing data from the comparator to the one or more downstream critical systems that utilize the data.
9. The electronic avionics system of claim 1 , wherein said comparator action results in said corrupt data being replaced in critical systems with surrogate data that utilize the data.
10. The electronic avionics system of claim 9 , wherein surrogate data is derived from at least one of the data source or an other data source.
11. The electronic avionics system of claim 9 , wherein surrogate data is derived from the database.
12. The electronic avionics system of claim 1 , wherein said comparator provides a warning notification to downstream critical systems to enable said system to recognize said corrupt data as corrupt.
13. The electronic avionics system of claim 12 , wherein said downstream critical systems provides an alert to a user based on recognition of receipt of corrupt data.
14. The electronic avionics system of claim 1 , wherein after said comparator compares said data from said data source and said ideal flight data, said comparator passes said data from comparator to one or more downstream critical systems that utilize the data.