Restoring navigational performance for a navigational system
A method of restoring navigational performance for a navigational system, the method comprising receiving by a first navigational system and a second navigational system a collection of data points to establish a real-time navigational route for the aircraft, comparing navigational performance values and/or drift ranges and establishing a new navigational route based on the collection of data points.
1. A method of restoring navigational performance for a moving vehicle with a navigational system, the method comprising:
receiving by a first navigational system, located within the vehicle, a first collection of data points;
receiving by an inertial navigation system (INS), located within the vehicle, a second collection of data points;
with a computer:
processing the first and second set collection of data points to establish a real-time navigational route for the moving vehicle;
comparing the second collection of data points to a planned navigational route to determine a drift range between the planned navigational route and the real-time navigational route;
determining that the drift range is greater than a predetermined error range;
disabling the first navigational system;
determining a last known location based on the first collection of data points; and
establishing a new navigational route based on the last known location using the INS.
2. The method of claim 1 , further comprising determining via the computer an actual navigational performance value based on the first and second collection of data points.
3. The method of claim 2 , further comprising determining via the computer an accuracy of the real-time navigational route by comparing the actual navigational performance value to a required navigational performance value to determine if the actual navigational performance value is within a desired percent error of the required navigational performance value.
4. The method of claim 3 , further comprising continuously recalibrating via the computer the INS until the required navigational performance value is within the desired percent error of the actual navigational performance value based on a future error accumulation rate.
5. The method of claim 1 , further comprising determining via the computer the last known location using at least one of navigational aids data, star tracking data, or terrain matching data.
6. The method of claim 5 , further comprising via the computer comparing the at least one of navigational aids data, star tracking data, or terrain matching data to the collection of data points.
7. The method of claim 1 , further comprising determining via the computer whether an accurate determining of the last known location can be established in time for a destination arrival.
8. The method of claim 7 , wherein when the last known location cannot be determined in time for a destination arrival, establishing via the computer a detour navigational route to provide time required to determine the last known location.
9. The method of claim 8 , wherein when the detour navigational route cannot be determined sending via the computer an alert to a user interface to switch to a manual approach.
10. The method of claim 1 , wherein the first navigational system is a Global Navigation Satellite System (GNSS).
11. The method of claim 1 further comprising calculating via the computer an error accumulation rate for the INS based on the collection of data points.
12. The method of claim 11 further comprising recalibrating via the computer the INS based on the error accumulation rate.
13. The method of claim 12 further comprising predicting via the computer a future error accumulation rate before a destination arrival.
14. A method of restoring navigational performance for an aircraft with a navigational system in response to a spoofed signal, the method comprising:
receiving by a first navigational system and an inertial navigation system (INS) a collection of data points to establish a real-time navigational route for the aircraft;
with a computer:
determining an actual navigational performance value associated with the real-time navigational route;
comparing the actual navigational performance value to a required navigational performance value;
determining a spoofed signal for the first navigational system when the actual navigation performance value is outside a desired percent error of the required navigational performance value;
determining a last known location based on the collection of data points when the spoofed signal is determined;
disabling navigation for the first navigational system; and
with the INS establishing a new navigational route based on the last known location.
15. The method of claim 14 further comprising determining via the computer an accuracy of the real-time navigational route by determining a drift range between a planned navigational route and the real-time navigational route.
16. The method of claim 15 wherein the disabling the first navigational system further comprises determining via the computer when the drift range is greater than a predetermined drift range.
17. The method of claim 14 , further comprising determining via the computer the last known location when the actual navigation performance value is greater than the required navigational performance value.
18. The method of claim 14 , further comprising recalibrating via the computer the INS until the required navigational performance value is within the desired percent error of the actual navigational performance value.
19. The method of claim 14 , further comprising determining via the computer the last known location of the aircraft using at least one of navigational aids data, star tracking data, or terrain matching data.
20. The method of claim 19 , further comprising comparing via the computer the at least one of navigational aids data, star tracking data, or terrain matching data to the collection of data points.
21. The method of claim 14 , further comprising determining via the computer whether an accurate determining of the last known location of the aircraft can be established in time for a destination arrival.
22. The method of claim 21 , wherein in an event where the last known location of the aircraft cannot be determined in time for a destination arrival, establishing via the computer a detour navigational route to provide a time required to determine the last known location.
23. The method of claim 22 , further comprising predicting via the computer a future error accumulation rate before a destination arrival.
24. The method of claim 22 , wherein in an event where the detour navigational route cannot be determined sending via the computer an alert to a user interface with instructions to switch to a manual approach.
25. The method of claim 14 , wherein the first navigational system is a Global Navigation Satellite System (GNSS).