Navigation system with solution separation apparatus for detecting accuracy failures

• US 5,760,737 A
• Filed: 09/11/1996
• Issued: 06/02/1998
• Est. Priority Date: 09/11/1996
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Brenner, Mats A.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/712,232
• Time in Patent Office: 629 Days
• Field of Search: 342/357, 342/450, 342/457, 342/464, 364/449.7, 364/449
• US Class Current: 342/357.58
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial

Abstract

A navigation system, incorporating a unique method for detecting failures and determining an accuracy or error bound, has a receiver for receiving signals from several remote transmitters and a processor for determining a position solution from the signals. The processor, preferably employing Kalman filtering techniques, also determines several position subsolutions from subsets of the signals. The processor then computes covariance-based solution separation parameters based on statistical worst-case differences, or separations, between the position solution and the subsolutions. Similarly, the processor also computes error parameters defining statistical worst-case errors in each position subsolution. With the solution separation and the subsolution error parameters, the processor determines an error bound for the position solution. The processor also uses the separation parameters as detection thresholds for detecting transmitter failures. In one embodiment, the processor incorporates inertial reference data into the solutions and ultimately into the error bound calculation, thereby improving the ability of the navigation system to monitor its own accuracy, or integrity.

Claims

1. A navigation system for a vehicle, comprising:

receiving means for mounting to the vehicle and for receiving a plurality of signals from a plurality of transmitters;

solution means for determining a position solution for the vehicle, based on the plurality of signals;

subsolution means for determining a plurality of position subsolutions for the vehicle, with each subsolution based on a respective subset of the plurality of signals;

solution separation means for determining a plurality of solution separation parameters, with each solution separation parameter based on statistics of a separation between the position solution and a respective subsolution; and

error bound means for determining an error bound for the position solution, based on at least one of the solution separation parameters.

2. The system of claim 1 wherein the solution separation means determines each solution separation parameter from statistics of a horizontal separation between the position solution and the respective subsolution.

6. The system of claim 1 including:

subsolution error means for determining a plurality of subsolution error parameters, with each error parameter based on error statistics of a respective position subsolution; and

wherein the error bound means determines the error bound from at least one of the solution separation parameters and at least one of the subsolution error parameters.

7. The system of claim 6 wherein the subsolution error means includes:

means for determining a plurality of error covariance matrices, with each error covariance matrix based on error statistics of the respective subsolution;

means for determining a respective maximum eigenvalue of each of the error covariance matrices; and

wherein the subsolution error means determines each error parameter from the respective maximum eigenvalue and a preset probability of missed detection P_MD.

8. The system of claim 7 wherein the subsolution error means determines each error parameter from ##EQU15## where λ

_n represents the respective maximum eigenvalue and Q^-1 represents the inverse of a cumulative distribution function.

9. The system of claim 6 wherein the error bound means includes:

means for determining a plurality of parameter sums, with each parameter sum including one of the solution separation parameters and one of the subsolution error parameters;

means for determining a maximum parameter sum from the plurality of parameter sums; and

means for selecting the maximum sum as the error bound.

10. The system of claim 1 including:

detection mean for detecting a transmitter error based on at least one of the solution separation parameters.

11. The system of claim 10 wherein the detection means includes:

discriminator means for computing a plurality of discriminators, with each discriminator based on the position solution and a respective subsolution; and

indicator means for indicating whether one of the discriminators is greater than one of the solution separation parameters.

12. The system of claim 11 wherein the discriminator means determines each discriminator from a distance between the position solution and the respective subsolution.

13. The system of claim 12 wherein the distance between the position solution and the respective subsolution is defined by ##EQU16## where Δ

r₀ (x) and Δ

r₀ (y) denote respective horizontal components of the position solution, and Δ

r_n (x) and Δ

r_n (y) denote respective horizontal components of the respective subsolution.

14. The system of claim 1 including:

means for comparing the error bound to a maximum allowable error of the navigation system; and

means for indicating if the error bound is not less than the maximum allowable error.

15. The system of claim 1:

wherein the solution means determines the position solution according to least-squares estimation; and

wherein the subsolution means determines each position subsolution according to least-squares estimation.

16. The system of claim 1:

wherein the solution means determines the position solution from past and present values of the plurality of signals; and

wherein the subsolution means determines each position subsolution from past and present values of its respective subset of the plurality of signals.

17. The system of claim 16:

wherein the solution means includes Kalman filtering means for determining the position solution from past and present values of the plurality of signals; and

wherein the subsolution means includes Kalman filtering means for determining each position solution from past and present values of its respective subset of the plurality of signals.

18. The system of claim 17 including:

sensing means for sensing motion of the vehicle and providing motion data to the solution means and the subsolution means;

wherein the solution means determines the position solution from the motion data and past and present values of the plurality of signals; and

wherein the subsolution means determines each position subsolution from the motion data and past and present values of its respective subset of the plurality of signals.

19. The system of claim 18 wherein the sensing means includes:

a plurality of accelerometers for providing acceleration data to the solution means and the subsolution means; and

a plurality of gyroscopes for providing attitude data to the solution means and the subsolution means.

20. The system of claim 18 including:

an altimeter for providing altitude data to the solution means and to the subsolution means.

21. The system of claim 1 including:

sensing means for sensing motion of the vehicle and providing motion data to the solution means and the subsolution means;

wherein the solution means determines the position solution from the motion data and past and present values of the plurality of signals; and

wherein the subsolution means determines each position subsolution from the motion data and past and present values of its respective subset of the plurality of signals.

22. The system of claim 1 wherein each of the plurality of transmitters orbits the earth.

3. The system of claim I wherein the solution separation means determines each solution separation parameter from a respective covariance matrix describing the statistics of the separation between the position solution and the respective position subsolution.

4. The system of claim 3 wherein the solution separation means determines each solution separation parameter from the maximum eigenvalue of the respective covariance matrix.

5. The system of claim 4 wherein the solution separation means determines each solution separation parameter from ##EQU14## where λ

_n represents the maximum eigenvalue of its respective covariance matrix, Q^-1 represents the inverse of a cumulative distribution function, P_FD represents a preset probability of false detection, and N represents the number of signals in the plurality of signals.

23. A position measurement system for a vehicle, comprising:

receiving means for mounting to the vehicle and for receiving a plurality of signals from a plurality of transmitters;

solution means for determining a position solution for the vehicle, based on the plurality of signals;

subsolution means for determining a plurality of position subsolutions for the vehicle, with each subsolution based on a respective subset of the plurality of signals;

solution separation means for determining a plurality of solution separation parameters, with each solution separation parameter based on statistics of a separation between the position solution and a respective subsolution; and

detection means for detecting a transmitter failure based on at least one of the solution separation parameters.

24. The system of claim 23 wherein the detection means includes:

discriminator means for computing a plurality of discriminators, with each discriminator based on the position solution and the respective subsolution; and

indicator means for indicating whether one of the discriminators is not less than one of the solution separation parameters.

25. The system of claim 23 wherein the discriminator means determines each discriminator from a distance between the position solution and the respective subsolution.

26. The system of claim 25 wherein the distance between the position solution and the respective subsolution is defined by ##EQU17## where Δ

r₀ (x) and Δ

r₀ (y) denote respective horizontal components of the position solution, and Δ

r_n (x) and Δ

r_n (y) denote respective horizontal components of the subsolution.

27. The system of claim 23 wherein the solution separation means determines each solution separation parameter from a respective covariance matrix describing the statistics of the separation between the position solution and the respective position subsolution.

28. The system of claim 27 wherein the solution separation means determines each solution separation parameter from the maximum eigenvalue of the respective covariance matrix.

29. The system of claim 28 wherein the solution separation means determines each solution separation parameter from ##EQU18## where λ

_n represents the maximum eigenvalue of its respective covariance matrix, Q^-1 represents the inverse of a cumulative distribution function, P_FD represents a preset probability of false detection, and N represents the number of signals in the plurality of signals.

30. The system of claim 23 including:

subsolution error means for determining a plurality of subsolution error parameters, with each error parameter based on error statistics of a respective position subsolution; and

error bound means for determining an error bound for the position solution based on one of the solution separation parameters and one of the subsolution error parameters.

31. A method of operating and monitoring a position measurement system for a vehicle, the method comprising:

determining a position solution for the vehicle, based on a plurality of signals from a plurality of transmitters;

determining a position subsolution for the vehicle, based on a subset of the plurality of signals;

determining a solution separation parameter from statistics of a separation between the position solution and the position subsolution;

determining a discriminator based on the position solution and the position subsolution;

detecting a transmitter failure based on the relationship of the discriminator and the solution separation parameter.

32. The method of claim 31 including:

determining an error bound for the position solution, based on the solution separation parameter;

comparing the error bound to a maximum allowable error; and

indicating an accuracy failure if the error bound is not less than the maximum allowable error.

33. The method of claim 31 wherein:

the discriminator is based on a distance between the position solution and the subsolution; and

a transmitter failure is detected if the discriminator is not less than the solution separation parameter.

34. The method of claim 33 wherein the distance between the position solution and the respective subsolution is defined by ##EQU19## where Δ

r₀ (x) and Δ

r₀ (y) denote respective horizontal components of the position solution, and Δ

r_n (x) and Δ

r_n (y) denote respective horizontal components of the respective subsolution.

35. The method of claim 31 wherein the solution separation parameter is determined from an eigenvalue of a covariance matrix describing the statistics of the separation between the position solution and the position subsolution.

36. The method of claim 35 wherein the solution separation parameter is determined from ##EQU20## where λ

_n represents the maximum eigenvalue of the covariance matrix, Q^-1 represents the inverse of a cumulative distribution function, P_FD represents a preset probability of false detection, and N represents the number of signals in the plurality of signals.

37. The method of claim 32 wherein determining the error bound includes:

determining an error parameter from error statistics of the position subsolution; and

adding the error parameter to the solution separation parameter to determine the error bound.

38. The method of claim 37 wherein the error parameter is determined from a maximum eigenvalue of a covariance matrix describing the error statistics of the position subsolution.

39. The method of claim 38 wherein the error parameter is determined from ##EQU21## where λ

_n represents the maximum eigenvalue, Q^-1 represents the inverse of a cumulative distribution function, and P_MD represents a preset probability of missed detection.

40. The method of claim 31 wherein:

determining the position solution includes Kalman filtering past and present values of the plurality of signals; and

determining the position subsolution includes Kalman filtering past and present values of the its respective subsets of the plurality of signals.

41. The method of claim 40 wherein:

the position solution is determined from vehicle motion data and past and present values of the signals; and

the position subsolution is determined from vehicle motion data and past and present values of the subset of signals.

42. The method of claim 41 wherein the motion data includes acceleration data and attitude data for the vehicle.

43. The method of claim 40 wherein the position solution is also determined from altimeter data and the position solution is also determined from altimeter data.