METHOD TO HANDLE SINGLE FAILURE GPS FAULTS IN HIGH INTEGRITY RELATIVE POSITIONING SYSTEMS

• US 20130050020A1
• Filed: 08/23/2011
• Published: 02/28/2013
• Est. Priority Date: 08/23/2011
• Status: Abandoned Application

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Peck, Stephen R., Fries, Robert M., Wu, Shuwu
• Application Number:
  US13/216,130
• Publication Number:
  US 20130050020A1
• Time in Patent Office: Days
• US Class Current: 342/357.27
• 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 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry

Abstract

A method and system to handle single failure GPS faults in high integrity relative positioning systems is provided. The system is configured to receive a number of reference measurements in carrier-phase real time kinetic positioning systems and identify if a single fault exists. The system identifies the type of fault and mitigates the effects of the single fault to provide a positioning system with a high integrity that is suitable for applications involving risk to human lives.

Claims

1. A method for processing single failure GPS receiver faults, the method comprising:

receiving, at a processor, at least two sets of GPS reference measurements and at least one set of remote user GPS measurements;

determining, at the processor, a GPS relative positioning solution (H0 solution) based on the at least two sets of GPS reference measurements and the at least one set of remote user GPS measurements;

excluding a particular set of the at least two sets of GPS reference measurements from the GPS relative positioning solution (H0 solution) to obtain an excluded GPS measurement data set, at the processor;

excluding a different set of the at least two sets of GPS reference measurements from the GPS relative positioning solution (H0 solution) to obtain at least one other excluded GPS reference measurement data set, at the processor;

calculating, at the processor, a H1 protection level based on a priori probability of a single failure GPS receiver fault;

calculating, at the processor, at least one other H1 protection level based on a priori probability of a single failure GPS receiver fault and the bias between the excluded solution and the H0 solution;

identifying a maximum of the H1 protection level and the at least one other H1 protection level to determine a final H1 protection level, at the processor and the bias between the excluded solution and the H0 solution;

determining one or more overall protection levels based on the final H1 protection level, at the processor; and

verifying an integrity requirement based on the overall protection levels, at the processor.

2. The method of claim 1, wherein determining the H1 protection level and the at least one other H1 protection level based on a priori probability further comprises:

determining a GPS positioning solution (H1 solution);

determining one or more position-domain absolute differences (H1 bias) between the GPS positioning solution (H1 solution)and the GPS relative positioning solution (H0 solution);

and

adding the H1 bias to the H1 protection level and the at least one other H1 protection level to determine the final H1 protection level for the excluded set of GPS reference measurements and the at least one other excluded set of GPS reference measurements.

3. The method of claim 1, wherein determining the one or more overall protection levels includes calculating an H0 protection level.

4. The method of claim 1, wherein the protection levels are determined in the position domain.

5. The method of claim 3, wherein the one or more overall protection levels are the maximum H0 protection level and the maximum H1 protection level.

6. The method of claim 1, wherein determining when a single GPS receiver fault exists is based on the at least two sets of GPS references.

7. The method of claim 1, wherein the GPS relative positioning solution (H0 solution) and the GPS positioning solution (H1 solution) and their associated protection levels are determined by GERAFS processing.

8. The method of claim 1, wherein the GPS relative positioning solution (H0 solution) and the GPS positioning solution (H1 solution) and their associated protection levels are determined using a carrier-smoothed-code solution.

9. The method of claim 1, wherein the GPS relative positioning solution (H0 solution) and the GPS positioning solution (H1 solution) and their associated protection levels are determined using a combination of GERAFS and carrier-smoothed-code solutions.

10. A method for processing single failure GPS faults, the method comprising:

determining an H1 integrity risk at a processor;

determining an overall integrity allocation at the processor;

calculating an unbiased relative positioning solution (H0 solution) at the processor;

calculating a biased relative positioning solution (H1) under a single failure GPS fault at the processor;

determining position-domain absolute differences (H1 bias) between the H1 solution and the H0 solution, at the processor;

calculating a H1 protection level based on a priori probability for a single failure GPS faults, at the processor;

calculating a final H1 protection level by adding the H1 bias to the H1 protection level, at the processor;

calculating, at the processor, an overall protection levels based on the final H1 protection level; and

verifying, at the processor, an integrity requirement based on the one or more overall protection levels.

11. The method of claim 10, wherein the type of the single fault is an ephemeris error, the method further comprising:

determining a maximum ephemeris error;

determining relative positioning solution under the maximum ephemeris error; and

determining relative positioning solution under biased GPS measurements.

12. The method of claim 10, wherein the H1 integrity risk is a product of an ephemeris fault onset risk, an ephemeris fault exposure time, and an H1 protection level risk.

13. The method of claim 10, wherein the H1 integrity risk is a product of an inertial measurement unit (IMU) fault onset risk, an IMU fault exposure time, and an H1 protection level risk.

14. The method of claim 10, wherein calculating the one or more overall protection levels comprises calculating an H0 protection level.

15. The method of claim 10, wherein the each protection level is calculated in the position domain.

16. The method of claim 14, wherein the one or more over protection levels are the maximum of the H0 protection level and the H1 protection level.

17. The method of claim 10, wherein the unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined by GERAFS processing.

18. The method of claim 10, wherein unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined using a carrier-smoothed-code solution.

19. The method of claim 10, wherein the unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined using any combination of GERAFS and carrier-smoothed-code solutions.

20. A system for processing single failure GPS receiver faults comprising:

at least one processor; and

at least one module executing on the at least one processor to;

receive at least two sets of GPS reference measurements and at least one set of remote user GPS measurements;

determine a GPS relative positioning solution (H0 solution) based on the at least two sets of GPS reference measurements and the at least one set of remote user GPS measurements;

exclude a particular set of the at least two sets of GPS reference measurements from the GPS relative positioning solution (H0 solution) to obtain an excluded data set;

exclude a different set of the at least two sets of GPS reference measurements from the GPS relative positioning solution (H0 solution) to obtain at least one other excluded set of GPS reference measurements;

calculate a H1 protection level based on a priori probability of a single failure GPS receiver fault;

calculate at least one other H1 protection level based on a priori probability of a single failure GPS receiver fault;

identify a maximum of the H1 protection level and the at least one other H1 protection level to determine a final H1 protection level;

determine one or more overall protection levels based on the final H1 protection level; and

verify an integrity requirement based on the overall protection levels.

21. The system of claim 20, wherein the at least one module is further configured to:

determine a GPS positioning solution (H1 solution);

determine one or more position-domain absolute differences (H1 bias) between the GPS positioning solution (H1 solution) and the GPS relative positioning solution (H0 solution); and

add the H1 bias to the one or more H1 protection levels to determine the final H1 protection level for the excluded particular set of GPS reference measurements.

22. The system of claim 20, wherein determining the one or more overall protection levels includes calculating an H0 protection level.

23. The system of claim 20, wherein the protection levels are determined in the position domain.

24. The system of claim 21, wherein the overall protection levels are the maximum of H0 and H1 protection levels.

25. The system of claim 20, wherein the H0 or H1 relative positioning solution and its associated protection levels are determined by GERAFS processing.

26. The system of claim 20, wherein the H0 or H1 relative positioning solution and its associated protection levels are determined using a carrier-smoothed-code solution.

27. The system of claim 20, wherein the H0 and H1 relative positioning solutions and their associated protection levels are determined using any combination of GERAFS and carrier-smoothed-code solutions.

28. A system for processing single failure GPS receiver faults comprising:

at least one processor; and

at least one module executing on the at least one processor to;

determine an H1 integrity risk;

determine an overall integrity allocation;

calculate an unbiased relative positioning solution (H0 solution);

calculate a biased relative positioning solution (H1) under a single failure GPS fault;

determine position-domain absolute differences (H1 bias) between the H1 solution and the H0 solution;

calculate a H1 protection level based on a priori probability for a single failure GPS faults;

calculate a final H1 protection level by adding the H1 bias to the H1 protection level;

calculate an overall protection levels based on the final H1 protection level; and

verify an integrity requirement based on the one or more overall protection levels.

29. The system of claim 28, wherein the type of the single fault is an ephemeris error, the system further comprising the module executing on the at least one processor to:

determine a maximum ephemeris error;

determine a relative positioning solution under the maximum ephemeris error; and

determine a relative positioning solution under biased GPS measurements.

30. The system of claim 28, wherein the H1 integrity risk is a product of an ephemeris fault onset risk, an ephemeris fault exposure time, and an H1 protection level risk.

31. The system of claim 28, wherein the H1 integrity risk is a product of an inertial measurement unit (IMU) fault onset risk, an IMU fault exposure time, and an H1 protection level risk.

32. The system of claim 28, wherein calculating the overall protection levels comprises calculating an H0 protection level.

33. The system of claim 28, wherein the each protection level is calculated in the position domain.

34. The system of claim 32, wherein the over protection levels are the maximum of the H0 protection level and the H1 protection level.

35. The system of claim 28, wherein the unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined by GERAFS processing.

36. The system of claim 28, wherein unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined using a carrier-smoothed-code solution.

37. The system of claim 28, wherein the unbiased relative positioning solution (H0 solution) and the biased relative positioning solution (H1) and their associated protection levels are determined using any combination of GERAFS and carrier-smoothed-code solutions.