NAVIGATION SYSTEM WITH APPARATUS FOR DETECTING ACCURACY FAILURES

• US 20090182494A1
• Filed: 01/15/2008
• Published: 07/16/2009
• Est. Priority Date: 01/15/2008
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: McDonald, James A., Vanderwerf, Kevin D.
• Application Number:
  US12/014,631
• Publication Number:
  US 20090182494A1
• Time in Patent Office: Days
• US Class Current: 701/200
• CPC Class Codes: G01S 19/20 Integrity monitoring, fault detection or fault isolation of space segment

Abstract

A navigation system for a vehicle having a receiver operable to receive a plurality of signals from a plurality of transmitters includes a processor and a memory device. The memory device has stored thereon machine-readable instructions that, when executed by the processor, enable the processor to determine a set of pseudo-range measurements derived from the plurality of signals, employing at least one Kalman filter process, determine from the measurements an error covariance matrix for a main navigation solution, and using a solution separation technique, determine at least one protection level value based on the error covariance matrix.

Claims

1. A navigation system for a vehicle having a receiver operable to receive a plurality of signals from a plurality of transmitters, the navigation system comprising:

a processor; and

a memory device having stored thereon machine-readable instructions that, when executed by the processor, enable the processor to;

determine a set of pseudo-range measurements derived from the plurality of signals,

employing at least one Kalman filter process, determine from the measurements an error covariance matrix for a main navigation solution including associated data characterizing at least one velocity state of the vehicle, and

using a solution separation technique, determine at least one protection level value based on the error covariance matrix.

2. The system of claim 1 wherein the instructions further enable the processor to determine a set of error estimates corresponding to delta pseudo-range measurements derived from the plurality of signals.

3. The system of claim 1 wherein the instructions further enable the processor to determine an error covariance matrix for at least one navigation sub-solution.

4. The system of claim 3 wherein determining at least one protection level value comprises determining a plurality of solution separation parameters, each solution separation parameter being based on statistics of a separation between the main navigation solution and a respective navigation sub-solution.

5. The system of claim 4 wherein determining at least one protection level value further comprises determining an error bound for the main navigation solution based on at least one of the solution separation parameters.

6. The system of claim 4 wherein determining at least one protection level value further comprises determining each solution separation parameter from a respective covariance matrix describing the statistics of the separation between the main navigation solution and the respective navigation sub-solution.

7. The system of claim 1 wherein the at least one protection level value comprises a vertical-velocity integrity value.

8. The system of claim 1 wherein the at least one protection level value comprises a flight-path-angle integrity value.

9. The system of claim 1 wherein the at least one protection level value comprises a track-angle integrity value.

16. The system of claim 1 wherein the at least one protection level value comprises a vertical-velocity integrity value.

17. The system of claim 1 wherein the at least one protection level value comprises a flight-path-angle integrity value.

18. The system of claim 1 wherein the at least one protection level value comprises a track-angle integrity value.

10. A navigation system for a vehicle having a receiver operable to receive a plurality of signals from a plurality of transmitters, the navigation system comprising:

a processor; and

a memory device having stored thereon machine-readable instructions that, when executed by the processor, enable the processor to;

determine from the plurality of signals an error covariance matrix for a main navigation solution,

determine from the matrix a set of values corresponding to horizontal and vertical velocity states of the vehicle, and

based on said set of values, determine at least one protection level value associated with said velocity states.

11. The system of claim 10 wherein the set of values corresponds to delta pseudo-range measurements derived from the plurality of signals.

12. The system of claim 10 wherein determining the set of values comprises determining an error covariance matrix for at least one navigation sub-solution.

13. The system of claim 12 wherein determining at least one protection level value comprises determining a plurality of solution separation parameters, each solution separation parameter being based on statistics of a separation between the main navigation solution and a respective navigation sub-solution.

14. The system of claim 13 wherein determining at least one protection level value further comprises determining an error bound for the main navigation solution based on at least one of the solution separation parameters.

15. The system of claim 13 wherein determining at least one protection level value further comprises determining each solution separation parameter from a respective covariance matrix describing the statistics of the separation between the main navigation solution and the respective navigation sub-solution.

19. A computer-readable medium having computer-executable instructions for performing steps comprising:

determining a set of pseudo-range measurements derived from the plurality of signals,

employing at least one Kalman filter process, determining from the measurements an error covariance matrix for a main navigation solution, and

using a solution separation technique, determining at least one protection level value based on the error covariance matrix.

20. A method, comprising the steps of:

accessing from a first computer the computer-executable instructions of claim 19; and

providing the instructions to a second computer over a communications medium.