FILTERING GNSS-AIDED NAVIGATION DATA TO HELP COMBINE SENSOR AND A PRIORI DATA

• US 20150241220A1
• Filed: 02/27/2014
• Published: 08/27/2015
• Est. Priority Date: 02/27/2014
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: McKitterick, John B., Hawkinson, Wesley J.
• Application Number:
  US14/192,361
• Publication Number:
  US 20150241220A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01C 21/1652 with ranging devices, e.g. LIDAR or RADAR
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
• CPC Class Codes: G01S 19/426 by combining or switching between position solutions or signals derived from different modes of operation in a single system
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled

Abstract

Systems and methods for filtering GNSS-Aided navigation data for helping combine sensor data and a priori data are provided. In at least one embodiment, the method comprises identifying an un-smoothed navigation solution inclusive of a navigation system reset, wherein a value is associated with the navigation system reset. The value associated with the navigation system reset is then subtracted from the un-smoothed navigation solution to generate an initial navigation solution. Further, the value associated with the navigation system reset is incrementally added to the initial navigation solution at a configurable rate to generate a smoothed navigation solution.

Claims

1. A method for improving a navigation solution, the method comprising:

identifying an un-smoothed navigation solution inclusive of a navigation system reset, wherein a value is associated with the navigation system reset;

subtracting the value associated with the navigation system reset from the un-smoothed navigation solution to generate an initial navigation solution; and

incrementally adding the value associated with the navigation system reset to the initial navigation solution at a configurable rate to generate a smoothed navigation solution.

2. The method of claim 1, wherein identifying the un-smoothed navigation solution comprises comparing the un-smoothed navigation solution with a navigation solution using a reference navigation system.

3. The method of claim 2, wherein the reference navigation system includes at least one of:

a global navigation satellite system, an inertial navigation system, a Radio Detection and Ranging sensor, and a Light Detection and Ranging sensor.

4. The method of claim 1, wherein the smoothed navigation solution is used in creating a scene for a synthetic vision system.

5. The method of claim 1, wherein incrementally adding the value associated with the navigation system reset involves adding the value at a constant rate.

6. The method of claim 1, wherein the value associated with the navigation system reset is equal to the change in the navigation solution due to the navigation system reset.

7. The method of claim 1, wherein the value associated with the navigation system reset is less than the change in the navigation solution due to the navigation system reset.

8. The method of claim 1, wherein identifying the un-smoothed navigation solution inclusive of a navigation system reset includes identifying only the navigation system resets that are above a threshold.

9. A navigation system comprising:

at least one inertial measurement unit configured to provide inertial measurements;

at least one aiding device configured to generate aiding device measurement data;

a memory device configured to store computer readable instructions, and

a navigation processor configured to provide a navigation solution, wherein the navigation processor is coupled to receive the inertial measurements from the inertial measurement unit and the aiding device measurement data from the aiding device, wherein computer readable instructions direct the navigation processor to;

identify an un-smoothed navigation solution inclusive of a navigation system reset wherein a value is associated with the navigation system reset;

subtract the value associated with the navigation system reset from the un-smoothed navigation solution to generate an initial navigation solution; and

incrementally add the value associated with the navigation system reset to the initial navigation solution at a configurable rate to generate a smoothed navigation solution.

10. The navigation system of claim 9, wherein identifying an un-smoothed navigation solution comprises comparing the un-smoothed navigation solution with a navigation solution using a reference navigation system.

11. The navigation system of claim 10, wherein the reference navigation system includes at least one of:

a global navigation satellite system, an inertial navigation system, a Radio Detection and Ranging sensor, and a Light Detection and Ranging sensor.

12. The navigation system of claim 9, wherein the smoothed navigation solution is used in creating a scene for a synthetic vision system.

13. The navigation system of claim 9, wherein incrementally adding the value associated with the navigation system reset comprises adding the value at a constant rate.

14. The navigation system of claim 9, wherein the value associated with the navigation system reset is equal to the change in the navigation solution due to the navigation system reset.

15. The navigation system of claim 9, wherein the value associated with the navigation system reset is less than the change in the navigation solution due to the navigation system reset.

16. The navigation system of claim 9, wherein identifying the un-smoothed navigation solution inclusive of a navigation system reset includes identifying only the navigation system resets that are above a threshold.

17. A program product comprising a processor-readable medium on which program instructions are embodied, wherein the program instructions are configured, when executed by at least one programmable processor, to cause the at least one programmable processor:

to identify an un-smoothed navigation solution inclusive of a navigation system reset wherein a value is associated with the navigation system reset;

to subtract the value associated with the navigation system reset from the un-smoothed navigation solution to generate an initial navigation solution; and

to incrementally add the value associated with the navigation system reset to the initial navigation solution at a configurable rate to generate a smoothed navigation solution.

18. The program product of claim 17, wherein identifying the un-smoothed navigation solution comprises comparing the un-smoothed navigation solution with a navigation solution using a reference navigation system.

19. The program product of claim 18, wherein the reference navigation system includes at least one of:

a global navigation satellite system, an inertial navigation system, a Radio Detection and Ranging sensor, and a Light Detection and Ranging sensor.

20. The program product of claim 17, wherein the smoothed navigation solution is used in creating a scene for a synthetic vision system.