METHOD AND APPARATUS FOR DETERMINING THE OPERATIONAL STATE OF A NAVIGATION SYSTEM

• US 20100088064A1
• Filed: 10/03/2008
• Published: 04/08/2010
• Est. Priority Date: 10/03/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Russell, Richard S., Snyder, Scott I., Vallot, Lawrence C., Lund, Christopher A.
• Granted Patent: US 7,840,381 B2
• Time in Patent Office: Days
• US Class Current: 702/179
• CPC Class Codes: G01C 25/00 Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass testing, calibrating or compensating compasses G01C17/38

Abstract

A method of determining an operational state of a navigation system of a platform is provided. The method comprises testing at least a portion of hardware in the navigation system. Additionally, a measurement of at least one navigation variable from an inertial sensor is combined with a measurement of another navigation variable. A plurality of residuals for the measurement of at least one navigation variable and the measurement of another navigation variable are determined with a blending filter. An error for the measurement of at least one navigation variable is estimated based on the plurality of residuals. The method also predicts an error for the measurement of at least one navigation variable while the navigation system is in route. A determination is made as to whether the navigation system meets operational standards based on testing at least a portion of hardware, estimating an error for the measurement of at least one navigation variable, and predicting an error for the measurement of at least one navigation variable. Finally, one of a first state and a second state of the navigation system is output, the first state indicating that the navigation system does meet operational standards and the second state indicating that the navigation system does not meet operational standards.

Claims

1. A method of determining an operational state of a navigation system comprising:

testing at least a portion of hardware in the navigation system;

combining a measurement of at least one navigation variable from an inertial sensor with a measurement of another navigation variable;

determining a plurality of residuals for the measurement of at least one navigation variable and the measurement of another navigation variable with a blending filter;

estimating an error for the measurement of at least one navigation variable based on the plurality of residuals;

predicting an error for the measurement of at least one navigation variable while the navigation system is en route;

determining whether the navigation system meets operational standards based on testing at least a portion of hardware, estimating an error for the measurement of at least one navigation variable, and predicting an error for the measurement of at least one navigation variable; and

outputting one of a first state and a second state of the navigation system, the first state indicating that the navigation system does meet operational standards and the second state indicating that the navigation system does not meet operational standards.

2. The method of claim 1, wherein determining whether the navigation system meets operational standards is based on determining a Root Mean Square (RMS) value for the plurality of residuals.

3. The method of claim 1, wherein determining whether the navigation system meets operational standards is based on determining whether noise within the blending filter is exhibiting normal characteristics.

4. The method of claim 1, further comprising:

measuring the at least one navigation variable with an inertial sensor;

measuring the another navigation variable with an aiding source;

5. The method of claim 1, wherein predicting the error for the measurement of at least one navigation variable while the navigation system is en route, predicts the error for the measurement of at least one navigation variable using only measurements from inertial sensors.

6. The method of claim 1, wherein predicting the error for the measurement of at least one navigation variable while the navigation system is en route, predicts the error for the measurement of at least one navigation variable once using only measurements from the inertial sensors and again using measurements from inertial sensors and an aiding source.

7. The method of claim 1, wherein determining whether the navigation system meets operational standards is based on determining whether the error for the measurement of at least one navigation variable is within an expected range for a performance class of the inertial sensor.

8. The method of claim 7, wherein the system is determined to be in the first state when no errors are found when testing at least a portion of hardware, when the error for the measurement of at least one navigation variable is consistent with a modeled amount, and when the error for the measurement of at least one navigation variable is within an expected range of the measurement device.

9. An apparatus for determining the operational state of a navigation system comprising:

a processor for executing software;

an output device communicatively coupled to the processor;

at least one inertial sensor communicatively coupled to the processor;

a Global Positioning System (GPS) receiver coupled to the processor;

a storage medium communicatively coupled to the processor from which the processor reads at least a portion of the software for execution thereby, wherein the software is configured to cause the processor to;

test at least a portion of hardware that takes navigational measurements;

receive a measurement of at least one navigation variable from the at least one inertial sensor;

receive a measurement from the an aiding source;

combine the measurement of at least one navigation variable with the measurement from the aiding source;

determine a plurality of residuals for the measurement of at least one navigation variable with a blending filter;

estimate an error for the measurement of at least one navigation variable based on the plurality of residuals;

predicting an error for the measurement of at least one navigation variable while the navigation system is en route;

determine whether the navigation system meets operational standards based on the test of at least a portion of hardware, the estimate of an error for the measurement of at least one navigation variable, and the prediction of an error for the measurement of at least one navigation variable; and

output one of first state and a second state of the navigation system on the output device, the first state indicating that the system does meet operational standards and the second state indicating that the system does not meet operational standards.

10. The apparatus of claim 9, wherein the software is further configured to cause the processor to:

determine a Root Mean Square (RMS) value for the plurality of residuals; and

determine whether the navigation system meets operational standards based on the RMS value for the plurality of residuals.

11. The apparatus of claim 9, wherein the software is further configured to cause the processor to:

determine whether noise within the blending filter is exhibiting normal characteristics; and

determine whether the navigation system meets operational standards based on whether the noise within the blending filter is exhibiting normal characteristics.

12. The apparatus of claim 9, wherein the software is further configured to cause the processor to:

predict an error for the measurement of at least one navigation variable using only the measurement from the at least one inertial sensor.

13. The apparatus of claim 9, wherein the software is further configured to cause the processor to:

predict an error for the measurement of at least one navigation variable once using only the measurement from the at least one inertial sensor, and again using the measurement from the at least one inertial sensor and the measurement from the aiding source.

14. The apparatus of claim 9, wherein the software is further configured to cause the processor to:

determine whether the error for a measurement of at least one navigation variable is within an expected range for that measurement device; and

determine whether the navigation system meets operational standards based on whether the estimated inertial errors are within an expected range for a given inertial sensor performance class.

15. A program product comprising a processor-readable medium on which program instructions are embodied, wherein the program instructions are operable to:

test at least a portion of hardware that takes navigational measurements;

combine a measurement of at least one navigation variable from an inertial sensor with a measurement of another navigation variable;

determine a plurality of residuals for the measurement of at least one navigation variable with a blending filter;

estimate an error for the measurement of at least one navigation variable based on the plurality of residuals;

predict an error for the measurement of at least one navigation variable while the navigation system is en route;

determine whether the navigation system meets operational standards based on the test of at least a portion of hardware, the estimate of an error for the navigation variable, and the prediction of an error of at least one navigation variable; and

output one of first state and a second state of the navigation system, the first state indicating that the navigation system does meet operational standards and the second state indicating that the navigation system does not meet operational standards.

16. The program product of claim 15, wherein the program instructions are further operable to:

determine a Root Mean Square (RMS) value for the plurality of residuals; and

determine whether the navigation system meets operational standards based on the RMS value for the plurality of residuals.

17. The program product of claim 15, wherein the program instructions are operable to:

determine whether noise within the blending filter is exhibiting normal characteristics; and

determine whether the navigation system meets operational standards based on whether the noise within the blending filter is exhibiting normal characteristics.

18. The program product of claim 15, wherein the program instructions are operable to:

receive a measurement of at least one navigation variable from at least one inertial sensor;

receive a measurement from a global positioning system (GPS) receiver;

19. The program product of claim 18, wherein the program instructions are operable to:

predict an error of at least one navigation variable once using only the measurement from the at least one inertial sensor, and again using the measurement from the at least one inertial sensor and the measurement from the GPS receiver.

20. The program product of claim 15, wherein the program instructions are operable to:

determine whether the error for a measurement of at least one navigation variable is within an expected range for that measurement device; and

determine whether the navigation system meets operational standards based on whether the error for a measurement of at least one navigation variable is within an expected range for an inertial sensor.