Heading determination using sensors mounted on rotatable assembly

• US 8,521,428 B1
• Filed: 10/15/2009
• Issued: 08/27/2013
• Est. Priority Date: 10/15/2009
• Status: Active Grant

• Current Assignee: Moog Incorporated
• Original Assignee: Moog Incorporated
• Inventors: Liccardo, Darren S., James, John J., Horton, Michael A., Stockwell, Walter K.
• Primary Examiner(s): Black, Thomas
• Assistant Examiner(s): LI, CE LI
• Application Number:
  US12/579,879
• Time in Patent Office: 1,412 Days
• Field of Search: 701/1, 701/3, 701/4, 701/500, 701/501, 701/504, 701/510, 701/511, 701/518, 701/519, 702150-153, 73/17.5, 73/17.7, 73/17.8
• US Class Current: 701/511
• CPC Class Codes: G01C 21/18 Stabilised platforms, e.g. by gyroscope
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices

Abstract

A system and method for more accurately and robustly determining the heading of a vehicle by taking measurements of angle rates using rate sensors mounted on a movable mechanical assembly. In a quasi-static state of the vehicle, the mechanical assembly is rotated around axes perpendicular to the tangent plane of the Earth, and angle rates are measured by the rate sensors at different rotational angles of the mechanical assembly. The measurements of the angle rates are then computed to determine the initial heading of the vehicle relative to the true north of the Earth in the quasi-static state of the vehicle. After determining the initial heading, navigation state propagation is performed to determine the heading of the vehicle in non-quasi-static state of the vehicle. By taking measurements of the rate sensors at different rotation angles and performing computation, the heading of the vehicle relative to the Earth'"'"'s true north can be determined using less accurate angle sensors.

Claims

1. A computer-implemented method for estimating heading of a vehicle, comprising:

receiving first angular rate measurements from a plurality of rate sensors mounted on a rotatable assembly at a first time, the rotatable assembly rotated to a first rotation angle and the vehicle having first heading at the first time;

receiving second angular rate measurements from the plurality of rate sensors at a second time subsequent to the first time, the rotatable assembly rotated to a second rotation angle, the vehicle having second heading that is substantially the same as the first heading at the second time;

computing the first heading relative to a reference vector representing rotation of the Earth based on the first angular rate measurements and the second angular rate measurements; and

computing a third heading of the vehicle at a third time subsequent to the second time based on the first heading responsive to receiving third angular rate measurements from the plurality of rate sensors;

wherein computing the first heading comprises;

projecting the first and second rate measurements to a tangent plane of the Earth to obtain tangent plane data;

fitting the tangent plane data to a conic;

constraining the conic to a circle to obtain a circle transform;

projecting the tangent plane data through the circle transform to obtain transformed data;

fitting the transformed data to a polynomial in the tangent plane;

computing tangent plane angles of the vehicle with respect to a reference direction; and

detecting zero-crossing of the tangent plane angles by interpolating a rotation angle of the rotatable assembly to obtain the first heading.

2. The method of claim 1, wherein computing the third heading comprises propagating a state of the vehicle in time based on the first heading with discrete time increments.

3. The method of claim 1, further comprising computing estimated error of the third heading by computing a state covariance of an Extended Kalman Filter based on a parameter representing characteristics of one or more of the plurality of rate sensors.

4. The method of claim 1, further comprising computing fourth heading to replace the first heading responsive to an estimated error of the third heading exceeding a threshold or receiving user input based on additional rate measurements taken at different rotation angles of the rotatable assembly.

5. The method of claim 4, further comprising initiating a recovery process to compute heading based on the first heading responsive to detecting change of heading of the vehicle during taking of the additional rate measurements to compute the fourth heading.

6. The method of claim 1, further comprising receiving additional angular rate measurements at rotation angles of the rotatable assembly different from the first rotation angle and the second rotation angle, the heading of vehicle maintained at the first heading during taking of the additional angular rate measurements, the first heading computed based further on the additional angular rate measurements.

7. The method of claim 1, wherein the third heading is computed based further on a correction signal received from a non-rate sensor.

8. A navigation system for estimating heading of a vehicle, comprising:

an initial static heading determination module configured to;

receive first angular rate measurements from a plurality of rate sensors mounted on a rotatable assembly at a first time, the rotatable assembly rotated to a first rotation angle and the vehicle having first heading at the first time;

receive second angular rate measurements from the plurality of rate sensors at a second time subsequent to the first time, the rotatable assembly rotated to a second rotation angle and the vehicle having second heading that is substantially the same as the first heading at the second time; and

compute the first heading relative to a reference vector representing rotation of the Earth based on the first angular rate measurements and the second angular rate measurements; and

a dynamic heading tracking module configured to compute third heading of the vehicle at a third time subsequent to the second time based on the first heading responsive to receiving third angular rate measurements from the plurality of rate sensors;

wherein the initial static heading determination module is configured to compute the first heading by;

projecting the first and second rate measurements to a tangent plane of the Earth to obtain tangent plane data;

fitting the tangent plane data to a conic;

constraining the conic to a circle to obtain a circle transform;

projecting the tangent plane data through the circle transform to obtain transformed data;

fitting the transformed data to a polynomial in the tangent plane;

computing tangent plane angles of the vehicle with respect to a reference direction; and

detecting zero-crossing of the tangent plane angles by interpolating a rotation angle of the rotatable assembly to obtain the first heading.

9. The navigation system of claim 8, wherein the dynamic heading tracking module is configured to compute the third heading by propagating a state of the vehicle in time based on the first heading with discrete time increments.

10. The navigation system of claim 8, wherein the dynamic heading tracking module comprise a correction module configured to estimate an error of the third heading by computing a state covariance of an Extended Kalman Filter based on a parameter representing characteristics of one or more of the plurality of rate sensors.

11. The navigation system of claim 8, further comprising an in-run static heading determination module configure to compute fourth heading to replace the first heading responsive to an estimated error of the third heading exceeding a threshold or receiving user input based on additional rate measurements taken at different rotation angles of the rotatable assembly.

12. The navigation system of claim 11, further comprising a recovery module configured to initiate a recovery process to compute heading based on the first heading responsive to detecting change of heading of the vehicle during taking of the additional rate measurements to compute the fourth heading.

13. The navigation system of claim 8, wherein the initial static heading determination module is further configured to receive additional angular rate measurements at rotation angles of the rotatable assembly different from the first rotation angle and the second rotation angle, the heading of vehicle maintained at the first heading during taking of the additional angular rate measurements, the first heading computed based further on the additional angular rate measurements.

14. The navigation system of claim 8, wherein the dynamic heading tracking module is further configured to compute the third heading based further on a correction signal received from a non-rate sensor.

15. A computer readable storage medium storing instructions thereon, the instructions when executed by a processor in a navigation system for determining heading of a vehicle cause the processor to:

receive first angular rate measurements from a plurality of rate sensors mounted on a rotatable assembly at a first time, the rotatable assembly rotated to a first rotation angle and the vehicle having first heading at the first time;

receive second angular rate measurements from the plurality of rate sensors at a second time subsequent to the first time, the rotatable assembly rotated to a second rotation angle and the vehicle having second heading that is substantially the same as the first heading at the second time;

compute the first heading relative to a reference vector representing rotation of the Earth based on the first angular rate measurements and the second angular rate measurements; and

compute third heading of the vehicle at a third time subsequent to the second time based on the first heading responsive to receiving third angular rate measurements from the plurality of rate sensors; and

further comprising instructions that cause the processor to;

project the first and second rate measurements to a tangent plane of the Earth to obtain tangent plane data;

fitting the tangent plane data to a conic;

constraining the conic to a circle to obtain a circle transform;

projecting the tangent plane data through the circle transform to obtain transformed data;

fitting the transformed data to a polynomial in the tangent plane;

computing tangent plane angles of the vehicle with respect to a reference direction; and

detecting zero-crossing of the tangent plane angles by interpolating a rotation angle of the rotatable assembly to obtain the first heading.

16. The computer readable storage medium of claim 15, wherein instructions to compute the third heading comprises instructions to propagate a state of the vehicle in time based on the first heading with discrete time increments.

17. The computer readable storage medium of claim 15, further comprising instructions to compute estimated error of the third heading by computing a state covariance of an Extended Kalman Filter based on a parameter representing characteristics of one or more of the plurality of rate sensors.