ORIENTATION MODEL FOR INERTIAL DEVICES

• US 20160363460A1
• Filed: 06/10/2016
• Published: 12/15/2016
• Est. Priority Date: 06/12/2015
• Status: Abandoned Application

• Current Assignee: 7725965 Canada Inc.
• Original Assignee: 7725965 Canada Inc.
• Inventors: SARBISHEI, Omid
• Application Number:
  US15/179,182
• Publication Number:
  US 20160363460A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices

Abstract

There is described a computationally efficient quaternion-based orientation estimation model for a moving object using a specialized gradient descent correction step.

Claims

1. A computer-implemented method for estimating an orientation of a moving object in three-dimensional space, the method comprising:

obtaining filtered and calibrated angular velocity readings of the object;

computing a first correction vector by directing a quaternion orientation estimate at time t−

1 towards the angular velocity readings found at time t to generate a quaternion orientation estimate of the angular velocity readings at time t;

obtaining filtered and calibrated proper acceleration readings of the object;

computing a second correction vector by directing the quaternion orientation estimate of the angular velocity readings at time t towards the proper acceleration readings found at time t; and

using the second correction vector as a measurement error for estimating the orientation of the moving object at time t.

2. The method of claim 1, further comprising obtaining filtered and calibrated heading angle readings of the object, and wherein computing the second correction vector comprises directing the quaternion orientation estimate of the angular velocity readings at time t towards the proper acceleration readings and the heading angle readings found at time t.

3. The method of claim 1, further comprising detecting a temporary disturbance in the proper acceleration readings at time t, and adjusting the second correction vector at time t to account for the temporary disturbance.

4. The method of claim 3, wherein adjusting the second correction vector at time t comprises applying at least one confidence weight to the proper acceleration readings, and adjusting the confidence weight at time t when the temporary disturbance is detected.

5. The method of claim 2, further comprising detecting a temporary disturbance in at least one of the proper acceleration readings and the heading angle readings at time t, and adjusting the second correction vector at time t to account for the temporary disturbance.

6. The method of claim 1, further comprising determining a zero-bias drift in the angular velocity readings for stationary positions of the object by computing a mean value of the angular velocity readings, and correcting for the zero-bias drift.

7. The method of claim 2, further comprising determining a zero-bias drift in the angular velocity readings for stationary or non-stationary positions of the object using the quaternion orientation estimate at time t−

1, and correcting for the zero-bias drift.

8. The method of claim 1, wherein the first correction vector and the second correction vector are both quaternions, computing the first correction vector comprises numerically integrating a quaternion derivative which is found using the proper angular velocity readings, and computing the second quaternion comprises computing a gradient descent.

9. The method of claim 1, wherein the method is implemented by an inertial measurement unit (IMU) sensor array.

10. The method of claim 2, wherein the method is implemented by a Magnetic Angular Rate and Gravity (MARG) sensor array.

11. A system for estimating an orientation of a moving object in three-dimensional space, the system comprising:

a processing unit; and

a non-transitory memory communicatively coupled to the processing unit and comprising computer-readable program instructions executable by the processing unit for;

obtaining filtered and calibrated angular velocity readings of the object;

computing a first correction vector by directing a quaternion orientation estimate at time t−

1 towards the angular velocity readings found at time t to generate a quaternion orientation estimate of the angular velocity readings at time t;

obtaining filtered and calibrated proper acceleration readings of the object;

computing a second correction vector by directing the quaternion orientation estimate of the angular velocity readings at time t towards the proper acceleration readings found at time t; and

using the second correction vector as a measurement error for estimating the orientation of the moving object at time t.

12. The system of claim 11, wherein the memory and processing unit are provided on a single integrated circuit as part of a microcontroller.

13. The system of claim 11, wherein the system is embedded on the object.

14. The system of claim 11, wherein the program instructions are further executable by the processing unit for obtaining filtered and calibrated heading angle readings of the object, and wherein computing the second correction vector comprises directing the quaternion orientation estimate of the angular velocity readings at time t towards the proper acceleration readings and the heading angle readings found at time t.

15. The system of claim 11, wherein the program instructions are further executable by the processing unit for detecting a temporary disturbance in the proper acceleration readings at time t, and adjusting the second correction vector at time t to account for the temporary disturbance.

16. The system of claim 15, wherein adjusting the second correction vector at time t comprises applying at least one confidence weight to the proper acceleration readings, and adjusting the confidence weight at time t when the temporary disturbance is detected.

17. The system of claim 14, wherein the program instructions are further executable by the processing unit for detecting a temporary disturbance in at least one of the proper acceleration readings and the heading angle readings at time t, and adjusting the second correction vector at time t to account for the temporary disturbance.

18. The system of claim 11, wherein the program instructions are further executable by the processing unit for determining a zero-bias drift in the angular velocity readings for stationary positions of the object by computing a mean value of the angular velocity readings, and correcting for the zero-bias drift.

19. The system of claim 14, wherein the program instructions are further executable by the processing unit for determining a zero-bias drift in the angular velocity readings for stationary or non-stationary positions of the object using the quaternion orientation estimate at time t−

1, and correcting for the zero-bias drift.

20. The system of claim 11, wherein the first correction vector and the second correction vector are both quaternions, computing the first correction vector comprises numerically integrating a quaternion derivative which is found using the proper angular velocity readings, and computing the second quaternion comprises computing a gradient descent.