INERTIAL SENSOR ORIENTATION DETECTION AND MEASUREMENT CORRECTION FOR NAVIGATION DEVICE

• US 20110313650A1
• Filed: 06/21/2010
• Published: 12/22/2011
• Est. Priority Date: 06/21/2010
• Status: Abandoned Application

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Tomé, Phillip
• Application Number:
  US12/819,962
• Publication Number:
  US 20110313650A1
• Time in Patent Office: Days
• US Class Current: 701/200
• CPC Class Codes: G01C 21/185 for gravity

Abstract

Implementations relating to methods, apparatuses and systems are disclosed for obtaining corrected inertial measurements based on an observed orientation of an inertial sensor system relative to a reference body.

Claims

1. A method, comprising:

processing one or more linear inertial measurements and one or more rotational inertial measurements obtained from an inertial sensor system to obtain one or more transformation values based, at least in part, on a linear acceleration vector and a rotational velocity vector indicated by said measurements,

said one or more transformation values enabling transformation of at least one subsequent inertial measurement obtained from the inertial sensor system to at least one corrected inertial measurement.

2. The method of claim 1, further comprising:

obtaining the at least one subsequent inertial measurement from the inertial sensor system; and

applying the one or more transformation values to the at least one subsequent inertial measurement to obtain the at least one corrected inertial measurement based, at least in part, on the one or more transformation values.

3. The method of claim 1, wherein processing the one or more linear inertial measurements further comprises:

processing the one or more linear inertial measurements in response to the linear acceleration vector meeting or exceeding a first threshold value.

4. The method of claim 3, wherein processing the one or more linear inertial measurements further comprises:

processing the one or more linear inertial measurements in response to a rate of rotation indicated by the rotational velocity vector obtained from the one or more rotational inertial sensors being less than a second threshold value.

5. The method of claim 4, wherein processing the one or more rotational inertial measurements further comprises:

processing the one or more rotational inertial measurements in response to the rotational velocity vector indicating a rate of rotation meeting or exceeding a third threshold value;

wherein the third threshold value is greater than the second threshold value.

6. The method of claim 1, wherein obtaining the one or more linear inertial measurements further comprises:

obtaining at least three linear inertial measurements indicating the linear acceleration vector from at least three linear inertial sensors of the inertial sensor system; and

wherein processing the one or more linear inertial measurements further comprises;

determining the linear acceleration vector as a combination of the at least three linear inertial measurements.

7. The method of claim 1, wherein obtaining the one or more rotational inertial measurements further comprises:

obtaining at least three rotational inertial measurements indicating the rotational velocity vector from at least three rotational inertial sensors of the inertial sensor system; and

wherein processing the one or more rotational inertial measurements further comprises;

determining the rotational velocity vector as a combination of the at least three rotational inertial measurements; and

wherein the one or more transformation values is further based, at least in part, on a rate of rotation indicated by the rotational velocity vector.

8. The method of claim 1, further comprising:

applying the one or more transformation values to the at least one subsequent inertial measurement to obtain the at least one corrected inertial measurement based, at least in part, on the one or more transformation values; and

processing the at least one corrected inertial measurement to obtain an indication of a geographic position and/or heading of the inertial sensor system.

9. The method of claim 8, wherein processing the at least one corrected inertial measurement further comprises:

processing the at least one corrected inertial measurement in combination with one or more navigation signals obtained at a wireless receiver from a navigation system to obtain the indication of the geographic position and/or heading of the inertial sensor system.

10. The method of claim 8, wherein the one or more linear inertial measurements comprise a set of linear inertial measurements of a plurality of sets of linear inertial measurements obtained from the one or more linear inertial sensors;

wherein the method further comprises processing the plurality of sets of linear inertial measurements to obtain the one or more transformation values;

wherein the set of linear inertial measurements is weighted relative to one or more other sets of linear inertial measurements based, at least in part, on a magnitude of the linear acceleration vector relative to one or more other linear acceleration vectors indicated by the one or more other sets of linear inertial measurements.

11. A system, comprising:

a navigation device, comprising;

an inertial sensor system comprising one or more inertial sensors;

an electronic storage medium; and

a logic subsystem to;

process one or more linear inertial measurements and one or more rotational inertial measurements obtained from an inertial sensor system to obtain one or more transformation values based, at least in part, on a linear acceleration vector and a rotational velocity vector indicated by said measurements,

said one or more transformation values enabling transformation of at least one subsequent inertial measurement obtained from the inertial sensor system to at least one corrected inertial measurement.

12. The system of claim 11, wherein the logic subsystem is further adapted to:

apply the one or more transformation values to the at least one subsequent inertial measurement to obtain the at least one corrected inertial measurement based, at least in part, on the one or more transformation values.

13. The system of claim 11, wherein the inertial sensor system further comprises:

at least three linear inertial sensors for obtaining the one or more linear inertial measurements; and

at least three rotational inertial sensors for obtaining the one or more rotational inertial measurements.

14. The system of claim 11, wherein the logic subsystem is further adapted to process the one or more linear inertial measurements in response to the linear acceleration vector meeting or exceeding a first threshold value.

15. The system of claim 14, wherein the logic subsystem is further adapted to process the one or more linear inertial measurements in response to a rate of rotation indicated by the rotational velocity vector obtained from the one or more rotational inertial sensors being less than a second threshold value.

16. The system of claim 15, wherein the logic subsystem is further adapted to process the one or more rotational inertial measurements in response to the rotational velocity vector indicating a rate of rotation meeting or exceeding a third threshold value;

wherein the third threshold value is greater than the second threshold value.

17. The system of claim 11, wherein the logic subsystem is further adapted to:

apply the one or more transformation values to the at least one subsequent inertial measurement to obtain the at least one corrected inertial measurement based, at least in part, on the one or more transformation values; and

process the at least one corrected inertial measurement to obtain an indication of a geographic position and/or heading of the navigation device.

18. The system of claim 11, further comprising a wireless receiver;

and

wherein the logic subsystem is further adapted to;

process the at least one corrected inertial measurement in combination with one or more navigation signals obtained at the wireless receiver from a navigation system to obtain an indication of geographic position and/or heading of the inertial sensor system.

19. The system of claim 11, wherein the logic subsystem comprises a computing platform including one or more processors programmed with instructions.

20. An electronic storage media having instructions stored thereon executable by one or more processors to:

process one or more linear inertial measurements and one or more rotational inertial measurements obtained from an inertial sensor system to obtain one or more transformation values based, at least in part, on a linear acceleration vector and a rotational velocity vector indicated by said measurements,

said one or more transformation values enabling transformation of at least one subsequent inertial measurement obtained from the inertial sensor system to at least one corrected inertial measurement.

21. The electronic storage media of claim 20, wherein the instructions are further executable by the one or more processors to:

apply the one or more transformation values to the at least one subsequent inertial measurement to obtain the at least one corrected inertial measurement based, at least in part, on the one or more transformation values.

22. A system, comprising:

means for obtaining one or more linear inertial measurements indicating a linear acceleration vector;

means for obtaining one or more rotational inertial measurements indicating a rotational velocity vector;

means for processing the one or more linear inertial measurements and the one or more rotational inertial measurements to obtain one or more transformation values based, at least in part, on the linear acceleration vector and the rotational velocity vector; and

means for applying the one or more transformation values to at least one subsequently obtained inertial measurement to transform the at least one inertial measurement to at least one corrected inertial measurement.