Electromagnetic position and orientation tracking system with distortion compensation employing wireless sensors

• US 6,369,564 B1
• Filed: 01/03/2001
• Issued: 04/09/2002
• Est. Priority Date: 11/01/1999
• Status: Expired due to Term

• Current Assignee: Chittenden Bank (People's United Financial Incorporated)
• Original Assignee: Polhemus Incorporated
• Inventors: Jones, Herbert S. Jr., Khalfin, Igor
• Primary Examiner(s): PATIDAR, JAY M
• Application Number:
  US09/755,303
• Time in Patent Office: 461 Days
• Field of Search: 324/207.11, 324/207.12, 324/207-4-2, 324/207.26, 324/228, 324/236, 324/239, 324/243, 600/424, 600/407, 600/409, 600/587, 600/595, 702/150, 702/152, 702/153
• US Class Current: 324/207.17
• CPC Class Codes: G01B 3/1084 Tapes combined with arrangements for functions other than measuring lengths
• CPC Class Codes: G01S 1/024 of beacon transmitters
• CPC Class Codes: G01V 3/08 operating with magnetic or electric fields produced or modified by objects or geological structures or by detecting devices with electromagnetic waves G01V3/12
• CPC Class Codes: G02B 27/017 Head mounted
• CPC Class Codes: G06F 3/012 Head tracking input arrangements

Abstract

A solution to the electromagnetic position/orientation tracking problem is presented in an environment wherein strong electromagnetic distortion may be present includes at least one source of an AC electromagnetic field, at least one witness sensor measuring components of the electromagnetic induction vector at known spatial points close to, or within the volume of interest, at least one wireless probe sensor placed on the object being tracked, and a control and processing unit. The wireless sensor has a known response or distortion to the electromagnetic field generated by the primary source. The control/processing unit uses data from the witness sensor(s) to locate the probe sensor, treating the probe sensor as a secondary source of the AC electromagnetic field; that is, as a transponder with initially known magnetic parameters. This information is utilized by a position and orientation algorithm executed by the control/processing unit to define coordinates and attitude of the secondary source and, in turn, the position and orientation H of the object of interest. In the preferred embodiment, the probe sensor is an LC-contour tuned to the frequency of the tracker source. As such, the signal from the probe sensor is 90° phase shifted with respect to the tracker source signal and other signals in the system, including distortion. This allows the witness sensors and processing unit to separate the environmental distortion signal from the probe sensor signal by distinguishing the phase of the signal from the probe sensor.

Claims

1. Apparatus for determining the position and orientation of an object within a volume of interest with respect to a known reference frame in the presence of electromagnetic distortion, the apparatus comprising:

a primary source of an electromagnetic field;

at least one wireless probe sensor supported on the object, the probe sensor acting as a secondary source of the electromagnetic field with a known distortion profile having measurable magnetic induction-vector components;

one or more stationary witness sensors supported near or within the volume of interest, each witness sensor being operative to detect the induction-vector components associated with each probe sensor using a fixed known position and orientation of each witness sensor; and

at least one system processor in communication with each witness sensor, the processor being operative to perform the following functions;

a) distinguish the secondary source signal from the primary source signal and distortion signal,

b) compute the characteristics of the secondary electromagnetic source as it seen by each witness sensor, and

c) compute the position and orientation of the object given the computed characteristics of the secondary source in conjunction with the fixed position and orientation of each witness sensor in the known reference frame.

2. The apparatus of claim 1, wherein the probe sensor is an element which produces induction-vector components which are phase-shifted relative to the primary source of the electromagnetic field.

3. The apparatus of claim 2, wherein:

the primary source has a frequency associated therewith; and

the element features a LC contour of a known distortion at the frequency.

4. The apparatus of claim 3, wherein the element is a conducting ring.

5. The apparatus of claim 1, wherein the object moves within the volume;

and

one or more of the functions performed by the processor are repeated at regular intervals to track the motion of the object.

6. The apparatus of claim 1, wherein the computed characteristics include the strength, position and orientation of the secondary source.

7. The apparatus of claim 1, wherein the volume of interest includes at least a portion of a vehicle interior, and wherein the probe sensor is supported relative to an operator of the vehicle.

8. The apparatus of claim 7, wherein vehicle interior forms part of an aircraft cockpit, and wherein the probe sensor is mounted on a helmet worn by the operator.

9. The apparatus of claim 1, wherein the secondary source is treated as a point source.

10. The apparatus of claim 1, wherein the secondary source is approximated as a dipole source or sources.

11. The apparatus of claim 1, wherein each witness sensor measures three components of the induction vector along three orthogonal axes.

12. Apparatus for determining the position and orientation of an object within a volume of interest with respect to a known reference frame in the presence of electromagnetic distortion, the apparatus comprising:

a primary source of an electromagnetic field having a frequency associated therewith;

at least one probe sensor element supported on the object, the element having an LC contour tuned to the frequency of the primary source, enabling the element to function as a secondary source having a known distortion profile with measurable magnetic induction-vector components that are phase-shifted relative to the primary source of the electromagnetic field;

one or more stationary witness sensors supported near or within the volume, each witness sensor being operative to detect the induction-vector components associated with each probe sensor element using a fixed position and orientation in a known reference frame; and

a processor in communication with each witness sensor, the processor being operative to perform the following functions;

a) distinguish secondary source signal from the primary source signal and distortion signal,

b) compute the characteristics of the secondary electromagnetic source as it seen by each witness sensor, and

c) compute the position and orientation of the object given the computed characteristics of the secondary source in conjunction with the fixed position and orientation of each witness sensor in known reference frame.

13. The apparatus of claim 12, wherein the element is a ring.

14. The apparatus of claim 12, wherein the object moves within the volume;

and

one or more of the functions performed by the processor are repeated at regular intervals to track the motion of the object.

15. The apparatus of claim 12, wherein the computed characteristics include the strength, position and orientation of the secondary source.

16. The apparatus of claim 12, wherein the volume includes at least a portion of a vehicle interior, and wherein the probe sensor is supported relative to an operator of the vehicle.

17. The apparatus of claim 16, wherein vehicle interior forms part of an aircraft cockpit, and wherein the probe sensor is mounted on a helmet worn by the operator.

18. The apparatus of claim 12, wherein the secondary source is approximated as a point or dipole source or sources.

19. The apparatus of claim 12, wherein each witness sensor measures three components of the induction vector along three orthogonal axes.

20. A method of determining the position and orientation of an object within a bounded volume in the presence of electromagnetic distortion, comprising the steps of:

a) generating a primary electromagnetic field from a stationary source at a frequency;

b) providing a probe sensor on the object having a known distortion profile at the frequency which generates a secondary electromagnetic field with measureable magnetic induction-vector components;

c) placing a witness sensor at one or more stationary points near or within the volume, each witness sensor being operative to detect the magnetic induction-vector components of the secondary field;

d) computing the characteristics of the secondary electromagnetic source with respect to each witness sensor, and

e) computing the position and orientation of the object given the computed characteristics of the secondary source in conjunction with the fixed position and orientation of each witness sensor relative to the stationary source.

21. The method of claim 20, wherein:

steps d) and e) are performed prior to step b) to compute a background profile of the primary field; and

steps d) and e) are repeated at regular intervals following step b) to track the motion of the object.

22. The method of claim 20, wherein the step of computing the characteristics of the secondary electromagnetic field include computing the strength, position and orientation of the field.

23. The method of claim 20, wherein the object is positioned within a vehicle interior.

24. The method of claim 20, wherein the object is supported on the body of an individual.

25. The method of claim 20, further including the step of approximating the secondary source as a point or dipole source or sources.

26. The method of claim 20, wherein three components of the induction vector are measured at each stationary point.