Method for calibrating a navigation system

• US 9,675,424 B2
• Filed: 07/22/2009
• Issued: 06/13/2017
• Est. Priority Date: 06/04/2001
• Status: Active Grant

• Current Assignee: Surgical Navigation Technologies, Inc. (Medtronic Plc)
• Original Assignee: Surgical Navigation Technologies, Inc. (Medtronic Plc)
• Inventors: Jascob, Bradley, Kessman, Paul, Smith, Aaron, Simon, David
• Primary Examiner(s): Le, Son
• Assistant Examiner(s): ALLGOOD, ALESA M
• Application Number:
  US12/507,722
• Publication Number:
  US 20090287443A1
• Time in Patent Office: 2,883 Days
• Field of Search: 324202, 32420723, 32420713, 32420717, 600424, 702150
• CPC Class Codes: A61B 2017/00725 Calibration or performance testing
• CPC Class Codes: A61B 2034/2051 Electromagnetic tracking systems
• CPC Class Codes: A61B 2034/2072 Reference field transducer attached to an instrument or patient
• CPC Class Codes: A61B 2090/0481 against EM radiation, e.g. microwave
• CPC Class Codes: A61B 2090/376 using X-rays, e.g. fluoroscopy
• CPC Class Codes: A61B 34/20 Surgical navigation systems; Devices for tracking or guiding surgical instruments, e.g. for frameless stereotaxis
• CPC Class Codes: A61B 90/36 Image-producing devices or illumination devices not otherwise provided for

Abstract

A method and apparatus for electromagnetic navigation of a surgical probe near a metal object. The electromagnetic navigation system includes a transmitter coil array and a shield. The transmitter coil array has a plurality of transmitter coils and is operable to generate the electromagnetic field to navigate the probe. The shield is positioned adjacent the metal object and is operable to shield the metal object from the electromagnetic field generated by the transmitter coil array, such that the shield substantially reduces distortion of the electromagnetic field by the metal object.

Claims

1. A method for calibrating an electromagnetic navigation system having a transmitter coil array that generates an electromagnetic field in a procedure region, said method comprising:

(a) positioning the electromagnetic navigation system in a working environment having a metallic object outside of the procedure region of the electromagnetic field that causes a metallic distortion in the electromagnetic field in the procedure region, wherein an instrument is positionable in the procedure region within a portion of the electromagnetic field;

(b) positioning a calibration sensor at a first calibration point in the procedure region of the working environment;

(c) energizing a first coil in the transmitter coil array to generate a first field of the electromagnetic field;

(d) sensing a first field strength of the first field with the calibration sensor in the procedure region; and

(e) positing the calibration sensor at a second calibration point in the procedure region of the working environment and repeating (c) and (d) at the second calibration point, wherein effects of the metallic distortion caused by the metallic object are taken into account during the calibration and wherein the metallic object is a medical device.

2. The method as defined in claim 1 wherein positioning the calibration sensor at a first calibration point further comprises utilizing a robotic unit to position the calibration sensor at the first calibration point.

3. The method as defined in claim 1 further comprising creating a look-up table for a plurality of calibration points which is operable to be used during a navigation process, where the look-up table stores field strengths for the plurality of calibration points that take into affect the metallic distortion of the electromagnetic field caused by the metallic object.

4. The method as defined in claim 1 further comprising energizing the plurality of coils in the transmitter coil array in at least one of a time division multiplex manner, frequency division multiplex manner, or a combination of both.

5. The method as defined in claim 1 further comprising energizing a plurality of coils sequentially in the transmitter coil array to generate a plurality of fields of the electromagnetic field and sensing field strengths of each of the plurality of fields with the calibration sensor.

6. The method as defined in claim 5 further comprising repeating step (e) to generate about eight thousand calibration points.

7. The method as defined in claim 5 wherein the medical device is selected from a group consisting of an operating room table, fluoroscope, a microscope, an ultrasound hand piece, a high-intensity focused ultrasound systems, a computer topography imaging (CT)system, an interoperative computer topography, system, a magnetic resonance imaging (MR) system, an interoperative magnetic resonance system and a surgical robot.

8. The method as defined in claim 7 wherein at least one of function and movement of the medical device is simulated during the calibration process.

9. The method of claim 8, further comprising:

determining an orientation and location of a metal object.

10. The method of claim 9, wherein determining an orientation and location includes;

predetermining a position of the metal object in an area where the electromagnetic navigation system is to be used; and

maintaining the orientation and location of the metal object in the area.

11. The method as defined in claim 1 further comprising:

storing the sensed first field strength at the first calibration point and the second calibration point in a memory device; and

navigating a probe through the electromagnetic field by using the stored field strengths sensed by the calibration sensor.

12. The method as defined in claim 11 wherein navigating the probe includes navigating a probe selected from at least one of a surgical probe, catheter, steerable catheter, endoscope, shunt, drill guide, awl/tap, orthopedic instrument and a combination thereof.

13. The method as defined in claim 11 further comprising providing a dynamic reference arc that is affixed relative to a patient and used as a reference point for the probe.

14. The method as defined in claim 11 further comprising comparing the stored field strengths sensed by the calibration sensor with field strengths measured by the probe.

15. The method as defined in claim 14 further comprising using the stored field strengths sensed by the calibration sensor to interpolate fields at a guess point in space.

16. The method as defined in claim 15 further comprising computing the difference in field strengths between the guess point with the field strength measured by the probe.

17. The method as defined in claim 16 further comprising using the measured difference to refine the guess point during a minimization process to select a new guess point that is closer to the probe location.

18. The method as defined in claim 17 further comprising minimizing the error between the guess point and the actual location of the probe to an acceptable value.

19. The method of claim 18, further comprising:

selecting the guess point in three dimensional space; and

determining the error between electromagnetic field strengths at the selected guess point and the sensed electromagnetic field strengths at the actual location of the probe; and

wherein the actual location of the probe is the location of the probe in three dimensional space.

20. A method for calibrating an electromagnetic navigation system having a transmitter coil array that generates an electromagnetic field in a three dimensional space, said method comprising:

positioning a metallic object adjacent at least a procedure region of the electromagnetic field;

positioning a calibration sensor at a first calibration point in the three dimensional space, energizing a plurality of coils sequentially in the transmitter coil array to generate a plurality of fields of the electromagnetic field;

sensing first field strengths of each of the plurality of fields with the calibration sensor at the first calibration point; and

moving the calibration sensor to a second calibration point in the three dimensional space different from the first calibration point, energizing the plurality of coils sequentially in the transmitter coil array to generate the plurality of fields;

sensing second field strengths of each of the plurality of fields with the calibration sensor at the second calibration point; and

storing the sensed first field strengths and the second field strengths;

wherein effects of metallic distortion caused by the metallic object is taken into account during the calibrating at least by sensing the generated first field strengths and second field strengths that include distortion due to the metallic object.

21. The method of claim 20, further comprising:

maintaining the position of the metallic object relative to the transmitter coil array after calibrating the electromagnetic system having the transmitter coil array.

22. The method as defined in claim 20 further comprising positioning the calibration sensor at a plurality of different calibration points in the three dimensional space different from any previous calibration point, energizing the plurality of coils sequentially in the transmitter coil array to generate the plurality of fields, and sensing a field strength of each of the plurality of fields with the calibration sensor at each of the plurality of different calibration points;

wherein the metallic object is away from the plurality of different calibration points and affects the sensed field strength at each calibration point.

23. The method of claim 22, wherein positioning the calibration sensor at a plurality of different calibration points in the three dimensional space includes moving the calibration sensor to each of the plurality of different calibration points with a robotic unit.

24. The method of claim 22, wherein the plurality of different calibration points is in a grid pattern in the three dimensional space.

25. The method of claim 22, wherein the plurality of different calibration points include substantially all of the points that are about 15 millimeters apart in a one (1) cubic meter three dimensional volume.

26. The method of claim 25, wherein the sensed field strengths at all of the plurality of different calibration points in the three dimensional volume are stored in a storage device.

27. The method of claim 26, wherein the storage device stores all of the sensed field strengths at the plurality of different calibration points in a look-up table that is operable to be accessed during a navigated procedure.

28. The method of claim 27, further comprising:

interpolating a physical location of an instrument in the three dimensional space based upon the stored plurality of different calibration points including;

positioning an instrument in the three dimensional space at an instrument point;

energizing the plurality of coils in the transmitter coil array to generate fields;

sensing field strengths of the fields generated by the plurality of coils in the transmitter coil array at the instrument point; and

comparing the sensed fields at the instrument point to the look-up table.

29. The method of claim 28, further comprising:

interpolating a sensed field strength relative to those in the look-up table when the sensed field at the instrument is not identical to one of the sensed field strengths at the plurality of different calibration points in the look-up table.

30. The method of claim 29, wherein interpolating the sensed field strength includes linear interpolation and spline interpolation of the sensed field strength relative to those in the look-up table.

31. The method of claim 29, wherein comparing the sensed fields at the instrument to the look-up table includes:

selecting a guess point in the three dimensional space;

determining an error between field strengths at the selected guess point and the sensed fields at the instrument point; and

minimizing the determined error.

33. The method of claim 31, wherein positioning a calibration sensor at a calibration position in three dimensional space includes positioning the calibration sensor at a plurality of different positions in the three dimensional space and sensing electromagnetic field strengths generated by a plurality of coils of the transmitter coil array.

34. The method of claim 33, wherein instructing a coil array controller to drive a particular coil in the transmitter coil array includes driving the particular coil in a time multiplex manner, frequency multiplex manner, or sequential manner relative to other coils in the transmitter coil array.

35. The method of claim 33, wherein the plurality of different positions in the three dimensional space substantially defines a selected grid of points in the three dimensional space;

wherein positioning a calibration sensor at the plurality of different positions in the three dimensional space includes moving the calibration sensor with a robotic device to each point of the selected grid of points in the three dimensional space.

36. The method of claim 33, further comprising:

maintaining the position of the metallic object relative to the transmitter coil array after storing the determined electromagnetic field strengths at the plurality of different positions.

41. The method of claim 36, further comprising:

interpolating between stored electromagnetic field strengths to determine the location of the instrument in the three dimensional space if the sensed electromagnetic field strengths with the instrument are not identical to stored strengths in the storage device.

42. The method of claim 41 wherein the plurality of different positions in the three dimensional space defines a grid in the three dimensional space to allow for interpolation between the plurality of different positions in the three dimensional space.

43. The method of claim 42, wherein the grid in the three dimensional space is defined by the plurality of different positions about 15 millimeters apart within the three dimensional space.

44. The method of claim 43, wherein the three dimensional space is about one (1) cubic meter.

32. A method for calibrating an electromagnetic navigation system having a transmitter coil array integral with a metallic object that generates an electromagnetic field in a three dimensional space, said method comprising:

operating the transmitter coil array that is integral with the metallic object that generates the electromagnetic field in the three dimensional space;

positioning a calibration sensor at a calibration position in three dimensional space;

instructing a coil array controller to drive a particular coil in the transmitter coil array to generate at least a portion of the electromagnetic field that includes metallic distortion effect due to the metallic object;

sensing at least a portion of the electromagnetic field having the metallic distortion effect with the calibration sensor at the calibration position;

determining an electromagnetic field strength of the sensed at least a portion of the electromagnetic field having the metallic distortion effect for the calibration position by a navigation probe interface; and

storing the determined electromagnetic field strength at the calibration position with a storage device;

wherein effects of metallic distortion effect caused by the metallic object is taken into account during the calibrating at least by sensing the generated at least a portion of the electromagnetic field that includes distortion due to the metallic object.

37. The method of claim 32, wherein the determined electromagnetic field strengths generated by all of the coils of the transmitter coil array are stored in the storage device.

38. The method of claim 37, wherein all of the stored determined electromagnetic field strengths are saved in a look-up table.

39. The method of claim 38, further comprising:

determining a location of an instrument in the three dimensional space including;

sensing a generated electromagnetic field strength of all of the coils in the transmitter coil array in three dimensional space;

comparing the sensed electromagnetic field strengths generated by all of the coils in the transmitter coil array to the look-up table; and

determining the location of the instrument based upon the comparison of the sensed electromagnetic field strengths with the instrument to the look-up table.

40. The method of claim 39, wherein comparing the sensed electromagnetic field strengths generated by all of the coils in the transmitter coil array to the look-up table includes:

selecting a guess point in three dimensional space;

determining an error between electromagnetic field strengths at the selected guess point and the sensed electromagnetic field strengths at the instrument point; and

minimizing the determined error.