Head mounted information systems and related methods

• US 9,354,447 B2
• Filed: 01/18/2011
• Issued: 05/31/2016
• Est. Priority Date: 01/18/2010
• Status: Active Grant

• Current Assignee: Intel Corporation
• Original Assignee: Intel Corporation
• Inventors: Abdollahi, Hamid, Eisenhardt, Dan, Chen, Li, Lee, David Robertson
• Primary Examiner(s): Wang, Quan-Zhen
• Assistant Examiner(s): Liang, Dong Hui
• Application Number:
  US13/522,684
• Publication Number:
  US 20130044043A1
• Time in Patent Office: 1,960 Days
• US Class Current: 1/1
• CPC Class Codes: A42B 3/0433 Detecting, signalling or lighting devices
• CPC Class Codes: A63B 2071/0666 worn on the head or face, e.g. combined with goggles or glasses
• CPC Class Codes: A63B 2220/12 Absolute positions, e.g. by using GPS
• CPC Class Codes: A63B 2220/30 Speed
• CPC Class Codes: A63B 2220/34 Angular speed
• CPC Class Codes: A63B 2220/40 Acceleration
• CPC Class Codes: A63B 2220/44 Angular acceleration
• CPC Class Codes: A63B 2244/19 Skiing
• CPC Class Codes: A63B 2244/203 Diving
• CPC Class Codes: A63B 69/18 for skiing
• CPC Class Codes: A63B 71/0619 Displays, user interfaces and indicating devices, specially adapted for sport equipment, e.g. display mounted on treadmills
• CPC Class Codes: A63B 71/0622 Visual, audio or audio-visual systems for entertaining, instructing or motivating the user
• CPC Class Codes: A63B 71/0669 Score-keepers or score display devices
• CPC Class Codes: A63C 2203/18 Measuring a physical parameter, e.g. speed, distance
• CPC Class Codes: A63C 2203/24 Processing or storing data, e.g. with electronic chip
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G02B 2027/014 comprising information/image processing systems
• CPC Class Codes: G02B 2027/0187 slaved to motion of at least a part of the body of the user, e.g. head, eye
• CPC Class Codes: G02B 27/017 Head mounted

Abstract

A head mounted information system comprises a frame configured to be worn by a user, a sensor unit coupled to the frame, and a processor unit coupled to the frame. The processor unit is connected to receive signals from the sensor unit. The sensor unit comprises a gyroscope configured to produce angular velocity signals representing a head angular velocity about a generally horizontal axis oriented generally perpendicular to a direction the user is facing when the user is wearing the frame. The processor unit is configured to detect a jump by the user based on the angular velocity signals received from the sensor unit and generate a jump output signal indicting one or more jump parameters. A display unit may also be coupled to the frame to display the jump parameters to the user.

Claims

1. A head mounted information system comprising:

a frame configured to be worn by a user;

a sensor unit coupled to the frame, the sensor unit comprising a gyroscope configured to produce angular velocity signals representing a head angular velocity about a generally horizontal z-axis oriented generally perpendicular to a direction the user is facing when the user is wearing the frame; and

,

a processor unit coupled to the frame, the processor unit connected to receive signals from the sensor unit,

wherein the processor unit is configured to receive the angular velocity signals from the sensor unit, monitor the head angular velocity to determine a first peak angular velocity and a second peak angular velocity, calculate a head angular acceleration by taking a derivative of the head angular velocity, detect a jump by the user when the head angular velocity indicates upward head tilting exceeding a first jumping angular velocity threshold, the head angular acceleration indicates upward head tilting exceeding an angular acceleration threshold and an absolute value of a sum of the first and second peak angular velocities exceeds a second jumping angular velocity threshold, and

wherein the processor is further configured to generate a jump output signal indicting one or more jump parameters.

2. A system according to claim 1 wherein the processor is configured to detect a head nod and generate a head nod output signal when the head angular velocity exceeds a first nodding angular velocity threshold, and:

the head angular velocity does not exceed the first jumping angular velocity threshold;

the head angular acceleration does not exceed the angular acceleration threshold;

or,

the absolute value of the sum of the first and second peak angular velocities does not exceed the second jumping angular velocity threshold.

3. A system according to claim 2 wherein the processor is configured to generate the head nodding signal only when the absolute value of the sum of the first and second peak angular velocities is less than a second nodding angular velocity threshold and a time interval between occurrences of the first and second peak angular velocities is less than a nodding time threshold.

4. A system according to claim 1 wherein the processor is configured to determine a takeoff time comprising a time at which a maximum upward head angular velocity occurs.

5. A system according to claim 4 wherein the processor is configured to detect a landing when the head angular velocity indicates downward head tilting exceeding a landing angular velocity threshold, and to determine a landing time comprising a time at which a maximum downward head angular velocity occurs.

6. A system according to claim 5 wherein the jump output signal comprises a jump airtime, and the processor is configured to calculate the jump airtime by taking a difference between the landing time and the takeoff time.

7. A system according to claim 4 wherein the processor is configured to determine a time period during which the head angular velocity indicates downward head tilting, to detect a landing when the time period exceeds a landing time threshold, and to determine a landing time comprising a midpoint of the time period.

8. A system according to claim 1 wherein the sensor unit comprises a GPS receiver configured to produce speed signals representing a speed of the user.

9. A system according to claim 8 wherein the processor is configured to detect a jump only if the speed of the user exceeds a speed threshold.

10. A system according to claim 1 wherein the sensor unit comprises a three axis accelerometer configured to produce acceleration signals representing linear accelerations of the user, and wherein the processor is configured to determine a speed of the user based on the acceleration signals.

11. A system according to claim 1 comprising a display unit coupled to the frame, the display unit comprising a display for producing an image, wherein the processor is configured to produce a video output signal comprising at least in part the jump output signal and provide the video output signal to the display unit for displaying the one or more jump parameters to the user.

12. A system according to claim 11 wherein the video output signal indicates at least a jump airtime.

13. A system according to claim 1 wherein the processor is configured to transform the angular velocity signals from a time domain to a frequency domain and detect a jump when a frequency spectrum of the angular velocity signals has a peak above a jump frequency threshold.

14. A system according to claim 13 wherein the processor is configured to determine a takeoff time based on a time at which the peak in the frequency spectrum occurs.

15. A system according to claim 13 wherein the processor is configured to detect a landing when a frequency spectrum of the angular velocity signals has a peak above a jump frequency threshold.

16. A system according to claim 15 wherein the processor is configured to determine a landing time based on a time at which the peak in the frequency spectrum occurs.

17. A system according to claim 13 wherein the jump frequency threshold is 40Hz.

18. A system according to claim 1 wherein the sensor unit comprises a three axis gyroscope configured to produce angular velocity signals about the z-axis, an x-axis and a y-axis, wherein the x-axis and y-axis are generally perpendicular to each other and to the z-axis, and wherein the processor is configured to, after detecting a jump and before detecting a landing, determine rotations about the x-axis, y-axis and z-axis.

19. A system according to claim 18 wherein the processor is configured to display orientation information in real time based on the determined rotations.

20. A system according to claim 18 wherein the processor is configured to provide spin information in the jump output signal based on the determined rotations.

21. A system according to claim 18 wherein the processor is configured to provide a jump success indication in the jump output signal based on the determined rotations.

22. A system according to claim 21 wherein the jump success indication is positive when the processor determines a y-axis rotation equal to an integer multiple of 180 degrees, and the jump success indication is negative when the processor determines a y-axis rotation equal to an odd integer multiple of 90 degrees.

23. A system according to claim 1 comprising:

a display unit coupled to the frame, the display unit comprising a display for producing an image;

wherein the processor unit is configured to produce a video output signal indicating performance information based on signals received from the sensor unit and provide the video output signal to the display unit for displaying the performance information to the user.

24. A system according to claim 23 incorporated into a pair of goggles.

25. A system according to claim 23 incorporated into a helmet.

26. A system according to claim 23 wherein the display unit is incorporated into pair of goggles and the sensor unit and the processor unit are incorporated into a helmet.

27. A method of determining one or more jump parameters of a user of a head mounted information system comprising a gyroscope mounted on a frame configured to be worn by the user, the gyroscope configured to produce angular velocity signals representing a head angular velocity about a generally horizontal axis oriented generally perpendicular to a direction the user is facing when the user is wearing the frame, the method comprising:

comparing the head angular velocity to a first jumping angular velocity threshold;

calculating a head angular acceleration by taking a derivative of the head angular velocity and comparing the head angular acceleration to an angular acceleration threshold;

determining a first peak angular velocity and a second peak angular velocity and comparing an absolute value of a sum of the first and second peak angular velocities to a second jumping angular velocity threshold; and

detecting a jump occurrence when the head angular velocity indicates upward head tilting exceeding the first jumping angular velocity threshold, the head angular acceleration indicates upward head tilting exceeding the angular acceleration threshold and the absolute value of the sum of the first and second peak angular velocities exceeds the second jumping angular velocity threshold and;

providing an output signal to the user indicating the jump occurrence.

28. A method according to claim 27 comprising determining a takeoff time comprising a time at which a maximum upward head angular velocity occurs.

29. A method according to claim 28 comprising detecting a landing when the head angular velocity indicates downward head tilting exceeding a landing angular velocity threshold, and determining a landing time comprising a time at which a maximum downward head angular velocity occurs.

30. A method according to claim 29 comprising calculating a jump airtime by taking a difference between the landing time and the takeoff time, wherein the output signal indicates the jump airtime.

31. A method according to claim 28 comprising determining a time period during which the head angular velocity indicates downward head tilting, detecting a landing when the time period exceeds a landing time threshold, and determining a landing time comprising a midpoint of the time period.

32. A method according to claim 27 wherein the gyroscope is configured to produce angular velocity signals about three generally perpendicular axes, the method comprising:

detecting a jump takeoff;

detecting a jump landing;

integrating the angular velocity signals from the gyroscope between the jump takeoff and the jump landing to determine rotations about the three generally perpendicular axes; and

,

generating a jump output signal comprising spin information based on the determined rotations.

33. A method of determining one or more jump parameters of a user of a head mounted information system comprising a gyroscope mounted on a frame configured to be worn by the user, the gyroscope configured to produce angular velocity signals representing a head angular velocity about a generally horizontal axis oriented generally perpendicular to a direction the user is facing when the user is wearing the frame, the method comprising:

transforming the angular velocity signals from a time domain into a frequency domain;

monitoring the head angular velocity to determine a first peak angular velocity and a second peak angular velocity;

calculating a head angular acceleration by taking a derivative of the head angular velocity,

detecting a jump occurrence when a peak in frequency domain angular velocities occurs above a jump frequency threshold, the head angular velocity indicates upward head tilting exceeding a first jumping angular velocity threshold, the head angular acceleration indicates upward head tilting exceeding an angular acceleration threshold and an absolute value of a sum of the first and second peak angular velocities exceeds a second jumping angular velocity threshold; and

,

providing an output signal to the user indicating the jump occurrence.

34. A method according to claim 33 comprising determining a takeoff time based on a time at which the peak in frequency domain angular velocities occurs.

35. A method according to claim 33 comprising detecting a landing when a second peak in frequency domain angular velocities occurs above the jump frequency threshold.

36. A method according to claim 35 comprising determining a landing time based on a time at which the second peak in frequency domain angular velocities occurs.

37. A method according to claim 33 wherein the jump frequency threshold is 40Hz.