Launch monitor system with a calibration fixture and a method for use thereof

• US 6,781,621 B1
• Filed: 03/29/2000
• Issued: 08/24/2004
• Est. Priority Date: 09/18/1998
• Status: Expired due to Fees

• Current Assignee: Acushnet Company (FILA Holdings Corp.)
• Original Assignee: Acushnet Company (FILA Holdings Corp.)
• Inventors: Aoyama, Steven, Pelletier, Diane I., Hebert, Edmund A., Winfield, Douglas C., Gobush, William, Days, Charles, Silveira, James Alan
• Primary Examiner(s): Kelley, Chris
• Assistant Examiner(s): BUGG, GEORGE A
• Application Number:
  US09/537,295
• Time in Patent Office: 1,609 Days
• Field of Search: 348/61, 348/169-172, 348/77, 348/78, 348/135-140, 348/157, 348/189
• US Class Current: 348/157
• CPC Class Codes: A63B 43/008 with means for improving visibility, e.g. special markings or colours illuminating or reflecting means A63B43/06
• CPC Class Codes: A63B 69/3614 using electro-magnetic, magnetic or ultrasonic radiation emitted, reflected or interrupted by the golf club

Abstract

The present invention is directed to a launch monitor system that measures flight characteristics of an object moving in a predetermined field-of-view. The system includes a support structure, a lighting unit, a camera unit disposed on the support structure, and a calibration assembly. The calibration assembly includes a calibration fixture and at least one telescoping member. A first end of the telescoping member is coupled to the support structure and a second end is contactable with or coupled to the fixture. In an extended position of the telescoping member, the calibration fixture is in the field-of-view of the camera unit. In a retracted position, the calibration fixture out of the field-of-view. The calibration fixture further includes contrasting markings. In another embodiment, the system includes a frame and the launch monitor is pivotally suspended from the frame so that it self-levels. The present invention further includes a method of calibrating a launch monitor having a calibration fixture.

Claims

1. A launch monitor system for measuring flight characteristics of an object moving in a predetermined field-of-view, the system comprising:

a support structure;

a lighting unit disposed on the support structure and directing light into the predetermined field-of-view;

a first camera unit disposed on the support structure and pointed toward the predetermined field-of-view; and

a calibration assembly including

a calibration fixture; and

at least one telescoping member having a first end coupled to the support structure and a second end contactable with the calibration fixture, wherein the telescoping member has an extended position placing the calibration fixture in the field-of-view of the first camera unit;

wherein the calibration fixture is coupled to the second end of the telescoping member, and the telescoping member has a retracted position where the calibration fixture is out of the field-of-view of the first camera unit; and

wherein the calibration fixture further includes a back wall and first, second and third walls spaced from one another and extending outwardly from the back wall, and two legs, each leg being pivotally connected to the first and second walls.

2. The launch monitor system of claim 1, wherein the calibration fixture further includes contrasting markings in at least two different planes.

3. The launch monitor system of claim 2, wherein the contrasting markings are reflective markings.

4. The launch monitor system of claim 2, wherein the contrasting markings are painted markings.

5. The launch monitor system of claim 2, wherein the calibration fixture further includes contrasting markings in at least three different planes.

6. The launch monitor system of claim 1, further including a second camera unit disposed on the support structure and pointed toward the predetermined field-of-view, and the telescoping member is disposed between the first camera unit and the second camera unit.

7. The launch monitor system of claim 6, further including a computer with at least one algorithm, each camera for taking at least one image of the calibration fixture, wherein the computer converts each image into calibration data.

8. A launch monitor system for measuring flight characteristics of an object moving in a predetermined field-of-view, the system comprising:

a support structure;

a lighting unit disposed on the support structure and directing light into the predetermined field-of-view;

a first camera unit disposed on the support structure and pointed toward the predetermined field-of-view; and

a calibration assembly including;

a calibration fixture; and

at least one telescoping member having a first end coupled to the support structure and a second end contactable with the calibration fixture, wherein the telescoping member has an extended position placing the calibration fixture in the field-of-view of the first camera unit;

wherein the calibration fixture includes contrasting markings in at least three different planes; and

wherein the calibration fixture further includes a back wall and first, second and third walls spaced from one another and extending outwardly from the back wall.

9. The launch monitor system of claim 8, wherein the first and second walls are disposed on either side of the third wall, the first and second walls have a first length and the third wall has a second length different from the first length.

10. The launch monitor system of claim 9, wherein the first length is less than the second length.

11. The launch monitor system of claim 9, wherein the first length is greater than the second length.

12. The launch monitor system of claim 8, wherein the contrasting markings are disposed on the free ends of the first, second, and third walls and a surface of the back wall.

13. The launch monitor system of claim 12, wherein the contrasting areas are retro-reflective dots.

14. The launch monitor system of claim 13, wherein one row is disposed on the free end of each first, second, and third wall, and the remaining two rows are disposed on the back wall on either side of the third wall.