US20050026710A1

US20050026710A1 - Apparatus and method for monitoring launch parameters of a launched sports object

Info

Publication number: US20050026710A1
Application number: US10/884,396
Authority: US
Inventors: Yi-Ching Pao
Original assignee: Individual
Current assignee: Individual
Priority date: 2003-08-01
Filing date: 2004-07-01
Publication date: 2005-02-03
Also published as: WO2005011823A2; WO2005011823A3

Abstract

A video image acquisition apparatus is disclosed. The apparatus has one or multiple digital cameras taking images of a flying golf ball created by at least two flashes or strobes of light on continuous video mode at a predetermined frame rate. Each image frame is then subtracted from the background and compared to determine the existence of the ball image in flight thus eliminating a dependency upon the camera shutter speed which must be synchronized with the flashes in prior art design. Furthermore, another video image acquisition apparatus is also disclosed that consists of at least two video cameras taking images of flying golf balls created by at least two flashes or strobes of light at predetermined time intervals. The apparatus then applies triangulate calculation of the two camera images to determine the exact physical locations of the flying golf balls in space at a given time of flight.

Description

CROSS REFERENCE TO RELATED APPLICATION

This utility patent application is based upon thus claims the priority of a provisional application Ser. No. 60/491,886, filed Aug. 1, 2003, by the same inventor.

BACKGROUND OF THE INVENTION

1. Field of the Invention
The present invention relates generally to the field of electronic monitoring of high-speed events. More particularity, the present invention is directed to a video image acquisition apparatus for monitoring launch parameters of a launched sports object such as a flying golf ball.
2. Description of the Related Art
There are a number of apparatus or monitoring systems available since the 70's to measure high-speed events, in particular the launch parameters of flying golf balls. However, any apparatus or systems designed for measuring golf ball launch parameters will have some inherent limitations as well as optimal operational specifications. Over the years, high-speed camera and/or stroboscopic photography technologies have been used by a number of golf equipment manufacturers in the development process for golf ball and golf club such as the early invention of U.S. Pat. No. 4,158,853. As this type of technology has become increasingly prevalent for the measurement of golf ball launch parameters, the use of high-speed camera images has become more available and sophisticated such as described in U.S. Pat. Nos. 5,471,383, 6,241,622, 6,579,190 and 6,592,465.
However, all these prior arts use similar approaches with high shutter speed and multi-shuttering camera or cameras to capture two-dimensional (2-D) fast flying ball images for launch parameter calculations. These require specialty and expensive high shutter speed or multi-shuttering camera and cameras to meet the image capturing requirements. Furthermore, the physical locations of the balls in space at any given time is not precisely measured as limited by the camera resolution and image distortion to be described later. Inherent measurement errors of these 2-D high speed camera and stroboscopic photography systems fall into two categories, namely camera hardware limitations (such as camera pixel resolution, focus, and lens distortion) and dynamic set-up variables (operator and system setup related variables such as camera height and distance to ball, camera leveling). As described herein, these components of measurement error have an interdependent relationship with one another, meaning that the accuracy of each parameter depends upon the accuracy of every other parameter.
During golf ball launch, a 2-D camera system is often used to measure ball speed, launch angle, back-spin RPMs (revolutions per minute), and sometimes azimuth (in degrees of Push or Pull) and side-spin RPMs. By accurately measuring these parameters, algorithms shaped by field-testing and calibration can be used to predict golf ball flight (and roll). The purpose of the camera is to capture two or more successive images of a high-speed occurrence—a speeding golf ball moving up to 200 MPH (miles per hour) with a ball spin of up to 12,000 RPMs and launch angles from 0 to 65 degrees. These images are then processed by image recognition software or spatial mapping software that calculates the launch parameters of the shot based upon the movement of pre-defined markings on the golf ball over a series of images.
To provide image processing software with meaningful images to accurately calculate golf ball launch parameters, the orientation of the camera along the x-, y-, and z-axes spatially, as well as the side to side and/or up and down position of the camera lens, for every starting and dynamic ball location, are critical. Otherwise, parallax views will severely limit the ability of a camera system to provide representative images of the golf ball launch parameters (a three-dimensional occurrence), hence limiting the accuracy of prediction of ball flight and roll with such systems. A good illustrative example of error from parallax view is when one tries to measure ball speed with a 2-D camera positioned at a perpendicular angle to the target line. To better understand the concept of parallax viewing error, imagine trying to read the gas gauge of our automobile from the passenger seat. Here, the fuel gauge does not appear the same way as it does to the driver whose sitting position faces the fuel gauge straight on. Trying to measure ball speed with a non-zero azimuth with a camera system works the same way. FIG. 1 illustrates ball speed measurement error across positive (PUSH) and negative (PULL) azimuth angles. As one can see, only when the direction of the ball 5 is 90 degrees to the view angle of the camera 10 as in trajectory 1, will one get reliable and accurate results with little or minimum error. In general, shots with a (+) azimuth, a PUSH traveling towards the camera 10 as in trajectory 2, will appear to have a progressively higher ball speed than the actual, while those shots with a (−) azimuth, a PULL traveling away from the camera 10 as in trajectory 3, will appear to have a progressively lower ball speed than the actual. In essence, under the circumstance of FIG. 1, the ball speed measurement calculation is dependent upon the azimuth angle of the ball 5.
Non-zero azimuth shots introduce parallax error also into the launch angle measurements of the camera 10 and this is demonstrated in FIG. 2. While the camera 10 will see the three shots depicted in the image as having the same launch angle, the shot with positive azimuth traveling towards the camera, having a trajectory 2, will have an actual launch angle lower than the reported launch angle, while the shot with negative azimuth traveling away from the camera, having a trajectory 3, will have an actual launch angle higher than the reported launch angle. In essence, under the circumstance of FIG. 2, the launch angle measurement calculation is dependent upon the azimuth angle of the ball 5 as well. Thus, unless a straight shot of 0 degrees azimuth is achieved, as signified by trajectory 1 of FIG. 1 and FIG. 2, a camera system will have the effect of parallax error spill into both ball speed and launch angle calculations. Furthermore, when using correction formulas to compensate for the effect of azimuth errors on other parameters, the azimuth angle itself is often miscalculated due to difficulty of producing an accurate azimuth calculation. While some prior art attempts to reconcile the errors of ball speed and launch angle with an azimuth estimation and correction formulas based on size variations of the ball image are presented such as in U.S. Pat. No. 6,579,190, the limitation or pixel resolution of typically-used high shutter speed cameras results in an azimuth accuracy limited to +/−3 or 5 degrees, or equivalently a 6-10 degrees error variance by using single camera picture with multiple ball sizes or diameters captured with multiple shutter sequences. The physical diameter of a golf ball, as compared to the frame size required to capture multiple ball images in launch condition, limits the resolution to accurately estimate the ball azimuth angle. Simply put, a wrongful use of the azimuth correction formula can easily result in a 5+ MPH error in ball speed and a 3+ degrees error in launch angle. The present invention successfully provides better and improved solutions to the camera feature requirements and measurement of actual ball locations.

SUMMARY OF THE INVENTION

The present invention relates to video apparatus for improved monitoring of the launch position, velocity and spins of a golf ball. By using stroboscopic photography with at least two flashes at a predetermined interval triggered by either acoustic, optical or electronic means and a digital CMOS (Complementary Metal-Oxide-Semiconductor) or CCD (charge coupled device) camera system, running at a continuous video mode, the present invention is capable of capturing all needed ball image information for computer processing, analysis and display of useful data. Furthermore, according to one embodiment of the present invention, a dual camera system with at least two cameras spaced out by a distance greater than the ball diameter and mounted preferably vertically to the ground is capable of providing much improved measurement of ball location in three-dimensional space at the times of the flashes, hence enabling more precise determination of the ball azimuth angle, ball speed, and launch angle.
Preferred embodiments of the present invention are presented including a dual camera system interfaced with a data collecting computer, flashes with trigger mechanism located at a given distance to the ball flight trajectory path.
To the accomplishment of the above and related objects, this invention may be embodied in the form illustrated in the accompanying drawings, attention being called to the fact, however, that the drawings are illustrative only, and that changes may be made in the specific construction illustrated.

BRIEF DESCRIPTION OF THE DRAWINGS

Various other objects, features and attendant advantages of the present invention will become fully appreciated as the same becomes better understood when considered in conjunction with the accompanying drawing, in which like reference characters designate the same or similar parts throughout the several views, and wherein:
FIG. 1 illustrates prior art ball speed measurement error across positive (PUSH) and negative (PULL) azimuth angles;
FIG. 2 illustrates the parallax error of prior art launch angle measurements from non-zero azimuth shots;
FIG. 3 illustrates a preferred embodiment and arrangement of the present invention wherein a dual camera system interfaced with a data collecting computer and flashes with triggering mechanism located at a given distance to a ball flight trajectory path;
FIG. 4 illustrates two captured flying golf ball images each with a ball mark in a high speed camera or a stroboscopic photography system;
FIG. 5 illustrates two different modes of camera shuttering design used in a stroboscopic photography system, they are (a) prior art high shutter speed camera which must synchronize its timing with the strobe or flash light pulses and (b) the continuous mode of operation which is independent to strobe or flash light pulses according to the present invention;
FIG. 6 shows two ball images captured through the present invention of digital camera running at continuous video mode followed by applying image subtraction and enhancement technique;
FIG. 7 illustrates an improved way of measuring the ball azimuth position with a dual camera system of the present invention;
FIG. 8 shows ball images obtained from the dual camera system of the present invention, they are (a) ball image captured from the top camera and (b) ball image captured from the bottom camera;
FIG. 9 illustrates a preferred camera arrangement of the present invention with vertical mounting; and
FIG. 10 illustrates a horizontal camera mounting with associated creation of undesirable shift in the ball images.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

In the following detailed description of the present invention, numerous specific details are set forth in order to provide a thorough understanding of the present invention. However, it will become obvious to those skilled in the art that the present invention may be practiced without these specific details. In other instances, well-known methods, procedures, materials, components and circuitry have not been described in detail to avoid unnecessary obscuring aspects of the present invention. The detailed description is presented largely in terms of simplified orthogonal and perspective views. These descriptions and representations are the means used by those experienced or skilled in the art to concisely and most effectively convey the substance of their work to others skilled in the art.
Reference herein to “one embodiment” or an “embodiment” means that a particular feature, structure, or characteristics described in connection with the embodiment can be included in at least one embodiment of the invention. The appearances of the phrase “in one embodiment” in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. Further, the order of process flow representing one or more embodiments of the invention do not inherently indicate any particular order nor imply any limitations of the invention.
FIG. 3 illustrates a preferred embodiment and arrangement of the present invention wherein a dual camera system, including camera A 26 and camera B 28, interfaced with a data collecting computer 30 and a flash light 24 with a flash light trigger 22 located at a given distance to a ball flight trajectory 18. The data collecting computer 30 has a computer display 32 for displaying information. Two ball images 14 and 16 that reflect the stroboscopic images, created by two flashes emitted by the flash light 24 after triggering by the flash light trigger 22, are referenced to the tee 20 location through a ball flight trajectory 18.
FIG. 4 illustrates two captured and displayed flying golf ball images 40 and 42 respectively with ball marks 40 a and 42 a in a typical high shutter speed camera or a stroboscopic photography system. Numerous ball flight parameters are calculated according to these ball images 40 and 42 immediately after launch. The ball marks 40 a and 42 a are of the shape of a bar or line and these are typically used in the art to provide back, side and rifle spins information. Distance d between the two ball images 40 and 42 is used to calculate the ball speed and the launch angle 37 is determined by the angle between ground 36 and ball flight trajectory 38 at the tee 20 location. As illustrated earlier, the actual ball speed and launch angle are highly dependent upon the exact ball location in three-dimensional space. Thus, accurate determination of the ball locations from the camera images becomes vitally important to extract meaningful and accurate ball flight data hence predicting ball flight trajectory and ball landing distance satisfactorily.
FIG. 5 illustrates two different modes of camera shuttering design used in a stroboscopic photography system. Typical camera designs in stroboscopic photography use high shutter speed or multiple-shuttering which opens and closes successively in synchrony with the flashes or strobe lights and this is illustrated in FIG. 5(a) where the camera shutter is open when the flashlight is on and close when the flashlight is off. As the conditions of ball launch require the time interval between flashes to be very short, in the range of a couple of milliseconds, the camera shutter speed or image capturing speed need to be correspondingly fast and more often to be specially designed or customized at a much higher camera cost. The present invention, on the other hand, bypasses the use of multi-shuttering or high shutter speed camera design and, instead, uses a digital camera under a continuous video mode at a low frame rate and this is depicted in FIG. 5(b). Thus, under the present invention the shutter and frame speeds of the camera become irrelevant. Additionally, by using digital frame background subtraction and freezing and recognizing the ball images, one can achieve the same result by using almost any type of digital cameras hence drastically reducing the camera feature requirements and lowering the camera cost. FIG. 6 shows two typical ball images 44 and 46 captured through a continuous video mode followed by applying image subtraction and enhancement technique.
FIG. 7 illustrates an improved way of measuring the ball azimuth position with a dual camera system, having a camera A 26 and a camera B 28, of the present invention. With the orientation of FIG. 7, the ball azimuth position means the left and right position of the golf ball. In the case of a prior art such as U.S. Pat. No. 6,579,190, a single camera 50 is used to capture ball size images. A comparison of the ball size (i.e., the ball diameter bd) is then applied to determine the displacement of ball in the azimuth direction (i.e., PUSH or PULL), distance daz. As the ball diameter bd is relatively small, about 1.68 inches, the azimuth displacement daz does not create a significant difference of the camera viewing angle and this is denoted as Angle 1. Hence such a small viewing angle difference results in a low resolution of the determination of azimuth angle. However, in the case of the current invention as illustrated in the lower part of FIG. 7, the same azimuth displacement daz in our vertically spaced dual camera system, with an inter-camera distance dc greater than the ball diameter bd, creates a much more significant difference of the camera viewing angle Angle 2 and this in turn provides a much higher resolution of the determination of azimuth angle hence increasing the measurement accuracy of all major ball launch parameters such as the ball speed and launch angle. Furthermore, no ball marking is required here as the ball position is determined by using the geometric center of the ball image and this provides a solid reference and better defined image boundary in determining the actual ball location regardless of any variations in the viewing angle or the distance and the current invention is much less sensitive to variations in the external lighting condition, focusing and blurring commonly associated with the round edges of the ball. This is very different from both the single camera approach used in U.S. Pat. No. 6,579,190 and the horizontally mounted dual camera approach used in U.S. Pat. No. 5,471,383 where multiple and patterned reflective dots specially marked on the ball are used.
FIG. 8 shows some typical ball images obtained from the dual camera system of the present invention. FIG. 8(a) shows the ball images captured with camera A 26 while FIG. 8(b) shows strobe or flash light illuminated ball images captured with camera B 28. Notice that the X-axis locations of the ball images are relatively the same in both pictures.
FIG. 9 further illustrates a preferred camera arrangement of the present invention with vertically mounted camera A 26 and camera B 28. As illustrated, the two camera images obtained from the vertically mounted dual camera system present another significant improvement in that one can visualize that the ball horizontal positions (i.e., along the X-axis direction) between the two cameras are relatively the same in reference to the edges of the picture. This is so as the view angles of the two cameras are aligned along the X-axis and the difference in their view angles mainly appears along the Y-axis. Thus, this vertical arrangement of the two cameras 26 and 28 is important as the locations of the first ball image 14 and the second ball image 16 are sensitive to the ball speed and launch angle for typical low angle golf shots from drivers and low irons (e.g., in a range from a few degrees to may be 20 degrees).
On the other hand, a horizontal camera mounting of camera A 56 and camera B 58 creates unnecessary shift in the ball images and this is illustrated in FIG. 10. Specifically, the ball image locations along the X-direction are highly sensitive to the viewing angles of the cameras 56 and 58 and, which are also dependent on the ball speed where its X-axis speed component is much higher than its Y-axis component for typical ball launch conditions of low angle shots (e.g., from drivers or low irons). As a result, complicated viewing angle and special corrections become necessary when the corresponding ball image locations are separated too far apart along the X-axis as illustrated in FIG. 10. Hence the horizontal camera mounting of the dual camera system is less preferred due to its associated problem of X-axis ball image separation.

Actual field and calibration test have been conducted to validate the effectiveness of the current invention and a brief summary of such tests is listed in Table 1 that demonstrates the effectiveness and usefulness of the current invention.

TABLE 1


Actual Field Test Data With Current Invention

Actual Estimated

GA CAM Results

	Carry			Carry				Ball	Launch	Back-	Side
File	Dis-	Off-	Short	Dis-	Off-	Short	Azi-	Speed	Angle	spin	spin
Name	tance	line	Shape	tance	line	Shape	muth	(rph)	(deg)	(rpm)	(rpm)

Drivers
BRFast02	245	−5	0	251	7	0.5	−4	160	11.1	3172	625
BRFast03	230	30	3	253	12	0.5	−4	163	10.5	3355	779
BRTM01	225	30	2	244	20	0	4	147	12.6	1812	83
BRTM02	235	5	1	246	12	0	3	149	13.6	1629	18
BRTM03	230	−30	−1.5	238	−33	−0.5	−6	150	10.7	1098	−276
BRHook02	185	−50	−2	191	−52	−2.5	−6	157	11.3	3307	−1448
BRHook03	240	−25	−1	195	−17	−1.5	5	156	10.5	2508	−1492
BRSlice01	250	15	1	260	15	1	−6	159	8.5	1689	1035
BRSlice02	235	25	1.5	224	38	1.5	1	141	12.9	2325	1088
BRSlice03	235	25	1.5	245	13	1	−2	148	14	1985	595
6-iron
6iTM01	160	15	0.5	150	−1	0	−1	110	15.3	6092	86
6iTM02	165	−10	−0.5	162	−4	−0.5	3	117	15.7	6607	−580
6iHookTM01	160	−30	−3	138	−30	−0.5	−7	111	14.1	6480	−878
6iHookTM02	165	−20	−2	156	−10	−0.5	0	112	15.6	5339	−494
6iSliceTM01	155	10	1.5	150	9	0.5	2	113	16.2	7480	257
6iSliceTM02	160	2	0	144	−36	−0.5	−12	106	15.5	6722	−431
Sand Wedge
SW01	105	−5	0	102	16	0.5	14	82	35.7	3581	−828
SW02	100	−5	0	97	−11	−1.5	0	77	33.4	2767	−1380
SW03	100	0	0	91	−11	−1	−1	80	36	3160	−1172
SW04	80	5	0	89	5	0	5	76	38.4	4216	−225
SW05	100	0	0	101	−6	−0.5	1	82	36	2326	−717

For example, with a driver of BRFast02, an Actual Estimated (current invention) Carry Distance of 245 is obtained versus a reference from GA CAM Results of 251. For a second example, with a 6-iron of 6iSliceTM01, an Actual Estimated (current invention) Carry Distance of 150 is obtained versus a reference from GA CAM Results of 155.

A video apparatus for improved monitoring of various launch parameters for a golf ball is described. Using an exemplary embodiment of stroboscopic photography with at least two consecutively triggered strobes or flashes and a digital camera system running at a continuous video mode, the present invention is capable of capturing all needed ball image information for processing, analysis and display of useful data. Furthermore, another embodiment of vertically arranged dual camera system with at least two cameras is also described for providing improved measurement of ball location in three-dimensional space at the times of the flashes. However, for those skilled in this field, these exemplary embodiments can be easily adapted and modified to suit additional applications without departing from the spirit and scope of this invention. Thus, it is to be understood that the scope of the invention is not limited to the disclosed embodiments. On the contrary, it is intended to cover various modifications and similar arrangements based upon the same operating principle. The scope of the claims, therefore, should be accorded the broadest interpretations so as to encompass all such modifications and similar arrangements.

Claims

1. An electronic imaging apparatus for monitoring the early flight of a launched sports object, the imaging apparatus comprising:

(a) A triggerable flash device for emanating at least two flashed illuminations, separated by a predetermined time interval, at the sports object thus creating at least two corresponding flight scenes of the sports object;

(b) an electronic camera system, located near the launched sports object and activated under a continuous video mode, for capturing image frame data corresponding to said flight scenes; and

(c) a computing device coupled to the electronic camera system for acquiring, processing and analyzing the captured image frame data into displayable sports object launch parameters

2. The imaging apparatus of claim 1 further comprises an image frame background subtraction mechanism to freeze and recognize the sports object image in flight for the processing and analyzing of the captured image frame data.

3. The imaging apparatus of claim 2 further comprises an image enhancement mechanism to enhance the contrast and image sharpness of the sports object image from the captured image frame data for the processing and analyzing of the captured image frame data.

4. The imaging apparatus of claim 1 wherein said flash device is triggered with an acoustic, an optical or an electronic device.

5. The imaging apparatus of claim 1 wherein said sports object is a golf ball and wherein said launch parameters comprise a launch angle, a launch speed and a launch azimuth in degrees of push or Pull.

6. The imaging apparatus of claim 5 wherein the surface of said golf ball further comprises one or two markings whereby, based upon the location and orientation of the one or two markings contained in the captured image frame data, the computing device determines additional sports object launch parameters of back-spin RPM (revolutions per minute), side-spin RPM and rifle-spin RPM.

7. The imaging apparatus of claim 5 wherein the shape of each of said markings is a bar or a line.

8. The imaging apparatus of claim 1 wherein said electronic camera system further comprises at least one digital CMOS or CCD camera located with a predetermined spatial relationship with a pre-launch position of the sports object.

9. An electronic imaging apparatus for monitoring the early flight of a launched sports object, the imaging apparatus comprising:

(b) an electronic camera system located near the launched sports object but spaced from it by a predetermined distance D_cmtransverse to the sports object launch direction, for capturing image frame data corresponding to said flight scenes, the camera system further comprising at least a first and a second camera wherein the second camera being mounted essentially vertically above and separated from the first camera by a predetermined distance D_spthereby creating a corresponding difference in golf ball viewing angle Δθ between the first camera and the second camera; and

whereby, owing to the creation of said difference in golf ball viewing angle Δθ, the repeatability and accuracy of said launch parameters can be correspondingly improved.

10. The imaging apparatus of claim 9 wherein said first camera is mounted near the ground.

11. The imaging apparatus of claim 9 wherein said distance D_spis set to be greater than an equivalent diameter of the sports object.

12. The imaging apparatus of claim 9 wherein said sports object is a golf ball having a diameter of about 1.7 inches.

13. The imaging apparatus of claim 12 wherein said distance D_cmis set within a range from about 12 to about 24 inches and said distance D_spis set within a range from about 4 to about 8 inches thereby creating a difference in golf ball viewing angle Δθ between about 9 to about 34 degrees.

14. The imaging apparatus of claim 9 further comprises a triangulate calculation mechanism applied to the at least two captured image frame data from both of the first and the second camera to determine the spatial location of the sports object at an instant of flight time corresponding to each flashed illumination.

15. The imaging apparatus of claim 9 further comprises an image enhance.ement technique to enhance the contrast and image sharpness of the sports object image from the captured image frame data for the processing and analyzing of the captured image frame data.

16. The imaging apparatus of claim 9 wherein said flash device is triggered with an acoustic, an optical or an electronic device.

17. The imaging apparatus of claim 9 wherein said sports object is a golf ball and wherein said launch parameters comprise a launch angle, a launch speed and a launch azimuth in degrees of push or Pull.

18. The imaging apparatus of claim 17 wherein the surface of said golf ball further comprises one or two markings whereby, based upon the location and orientation of the one or two markings contained in the captured image frame data, the computing device determines additional sports object launch parameters of back-spin RPM (revolutions per minute), side-spin RPM and rifle-spin RPM.

19. The imaging apparatus of claim 18 wherein the shape of each of said markings is a bar or a line.

20. The imaging apparatus of claim 9 wherein each of said at least a first and a second camera is a digital CMOS or CCD camera.

21. A method of monitoring the early flight of a launched sports object, the method comprises:

(a) emanating at least two flashed illuminations, separated by a predetermined time interval, at the sports object thus creating at least two corresponding flight scenes of the sports object;

(b) electronically capturing, near the launched sports object and under a continuous video mode, image frame data corresponding to said flight scenes; and

(c) acquiring, processing and analyzing the captured image frame data into sports object launch parameters.

22. The method of claim 21 wherein the processing and analyzing the captured image frame data further comprises a step of using an image frame background subtraction technique to freeze and recognize the sports object image in flight.

23. The method of claim 22 wherein the processing and analyzing of the captured image frame data further comprises a step of using an image enhancement technique to enhance the contrast and image sharpness of the sports object image from the captured image frame data.

24. The method of claim 21 wherein said sports object is a golf ball and wherein said launch parameters comprise a launch angle, a launch speed and a launch azimuth in degrees of push or Pull.

25. The method of claim 24 further comprises providing the surface of said golf ball with one or two markings and, based upon the location and orientation of the one or two markings contained in the captured image frame data, determining additional sports object launch parameters of back-spin RPM (revolutions per minute), side-spin RPM and rifle-spin RPM.

26. The method of claim 21 wherein said electronically capturing of image frame data further comprises a step of using at least one digital CMOS or CCD camera located with a predetermined spatial relationship with a pre-launch position of the sports object.

27. A method of monitoring the early flight of a launched sports object, the method comprises:

(b) capturing image frame data corresponding to said flight scenes with an electronic camera system located near the launched sports object but spaced from it by a predetermined distance D_cmtransverse to the sports object launch direction, wherein the camera system further comprising at least a first and a second camera wherein the second camera being mounted essentially vertically above and separated from the first camera by a predetermined distance D_spthereby creating a corresponding difference in golf ball viewing angle Δθ between the first camera and the second camera; and

28. The method of claim 27 further comprises mounting said first camera near the ground.

29. The method of claim 27 further comprises setting said distance D_spto be greater than an equivalent diameter of the sports object.

30. The method of claim 27 wherein said sports object is a golf ball having a diameter of about 1.7 inches.

31. The method of claim 30 further comprises setting said distance D_cmto be within a range from about 12 to about 24 inches and said distance D_spto be within a range from about 4 to about 8 inches thereby creating a difference in golf ball viewing angle Δθ between about 9 to about 34 degrees.

32. The method of claim 27 wherein the processing and analyzing of the captured image frame data further comprises applying triangulate calculation to the at least two captured image frame data from both of the first and the second camera and determining the spatial location of the sports object at an instant of flight time corresponding to each flashed illumination.

33. The method of claim 27 wherein the processing and analyzing of the captured image frame data further comprises using an image enhancement technique and enhancing the contrast and image sharpness of the sports object image from the captured image frame data.

34. The method of claim 27 wherein said sports object is a golf ball and wherein said launch parameters further comprise a launch angle, a launch speed and a launch azimuth in degrees of push or Pull.

35. The method of claim 34 further comprises providing the surface of said golf ball with one or two markings and, based upon the location and orientation of the one or two markings contained in the captured image frame data, determining additional sports object launch parameters of back-spin RPM (revolutions per minute), side-spin RPM and rifle-spin RPM.