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公开(公告)号：US20060281572A1
公开(公告)日：2006-12-14
申请号：US11495607
申请日：2006-07-31
申请人： William Gobush , Diane Pelletier , Douglas Winfield , Charles Days , Steven Aoyama , Edmund Hebert , James Silveira
发明人： William Gobush , Diane Pelletier , Douglas Winfield , Charles Days , Steven Aoyama , Edmund Hebert , James Silveira
IPC分类号： A63B69/36
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
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公开(公告)号：US06500073B1
公开(公告)日：2002-12-31
申请号：US09468351
申请日：1999-12-21
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63B6936
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
摘要翻译： 一种发射监视器系统，包括支撑结构，设置在该支撑结构上的第一光反射元件，照明单元和照相机单元。 计算机接收由相机单元接收的光图案产生的信号，并计算对象的各种飞行特性。 系统可以来回移动以改变摄像机单元的视场。 该系统还根据计算的飞行特性计算和显示物体轨迹，这些飞行特性考虑了物体的特征和大气条件。
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公开(公告)号：US07086955B2
公开(公告)日：2006-08-08
申请号：US10889132
申请日：2004-07-13
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
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公开(公告)号：US06764412B2
公开(公告)日：2004-07-20
申请号：US10270665
申请日：2002-10-16
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63B6936
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
摘要翻译： 一种发射监视器系统，包括支撑结构，设置在该支撑结构上的第一光反射元件，照明单元和照相机单元。 计算机接收由相机单元接收的光图案产生的信号，并计算对象的各种飞行特性。 系统可以来回移动以改变摄像机单元的视场。 该系统还根据计算的飞行特性计算和显示物体轨迹，这些飞行特性考虑了物体的特征和大气条件。
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公开(公告)号：US06616543B1
公开(公告)日：2003-09-09
申请号：US09566804
申请日：2000-05-08
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63F924
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
摘要翻译： 一种发射监视器系统，包括支撑结构，设置在该支撑结构上的第一光反射元件，照明单元和照相机单元。 计算机接收由相机单元接收的光图案产生的信号，并计算对象的各种飞行特性。 系统可以来回移动以改变摄像机单元的视场。 该系统还根据计算的飞行特性计算和显示物体轨迹，这些飞行特性考虑了物体的特征和大气条件。
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公开(公告)号：US06241622B1
公开(公告)日：2001-06-05
申请号：US09156611
申请日：1998-09-18
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63B6936
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and a camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
摘要翻译： 一种发射监视器系统，包括支撑结构，设置在该支撑结构上的第一光反射元件，照明单元和照相机单元。 计算机接收由相机单元接收的光图案产生的信号，并计算对象的各种飞行特性。 系统可以来回移动以改变摄像机单元的视场。 该系统还根据计算的飞行特性计算和显示物体轨迹，这些飞行特性考虑了物体的特征和大气条件。
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公开(公告)号：US06488591B1
公开(公告)日：2002-12-03
申请号：US09566803
申请日：2000-05-08
申请人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63B6936
CPC分类号： A63B24/0003 , A63B24/0021 , A63B43/008 , A63B43/06 , A63B69/3614 , A63B69/3658 , A63B71/06 , A63B2024/0028 , A63B2024/0031 , A63B2024/0034 , A63B2102/32 , A63B2207/02 , A63B2220/05 , A63B2220/16 , A63B2220/20 , A63B2220/30 , A63B2220/35 , A63B2220/70 , A63B2220/805 , A63B2220/806 , A63B2220/807 , A63B2220/808 , A63B2220/89 , A63B2225/02 , G01S11/12 , G01S17/107 , G01S17/50 , G01S17/66 , G01S17/89
摘要： A launch monitor system including a support structure, a first light-reflecting element disposed on this support structure, a lighting unit and an camera unit. A computer receives signals generated by light patterns received by the camera unit and computes a variety of flight characteristics for the object. The system may be moved back and forth to vary the field-of-view of the camera unit. The system also computes and displays object trajectories from the computed flight characteristics which account for the characteristics of the object and the atmospheric conditions.
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8.发明授权公开(公告)号：US07369158B2
公开(公告)日：2008-05-06
申请号：US10892327
申请日：2004-07-16
申请人： William Gobush , Diane I. Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane I. Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
CPC分类号： A63B69/3614 , A63B43/008
摘要： 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.
摘要翻译： 本发明涉及一种测量在预定视野内移动的物体的飞行特性的发射监测系统。 该系统包括支撑结构，照明单元，设置在支撑结构上的照相机单元和校准组件。 校准组件包括校准夹具和至少一个伸缩构件。 伸缩构件的第一端联接到支撑结构，并且第二端可与固定装置接触或联接到固定装置。 在伸缩构件的延伸位置中，校准夹具处于相机单元的视场中。 在缩回位置，校准夹具处于视场外。 校准夹具还包括对比标记。 在另一个实施例中，系统包括框架，并且发射监测器从框架枢转地悬挂使得其自动调平。 本发明还包括校准具有校准夹具的发射监测器的方法。
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公开(公告)号：US06781621B1
公开(公告)日：2004-08-24
申请号：US09537295
申请日：2000-03-29
申请人： William Gobush , Diane I. Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
发明人： William Gobush , Diane I. Pelletier , Douglas C. Winfield , Charles Days , Steven Aoyama , Edmund A. Hebert , James Alan Silveira
IPC分类号： A63B6936
CPC分类号： A63B69/3614 , A63B43/008
摘要： 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.
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公开(公告)号：US20060019772A1
公开(公告)日：2006-01-26
申请号：US11214428
申请日：2005-08-29
申请人： Michael Sullivan , Steven Aoyama , Edmund Hebert , Derek Ladd , William Morgan , Michael Jordan
发明人： Michael Sullivan , Steven Aoyama , Edmund Hebert , Derek Ladd , William Morgan , Michael Jordan
CPC分类号： A63B37/0004 , A63B37/0003 , A63B37/0006 , A63B37/0012 , A63B37/0021 , A63B37/0061 , A63B37/0078 , A63B37/008 , A63B37/0083 , A63B37/0089 , A63B37/009 , A63B37/0094 , A63B37/0096 , A63B2043/001
摘要： A high performance golf ball having a reduced overall distance while maintaining the appearance of a high performance trajectory. The golf ball includes a combination of low CoR core and cover materials coupled with a less aerodynamic dimple pattern that achieves a reduction in carry and overall distance of 15 and 25 yards versus a conventional golf ball, while still providing the look, sound, feel and apparent flight of a conventional golf ball. A high performance golf ball having a reduced distance is also achieved by controlling dimensionless coefficients of lift/weight and drag/weight at certain Reynolds numbers and spin ratios for various CoR.
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