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    Launch monitor system with a calibration fixture and a method for use thereof
    1.
    发明授权
    Launch monitor system with a calibration fixture and a method for use thereof 失效
    使用校准夹具启动监控系统及其使用方法

    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

    IPC分类号： H04N7/18 ,  A63B67/02

    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。