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Realization of Spindle Prompt Normal Posture Alignment for assembly holemakingon Large Suspended Panel

机译:主轴呈现出集合Holemakenon大型悬挂面板的正常姿态对齐

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To satisfy the requirement of assembly hole-making in large suspended panel, a 5-DOF spindle normal posture alignment mechanism (abbreviate as SNPAM) is designed, and a method for promptly adjusting spindle normal direction is proposed. In this method, spindle centering adjustment in a large scope is quickly realized by using image sensor. With laser displacement sensors, coordinates of three laser projective points around the hole-marker are achieved. By rebuilding kinetic transfer equation of the SNPAM, inversely solving control increments of active pairs are gained, and spindle normal posture alignment is accomplished in a small scope. Research on connecting holes of one aircraft wing-to-body shows the method has such virtues as simple operate, convenient control, good real-time, which is especially fit for automatic hole-making in large suspended panel.
机译:为了满足大型悬挂面板中的装配孔的要求,设计了5-DOF主轴正常姿势对准机构(缩写为SNPAM),提出了一种用于迅速调节主轴法线方向的方法。在该方法中,通过使用图像传感器快速实现大范围的主轴定心调整。利用激光位移传感器,实现了孔标记周围的三个激光投射点的坐标。通过重建SNPAM的动力学传输方程,获得了有源对的反向控制增量,并且在小范围内完成主轴正常姿势对准。一架飞机机翼到体的连接孔的研究该方法具有简单的操作,方便的控制,实时良好,特别适用于大型悬挂面板中的自动孔。

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