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利用几何方法对EAST ECRH系统天线的转动镜面空间连杆驱动机构进行分析,详细推导出两个方向直线驱动滑块运动位移与反射波束角度之间的函数关系,为波束进入等离子体内部方位的精确控制提供可靠的数学模型。
The geometrical method is used to analyze the rotating mirror spatial link driving mechanism of the EAST ECRH system antenna. The function relationship between the movement displacement and the reflected beam angle of the linear driving slider in two directions is deduced in detail. The accuracy of the beam orientation into the interior of the plasma Control provides a solid mathematical model.