首页> 外国专利> METHOD AND DEVICE FOR CORRECTING SYSTEMATIC TRACK SIGNAL ERRORS OF INCREMENTAL POSITION OR ANGLE OF ROTATION SENSORS

METHOD AND DEVICE FOR CORRECTING SYSTEMATIC TRACK SIGNAL ERRORS OF INCREMENTAL POSITION OR ANGLE OF ROTATION SENSORS

机译:校正旋转传感器增量位置或角度的系统轨迹信号误差的方法和装置

摘要

The invention relates to a method for correcting systematic track signal errors of incremental position or angle of rotation sensors which generate at least two, approximately sinusoidal track signals which have the same period and which are off-set by a phase angle. Said method comprises the following steps: a) detecting the track signal values (xk, yk) in the current measuring cycle (k); b) correcting the detected track signal values (xk, yk) using a stored error correction value (GPP-1), thereby obtaining corrected track signal values (xk', yk'); c) transforming the corrected track signal values (xk', yk') to give polar coordinate values (rk; ϕk); d) producing an error radius (rek); e) weighting said error radius (rek) with an evaluation variable (wk), thereby obtaining a weighted error variable (uk); f) producing an angular difference (Δϕk) from the angle (ϕk) obtained by transformation and an angle (ϕk-1) obtained and stored in the preceding measuring cycle (k-1); g) multiplying the weighted error variable (uk) by the angular difference (Δϕk), thereby obtaining an area value (Fk); h) adding up the determined area value (Fk) and a cumulative area value (FSk-1) stored in a proceeding measuring cycle (k-1), thereby producing a new cumulative area value (FS k); i) storing the new cumulative area value (FS k) and the angle (ϕk); k) repeating steps a) to i) until a correction interval (P) comprising one ore more periods of the track signals has passed; l) storing the cumulative area value (FS k) at the end of the correction interval (P) as the new error correction value (Gp).
机译:本发明涉及一种用于校正旋转的增量位置或角度传感器的系统跟踪信号误差的方法,该误差产生至少两个近似正弦的跟踪信号,这些信号具有相同的周期并且被相位角偏移。所述方法包括以下步骤:a)在当前测量周期(k)中检测跟踪信号值(xk,yk); b)使用存储的纠错值(GPP-1)来校正检测到的轨道信号值(xk,yk),从而获得校正后的轨道信号值(xk',yk'); c)变换校正后的轨迹信号值(xk',yk')以给出极坐标值(rk; ϕk); d)产生误差半径(rek); e)用评估变量(wk)对所述误差半径(rek)加权,从而获得加权误差变量(uk); f)从通过变换获得的角度(ϕk)和在先前的测量周期(k-1)中获得并存储的角度(ϕk-1)产生角度差(Δϕk); g)将加权误差变量(uk)乘以角度差(Δϕk),从而获得面积值(Fk); h)将确定的面积值(Fk)和存储在进行中的测量周期(k-1)中的累积面积值(FSk-1)相加,从而产生新的累积面积值(FS k); i)存储新的累积面积值(FS k)和角度(ϕk); k)重复步骤a)至i),直到经过一个或多个轨道信号周期的校正间隔(P)为止; l)将校正间隔(P)末尾的累积面积值(FS k)存储为新的误差校正值(Gp)。

著录项

  • 公开/公告号EP1776564B1

    专利类型

  • 公开/公告日2010-11-17

    原文格式PDF

  • 申请/专利权人 AEROLAS GMBH AEROSTATISCHE LAGER-LASERTECHNIK;

    申请/专利号EP20050764312

  • 发明设计人 BRUECKL STEFAN;

    申请日2005-08-09

  • 分类号G01D5/244;

  • 国家 EP

  • 入库时间 2022-08-21 18:00:02

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