TWI417512B - Linear measurement method and linear measuring device - Google Patents
Linear measurement method and linear measuring device Download PDFInfo
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- TWI417512B TWI417512B TW098136156A TW98136156A TWI417512B TW I417512 B TWI417512 B TW I417512B TW 098136156 A TW098136156 A TW 098136156A TW 98136156 A TW98136156 A TW 98136156A TW I417512 B TWI417512 B TW I417512B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/28—Measuring arrangements characterised by the use of mechanical techniques for measuring roughness or irregularity of surfaces
- G01B5/285—Measuring arrangements characterised by the use of mechanical techniques for measuring roughness or irregularity of surfaces for controlling eveness
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/20—Measuring arrangements characterised by the use of mechanical techniques for measuring contours or curvatures
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D11/00—Component parts of measuring arrangements not specially adapted for a specific variable
- G01D11/30—Supports specially adapted for an instrument; Supports specially adapted for a set of instruments
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N19/00—Investigating materials by mechanical methods
- G01N19/08—Detecting presence of flaws or irregularities
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Description
本申請主張基於2008年10月29日申請之日本專利申請第2008-277597號之優先權。該申請之全部內容藉由參照援用於該說明書中。 The present application claims priority based on Japanese Patent Application No. 2008-277597, filed on Oct. 29, 2008. The entire contents of this application are incorporated herein by reference.
本發明涉及利用3點法測量直線性之方法及測量直線性之裝置。 The present invention relates to a method of measuring linearity using a 3-point method and a device for measuring linearity.
可由三點法進行測量對象物之表面直線性(專利文獻1)的測量。例如,利用3個位移計之基準點移動之軌跡即仿效曲線之輪廓、測量對象物之表面輪廓、及3個位移計之俯仰成分之輪廓來記述3個位移計之測量數據,藉由將該記述式作為聯立方程式解出,可決定表面輪廓。 The measurement of the surface linearity of the object to be measured (Patent Document 1) can be performed by the three-point method. For example, the measurement data of the three displacement meters is described by using the trajectory of the reference point movement of the three displacement meters, that is, the contour of the simulation curve, the surface contour of the measurement object, and the contour of the pitch components of the three displacement meters. The description is solved as a simultaneous equation, which determines the surface contour.
專利文獻1:日本專利公開2003-254747號公報 Patent Document 1: Japanese Patent Publication No. 2003-254747
為了基於藉由三點法測量之數據來分離位移計啟動之軌跡即仿效曲線之輪廓、3個位移計移動時產生之俯仰成分之輪廓、及測量對象物之表面輪廓,必須高精度調整3個位移計之零點。例如,為了測量平坦度為幾μm之表面之直線性,必須將3個位移計之零點從目標位置之偏移量設為幾十奈米~幾奈米以下。 In order to separate the trajectory of the displacement meter based on the data measured by the three-point method, that is, the contour of the simulation curve, the contour of the pitch component generated when the three displacement gauges move, and the surface contour of the measurement object, it is necessary to adjust three precisions with high precision. Zero point of the displacement meter. For example, in order to measure the linearity of the surface having a flatness of several μm , it is necessary to set the offset of the zero point of the three displacement gauges from the target position to several tens of nanometers to several nanometers or less.
而且,雷射位移計等非接觸之位移計之零點根據測量對象物之表面性狀,例如由砂輪引起之研磨痕之狀態、粗糙度、材質、反射率、透射率等變動。而且,零點之變動 量具有個體差。因此,難以事先高精度地進行位移計之零點調整。 Further, the zero point of the non-contact displacement meter such as a laser displacement meter varies depending on the surface properties of the object to be measured, for example, the state of the polishing mark caused by the grinding wheel, the roughness, the material, the reflectance, the transmittance, and the like. Moreover, the change of zero The amount has individual differences. Therefore, it is difficult to perform the zero point adjustment of the displacement meter with high precision in advance.
本發明之目的在於,提供一種不必高精度進行3個位移計之零點調整而可以計算測量對象物之表面輪廓之直線性測量方法。 An object of the present invention is to provide a linear measuring method capable of calculating a surface contour of a measuring object without performing zero adjustment of three displacement meters with high precision.
本發明之其他目的在於,提供一種運用上述方法測量直線性之直線性測量裝置。 Another object of the present invention is to provide a linearity measuring apparatus for measuring linearity by the above method.
根據本發明之一觀點,提供一種直線性測量方法,該方法,具有:使排列在第1方向、相對位置被固定之3個位移計與測量對象物相對,並使得位移計或對象物的其中一方移動進行測量之物為活動物,另一方為固定物,將該位移計及該測量對象物之一方之活動物,相對於另一方之固定物一邊朝第1方向移動,一邊測量從3個位移計到分別在測量對象物之表面沿著朝第1方向延伸之測量對象線排列之3個被測量點之距離之步驟;根據上述3個位移計之測量結果計算對上述活動物之相對位置被固定之基準點之軌跡即仿效曲線之輪廓之步驟;將上述仿效曲線計算出之輪廓之2次成分,基於事先測量出之仿效曲線之輪廓之2次成分進行校正之步驟;基於被校正之仿效曲線之輪廓,計算上述測量對象物之表面輪廓之步驟。 According to one aspect of the present invention, there is provided a method for measuring a linearity, comprising: displacing three displacement meters arranged in a first direction and a relative position with an object to be measured, and causing a displacement gauge or an object thereof The object that is moved by one of the objects is a moving object, and the other is a fixed object, and the movable object that is one of the objects to be measured is moved in the first direction with respect to the other fixed object, and the measurement is performed from three a step of measuring the distance to the three measured points arranged on the surface of the measuring object along the measuring object line extending in the first direction; calculating the relative position to the living object based on the measurement results of the three displacement meters The trajectory of the fixed reference point is a step of emulating the contour of the curve; the second component of the contour calculated by the above imitating curve is corrected based on the second component of the contour of the imitating curve measured in advance; based on the corrected The step of emulating the contour of the curve and calculating the surface profile of the object to be measured.
根據本發明之另一觀點,提供一種直線性測量裝置,其具有:支撐測量對象物之工作臺;感測器頭,包括測量到分別在該測量對象物之表面排列於該第1方向之被測量點之距離之3個位移計;導向機構,相對於另一方之固定物沿著上述第1方向可移動地支撐上述感測器頭及上述工作臺之一方之活動物;及控制裝置,存儲有相對固定在上述活動物之基準點之軌跡即仿效曲線之2次成分,基於由上述3個位移計測量之測量數據,求出沿著平行於上述第1方向之測量對象線之上述表面之輪廓,上述控制裝置,執行:一邊朝上述第1方向移動上述活動物,一邊藉由3個位移計之每一個,測量到沿上述測量對象線之表面上之被測量點之距離而取得測量數據之步驟;基於上述3個位移計之測量結果,計算對上述活動物之相對位置被固定之基準點之軌跡即仿效曲線之輪廓之步驟;將上述仿效曲線之計算出之輪廓之2次成分,基於被存儲之仿效曲線之輪廓之2次成分進行校正之步驟;及基於被校正之仿效曲線之輪廓,計算上述測量對象物之表面輪廓之步驟。According to another aspect of the present invention, a linearity measuring apparatus includes: a table for supporting an object to be measured; and a sensor head including a body that is measured to be aligned in the first direction on a surface of the object to be measured a three displacement meter for measuring the distance of the point; the guiding mechanism movably supporting the movable body of the sensor head and one of the working tables along the first direction with respect to the other fixed object; and the control device stores a second component which is a trajectory fixed to a reference point of the living object, that is, a simulation curve, and the surface along the measurement target line parallel to the first direction is obtained based on measurement data measured by the three displacement meters In the contour, the control device performs the measurement of the distance along the measured point on the surface of the measurement target line by measuring the moving object in the first direction and measuring the distance along the surface of the measurement target line by each of the three displacement meters. The step of calculating the trajectory of the reference point to which the relative position of the living object is fixed, that is, the contour of the emulation curve, based on the measurement results of the three displacement meters a step of correcting the second component of the contour of the calculated contour curve based on the second component of the contour of the stored imitative curve; and calculating a surface profile of the object to be measured based on the contour of the corrected imitative curve The steps.
藉由不受仿效曲線之輪廓變動之影響之方法事先測量仿效曲線之輪廓之2次成分,即使在未進行位移計之零點調整之情況下,也可確定仿效曲線之2次成分。由此,不必進行精密之零點調整而能夠進行測量對象物之表面輪廓的測量。By measuring the secondary component of the contour of the emulation curve in advance without being affected by the contour variation of the emulation curve, the second component of the emulation curve can be determined even if the zero adjustment of the displacement gauge is not performed. Thereby, it is possible to perform measurement of the surface contour of the measurement object without performing precise zero adjustment.
於圖1A表示根據實施例之直線性測量裝置之槪要透視透視圖。活動工作臺10藉由工作臺導向機構11被支撐為可朝一方向移動。定義將活動工作臺10之移動方向設為x軸、將垂直下方設為z軸之xyz直角坐標系。Fig. 1A shows a perspective perspective view of a linear measuring device according to an embodiment. The movable table 10 is supported by the table guiding mechanism 11 so as to be movable in one direction. An xyz rectangular coordinate system in which the moving direction of the movable table 10 is set to the x-axis and the vertical lower side is set to the z-axis is defined.
導軌18在活動工作臺10之上方支撐研磨頭15。研磨頭15可沿著導軌18在y軸方向移動。而且,研磨頭15也可相對於導軌18在z方向移動。即,研磨頭15可相對於活動工作臺10升降。在研磨頭15之下端安裝有砂輪16。砂輪16具有圓柱狀之外形,以其中心軸平行於y軸之姿勢安裝在研磨頭15。The guide rail 18 supports the polishing head 15 above the movable table 10. The polishing head 15 is movable along the guide rail 18 in the y-axis direction. Moreover, the polishing head 15 can also move in the z direction with respect to the guide rail 18. That is, the polishing head 15 can be raised and lowered with respect to the movable table 10. A grinding wheel 16 is attached to the lower end of the polishing head 15. The grinding wheel 16 has a cylindrical outer shape and is attached to the polishing head 15 with its central axis parallel to the y-axis.
於活動工作臺10上保持測量對象物(被研磨物)20。在使砂輪16接觸於測量對象物20之表面之狀態下,一邊旋轉砂輪16,一邊藉由朝x方向移動活動工作臺10,從而可研磨測量對象物20之表面。The object to be measured (object to be polished) 20 is held on the movable table 10. In a state where the grinding wheel 16 is brought into contact with the surface of the object 20 to be measured, the surface of the object 20 to be measured can be polished by moving the movable table 10 in the x direction while rotating the grinding wheel 16.
控制裝置19控制活動工作臺10及研磨頭15之移動。The control device 19 controls the movement of the movable table 10 and the polishing head 15.
如圖1B所示,在研磨頭15之下端安裝有感測器頭30。在感測器頭30,安裝有3個位移計31i、31j、31k。在位移計31i、31j、31k例如利用雷射位移計。位移計31i、31j、31k可分別測量從位移計到測量對象物20之表面上之被測量點之距離。3個位移計31i、31j、31k排列在y方向。而且,3個位移計31i、31j、31k之被測量點也排列在y方向。因此,可測量沿著平行於y方向之測量對象線之表面之高度。藉由一邊朝y方向移動研磨頭15一邊進行測量,可測量沿著測量對象物20表面之測量對象線之表面輪廓。測量數據從位移計31i、31j、31k輸入到控制裝置19。As shown in FIG. 1B, a sensor head 30 is mounted at the lower end of the polishing head 15. In the sensor head 30, three displacement meters 31i, 31j, and 31k are mounted. The displacement meters 31i, 31j, 31k use, for example, a laser displacement meter. The displacement meters 31i, 31j, 31k can measure the distances from the displacement gauge to the measured points on the surface of the object 20 to be measured, respectively. The three displacement meters 31i, 31j, and 31k are arranged in the y direction. Further, the measured points of the three displacement meters 31i, 31j, and 31k are also arranged in the y direction. Therefore, the height of the surface of the measuring object line parallel to the y direction can be measured. By measuring while moving the polishing head 15 in the y direction, the surface profile of the measurement target line along the surface of the object 20 can be measured. The measurement data is input from the displacement meters 31i, 31j, 31k to the control device 19.
參照圖2對坐標系及各種函數進行說明。在圖2中,將上方設為z軸之正方向。因此,感測器頭30和測量對象物20之上下關係與圖1B所示之上下關係相反。位移計31i、31j、31k朝向y軸之負方向按該順序以等間隔P配置。將連接兩端之位移計31i、31k之零點之線段之中點定義為基準點。將從基準點到中央之位移計31j之零點之高度(零點誤差)設為δ。The coordinate system and various functions will be described with reference to Fig. 2 . In Fig. 2, the upper direction is set to the positive direction of the z-axis. Therefore, the upper and lower relationship of the sensor head 30 and the measuring object 20 is opposite to the above-described relationship shown in FIG. 1B. The displacement meters 31i, 31j, and 31k are arranged at equal intervals P in this order in the negative direction of the y-axis. The midpoint of the line segment connecting the zero points of the displacement meters 31i and 31k at both ends is defined as a reference point. The height (zero point error) of the zero point of the displacement meter 31j from the reference point to the center is set to δ.
將測量對象物20之表面、沿著測量對象線之輪廓設為W(y)。將朝y方向移動感測器頭30時基準點之軌跡(仿效曲線)設為h(y)。理想地,仿效曲線h(y)係直線,但是實際上從理想的直線歪曲。The surface of the object 20 to be measured and the contour along the line to be measured are set to W(y). The trajectory (imitation curve) of the reference point when moving the sensor head 30 in the y direction is set to h(y). Ideally, the emulation curve h(y) is a straight line, but actually distort from the ideal straight line.
將連接兩端之位移計31i、31k之零點之直線從y軸傾斜之角度設為θ(y)。理想地,傾斜角θ(y)=0,但是實際上隨著感測器頭30之移動而產生俯仰,由此傾斜角θ(y)與仿效曲線h(y)之傾斜度為獨立變動。位移計31i之零點和基準點之高度之差、及位移計31k之零點和基準點之高度之差可表示為T(y)×P。此處,與俯仰成分T(y)=sin(θ(y))近似。若將位移計31i、31j、31k之測量值分別設為i(y)、j(y)、k(y),則下述式成立。The angle at which the straight line connecting the zero points of the displacement meters 31i and 31k at both ends is inclined from the y-axis is θ(y). Ideally, the tilt angle θ(y) = 0, but actually the pitch is generated as the sensor head 30 moves, whereby the tilt angle θ(y) and the slope of the emulation curve h(y) are independently varied. The difference between the height of the displacement point 31i and the height of the reference point, and the difference between the height of the displacement gauge 31k and the height of the reference point can be expressed as T(y) × P. Here, it is approximated by the pitch component T(y)=sin(θ(y)). When the measured values of the displacement meters 31i, 31j, and 31k are respectively set to i(y), j(y), and k(y), the following expression holds.
W(y+P)=h(y)+i(y)+T(y)×P ...(1)W(y+P)=h(y)+i(y)+T(y)×P (1)
W(y)=h(y)+j(y)+δ...(2)W(y)=h(y)+j(y)+δ...(2)
W(y-P)=h(y)+k(y)-T(y)×P ...(3)W(y-P)=h(y)+k(y)-T(y)×P (3)
由於傾斜角θ(y)非常小,因此,使cos(θ(y))近似於1。Since the inclination angle θ(y) is very small, cos(θ(y)) is approximated to 1.
測量對象物20之形狀,例如係一邊之長度為2m之正方形,位移計之間隔P例如係100mm。The shape of the object 20 to be measured is, for example, a square having a length of 2 m on one side, and the interval P of the displacement meter is, for example, 100 mm.
若從式(1)、(2)、(3)消去T(y)和h(y),則可得到以下式。When T(y) and h(y) are eliminated from the formulas (1), (2), and (3), the following formula can be obtained.
W(y+P)-2W(y)+W(y-P)+2δ=i(y)-2j(y)+k(y)...(4)W(y+P)-2W(y)+W(y-P)+2δ=i(y)-2j(y)+k(y)...(4)
此處,假設用以下3次式(5)表示表面輪廓W(y)。Here, it is assumed that the surface profile W(y) is expressed by the following three equations (5).
W(y)=ay3 +by2 +cy+d ...(5)W(y)=ay 3 +by 2 +cy+d ...(5)
若將式(5)代入到式(4),則得到以下式(6)。When the formula (5) is substituted into the formula (4), the following formula (6) is obtained.
6aP2 y+2bP2 +2δ=i(y)-2j(y)+k(y)...(6)6aP 2 y+2bP 2 +2δ=i(y)-2j(y)+k(y)...(6)
式(6)之右邊全部係測量數據,位移計之間隔P為已知。從而,左邊之未知數a可從右邊之變量y之1次成分計算。但是,即使求出右邊之y之0次成分,左邊之零點誤差δ由於係未知,所以不能夠決定未知數b。即,可決定表面輪廓W(y)之3次成分a,但不可決定2次成分b。另外,也可與3次成分同樣地決定表面輪廓W(y)之4次以上之成分。The right side of equation (6) is the measurement data, and the interval P of the displacement meter is known. Thus, the unknown a on the left can be calculated from the first component of the variable y on the right. However, even if the zeroth component of y on the right side is obtained, the zero point error δ on the left side is unknown, so the unknown number b cannot be determined. That is, the third component a of the surface profile W(y) can be determined, but the secondary component b cannot be determined. Further, the component of the surface profile W(y) of four or more times may be determined in the same manner as the third component.
於實施例中,為了彌補不可決定表面輪廓W(y)之2次成分,事先測量好仿效曲線h(y)之2次成分。仿效曲線h(y)之2次成分相當於導軌18之撓度,所以可認定在每次測量時沒有大的變動。從而,事先測量好仿效曲線h(y)之2次成分,則在每次進行測量對象物之表面輪廓的測量時,不需要重新測量仿效曲線h(y)之2次成分。另外,可認定仿效曲線h(y)之3次以上之成分在每次測量表面輪廓時(在感測器頭30每次移動時)不可預測地變動。因此,即使事先測量好仿效曲線h(y)之3次以上之成分,也不可基於事先測量出之3次以上之成分來校正實際之測量對象物之測量結果。In the embodiment, in order to compensate for the secondary component of the undeterminable surface profile W(y), the secondary component of the simulation curve h(y) is measured in advance. The second component of the emulation curve h(y) corresponds to the deflection of the guide rail 18, so that it is considered that there is no large variation in each measurement. Therefore, when the secondary component of the simulation curve h(y) is measured in advance, it is not necessary to re-measure the secondary component of the simulation curve h(y) every time the measurement of the surface profile of the measurement object is performed. Further, it can be considered that the components of the simulation curve h(y) three or more times are unpredictably changed each time the surface profile is measured (when the sensor head 30 moves each time). Therefore, even if the component of the simulation curve h(y) is measured three times or more in advance, the measurement result of the actual measurement object cannot be corrected based on the component measured three times or more in advance.
於圖3A作為一例表示事先測量仿效曲線h(y)之2次成分之方法之流程圖。如圖3B所示,在步驟S1中將測量對象物20放置於活動工作臺10之上。沿著測量對象物20之表面上之平行於y方向之任意直線移動傾斜儀35而測量沿著該直線表面之傾斜之分布。根據該傾斜之分布計算表面輪廓W(y)。由傾斜儀進行之測量不受導軌18之歪斜之影響。FIG. 3A is a flowchart showing a method of measuring the secondary component of the emulation curve h(y) in advance as an example. As shown in FIG. 3B, the measurement object 20 is placed on the movable table 10 in step S1. The inclination of the slope along the straight surface is measured by moving the inclinometer 35 along an arbitrary straight line parallel to the y direction on the surface of the measuring object 20. The surface profile W(y) is calculated from the distribution of the inclination. The measurement by the inclinometer is not affected by the skew of the guide rail 18.
於步驟S2中,藉由利用位移計31j測量沿著與由傾斜儀35測量傾斜分布之直線相同之直線之表面輪廓,從而取得測量數據j(y)。In step S2, the measurement data j(y) is obtained by measuring the surface profile of the same line as the straight line measuring the oblique distribution by the inclinometer 35 by using the displacement meter 31j.
於步驟S3中,計算仿效曲線h(y)之2次成分。以下,對該計算方法進行說明。由位移計31j計測之表面輪廓與根據由傾斜儀進行之計測求出之表面輪廓W(y)相同。因此,在根據由傾斜儀進行之計測求出之表面輪廓W(y)和由位移計31j測量之測量數據j(y)之間,式(2)之關係成立。由於零點誤差δ係常數,所以可根據表面輪廓W(y)之2次成分和測量數據j(y)之2次成分計算仿效曲線h(y)之2次成分。計算出之2次成分存儲在控制裝置19。In step S3, the secondary component of the emulation curve h(y) is calculated. Hereinafter, the calculation method will be described. The surface profile measured by the displacement meter 31j is the same as the surface profile W(y) obtained from the measurement by the inclinometer. Therefore, the relationship of the equation (2) holds between the surface contour W(y) obtained by the measurement by the tilt meter and the measurement data j(y) measured by the displacement meter 31j. Since the zero point error δ is a constant, the secondary component of the simulation curve h(y) can be calculated from the secondary component of the surface profile W(y) and the secondary component of the measurement data j(y). The calculated secondary component is stored in the control device 19.
仿效曲線h(y)之輪廓一般在每次朝y方向移動研磨頭15時變化,不限於每次成為相同之輪廓。但是,可認定仿效曲線h(y)之2次成分係決定仿效曲線之大致形狀之低次成分且重現性高。即,可認定在每次測量時無大之變動。 The contour of the emulation curve h(y) generally changes each time the polishing head 15 is moved in the y direction, and is not limited to being the same contour each time. However, it can be considered that the secondary component of the emulation curve h(y) determines the low-order component of the approximate shape of the emulation curve and has high reproducibility. That is, it can be considered that there is no major change in each measurement.
於圖4表示根據實施例之直線性測量方法之流程圖。首先,將測量對象物20裝載於活動工作臺10。該測量對象物20不需要與在圖3A所示之步驟利用傾斜儀測量表面輪廓之測量對象物20相同。 A flow chart of the linearity measuring method according to the embodiment is shown in FIG. First, the object 20 to be measured is loaded on the movable table 10. The object 20 to be measured does not need to be the same as the object 20 to be measured by measuring the surface profile with the inclinometer in the step shown in FIG. 3A.
於步驟SA1中,一邊朝y方向移動研磨頭15及感測器頭30,一邊由位移計31i、31j、31k測量到測量對象物20表面之被測量點之距離i(y)、j(y)、k(y)。被測量之數據輸入到控制裝置19。 In step SA1, while moving the polishing head 15 and the sensor head 30 in the y direction, the distances i(y), j(y) of the measured points on the surface of the object 20 are measured by the displacement meters 31i, 31j, and 31k. ), k(y). The measured data is input to the control device 19.
於步驟SA2中,在測量數據i(y)、j(y)、k(y)運用低通濾波器而除去雜訊成分。為了有效地使低通濾波器作用,測量數據i(y)、j(y)、k(y)以相對於位移計之間隔P非常窄之刻度取得。例如,以0.05mm之刻度寬取得測量數據i(y)、j(y)、k(y)。 In step SA2, a low-pass filter is applied to the measurement data i(y), j(y), and k(y) to remove the noise component. In order to effectively act on the low-pass filter, the measurement data i(y), j(y), k(y) are taken at a very narrow scale with respect to the interval P of the displacement meter. For example, measurement data i(y), j(y), k(y) are obtained with a scale width of 0.05 mm.
於步驟SA3中,對運用低通濾波器之後的測量數據i(y)、j(y)、k(y)進行採樣而生成步驟數據。採樣之周期例如為位移計之間隔P之一半,即50mm。 In step SA3, the measurement data i(y), j(y), k(y) after the low-pass filter is applied is sampled to generate step data. The sampling period is, for example, one half of the interval P of the displacement meter, that is, 50 mm.
於步驟SA4中,基於步驟數據i(y)、j(y)、k(y),利用遺傳算法導出仿效曲線h(y)和俯仰成分T(y)。 In step SA4, the emulation curve h(y) and the pitch component T(y) are derived using a genetic algorithm based on the step data i(y), j(y), k(y).
於圖5表示運用遺傳算法之步驟SA4之詳細流程圖。在該遺傳算法中,將仿效曲線h(y)和俯仰成分T(y)之羣組設為1個個體。 A detailed flow chart of step SA4 using the genetic algorithm is shown in FIG. In the genetic algorithm, a group of the emulation curve h(y) and the pitch component T(y) is set to one individual.
於步驟SB1中生成初代個體群。例如,個體數為200。其中一例是將1個個體之仿效曲線h(y)和俯仰成分T(y)設為0。其他之199個個體之仿效曲線h(y)和俯仰成分T(y)根據隨機數決定。另外,在初始狀態中也可將所有個體之仿效曲線h(y)及俯仰成分T(y)設定為0。 A first generation individual group is generated in step SB1. For example, the number of individuals is 200. An example of this is to set the emulation curve h(y) and the pitch component T(y) of one individual to zero. The other 199 individuals' imitate curves h(y) and pitch components T(y) are determined according to random numbers. In addition, in the initial state, the emulation curve h(y) and the pitch component T(y) of all individuals can also be set to zero.
於步驟SB2中,由評估函數評估各個體,計算各個體之適合度。根據表面輪廓W(y)設定評估函數。3個位移計31i、31j、31k測量沿著同一測量對象物20表面之同一測量對象線之輪廓,所以利用式(1)~式(3)分別計算之3個表面輪廓W1(y)、W2(y)、W3(y)應該一致。 In step SB2, each body is evaluated by an evaluation function, and the fitness of each body is calculated. The evaluation function is set according to the surface profile W(y). The three displacement meters 31i, 31j, and 31k measure the contours of the same measurement target line along the surface of the same measurement object 20, so the three surface contours W 1 (y) calculated by the equations (1) to (3), respectively. W 2 (y) and W 3 (y) should be consistent.
因此,首先求出W1(y)和W2(y)之差量W1(y)-W2(y)、及W2(y)和W3(y)之差量W2(y)-W3(y)。用多項式表示表面輪廓W(y)時0次成分相當於測量對象物20和感測器頭30之間隔,1次成分相當於測量對象物20之姿勢。即,表面輪廓W(y)之0次成分和1次成分不直接關係到測量對象物20之表面輪廓。因此,從差量W1(y)-W2(y)及差量W2(y)-W3(y)除去0次成分和1次成分。 Thus, first obtains a difference W 1 (y) and W 2 (y) the amount W 1 (y) -W 2 ( y), and W 2 (y) and W 3 (y) of the difference between the amount of W 2 (y )-W 3 (y). When the surface contour W(y) is expressed by a polynomial, the zero-order component corresponds to the interval between the measurement target 20 and the sensor head 30, and the primary component corresponds to the posture of the measurement target 20. That is, the 0th order component and the 1st order component of the surface profile W(y) are not directly related to the surface profile of the measuring object 20. Therefore, the zero-order component and the primary component are removed from the difference W 1 (y) - W 2 (y) and the difference W 2 (y) - W 3 (y).
計算除去0次成分和1次成分之差量W1(y)-W2(y)及差量W2(y)-W3(y)之各標準偏差(standard deviation:又稱標準離差或均方根差)。將這2個標準偏差之和設為評估函數。可謂評估函數之值越小,適合度越高。根據適合度排序所有個體。 Calculate the standard deviation (standard deviation: also known as standard deviation) of the difference W 1 (y)-W 2 (y) and the difference W 2 (y)-W 3 (y) of the zero-order component and the first-order component. Or rms difference). The sum of these two standard deviations is set as an evaluation function. The smaller the value of the evaluation function, the higher the fitness. Sort all individuals according to fitness.
於步驟SB3中,選擇成為交叉對象之個體。作為一例,越是適合度高的個體,選擇個體之概率設定為越高。基於該選擇概率,選擇由2個個體構成之10對。In step SB3, the individual who becomes the intersection object is selected. As an example, the more appropriate the individual, the higher the probability of selecting an individual. Based on the selection probability, 10 pairs composed of 2 individuals are selected.
於步驟SB4中,使選擇出之個體對之仿效曲線h(y)或俯仰成分T(y)之至少一方交叉,生成新的個體。In step SB4, the selected individual crosses at least one of the emulation curve h(y) or the pitch component T(y) to generate a new individual.
參照圖6說明交叉之方法。表示在這代個體中被選擇為交叉對象之2個個體Ua及Ub之仿效曲線h(y)及俯仰成分之輪廓T(y)。更換(交叉)個體Ua之仿效曲線h(y)之一部分和個體Ub之仿效曲線h(y)對應之部分,生成新的個體Uc及Ud。新的個體Uc及Ud之俯仰成分之輪廓T(y)分別仍繼承原來個體Ua及Ub之俯仰成分之輪廓T(y)。這樣,從2個個體新生成2個個體。在步驟SB3中選擇10對個體,所以在步驟SB4中新生成10對,即20個個體。The method of intersection will be described with reference to FIG. The emulation curve h(y) and the contour T(y) of the pitch component of the two individuals Ua and Ub selected as the intersecting objects in this generation are shown. A part of the emulation curve h(y) of the individual Ua is replaced (crossed) with the part corresponding to the emulation curve h(y) of the individual Ub, and new individuals Uc and Ud are generated. The contour T(y) of the pitch components of the new individuals Uc and Ud still inherits the contour T(y) of the pitch components of the original individuals Ua and Ub, respectively. In this way, two individuals are newly generated from two individuals. Ten pairs of individuals are selected in step SB3, so 10 pairs, that is, 20 individuals, are newly generated in step SB4.
另外,也可交叉俯仰成分之輪廓T(y),也可交叉仿效曲線h(y)和俯仰成分之輪廓T(y)之兩者。Alternatively, the contour T(y) of the pitch component may be crossed, or both the contour curve h(y) and the contour T(y) of the pitch component may be crossed.
若步驟SB4結束,則在步驟SB5中,選擇成為突然變異之對象之個體。作為一例,適合度高的10個個體除外,從剩餘之190個個體選擇80個。When the step SB4 ends, in step SB5, the individual who is the subject of the sudden mutation is selected. As an example, except for 10 individuals with high suitability, 80 are selected from the remaining 190 individuals.
於步驟SB6中,在選擇之個體上產生突然變異,生成新的個體。In step SB6, a sudden mutation occurs on the selected individual to generate a new individual.
參照圖7對突然變異之方法進行說明。在圖7顯示在步驟SB5中選擇之1個個體Ue。在個體Ue之仿效曲線h(y)重疊任意幅度及高度之高斯曲線,生成新的個體Uf。另外,也可在個體Ue之俯仰成分之輪廓T(y)重疊高斯曲線,也可在仿效曲線h(y)和俯仰成分之輪廓T(y)之兩方重疊高斯曲線。由於在步驟SB5中選擇了80個個體,因此在步驟SB6,新生成80個個體。The method of sudden variation will be described with reference to FIG. An individual Ue selected in step SB5 is shown in FIG. A new individual Uf is generated by superimposing a Gaussian curve of arbitrary amplitude and height on the emulation curve h(y) of the individual Ue. Alternatively, the Gaussian curve may be superimposed on the contour T(y) of the pitch component of the individual Ue, or the Gaussian curve may be superimposed on both the emulation curve h(y) and the contour T(y) of the pitch component. Since 80 individuals are selected in step SB5, 80 individuals are newly generated in step SB6.
於步驟SB7中,淘汰適合度低的個體。具體而言,在當這代200個個體中用新生成之100個體替換適合度低的100個個體。由此,決定新的一代200個個體。In step SB7, individuals with low fitness are eliminated. Specifically, 100 individuals with low fitness were replaced with newly generated 100 individuals in this generation of 200 individuals. Thus, a new generation of 200 individuals is determined.
於步驟SB8中,評估新一代200個個體而求出適合度。另外,對未在步驟SB7淘汰之上一代100個個體已計算適合度,所以沒有必要重新計算適合度。根據適合度排序新一代200個個體。In step SB8, a new generation of 200 individuals is evaluated to determine the fitness. In addition, the fitness has been calculated for the 100 individuals who have not eliminated the previous generation at step SB7, so it is not necessary to recalculate the fitness. Sort a new generation of 200 individuals according to fitness.
於步驟SB9中,判定世代數是否達到目標值,在未達到目標值時返回步驟SB3。在達到目標值時,在步驟SB10中,將最新一代個體中適合度最高的個體之仿效曲線h(y)及俯仰成分之輪廓T(y)作為最佳解。In step SB9, it is determined whether or not the generation number reaches the target value, and if the target value is not reached, the process returns to step SB3. When the target value is reached, in step SB10, the emulation curve h(y) of the most suitable individual among the latest generation individuals and the contour T(y) of the pitch component are taken as the optimal solution.
於圖8表示評估值之位移。橫軸表示世代數,縱軸表示在當這代個體中適合度最高的個體之評估函數之值(評估值)。可知隨著世代演變,評估值下降(適合度上升)。在2000代,評估函數之值下降到大約0.4μm2 。可知標準偏差成為0.63μm,得到充分之精度。而且,在500代左右,評估值收斂到90%程度,其後,根據最佳解之探索緩慢演變之情況,認為遺傳算法之各參數之設定也適當。The displacement of the evaluation value is shown in FIG. The horizontal axis represents the number of generations, and the vertical axis represents the value (evaluation value) of the evaluation function of the individual with the highest fitness among the generations. It can be seen that as the generation evolves, the evaluation value decreases (the fitness increases). In the 2000s, the value of the evaluation function dropped to approximately 0.4 μm 2 . It can be seen that the standard deviation is 0.63 μm, and sufficient accuracy is obtained. Moreover, in the case of about 500 generations, the evaluation value converges to 90%, and then, based on the slow evolution of the exploration of the optimal solution, it is considered that the parameters of the genetic algorithm are also appropriately set.
於圖9A表示適合度最高的個體之仿效曲線h(y)及俯仰成分之輪廓T(y)。縱軸表示h(y)及T(y)之值,h(y)之單位係[μm],T(y)之單位係[10μrad]。橫軸以單位[mm]表示y方向之位置。另外,仿效曲線h(y)及俯仰成分之輪廓T(y)之0次成分和1次成分與表面輪廓無關,所以在圖9A除去0次成分和1次成分而表示。 Fig. 9A shows the emulation curve h(y) of the most suitable individual and the contour T(y) of the pitch component. The vertical axis represents the values of h(y) and T(y), the unit of h(y) is [μm], and the unit of T(y) is [10 μrad]. The horizontal axis represents the position in the y direction in units of [mm]. Further, the zero-order component and the primary component of the contour curve h(y) and the contour T(y) of the pitch component are not related to the surface profile, and therefore, the zero-order component and the primary component are removed in FIG. 9A.
於圖9B表示由位移計31i、31j、31k測量之測量數據i(y)、j(y)、k(y)。橫軸以單位[mm]表示y方向之位置,縱軸以單位[μm]表示測量數據之值。另外,除去0次成分及1次成分。 The measurement data i(y), j(y), k(y) measured by the displacement meters 31i, 31j, 31k are shown in Fig. 9B. The horizontal axis represents the position in the y direction in units of [mm], and the vertical axis represents the value of the measurement data in units [μm]. In addition, the 0th component and the primary component were removed.
於圖9C表示將仿效曲線h(y)及俯仰成分之輪廓T(y)之最佳解代入到式(1)~(3)而求出之表面輪廓W1(y)、W2(y)、W3(y)。可知根據最佳解計算之3個表面輪廓與在圖9B所示之3個測量數據相比差小。 FIG. 9C shows the surface contours W 1 (y), W 2 (y) obtained by substituting the optimal solution of the simulation curve h(y) and the contour T(y) of the pitch component into the equations (1) to (3). ), W 3 (y). It can be seen that the three surface profiles calculated from the optimal solution are small compared to the three measurement data shown in FIG. 9B.
如此,藉由利用遺傳算法,不必直接解出包括3個未知函數之聯立方程式,可求出仿效曲線h(y)、俯仰成分之輪廓T(y)、及表面輪廓W(y)之最佳解。 Thus, by using the genetic algorithm, it is not necessary to directly solve the simultaneous equations including the three unknown functions, and the simulation curve h(y), the pitch component T(y), and the surface contour W(y) can be found. Good solution.
於上述遺傳算法中,由仿效曲線h(y)和俯仰成分之輪廓T(y)定義遺傳算法之候選解,根據表面輪廓W(y)定義評估函數。此外,也可以由仿效曲線h(y)、俯仰成分之輪廓T(y)、表面輪廓W(y)中2個輪廓定義候選解,也可由剩餘之1個輪廓定義評估函數。 In the above genetic algorithm, the candidate solution of the genetic algorithm is defined by the emulation curve h(y) and the contour T(y) of the pitch component, and the evaluation function is defined according to the surface contour W(y). Further, the candidate solution may be defined by two contours in the contour curve h(y), the contour T(y) of the pitch component, and the surface contour W(y), or the evaluation function may be defined by the remaining one contour.
於圖4之步驟SA5中,進行仿效曲線h(y)之2次成分之校正。如式(6)所示,不能夠從聯立方程式(1)~(3)確定仿效曲線h(y)之2次成分。因此,由遺傳算法求出之仿效曲線h(y)之最佳解之2次成分沒有意義 。從而,從藉由遺傳算法得到之仿效曲線h(y)之最佳解除去2次成分而求出僅包含3次以上之成分之仿效曲線h(y)。在僅包含該3次以上之成分之仿效曲線h(y)上,使在圖3A之步驟S2計算出之仿效曲線h(y)之2次成分重疊。由此,求出包含有意義之2次成分之仿效曲線h(y)。 In step SA5 of Fig. 4, the correction of the secondary component of the simulation curve h(y) is performed. As shown in the equation (6), the secondary component of the emulation curve h(y) cannot be determined from the simultaneous equations (1) to (3). Therefore, the second component of the optimal solution of the imitation curve h(y) obtained by the genetic algorithm has no meaning. . Therefore, the second-order component is removed from the optimum solution of the simulation curve h(y) obtained by the genetic algorithm, and the simulation curve h(y) containing only three or more components is obtained. On the emulation curve h(y) including only the three or more components, the second component of the emulation curve h(y) calculated in step S2 of Fig. 3A is superposed. Thus, an emulation curve h(y) containing a meaningful secondary component is obtained.
於步驟SA6中,藉由將在步驟SA5校正2次成分之仿效曲線h(y)、及位移計31j之測量數據j(y)代入到式(2),從而求出表面輪廓W(y)之2次以上之成分。另外,由於零點誤差δ係常數,所以,即使零點誤差δ未知,也能夠確定表面輪廓W(y)之2次以上之成分。 In step SA6, the surface contour W(y) is obtained by substituting the simulation curve h(y) for correcting the secondary component in step SA5 and the measurement data j(y) of the displacement gauge 31j into the equation (2). 2 or more ingredients. Further, since the zero point error δ is a constant, even if the zero point error δ is unknown, it is possible to determine the component of the surface contour W(y) twice or more.
朝x方向偏離活動工作臺10,藉由重複從圖4之步驟SA1到SA6之步驟,從而可測量測量對象物20整面之表面輪廓。即使朝x方向偏離活動工作臺10,可認定仿效曲線h(y)之2次成分也不變化。因此,在每朝著x方向偏離活動工作臺10時,不需要再執行由圖3A所示之傾斜儀進行之測量。而且,即使更換測量對象物20,也不需要再執行由傾斜儀進行之測量。 Deviating from the movable table 10 in the x direction, by repeating the steps from steps SA1 to SA6 of Fig. 4, the surface profile of the entire surface of the measuring object 20 can be measured. Even if the moving table 10 is deviated in the x direction, it can be considered that the secondary component of the emulation curve h(y) does not change. Therefore, when it is deviated from the movable table 10 in the x direction, it is not necessary to perform the measurement by the inclinometer shown in Fig. 3A. Moreover, even if the object 20 to be measured is replaced, it is not necessary to perform the measurement by the inclinometer.
由傾斜儀測量表面輪廓需要很多之功夫和時間,難以自動化。在根據實施例之方法中,藉由利用容易自動化之位移計之測量,可容易地測量測量對象物20之表面輪廓。 Measuring the surface contour by the inclinometer requires a lot of effort and time and is difficult to automate. In the method according to the embodiment, the surface profile of the measuring object 20 can be easily measured by using the measurement of the displacement meter which is easy to automate.
於上述實施例中,在零點誤差δ殘留時也可確定表面輪廓W(y)之2次成分。因此,沒有必要進行精密的零點調整。 In the above embodiment, the secondary component of the surface profile W(y) can also be determined when the zero point error δ remains. Therefore, there is no need for precise zero adjustment.
於上述實施例中,相對測量對象物20移動了位移計31i、31j、31k,但相反也可相對位移計31i、31j、31k移動測量對象物20。例如,在圖1A中,朝x方向排列位移計31i、31j、31k,一邊朝x方向移動測量對象物20一邊進行測量,從而可測量沿著測量對象物20表面之平行於x方向之測量對象線之表面輪廓。將圖1B所示之感測器頭30以平行於z軸之旋轉軸為中心旋轉90°,從而可以使位移計31i、31j、31k排列在x方向。也可以在感測器頭30設置這種旋轉機構。In the above embodiment, the displacement measuring instruments 20i, 31j, and 31k are moved relative to the measuring object 20, but the measuring object 20 can be moved relative to the displacement meters 31i, 31j, and 31k. For example, in FIG. 1A, the displacement meters 31i, 31j, and 31k are arranged in the x direction, and the measurement object 20 is moved while moving in the x direction, so that the measurement object parallel to the x direction along the surface of the measurement object 20 can be measured. The contour of the surface of the line. The sensor head 30 shown in Fig. 1B is rotated by 90° about the rotation axis parallel to the z-axis, so that the displacement meters 31i, 31j, 31k can be arranged in the x direction. It is also possible to provide such a rotating mechanism in the sensor head 30.
藉由重疊沿著平行於y方向之多個測量對象線之表面輪廓、和沿著平行於x方向之多個測量對象線之表面輪廓,可得到測量對象物20表面之2維表面輪廓資訊。The two-dimensional surface contour information of the surface of the measuring object 20 can be obtained by overlapping the surface contours of the plurality of measuring object lines parallel to the y direction and the surface contours of the plurality of measuring object lines parallel to the x direction.
根據以上實施例說明了本發明,但本發明不限於這些。熟悉本案技術之人士當然理解例如可進行各種變更、改良、組合等。The present invention has been described based on the above embodiments, but the present invention is not limited to these. Those skilled in the art will understand, for example, that various modifications, improvements, combinations, and the like can be made.
10...活動工作臺10. . . Activity workbench
11...工作臺導向機構11. . . Workbench guiding mechanism
15...研磨頭15. . . Grinding head
16...砂輪16. . . Grinding wheel
18...導軌18. . . guide
19...控制裝置19. . . Control device
20...測量對象物20. . . Measuring object
30...感測器頭30. . . Sensor head
31i、31j、31k...位移計31i, 31j, 31k. . . Displacement meter
35...傾斜儀35. . . Inclinometer
圖1之(1A)係根據實施例之直線性測量裝置之透視圖,(1B)係感測器頭部分之概略圖。Fig. 1 (1A) is a perspective view of a linear measuring device according to an embodiment, and (1B) is a schematic view of a head portion of the sensor.
圖2係表示測量對象物之表面輪廓W(y)、位移計之測量數據i(y)、j(y)、k(y)、仿效曲線h(y)、及俯仰成分T(y)之定義之線圖。2 is a view showing a surface contour W(y) of the object to be measured, measurement data i(y), j(y), k(y) of the displacement meter, a simulation curve h(y), and a pitch component T(y). A line graph of the definition.
圖3之(3A)係表示事先測量仿效曲線之2次成分之方法之流程圖,3(B)係表示由傾斜儀測量表面輪廓之樣子之概略圖。Fig. 3 (3A) is a flow chart showing a method of measuring the secondary component of the simulation curve in advance, and Fig. 3 (B) is a schematic view showing the appearance of the surface profile by the inclinometer.
圖4係根據實施例之直線性測量方法之流程圖。4 is a flow chart of a linear measurement method according to an embodiment.
圖5係根據實施例之直線性測量方法中採用之遺傳算法之流程圖。Fig. 5 is a flow chart of a genetic algorithm employed in the linearity measuring method according to the embodiment.
圖6係用於說明由遺傳算法進行之交叉之圖。Figure 6 is a diagram for explaining the intersection of genetic algorithms.
圖7係用於說明由遺傳算法進行之突然變異之圖。Figure 7 is a diagram for explaining the sudden variation by the genetic algorithm.
圖8係表示藉由遺傳算法,評估值隨著世代增加而減小(適合度變高)之情況之圖表。Fig. 8 is a graph showing a case where the evaluation value is decreased (the fitness becomes higher) as the generation value increases by the genetic algorithm.
圖9之(9A)係表示由遺傳算法求出之仿效曲線h(y)及俯仰成分T(y)之最佳解之圖表,(9B)係表示3個位移計之測量數據之圖表,(9C)係表示運用藉由遺傳算法求出之最佳解時表面輪廓之圖表。Fig. 9 (9A) is a graph showing the best solution of the simulation curve h(y) and the pitch component T(y) obtained by the genetic algorithm, and (9B) is a graph showing the measurement data of the three displacement meters, ( 9C) is a graph showing the surface profile of the best solution obtained by genetic algorithm.
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